8/14/19 8900.1 CHG 674
CHAPTER
4 PART 129 OPERATIONSAdvisory Circulars (AC) referenced throughout this section provide guidance for compliance with specific regulations. They define acceptable means, but not the only means, of accomplishing or showing compliance with regulations.
Principal Operations Inspectors (POI). POIs assigned to evaluate an EFVS application are responsible for managing the evaluation process, coordinating the review and evaluation of the submitted EFVS application with other assigned PIs and ASIs, initiating FAA internal coordination when required, and issuing the authorization.
The Flight Technologies and Procedures Division. The Flight Technologies and Procedures Division is responsible for providing the technical and policy support and consultation to the ASIs conducting the application evaluation and coordinating with other FAA divisions, as applicable.
IFOs.
IFOs must initiate coordination with the Flight Technologies and Procedures Division EFVS Focal Point when an applicant presents a means to obtain EFVS authorization that is not described in AC 90-106, Enhanced Flight Vision Systems.
IFOs must ensure that all information and documentation recommended in AC 90-106 are addressed in the foreign air carrier’s submission.
Resources.
The following are the primary references for ASIs conducting an
EFVS application evaluation:AC 90-106. AC 90-106 describes EFVS operations, information, and documentation. ASIs must use the AC as the primary reference to help determine if foreign air carriers have met FAA expectations during the evaluation of an application.
Volume 12, Chapter 4, Section 4. ASIs must use this as a general guideline for conducting the evaluation of an application.
International Civil Aviation Organization (ICAO) Annex 6, Part I, Attachment H, Automatic Landing Systems, Head-Up Display (HUD) or Equivalent Displays and Vision Systems (EVS). The attachment contains ICAO guidance for EFVS.
Airplane Flight Manual (AFM)/Rotorcraft Flight Manual (RFM) or AFM Supplement (AFMS)/RFM Supplement (RFMS). The AFM/RFM contains information pertaining to the certification of an EFVS.
The Flight Technologies and Procedures Division EFVS Focal Point. This is the policy division for EFVS and foreign air carrier authorizations. ASIs should contact the EFVS Focal Point listed on the following Flight Technologies and Procedures Division Flight Operations Group web page for technical support or when directed by guidance: https://www.faa.gov/about/office_org/headquarters_offices/avs/offices/afx/afs/afs400/afs410/efvs/.
AFM(S)/RFM(S)
provisions for EFVS. Foreign-registered airplanes used by a
foreign air carrier for EFVS operations within the United
States must have AFM(S) provisions reflecting an appropriate
level of EFVS capability that meets the display, features, and
requirements of § 91.176.
Figure 4-4A. Sample C048 Table 1 – Authorized Airplanes, Equipment, and EFVS Operations
Airplane (M/M/S) |
EFVS System/Sensor |
EFVS Operation(s) |
EFVS Operational Credit |
[With sub-list attribute] |
[Dropdown List] |
[Dropdown List] |
[Dropdown List] |
Only airplanes from a foreign air carrier’s aircraft list in WebOPSS assigned an EFVS authorization will populate the dropdown list provided in the “Airplane (M/M/S)” column in Table 1. To add the EFVS authorization to an airplane, go to “CHDO” – “Maintain Operator Data” – “Aircraft,” select the foreign air carrier’s airplane to edit, and add “EFVS” to the “Authorizations” section.
Completed
the foreign air carrier’s approved EFVS training; and
Been qualified for EFVS operations by one of the foreign air carrier’s check pilots or a CAA inspector from the State of the Operator.
Each foreign air carrier operating within the United States in common carriage must ensure they are in compliance with all U.S. regulatory requirements, including more restrictive foreign air carrier operating requirements levied by the State of the Operator.
Before
authorizing a type of IAP, the POI must ensure the foreign air
carrier has established the aircraft system eligibility and
that its manual, which the State of the Operator must have
approved/accepted, includes both flightcrew training and
procedures, as applicable, for the types of approaches
authorized.Direct all questions regarding the issuance of C052 to the International Program Division or the Flight Technologies and Procedures Division.
An RNP APCH typically addresses only the requirement for the lateral navigation (LNAV) aspect (2D navigation) along straight segments. RNP APCHs that contain a curved segment (Radius to Fix (RF) leg), FAS specifying less than 0.3 nautical miles (NM) accuracy, or a Missed Approach Segment (MAS) that specifies less than 1.0 NM accuracy, require more rigorous equipment qualification and training so Special Authorization is required. These are referred to as RNAV RNP IAP with Authorization Required (AR) or RNP AR approaches.
C052 does not authorize RNP AR operations. Authorization for RNAV RNP AR approaches is through nonstandard OpSpec C384 (refer to AC 90-101, Approval Guidance for RNP Procedures With AR).
Three
groups of IAPs may be authorized in Table 1 of C052:Column One: Nonprecision Approach Procedures Without Vertical Guidance. Foreign air carriers must ensure the aircraft will not go below the MDA without the required visual references specified in § 91.175.
The ICAO term for an airport surveillance radar (ASR) approach is “surveillance radar approach (SRA).”
Belgium labels these approaches as “SRE.” Select “ASR/SRA/SRE” in column one to authorize these approaches.
Column Two: Approaches with Vertical Guidance (APV). Column two provides for the authorization of APV. These approaches provide vertical guidance, but do not meet the same standards as precision approach systems (e.g., instrument landing systems (ILS) and Ground Based Augmentation Systems (GBAS)). APVs are trained using an approved method that allows descent to a published DA.
APV approaches may contain localizer performance with vertical guidance (LPV) minima requiring wide area augmentation system (WAAS) and LNAV/vertical navigation (VNAV) minima. The approaches may be flown with either barometric vertical navigation (baro‑VNAV) or WAAS-based VNAV (refer to C052 subparagraph c to determine applicable lines of minima). The AIM and the approach chart legend also have this information.
Aircraft accomplishing RNP APCHs (RNAV (GPS) or RNAV Global Navigation Satellite Systems (GNSS)) are required to monitor lateral and, if approved for operational credit, vertical guidance deviations. For baro-VNAV approach operations on an RNP APCH using the LNAV/VNAV minima, the current vertical deviation limits are +100/‑50 feet (ft). Aircraft qualified using the deviation display requirements for navigation in AC 20-138, Airworthiness Approval of Positioning and Navigation Systems, may use a vertical deviation limit of ±75 ft (or a smaller value). This information must be published in the AFM or a Supplemental Type Certificate (STC), or verified by the Aircraft Evaluation Group (AEG).
To authorize RNAV APVs, select “RNAV (GPS)” (for part 97 approaches) or “RNAV (GNSS)” (for foreign approaches) from the dropdown list in column two of the OpSpec C052 template Table 1.
Column Three: Precision Approach Procedures (ILS & GLS). Column three provides for the authorization of CAT I precision IAPs from an electronic glideslope (GS) (ILS or GBAS Landing System (GLS)).
“RNAV/ILS” in column three may be selected only if the foreign air carrier meets the requirements in OpSpec C063.
For
pilot qualifications, the initial qualification segment of
the foreign air carrier’s approved precision runway
monitor (PRM) training program must be successfully completed
prior to conducting PRM approach and landing operations.
Initial training materials must include published PRM
approach chart materials, the AIM, related Notices to Airmen
(NOTAM), and the latest available FAA-produced and approved
PRM PowerPoint presentation entitled, “Precision Runway
Monitor (PRM) Pilot Procedures,” that each pilot must
view, and which appears on the FAA website at
http://www.faa.gov/training_testing/training/prm/.
Pilots trained in PRM operations under previous guidance are not required to retrain using the new PRM PowerPoint training. However, pilots are required to know the change in the “Attention All Users Page” format, understand the flight management computer (FMC) coding of a simultaneous offset instrument approach (SOIA) RNAV and how that coding affects the conduct of a missed approach. Testing of knowledge objectives is required as part of initial and recurrent qualification training. See subparagraph i).
Figure 4-4B. Sample C052 Table 1 – Authorized Instrument Approach Procedures
Nonprecision Approaches Without Vertical Guidance |
Approaches With Vertical Guidance (APV) |
Precision Approach Procedures (ILS & GLS) |
ASR/SRA/SRE |
LDA with glideslope |
ILS |
AZI |
RNAV (GPS) |
PAR |
AZI/DME |
RNAV (GNSS) |
ILS/DME |
AZI/DME/BC |
SDF with glideslope |
RNAV/ILS |
GPS |
LOC BC with glideslope |
GLS |
LDA |
|
|
LDA/DME |
|
|
LOC |
|
|
LOC BC |
|
|
LOC/DME |
|
|
NDB |
|
|
NDB/DME |
|
|
RNAV (GPS) |
|
|
VOR/DME RNAV |
|
|
SDF |
|
|
TACAN |
|
|
VOR |
|
|
VOR/DME |
|
|
LOC/BC/DME |
|
|
GPS
Authorization. Volume 4, Chapter 1, Section 2 provides more
extensive guidance on GPS and GPS WAAS equipment. The applicant
must show that it has the ability to safely conduct GPS
operations.The titles of all remaining GPS overlay procedures have been revised on the approach charts to read “…or GPS” (e.g., “VOR or GPS RWY 24”). Therefore, all the approaches that can be used by GPS now contain “GPS” in the title (e.g., “VOR or GPS RWY 24,” “GPS RWY 24,” or “RNAV (GPS) RWY 24”). During these GPS approaches, underlying ground-based NAVAIDs are not required to be operational and associated aircraft avionics need not be installed, operational, turned on, or monitored (although monitoring of the underlying approach is suggested when equipment is available and operational).
Existing overlay approaches may be requested using the GPS title. For example, request “GPS RWY 24” to fly the very high frequency (VHF) omni-directional range (VOR) or GPS RWY 24 approach.
VOR/distance measuring equipment (DME) RNAV approaches will continue to be identified as VOR/DME RNAV RWY [Number] (e.g., VOR/DME RNAV RWY 24). VOR/DME RNAV procedures which can be flown by GPS will be annotated with “or GPS” (e.g., VOR/DME RNAV or GPS RWY 24).
Some approach-certified receivers will only support a glidepath with performance similar to baro-VNAV, and are authorized to fly the LNAV/VNAV line of minima on the RNAV (GPS) approach charts.
Receivers with additional capability, such as update rate and integrity limits, are authorized to fly the LPV or Localizer Performance (LP) line of minima. WAAS approach procedures may provide LPV, LNAV/VNAV, LP, and LNAV minimums and are charted as RNAV (GPS) RWY [Number] (e.g., RNAV (GPS) RWY 24). For further guidance, please refer to the AIM or contact the Flight Technologies and Procedures Division.
Some WAAS installations do not support approaches at all, while some do not support LPV or LP lines of minima.
Local
Area Augmentation System (LAAS). An additional augmentation
system, the LAAS was developed to provide precision approaches
similar to ILS at airfields. These precise approaches are based
on GPS signals augmented by ground equipment. The international
term for LAAS is GBAS and the approaches which use the
equipment are referred to as GBAS Landing System (GLS) or GNSS
Landing System (GLS) approaches. LAAS equipment consists of a
GBAS Ground Facility (GGF) supported by a minimum of four
accurately surveyed reference stations and an uplink antenna
called the VHF Data Broadcast (VDB) antenna, as well as an
aircraft LAAS receiver. The GGF can support multiple runway
ends or landing areas served by procedures that are within the
service coverage.Throughout this section, reference to a GLS approach indicates the use of a GBAS or GNSS Landing System, unless otherwise indicated.
Similar to LPV and ILS approaches, GLS provides lateral and vertical guidance. By design, LAAS was developed as an “ILS look-alike” system from the pilot perspective. Unlike WAAS, LAAS may support approaches to CAT III minimums in the future due to its nearly identical performance standards to ILS in terms of accuracy, integrity, availability, and continuity. Portions of the GLS approach prior to and after the FAS may be based on RNAV or RNP segments. Therefore, a switch transition between RNAV or RNP and GLS modes may be required. In the future, the GGF may be able to support portions of the procedure outside the FAS.
There are differences from LPV, GLS, and ILS approaches in terms of charting, procedure selection, and identification. The LAAS procedure is titled “GLS RWY XX” on the approach chart. In the aircraft, pilots selects a five-digit GBAS channel number or associated approach within the flight management system (FMS) menu. Selection of the GBAS channel number by pilot or FMS also tunes the VDB. The VDB provides information to the airborne receiver where the guidance is synthesized. The LAAS procedure is identified by a four alpha‑numeric character field referred to as the Reference Path Indicator (RPI) or approach ID. This identifier is analogous with the IDENT feature of the ILS. The RPI is charted. Following procedure selection, confirmation that the correct LAAS procedure is loaded is accomplished by cross-checking the charted RPI with the cockpit-displayed RPI or audio identification of the RPI with Morse code (for some systems). Once selected and identified, the pilot will fly the GLS approach using the same techniques as an ILS.
All
published Standard Instrument Approach Procedures (SIAP) in the
United States meet this requirement.When electronic or a pre-stored computed vertical guidance is not used, Vertical Speed (VS) or Flight Path Angle (FPA) may be used to achieve a CDFA profile.
Compared to the “step down” descent approach technique, where the aircraft descends step-by-step prior to the next minimum altitude, a CDFA technique has safety and operational advantages, such as standardization of procedures, simplification of the decision process (one technique and one decision at one point), and use of a stable flightpath. However, precision approach (ILS, GLS) obstacle penetration is not provided.
Reduced
Precision CAT I Landing Minima. OpSpec C052 specifies the
equipment usage requirements and part 97 SIAP depiction required
for reduced CAT I landing minima. Credit is given for flight
director (FD), autopilot, and HUD usage. The POI should allow
the use of 1800 RVR minima to runways without centerline
(CL) lighting or TDZ lighting, provided the SIAP contain a
straight-in ILS minimum with the chart note, “RVR 1800
Authorized with use of FD or autopilot or HUD to DA.”
Additionally, the foreign air carrier issued C052 is allowed to
continue to use 1800 RVR line of minima on SIAPs without the
above procedural note when the TDZ and/or CL lights are
inoperative, if the approach is conducted in accordance with the
equipment requirements outlined in C052. This is reflected in
the published inoperative components table for IAPs.Aircraft and Associated Aircraft Systems. The authorized aircraft must be equipped with an FD, autopilot, or HUD that provides guidance to DA. The FD, autopilot, or HUD must be used in approach mode (e.g., tracking the Localizer (LOC) and the GS). ASIs must establish that the FD, autopilot, or HUD are certified for use down to an altitude of 200 ft above ground level (AGL) or lower.
Flightcrew Procedures.
The flightcrew must use the FD, autopilot, or HUD to DA or to the initiation of a missed approach, unless visual references with the runway environment are established, thus allowing safe continuation to a landing.
If the FD, autopilot, or HUD malfunctions or becomes disconnected, the flightcrew must execute a missed approach unless the runway environment is in sight.
Flightcrew Qualification. Each member of the flightcrew must have demonstrated proficiency using the FD, autopilot, or HUD (as appropriate) in the foreign air carrier’s training program, which is approved by their CAA.
Training
Requirements. The flightcrew must be current and qualified for
CAT II operations. Each member of the flightcrew must have
demonstrated proficiency using the HUD in the foreign air
carrier’s training program approved by their CAA. This
requirement applies both to initial eligibility for Special
Authorization CAT I as well as recurrent training.The flightcrew must use the HUD to DH in a mode used for CAT II or CAT III operations. This mode provides greater lateral and vertical flightpath accuracy and more sensitive alarm limits.
The flightcrew must use the HUD to DH, or to the initiation of missed approach, unless adequate visual references with the runway environment are established that allow safe continuation to a landing. Should the HUD malfunction during the approach, the flightcrew must execute a missed approach unless visual reference to the runway environment has been established.
The crosswind component on the landing runway must be 15 knots or less, unless the AFM’s crosswind limitations are more restrictive.
The part 97 SIAP must have a published Special Authorization CAT I minimum.
Unlike the other approaches authorized in C052, the mid-RVR report may not be substituted for the TDZ RVR report when using Special Authorization CAT I minima.
Where parallel RCLs are less than 4,300 ft apart, but not less than 3,000 ft apart, simultaneous PRM approaches may be conducted. Similarly, where parallel RCLs are less than 3,000 ft apart, but no less than 750 ft, SOIA may be conducted using an ILS, LDA approach with GS, LNAV/VNAV, or LPV. Those approaches are labeled “ILS PRM” and “LDA PRM,” respectively, on instrument approach charts. Air traffic control (ATC) provides one PRM monitor controller for each runway to provide intrusion protection for the no transgression zone (NTZ), located between the two final approach courses. Whenever the runway spacing (or in the case of SOIA the approach course spacing) is less than 3,600 ft and at least 3,000 ft, NTZ monitoring is accomplished using a special PRM radar.
Utilization of vertical guidance is required for all PRM approaches.
RNAV (GPS) PRM approaches may be substituted for the ILS PRM and/or the LDA PRM approach.
Pilots
must have completed PRM training prior to conducting any PRM
approach.
An ILS PRM and its overlaid RNAV (GPS) PRM approach are procedurally equivalent.
LDA PRM and its overlaid RNAV (GPS) PRM approach are procedurally equivalent.
Pilots may request the RNAV (GPS) PRM approach in lieu of the ILS PRM or LDA PRM approach; however, they may only conduct the approach when specifically cleared to do so by ATC.
Traffic Alert. One important element of the additional training is the pilot understands the difference between a normal missed approach initiated by a pilot and a breakout initiated by a PRM final monitor controller. It must be clear to flightcrews that when the final monitor controller uses the words “Traffic Alert,” the controller will then give critical instructions that the pilot must act on promptly to preserve adequate separation from an airplane straying into the adjoining approach path.
ATC Breakout Maneuver Command to Turn and Either a Climb or Descent. The flightcrew must immediately follow the final monitor controller’s vertical (climb/descend/maintain altitude) and horizontal (turn) commands. If the flightcrew is operating the Traffic Alert and Collision Avoidance System (TCAS) in the Traffic Advisory (TA)/Resolution Advisory (RA) mode and receives a TCAS RA at any time while following the final monitor controller’s command, the flightcrew will simultaneously continue to turn to the controller’s assigned heading and follow the vertical guidance provided by the TCAS RA.
Time-to-Turn Standard. Regardless of airplane type, tests and data analysis revealed that pilots normally passed through an angle of bank of at least 3 degrees while rolling into a breakout turn within 10 seconds of receiving a breakout command. (Bank angles of between 20 and 30 degrees were normally achieved during the breakout.) The foreign air carrier must show that its CAA has determined that pilots can readily meet this time-to-initiate-turn standard prior to the POI authorizing ILS/PRM, LDA/PRM, or RNAV (GPS) PRM approaches in C052.
Flightcrews are required to manually fly the breakout maneuver unless otherwise approved.
The foreign air carrier should demonstrate its ability to meet this standard by having representative pilots perform the breakout maneuver while the POI or the POI’s designated representative observes.
The
demonstration should conform to procedures contained in the
foreign air carrier’s approved operating manual for its
flightcrews.
The foreign air carrier should submit procedures to its POI for this authorization.
In a breakout, ATC will never command a descent below the applicable minimum vector altitude (MVA), thus ensuring that no flight will be commanded to descend below 1,000 ft above the highest obstacle during a breakout.
ATC Command to Turn With TCAS RA. In the unlikely event that a flightcrew should simultaneously receive a final monitor controller’s command to turn and a TCAS RA, the flightcrew must follow both the final monitor controller’s turn command and the TCAS RA’s climb or descent command.
TCAS RA Alone. In the extremely unlikely event that an RA occurs without a concurrent breakout instruction from the final monitor controller, the pilot should follow the RA and advise the controller of the action taken as soon as possible. In this instance, it is likely that a breakout command would follow.
TCAS Not Required. An operator does not need an operative TCAS to conduct ILS/PRM, LDA/PRM, or RNAV (GPS) PRM approaches.
Initial ground training—required.
This training must include all elements of the “Attention All Users Page” of an ILS/PRM, LDA/PRM, or RNAV (GPS) PRM as authorized, along with viewing the latest version of the PRM training PowerPoint presentation. (For the most current version, visit http://www.faa.gov/training_testing/training/prm/.)
The FAA does not require flightcrews trained previously in PRM operations under earlier guidance to requalify with each new version of the PRM training PowerPoint presentation.
The
ground portion of the training program must support the
following knowledge objectives. Each flightcrew member must:
Describe the PRM system to include the meaning of “no transgression zones.”
Know that an airplane on an adjacent approach path may be less than 4,300 ft away and may be flying at a different speed.
Know that the Automated Terminal Information Service (ATIS) broadcasts a pilot advisory when ILS/PRM, LDA/PRM, or RNAV (GPS) PRM approaches are in progress.
Identify the differences between PRM approach charts and normal approach charts, including the special instruction pages for PRM.
Explain the unique communication requirements (equipment and procedures) for ILS/PRM, LDA/PRM, and RNAV (GPS) PRM approaches.
Know that an unpublished missed approach instruction that ATC may issue prior to published MAPs is called a “breakout.”
Know that a breakout may include instructions to descend and that the descent will be to no lower than the MVA for the sector. The MVA guarantees 1,000 ft above the highest obstruction in that sector. The rate of descent that controllers expect is not more than 1,000 ft per minute.
Know that a pilot must initiate a breakout maneuver manually and immediately upon hearing the “Traffic Alert” command from ATC, and that adequate separation requires that the pilot establish a 3-degree-per-second rate of turn within 8 seconds.
Know that the three areas (ATIS, Dual VHF Comm. Required, and All “Breakouts”) in the “Attention All Users Page” must be briefed (in flight) prior to conducting an ILS/PRM, LDA/PRM, or RNAV (GPS) PRM approach.
Know that flightcrews may operate the TCAS in the TA/RA mode when conducting PRM approaches, including the following points:
When an RA occurs with a concurrent ATC breakout command—follow the turn required in the ATC instructions; follow the climb or descent in the RA command (split commands);
When an RA occurs without a concurrent ATC breakout command—follow the RA and contact ATC as soon as practical;
TCAS provides only vertical resolution to aircraft conflicts; and
An operative TCAS is not required for PRM operations.
Know
procedures for SOIAs, including the following points:
A visual segment of the LDA/PRM or the offset RNAV (GPS) PRM approach is established beginning at the offset approach MAP to permit;
Visual acquisition of the traffic to the parallel runway and advising ATC;
Visual acquisition of the runway environment;
LDA PRM or the offset RNAV (GPS) PRM course is maintained until the MAP. At the MAP, the pilot must have the parallel traffic in sight and the runway environment in sight, or fly the missed approach;
At the MAP with the parallel traffic and the runway in sight, the pilot may continue to a landing;
Maneuver to align with the RCL;
Stabilize on glidepath no lower than 500 ft above TDZ; and
Avoid wake turbulence from the parallel runway traffic.
Testing of these knowledge objectives is recommended.
Initial flight training—required.
Breakout maneuver—required.
Initial breakout flight training must focus on the descending breakout.
Foreign air carriers applying for initial approval to conduct PRM approaches must complete breakout flight training by the end of the next full training cycle after receiving OpSpec approval. The FAA does not require duplicative flight training in breakout maneuvers between the types of PRM approaches. Breakout covered in flight training for one type of PRM satisfies the requirement for all other types of PRM approaches.
Recurrent ground training—required: Review of the ground training elements and the Precision Runway Monitor (PRM) Pilot Procedures slideshow (for additional details, see subparagraphs b)5)c3 and i)4)).
Recurrent flight training.
Required: None.
Recommended:
ILS/PRM approach,
LDA/PRM approach, and
Breakout.
That foreign air carrier meets the ground and flight training requirements contained in subparagraph i)4); and
The CAA for the foreign air carrier authorizes these types of approaches.
A definition of RNAV (GPS) PRM has been added to the A002 template.
Questions regarding the issuance of C055 should be directed to the Flight Technologies and Procedures Division or the International Program Division. If the PI directs questions to the International Program Division, the PI should copy the Flight Technologies and Procedures Division and vice versa.
Airports
With at Least One Operational Navigational Facility. The first
part of the table in C055 is for airports with at least one
operational navigational facility providing a straight-in
Nonprecision Approach (NPA) procedure, a straight-in precision
approach procedure, or, when applicable, a circling maneuver
from an IAP. Obtain the required ceiling and visibility by
adding 400 ft to the MDA/minimum descent height (MDH) or, when
applicable, the authorized DA/H and by adding 1 statute mile
(sm) or 1,600 meters (m) to the authorized landing minimum.
The
following are some, but not all, of those requirements. Refer
to the criteria in AC 120-28 for further requirements.The aircraft is capable of engine inoperative CAT III.
The carrier has established appropriate procedures.
Performance and obstruction clearance information has been provided to the flightcrew.
Appropriate aircraft configuration, wind limits, and other appropriate information is provided to the flightcrew.
The ICAO equivalent to AC 120-28 is ICAO Doc 9365/AN910, Manual of All‑Weather Operations.
The aircraft is suitably equipped with GPS WAAS equipment; and
The foreign air carrier is authorized to conduct LPV and/or LP approach and landing operations by the State of the Operator.
When
using WAAS at an alternate airport, flight planning must be
based on flying the RNAV (GPS) LNAV minimums line, minimums on
a GPS approach procedure, or conventional approach procedure
with “or GPS” in the title.RNAV (GPS) (or RNAV GNSS) are based on a single navigational facility when determining the approach facility configuration in Table 1 of C055, even if there are two or more RNAV (GPS) approaches to different suitable runways.
The FAA is removing the “NA” (alternate minimums not authorized) symbol from select RNAV (GPS) and GPS approach procedures so they may be used by approach approved WAAS receivers at alternate airports. Some approach procedures will still require the NA for other reasons (e.g., no weather reporting); therefore, it cannot be removed from all procedures. Every procedure is individually evaluated for removal of NA from RNAV (GPS) and GPS procedures.
The first selectable text option states requirements for CAT II and CAT III credit applicable to alternate airport flight planning, and must be loaded if the operator is authorized the CAT II or CAT III credit described in subparagraph i)1) above.
The second selectable text option authorizes operators equipped with WAAS to use GPS approaches when determining an alternate, and lists the restrictions associated with using GPS approaches in alternate planning.
The third selectable text option authorizes both (the air carrier is authorized CAT II or III and GPS/WAAS alternate minimums).
OPSPEC
C056—IFR TAKEOFF MINIMUMS—AIRPLANES (OPTIONAL).
Figure 4-4C. Sample C056 Table 1
Lowest RVR in Feet (TDZ/MD/Rollout) |
Airplane Type* |
HUD System* |
Additional Limitations and Provisions* |
TDZ 1800 TDZ 1600 TDZ 2600 TDZ 5000 1200/1200/1200 1000/1000/1000 700/700/700 600/600/600 500/500/500 300/300/300 |
ALL** |
N/A*** |
N/A**** |
*The last three columns have space for manual entry.
**If the foreign air carrier operates all M/M/S aircraft to the same RVR value, then select “ALL.” Otherwise, identify each M/M/S for each RVR value in separate row(s), as appropriate. Examples:
i. If the foreign air carrier operates all M/M/S aircraft to TDZ 1600, then select “TDZ 1600” in the “Lowest RVR” column and “ALL” in the “Airplane Type” column.
ii. If the lowest RVR authorized for the foreign air carrier’s aircraft is the same for all except one type, then select the RVR value that is common to all and in the “Airplane Type” column enter: “All airplane types except for [enter the M/M/S exception].” In a separate row, identify the lowest RVR value for the M/M/S exception.
iii. If the foreign air carrier operates several M/M/S aircraft, each with a different RVR, then enter each M/M/S in its own separate row.
***Select “N/A” if the HUD is not authorized for takeoff. If the HUD system is authorized, then type in the HUD system.
****Select “N/A” if no limitations apply and use of the HUD is not authorized for takeoff. Select the blank space and type in any additional limitations not covered by C056.
An example of a limitation: authorized for the B737-800 to 500/500/500, but when using the HUD on the B737-800 limited to 600/600/600. This may be a limitation provided by the CAA if the HUD is new.
Additionally,
the POI must select:The static text in C056 subparagraphs c(3) and e, if the foreign air carrier is operating airplanes with a seating configuration of 30 certificated seats or less or a maximum payload capacity of 7,500 pounds or less.
The radio button specifying the limitations and requirements applicable to the lowest RVR value selected in the table in C056 subparagraph b. Select the radio button that included all of the selectable text, up to and including the lowest RVR value based on the lowest RVR value selected in the table in subparagraph b. The POI must preview the template to ensure that they have selected the correct radio button. If the lowest RVR value in the table is less than 1800, then select as follows:
The first radio button if in the table the lowest RVR selected is TDZ 1600. When previewing the template, the POI would see subparagraphs d(1) and d(2).
The second radio button if in the table the lowest RVR selected is TDZ 1200. When previewing the template, the POI would see subparagraphs d(1), d(2), d(3), and d(4).
The third radio button if in the table the lowest RVR selected is TDZ 1000. When previewing the template, the POI would see subparagraphs d(1), d(2), d(3), d(4), and d(5).
The fourth radio button if in the table the lowest RVR selected is TDZ less than 1000 ft, up to and including 500 ft. When previewing the template, the POI would see subparagraphs d(1), d(2), d(3), d(4), d(5), and d(6).
The fifth radio button if in the table the lowest RVR selected is TDZ less than 500 ft, up to and including 300 ft. When previewing the template, the POI would see subparagraphs d(1), d(2), d(3), d(4), d(5), d(6), and d(7).
See Table 4-4A, Runway Equipment Requirements for Takeoff Minima, for a graphical presentation of requirements covered by C056.
Table 4-4A. Runway Equipment Requirements for Takeoff Minima
Runway Visual Aid Required |
Lowest Allowable Takeoff Minimum Authorization [visibility or RVR (TDZ/Mid/Rollout)] |
Adequate visual reference, or Any one of the following: - Centerline (CL) lighting - High Intensity Runway Light (HIRL) - Runway centerline marking (RCLM) |
RVR not available; 1/4 mile (mi) (500 meters (m)); or RVR 1600 feet (ft) (500 m)/Not Required/Not Required. (Mid-point can substitute for an unavailable touchdown.) |
Note: Below RVR 1600, two operating RVR sensors are required. All operating RVR sensors are controlling (except per the note below for far-end sensors). Extremely long runways (e.g., Denver International Airport (DEN) 16R) utilize four RVR sensors (i.e., TDZ, mid, rollout, and far-end). When a fourth far-end RVR value is reported, it is not controlling and is not to be used as one of the two required operative RVR sensors. Visual aids (CL lighting, RCLM) must be visible (e.g., not obstructed by snow). |
|
Day: CL lighting or HIRL or RCLM Night: CL lighting or HIRL |
RVR 1200 ft (350 m)/1200 ft (350 m)/1000 ft (300 m) |
RCLM and HIRL, or CL lighting |
RVR 1000 ft/1000 ft/1000 ft (300 m) |
HIRL and CL lighting |
RVR 600 ft/600 ft/600 ft (175 m) or RVR 500 ft/500 ft/500 ft (150 m) |
With an approved HUD takeoff guidance system, HIRL, and CL lighting |
RVR 300 ft/300 ft/300 ft (75 m) |
Note: Additionally, RVR 300 ft/300 ft/300 ft (75 m) takeoff is conducted on a runway with a published landing minimum of RVR 300 and Localizer (LOC) front course guidance displayed on the HUD. |
|
OPSPEC
C060—CATEGORY II AND CATEGORY III INSTRUMENT APPROACH AND
LANDING OPERATIONS—U.S. AIRPORTS (OPTIONAL). The FAA
authorizes CAT II and CAT III operations by issuing OpSpec C060. Each
airplane type M/M/S used in CAT II or CAT III operations must be
listed in C060 Subparagraph b, Authorized Approach and Landing
Minimums, along with the DH/alert height (AH), and lowest RVR
authorized. Foreign air carriers requesting authorization for CAT II
or CAT III operations at U.S. airports should meet the following
criteria.The FAA evaluates CAT II and CAT III operations in accordance with AC 120-28, AC 120-29, equivalent European Aviation Safety Agency (EASA) criteria, or ICAO Doc 9365/AN910.
CAT II or CAT II/III approved airplane M/M/S (see subparagraph c) below),
Approach and landing systems used (see subparagraph d)),
Operational minimums (see subparagraph e)), and
Special equipment or limitations (see subparagraph f)).
Figures 4-4D and 4-4E below illustrate the standard approach/landing system and landing minimums entries used in C060 Table 1 for CAT II and Table 2 for CAT III authorizations.
Figure 4-4D. Sample C060 Table 1 – CAT II Airplane Systems and Landing Minimums
Airplane M/M/S |
Approach/Landing System* |
DH |
TDZ/Mid/RO RVR |
Special Operational Equipment and Limitations |
|
Autopilot HUD FP HUD Autoland |
150 DH 100 DH |
1600/600/300 1200/600/300 1000/600/300 |
|
* The term HUD assumes Manual HUD, HUD = CAT II certified Head-Up Display; FP HUD = CAT III certified Head-Up Display; FP = Fail Passive Landing or Rollout Control System; NA = Not Applicable.
Figure 4-4E. Sample C060 Table 2 – CAT III Airplane Systems and Landing Minimums
Airplane M/M/S |
Approach/ Landing System* |
Rollout System* |
DH/AH |
TDZ/Mid/RO RVR |
Special Operational Equipment and Limitations |
|
FP HUD FP Autoland FO Autoland |
None FP FO |
50 DH 30 DH 200 AH 100 AH 50 AH |
700/700/300 600/600/300 600/400/300 400/400/300 300/300/300 |
|
* FP HUD = CAT III certified Head-Up Display; FP = Fail Passive Landing or Rollout Control System; FO = Fail Operational Landing or Rollout Control System; NA = Not Applicable.
A
foreign air carrier’s airplane M/M/S will populate Table
1 of C060 for CAT II operations and, where authorized, Table 2
for CAT III operations based on the assignment of the CAT II
and CAT III authorizations to specific airplanes in the
Operator—Aircraft listing.CAT II airplanes typically have an AFM or AFMS statement showing compliance with the airworthiness performance and integrity criteria found in AC 120-29.
Airplanes used for Special Authorization CAT II or 1000 RVR CAT II operations require guidance or flight control systems (fail passive (FP) HUD or autoland) showing compliance with the airworthiness and performance criteria found in AC 120-28.
CAT III airplanes typically have an AFM or AFMS statement showing compliance with the airworthiness performance and integrity criteria found in AC 120-28.
Autopilot: autopilot approach coupler used to DH, followed by manual control landing.
HUD: CAT II certified HUD providing guidance to DH, flown under manual control.
FP HUD: CAT III certified FP HUD providing guidance at least to touchdown, flown under manual control.
Autoland: any certified autoland system.
Select the appropriate phrase for each M/M/S to place in the CAT II “Approach/Landing System” column: Autopilot, HUD, FP HUD, or Autoland. Any of the above approach/landing systems may be selected for 1600 RVR or 1200 RVR CAT II operations. If a foreign air carrier desires to use two systems during approach (e.g., HUD monitored autopilot), only the primary control system in use needs to be listed. “FP HUD” or “Autoland” must be selected if foreign air carriers conduct Special Authorization CAT II or 1000 RVR CAT II operations.
If the foreign air carrier is approved to conduct only CAT II operations (i.e., CAT III not authorized), the table will automatically populate with “NA.”
Approach/landing
systems:
FP HUD.
FP Autoland: any FP autoland system.
FO Autoland: fail operational (FO) autoland system.
Rollout systems:
None: no rollout guidance or automatic rollout system.
FP: any FP rollout system.
FO: FO automatic rollout system.
Select the appropriate phrase for each M/M/S to place in the CAT III “Approach/Landing System” column: FP HUD, FP Autoland, or FO Autoland. Select the appropriate rollout system: None, FP, or FO.
Table 4-4B. Category II Operating Minimums
CAT II RVR Minimums |
|||
Type of Operation |
TDZ RVR |
Mid RVR |
Rollout RVR |
Standard CAT II |
1600 (500 m) |
600 (175 m)# |
300 (75 m)# |
Standard CAT II |
1200 (350 m) |
600 (175 m)# |
300 (75 m) |
Standard CAT II to 1000 RVR |
1000 (300 m) |
600 (175 m)# |
300 (75 m) |
Special Authorization CAT II |
1200 (350 m) |
600 (175 m)# |
300 (75 m) |
# If available
Select TDZ/Mid/RO RVR CAT II minimums as follows:
Select 1600/600/300 for new CAT II foreign air carriers during the 6-month Operator Use Suitability Demonstration (OUSD) or as a final authorization if desired by the foreign air carrier or the POI.
The POI should issue an initial, interim authorization using the higher minimums, and reissue C060 authorizing lower minimums upon completion of the approval demonstration phases. Foreign air carrier approval requirements are shown in Volume 4, Chapter 2, Section 8, Paragraph 4-365, Foreign Air Carrier CAT II/III Operations in the United States.
Select
1200/600/300 for a Standard CAT II authorization. A 100 ft DH
should be selected.
Select 1000/600/300 for a Standard CAT II authorization to conduct 1000 RVR CAT II operations. A 100 ft DH should be selected in Table 1 of C060. This option requires an autoland or FP HUD to be flown to touchdown.
No additional lines of minimums need to be selected for the authorization of Special Authorization CAT II operations. Special Authorization CAT II minimums and DH are 1200 RVR and 100 ft.
Table 4-4C. Category III Operating Minimums
Landing System |
Rollout System |
TDZ RVR |
Mid RVR |
Rollout RVR |
FP (CAT IIIa) |
None |
700 (200 m) |
700 (200 m) |
300 (75 m) |
FP or FO |
None |
600 (175 m) |
600 (175 m) |
300 (75 m) |
FP |
FP or FO |
600 (175 m) |
400 (125 m) |
300 (75 m) |
FO |
FP |
400 (125 m) |
400 (125 m) |
300 (75 m) |
FO |
FO |
300 (75 m) |
300 (75 m) |
300 (75 m) |
When the foreign air carrier’s airplanes have FP landing systems, or have been demonstrated for CAT IIIa operations, with AFM statements describing compliance with only AC 120-28C criteria (or earlier editions):
Select 700/700/300; or
Select 600/600/300 for airplanes having FP landing systems that have been authorized RVR 600 minimums under AC 120-28D, Paragraph 4.3.7, Category IIIa.
When the foreign air carrier’s airplanes have an AFM statement showing compliance with AC 120-28D criteria (or subsequent editions), or airplanes with FO landing and FO or FP rollout systems and an AFM statement showing compliance with AC 120-28C criteria (or earlier editions):
Select 600/400/300 for airplanes using FP landing and FP or FO rollout systems;
Select 400/400/300 for airplanes using FO landing and FP rollout systems; or
Select
300/300/300 for airplanes using FO landing and FO rollout
systems.
AC 120-29,
AC 120-28, and
TC or STC.
Authorized
CAT II Approaches.Minimums of TDZ 1600 RVR and TDZ 1200 RVR require the flightcrew to use an approach coupler or to fly at least to DH under manual control using a HUD for flight guidance. A manually flown landing is assumed and need not be specified.
Minimums of 1000 RVR, as published via a chart note on the part 97 procedure, require the flightcrew to use autoland or to fly under manual control using an FP HUD to touchdown.
For manual control using a HUD to touchdown, the FP HUD must be flown in the AIII approach mode.
The flightcrew has been trained at the lower visibilities before they can be authorized. If the flightcrew is currently authorized CAT III operations, no further training is required for this authorization in C060.
Foreign air carriers authorized Special Authorization CAT II, as described in subparagraph j)2), may also be authorized to conduct approaches to standard CAT II facilities when the TDZ and/or CL lights are inoperative or when the Approach Lighting System With Sequenced Flashing Lights (ALSF) is downgraded. For example, no sequence flashing lights (SFL) or when operated as simplified short approach lighting system with runway alignment indicator lights (SSALR) or simplified short approach lighting system (SSALS). They must comply with all requirements in subparagraph j)2), using minimums appropriate to the RVR available and using autoland or manual HUD to touchdown.
The ILS facilities used are CAT I ILS installations that meet the GS and LOC signal quality requirements of CAT II facilities. The required increase in airplane capabilities of HUD or autoland to touchdown mitigates the reduced-lighting requirements.
Special Authorization CAT II requires the flightcrew to use autoland or to fly under manual control using an FP HUD to touchdown. These minimums may be no lower than 1200 RVR.
Authorized
Restricted/Nonstandard U.S. CAT II or CAT III Airports and
Runways. The U.S. ILS facilities provided in the Flight
Technologies and Procedures Division Restricted U.S. Facilities
Approved for Category II/III Operations list are approved only
for the specific airplanes listed when conducting CAT III
operations or CAT II operations using autoland or FP HUD to
touchdown. The characteristics of the pre-threshold terrain,
runway TDZ slope, or steep GS at these facilities may cause
abnormal performance in flight control systems. Additional
analysis and/or flight demonstrations are typically required for
each airplane type before approval of CAT II/III minimums at
each runway. Publication of a part 97 SIAP or additional
operators and their airplanes may be approved by the Flight
Technologies and Procedures Division as provided in AC 120-28,
Appendix 8, Irregular Terrain Assessment. Approved airplanes are
equipped with either autoland or FP HUD flight guidance
equipment. The restrictions at U.S. facilities for the
certificate holder are provided as selectables for listing in
Table 3 of C060 (see Figure 4-4F below).Figure 4-4F. Sample C060 Table 3 – Restricted/Nonstandard U.S. Facilities
Approach Category, Airport Name/Identifier, Runway(s) |
Limitations |
Pittsburgh/Greater Pittsburgh Intl, PA; KPIT RY10L; RVR 300 |
Airplanes approved: A319, A320, B757, and B767 |
Pittsburgh/Greater Pittsburgh Intl, PA; KPIT RY10R; RVR 600 and RVR 300 |
Restricted to 600 RVR until less than 600 RVR SMGCS operations are approved. Airplanes approved RVR 600: B757 and B767. Airplanes approved RVR 300: A319 and A330. |
OpSpec
C063 authorization must not be issued to a foreign air carrier
unless the State of the Operator CAA has approved the foreign
air carrier for RNAV 1 DPs and STARs (to include operations,
procedures, aircraft and aircraft equipment, and flightcrew
training to conduct RNAV 1 DP and STAR).PIs must coordinate all acceptable criteria other than these specified in subparagraph b) with the International Program Division who will coordinate with the Flight Technologies and Procedures Division, as appropriate.
Definitions
Related to This Authorization. Some important definitions as
they relate to this authorization:Area Navigation (RNAV) 1 Departure Procedures (DP) and Standard Terminal Arrival Routes (STAR). RNAV 1 terminal procedures require the aircraft’s track-keeping accuracy remain bounded by +1 NM for 95 percent of the total flight time. RNAV 1 terminal procedures requiring, as a minimum, a DME/DME/Inertial Reference Unit (IRU)-based and/or GPS-based RNAV system satisfying the criteria of AC 90-100.
Climb Via and Descent Via. Refer to Information for Operators (InFO) 14003, “Climb Via” Phraseology for Standard Instrument Departure (SID), Modification to “Descend Via” Phraseology for Standard Terminal Arrival (STAR), and Phraseology Associated with Speed Instructions.
Flight Management System Procedure (FMSP). An RNAV arrival, departure, or approach procedure developed for use by aircraft equipped with an FMS.
The number of FMSPs in the NAS is limited, and FMSP criteria are no longer preferred for the design of RNAV procedures.
Instrument Departure Procedure (DP). Instrument DPs are published IFR procedures that provide obstruction clearance from the terminal area to the en route structure. There are two types of DPs: ODPs and SIDs.
Obstacle Departure Procedure (ODP). An ODP is a published IFR DP that provides obstruction clearance via the least onerous route from the terminal area to the appropriate en route structure. ODPs are recommended for obstruction clearance unless an alternate DP (such as a SID or radar vector) has been specifically assigned by ATC. The RNAV 1 ODP must be retrievable from the FMS database and included in the filed flight plan.
Standard Instrument Departure (SID). A SID is a published IFR ATC DP that provides obstacle clearance and a transition from the terminal area to the en route structure. SIDs are primarily designed for air traffic system enhancement to expedite traffic flow and to reduce pilot/controller workload.
Standard Terminal Arrival Route (STAR). An RNAV STAR is a published IFR ATC arrival procedure that provides a transition from the en route structure to the terminal area.
Tailored Arrivals. Tailored arrivals are preplanned fixed routes received via data link from the U.S. oceanic air traffic system to Future Air Navigation System 1/A (FANS 1/A)-equipped aircraft. Currently, tailored arrival models are limited. Except for the instrument approach portion of an arrival, tailored arrival routes are neither stored in the aircraft navigation database nor published.
Foreign
Air Carrier Actions. A foreign air carrier applying to the FAA
for the issuance of C063 must provide the responsible IFO with
evidence that the State of the Operator has approved the foreign
air carrier for this operation. The approval must include:Documentation (e.g., foreign-issued OpSpecs, official letter) from the State of the Operator’s CAA stating that the foreign air carrier is approved for RNAV 1 DP and STAR in accordance with XXXX (e.g., ICAO Doc 9613) criteria that the aircraft and aircraft equipment are eligible and approved for RNAV 1 DP and STAR, and that the flightcrews are trained to conduct RNAV 1 DPs and STARs (see subparagraph b));
RNAV system make, model, and part number(s) approved;
Procedures using RNAV 1 DP and STAR (see subparagraph d)); and
Any other pertinent information.
The FAA and PIs are not responsible for evaluating a foreign air carrier’s training program. Foreign air carrier training programs are evaluated and approved by the State of the Operator CAA. PIs may accept equipment eligibility that has been determined eligible and approved by a foreign air carrier’s CAA, when it is also documented by the AFM/RFM or other FAA-recognized means.
Per AC 90-100 and AC 90-105, data suppliers and avionics data suppliers must have a Letter of Authorization (LOA) in accordance with AC 20-153, Acceptance of Aeronautical Data Processes and Associated Databases. It is the responsibility of the foreign air carrier to ensure that data supplier(s) are compliant.
The
ATC Flight Plan must contain information in item 18 of the
International Flight Plan (FAA Form 7233-4, Pre-Flight Pilot
Checklist and International Flight Plan) indicating the RNAV
capabilities and include applicable descriptors.
If the responsible IFO is unable to determine equipment eligibility for RNAV 1 DPs and STARs via the Flight Technologies and Procedures Division Flight Operations Group web page, contact the International Program Division, who will coordinate with the Flight Operations Group, as appropriate.
Add the following statement in C063 Table 1, “Limitations and Provisions” column for each M/M/S aircraft with documented FMS autoload/uplink function and approved for tailored arrival operations: “Tailored Arrivals (TA) authorized.”
Confirm that each of the operator’s M/M/S aircraft have been approved for data link communication via OpSpec A003.
Title 14 CFR Part 91, §§ 91.123, 91.205, and 91.503; Part 95; and Part 129, § 129.17.
FAA Order 1050.1, Environmental Impacts: Policies and Procedures.
FAA Order JO 7110.65, Air Traffic Control.
FAA Order JO 7400.2, Procedures for Handling Airspace Matters.
FAA Order 8260.3, United States Standard for Terminal Instrument Procedures (TERPS).
FAA Order 8260.19, Flight Procedures and Airspace.
AC 20-138, Airworthiness Approval of Positioning and Navigation Systems.
AC 20-153, Acceptance of Aeronautical Data Processes and Associated Databases.
AC 90-96, Approval of U.S. Operators and Aircraft to Operate Under Instrument Flight Rules (IFR) in European Airspace Designated for Basic Area Navigation (B‑RNAV)/RNAV 5 and Precision Area Navigation (P-RNAV).
AC 90-100, U.S. Terminal and En Route Area Navigation (RNAV) Operations.
AC 90-105, Approval Guidance for RNP Operations and Barometric Vertical Navigation in the U.S. National Airspace System and in Oceanic and Remote Continental Airspace.
ICAO Global Operational Data Link (GOLD) Manual.
ICAO Doc 9613, Performance-based Navigation (PBN) Manual.
The FAA does not encourage foreign air carriers to list aircraft-specific limitations for airports with curfew hours in their OpSpecs. If an airport authority requires foreign air carriers to list such limitations in their OpSpecs, then they should be listed in Table 1 of C067. A sample of Table 1 shows an example of limitations for foreign air carrier operations into specific airports with curfew hours (see Figure 4-4G, Sample C067 Table 1 – Special Airplane Authorizations for Certain Airports).
Operations
using the Reginald Bennett International Runway
Reflectorization System in Alaska.Figure 4-4G. Sample C067 Table 1 – Special Airplane Authorizations for Certain Airports
Airport (Airport Location/Identifier) |
Airplane |
Special Provisions/Limitations |
KDCA, Ronald Reagan Washington National Airport, DC |
Boeing 737-800 |
Limitations during the curfew hours. Max Takeoff—159,000 pounds Max Landing—137,600 pounds. |
KEWR, Newark Liberty International Airport, NY |
B747-8F |
Limited to taxi speed restriction of 17 kt/20 mph.1 |
1 Unless there exists a special provision or limitation (e.g., taxi restriction imposed by the State of the Operator), PI(s) do not need to list airports used by foreign air carriers operating Airplane Design Group VI (ADG-VI)/ICAO Group F aircraft (e.g., A380, B747-8, or AN‑124) into a U.S. airport if the airport has a Modification of Standard (MoS) for that aircraft.
The airport (military and non-military) is operated by the U.S. Government;
The equivalent safety standards for airport(s) certificated under part 139 are met; and
The equivalent airport classification requirements under part 139 serve the types of airplanes and the types of operations to be conducted.
Foreign
air carriers should obtain permission to operate from:The airport manager of non-military airports.
The base operations of military airports.
The designated airport manager for a joint-use civil and military airport.
Refer to the U.S. Chart Supplements (airport database of every U.S. airport) for airport permission contact details.
Line station office information:
Location(s).
Name of station manager or point of contact (POC).
Maintenance personnel information (or contractor information) and any other contractors (e.g., deicing or baggage/cargo handlers), including contact information (name, address, phone/fax numbers) for all contractors, and a list of which tasks are to be performed by each of the contractors.
Copy of U.S. economic authority (if required) issued by the Department of Transportation (DOT) to the foreign air carrier to assure that it reflects the addition of the requested airport.
Written documentation that the foreign air carrier has:
Airport analysis for the aircraft it intends to operate into the new airport and its alternate airports (e.g., an excerpt from a CAA-approved manual if in English or a letter from a CAA).
Properly trained the servicing personnel in accordance with the foreign air carrier’s CAA-approved policies and procedures.
Properly trained contract baggage and cargo handlers to the foreign air carrier’s CAA-approved policies and procedures, which should include dangerous goods training (if applicable).
Properly trained its aircraft maintenance personnel (or contractor maintenance personnel) to its CAA-approved policies and procedures.
A copy of the State of the Operator required manuals (which should address the above-mentioned procedures) available at each new airport.
Part 91 (in particular, §§ 91.13, 91.103, and 91.123).
Part 93.
Part 129.
Part 139.
Any other applicable regulations and laws of the United States.
Foreign air carriers may find a link to the FSIMS list of U.S. special airports in the U.S. AIP. Refer to the U.S. AIP, page GEN 1.7-55.
Any
regulations of the State of the Operator that are more
restrictive than the equivalent U.S. regulations, as approved
by the State of the Operator, for the foreign air carrier
applying to operate to an airport within the United States.
Examples:If the State of the Operator requires that to operate to XXX airport with the B777 all takeoffs and landings must be conducted by the PIC, then this limitation must be entered into C067 Table 1.
If the State of the Operator requires that takeoffs and landings in the B747 into XXX airport may only be conducted between sunrise and sunset and the XXX airport limits B747 operations only between midnight and 6 a.m., then the more restrictive State of the Operator limitation must be entered into C067 Table 1.
Close-In NADP operations, and/or
Distant NADP operations.
For each NADP, the foreign air carrier will specify the altitude above field elevation (AFE) at which flightcrews will initiate thrust reduction from takeoff thrust (close-in profile) or airplane configuration change (distant profile), excluding gear retraction.
Close-in NADP. The foreign air carrier will use the following NADP criteria for individual airplane types intended to provide noise reduction for noise-sensitive areas located in close proximity to the departure end of the runway:
Initiate thrust cutback at an altitude of no less than 800 ft AFE and prior to initiation of flaps or slats retraction.
The thrust cutback may be made by manual throttle reduction or by approved automatic means. Flightcrews may arm the automatic means before takeoff for cutback at or above 800 ft AFE or it may be pilot-initiated at or above 800 ft AFE.
For
airplanes without an operational automatic thrust restoration
system, achieve and maintain no less than the thrust level
necessary, after thrust reduction, to maintain the takeoff
path engine-inoperative climb gradients specified in part 25,
§ 25.111(c)(3), with the flaps/slats configuration of
the airplane, in the event of an engine failure.
For airplanes with an operational automatic thrust restoration system, achieve and maintain no less than the thrust level necessary, after thrust reduction, to maintain a takeoff path engine-inoperative climb gradient of zero percent. This climb gradient is contingent upon the ability of the automatic thrust restoration system to (at a minimum) restore sufficient thrust to maintain the takeoff path engine-inoperative climb gradients specified in § 25.111(c)(3), with the flaps/slats configuration of the airplane, in the event of an engine failure.
During the thrust reduction, coordinate the pitchover rate and thrust reduction to provide a decrease in pitch consistent with allowing indicated airspeed to decay no more than 5 knots below the all-engine target climb speed, and in no case to less than takeoff safety speed (multi) (V2) for the airplane configuration. The acceptable speed tolerances for automated throttle systems are found in AC 25-15, Approval of Flight Management Systems in Transport Category Airplanes.
Maintain the speed and thrust criteria as described in steps a)2)b2 through 5 to 3,000 ft AFE or above, or until the airplane has been fully transitioned to the en route climb configuration (whichever occurs first), then transition to normal en route climb procedures.
Distant NADP. The foreign air carrier will use the following NADP criteria for individual airplane types intended to provide noise reduction for all other noise sensitive areas.
Initiate flaps/slats retraction prior to thrust cutback initiation. Flightcrews should initiate thrust cutback at an altitude no less than 800 ft AFE.
Flightcrews may make the thrust cutback by manual throttle reduction or by approved automatic means. Flightcrews may arm the automatic means prior to takeoff for cutback at or above 800 ft AFE or the flightcrew may initiate it at or above 800 ft AFE.
Same as subparagraph a)2)b3.
Same as subparagraph a)2)b4
Same as subparagraph a)2)b5.
Same as subparagraph a)2)b6.
For
those airplanes that have a performance requirement to reduce
takeoff flaps to an intermediate takeoff flap setting at 400 ft
AFE or above, the next flap/slats retraction should be
initiated at an altitude of no less than 800 ft AFE.Do not issue C075 if the foreign air carrier is not authorized for either the circling maneuver or contact approach.
This does not authorize the pilots to go below the lowest minimum authorized by the State of the Operator.
Pilots
Restricted to Circling in Visual Conditions. Any pilot who
possesses a pilot certificate restricting circling approaches to
visual meteorological conditions (VMC) is not eligible to
conduct circle-to-land maneuvers except as provided:Foreign air carriers conducting circle-to-land maneuvers without training and checking are subject to the same provisions as pilots restricted to circling in visual conditions.
C077
Subparagraph c(3). In lieu of a CVFP, a charted visual procedure
that the foreign air carrier’s CAA approved is highly
recommended for all terminal VFR departures/arrivals that fall
under C077. The proximity of obstacles to the departure
flightpath, visibility, the accuracy of the guidance and control
systems, the pilot’s proficiency, and the foreign air
carrier’s training should determine the size of the area
in which obstacle clearance or avoidance must be considered.Use of the charted visual DP requires that all of the conditions and limitations of C077 subparagraph d(1) through (4) be met. These procedures are established by the FAA and published in the FAA Chart Supplement as a Terminal Area Graphic Notice in the Special Notices section and may also be located online at the Aeronav products web page at https://www.faa.gov/air_traffic/flight_info/aeronav/digital_products/dafd/.
Flightcrews must specifically request this type of procedure by name and ATC may issue a clearance for the aircraft to depart using the visual DP. In this instance, the flight will have an IFR flight plan filed and will have received its IFR clearance prior to departure. This will include a clearance to depart the airport under VFR using the procedure published in the Graphic Notice for the airport of departure. The IFR clearance is activated at the point and/or altitude described in the Graphic Notice.
Flightcrews must comply with flightpath/course to be flown, altitudes, and speed limitations published on the procedure, in addition to maintaining their own terrain and obstruction clearance until their IFR clearance is activated at a specific point and/or above a specific altitude as defined by the procedure.
Special
Limitations and Provisions for VFR in C077 Subparagraph f.
Subparagraph f provides special limitations and provisions for
all VFR operations. This subparagraph is applicable to all of
the provisions and limitations of C077.
Sources
of Traffic and Airport Advisories. Foreign air carriers may be
authorized to use any two-way radio source of air TA information
listed in the AIM (for operations in U.S. airspace) or
equivalent AIPs.Additional information on the FAA’s IASA program, including a country’s IASA category, is found on the FAA website at http://www.faa.gov/about/initiatives/iasa/. For FAA policy information, see Volume 12, Chapter 2, Section 1.
Special
Authorizations. Foreign air carrier Special Authorizations
include CAT II/III, ILS/PRM, land-and-hold-short operations
(LAHSO), Reduced Vertical Separation Minimum (RVSM), etc.
Special Authorizations requiring initial approval, acceptance,
authorization, and/or continued oversight by the foreign air
carrier’s CAA must be reviewed by the responsible IFO. The
review will determine if adequate oversight by the foreign air
carrier’s CAA is occurring on a continuous basis. If it is
determined that adequate oversight is not occurring, the IFO
should consider an amendment to withdraw those Special
Authorizations from the foreign air carrier’s OpSpecs.
Initiate the amendment only after consultation and clearance by
the International Program Division.Additional aircraft must be for the same M/M/S and configuration of aircraft, typically for inspection, maintenance, or alterations. The Special Authorization must be in the interest of safety. See Volume 12, Chapter 1, Section 2 for additional details.
Figure 4-4H. Example Scheduled Operations Table
ROUTING INCLUDING CITIES AND ICAO AIRPORT ID(s) |
FREQUENCY |
KMIA Miami, Florida—MTPP Port au Prince, Haiti |
Seven weekly |
Obtain the “list of areas of en route operation.” The WebOPSS guidance subsystem contains detailed information on geographical areas. The areas authorized for issuance to a foreign air carrier in part 129 OpSpecs are:
USA—The 48 Contiguous United States and the District of Columbia,
USA—The Commonwealth of the Northern Mariana Islands,
USA—The Commonwealth of Puerto Rico,
USA—The State of Alaska,
USA—The State of Hawaii,
USA—The Territory of American Samoa,
USA—The Territory of Guam, and
USA—The Territory of the U.S. Virgin Islands.
Select the individual areas of en route operations to be authorized. If the foreign air carrier was not authorized for nonscheduled operations, then select “Not Authorized.”
Figure 4-4I. Example Nonscheduled Operations Table
UNITED STATES GEOGRAPHIC AREA |
FREQUENCY |
USA—The 48 Contiguous United States and the District of Columbia |
6 flights per year |
State of the Operator authorization;
Evidence that the requirements of C091 were met for the proposed runway(s) of operations at those airports, including potential alternates;
For destination airports, U.S. airport MoS approval for that make and model (M/M) (e.g., A-380 or B747-8); and
For alternate airports, the process the foreign air carrier used to evaluate the airport to ensure it could accommodate the aircraft.
It
is the foreign air carrier’s responsibility to confirm
that they can comply with the requirements of C091 and supply
the POI sufficient documentation to verify their compliance.
The foreign air carrier is responsible for any necessary
coordination and letters of understanding with applicable ATC
facilities and the airport operators to meet the requirements
of C091. For scheduled destination U.S. airports serving
ADG-VI/ICAO Group F airplanes, taxi routes used and procedures
to follow will be established in a written Taxi Operational
Plan approved by the airport operator, ATC, and local control.
Taxi Operational Plans may be applicable to either:A specific foreign air carrier;
All operators of a specific type of ADG-VI/ICAO Group F airplane (e.g., all A‑380s serving that airport); or
All ADG-VI/ICAO Group F airplanes serving the airport (e.g., all A-380s and B747-8s).
The foreign air carrier’s compliance with the requirements of C091 eliminates them from having to demonstrate their capability to operate to the lower criteria specified in C091 prior to issuing C091 for that aircraft and airport combination.
The
overall runway plus shoulder width is 280 ft (85 m) for U.S.
ADG-VI and 250 ft (75 m) for ICAO Group F. In order to reduce
the jet blast impact to 150 ft (45 m) of runway surface, the
FAA recommends stabilized shoulders beyond the runway edge. The
FAA 150 ft runway (width) evaluation for the A-380, along with
the recommendations for these operations contained in ICAO
Annex 14 and the A-380 AFM has led to the following runway
width authorization for A-380 operation in the United States:Runways for takeoffs and landings will be at least 150 ft (45 m) wide with stabilized runway shoulders on both sides of the runway extending an additional 50 ft (15 m) outward from the runway edge. The additional safety width is prescribed because the standard ADG-V runway shoulder width is only 35 ft (10 m).
Runways as narrow as 150 ft (45 m) wide, with or without the 35 ft (10 m) wide stabilized shoulders, may be used for takeoffs and landings provided applicable flight manual procedures for takeoffs on such runways are followed. Procedures must be implemented for the full length of the runway to be inspected by the airport operator for foreign object damage (FOD) after each takeoff prior to successive aircraft operations.
Only the airport operator conducts runway inspections for FOD. Hence, the foreign air carrier should make sure, or have some documentation, that the airport operator will do it. The document is the required Federal Airport Certification Manual under part 139.
Currently, there is no method to authorize part 375 operators to fly special instrument procedures or RVFPs due to tracking, notification, and coordination requirements associated with the authorization.
RVFP.
An RVFP is an IFR procedure flown with an IFR-approved RNAV
system in visual conditions. The procedure is selected from an
approved database and must be flown as published. RVFPs may have
altitude and airspeed restrictions associated with a waypoint.
RVFPs are designed to promote flightpath repeatability, to
reduce ATC communications, and to enhance safety by providing a
stabilized approach to a designated runway.
For
new approaches: FAA Form 8260-7A defines the procedure, and
FAA Form 8260-7B defines the foreign air carrier
requirements. FAA Form 8260-7B requires PI and foreign air
carrier signatures.
For older approaches: FAA Form 8260-7 defines the procedure and FAA Form 8260-10, Standard Instrument Approach Procedure, defines the foreign air carrier requirements. FAA Form 8260-10 requires PI and foreign air carrier signatures.
For special non-part 97 DPs: FAA Form 8260-15A, Takeoff Minimums and Obstacle Departure Procedures (ODP); FAA Form 8260-15B, Graphic Departure Procedures (DP); and/or FAA Form 8260-15C, Departure (Data Record), defines the procedure; and FAA Form 8260-7B defines the foreign air carrier requirements. FAA Form 8260-7B requires PI and foreign air carrier signatures.
The foreign air carrier will provide their CAA with the forms for review.
The CAA will review the foreign air carrier’s existing procedures, documentation, equipment, manuals, and training to ensure any requirements specific to the procedure and listed on the 8260 forms are satisfactorily addressed. These requirements may require special aircraft performance, equipment, avionics/software, and/or crew training.
If existing foreign air carrier procedures do not address all requirements, the foreign air carrier must submit a plan to the CAA with the necessary changes needed to comply with the requirements of the special procedure. This plan must address any aircraft-specific requirements for each M/M/S that the foreign air carrier plans to use to fly the special.
Once documentation is received from the CAA concurring with the implementation plan and usage of the procedure, the PI reviews the implementation plan.
PIs and the foreign air carrier’s representative will sign the FAA Form 8260-7B after the following:
The PI has discussed the procedure requirements with the foreign air carrier; and
The foreign air carrier has provided the PI with documentation showing compliance with procedure requirements (i.e., aircraft performance, aircraft equipment, crew qualifications, etc.) or an implementation plan that shows a reasonable expectation that they will be able to safely meet all procedural requirements.
The
PI will give a signed copy of the FAA Form 8260-7B to the
foreign air carrier and maintain a signed copy in the office
file in accordance with the record retention requirements.
These forms allow the foreign air carrier to receive customized charts and navigation database coding (if applicable) from chart vendors and training from most contract training vendors.
It may take some time for the operator to fully implement their plan and qualify all relevant personnel to conduct the procedure(s).
The OpSpec must not be authorized until the foreign air carrier has implemented their plan and is fully prepared to fly the procedure. For additional detail/requirements, see subparagraphs d)5)c and d)6).
Signing the back of FAA Form 8260-7 or FAA Form 8260-7B is not the formal issuance of the authority for use of a special procedure. Conveyance of authority is by the issuance of C381.
The PI should review the requirements contained in the procedure to ensure that the aircraft type(s) in question can perform the procedure before sending the application for both International Program Division and Flight Technologies and Procedures Division management review (if required). Some special instrument procedures require nonstandard/higher missed approach climb gradients and specific qualities or levels of avionics.
The training is duplicative;
The multiple specials are basic instrument approaches to a private-use landing area; or
No additional performance or training requirements for a specific airfield are noted on forms.
Charts.
The Flight Technologies and Procedures Division will send the
PI the FAA 8260 forms described above. The foreign air carrier
will use these forms to get a chart produced. The foreign air
carrier will submit a copy of the completed chart to their PI.
Upon receipt, the PI will forward a copy of the chart to the
Flight Technologies and Procedures Division for review and
distribution in accordance with Order 8260.60. The PI must not
authorize operational implementation of the procedure until the
Flight Technologies and Procedures Division receives the chart.
In some cases, a third-party developer will create a chart for
the foreign air carrier and submit it to the Flight
Technologies and Procedures Division for distribution. The
Division will distribute this chart to the PI who, in turn,
will give it to the foreign air carrier.If a demonstration flight is not stipulated on FAA Form 8260-7B, a demonstration flight may still be required at the discretion of the CAA, the FAA, or both before a foreign air carrier can use a new or amended special Instrument Flight Procedure (IFP). Flight simulator and tabletop reviews are other ways a CAA may confirm an operation can be conducted safely. Consideration should be given to the foreign air carrier’s experience at that airport, profiles and procedures, aircraft capabilities, deviation from IFP criteria, and local environmental considerations (e.g., terrain, radar and communications coverage, and obstacles) when determining if public interest necessitates that a flight demonstration, simulator, or tabletop review be accomplished by the applicant’s CAA.
If it is determined that public interest necessitates a demonstration flight/simulator or tabletop review be accomplished, the FAA will dictate the requirements and criteria for satisfactorily completing the demonstration. The PI must then forward to the applicant those criteria. All demonstrations must be accomplished by the applicant’s CAA. Once written documentation is received from the applicant verifying the satisfactory accomplishment, the PI may then continue to proceed with processing the application request.
The PIs, with joint division management concurrence, may issue a provisional authorization allowing a foreign air carrier to conduct a special IFP if the applicant’s CAA inspector will be observing the flight to evaluate that procedure during routine operations in VMC. The provisional authorization should only be used after a careful evaluation has been made of the special IFP for safety-related factors. Issue this provisional authorization by adding the special IAP to the appropriate C381 with the provision that the authorization is only applicable to flights observed by the applicant’s CAA inspector in VMC.
The foreign air carrier has implemented their plan to address all of the FAA 8260 form requirements (including training, dispatch, equipment, performance, etc.) and has a chart, and the demonstration flight(s), if required, is completed satisfactorily.
The International Program Division and the Flight Technologies and Procedures Division management concur with the authorization, if required.
The foreign air carrier documents to the responsible PI that they have signed (if required) a letter of agreement with responsible Terminal Radar Approach Control (TRACON). If a letter of agreement is not required, the Flight Technologies and Procedures Division has notified the appropriate air traffic facility of the new foreign air carrier prior to the foreign air carrier flying the procedure (if required).
The FAA sets criteria for “special procedures” within U.S. airspace. There is no ICAO standard for these procedures. To operate a special procedure at a private airport, the foreign air carrier must attain written permission from the owner/manager of the airport.
Effective Dates. Procedure effective dates can be critical to flight safety. Procedures must not be used after the expired effective date. For example, some procedure amendments use the same fix names but with the fixes in a slightly different location, and those fix locations will change on the effective date, allowing the use of the expiring procedure until the effective date and the new procedure on and after the effective date. If the procedure has a specific effective date set by the Flight Technologies and Procedures Division, add a reference to that effective date in the “Limitations and Provisions” column of Table 1 of C381 for the new procedure, as well as the expiring procedure (if applicable).
Amendments/Cancellations. When an approved special or RVFP is amended or canceled, the Flight Technologies and Procedures Division will notify the PI for each foreign air carrier that is authorized to use the special or RVFP. For an amended special or RVFP, the amendment cancels the previously approved special or RVFP on the effective date set by the Flight Technologies and Procedures Division. The PI must remove the previously approved special or RVFP from the foreign air carrier’s C381.
Rescinding Concurrence. Both the International Program Division and the Flight Technologies and Procedures Division management have the authority to rescind their concurrence. The PI must rescind authorization for use of a procedure immediately upon written notification from division management. Following is a list of examples for which division management may rescind their concurrence:
The foreign air carrier deviates from the procedure requirements;
Division management becomes aware of any additional operational/training requirements; or
Any other factors that affect the safe operation of the procedure.
OpSpec C052. Part 129 foreign air carriers must be issued C052. The “type” (e.g., RNAV, ILS, and LDA) of instrument approach listed in C381 in Table 1 must be listed in the table of authorized approaches in C052. RVFP and RNP AR procedures will not be listed in C052.
OpSpec
C063. Part 129 foreign air carriers may require a C063
authorization. C063 authorizes RNAV 1, RNP 1, and other
Performance-based Navigation (PBN) flight operations and is
required for certificate holders/operators/program managers
authorized to conduct RNAV 1, RNP 1, or other PBN flight
operations in C381.
OpSpec C077. Part 129 foreign air carriers must be issued C077 if operating under IFR. C077 provides arrival and departure guidance for instrument and visual flight operations (e.g., VFR departure on an IFR clearance). C077 provides guidance on the use of a CVFP. Determine if a VFR operation into or out of an airport is part of the C381 authorization.
OpSpec C080. Part 129 foreign air carriers may require a C080 authorization. Determine the type of airport and operation being conducted in association with C381 authorization.
OpSpec C384. Part 129 foreign air carriers should be issued C384 when an RNP AR-like special procedure, normally titled RNAV (RNP), is authorized in C381. Approval to fly an AR-like special without C384 will be granted by division management (the International Program Division and the Flight Technologies and Procedures Division) and documented on FAA Form 8260-7B. The authorization in C384 must contain the lowest RNP and additional aircraft capabilities meeting the requirements of the special procedure authorized in C381.
The PI will copy the responsible IFO manager and the International Field Office Management Branch on all procedure amendments or cancellations, required forms, and new charts. See subparagraph e) for additional details.
Oversight
and Auditing. Oversight management and guidance of foreign air
carrier authority and use of special instrument procedures is
not currently in the FAA automated work programs. It may occur
under the initiative of planned activities by IFOs for those
part 129 foreign air carriers who are addressed in National
Work Programs for inspectors. PIs are requested to review the
C381 for their assigned foreign air carriers annually to ensure
the currency of the special instrument procedures is maintained
and disseminated. IFOs must maintain files for foreign air
carriers authorized to conduct special procedures in accordance
with the recordkeeping requirements. For example:The documentary elements of the special instrument procedure (e.g., the 8260‑series forms, a copy of the current chart as issued to the foreign air carrier, and related correspondences);
The status of the special authority; and
The Flight Technologies and Procedures Division has the current foreign air carrier contact data.
In another M/M/S and is only requesting to add another aircraft, and provides the PI with documentation that they can fly the procedure without any need for amendment to the procedure; or
The Flight Technologies and Procedures Division notified the PI of an amendment and the foreign air carrier documents: CAA authorization and flyability if required. Some procedure amendments do not require flyability (e.g., renaming of a waypoint). All procedure amendments require a new chart. Flyability is typically conducted in a simulator and refers to:
The capability to maintain track during a go-around or missed approach.
All published airspeeds and maneuvers required to emulate desired flightpaths (lateral and vertical) are flyable with the intended equipment.
PIs who feel that the approval is beyond the scope of their training or experience may request the Flight Technologies and Procedures Division or division management SMEs’ assistance. The Flight Technologies and Procedures Division and division management SMEs will assist, as appropriate. (Refer to the C381 information document for International Program Division and Flight Technologies and Procedures Division contacts.)
Informational
Sharing. Certain specials (e.g., LOC/DME RWY 15 and RNAV (GPS) Z
RWY 15 to Aspen, CO) allow access to challenging airports with
steep, close terrain. Responsible PIs may find it helpful to set
up an informational sharing meeting that includes the
International Program Division, the Flight Technologies and
Procedures Division, the foreign air carrier, or the foreign air
carrier’s CAA (operations representative or management
personnel listed on the operator’s OpSpec A006) to discuss
FAA Form 8260-7B requirements and best practices.
Figure 4-4J. Special Instrument and RNAV Visual Flight Procedures Process Flowchart
Figure 4-4J. Special Instrument and RNAV Visual Flight Procedures Process Flowchart (Continued)
Figure 4-4J. Special Instrument and RNAV Visual Flight Procedures Process Flowchart (Continued)
OPSPEC
C384—RNP AR—AREA NAVIGATION (RNAV) REQUIRED NAVIGATION
PERFORMANCE (RNP) AUTHORIZATION REQUIRED (AR) (OPTIONAL FOR FOREIGN
AIR CARRIERS OPERATING TO THE UNITED STATES).The U.S. approach plate terminology is changing from RNP special aircraft and aircrew authorization required (SAAAR) to RNP AR as the charts are revised or amended. ICAO documents and AC 90-101 have already been harmonized with the new terminology and are using RNP AR.
The FAA must have confidence that the approval follows ICAO Doc 9613 guidance for State of Operation responsibilities. Without this information, the FAA would not be able to determine that safety in air commerce exists as prescribed by § 129.11 before amending the foreign air carrier’s OpSpecs for operations within U.S. airspace.
RNP
AR approaches provide an unprecedented flexibility in
construction of approach procedures. These operations are RNAV
procedures with a specified level of performance and
capability. RNP AR approach procedures build upon the
performance-based NAS concept. The performance requirements to
conduct an approach are defined. Aircraft are qualified against
these performance requirements. Obstacle Evaluation Areas (OEA)
for approaches using conventional navigation aids are based on
a predefined aircraft capability and navigation system. RNP AR
criteria for obstacle evaluation are flexible and designed to
adapt to unique operational environments. This allows
approach-specific performance requirements, as necessary, for
that approach procedure. The operational requirement can
include avoiding terrain or obstacles, deconflicting airspace,
or resolving environmental constraints.RNP AR RF leg capability, and
Reduced lateral OEA on the missed approach (also referred to as a missed approach requiring RNP less than 1.0).
Relevant ICAO Standards include Annex 6, Part I, Appendix 6, pages APP 6-3 and 6-4, items 15 and 16. If the information is not in the foreign air carrier’s OpSpecs, then the PI must request that the foreign air carrier provide them with another form of documentation from the State of the Operator.
Documentation
(e.g., foreign-issued OpSpecs and official letter) from the
State of the Operator’s CAA stating that:The foreign air carrier is approved for RNP AR in accordance with certification (e.g., ICAO Doc 9613) criteria (see subparagraph b)).
Aircraft and aircraft equipment are eligible and approved for RNP AR. Additionally, for each approved aircraft M/M/S, the following information must be included:
The navigation system M/M/S and software version;
All applicable limitations, to include a list of approved airports;
Identify if autopilot coupled or FD required; and
Lowest RNP.
The PI must not enter into Table 1 of C384 any limitations, RNP values, etc., less than those authorized by the foreign air carrier’s CAA. Only operations that are relevant to operations within U.S. airspace must be included in Table 1.
CAA-approved equipment eligibility may be documented by the foreign air carrier by providing to the FAA the relevant copy of an AFM, if the AFM is in English.
Flightcrews are trained to conduct RNP AR. The training program addresses the special characteristics of the proposed area of operation (within the United States) and all operational (navigation) practices and procedures associated with RNP AR. Flight operations officers/flight dispatchers are trained in dispatching or releasing a flight for RNP AR. Relevant ICAO Standards include Annex 6, Part I, 3.1.4, 4.2.1, 9.3.1, 9.4.3, 9.4.3.5, and 10.3, and Attachment E.
Procedures for using RNP AR are included in the foreign air carrier’s documentation (e.g., operations manual). Relevant ICAO Standards include Annex 8, Airworthiness of Aircraft, Chapter 7, 7.2, 7.3, 7.4, 7.5, and 7.6. If the foreign air carrier’s documentation (e.g., operations manual) is in English, it may be used for documentation by the foreign air carrier.
Has an approved/accepted RNP monitoring program that collects data on RNP AR procedures.
Has an approved/accepted Navigation Data Validation Program. Subsequent software updates need to be brought to the attention of the FAA for approval.
Has established maintenance procedures to include procedure for removing the aircraft from, and returning the aircraft to, RNP AR operational capability by trained maintenance personnel.
Has
an approved/accepted MEL revised for RNP AR (as appropriate).
For U.S.‑registered aircraft to be used, the foreign air
carrier must submit the MEL revision for approval to the FAA
in accordance with § 129.14.
Has successfully completed all validations and demonstrations. Refer to AC 90‑101 for acceptable number of validations and demonstrations when operating in U.S. airspace. If the demonstrations are still ongoing, then provide details of any limitations relating to operations during the demonstration period.
Has completed an RNP AR Compliance Traceability Matrix/RNP AR Compatibility Trace Matrix. All matrix items highlighted in yellow require a response. To assist the FAA in expeditious review of the application, the FAA recommends that the applicant provide detailed references in its responses (e.g., Boeing Aircraft Qualifications Document D6‑83991, appendix B, pages 29–31). A copy of the compliance matrix, along with other educational materials, may be found at: https://www.faa.gov/about/office_org/headquarters_offices/avs/offices/afx/afs/afs400/afs410/pbn/.
The International Program Division will forward the application to the Flight Technologies and Procedures Division Flight Operations Group for technical review as appropriate.
The
PAI determines the proper nomenclature of the equipment
manufacturer’s make, model, and software version. The PAI
also determines that the RNP AR equipment and system is
installed in accordance with approved data and meets the
criteria equivalent to AC 90-100. To ensure the proper
configuration control of the approved RNP AR operating system,
it is required to list both the hardware and the software part
numbers or version/revision numbers in Table 1 of C384.The ATC Flight Plan must contain information in item 18 of FAA Form 7233-4 indicating the RNP AR capabilities and include applicable descriptors.
The foreign air carrier provided the PI with all of the information in subparagraph g).
The PI has written division management concurrence from the International Program Division and the Flight Technologies and Procedures Division. See Figure 4-4L, RNP AR Approval Checklist (Optional).
For new aircraft, the aircraft qualification documentation may be approved as part of an aircraft certification project in coordination with AIR-6B1 and reflected in the approved flight manual and related documents. The RNP AR operational documentation may be accepted by the AEG in coordination with the Flight Technologies and Procedures Division.
For
existing aircraft for which there is a U.S. TC, the aircraft
manufacturer should submit the aircraft qualification and RNP
AR operational documentation to the Flight Technologies and
Procedures Division. The Flight Technologies and Procedures
Division will coordinate with other FAA offices and may accept
the package as appropriate for RNP AR operations. Acceptance
will be documented in a letter to the aircraft manufacturer.
For foreign-registered aircraft for which there is no U.S. TC, the foreign air carrier must provide a copy of the aircraft manufacturer aircraft qualification and RNP AR operational documentation as part of their application package for C384.
Relevant ICAO references include: ICAO Doc 9613, Attachment C, 3.3, Aircraft Eligibility; and ICAO Doc 9905, Required Navigation Performance Authorization Required (RNP AR) Procedure Design Manual, Chapter 1, 1.3, Aircraft Qualification, and Chapter 6, 6.3.2.5, Aircraft Eligibility, and 6.3.3, Aircraft Requirements.
Software or hardware changes must be supported by the manufacturer’s updated aircraft qualification and operational documentation.
The multiple configurations of existing and new aircraft make it impossible to give a hard and fast rule. There are some situations where the proposed series has identical capabilities to a foreign air carrier’s existing fleet and this addition provides flexibility to grant the C384 amendment with minimal delay while providing appropriate levels of review for aircraft with differences.
Figure 4-4K. Sample C384 Table 1 – Aircraft and Navigation Systems Eligible for RNP AR
Aircraft1 M/M/S |
Navigation System2 |
Limitations3 |
Autopilot Coupled or Flight Director Required4 |
Lowest RNP5 |
Additional Aircraft Capabilities |
|
M/M |
Software Version |
|||||
|
|
|
Not authorized to use temperature compensation system. Not authorized procedures with missed approaches requiring RNP less than 1.0. None |
Autopilot Coupled with Flight Director Autopilot and/or Flight Director Flight Director only |
RNP |
RF Legs6 Missed approach requiring less than RNP 1.0. |
1 Select the aircraft M/M/S authorized for RNP AR into the United States.
2 Enter navigation system M/M and software version. The specific M/M of navigation equipment, including the current software version installed on each associate aircraft M/M, must be entered in the column labeled “Navigation System.” The Navigation System column is further broken down into two columns: one for M/M and one for the software version. PIs should remind foreign air carriers that any change to C384 (e.g., a change in the software version) constitutes a change to the OpSpec and must be authorized prior to use in U.S. airspace.
3 Enter limitations in the column labeled “Limitations.” If there are no limitations, then select “None” from the dropdown list; do not leave it blank. Enter all applicable limitations as follows:
“Not authorized to use temperature compensation system.” Enter this limitation unless the aircraft has temperature compensation in accordance with AC 90-101, appendix 2, paragraph 3a(7), and the foreign air carrier provides pilot training on the use of the temperature compensation function.
“Not authorized procedures with missed approaches requiring RNP less than 1.0.” Enter this limitation when the aircraft/navigation system does not meet AC 90-101, appendix 2 criteria—approaches with a missed approach less than RNP 1.0.
4 Enter autopilot or FD requirement. RNP AR procedures with RNP values less than RNP 0.3 or with RF legs require the use of autopilot or FD driven by the RNAV system in all cases. In the column labeled “Autopilot Coupled or Flight Director Required,” select one of the following in accordance with the aircraft/navigation system qualification:
“Autopilot Coupled with Flight Director,” or
“Flight Director Only.”
PIs may also select “Autopilot and/or Flight Director” if International Program Division concurrence was received and the foreign air carrier will be training their flightcrews for both autopilot and FD to that RNP value.
5 Enter lowest authorized RNP value in the column labeled “Lowest RNP.” These values will vary depending on the M/M/S and navigation system combination.
Many aircraft will have different RNP values associated with “Autopilot Coupled with Flight Director” or “Flight Director Only” operations.
6 Since all operators in U.S. airspace must have RF leg capability, the “RF Legs” option on the “Additional Aircraft Capabilities” dropdown list must be selected for all foreign air carriers to whom C384 is issued. Any foreign air carrier who does not have RF leg capability must not be issued C384.
Figure 4-4L. RNP AR Approval Checklist (Optional)
SECTION 1: OPERATOR DETAILS, DATE, TYPE OF REQUEST |
||||||
Enter Operator Name: |
||||||
Enter Operator Point of Contact: |
||||||
Select the applicable check box. Initial RNP AR Application* C384 Amendment to RNP AR Request** (Enter details) |
||||||
Enter*** |
||||||
Aircraft M/M/S |
Navigation System |
Limitations |
Autopilot Coupled or FD Required |
RNP |
Aircraft Capabilities |
|
M/M |
Software Version |
|||||
_____ |
______ |
__ |
__________ |
__________ |
__ |
_________ |
_____ |
______ |
__ |
__________ |
__________ |
__ |
_________ |
_____ |
______ |
__ |
__________ |
__________ |
__ |
_________ |
_____ |
______ |
__ |
__________ |
__________ |
__ |
_________ |
Enter date of the application****______________________________ month (MM)/day(DD)/year(YYYY) |
||||||
Figure 4-4L. RNP AR Approval Checklist (Optional) (Continued)
SECTION 2: DOCUMENTATION***** |
Select the applicable check box. Aircraft Qualification Navigation Data Validation Program Established Maintenance Procedures Training (e.g., flightcrew/dispatch) Minimum Equipment List (MEL) Revision (as required) Operational Procedures Requirements RNP Monitoring Program Conditions or Limitations for Approval Dispatch/Flight Following Procedures Validation Successfully Completed (as required) RNP AR Compliance Traceability Matrix/RNP AR Compatibility Trace Matrix |
SECTION 3: COMMENTS (Enter as applicable.) |
Remarks: |
Figure 4-4L. RNP AR Approval Checklist (Optional) (Continued)
SECTION 4: PI ACTIONS (Select the applicable check boxes.) |
|
Kickoff/preapplication meeting scheduled Completed kickoff/preapplication meeting PIs reviewed application and provided recommendation for operations approval as follows: As authorized by CAA With the following additional limitations: _____________________________________ _____________________________________ _____________________________________ _____________________________________ _____________________________________ _____________________________________ Recommend denial of request for the following reasons: _____________________________________ _____________________________________ _____________________________________ _____________________________________ _____________________________________ _____________________________________ _____________________________________ POI Name:____________________________ POI Signature:_________________________ PAI Name:____________________________ PAI Signature:_________________________ |
Front Line Manager’s (FLM) concurrence with PI recommendations. FLM Name: _________________________ FLM Signature: ______________________ PI entered the application into the Headquarters NextGen Tracker and forwarded to AFS-50 on the following date: __________________ Enter MM/DD/YYYY |
Figure 4-4L. RNP AR Approval Checklist (Optional) (Continued)
SECTION 5: JOINT AFS-50 AND AFS-400 DIVISION MANAGEMENT APPROVAL/DISAPPROVAL |
|
Received written joint AFS-50 and AFS‑400 division management concurrence Concurrence date ____________ MM/DD/YYYY Concurrence as requested Concurrence with the following additional limitations and provisions: ___________________________________ ___________________________________ ___________________________________ ___________________________________ ___________________________________ ___________________________________ ___________________________________ ___________________________________ PI issued OpSpec C384 ______________ MM/DD/YYYY |
Received written joint AFS-50 and AFS-400 division management denial Denial date ____________ MM/DD/YYYY Joint AFS-50 and AFS-400 division management denial for the following reasons: ______________________________________ ______________________________________ ______________________________________ ______________________________________ ______________________________________ ______________________________________ ______________________________________ PI notified operator of denial ____________ MM/DD/YYYY |
*Initial application must be checked when no C384 has been issued.
**Amendment request must be checked when an amendment to the basis on which C384 has been issued has been requested by the foreign air carrier. For example, the foreign air carrier completed the required demonstrations for a lower RNP value in U.S. airspace and is requesting an amendment to C384 previously issued by the FAA.
PIs do not need to request an amended joint International Program Division and Flight Technologies and Procedures Division management concurrence memo prior to amending the “Lowest RNP” value if the joint division management concurrence memo authorized a lower RNP value at the end of a specified period, or upon the foreign air carrier’s completion of a number of RNP AR approaches.
***Entries in this block must reflect what the State of the Operator approved the foreign air carrier for. They follow the layout of C384 Table 1.
****Application date refers to the date when all of the required documentation has been provided by the applicant to the PI (see subparagraph g) for details).
*****Airbus Compliance Documents (ACD) and the Boeing companion “RNP Capabilities Documents” are formal, controlled documents detailing the RNP capability of the aircraft and supporting how the customer must operate the aircraft to safely conduct RNP AR approach operations. The FAA cannot determine aircraft eligibility for any Airbus or Boeing aircraft without this documentation to support the foreign air carrier’s claim of eligibility. Due to the variety of Airbus and Boeing aircraft configurations for the various Airbus and Boeing type designs, the FAA cannot rely on a foreign air carrier’s claims of compliance and performance; and, as a result, the FAA requires confirmation from Airbus through the ACD(s) and from Boeing through the RNP Capabilities Document(s).
Vol. 12, Ch. 4
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| File Type | application/vnd.openxmlformats-officedocument.wordprocessingml.document |
| File Modified | 0000-00-00 |
| File Created | 2021-01-15 |