737PBN运行要求的构型能力

稀饭三宝 · 发表于 2016-4-13 08:43:39

分享一份波音的SL，系统阐述737飞机要执行各类PBN（RNAV、RNP）运行所要求的机载构型。
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1. Only applies once 50m (40m, Cat H) obstacle clearance has been obtained at the start of the climb
2. RNAV 5 is an en-route navigation specification which may be used for the initial part of the STAR outside 30 NM and above MSA.
3. The RNP 1 specification is limited to use on STARs, SIDs, the initial and intermediate segments of IAPs and the missed approach after the initial climb phase.
Beyond 30 NM from the ARP, the accuracy value for alerting becomes 2 NM.
4. A-RNP also permits a range of scalable RNP lateral navigation accuracies – see reference a) Part C, Chapter 4, 4.3.3.7.4.
5. Optional – requires higher continuity
6. There are two sections to the RNP APCH specification: Part A is enabled by GNSS and baro-VNAV, Part B is enabled by SBAS which is not yet certified on Boeing airplanes.
7. There are two sections to the RNP APCH specification: Part A is enabled by GNSS and baro-VNAV, Part B is enabled by SBAS which is not yet certified on Boeing airplanes.
8. The RNP 0.3 specification is primarily intended for helicopter operations and does not apply to Boeing airplanes.
9. RNP Approach requires Standby Power for the left FMCS and left CDS (cut into production for all airplanes starting at line position 2252 (delivered May 2007)).
a - The navigation application is limited to use on STARS and SIDs only
b- The area of application can only be used after the initial climb of a missed approach phase
c- Beyond 30 NM from the airport reference point (ARP), the accuracy value for alerting becomes 2 N
ATTACHMENT II To: 737-SL-02-025t
16 June 2015
Page 1 of 10
Detailed Airplane Configurations for PBN RNP Designators
RNAV 10 (Designated and Authorized as RNP-10)
The following is the minimum equipment recommended to qualify for RNAV 10 (RNP-10) operations:
• 2 -Inertial Reference Systems
• 2 -Flight Management Computers
• 2 – CDU or MCDU
• 2 EFIS/MAP or PFD/ND displays configurations
• 2 Display Electronic Units or EFIS Symbol Generators *
• 1 FCC
• 1 Flight Director
• Autopilot coupled
• Current Navigation Database
• Communications (see note)
*Single configuration requires regulatory agency approval.
Note:
The ICAO PBN manual does not specify communication requirements for RNAV 10 / RNP-10. Operators should assure that their airplane conforms to regulatory requirements specified for their area of operations. Dual HF systems are one acceptable means of meeting RNP 10 communication requirements.
For inertial coasting as primary means of navigation, the 737 is limited based upon IRS drift rate to 6.2 hours after a full IRS alignment. Global Positioning System (GPS) Sensor input to the navigation solution is required to lift the time limitation.
ATTACHMENT II To: 737-SL-02-025
16 June 2015
Page 2 of 10
Export Controlled ECCN: 9E991
BOEING PROPRIETARY
Detailed Airplane Configurations for PBN RNP Designators (continued)
RNAV-5 (Basic RNAV)
The following is the minimum equipment recommended to qualify for RNAV 5 operations:
• 2 Inertial Reference Systems
• 1 Flight Management Computer
• 1 CDU or MCDU
• Any of the following navigation sensors:
o DME receiver for DME/DME radio updating
o VOR VHF with DME receiver for VOR/DME radio updating.
o GPS Receiver
 Single Multi-mode Receivers with GPS functionality (737-600/700/800/900/900ER)
 Single analog Multi-mode Receivers with GPS functionality or GPSSUs (737-300/400/500)
• 2 EFIS/MAP or PFD/ND displays configurations
• 2 Display Electronic Units or EFIS Symbol Generators *
• 1 FCC
o 1 Flight Director
• Current Navigation Database
*Single configuration requires regulatory agency approval.
ATTACHMENT II To: 737-SL-02-025
16 June 2015
Page 3 of 10
Export Controlled ECCN: 9E991
BOEING PROPRIETARY
Detailed Airplane Configurations for PBN RNP Designators (continued)
RNP-4
The following is the minimum equipment recommended to qualify for RNP-4 operations:
• 2 -Inertial Reference Systems
• 2 –Flight Management Computers (U10.7 and later)
• 2 –MCDUs -FANS capable.
• 2- GPS Receivers
o Multi-mode Receivers with GPS functionality(737-600/700/800/900/900ER)
o Analog Multi-mode Receivers with GPS functionality or GPSSUs (737-300/400/500)
• FANS activation*
o SATCOM
o ACARS or CMU / 737 classics 8 MCDU
• 2 EFIS/MAP or PFD/ND displays configurations
• 2 Display Electronic Units or EFIS Symbol Generators
• 2 FCCs
o 2 Flight Directors
o Autopilot coupled
• Current Navigation Database
*Must be Aircraft Equipment Interoperability Test (AEIT) compliant.
Note:
Either DME receiver for DME/DME or VHF VOR receiver with DME receiver for VOR/DME for radio updating is not required but is not required to be disabled.
Alternate means of meeting RNP 4 communication requirements may be acceptable to your regulatory agency. Verify RNP 4 communication equipment requirements with your regulatory agency during operational approval.
ATTACHMENT II To: 737-SL-02-025
16 June 2015
Page 4 of 10
Export Controlled ECCN: 9E991
BOEING PROPRIETARY
Detailed Airplane Configurations for PBN RNP Designators (continued)
RNP-2
The following is the minimum equipment recommended to qualify for RNP-2 operations:
• 2 Inertial Reference Systems
• 2 Flight Management Computers
• 2 CDUs or MCDUs*
• 2- GPS Receivers*
o Multi-mode Receivers with GPS functionality(737-600/700/800/900/900ER)
o Analog Multi-mode Receiver with GPS functionality or GPSSUs (737-300/400/500)
• 2 EFIS/MAP or PFD/ND displays configurations
• 2 Display Electronic Units or EFIS Symbol Generators*
• 1 FCC
• 1 Flight Director
• Current Navigation Database
*Single configuration requires regulatory agency approval.
Note:
Sensor input other than GPS requires agency approval.
Either DME receiver for DME/DME or VHF VOR receiver with DME receiver for VOR/DME for radio updating is not required and is not required to be disabled.
ATTACHMENT II To: 737-SL-02-025
16 June 2015
Page 5 of 10
Export Controlled ECCN: 9E991
BOEING PROPRIETARY
Detailed Airplane Configurations for PBN RNP Designators (continued)
RNAV 1 AND RNAV 2
The following is the minimum equipment recommended to qualify for RNAV 1 and RNAV 2 operations:
• 2 Inertial Reference Systems
• 1 Flight Management Computer
• 1 CDU or MCDU
• Any of the following navigation sensors:
o DME receiver for DME/DME radio updating
o VOR VHF with DME receiver for VOR/DME
o GPS Receiver
 Single Multi-mode Receivers with GPS functionality(737-600/700/800/900/900ER)
 Single analog Multi-mode Receivers with GPS functionality or GPSSUs (737-300/400/500)
• 2 EFIS/MAP or PFD/ND displays configurations
• 2 Display Electronic Units or EFIS Symbol Generators*
• 1 FCC
o 1 Flight Director
• Current Navigation Database
*Single configuration requires regulatory agency approval.
ATTACHMENT II To: 737-SL-02-025
16 June 2015
Page 6 of 10
Export Controlled ECCN: 9E991
BOEING PROPRIETARY
Detailed Airplane Configurations for PBN RNP Designators (continued)
RNP-1
The following is the minimum equipment recommended to qualify for RNP-1 operations:
• 2 Inertial Reference Systems
• 2 Flight Management Computers
• 2 CDUs or MCDUs*
• Dual sensors of either:
o DME receiver for DME/DME radio updating
o GPS Receiver
 Single Multi-mode Receivers with GPS functionality(737-600/700/800/900/900ER)
 Single analog Multi-mode Receivers with GPS functionality or GPSSUs (737-300/400/500)
• 2 EFIS/MAP or PFD/ND displays configurations
• 2 Display Electronic Units or EFIS Symbol Generators *
• 1 FCC
o 1 Flight Director
• Current Navigation Database
*Single configuration requires regulatory agency approval.
Note:
A single 737NG DME receiver can tune up to four DME channels as inputs into both FMCs. This allows a single DME to support a dual FMC configuration.
ATTACHMENT II To: 737-SL-02-025
16 June 2015
Page 7 of 10
Export Controlled ECCN: 9E991
BOEING PROPRIETARY
Detailed Airplane Configurations for PBN RNP Designators (continued)
Advanced RNP (A-RNP)
The A-RNP is intended to simply the process of obtaining operational approval for multiple ICAO PBN operations, which could include RNAV 5, RNAV 2, RNAV 1, RNP 2, RNP 1 and RNP APCH. Regulatory agency airplane qualification requirements for Advanced RNP are evolving.
At the date of publication of this service letter, the only required feature of A-RNP is RF leg capability. All 737 airplanes equipped with FMC with OPS software U10.7 or higher meet this requirement.
A 737 airplane which that meets the 737 RNP AR airplane qualification requirements will qualify for the A-RNP requirements defined in the current (4th) edition of the ICAO PBN Manual.
ATTACHMENT II To: 737-SL-02-025
16 June 2015
Page 8 of 10
Export Controlled ECCN: 9E991
BOEING PROPRIETARY
Detailed Airplane Configurations for PBN RNP Designators (continued)
RNP APCH
The following list is the minimum equipment recommended to qualify for RNP-APCH operations:
• 2 Inertial Reference Systems
• 2 Flight Management Computers* (See FMC RNP Capabilities Document for appropriate software required)
• 2 CDUs or MCDUs*
• 2 GPS Receivers*
o Multi-mode Receiver with GPS functionality(737-600/700/800/900/900ER)
o Analog Multi-mode Receiver with GPS functionality or GPSSUs (737-300/400/500)
• 2 EFIS/MAP or PFD/ND displays configurations
• 2 Display Electronic Units or EFIS Symbol Generators*
• 1 FCC
• 1 Flight Director
• Current Navigation Database
*Single configuration requires regulatory agency approval.
ATTACHMENT II To: 737-SL-02-025
16 June 2015
Page 9 of 10
Export Controlled ECCN: 9E991
BOEING PROPRIETARY
Detailed Airplane Configurations for PBN RNP Designators (continued)
RNP AR
The following list is the minimum equipment recommended to qualify for RNP-AR operations:
• 2 Inertial Reference Systems
• 2 Flight Management Computers (See FMC RNP Capabilities Document for appropriate OFP software required)
• 2 CDUs or MCDUs
• 2 GPS Receivers*
o Multi-mode Receivers with GPS functionality(737-600/700/800/900/900ER)
o Analog Multi-mode Receivers with GPS functionality or GPSSUs (737-300/400/500)
• 2 Radio Altimeters
• 2 Independent Air Data Systems
• 2 EFIS/MAP or PFD/ND displays (as installed)
• 2 Display Electronic Units or EFIS Symbol Generators(as installed)
• 2 FCCs
o 2 Flight Directors
• Current Navigation Database
• EGPWS
* RNP AR APCH authorization is based on GNSS as the primary NAVAID infrastructure. The use of DME/DME as the alternative means of achieving area navigation may be authorized for individual operators when the DME infrastructure supports the RNP and when authorized by the State. RNP AR APCH shall not be used in areas of known navigation signal (GNSS) interference. Input from DME for position updating may be enabled during approach operations while dual GPS is the primary means of navigation.
Note:
Regulatory agency minimum equipment/functionality requirements may differ.
• NPS may be required based on regulatory agency requirements for monitoring total system error (TSE).
• Autopilot Coupled
• Go-Around Roll Mode – LNAV
ATTACHMENT II To: 737-SL-02-025
16 June 2015
Page 10 of 10
Export Controlled ECCN: 9E991
BOEING PROPRIETARY
Detailed Airplane Configurations for PBN RNP Designators (continued)
BARO VNAV
All Boeing 737 FMCs have been demonstrated to meet the requirements of Advisory Circular 20-129 for vertical navigation (VNAV) and terminal area operation and instrument approaches (excluding ILS G/S), as defined in the Airplane Flight Manual (AFM). The 737 FMC Baro VNAV function has been analyzed and determined to meet EASA AMC 20-27 requirements.

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