# N454PA: 2002 Boeing 747-46NF - Status: Valid registration - Airframe: [Boeing 747-46NF](https://openairdocs.org/model/boeing-747-46nf) (registry code 13848BT, 366 seats) - Engine: [GE CF6-80 series](https://openairdocs.org/engine/ge-cf6-80-series) (registry code 30025) - Data sheets: [TCDS E13NE](https://openairdocs.org/tcds/E13NE) (General Electric Company GE Aerospace) (OpenAirDocs) - Serial number: 30812 - Year built: 2002 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: July 19, 2002 - Certificate issued: August 2, 2022 - Expires: August 31, 2029 - Mode S code: A5823E - Registered owner: [Atlas Air Inc](https://openairdocs.org/faa-owner/ATLAS%20AIR%20INC) - Location: [Purchase, NY](https://openairdocs.org/faa-place/NY/Purchase) - Owner type: Corporation - Owner's area on the map: 41.0382° N, 73.7107° W: Placed by OpenAirDocs at the center of ZIP code 10577, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=454PA - Page: https://openairdocs.org/aircraft/N454PA From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination. The registry lists only the engine series, so ADs for every GE CF6-80 model are included. ## ADs that may apply (OpenAirDocs): 61 in force ### Matched by airframe (Boeing 747-46NF) None in force. ### Matched by engine (GE CF6-80 series) - [AD 2024-24-03](https://openairdocs.org/ad/2024-24-03): Engine Exhaust · Boeing MD-11, MD-11F and CF6-80C2D1F. Effective Jan 13, 2025 - [AD 2023-20-08](https://openairdocs.org/ad/2023-20-08): Engine (Turbine/Turboprop) · General Electric CF6-80C2B1F, CF6-80C2B2F, CF6-80C2B4F and 4 more. Effective Oct 19, 2023 - [AD 2021-26-22](https://openairdocs.org/ad/2021-26-22): Turbine Section · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 21 more. Effective Mar 14, 2022 - [AD 2022-02-18](https://openairdocs.org/ad/2022-02-18): Engine Mount Section · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 3 more. Effective Feb 25, 2022 - [AD 2021-14-11](https://openairdocs.org/ad/2021-14-11): Turbine Section · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 25 more. Effective Aug 27, 2021 - [AD 2021-03-02](https://openairdocs.org/ad/2021-03-02): Fuel Control/Turbine Engines · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 16 more. Effective Mar 31, 2021 - [AD 2020-22-02](https://openairdocs.org/ad/2020-22-02): Engine Fuel and Control · General Electric CF6-80C2A5F, CF6-80C2B1F, CF6-80C2B2F and 13 more. Effective Dec 3, 2020 - [AD 2018-07-05](https://openairdocs.org/ad/2018-07-05): Turbine Section · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 1 more. Effective May 11, 2018 - [AD 2017-11-15](https://openairdocs.org/ad/2017-11-15): Turbine/ Turboprop Engine--Turbine Section · General Electric CF6-80C2L1F. Effective Jul 13, 2017 - [AD 2016-08-10](https://openairdocs.org/ad/2016-08-10): Accessory heat shield · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 26 more. Effective Jun 1, 2016 - [AD 2014-21-01](https://openairdocs.org/ad/2014-21-01): Fuel manifold · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 26 more. Effective Nov 28, 2014 - [AD 2013-08-20](https://openairdocs.org/ad/2013-08-20): Fuel tube · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 14 more. Effective May 31, 2013 - [AD 2012-03-12](https://openairdocs.org/ad/2012-03-12): No. 3 bearing packing · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 21 more. Effective Apr 5, 2012 - [AD 2012-04-05](https://openairdocs.org/ad/2012-04-05): Electronic control unit (ECU) · General Electric CF6-80C2B1F, CF6-80C2B1F1, CF6-80C2B1F2 and 8 more. Effective Mar 30, 2012 - [AD 2011-23-04](https://openairdocs.org/ad/2011-23-04): Forward engine mount assembly side links · General Electric CF6-45A, CF6-45A2, CF6-50A and 14 more. Effective Dec 12, 2011 - [AD 2009-21-07](https://openairdocs.org/ad/2009-21-07): Thrust and thrust control · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 21 more. Effective Dec 1, 2009 - [AD 2009-14-08](https://openairdocs.org/ad/2009-14-08): High-pressure compressor rotor (HPCR) stages 11-14 spool/ shafts · General Electric CF6-80C2B5F. Effective Aug 5, 2009 - [AD 2009-08-06](https://openairdocs.org/ad/2009-08-06): Stage 1 high-pressure turbine (HPT) rotor disks · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 1 more. Effective May 18, 2009 - [AD 2009-07-10](https://openairdocs.org/ad/2009-07-10): High-pressure turbine rotor (HPTR) · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 1 more. Effective May 6, 2009 - [AD 2009-07-03](https://openairdocs.org/ad/2009-07-03): Eddy current inspection (ECI) · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 26 more. Effective Apr 30, 2009 - [AD 2009-04-10](https://openairdocs.org/ad/2009-04-10): Critical life-limited parts · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 30 more. Effective Mar 30, 2009 - [AD 2008-21-11](https://openairdocs.org/ad/2008-21-11): Low-pressure turbine (LPT) cases · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 25 more. Effective Nov 28, 2008 - [AD 2008-02-17](https://openairdocs.org/ad/2008-02-17): Thrust reverser actuation systems · General Electric CF6-50A, CF6-50C, CF6-50C1 and 16 more. Effective Feb 28, 2008 - [AD 2007-24-07](https://openairdocs.org/ad/2007-24-07): Thermal spray coating on certain stage 1 fan disks · General Electric CF6-80C2B1. Effective Jan 2, 2008 - [AD 2007-22-07](https://openairdocs.org/ad/2007-22-07): Electronic control unit (ECU) · General Electric CF6-80C2D1F. Effective Nov 28, 2007 - [AD 2007-21-06](https://openairdocs.org/ad/2007-21-06): Electronic control unit (ECU) · General Electric CF6-80C2A5F. Effective Nov 15, 2007 - [AD 2007-11-20](https://openairdocs.org/ad/2007-11-20): Fuel shroud retaining rings · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 22 more. Effective Jul 10, 2007 - [AD 2007-05-14](https://openairdocs.org/ad/2007-05-14): Cast titanium weld- repaired forward engine mount platforms · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 16 more. Effective Apr 9, 2007 - [AD 2006-16-06](https://openairdocs.org/ad/2006-16-06): Certain stage 1 high- pressure turbine (HPT) rotor disks · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 21 more. Effective Sep 5, 2006 - [AD 2006-06-08](https://openairdocs.org/ad/2006-06-08): Latching system of the fan reverser · General Electric CF6-80C2D1F. Effective Apr 25, 2006 - [AD 2005-17-05](https://openairdocs.org/ad/2005-17-05): High pressure compressor rotor (HPCR) · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 25 more. Effective Sep 27, 2005 - [AD 2005-06-07](https://openairdocs.org/ad/2005-06-07): Directional pilot valve (DPV) assembly · General Electric CF6-80A1, CF6-80A3, CF6-80C2A1 and 5 more. Effective Apr 25, 2005 - [AD 2004-22-07](https://openairdocs.org/ad/2004-22-07): Stage 2 nozzle guide vanes (HPT S2 NGVs) · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 16 more. Effective Dec 1, 2004 - [AD 2004-07-13](https://openairdocs.org/ad/2004-07-13): High pressure turbine (HPT) stage 1 disks · General Electric CF6-80C2A5F, CF6-80C2B5F, CF6-80C2B7F and 1 more. Effective May 6, 2004 - [AD 2003-12-08](https://openairdocs.org/ad/2003-12-08): Directional pilot valve · General Electric CF6-80A1, CF6-80A3, CF6-80C2A1 and 5 more. Effective Jul 23, 2003 - [AD 2003-02-07](https://openairdocs.org/ad/2003-02-07): Low pressure turbine (LPT) shrouds · General Electric CF6-50A, CF6-50C, CF6-50C1 and 30 more. Effective Mar 3, 2003 - [AD 2002-25-08](https://openairdocs.org/ad/2002-25-08): High pressure compressor rotor · General Electric CF6-45A, CF6-45A2, CF6-50A and 40 more. Effective Jan 23, 2003 - [AD 2002-22-12](https://openairdocs.org/ad/2002-22-12): Titeflex hoses · BAE Systems ATP, Avro 146-RJ100A, Avro 146-RJ70A and 122 more. Effective Dec 13, 2002 - [AD 2001-06-09](https://openairdocs.org/ad/2001-06-09): Aft Engine Mount Link Assemblies · General Electric CF6-80A3. Effective May 1, 2001 - [AD 2000-12-08](https://openairdocs.org/ad/2000-12-08): Mount Link Assemblies · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 4 more. Effective Aug 28, 2000 - [AD 2000-03-04](https://openairdocs.org/ad/2000-03-04): General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 19 more. Effective Apr 10, 2000 - [AD 99-01-01](https://openairdocs.org/ad/99-01-01): Accessory Gearbox (AGB) idler adapters · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 19 more. Effective Jan 21, 1999 - [AD 98-22-06](https://openairdocs.org/ad/98-22-06): Fan Disks · General Electric CF6-45A, CF6-45A2, CF6-50A and 41 more. Effective Nov 23, 1998 - [AD 97-22-14](https://openairdocs.org/ad/97-22-14): (HPCR) 3-9 Spool · General Electric CF6-50A, CF6-50C, CF6-50C1 and 29 more. Effective Nov 17, 1997 - [AD 96-16-07](https://openairdocs.org/ad/96-16-07): Rear Right Hand Mount Link · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 17 more. Effective Aug 28, 1996 - [AD 95-17-16](https://openairdocs.org/ad/95-17-16): Compressor Rear Frame · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 1 more. Effective Nov 7, 1995 - [AD 95-10-11](https://openairdocs.org/ad/95-10-11): Fan Reversers · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 17 more. Effective May 31, 1995 - [AD 94-20-06](https://openairdocs.org/ad/94-20-06): Oil System · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 16 more. Effective Dec 27, 1994 - [AD 94-07-04](https://openairdocs.org/ad/94-07-04): High Pressure Turbine Disk · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 1 more. Effective May 23, 1994 - [AD 94-06-03](https://openairdocs.org/ad/94-06-03): High Pressure Turbine Disk · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 16 more. Effective Apr 29, 1994 ### Historical (superseded or no longer in force) - [AD 2020-20-13](https://openairdocs.org/ad/2020-20-13) (historical): Turbine Section · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 21 more. Effective Nov 12, 2020 - [AD 2018-15-04](https://openairdocs.org/ad/2018-15-04) (historical): Turbine/Turboprop Engine--Turbine Section · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 21 more. Effective Oct 2, 2018 - [AD 2009-05-02](https://openairdocs.org/ad/2009-05-02) (historical): Drainless fuel manifold assemblies · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 26 more. Effective Mar 31, 2009 - [AD 2007-12-07](https://openairdocs.org/ad/2007-12-07) (historical): Electronic control units (ECUs) · General Electric CF6-80C2B1F, CF6-80C2B2F, CF6-80C2B4F and 5 more. Effective Jul 11, 2007 - [AD 2006-12-24](https://openairdocs.org/ad/2006-12-24) (historical): Five-link forward mount assembly · General Electric CF6-45A, CF6-45A2, CF6-50A and 14 more. Effective Jul 21, 2006 - [AD 2004-04-07](https://openairdocs.org/ad/2004-04-07) (historical): Stage 1 HPT rotor disks · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 21 more. Effective Mar 12, 2004 - [AD 2003-01-05](https://openairdocs.org/ad/2003-01-05) (historical): Dovetail slots · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 1 more. Effective Jan 28, 2003 - [AD 2002-07-12](https://openairdocs.org/ad/2002-07-12) (historical): Life Limits Section of Continued Airworthiness (ICA) - Selected Critical Life-limited Parts · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 27 more. Effective May 15, 2002 - [AD 2001-10-07](https://openairdocs.org/ad/2001-10-07) (historical): High Pressure Turbine Rotor Disks · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 19 more. Effective Jun 18, 2001 - [AD 2000-08-12](https://openairdocs.org/ad/2000-08-12) (historical): Life-limited Parts · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 10 more. Effective Oct 23, 2000 - [AD 2000-16-12](https://openairdocs.org/ad/2000-16-12) (historical): High Pressure Compressor Rotor Stage 3-9 Spools · General Electric CF6-45A, CF6-45A2, CF6-50A and 39 more. Effective Sep 5, 2000 - [AD 2000-04-14](https://openairdocs.org/ad/2000-04-14) (historical): Fuel tube flange seating · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 12 more. Effective May 1, 2000 - [AD 99-24-15](https://openairdocs.org/ad/99-24-15) (historical): High Pressure Compressor Rotor (HPCR) Stage 3-9 Spools · General Electric CF6-45A, CF6-45A2, CF6-50A and 39 more. Effective Jan 28, 2000 - [AD 99-18-20](https://openairdocs.org/ad/99-18-20) (historical): Inadvertent In-flight Thrust Reverser · General Electric Aircraft Engines CF6-50 Series (all), CF6-80A1, CF6-80A3 and 6 more. Effective Nov 2, 1999 - [AD 99-18-19](https://openairdocs.org/ad/99-18-19) (historical): Inadvertent Thrust Reverser · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 7 more. Effective Sep 24, 1999 - [AD 99-08-13](https://openairdocs.org/ad/99-08-13) (historical): General Electric CF6-80A, CF6-80A1, CF6-80A2 and 26 more. Effective May 13, 1999 - [AD 98-15-17](https://openairdocs.org/ad/98-15-17) (historical): Link Assembly · General Electric CF6-80A3. Effective Aug 7, 1998 - [AD 91-20-02](https://openairdocs.org/ad/91-20-02) (historical): Fuel Manifolds · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 12 more. Effective Nov 25, 1991 - [AD 90-26-01](https://openairdocs.org/ad/90-26-01) (historical): Fuel Manifold Systems · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 11 more. Effective Dec 20, 1990 All 80: https://openairdocs.org/aircraft/N454PA/ads.md ## Information bulletins (advisory) (5 in force) - [SAIB 2023-15](https://openairdocs.org/saib/2023-15): Falsified Forms from AOG Technics. Issued Dec 19, 2023 - [SAIB NE-11-27](https://openairdocs.org/saib/NE-11-27): Fuel Injector Nozzle - CF6-80 Improperly Welded Fuel Nozzles. Issued Apr 5, 2011 - [SAIB NE-10-37](https://openairdocs.org/saib/NE-10-37): Engine Fuel and Control: FADEC Fuel Metering Valve Resolver Feedback Faults. Issued Jul 12, 2010 - [SAIB NE-08-44](https://openairdocs.org/saib/NE-08-44): Engine Thrust Reverser Transcowl Clevis Pin. Issued Sep 3, 2008 - [SAIB NE-07-01](https://openairdocs.org/saib/NE-07-01): Dual engine flameouts on twin engine airplanes. Issued Oct 12, 2006 ## NTSB investigations None matched to N454PA. ## FAA accident and incident reports None matched to N454PA. ## Service difficulty reports (176, newest 50) As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR UIEA2026072400646](https://openairdocs.org/sdr/UIEA2026072400646), Jul 24, 2026: GENERATOR. FAULTED. CREW SET UP IAW DDG 49-11-01. CREW ISOLATED THAT LT PNEUMATIC & RT UTILITY. CREW STARTED NR 4 ENG. DURING START, AT THE TIME, NR 4 ENG GOING TO TAKE OVER POWER - [SDR UIEA2026072400654](https://openairdocs.org/sdr/UIEA2026072400654), Jul 24, 2026: RADAR. FAULTED. RADAR INTERMITTENT AND INAUCCURATE, NOT PAINTING ANY WEATHER. PERFORMED OPERATIONAL TEST PER AMM 33-43-00/501. NO ISSUES NOTED AT THE TIME. - [SDR UIEA2026041900218](https://openairdocs.org/sdr/UIEA2026041900218), Apr 18, 2026: OIL SYSTEM. LEAKING. ENG #1 OIL QTY DROPPED TO 1 AFTER T/O, FOLLOW WITHIN 20 MINS BY ENG OIL PRESS ADVISORY MSG. QRH FOLLOWED, AND ENG #1 WAS SHUT DOWN. WITHIN 15 MINS OF ENG SHUTDO - [SDR UIEA2026021600053](https://openairdocs.org/sdr/UIEA2026021600053), Feb 15, 2026: SHEAR TIE. CRACKED. FOUND CRACK ON SHEAR TIE AT BS 1000 RBL 33.99. REMOVED DAMAGE SHEAR TIE IAW SRM 51-40-02-0G-0 REV 115. INSTALL NEW SHEAR TIE IAW EI T2026A53M-210 REV 0 AND EO 4 - [SDR UIEA2026021600054](https://openairdocs.org/sdr/UIEA2026021600054), Feb 15, 2026: WEB. CORRODED. FOUND RT WING INBD FORE FLAP INTERNAL INBD SIDE WEB CRACKED. REMOVED DAMAGED WEB IAW SRM 51-40-02-0G-0 REV 105. 2. INSTALL A NEW WEB IAW EI T2026A57M-236 REV 0 - [SDR UIEA2026021600055](https://openairdocs.org/sdr/UIEA2026021600055), Feb 15, 2026: SEAT TRACK. CORRODED. FOUND M/D CGO SUBSTITUTE SEAT TRACK CRACK AT STA 1633 RBL 75.92. ACCOMPLISHED WORK SHEET 60030 AND IAW SRM 53-00-52-2R-13 REV 105 AND DWG 65B38751 SH62 REV A ,S - [SDR UIEA2026021600056](https://openairdocs.org/sdr/UIEA2026021600056), Feb 15, 2026: SEAT TRACK. CORRODED. CRACK - ON M/D FLOOR SUBSTITUTE SEAT TRACK AT STA 2070 RBL 75.92. ACCOMPLISHED WORK SHEET 60035 AND IAW SRM 53-00-52-2R-13 REV 105. JOB COMPLETED. - [SDR UIEA2026021600057](https://openairdocs.org/sdr/UIEA2026021600057), Feb 15, 2026: SEAT TRACK. CORRODED. FOUND M/D CARGO SUBSTITUTE SEAT TRACK CRACKED AT BS 1507, RBL 75.92. ACCOMPLISHED WORK SHEET NO: 60029 IAW SRM 53-00-52-2R-13 REV 105 AND DWG 65B38251 SH62 REV - [SDR UIEA2026021600058](https://openairdocs.org/sdr/UIEA2026021600058), Feb 15, 2026: SEAT TRACK. CORRODED. CORROSION ON M/D SEAT TRACK BS 700, RBL 33.99. PERFORM EI T2026A53M-256 REV 0 AND W/S NO: 60039 (SRM 53-00-52-2R-6 REV 105). ACCOMPLISH EI NO: T2026A53M-216 REV - [SDR UIEA2026021600059](https://openairdocs.org/sdr/UIEA2026021600059), Feb 15, 2026: CARGO TRACK. CORRODED. FOUND M/D CARGO TRACK CORRODED AT BS 1519, RBL 11.33. REMOVED AFFECTED FASTENERS TO GET ACCESS IAW SRM 51-40-02-0G-0 REV 105. REPAIR DAMAGE AREA IAW EI T2026A53 - [SDR UIEA2026021600060](https://openairdocs.org/sdr/UIEA2026021600060), Feb 15, 2026: DOOR SILL. NOT REPORTED. FWD LWR CARGO DOOR SURROUND LWR MAIN SILL WEB & OTR CHORD, LATCH SUPPORT FITTING PART 1 TIME LIMITED REPAIR STA 580 REQUIRES EO PART 2 HFEC INSPECTION & EO PART - [SDR UIEA2026021600061](https://openairdocs.org/sdr/UIEA2026021600061), Feb 15, 2026: ACTUATOR. FAULTED. FND FUNCTION FAIL AT R/H WLG ALTERNATE EXTENSION ROTARY ACTUATOR. REPLACED RT WLG ALTERNATE ROTARY ACTUATOR IAW AMM 32-36-01-004-001 REV 115 & AMM 32-36-01-404- - [SDR UIEA2025102801282](https://openairdocs.org/sdr/UIEA2025102801282), Oct 28, 2025: FIRE WARNING. FALSE ACTIVATION. CREW REPORTED DURING CRUISE, CARGO FIRE MAIN DECK ZONE 11 EICAS MSG. FOUND MESSAGE 26330/26331 NOT ACTIVE. CREW CONFIRMED NO ACTUAL SMOKE/FIRE ON MAIN DECK. CAR - [SDR UIEA2025102601281](https://openairdocs.org/sdr/UIEA2025102601281), Oct 26, 2025: EXHAUST FAN. ODOR. SMOKE SMELL IN COCKPIT. R & R COOLING EXHAUST FAN PER AMM 21-58-01. OPS CHK NORMAL. - [SDR UIEA2025020300114](https://openairdocs.org/sdr/UIEA2025020300114), Feb 3, 2025: MODULE. FAILED. ARCING SOUND HEARD FROM OVERHEAD PANEL ACCOMPANIED MOMENTARILY BY FIRE LIGHTS IN APU FIRE SWITCH.(

REMOVED AND REPLACED ENG/ APU FIRE EXT MODULE PER B747 AMM - [SDR UIEA2025010400004](https://openairdocs.org/sdr/UIEA2025010400004), Jan 5, 2025: PCB. DAMAGED. APU FIRE SWITCH ILLUMINATED INTERMITTENTLY FOR SEVERAL HOURS. A FEW TIMES FIRE APU WARNING EICAS MESSAGE ALSO DISPLAYED FOR A SPLIT SECOND. ALSO, CAN HEAR APU F - [SDR UIEA2024092500947](https://openairdocs.org/sdr/UIEA2024092500947), Sep 24, 2024: FIRE WARNING. FALSE ACTIVATION. APU FIRE MSG. COMPLIED WITH QRH 8.1. DISCHARGED APU FIRE BOTTLE(

DEACTIVATED APU AND TRANSFER TO DMI 217433 PER MEL 26-22-01 CAT C DUE DATE 5OCT24. R/R APU FI - [SDR UIEA2024071400670](https://openairdocs.org/sdr/UIEA2024071400670), Jul 14, 2024: OIL SYSTEM. PRESSURE LOSS. ENG 1 IFSD (OIL QTY & PRESSURE LOSS). R & R #1 ENG PER WO 133424. C/W ENG IDLE RUN IAW AMM 71-00-00, OPS CHECK GOOD. NO FAULTS OR LEAKS. - [SDR UIEA2024022300113](https://openairdocs.org/sdr/UIEA2024022300113), Mar 3, 2024: STRUCTURE. CRACKED. FX AIRCON BAY LH STA 1240 LBL 105" O/B CENTER SECTION LOWER CHORD CRACK(

CRACK CHORD REPLACED AS PER SRM 51-10-01 AND NEW CHORD HOLE TRANSFERRED AS PER SRM 51 - [SDR UIEA2024022300114](https://openairdocs.org/sdr/UIEA2024022300114), Mar 3, 2024: CLOSEOUT PANEL. CRACKED. M/D STA 1241 LBL 77-99 CLOSEURE PNL FOUND CRACK(

CLOSURE PNL REPLACED AS PER SRM 51-10-02 AND NEW PANEL HOLES TRANSFERRED AS PER SRM 51-40-05 AND NEW PANEL IN - [SDR UIEA2024022300115](https://openairdocs.org/sdr/UIEA2024022300115), Mar 3, 2024: WEB. UNKNOWN. MDDR 177930 REF EA-4453A0008 REV 0 AFT CARGO COMPARTMENT LATERAL BEAM UPPER FLOOR WEB AT STA 1840-1860 LBL 45.5 PERMANENT REPAIR (WITHIN 2000FC AFTER REPAIR OR - [SDR UIEA2024022300116](https://openairdocs.org/sdr/UIEA2024022300116), Mar 3, 2024: BEAM. CORRODED. AFT CARGO DOOR INNER SURFACE LOWER DOOR LINER CLOSE OUT BEAM SURFACE CORR FROM STA 1780-1920 SEVEN PLACES(

BEAM 6 LOCATIONS CORROSION REMOVED WITHIN SRM 52-30 - [SDR UIEA2024022300117](https://openairdocs.org/sdr/UIEA2024022300117), Mar 3, 2024: SKIN. PUNCTURED. #2 ENG R/H CORE UPPER SECTION 10" (COUNT FROM AFT) EXT SURFACE FOUND PUNCH HOLE(

#2 ENG R/H CORE COWL UPPER SECTION TITANIUM FAIRING EXTERNAL DOUBLER REPAIRED - [SDR UIEA2024022300118](https://openairdocs.org/sdr/UIEA2024022300118), Mar 3, 2024: CHANNEL. CRACKED. EMP L/H HORI STAB MOST O/B T/E WEDGE 'U' CHANNEL FOUND CRACK(

CRACK CHANNEL REPLACED AND INSTALLED AS PER RI-55-10-16734 REV A. NO FURTHER DEFECTS NOTED

) - [SDR UIEA2024022300119](https://openairdocs.org/sdr/UIEA2024022300119), Mar 3, 2024: STRUCTURE. CRACKED. EMP L/H HORI STAB MOST O/B WEB UPPER CHORD FOUND CRACK(

UPPER CHORD REPLACED AS PER SRM 51-10-02 AND NEW UPR CHORD HOLES TRANSFERED AS PER SRM 51-40-05 AND NE - [SDR UIEA2024022300120](https://openairdocs.org/sdr/UIEA2024022300120), Mar 3, 2024: WEB. CRACKED. EMP - L/H HORI STAB MOST O/B WEB FOUND CRACK(

WEB REPLACED AS PER SRM 51-10-02 AND NEW WEB HOLES TRANSFERRED AS PER SRM 51-40-05 AND NEW WEB INSTALLED AS PER - [SDR UIEA2024022300121](https://openairdocs.org/sdr/UIEA2024022300121), Mar 3, 2024: STRUCTURE. CRACKED. EMP - L/H HORI STAB MOST O/B WEB LOWER CHORD FOUND CRACK(

LOWER CHORD REPLACED AS PER SRM 51-10-02 AND NEW LOWER CHORD HOLES TRANSFERRED AS PER SRM 51-40-05 A - [SDR UIEA2024022300122](https://openairdocs.org/sdr/UIEA2024022300122), Mar 3, 2024: CHANNEL. CRACKED. EMP R/H HORI STAB MOST O/B T/E WEDGE 'U' CHANNEL CRACK(

'U' CHANNEL REPLACED AS PER RI-55-10-16735 REV A. NO FURTHER DEFECTS NOTED

) - [SDR UIEA2024022300123](https://openairdocs.org/sdr/UIEA2024022300123), Mar 3, 2024: STRUCTURE. CRACKED. EMP - R/H HORI STAB MOST O/B WEB UPPER CHORD CRACK(

UPPER CHORD REPLACED AS PER SRM 51-10-02 AND NEW UPPER CHORD HOLES TRANSFERRED AS PER SRM 51-40-05 AND NEW - [SDR UIEA2024022300124](https://openairdocs.org/sdr/UIEA2024022300124), Mar 3, 2024: STRUCTURE. CRACKED. EMP R/H HORI STAB MOST O/B WEB LOWER CHORD FOUND CRACK(

LOWER CHORD REPLACED AS PER SRM 51-10-02 AND NEW LOWER CHORD HOLES TRANSFERRED AS PER SRM 51-40-05 AND - [SDR UIEA2024022300125](https://openairdocs.org/sdr/UIEA2024022300125), Mar 3, 2024: WEB. CRACKED. EMP RH HORI STAB MOST O/B WEB FOUND CRACK(

WEB CRACK AREA REPAIRED AS PER SRM 55-10-09-2R-13 REPAIR 13 FIG 201. NO FURTHER DEFECTS NOTED

) - [SDR UIEA2024022500127](https://openairdocs.org/sdr/UIEA2024022500127), Mar 3, 2024: FITTING. CRACKED. L/H BS 1480 LONGERON EXTENSION FITTING 1EA CRACK WAS FOUND AT EXISTING TRIMMED OFF AREA APPROX 5/16 IN LENGTH(

LONGERON EXTENSION FITTING REPLACEMENT CARRIED - [SDR UIEA2024022600128](https://openairdocs.org/sdr/UIEA2024022600128), Mar 3, 2024: SKIN. DENTED. EMP - VERT FIN R/H SURFACE MOST UPPER AREA FWD FIXED PANEL FOUND DENT MARK(

DENT AREA REPAIRED AS PER RI-55-00-16750 REV.A. NO FURTHER DEFECTS NOTED

) - [SDR UIEA2024022600130](https://openairdocs.org/sdr/UIEA2024022600130), Mar 3, 2024: SKIN. DELAMINATED. RHW O/B FORE FLAP FOUND DELAMINATION(

PERFORMED REPAIR AT DELAMINATION AREA IAW SRM 51-70-07 PAR 5.C. NO FURTHER DEFECTS NOTED

) - [SDR UIEA2024022600131](https://openairdocs.org/sdr/UIEA2024022600131), Mar 3, 2024: SKIN. DELAMINATED. LHW O/B FORE FLAP FOUND DELAMINATION(

PERFORMED REPAIR AT DELAMINATION AREA IAW SRM 51-70-07 PAR 5.A. NO FURTHER DEFECTS NOTED

) - [SDR UIEA2024022600132](https://openairdocs.org/sdr/UIEA2024022600132), Mar 3, 2024: SKIN. DELAMINATED. LHW O/B FORE FLAP FOUND DELAMINATION(

PERFORMED REPAIR AT DELAMINATION AREA IAW SRM 51-70-07 PAR 5.A. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2024022600133](https://openairdocs.org/sdr/UIEA2024022600133), Mar 3, 2024: SKIN. DELAMINATED. RHW I/B AFT FLAP FOUND DELAMINATION. PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.C. NO FURTHER DEFECTS NOTED

) - [SDR UIEA2024030100140](https://openairdocs.org/sdr/UIEA2024030100140), Mar 3, 2024: LAMP. BROKEN. FOUND EMERGENCY LIGHTS L5735, L1853 AND L1854 LAMP BROKEN(

EMERGENCY LIGHTS L5735, L1853 AND L1854 LAMP REPLACED AND TEST IS NORMAL IAW AMM 33-51-00

) - [SDR UIEA2023122401011](https://openairdocs.org/sdr/UIEA2023122401011), Dec 24, 2023: ENGINE. SMOKE. ON CLIMBOUT THROUGH 800FT EICAS "CREW REST SMOKE". NOTICED HAZE COMING FROM CREW REST AREA. MESSAGE DISAPPEARED ON DECENT THROUGH 3500FT.(

REPLACED #3 ENGINE - [SDR UIEA2023121500999](https://openairdocs.org/sdr/UIEA2023121500999), Dec 15, 2023: WATER SEPARATOR. UNKNOWN. SMOKE CREW REST EICAS IMMEDIATELY AFTER ROTATION AND A SMELL OF SOMETHING BURNING. EICAS AND SMELL WENT AWAY AFTER 1-2 MINUTES. REPEAT WRITE-UP, REF LP 1723752. - [SDR UIEA2022123001222](https://openairdocs.org/sdr/UIEA2022123001222), Dec 31, 2022: WEB. CRACKED. AFT CGO STA 1840 L/H LBL 47 (NEAR L/H O/B CGO TRACK) FLOOR TORQUE BOX SKIN CRACKED.(

AFT CARGO COMPT BETWEEN STA 1840 & 1860 LBL 50, LATERAL BEAM INSTL WEB P/ - [SDR P5CA2022011700003](https://openairdocs.org/sdr/P5CA2022011700003), Feb 1, 2022: NONE. NONE. AIRCRAFT DAMAGE LOG CONTROL ITEM D16-001 - RH NOSE GEAR DOOR STA 292 DENT 1"X0.0312" A/Y=32 WITHIN LIMITS PER SRM 52-80-01-1A-1 DETAIL V.(

SOLID RIVET INSTALL - [SDR P5CA2022012600018](https://openairdocs.org/sdr/P5CA2022012600018), Feb 1, 2022: NONE. NONE. L/H STAB TIP FAIRING RIB #2 (COUNT FROM FWD) FOUND CRACKED(

HORI STAB TIP RIB - STRUCTURE WITH 11 RIBS-REPAIR

) - [SDR P5CA2022012600019](https://openairdocs.org/sdr/P5CA2022012600019), Feb 1, 2022: NONE. NONE. L/H STAB TIP FAIRING RIB #9 (COUNT FROM FWD) FOUND CRACKED(

HORI STAB TIP RIB - STRUCTURE WITH 11 RIBS-REPAIR

) - [SDR P5CA2022012600020](https://openairdocs.org/sdr/P5CA2022012600020), Feb 1, 2022: NONE. NONE. #4 PYLON VALVE ACCESS PNL #482EL 1EA HOLE FOUND ELONGATION(

#4 PYLON V/V ACCESS PNL #482EL FASTENER HOLE REPAIR

) - [SDR P5CA2022012600021](https://openairdocs.org/sdr/P5CA2022012600021), Feb 1, 2022: NONE. NONE. #4 ENG R/H CORE COWL EXHAUST LWR EDGE FOUND SEVERAL RIVET HOLES CRACKED.(

#4 ENG R/H CORE COWL PRECOOLER EXTERNAL DOUBLER REPAIR.

) - [SDR P5CA2022012700022](https://openairdocs.org/sdr/P5CA2022012700022), Feb 1, 2022: NONE. NONE. M/D - BALL MAT PNL FOUND BROKEN AT STA 1860-1920 RBL 55-77 BOTH LH AND RH FWD CORNER(

M/D - STA 1860-1920 RBL 55-77 CASTER PANEL DOUBLER REPAIRED AS PER RI-25 - [SDR P5CA2022012700023](https://openairdocs.org/sdr/P5CA2022012700023), Feb 1, 2022: NONE. NONE. LHW I/B MID FLAP O/B RIB AFT AREA ANGLE BRACKET FOUND CRACKED(

FABRICATE THE REPLACEMENT CLIP FROM 7075T651 BARE PLATE

) - [SDR P5CA2022012700024](https://openairdocs.org/sdr/P5CA2022012700024), Feb 1, 2022: NONE. NONE. LH WING L/E CAVITY LES 884.47 (NEAR REFUEL PNL) SUPPORT BEAM FOUND CRACK(

LH WING FIXED L/E LOWER SURFACE PANEL SUPPORT BEAM REPAIR AT ILES 848.5-908.5

) - [SDR P5CA2022012800025](https://openairdocs.org/sdr/P5CA2022012800025), Feb 1, 2022: NONE. NONE. RHW O/B FORE FLAP L/E FOUND DELAMINATION (24" TO I/B)(

REPAIRED WITH COMPOSITE HOT BOND METHOD AS PER SRM 51-70-07 PAR 5A 

) All 176: https://openairdocs.org/aircraft/N454PA/reports.md ## STCs that may be installed (OpenAirDocs) (6) Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do. ### Approved for the engine (GE CF6-80 series) - [STC SE01543CH](https://openairdocs.org/stc/SE01543CH): Replace Hamilton Sundstrand P/N 778839-13, 778839-14, 778839-19, 778839-20, 778839-37, 778839-38, 816682-1, 840618-2, 880724 carbon bushings with Cook Airtomic P/N AIR22947 Slotted Entry Busing in the High Pressure Shutoff Valve. Cook Airtomic. Lists CF6-80A - [STC SE01478CH](https://openairdocs.org/stc/SE01478CH): Installation of Cook Airtomic alignment joint p/n AIR 22912. Cook Airtomic. Lists CF6-80C2 Series - [STC SE00969CH](https://openairdocs.org/stc/SE00969CH): Install AeroControlex P/N 2605290-001 variable stator feedback control cable. AeroControlex Group TransDigm Inc. Lists CF6-80A - [STC SE01471AT](https://openairdocs.org/stc/SE01471AT): Replace right and left side Rohr, Inc. fire detection harness on GE CF6-80C2 engine. Unison Industries. Lists CF6-80C2 Series - [STC SE00463LA](https://openairdocs.org/stc/SE00463LA): Install fireproof blankets on the engine fan reverser intermediate fireseal, in lieu of fireproof intumescent coating. This STC is jointly by owned by Hi Temp Insulation and MRA Systems acting through Middle River Aircraft Systems, 103 Chesapeake Park Plaza, Baltimore, MD 21220. Hi Temp Insulation Inc. Lists CF6-80C2A1 - [STC SA2227SO](https://openairdocs.org/stc/SA2227SO): Installation of wiring and associated components for utilization of the Rolls Royce, Inc., ARINC, interface/readers UT1317 or UT1317/1, for the purpose of acquisition, recording, and analysis in real time of engine/aircraft/ systems. (767 SERIES POWERED BY RR RB-11-524 SERIES. Rolls Royce, Inc ## Earlier aircraft with N454PA The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N454PA before. - [Cancelled 1974-04-23](https://openairdocs.org/deregistered/N454PA-1974-04-23): Boeing 707-321B, S/N 19376, built 1967. Owner: [Pan American World Airways Inc](https://openairdocs.org/faa-owner/PAN%20AMERICAN%20WORLD%20AIRWAYS%20INC), [New York, NY](https://openairdocs.org/faa-place/NY/New%20York) ## Related - Other Boeing 747-46NF aircraft: https://openairdocs.org/model/boeing-747-46nf/aircraft.md - The GE CF6-80 series engine: https://openairdocs.org/engine/ge-cf6-80-series.md --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.