# N450PA: 2000 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: 30808 - Year built: 2000 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: October 12, 2000 - Certificate issued: April 10, 2025 - Expires: April 30, 2032 - Mode S code: A57362 - Registered owner: [Atlas Air Inc](https://openairdocs.org/faa-owner/ATLAS%20AIR%20INC) - Location: [White Plains, NY](https://openairdocs.org/faa-place/NY/White%20Plains) - Owner type: Corporation - Owner's area on the map: 41.0329° N, 73.7648° W: Placed by OpenAirDocs at the center of ZIP code 10601, 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=450PA - Page: https://openairdocs.org/aircraft/N450PA 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/N450PA/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 N450PA. ## FAA accident and incident reports None matched to N450PA. ## Service difficulty reports (307, 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 UIEA2026071300593](https://openairdocs.org/sdr/UIEA2026071300593), Jul 12, 2026: CIRCUIT CARD. FAULTED. MAIN DECK FIRE WARNING - NO EICAS MSG. SWAPED THE A4 WITH A29 CIRCURT CARD & PFMD GND TEST ,TEST PASSED IAW AMM 26-10-01 (NOW D00132 IN A4 POSITION,D00883 I - [SDR UIEA2026022600069](https://openairdocs.org/sdr/UIEA2026022600069), Feb 26, 2026: VALVE. INOPERATIVE. EQUIPMENT COOLING MESSAGE. SUSPECT FLT DECK FLOW REG VALVE INOP. OPENED FLOOR PANEL AND MANUALLY MOVED VALVE TO OPEN. TRANSFER TO DMI 248403 PER MEL 21-61-13 CA - [SDR UIEA2025111001295](https://openairdocs.org/sdr/UIEA2025111001295), Nov 11, 2025: TIRE. FAILED. #8 MLG BLEW OUT TOWER REPORTED SMOKE & TIRE DEBRIS ON RUNWAY. R & R NR 8 MWA IAW AMM 32-45-01 & IPC 32-45-03-02. C/W BLOWN TIRE CHAP 5 INSP IAW AMM 05-51-25. R - [SDR UIEA2025110701293](https://openairdocs.org/sdr/UIEA2025110701293), Nov 7, 2025: WHEEL. DAMAGED. NR 3 MAIN TIRE DAMAGED. REPLACED NR 3 AND 4 MLG WHEEL ASSY IAW AMM 32-45-01/401. PRESS & LEAK CHK OK. - [SDR UIEA2025101001267](https://openairdocs.org/sdr/UIEA2025101001267), Oct 10, 2025: INDICATION SYS. FAULTED. FLIGHT CREW REPORTED NR 4 HYD QTY INDICATION ERRATIC IN FLIGHT. PERFORMED WIRING CHECK BETWEEN DW 3112C PIN 2 AND DM7838EA PIN G15, DM 7838BA PIN D15, CHECKS NO - [SDR UIEA2025081001118](https://openairdocs.org/sdr/UIEA2025081001118), Aug 10, 2025: TIRE. FAILED. AT LANDING, #1 TIRE BLEW. FLAT SPOT FOUND. CREW HAD AUTOBRAKE SET AT 4 MINIMUM LEVEL DUE TO NO AUTOSPOILER AND BRAKE ROD. ONCE DISENGAGED, CREW MANUAL BRAKE DID - [SDR UIEA2025062800817](https://openairdocs.org/sdr/UIEA2025062800817), Jul 14, 2025: LONGERON FITTING. CRACKED. LEFT BS 1480 LONGERON EXTENSION FITTING FOUND CRACKED. CRACK LONGERON EXTENSION FITTING REPAIRED AS PER ATLAS AIR EO 4453A818 REV 20 PART 7. NO FURTHER DEFECTS - [SDR UIEA2025062800818](https://openairdocs.org/sdr/UIEA2025062800818), Jul 14, 2025: DOUBLER. CRACKED. MAIN DECK - L1 ENTRY DR UPR HINGE DOUBLER FND CRACKED. DOUBLER REPLACED AS PER SRM 51-10-02 AND NEW DOUBLER HOLES TRANSFERRED AS PER SRM 51-40-05 AND NEW DOUBLE - [SDR UIEA2025063000819](https://openairdocs.org/sdr/UIEA2025063000819), Jul 14, 2025: LUG. CRACKED. 1 EA CRACK WAS FOUND ON BS 1000 RBL 11.33 INTERCOSTAL LUG FITTING. INTERCOSTAL LUG FITTING REPLACED AS PER ATLAS AIR EO 4453C024 REV.4 PART 7 STEP 3. NO FURTHER - [SDR UIEA2025063000820](https://openairdocs.org/sdr/UIEA2025063000820), Jul 14, 2025: LUG. CRACKED. 1 EA CRACK WAS FOUND ON BS 1000 LBL 11.33" INTERCOSTAL LUG FITTING. INTERCOSTAL LUG FITTING REPLACED AS PER ATLAS AIR EO 4453C024 REV.4 PART 3 STEP 3. NO FURTHE - [SDR UIEA2025070100821](https://openairdocs.org/sdr/UIEA2025070100821), Jul 14, 2025: FAIRING. DELAMINATED. RIGHT WING I/B MID FLAP L/E FAIRING FOUND DELAMINATION AT I/B 13". PERFORMED PERMANENT REPAIR AS PER SRM 51-70-07 PAR 5. A. NO FURTHER DEFECTS NOTED. - [SDR UIEA2025070100822](https://openairdocs.org/sdr/UIEA2025070100822), Jul 14, 2025: FAIRING. DELAMINATED. RIGHT WING I/B AFT FLAP MID L/E FAIRING FOUND DELAMINATION AT O/B 180". PERFORMED PERMANENT REPAIR AS PER SRM 51-70-07 PAR 5. A. NO FURTHER DEFECTS NOTED. - [SDR UIEA2025070100823](https://openairdocs.org/sdr/UIEA2025070100823), Jul 14, 2025: FAIRING. DELAMINATED. LEFT WING I/B MID FLAP L/E FAIRING FOUND DELAMINATION AT O/B 70". PERFORMED PERMANENT REPAIR AS PER SRM 51-70-07 PAR 5. A. NO FURTHER DEFECTS NOTED. - [SDR UIEA2025070100824](https://openairdocs.org/sdr/UIEA2025070100824), Jul 14, 2025: FAIRING. DELAMINATED. RIGHT WING O/B MID FLAP L/E FAIRING FOUND DELAMINATION AT I/B 39". PERFORMED PERMANENT REPAIR AS PER SRM 51-70-07 PAR 5. A. NO FURTHER DEFECTS NOTED. - [SDR UIEA2025070100825](https://openairdocs.org/sdr/UIEA2025070100825), Jul 14, 2025: FAIRING. DELAMINATED. RIGHT WING O/B MID FLAP L/E FAIRING FOUND DELAMINATION AT I/B 12". PERFORMED PERMANENT REPAIR AS PER SRM 51-70-07 PAR 5. A. NO FURTHER DEFECTS NOTED. - [SDR UIEA2025070100826](https://openairdocs.org/sdr/UIEA2025070100826), Jul 14, 2025: FAIRING. PUNCTURED. LEFT WING I/B FORE FLAP MID L/E FAIRING FOUND PUNCH HOLE FROM I/B 133". PERFORMED PERMANENT REPAIR AS PER SRM 51-70-07 PAR 5. C. NO FURTHER DEFECTS NOTED. - [SDR UIEA2025070100827](https://openairdocs.org/sdr/UIEA2025070100827), Jul 14, 2025: FAIRING. DELAMINATED. RIGHT WING O/B MID FLAP L/E FAIRING FOUND DELAMINATION AT O/B 180". PERFORMED PERMANENT REPAIR AS PER SRM 51-70-07 PAR 5. A. NO FURTHER DEFECTS NOTED. - [SDR UIEA2025070100828](https://openairdocs.org/sdr/UIEA2025070100828), Jul 14, 2025: FAIRING. CHAFED. RHW I/B AFT FLAP I/B L/E FAIRING FOUND CHAFING. PERFORMED PERMANENT REPAIR AS PER SRM 51-70-07 PAR 5.G. NO FURTHER DEFECTS NOTED. - [SDR UIEA2025070300830](https://openairdocs.org/sdr/UIEA2025070300830), Jul 14, 2025: POWER SUPPLY. NO TEST. FUNCTIONAL TEST EMERGENCY LIGHTS BATTERY PACKS FOR CAPACITY (15 MIN. MINIMUM). FOUND EMERGENCY LT L1533, L5733, L5767 & M4915 WENT OFF IN LESS THAN 15 MINUTES. - [SDR UIEA2025070500835](https://openairdocs.org/sdr/UIEA2025070500835), Jul 14, 2025: LAMP. INOPERATIVE. DOOR L1 FWD EMERGENCY SILL LT L1853 FOUND INOP. DOOR L1 FWD EMERGENCY SILL LT L1853 LAMP REPLACED AND TEST NORMAL IAW AMM 33-51-05. - [SDR UIEA2025070700844](https://openairdocs.org/sdr/UIEA2025070700844), Jul 14, 2025: SEAT TRACK. CRACKED. M/D STA753 TO STA757 LBL11" SEAT TRACK FOUND CRACKED. SEAT TRACK CRACK AREA REPAIRED AS PER SRM 53-00-52-2R-12 REPAIR12 FIG 201. NO FURTHER DEFECTS NOTED. - [SDR UIEA2025070700846](https://openairdocs.org/sdr/UIEA2025070700846), Jul 14, 2025: SEAT TRACK. CHAFED. M/D STA 1980 TO STA 1985 RBL 11.33" SEAT TRACK CROWN CHAFED. CHAFED AREA SMOOTHED OUT AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01 AND SMOOTHED OUT A - [SDR UIEA2025070700847](https://openairdocs.org/sdr/UIEA2025070700847), Jul 14, 2025: SEAT TRACK. CHAFED. M/D STA 2020 TO STA 2026 RBL 11 SEAT TRACK CROWN CHAFED. CHAFED AREA SMOOTHED OUT AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01 AND SMOOTHED OUT AREA - [SDR UIEA2025070700848](https://openairdocs.org/sdr/UIEA2025070700848), Jul 14, 2025: SEAT TRACK. CHAFED. M/D STA 646 TO STA 656 LBL 11 SEAT TRACK CROWN FOUND CHAFED. CHAFE AREA SMOOTHED OUT AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01 AND SMOOTHED OUT AR - [SDR UIEA2025070700849](https://openairdocs.org/sdr/UIEA2025070700849), Jul 14, 2025: SEAT TRACK. CHAFED. M/D STA 1890 TO 1893 LBL 11 SEAT TRACK CROWN FOUND CHAFED. CHAFE AREA SMOOTHED OUT AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01 AND CHAFING SMOOTHED - [SDR UIEA2025070700850](https://openairdocs.org/sdr/UIEA2025070700850), Jul 14, 2025: SEAT TRACK. CHAFED. M/D STA 1968 TO STA 1970 LBL 11 SEAT TRACK CROWN FOUND CHAFED. CHAFE AREA SMOOTHED OUT AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01 AND SMOOTHED OUT - [SDR UIEA2025070700851](https://openairdocs.org/sdr/UIEA2025070700851), Jul 14, 2025: SEAT TRACK. SCRATCHED. M/D SEAT TRACK CTR GUIDE STUD AREAS FOUND SCRATCHED AT RBL 11 STA 1370, STA 1390, STA 1410. SCRATCH AREA SMOOTHED OUT AS PER SRM 51-10-02 AND REPROTECTED AS PER - [SDR UIEA2025070700852](https://openairdocs.org/sdr/UIEA2025070700852), Jul 14, 2025: SEAT TRACK. CORRODED. M/D STA 780, 783 LBL 11 SEAT TRACK CROWN CORRODED. CORROSION AREA REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, CORROSION REMOVED AREA MEASUR - [SDR UIEA2025070700854](https://openairdocs.org/sdr/UIEA2025070700854), Jul 14, 2025: SEAT TRACK. SCRATCHED. M/D SEAT TRACK CTR GUIDE STUD AREAS FOUND SCRATCHED AT RBL 11 STA 1430, STA 1450 & STA 1470. SCRATCH AREAS SMOOTHED OUT AS PER SRM 51-10-02 AND REPROTECTED AS P - [SDR UIEA2025070800855](https://openairdocs.org/sdr/UIEA2025070800855), Jul 14, 2025: SEAT TRACK. CORRODED. M/D STA 606-STA 624 LBL 11 SEAT TRACK CROWN CORRODED. CORROSION AREA REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, CORROSION REMOVED AREA MEA - [SDR UIEA2025070800856](https://openairdocs.org/sdr/UIEA2025070800856), Jul 14, 2025: SEAT TRACK. SCRATCHED. M/D SEAT TRACK CTR GUIDE STUD AREAS FOUND SCRATCHED AT RBL 11 STA 1611, STA 1631, STA 1772. SCRATCH AREAS SMOOTHED OUT AS PER SRM 51-10-02 AND REPROTECTED AS PE - [SDR UIEA2025070800857](https://openairdocs.org/sdr/UIEA2025070800857), Jul 14, 2025: SEAT TRACK. CORRODED. M/D STA 566-STA 592 LBL 11 SEAT TRACK CROWN CORRODED. CORROSION AREA REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, CORROSION REMOVED AREA MEA - [SDR UIEA2025070800858](https://openairdocs.org/sdr/UIEA2025070800858), Jul 14, 2025: SEAT TRACK. CORRODED. M/D STA 545-STA 559 LBL 11 SEAT TRACK CROWN CORRODED. CORRSION AREA REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, CORROSION REMOVED AREA MEAS - [SDR UIEA2025070800859](https://openairdocs.org/sdr/UIEA2025070800859), Jul 14, 2025: SEAT TRACK. CORRODED. M/D STA 872-STA 875 RBL 11 SEAT TRACK CROWN CORRODED. CORROSION AREA REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, CORROSION REMOVED AREA MEA - [SDR UIEA2025070800860](https://openairdocs.org/sdr/UIEA2025070800860), Jul 14, 2025: SEAT TRACK. CORRODED. M/D STA 750-STA 783 RBL 11 SEAT TRACK CROWN CORRODED. CORROSION AREA REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, CORROSION REMOVED AREA MEA - [SDR UIEA2025070800861](https://openairdocs.org/sdr/UIEA2025070800861), Jul 14, 2025: SEAT TRACK. SCRATCHED. M/D SEAT TRACK CTR GUIDE STUD AREA FOUND SCRATCHED AT LBL 11 STA 1430, STA 1450, STA 1470. SCRATCH AREA SMOOTHED OUT AS PER SRM 51-10-02 AND REPROTECTED AS PER - [SDR UIEA2025070800862](https://openairdocs.org/sdr/UIEA2025070800862), Jul 14, 2025: SEAT TRACK. CORRODED. M/D STA 730-STA 752 RBL 11 SEAT TRACK CROWN CORRODED. CORROSION AREA REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, CORROSION REMOVED AREA MEA - [SDR UIEA2025070800863](https://openairdocs.org/sdr/UIEA2025070800863), Jul 14, 2025: SEAT TRACK. CORRODED. M/D SEAT TRACK CTR GUIDE STUD AREAS FOUND SCRATCHED AT RBL 11.33 STA 1853 AND STA 1913. SCRATCH AREA SMOOTHED OUT AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM - [SDR UIEA2025070800864](https://openairdocs.org/sdr/UIEA2025070800864), Jul 14, 2025: SEAT TRACK. CORRODED. M/D STA 687-STA 694 RBL 11 SEAT TRACK CROWN CORRODED. CORROSION AREA REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, CORROSION REMOVED AREA MEA - [SDR UIEA2025070800865](https://openairdocs.org/sdr/UIEA2025070800865), Jul 14, 2025: GUIDE. CORRODED. M/D STA 1920 - 1980 SCD AFT SIDE GUIDE FOUND CORROSION. CORROSION AREA REMOVED AS PER CMM 25-55-06 AND REPROTECTED AS PER SRM 51-20-01 AND CORROSION REMOVED ARE - [SDR UIEA2025070800868](https://openairdocs.org/sdr/UIEA2025070800868), Jul 14, 2025: SEAT TRACK. CHAFED. M/D STA 1457 TO STA 1461 RBL 11 SEAT TRACK CROWN CHAFING. CHAFING AREA SMOOTHED OUT AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01 AND SMOOTHED OUT ARE - [SDR UIEA2025070800869](https://openairdocs.org/sdr/UIEA2025070800869), Jul 14, 2025: SEAT TRACK. CORRODED. M/D STA 617 - STA 635 RBL 11 SEAT TRACK CROWN CORRODED. CORROSION AREA REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, CORROSION REMOVED AREA M - [SDR UIEA2025070800870](https://openairdocs.org/sdr/UIEA2025070800870), Jul 14, 2025: SEAT TRACK. CORRODED. M/D STA 570 - STA 593 RBL 11 SEAT TRACK CROWN CORRODED. CORROSION AREA REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, CORROSION REMOVED AREA M - [SDR UIEA2025070800871](https://openairdocs.org/sdr/UIEA2025070800871), Jul 14, 2025: SEAT TRACK. CORRODED. M/D STA 546 TO STA 559 RBL 11 SEAT TRACK CROWN CORRODED. CORROSION AREA REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, CORROSION REMOVED AREA - [SDR UIEA2025070800872](https://openairdocs.org/sdr/UIEA2025070800872), Jul 14, 2025: SEAT TRACK. CORRODED. M/D STA 2200 - STA 2210 LBL 11 SEAT TRACK CROWN CORRODED. CORROSION AREA REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, CORROSION REMOVED AREA - [SDR UIEA2025070800873](https://openairdocs.org/sdr/UIEA2025070800873), Jul 14, 2025: TEE ANGLE. CRACKED. NR 3 PYLON O/B INNER MOST LWR TEE CRACKED AT NAC STA 344 APPROX. TEE CRACK AREA REPAIRED AS PER SRM 54-51-02-2R-2 REPAIR 2 FIG 201. NO FURTHER DEFECTS NOTED. - [SDR UIEA2025070900874](https://openairdocs.org/sdr/UIEA2025070900874), Jul 14, 2025: TEE ANGLE. CRACKED. NO. 2 PYLON - O/B MOST LOWER TEE CRACK FOUND AT NAC STA 332. TEE CRACK AREA REPAIRED AS PER SRM 54-51-02-2R-2 REPAIR 2 FIG 201. NO FURTHER DEFECTS NOTED. - [SDR UIEA2025070900875](https://openairdocs.org/sdr/UIEA2025070900875), Jul 14, 2025: BEAM. CRACKED. NWW SIDE PANEL HAS 1EA CRACK FOUND AT BEAM LHS WL130 BETWEEN STA 320 AND STA 340. BEAM REPLACED AS PER BOEING DWG: 65B07942&PL AND NEW BEAM HOLES TRANSFERRE - [SDR UIEA2025070900878](https://openairdocs.org/sdr/UIEA2025070900878), Jul 14, 2025: BEAM. CRACKED. NWW SIDE PANEL HAS 1 EA CRACK FWD AT BEAM RHS WL180 BETWEEN STA 265 AND 280.(

CRACKED BEAM REPLACED AS PER BOEING DWG NO.65B07942 & PL & EO 4453A043 REV 11 PA - [SDR UIEA2025070900879](https://openairdocs.org/sdr/UIEA2025070900879), Jul 14, 2025: SEAT TRACK. CRACKED. M/D STA 981 TO 983 LBL 75" SUBSTITUTE TRACK FOUND CRACKED. SUBSTITUTE TRACK CRACK AREA REPAIRED AS PER SRM 53-00-52-2R-13 REPAIR 13 FIG 201. NO FURTHER DEFECTS All 307: https://openairdocs.org/aircraft/N450PA/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 N450PA The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N450PA before. - [Cancelled 1975-08-21](https://openairdocs.org/deregistered/N450PA-1975-08-21): Boeing 707-321C, S/N 19272, built 1967. Exported to Romania. Owner: [Pan American World Airways Inc](https://openairdocs.org/faa-owner/PAN%20AMERICAN%20WORLD%20AIRWAYS%20INC), [Manhattan, NY](https://openairdocs.org/faa-place/NY/Manhattan) ## 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.