# N453PA: 2001 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: 30811
- Year built: 2001
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: August 22, 2001
- Certificate issued: March 8, 2025
- Expires: March 31, 2032
- Mode S code: A57E87
- 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=453PA
- Page: https://openairdocs.org/aircraft/N453PA

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/N453PA/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 N453PA.

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20030930022889I](https://openairdocs.org/incident/20030930022889I), Sep 30, 2003: Boeing 74746NF (N453PA), Miami, FL, Minor damage. (-23) "Industrial incident-no intent to fly". During a storm, a strong gust of wing blew a maintenance stand into the wing of a parked B-747. There was no…

## Service difficulty reports (178, 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 UIEA2026091000864](https://openairdocs.org/sdr/UIEA2026091000864), Sep 10, 2026: COALESCER BAG. ODOR. ELECTRICAL BURNING ODOR IN DESCENT. R & R WATER SEPARATOR COALESCER BAG ON PACK 1, 2, & 3, AND PERFORMED CH 5 INSP IAW AMM 21-51-05. OPS CHKD OK.
- [SDR UIEA2026063000563](https://openairdocs.org/sdr/UIEA2026063000563), Jun 30, 2026: IMPELLER. DAMAGED. FUEL IMBALANCE 2 - 3 STATUS MESSAGE. ACCOMPLISHED FIM 28-22 TASK 925, NO FINDING. TANK DIVE ACCOMPLISHED, FOUND A JET LEAK FROM OVRD PUMP DISCH CHECK VLV. R/R D
- [SDR UIEA2025041400459](https://openairdocs.org/sdr/UIEA2025041400459), Apr 15, 2025: SEAT TRACK. CRACKED. CRACK - FOUND M/D SUBSTITUTE TRACK CRACK, BETWEEN STA 1480 TO STA 1500, LBL 75.92.(<P>1. REMOVE AFFECTED FASTNERS TO GET ACCESS IAW SRM 51-40-02-0G-0 REV 103. 2
- [SDR UIEA2025041400461](https://openairdocs.org/sdr/UIEA2025041400461), Apr 15, 2025: SEAT TRACK. CRACKED. CRACK - FOUND M/D SUBSTITUTE TRACK CRACK, BETWEEN STA 1730, RBL 75.92.(<P>1. ACCOMPLISHED W/S NO: 50170 (SRM 53-00-52-2R-13 REV 103). 2. JOB COMPLETED AND CONDI
- [SDR UIEA2025041400462](https://openairdocs.org/sdr/UIEA2025041400462), Apr 15, 2025: SEAT TRACK. CRACKED. CRACK - FOUND M/D SUBSTITUTE TRACK CRACK, BETWEEN STA 1480 TO STA 1500, RBL 75.(<P>1. ACCOMPLISHED W/S NO. 50172 (SRM 53-00-52-2R-13 REV 103). 2. JOB COMPLETED 
- [SDR UIEA2025041400463](https://openairdocs.org/sdr/UIEA2025041400463), Apr 15, 2025: SEAT TRACK. CRACKED. CRACK - FOUND M/D FLOOR STRUCTURE TRACK SUBSTITUTE CRACK BETWEEN STA 980 TO STA 1000, LBL 75.92.(<P>1. ACCOMPLISHED W/S NO. 50160 (SRM 53-00-52-2R-13 REV 103). 
- [SDR UIEA2025041400464](https://openairdocs.org/sdr/UIEA2025041400464), Apr 15, 2025: SEAT TRACK. CRACKED. CRACK - FOUND M/D CGO COMPT SUB SEAT TRACK CRACK BETWEEN STA 660 TO STA 720, LBL 75.92, TTL 3 EA.(<P>1. ACCOMPLISHED W/S NO. 50182 (SRM 53-00-52-2R-13 REV 103).
- [SDR UIEA2025041400465](https://openairdocs.org/sdr/UIEA2025041400465), Apr 15, 2025: FLOORBEAM. CORRODED. CORROSION - MFOUND M/D FLOOR BEAM CORROSION AT STA 2240 RBL 57 TO RBL 85.(<P>1. REMOVE AFFECTED FASTENERS IAW SRM 51-40-02-0G-0 REV 103. 2. REPAIR DAMAGE AREA I
- [SDR UIEA2025041400468](https://openairdocs.org/sdr/UIEA2025041400468), Apr 15, 2025: FLOORBEAM. CORRODED. CORROSION - FOUND M/D FLOOR BEAMS TOP SURFACE CORROSION STA 1500 BETWEEN LBL 55 TO LBL 75.92.(<P>1. REMOVE AFFECTED FASTENERS TO GET ACCESS IAW SRM 51-40-02-0G-
- [SDR UIEA2025041400469](https://openairdocs.org/sdr/UIEA2025041400469), Apr 15, 2025: SPLICE ANGLE. CORRODED. CORROSION - FOUND SPLICE ANGLE CORROSION AT M/D COMPARTMENT BETWEEN STA 2280 TO STA 2300, RBL 68.(<P>1. REMOVE DAMAGE PART IAW SRM 51-40-02-0G-0 REV 103. 2. INS
- [SDR UIEA2025041400471](https://openairdocs.org/sdr/UIEA2025041400471), Apr 15, 2025: BRACKET. CORRODED. CORROSION - BRACKET LOWER FUSELAGE WING-TO-BODY SUPPORT BRACKET STA 920 BL 0.(<P>1. REMOVE DAMAGE PARTS IAW SRM 51-40-02-0G-0 REV 103. 2. INSTALL NEW PARTS IAW 
- [SDR UIEA2025041400473](https://openairdocs.org/sdr/UIEA2025041400473), Apr 15, 2025: ELT. EXPIRED. FWD M/D FIXED ELT BATTERY NEAR DUE DATE (03JUN25).(<P>1. REPLACED ELT TRANSMITTER IAW SWPM 20-60-06. 2. STEP A &AMP; B PERFORMED ELT INSTALLATION TEST IAW T/C N
- [SDR UIEA2025021600148](https://openairdocs.org/sdr/UIEA2025021600148), Feb 16, 2025: ENGINE. VIBRATION. ENG 1 VIB 4.0, N1 FAN, STEADY INCREASE THRU UPPER 20'S FLIGHT LEVEL.(<P>RAN ENG 1 PER 71-00-00-705-057-J00. NOTED 3.1 VIBRATION PEAK PER MCC ENGINEERING. OPS CH
- [SDR UIEA2024061200516](https://openairdocs.org/sdr/UIEA2024061200516), Jun 12, 2024: LINE. BROKEN. ADVISORY MSG "SMOKE CREW REST " AROUND 800 TO 1000 FEET AFTER T.O., FOLLOWED BY FUMES ON THE FLIGHT DECK.(<P>R/R CREW REST AREA TRIM AIR MODULATING VLV, REAPIRE
- [SDR UIEA2024032800229](https://openairdocs.org/sdr/UIEA2024032800229), Mar 28, 2024: UNKNOWN. FAULTED. DURING TAKEOFF NOTICED UNCOMMANDED ROLLING, ALSO ON LANDING AIRCRAFT ROLLED UNCOMMANDED TO LEFT.(<P>ABNORMALITY PRESSURIZED HYD, &AMP; TRIM RUDDER TO NEUTRAL, R
- [SDR UIEA2024021900092](https://openairdocs.org/sdr/UIEA2024021900092), Feb 19, 2024: WINGLET. NOT REPORTED. LEFT WINGLET SCRAPED.(<P>TRANSFERED TO DMI 203268 IAW CDL 57-28-01 DUE DATE 18JUN24. PLACARD INSTALLED.&NBSP;</P>)
- [SDR UIEA2023052600524](https://openairdocs.org/sdr/UIEA2023052600524), Jun 12, 2023: UNKNOWN. UNKNOWN. COCKPIT - RH RUDDER PEDAL CAVITIES, THE I/B SIDE VERTICAL METAL PANEL CORNER FOUND CRACKED.(<P>COCKPIT - RH RUDDER PEDAL CAVITIES, RH PILOT FWD PANEL SUPPORT WE
- [SDR UIEA2023052600525](https://openairdocs.org/sdr/UIEA2023052600525), Jun 12, 2023: UNKNOWN. UNKNOWN. COCKPIT - LH RUDDER PEDAL CAVITIES, THE I/B SIDE VERTICAL METAL PANEL CORNER FOUND CRACKED.(<P>COCKPIT - LH RUDDER PEDAL CAVITIES, LH PILOT FWD PANEL SUPPORT WE
- [SDR UIEA2023052600527](https://openairdocs.org/sdr/UIEA2023052600527), Jun 12, 2023: UNKNOWN. UNKNOWN. 1EA SURFACE CRACK FOUND ON LH STA 2231 STR 21L TO STR 22L REVEAL CRACK APPROX 2.375" IN LENGTH.(<P>STA 2231 STR 21L TO 22L, #5 DOOR REVEAL DOUBLER CRACK AREA RE
- [SDR UIEA2023053000528](https://openairdocs.org/sdr/UIEA2023053000528), Jun 12, 2023: UNKNOWN. UNKNOWN. AFT CARGO STA 1700 FLOOR BEAM MIDDLE AREA FOUND CHAFING.(<P>AFT CARGO STA 1700 FLOOR BEAM UPPER CHORD P/N: 65B07373-3 CHAFING AREA REPAIRED IAW RI-53-60-16278 R
- [SDR UIEA2023053000539](https://openairdocs.org/sdr/UIEA2023053000539), Jun 12, 2023: UNKNOWN. UNKNOWN. LHW I/B FORE FLAP UPPER SURFACE 59" TO I/B EDGE FOUND DELAMINATION(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR 5A. NO FURTHER DEFECTS NOTED</P
- [SDR UIEA2023053000540](https://openairdocs.org/sdr/UIEA2023053000540), Jun 12, 2023: UNKNOWN. UNKNOWN. LHW I/B FORE FLAP UPPER SURFACE 145" TO I/B EDGE FOUND DELAMINATION(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR 5A. NO FURTHER DEFECTS NOTED</
- [SDR UIEA2023053000541](https://openairdocs.org/sdr/UIEA2023053000541), Jun 12, 2023: UNKNOWN. UNKNOWN. LHW I/B FORE FLAP MID L/E FAIRING SKIN FOUND DELAMINATION(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR 5A. NO FURTHER DEFECTS NOTED</P>)
- [SDR UIEA2023053000542](https://openairdocs.org/sdr/UIEA2023053000542), Jun 12, 2023: UNKNOWN. UNKNOWN. LHW I/B FORE FLAP UPPER SURFACE 226" TO I/B EDGE FOUND DELAMINATION(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR 5A. NO FURTHER DEFECTS NOTED</
- [SDR UIEA2023053000543](https://openairdocs.org/sdr/UIEA2023053000543), Jun 12, 2023: UNKNOWN. UNKNOWN. LHW O/B FORE FLAP O/B L/E FAIRING SKIN FOUND DELAMINATION(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR 5A. NO FURTHER DEFECTS NOTED</P>)
- [SDR UIEA2023053000544](https://openairdocs.org/sdr/UIEA2023053000544), Jun 12, 2023: UNKNOWN. UNKNOWN. RHW O/B FORE FLAP L/E FAIRING SKIN 127" TO I/B FOUND DELAMINATION(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR 5A. NO FURTHER DEFECTS NOTED</P>
- [SDR UIEA2023060100552](https://openairdocs.org/sdr/UIEA2023060100552), Jun 12, 2023: UNKNOWN. UNKNOWN. LH STA 720 TENSION TIE FWD CHANNEL 1EA CRACK FOUND.(<P>STA 720 LH TENSION TIE CHANNEL CRACK AREA REPAIRED IAW SRM 53-20-30-2R-1 REPAIR 1. NO FURTHER DEFECTS NOT
- [SDR UIEA2023060100553](https://openairdocs.org/sdr/UIEA2023060100553), Jun 12, 2023: UNKNOWN. UNKNOWN. RH STA 760 TENSION TIE FWD CHANNEL 1EA CRACK FOUND.(<P>STA 760 RH TENSION TIE CHANNEL CRACK AREA REPAIRED IAW SRM 53-20-30-2R-1 REPAIR 1. NO FURTHER DEFECTS NOT
- [SDR UIEA2023060100554](https://openairdocs.org/sdr/UIEA2023060100554), Jun 12, 2023: UNKNOWN. UNKNOWN. LH STA 760 TENSION TIE FWD CHANNEL 1EA CRACK FOUND.(<P>STA 760 LH TENSION TIE CHANNEL CRACK AREA REPAIRED IAW SRM 53-20-30-2R-1 REPAIR 1. NO FURTHER DEFECTS NOT
- [SDR UIEA2023060400564](https://openairdocs.org/sdr/UIEA2023060400564), Jun 12, 2023: UNKNOWN. UNKNOWN. LHW I/B AILERON UPPER SURFACE AFT O/B CORNER FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA AS PER SRM 51-70-06 PAR 5G. NO FURTHER DEFECTS NOTED</P
- [SDR UIEA2023060500565](https://openairdocs.org/sdr/UIEA2023060500565), Jun 12, 2023: SHEAR TIE. UNKNOWN. STA 1000 FRONT SPAR SHEAR TIE CRACK FOUND RBL 33.99(<P>STA 1000 RBL 33.99 FRONT SPAR SHEAR TIE REPLACED AND INSTALLED IAW EO 4453C024 APRT 8 AND RI-53-43-16281 
- [SDR UIEA2023060500566](https://openairdocs.org/sdr/UIEA2023060500566), Jun 12, 2023: SHEAR TIE. UNKNOWN. STA 1000 FRONT SPAR SHEAR TIE CRACK FOUND LBL 75.92(<P>STA 1000 LBL 75.92 FRONT SPAR SHEAR TIE REPLACED AND INSTALLED IAW EO 4453C024 PART 6 AND RI-53-43-16285 
- [SDR UIEA2023060500567](https://openairdocs.org/sdr/UIEA2023060500567), Jun 12, 2023: UNKNOWN. UNKNOWN. BODY FAIRING 191KL UPPER SUPPORT AND LOWER FLANGE FOUND CRACK(<P>BODY FAIRING 191KL UPPER SUPPORT AND LOWER FLANGE CRACK AREAS REPAIRED IAW RI-53-40-16280 REV.A
- [SDR UIEA2023060500568](https://openairdocs.org/sdr/UIEA2023060500568), Jun 12, 2023: UNKNOWN. UNKNOWN. 1EA THOUGHT THICKNESS CRACK FOUND ON LH BS2231 S16 STRAP (COUNT FROM O/B SECOND LAYER) RUNNING FWD AT 4 O/C POSITION (VIEW LOOKING O/B).(<P>M/D - STA 2231 STR 1
- [SDR UIEA2023060500569](https://openairdocs.org/sdr/UIEA2023060500569), Jun 12, 2023: LONGERON. UNKNOWN. STA 1480 RH LONGERON EXTENSION FTG FOUND CRACKED(<P>STA 1480 RH LONGERON EXTENSION FTG P/N: 65B15034U24 REPLACED AND INSTALLED IAW EO 4453A818 PART 4. NO FURTHE
- [SDR UIEA2023060500570](https://openairdocs.org/sdr/UIEA2023060500570), Jun 12, 2023: LONGERON. UNKNOWN. STA 1480 LH LONGERON EXTENSION FTG FOUND CRACKED(<P>STA 1480 LH LONGERON EXTENSION FTG P/N: 65B15034U23 REPLACED AND INSTALLED IAW EO 4453A818 PART 3. NO FURTHE
- [SDR UIEA2023060600581](https://openairdocs.org/sdr/UIEA2023060600581), Jun 12, 2023: UNKNOWN. UNKNOWN. DAMAGE LOG D-4-15 - DENT BOTTOM OF BULK CARGO FRAME, STA 1992 WL175, L=3/4" X W=3/4" X D=1/32", PER SRM 53-00-01-1A-1 TABLE 1 DETAIL 3 ADL LIMIT.(<P>FX - STA 19
- [SDR UIEA2023060600582](https://openairdocs.org/sdr/UIEA2023060600582), Jun 12, 2023: UNKNOWN. UNKNOWN. FWD CARGO AFT ROW BALLMAT MID PANEL RH AFT CORNER CRK(<P>FWD CARGO COMPT AFT CTR BALLMAT PANEL P/N: 192511-3 CRACK AREA REPAIRED IAW RI-53-20-16283 REV.A. NO FU
- [SDR UIEA2023060700597](https://openairdocs.org/sdr/UIEA2023060700597), Jun 12, 2023: UNKNOWN. UNKNOWN. LH BS 740 TENSION TIE FWD CHANNEL 2EA CRACK WERE FOUND ON THE FASTENER HOLE AT 12 O'CLOCK AND 6 O'CLOCK POSITION.(<P>STA 740 LH TENSION TIE CHANNEL REPAIRED IAW
- [SDR UIEA2023060700608](https://openairdocs.org/sdr/UIEA2023060700608), Jun 12, 2023: UNKNOWN. UNKNOWN. LH WLG I/B W/W DOOR AFT CLOSING RIB AND SKIN CHAFING(<P>LH WLG I/B W/W DOOR AFT CLOSING RIB AND SKIN CHAFING AREA REPAIRED IAW RI 52-82-16282 REV A. NO FURTHER 
- [SDR UIEA2023060800609](https://openairdocs.org/sdr/UIEA2023060800609), Jun 12, 2023: UNKNOWN. UNKNOWN. EO 4453A516 PART 4, STA 400 RH WAS A REPAIR PREVIOUSLY INSTALLED IN THE MODIFICATION AREA.(<P>FX STA 400 RH FUS SKIN - NWW AFT CORNER SKIN PANEL MOD ACCOMPLISHE
- [SDR UIEA2023060800610](https://openairdocs.org/sdr/UIEA2023060800610), Jun 12, 2023: UNKNOWN. UNKNOWN. FX STA 400 LH NOSE WW AFT CORNER SKIN CRACK(<P>FX STA 400 LH FUS SKIN - NWW AFT CORNER SKIN PANEL MOD ACCOMPLISHED IAW EO 4453A516 PART 3 AND RI-53-18-16306 REV
- [SDR UIEA2023060900613](https://openairdocs.org/sdr/UIEA2023060900613), Jun 12, 2023: UNKNOWN. UNKNOWN. M/D SCD AFT DR SILL O/B ASSY UPPER SKIN LWR SIDE FOUND CORROSION CRACK.(<P>M/D SCD AFT DOOR SILL O/B SILL ASSY CHANNEL CORROSION CRACK AREA REPAIRED IAW RI-25-5
- [SDR UIEA2023060900614](https://openairdocs.org/sdr/UIEA2023060900614), Jun 12, 2023: UNKNOWN. UNKNOWN. RHW T/E O/B AFT FLAP O/B UPPER PANEL FOUND CHAFING(<P>PERFORMED REPAIR AT CHAFING AREA AS PER RI-57-50-16296 REV.A. NO FURTHER DEFECTS NOTED</P>)
- [SDR UIEA2023060900615](https://openairdocs.org/sdr/UIEA2023060900615), Jun 12, 2023: UNKNOWN. UNKNOWN. LHW T/E I/B FORE FLAP MOST O/B UPPER PANEL FOUND TWO DENTS(<P>PERFORMED REPAIR AT DENTS AREA PER SRM 51-70-10 REPAIR2 FIG203. NO FURTHER DEFECTS NOTED</P>)
- [SDR UIEA2023060900616](https://openairdocs.org/sdr/UIEA2023060900616), Jun 12, 2023: UNKNOWN. UNKNOWN. LHW T/E I/B AFT FLAP UPPER O/B PANEL FOUND CHAFING(<P>PERFORMED REPAIR AT CHAFING AREA IAW SRM 51-70-10 REPAIR 2 FIG 203. NO FURTHER DEFECTS NOTED</P>)
- [SDR UIEA2023061200637](https://openairdocs.org/sdr/UIEA2023061200637), Jun 12, 2023: BATTERY PACK. UNKNOWN. MAIN DECK EMERGENCY LT FND INOP DURING OPS CHK(<P>EMERGENCY LT BATTERY PACK M5170 REPLACED AS PER AMM 33-51-04. OPS CHECK GOOD</P>)
- [SDR UIEA2022070800758](https://openairdocs.org/sdr/UIEA2022070800758), Jul 11, 2022: NONE. NONE. FOUND PITTING IN STRUCTURE SURROUNDING #6 CARRIAGE SPINDLE BEARING(<P>R/R RH INBD MID FLAP IAW AMM 27-50-00</P>)
- [SDR P5CA2022021600041](https://openairdocs.org/sdr/P5CA2022021600041), Feb 13, 2022: NONE. NONE. FUSELAGE SKIN (P/N 65B23673-4) - PUNCTURE DAMAGE AT STA 690, BETWEEN S-34R AND S-35R(<P STYLE="MARGIN: 0IN; MARGIN-BOTTOM: .0001PT;"><SPAN>THE DAMAGED SKIN PORT
- [SDR P5CA2021080300272](https://openairdocs.org/sdr/P5CA2021080300272), Aug 1, 2021: CONTROLLER. FAULTED. DURING CLIMB OUT #1, #2 &AMP; #4 BLEED VALVE OFF LIGHT ILLUMINATED WITH BLEED SWITCHES SELECTED ON, CYCLED VALVES WITH NO RESOLUTION.(<P ><SPAN>REMOVED AND REPL

All 178: https://openairdocs.org/aircraft/N453PA/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 N453PA

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N453PA before.

- [Cancelled 1979-05-15](https://openairdocs.org/deregistered/N453PA-1979-05-15): Boeing 707-321B, S/N 19374, built 1968. Exported to Chile. 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.