# N452PA: 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: 30810 - Year built: 2000 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: November 15, 2000 - Certificate issued: March 28, 2025 - Expires: March 31, 2032 - Mode S code: A57AD0 - 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=452PA - Page: https://openairdocs.org/aircraft/N452PA 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/N452PA/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 N452PA. ## FAA accident and incident reports None matched to N452PA. ## Service difficulty reports (208, 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 UIEA2026081400759](https://openairdocs.org/sdr/UIEA2026081400759), Aug 13, 2026: CONTROL MODULE. FAULTED. GEAR DISAGREE MESSAGE. LANDING GEAR LEVER WOULD NOT GO UP AFTER T/O. LANDING GEAR STAYED IN DOWN POSITION. RETURNED TO AIRPORT. : TRANSFER TO DMI 257550 PER MEL - [SDR UIEA2026040200120](https://openairdocs.org/sdr/UIEA2026040200120), Mar 29, 2026: STRAP. WORN. FOUND HOLE WEAR 1 EA AT B52231 S-17L -8 REPAIR FRAME STRAP(

REMOVED REPAIR FRAME STRAP AT B52231 S-17L AS PER SRM 51-40-02. FABRICATED -8 REPAIR FRAME STRAP A - [SDR UIEA2026040200121](https://openairdocs.org/sdr/UIEA2026040200121), Mar 29, 2026: BULKHEAD WEB. CRACKED. CRACK SIGNAL INDICATION AT L/H AFT INNER CHORD IN ACCORDANCE WITH EO 4453C127 OPEN HOLE HEEL INSPECTION (2EA) REMOVED HI-LOK 10 EA TO PERFORM S.B 747 53A2467 & - [SDR UIEA2026040100118](https://openairdocs.org/sdr/UIEA2026040100118), Mar 29, 2026: KEELBEAM. CORRODED. LOWER FUSELAGE STA 1460 KEELBEAM STRUCTURE CORROSION (BETWEEN BOTH BODY L/G DOOR) REMOVED BOTH PANEL AT LWR FUSELAGE BS 1460 KEEL BEAM IAW SRM 51-40-02. PERFORM - [SDR UIEA2025090401161](https://openairdocs.org/sdr/UIEA2025090401161), Sep 4, 2025: ACTUATOR. FAULTED. OUTFLOW VALVE R EICAS MSG. REMOVED & REPLACED RT OUTFLOW VALVE ACTUATOR ASSY, RT ICU & DIODE IAW AMM 21-31-10/401, 21-31-07/401, SWPM 20-40, AIPC 21-31-01-01 & - [SDR UIEA2024112001097](https://openairdocs.org/sdr/UIEA2024112001097), Nov 20, 2024: FIRE WARNING. FALSE ACTIVATION. DURING FLIGHT N452PA HAD A MDC FIRE WARNING ALERT. CREW VERIFIED NO FIRE OR SMOKE, CONTINUED TO ANC.(

CONFIRM NO SMOKE OR FIRE FROM PREVIOUS LEG. PERFORMED CA - [SDR UIEA2024032100164](https://openairdocs.org/sdr/UIEA2024032100164), Mar 21, 2024: SMOKE DETECTOR. FALSE ACTIVATION. CREW REST SMOKE EICAS MSG. NO SMOKE OR FIRE CONFIRMED.(

WIRING CHECKED NORMAL PER B747-400 WDM 26-13-31 REV 33. NEED TO REPLACE R/H CREW REST SMOKE DETECTOR. - [SDR UIEA2024022100096](https://openairdocs.org/sdr/UIEA2024022100096), Feb 23, 2024: RELAY. INOPERATIVE. FOUND R54 RELAY (#4 FWD) GFI RELAY NOT EQUIP(

1) IAW SWPM 20-81-22, 20-20-00 REV. 84, WDM 28-22-31 REV.33 REPLACED #4 FWD GFI RELAY. 2) TRANSFER TO I/C 28-22- - [SDR UIEA2024022100097](https://openairdocs.org/sdr/UIEA2024022100097), Feb 23, 2024: CARGO TRACK. CRACKED. FND M/D CGO SUBSTITUTE TRACK CRACK AT STA 1485 LBL 75.92(

1) PERFORM JOB IAW WORKSHEET #40066 AND DWG #65B38251 SHEET 62 REV A, SHEET 32 REV -, 14440802, SHEE - [SDR UIEA2024022100099](https://openairdocs.org/sdr/UIEA2024022100099), Feb 23, 2024: CARGO TRACK. CRACKED. FND M/D CGO SUBSTITUTE TRACK CRACK AT STA 1485, RBL 75.92(

1) PERFORM JOB IAW WORK SHEET NO: 40068 AND DWG NO:14440802, SHEET 3, REV B, 65B38751, SHEET 62 REV - [SDR UIEA2024022100100](https://openairdocs.org/sdr/UIEA2024022100100), Feb 23, 2024: FLOORBEAM. CRACKED. FND FLOOR STRUCTURE CRACK AT M/D STA 980 RBL 75.92(

1) PERFORM JOB IAW WORKSHEET #40071 AND DWG #65B16004, SHEET 4 REV A , 65B38250, SHEET 17 REV A, SHEET 9 R - [SDR UIEA2024022100101](https://openairdocs.org/sdr/UIEA2024022100101), Feb 23, 2024: SKIN. DEBONDED. DISBOND - RH WING #7 SPOILER LWR SURFACE, AT INBD EDGE, T/E EDGE(

1) PERFORM INTERIM REPAIR AT #7 SPOILER INBD SIDE T/E AREA, REFER TO EGAT EI T2024A57M-294 R - [SDR UIEA2024022100102](https://openairdocs.org/sdr/UIEA2024022100102), Feb 23, 2024: SKIN. DEBONDED. DISBOND - EDGE, LH WING INBD AILERON OUTBD CORNER.(

1) PERFORM REPAIR OF DISBOND SKIN AREA AT LH WING INBD AILERON OUTBD SIDE IAW SRM 57-60-01. PLEASE REFER T - [SDR UIEA2024022100103](https://openairdocs.org/sdr/UIEA2024022100103), Feb 23, 2024: SKIN. CHAFED. CHAFING - SKIN PNL, RH WING INBD AILERON OUTBD TE AREA(

1) PERORM REPAIR OF CHAFING SKIN DAMAGE AT R/H WING INBD AILERON T/E OUTBD SIDE. PLEASE REFER TO THE J - [SDR UIEA2024022100104](https://openairdocs.org/sdr/UIEA2024022100104), Feb 23, 2024: FLOORBEAM. NONE. DEVIATION- DURING PERFORM SB 4453A087 PART 2, AT R/H STA 340 UPPER DECK FLOOR BEAM STRAP HAVE 1 EA FASTENER CAN'T REMOVED.(

1) PERFORM JOB IAW EI T2024A53M-24 - [SDR UIEA2024022100105](https://openairdocs.org/sdr/UIEA2024022100105), Feb 23, 2024: FLOORBEAM. NONE. DEVIATION- DURING PERFORM SB 4453A087 PART 2, AT R/H STA 500 UPPER DECK FLOOR BEAM STRAP HAVE 2 EA FASTENER CAN'T REMOVED.(

1) PERFORM JOB IAW EI T2024A53M-24 - [SDR UIEA2024022100106](https://openairdocs.org/sdr/UIEA2024022100106), Feb 23, 2024: FLOORBEAM. NONE. DEVIATION- DURING PERFORM SB 4453A087 PART 2, AT L/H STA 340 UPPER DECK FLOOR BEAM STRAP HAVE 1 EA FASTENER CAN'T REMOVED.(

1) PERFORM JOB IAW EI T2024A53M-24 - [SDR UIEA2024022100107](https://openairdocs.org/sdr/UIEA2024022100107), Feb 23, 2024: DOOR FRAME. CRACKED. FND DOOR CUTOUT CRACK AT L5 DOOR RELEASE HANDLE AREA, STA 2240, WL 250.(

1) PERFORM JOB IAW WORK SHEET #40078 2) JOB COMPLETED AND CONDITION CHECK NORMAL.

- [SDR UIEA2024022100108](https://openairdocs.org/sdr/UIEA2024022100108), Feb 23, 2024: CARGO TRACK. CRACKED. FND M/D CGO SUBSTITUTE TRACK CRACK AT STA 1720 ~ 1730, RBL 75.92(

1) PERFORM JOB IAW WORKSHEET #40069 AND DWG #65B38751, SHEET 62 REV A, SHEET 32 REV-, SHEET - [SDR UIEA2023090800828](https://openairdocs.org/sdr/UIEA2023090800828), Sep 7, 2023: UNKNOWN. UNKNOWN. #1 HYD QUANTITY DROPPING(

LOCATED LEAK OF HYDRAULIC LINE AT STA 900. REPAIRED PER GMM 3.24.1 USING A NEW SECTION OF PIPE AND 2 EA RYNGLOC FITTINGS. PRESSURE T - [SDR UIEA2023083100821](https://openairdocs.org/sdr/UIEA2023083100821), Aug 31, 2023: ACM. UNKNOWN. BURNING SMELL & VIBRATION ON FINAL. ISOLATED TO PACK 1. NO INDICATIONS, SHUT OFF PACK(

PACK 1 PLACED ON DMI 192433 PER MEL 21-51-01-03 & DMI 192434 PER 26 - [SDR UIEA2022040900276](https://openairdocs.org/sdr/UIEA2022040900276), Apr 7, 2022: FLAP. DAMAGED. DURING WALK AROUND, FOUND #7 L/E FLAP VARIABLE CAMBER DAMAGED(

REPLACED #7 L/E FLAP VARIABLE CAMBER PER AMM 27-81-02/401.  PERFORMED FLAP OPS AND - [SDR P5CA2022022100062](https://openairdocs.org/sdr/P5CA2022022100062), Mar 12, 2022: NONE. NONE. M/D STA 1778-1800 LBL 33 SEAT TRACK FOUND CORROSION.(

M/D STA 1778-1800 LBL 33 SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. - [SDR P5CA2022022100044](https://openairdocs.org/sdr/P5CA2022022100044), Mar 12, 2022: NONE. NONE. M/D STA 850 - 809 LBL 11.33" SEAT TRACK FOUND CORROSION(

M/D STA 805 - 809 LBL 11.33" SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51 - [SDR P5CA2022022100045](https://openairdocs.org/sdr/P5CA2022022100045), Mar 12, 2022: NONE. NONE. M/D - STA 1920 RBL 75.92 SEAT TRACK FOUND CORROSION.(

M/D - STA 1920 RBL 75.92 SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. - [SDR P5CA2022022100046](https://openairdocs.org/sdr/P5CA2022022100046), Mar 12, 2022: NONE. NONE. M/D - STA 1920 RBL 99 SEAT TRACK FOUND CORROSION(

M/D - STA 1920 RBL 99 SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKE - [SDR P5CA2022022100047](https://openairdocs.org/sdr/P5CA2022022100047), Mar 12, 2022: NONE. NONE. M/D - STA 1900 RBL 99 SEAT TRACK FOUND CORROSION(

M/D - STA 1900 RBL 99 SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKE - [SDR P5CA2022022100048](https://openairdocs.org/sdr/P5CA2022022100048), Mar 12, 2022: NONE. NONE. U/D STA 740 LH TENSION TIE AFT CHANNEL STARTING FROM THE FASTENER HOLE RUNNING O/B TO THE EDGE FOUND CRACKED APPROX 3/8" IN LENGTH.(

U/D STA 740 LBL 55" TO EN - [SDR P5CA2022022100049](https://openairdocs.org/sdr/P5CA2022022100049), Mar 12, 2022: NONE. NONE. M/D - STA 1880 RBL 99 SEAT TRACK FOUND CORROSION(

M/D - STA 1880 RBL 99 SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKE - [SDR P5CA2022022100050](https://openairdocs.org/sdr/P5CA2022022100050), Mar 12, 2022: NONE. NONE. M/D - STA 1840 RBL 99 SEAT TRACK FOUND CORROSION(

M/D - STA 1840 RBL 99 SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKE - [SDR P5CA2022022100051](https://openairdocs.org/sdr/P5CA2022022100051), Mar 12, 2022: NONE. NONE. M/D STA 1270-1278 RBL 11.33" SEAT TRACK FOUND CORROSION.(

M/D STA 1270-1278 RBL 11.33" SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 5 - [SDR P5CA2022022100052](https://openairdocs.org/sdr/P5CA2022022100052), Mar 12, 2022: NONE. NONE. M/D - STA 1820 RBL 99 SEAT TRACK FOUND CORROSION(

M/D - STA 1820 RBL 99 SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKE - [SDR P5CA2022022100053](https://openairdocs.org/sdr/P5CA2022022100053), Mar 12, 2022: NONE. NONE. M/D - STA 1777 - 1784 RBL 99 SEAT TRACK FOUND CORROSION(

M/D - STA 1777 - 1784 RBL 99 SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51 - [SDR P5CA2022022100054](https://openairdocs.org/sdr/P5CA2022022100054), Mar 12, 2022: NONE. NONE. M/D - STA 1908 RBL 33 SEAT TRACK FOUND CORROSION(

M/D - STA 1908 RBL 33 SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKE - [SDR P5CA2022022100055](https://openairdocs.org/sdr/P5CA2022022100055), Mar 12, 2022: NONE. NONE. M/D - STA 1877 RBL 33 SEAT TRACK FOUND CORROSION(

M/D - STA 1877 RBL 33 SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKE - [SDR P5CA2022022100056](https://openairdocs.org/sdr/P5CA2022022100056), Mar 12, 2022: NONE. NONE. M/D STA 1860 RBL 99 SEAT TRACK FOUND CORROSION.(

M/D STA 1860 RBL 99 SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKED W - [SDR P5CA2022022100057](https://openairdocs.org/sdr/P5CA2022022100057), Mar 12, 2022: NONE. NONE. M/D STA 1830-1836 RBL 33 SEAT TRACK FOUND CORROSION.(

M/D STA 1830-1836 RBL 33 SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. - [SDR P5CA2022022100058](https://openairdocs.org/sdr/P5CA2022022100058), Mar 12, 2022: NONE. NONE. M/D STA 1774-1776 RBL 33 SEAT TRACK FOUND CORROSION.(

M/D STA 1774-1776 RBL 33 SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. - [SDR P5CA2022022100059](https://openairdocs.org/sdr/P5CA2022022100059), Mar 12, 2022: NONE. NONE. M/D STA 1922 LBL 33 SEAT TRACK FOUND CORROSION.(

M/D STA 1922 LBL 33 SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKED W - [SDR P5CA2022022100060](https://openairdocs.org/sdr/P5CA2022022100060), Mar 12, 2022: NONE. NONE. M/D STA 1822-1825 LBL 33 SEAT TRACK FOUND CORROSION.(

M/D STA 1822-1825 LBL 33 SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. - [SDR P5CA2022022100061](https://openairdocs.org/sdr/P5CA2022022100061), Mar 12, 2022: NONE. NONE. M/D STA 1886-1890 LBL 33 SEAT TRACK FOUND CORROSION.(

M/D STA 1886-1890 LBL 33 SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. - [SDR P5CA2022022100063](https://openairdocs.org/sdr/P5CA2022022100063), Mar 12, 2022: NONE. NONE. M/D - STA 2196-2198 LBL 11.33 SEAT TRACK FOUND CORROSION(

M/D - STA 2196-2198 LBL 11.33 SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM - [SDR P5CA2022022100064](https://openairdocs.org/sdr/P5CA2022022100064), Mar 12, 2022: NONE. NONE. M/D - STA 2117-2120 LBL 11.33 SEAT TRACK FOUND CORROSION(

M/D - STA 2117-2120 LBL 11.33 SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM - [SDR P5CA2022022100065](https://openairdocs.org/sdr/P5CA2022022100065), Mar 12, 2022: NONE. NONE. M/D - STA 1470-1480 RBL 11.33 SEAT TRACK FOUND CORROSION(

M/D - STA 1470-1480 RBL 11.33 SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM - [SDR P5CA2022022100066](https://openairdocs.org/sdr/P5CA2022022100066), Mar 12, 2022: NONE. NONE. M/D - STA 1350-1360 RBL 11.33" SEAT TRACK FOUND CORROSION(

M/D - STA 1350-1360 RBL 11.33" SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SR - [SDR P5CA2022022100067](https://openairdocs.org/sdr/P5CA2022022100067), Mar 12, 2022: NONE. NONE. M/D - STA 1410-1418 RBL 11.33 SEAT TRACK FOUND CORROSION(

M/D - STA 1410-1418 RBL 11.33 SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM - [SDR P5CA2022022100068](https://openairdocs.org/sdr/P5CA2022022100068), Mar 12, 2022: NONE. NONE. M/D STA 1310-1318 RBL 11.33" SEAT TRACK FOUND CORROSION(

M/D STA 1310-1318 RBL 11.33" SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51 - [SDR P5CA2022022100069](https://openairdocs.org/sdr/P5CA2022022100069), Mar 12, 2022: NONE. NONE. M/D STA 1290-1298 RBL 11.33" SEAT TRACK FOUND CORROSION(

M/D STA 1290-1298 RBL 11.33" SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51 - [SDR P5CA2022022100070](https://openairdocs.org/sdr/P5CA2022022100070), Mar 12, 2022: NONE. NONE. M/D - STA 1337 RBL 11.33 SEAT TRACK FOUND CORROSION(

M/D - STA 1337 RBL 11.33 SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. - [SDR P5CA2022022200072](https://openairdocs.org/sdr/P5CA2022022200072), Mar 12, 2022: NONE. NONE. STA 2231 1EA CRACK WAS FOUND ON REVEAL RUNNING AFT THROUGH THE FASTENER HOLE AND EXTEND TOWARDS THE EDGE(

M/D STA 2231 STR 21L - 22L DOOR REVEAL DOUBLER CRACK All 208: https://openairdocs.org/aircraft/N452PA/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 N452PA The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N452PA before. - [Cancelled 1977-06-27](https://openairdocs.org/deregistered/N452PA-1977-06-27): Boeing 707-321C, S/N 19274, built 1967. Exported to Lebanon. 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.