# N1439A: 1997 Boeing 767-33A - Status: Valid registration - Airframe: [Boeing 767-33A](https://openairdocs.org/model/boeing-767-33a) (registry code 1385209, 330 seats) - Engine: [GE CF6-80C2B6F](https://openairdocs.org/engine/ge-cf6-80c2b6f) (registry code 30109) - Data sheets: [TCDS E13NE](https://openairdocs.org/tcds/E13NE) (General Electric Company GE Aerospace) (OpenAirDocs) - Serial number: 28495 - Year built: 1997 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: May 27, 2018 - Certificate issued: October 11, 2018 - Expires: October 31, 2028 - Mode S code: A0B169 - Registered owner: [Andromeda Leasing I LLC](https://openairdocs.org/faa-owner/ANDROMEDA%20LEASING%20I%20LLC) - Location: [Purchase, NY](https://openairdocs.org/faa-place/NY/Purchase) - Owner type: LLC - Owner's area on the map: 41.0382° N, 73.7107° W: Placed by OpenAirDocs at the center of ZIP code 10577, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=1439A - Page: https://openairdocs.org/aircraft/N1439A 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. ## ADs that may apply (OpenAirDocs): 34 in force ### Matched by airframe (Boeing 767-33A) None in force. ### Matched by engine (GE CF6-80C2B6F) - [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 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 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 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 2009-07-03](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 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 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 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 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 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 95-10-11](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 94-06-03](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 - [AD 93-14-18](https://openairdocs.org/ad/93-14-18): High pressure turbine (HPT) thermal shields · General Electric CF6-45A, CF6-45A2, CF6-50A and 40 more. Effective Oct 4, 1993 - [AD 91-15-25](https://openairdocs.org/ad/91-15-25): High Pressure Compressor Rotor · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 16 more. Effective Sep 6, 1991 - [AD 91-11-05](https://openairdocs.org/ad/91-11-05): High Pressure Compressor Rotor · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 16 more. Effective Jul 5, 1991 - [AD 91-05-21](https://openairdocs.org/ad/91-05-21): High Pressure Turbine · General Electric CF6-80C2A5, CF6-80C2B6, CF6-80C2B6F and 1 more. Effective Mar 27, 1991 ### 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 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 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 2000-16-12](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 99-08-13](https://openairdocs.org/ad/99-08-13) (historical): General Electric CF6-80A, CF6-80A1, CF6-80A2 and 26 more. Effective May 13, 1999 - [AD 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 ## Information bulletins (advisory) (4 in force) - [SAIB 2023-15](https://openairdocs.org/saib/2023-15): Falsified Forms from AOG Technics. Issued Dec 19, 2023 - [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 N1439A. ## FAA accident and incident reports None matched to N1439A. ## Service difficulty reports (179, 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 IXXA20250918053](https://openairdocs.org/sdr/IXXA20250918053), Sep 18, 2025: POWER SUPPLY. INOPERATIVE. FOUND INTERIOR EMERGENCY LIGHTS RIGHT CEILING, DOOR EXIT SIGN AND DOOR THRESHOLD LIGHT INOPERATIVE DURING EMERGENCY LIGHT TEST. PLACED ON DEFERRAL 66237. MINIMU - [SDR IXXA20250908001](https://openairdocs.org/sdr/IXXA20250908001), Sep 8, 2025: TUBE. DENTED. A DENT WAS FOUND DURING C-CHECK MAINTENANCE VISIT LOCATED INSIDE 532BB BETWEEN LOWER STRINGER L-6 AND L-7. THE DENT WAS MEASURED AS L=0.400" W=0.700" D=0.129". - [SDR IXX2025F00019](https://openairdocs.org/sdr/IXX2025F00019), Sep 8, 2025: BEAM. CORRODED. FLC DOOR CUTOUT LWR SILL BEAM EXFOLIATED STA622 - [SDR IXXA2025090300018](https://openairdocs.org/sdr/IXXA2025090300018), Sep 3, 2025: TUBE. DENTED. LEFT WING FUEL DISTRIBUTION TUBE HAS A DENT, LOCATED INSIDE 532BB BETWEEN LOWER STRINGER L-6 AND L-7 - [SDR IXXA20250831002](https://openairdocs.org/sdr/IXXA20250831002), Aug 31, 2025: SKIN. CORRODED. RIGHT WING TOP EXTERNAL SKIN CORRODED AT SKIN SPICE AT WING STA 383.5-395 - [SDR IXX2025F00016](https://openairdocs.org/sdr/IXX2025F00016), Aug 31, 2025: SKIN. DELAMINATED. VERTICAL STAB PANEL LEFT SIDE DELAMINATED - [SDR IXXA2025082801](https://openairdocs.org/sdr/IXXA2025082801), Aug 9, 2025: SKIN. DELAMINATED. RHS VERTICAL STAB SKIN PANEL DELAMINATED AT FSS 270 - [SDR IXXA2023090801](https://openairdocs.org/sdr/IXXA2023090801), Sep 8, 2023: SKIN. CRACKED. LH FWD ENTRY DOOR CUTOUT AFT LOWER CORNER SKIN CRACKED. - [SDR IXXA2023090101](https://openairdocs.org/sdr/IXXA2023090101), Sep 1, 2023: SUPPORT ANGLE. CRACKED. FLC DOOR CUTOUT UPPER TRANSITION AND CEILING PANEL CRACKED AT CENTER AND GOUGES AT FWD CORNER. REPLACED FLC DOOR CUTOUT CENTER AND FWD CORNER SUPPORT ANGLES IAW - [SDR IXXA2023082800001](https://openairdocs.org/sdr/IXXA2023082800001), Aug 28, 2023: LONGERON CLIP. CRACKED. #1 PYLON HAS TWO CRACKED LONGERON CLIPS ON THE O/B AND I/B SIDE OF WEB LOCATED JUST AFT OF HYD BAY DOORS . REMOVED AND REPLACED LONGERON CLIPS IN #1 PYLON . IAW - [SDR IXXA2023082802](https://openairdocs.org/sdr/IXXA2023082802), Aug 28, 2023: ROLLER TRAY. CORRODED. ROLLER TRAY CORRODED AT STA 654+88 RBL 20 AT LOCK. COMPLETED ROLLER TRAY SPLICE REPAIR IAW B767 SRM 53-00-53 REPAIR 1 DETAIL 4 REF. AMES DOC 47574REA01. - [SDR IXXA2023090401](https://openairdocs.org/sdr/IXXA2023090401), Aug 22, 2023: ROLLER TRAY. CORRODED. ROLLER TRAY CORRODED AT STA. 478 RBL44 - [SDR IXXA20230619037](https://openairdocs.org/sdr/IXXA20230619037), Jun 15, 2023: WINDOW. UNKNOWN. SUPPLEMENTAL-5 JULY 2023-KILN DUE TO SYSTEM OUTAGE, REPORT PREVIOUSLY SUBMITTED VIA ALTERNATE EMAIL PROCEDURES. LEFT FORWARD WINDOW EICAS DISPLAYED. NO OTHER IN - [SDR IXXA2022103101](https://openairdocs.org/sdr/IXXA2022103101), Oct 25, 2022: SKIN. CRACKED. LH LE WING STA 616.2 CRACKED - [SDR IXXA2023090601](https://openairdocs.org/sdr/IXXA2023090601), Aug 26, 2022: ROLLER TRAY. CORRODED. ROLLER TRAY CORRODED AT STA 478, RBL44 - [SDR IXXA20211018078](https://openairdocs.org/sdr/IXXA20211018078), Sep 27, 2021: STIFFENER. CRACKED. WEB ON STIFFENER AT STATION 971 LBL 90 HAS DAMAGED HOLE. REMOVED, FABRICATED AND REPLACED NEW STIFFNER AT STATION 971 LBL 90 IAW ENGINEERING ORDER 74783FAB01. - [SDR IXXA20211018077](https://openairdocs.org/sdr/IXXA20211018077), Sep 24, 2021: FAILSAFE. CRACKED. RIGHT FAILSAFE STRAP AT STA 955 HAS A CRACK INDICATION ON ULTRASOUND NDT INSPECTION. REPAIRED FAILSAFE STRAP AT STATION 955 IAW AMES ENGINEERING ORDER 472070RD0 - [SDR IXXA20211018075](https://openairdocs.org/sdr/IXXA20211018075), Sep 24, 2021: FLAP. DELAMINATED. LEFT WING TRAILING EDGE INBOUND TRAILING EDGE PLAP HAS DELAM AREA ON INBOUND EDGE. LAYED UP AND CURED IAW B767 SRM 51-70-10. - [SDR IXXA20211018074](https://openairdocs.org/sdr/IXXA20211018074), Sep 24, 2021: BEAM. CRACKED. INBOUND HYD BAY LATCH CHANNEL IS CRACKED AT #3 LATCH MOUNT AREA. REMOVED AND REPLACED BEAM IAW B767 SRM 51-40-02. - [SDR IXXA20211018069](https://openairdocs.org/sdr/IXXA20211018069), Sep 24, 2021: SKIN. DELAMINATED. RIGHT SIDE VERTICAL BETWEEN THE AUX SPAR AND FRONT SPAR THE COMPOSITE SKIN PANEL IS DELAMINATED. REPAIRED RIGHT SIDE VERT STAB PANEL BETWEEN THE AUX SPAR AND FT - [SDR IXXA20211018067](https://openairdocs.org/sdr/IXXA20211018067), Sep 23, 2021: WEB. CRACKED. FWD DOUBLER ON FAIRING SUPPORT WEB AT TA 1081 CRACKED, FABRICATED AND REPLACED NEW DOUBLER IAW B767 SRM 51-10-02. - [SDR IXXA20211017066](https://openairdocs.org/sdr/IXXA20211017066), Sep 23, 2021: DOUBLER. CRACKED. AFT DOUBLER ON FAIRING SUPPORT WEB AT STA 1081 CRACKED. FABRICATED AND REPLACED NEW DOUBLER IAW B767 SRM 51-10-02. - [SDR IXXA20211017068](https://openairdocs.org/sdr/IXXA20211017068), Sep 21, 2021: NONE. CRACKED. RIGHT STUB BEAM CRACKED AT STATION 903.5 RBL89.REPAIRED RIGHT CRACKED STUB BEAM AT STATION 903.5 RBL 89 IAW ENGINEERING ORDER 53-767-7702. - [SDR IXXA20211018076](https://openairdocs.org/sdr/IXXA20211018076), Sep 20, 2021: FORMER. CRACKED. NOSE FORMER IS CRACKED BY #9 SLAT INBOUND AUX TRACK AT WING LEADING STATION 562. REMOVED AND REPLACED DAMAGE NOSE FORMER IAW B767 SRM 51-40-02. - [SDR IXXA2021100018075](https://openairdocs.org/sdr/IXXA2021100018075), Sep 20, 2021: RIB. CRACKED. LEFT WING LEADING EDGE AT APPROXIMATELY LES 563.0 HAS CRACKED NOSE RIB. REMOVED AND REPLACED NOSE RIB ON LEFT WING LEADING EDGE AT WS STA 565.9 IAW B767 51-40-0 - [SDR IXXA20211018073](https://openairdocs.org/sdr/IXXA20211018073), Sep 18, 2021: NONE. CRACKED. #2 AFT STRUT FAIRING SMALL ANGLE ON BACK SIDE OF HYD COMPT OUTBOARD SIDE CRACKED. REMOVED AND REPLACED SMALL "C" ANGLE ON #2 AFT STRUT FAIRING FWD SIDE JUST AFT - [SDR IXXA20211018071](https://openairdocs.org/sdr/IXXA20211018071), Sep 18, 2021: CHANNEL. CRACKED. #2 AFT STRUT FAIRING WEB OUTBOARD "U" CHANNEL CRACKED AT BOTTOM IN RADIUS. REMOVED CHANNEL AND MATCH DRILLED NEW "U" CHANNEL IAW B767 SRM 51-40-05 AND INSTALLED - [SDR IXXA20211018072](https://openairdocs.org/sdr/IXXA20211018072), Sep 17, 2021: STIFFENER. CRACKED. #2 AFT STRUT FAIRING ANGLE ON INBOUND FORWARD SIDE OF AFT WEB RUNNING FORE AND AFT IS CRACKED. REMOVED AND REPLACED STRUT FAIRING ANGLE IAW B767 SRM 51-40-02. - [SDR IXXA20211018070](https://openairdocs.org/sdr/IXXA20211018070), Sep 16, 2021: BULKHEAD. CRACKED. #1 PYLON PANEL 437DB V FRAME CRACKED. REMOVED DAMAGED V FRAME AND INBD CHANNEL MATCH DRILLED HOLES IAW B767 1-40-05 AND REINSTALLED CHANNELS AND V FRAME IAW B76 - [SDR IXXA20200920036](https://openairdocs.org/sdr/IXXA20200920036), Sep 16, 2020: FLASHLIGHT. INOPERATIVE. RIGHT FLIGHT DECK EMERGENCY FLASHLIGHT IS INOPERATIVE. CENTER FLASHLIGHT IS OPERATIONAL. INITIATED DEFERRAL MAINTENANCE ITEM-17342. REMOVED AND REPLACED RIGHT F - [SDR UIEA2019091605511](https://openairdocs.org/sdr/UIEA2019091605511), Sep 13, 2019: CLAMP. NOT SEATED. "LEFT BLEED DUCT LEAK" CAUTION EICAS MSG. COMPLETED ASSOCIATED QRH PROCEDURE. INSPECTED LEFT PACK CROSS OVER DUCT, ISO VALVE, AND ACM AREA CLAMPS WITH BAY DOORS - [SDR UIEA2019090805459](https://openairdocs.org/sdr/UIEA2019090805459), Sep 8, 2019: UNKNOWN. MALFUNCTIONED. LP 1100481 (MIA) - SPAR VALVE CHECK FAILS DURING ENG START - RT ENG - RETURN TO BLOCKS. LP 1100482 (CVG) - INFO ONLY - DURING RT ENG START SPAR VALVE CYCLES NOR - [SDR UIEA2019082875308](https://openairdocs.org/sdr/UIEA2019082875308), Aug 27, 2019: OIL SYSTEM. UNDERSERVICED. "APU FAULT" EICAS, 2 ATTEMPTS UNSUCCESSFUL. SERVICED APU OIL IAW AMM 12-13-04. OPS CHECK OK, START ON FIRST ATTEMPT PER AMM 49-11-00. - [SDR UIEA2019082955285](https://openairdocs.org/sdr/UIEA2019082955285), Aug 25, 2019: PRESSURE SWITCH. FAILED. APU FAULT, SHUTDOWN DURING POWER TRANSFER. BIT CHECKED THE APU ECU AND FOUND IT WAS FLAGGING LOW OIL PRESSURE IAW FIM 49-11 FT 987. REMOVED AND REPLACED APU LOW - [SDR UIEA2019082755280](https://openairdocs.org/sdr/UIEA2019082755280), Aug 24, 2019: WARNING MESSAGE. FALSE ACTIVATION. AFT EQ EXH FAN 2 STATUS MESSAGE. T/S PER FIM 21-26 FAULT TREE 808. MESSAGE CLEARED, OPS CHECK NORMAL. - [SDR UIEA2019080984972](https://openairdocs.org/sdr/UIEA2019080984972), Aug 9, 2019: DISPLAY. MALFUNCTIONED. RADAR DISPLAYS SCATTERED RETURNS ACROSS ENTIRE DISPLAY WITH NO PRECIP IN VICINITY. PERFORMED WX RADAR OPERATIONAL TEST IAW AMM 34-43-00. OPS TEST OK, NO DEFECTS - [SDR UIEA2019080534938](https://openairdocs.org/sdr/UIEA2019080534938), Aug 2, 2019: SHUTOFF VALVE. UNKNOWN. EICAS AND STATUS MSG: R ENG HPSOV. PERFORMED RIGHT ENGINE RUN, NO MESSAGE DISPLAYED AT THIS TIME. PACK PRESSURE HOLDS GOOD. THERE ARE NO DEFECTS FOUND AT THIS T - [SDR UIEA2019080204931](https://openairdocs.org/sdr/UIEA2019080204931), Aug 1, 2019: WARNING MESSAGE. FALSE ACTIVATION. RIGHT ENGINE HPSOV DISPLAYED ON STATUS PAGE. PERFORMED A BITE TEST, NO FAULTS FOUND. SYSTEM OPS CHECKED GOOD IAW AMM 36-00-00. - [SDR UIEA2019080134899](https://openairdocs.org/sdr/UIEA2019080134899), Jul 30, 2019: WARNING MESSAGE. FALSE ACTIVATION. RIGHT ENGINE HPSOV MESSAGE DISPLAYED ON EICAS, IN FLIGHT. PERFORMED AIR SUPPLY BITE PROCEDURE IAW FIM 36-20-00/101. FOUND RH SYS PRV LIGHT ILLUMINATED. PERFORME - [SDR UIEA2019072704868](https://openairdocs.org/sdr/UIEA2019072704868), Jul 27, 2019: SWITCH. FAULTY. FWD CARGO FIRE SWITCH LIGHT ON THE P-8 PANEL WOULD NOT TEST DURING SYSTEM OR BRIGHT LIGHT TEST. (BULB GOOD) FWD CARGO FIRE SYSTEM PLACED ON MEL DEFERRAL IAW DDG - [SDR UIEA2019072604864](https://openairdocs.org/sdr/UIEA2019072604864), Jul 26, 2019: CONTROL VALVE. MALFUNCTIONED. L BLEED DUCT LEAK. (

TRANSFERRED TO DMI 115382 PER MEL 21-51-01-01, CAT 'C', DUE DATE: 05-AUG-19. PLACARDS INSTALLED AND MX ACTION C/W. 

LP 1053595 - [SDR UIEA2019072104800](https://openairdocs.org/sdr/UIEA2019072104800), Jul 21, 2019: OIL SYSTEM. LOW. APU WOULD NOT START.  (

PERFORMED B767 FIM 49-11 FT 987 APU BITE PROCEDURES. SERVICED OIL, CLEARED FAULTS. OPS CHECK GOOD.  

) - [SDR UIEA2019071604763](https://openairdocs.org/sdr/UIEA2019071604763), Jul 16, 2019: BRAKE. FIRE. ON EXITING RW, TWR ADVISED SMOKE & FIRE EMANATING FROM LEFT MAIN GEAR. EMERGENCY VEHICLES RESPONDED & SPRAYED GEAR.(

REMOVED AND REPLACED #6 BRAKE ASS - [SDR UIEA2019071204738](https://openairdocs.org/sdr/UIEA2019071204738), Jul 12, 2019: BLEED AIR SYS. MALFUNCTIONED. NO DUCT PRESSURE DURING APU OPERATION.(

TRANSFERRED TO MDDR 114602 PER 49-11-01-01 CAT C DUE 21JUL19 VALVE LOCKED OUT PER DDG 36-11-01.

LP 1080383 - M2: - [SDR UIEA2019071204739](https://openairdocs.org/sdr/UIEA2019071204739), Jul 9, 2019: UNKNOWN. MALFUNCTIONED. NO APU DUCT PRESSURE ON STARTUP AFTER LANDING. (

RE-STARTED APU DUCT PRESSURE NORMAL, NO FAULTS FOUND REF AMM 49-11-00 DUCT PRESSURE REF 49-52-00.RT ENGINE IGN. 1(A) INOP, DEFERRED IGN 1(A) PER MEL 74-00-01B CAT 'C'. TH - [SDR UIEA2019062864592](https://openairdocs.org/sdr/UIEA2019062864592), Jun 25, 2019: LIGHT. INTERMITTENT. RIGHT ENG BLEED OFF BACKLIGHTING, NO ILLUMINATION WITH ENG SHUT DOWN. FOUND DURING COCKPIT PRE-FLIGHT. RESET RT ENG BLEED SWITCH IAW AMM 36-20-00. OFF LIGHT CAM - [SDR UIEA2019062404564](https://openairdocs.org/sdr/UIEA2019062404564), Jun 24, 2019: EXCITER. MALFUNCTIONED. ITEM 1 - INFO, FIRST START ATTEMPT ON RIGHT ENGINE NO LIGHT OFF. ITEM 2 - STATUS MESSAGE: R ENG IGNITER 1(

RT ENG #1 IGNITION INOP. PLACED ON MEL 74-00-01B DM - [SDR UIEA2019062104551](https://openairdocs.org/sdr/UIEA2019062104551), Jun 20, 2019: SWITCH. BROKEN. CAPTAIN`S OXYGEN TEST RESET SWITCH BROKEN. REMOVED AND REPLACED CAPT OXYGEN STOWAGE PER ASSY AS REQ, LEAK CHECKED GOOD IAW AMM 35-11-51. - [SDR UIEA2019061874510](https://openairdocs.org/sdr/UIEA2019061874510), Jun 17, 2019: EXCITER. MALFUNCTIONED. # 2 ENGINE DID NOT START WITH SINGLE IGNITER , SWITCHED TO BOTH FOR BOTH ENGINE STARTS. PERFORMED NO.2 SYS IGNITION AUDIBLE TEST. CONFIRMED ONLY ONE IGNITER IS All 179: https://openairdocs.org/aircraft/N1439A/reports.md ## STCs that may be installed (OpenAirDocs) (5) 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 CF6-80C2B6F) - [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 - [STC SE01478CH](https://openairdocs.org/stc/SE01478CH): Installation of Cook Airtomic alignment joint p/n AIR 22912. Cook Airtomic - [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 - [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. Lists CF6-80 Series ## Earlier aircraft with N1439A The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N1439A before. - [Cancelled 2007-04-17](https://openairdocs.org/deregistered/N1439A-2007-04-17): Cessna 172R, S/N 17281358, built 2007. Exported to China. Owner: [Wichita, KS](https://openairdocs.org/faa-place/KS/Wichita) - [Cancelled 2004-03-23](https://openairdocs.org/deregistered/N1439A-2004-03-23): Fokker F.28 MK 0100, S/N 11434, built 1993. Exported to Canada. Owner: [American Airlines Inc](https://openairdocs.org/faa-owner/AMERICAN%20AIRLINES%20INC), [Dfw Airport, TX](https://openairdocs.org/faa-place/TX/Dfw%20Airport) - [Cancelled 1969-09-26](https://openairdocs.org/deregistered/N1439A-1969-09-26): Beech 36, S/N E-171, built 1969. Exported to South Africa. Owner: [Air Capital International Inc](https://openairdocs.org/faa-owner/AIR%20CAPITAL%20INTERNATIONAL%20INC), [Augusta, KS](https://openairdocs.org/faa-place/KS/Augusta) - [Cancelled 1967-05-29](https://openairdocs.org/deregistered/N1439A-1967-05-29): Piper PA-22-135, S/N 22550. Exported to Nicaragua. Owner: [Kirschner Jack B](https://openairdocs.org/faa-owner/KIRSCHNER%20JACK%20B), Managua ## Related - Other Boeing 767-33A aircraft: https://openairdocs.org/model/boeing-767-33a/aircraft.md - The GE CF6-80C2B6F engine: https://openairdocs.org/engine/ge-cf6-80c2b6f.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.