# N1489A: 1994 Boeing 767-31K - Status: Valid registration - Airframe: [Boeing 767-31K](https://openairdocs.org/model/boeing-767-31k) (registry code 1385192, 261 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: 27206 - Year built: 1994 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: June 28, 2018 - Certificate issued: October 11, 2018 - Expires: October 31, 2028 - Mode S code: A0C3FC - 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=1489A - Page: https://openairdocs.org/aircraft/N1489A 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 767-31K) 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 N1489A. ## FAA accident and incident reports None matched to N1489A. ## Service difficulty reports (293, 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 ABXA20260929441](https://openairdocs.org/sdr/ABXA20260929441), Sep 29, 2026: SWITCH. FAILED. EMER LIGHTS SWITCH DOES NOT CHANGE INTO ARMED WITH SWITCH GUARD DOWN. MTC REMOVED AND REPLACED EMERGENCY LIGHT SWITCH GUARD IAW AMM 33-51-00. OPS CHECK GOOD. A/ - [SDR ABXA20260906396](https://openairdocs.org/sdr/ABXA20260906396), Sep 6, 2026: WARNING MESSAGE. FALSE ACTIVATION. DURING APPROACH MESSAGE "FIRE/ OVHT SYS" ILLUMINATED , MTX PERFORMED AFOLTS TEST IAW B767 AMM 26-10-00. OPS CHECK GOOD. NFF RETURNED A/C TO SERVICE. - [SDR ABXA20260804347](https://openairdocs.org/sdr/ABXA20260804347), Aug 4, 2026: MODULE. DEFECTIVE. AT APPROXIMATELY 300FT AGL THE FLIGHT CREW RECEIVED THE AURAL WARNING, TOO LOW, FLAPS. BOTH THE FO AND PILOT CONFIRMED FLAPS 25 WAS INDICATED. THE PILOT CALLED - [SDR ABXA20260707310](https://openairdocs.org/sdr/ABXA20260707310), Jul 7, 2026: ESCAPE REEL. EXPIRED. DURING INSP/MTC, NR 3 ESCAPE REEL FOUND OUT OF DATE. DEFERRED THE NR 3 ESCAPE REEL IAW MEL 25-61-1-1 C/W MAINTENANCE PROCEDURE 25-61-1 MBCB 07/17/26 PLACARDS IN - [SDR ABXA20260623277](https://openairdocs.org/sdr/ABXA20260623277), Jun 23, 2026: EXTINGUISHER. UNSECURE. PIN TO COCKPIT FIRE EXTINGUISHER NEAR LAV DISCOVERED ON FLOOR BY MTC. REATTACHED PIN TO FIRE EXTINGUISHER HANDLE USING BREAKAWAY WIRE. PLACARDS INSTALLED. ACFT - [SDR ABXA20260622274](https://openairdocs.org/sdr/ABXA20260622274), Jun 22, 2026: WARNING MESSAGE. ILLUMINATED. AFTER PUSHBACK, DURING TAXI, LT REV ISLN VALVE. RETURNED TO GATE (BTB). PLACED LEFT T/R ON DI PER MEL 78-31-1 MBCB 07/02/2026 PLACARD INSTALLED A/C DOWNGRADED T - [SDR ABXA20260619271](https://openairdocs.org/sdr/ABXA20260619271), Jun 19, 2026: FIRE LOOP. FAULTED. LT ENG FIRE LP 1, STATUS MESSAGE IN FLIGHT ACFT LANDED NO PROBLEMS, MTX GROUNDED ACFT AND DEFERRED LP 1 LOOP IAW MEL ABX-26-11-1-1 AND RETURNED A/C TO SERVICE. - [SDR ABXA20260616263](https://openairdocs.org/sdr/ABXA20260616263), Jun 16, 2026: EXTINGUISHER. DAMAGED. DURING CREW PREFLIGHT, CREW SAID THE RT PORTABLE FIRE EXTINGUISHER BY LAV MOUNTED ON GROUND HAD A CROOKED PRESSURE GAUGE AND WAS WORRIED IT COULD RUPTURE IN FLI - [SDR ABXA20260427178](https://openairdocs.org/sdr/ABXA20260427178), Apr 27, 2026: ACTUATOR. MALFUNCTIONED. RUDDER RATIO EICAS MESSAGE ON TAXI OUT. REMOVED AND REPLACED RUDDER RATIO CHANGER ACTUATOR IAW B767 AMM 27-21-15 LEAK CHECK GOOD, OPS CHECK GOOD.RAN BOTH ENGINE - [SDR ABXA20260424172](https://openairdocs.org/sdr/ABXA20260424172), Apr 24, 2026: EEC. FAULTED. DURING TAXI, ON ENGINE START BOTH EEC TO ALT W/ L & R ENG EEC MODE EICAS MESSAGES. CREW RETURNED TO THE GATES (BTB). MTC DEFERRED IAW MEL 73-21-1-3 NO MX ACTION - [SDR ABXA20260422170](https://openairdocs.org/sdr/ABXA20260422170), Apr 22, 2026: PITOT TUBE. DEFECTIVE. AFTER ENGINE START AND TAXI OUT, CAPT PITOT ANNUNCIATOR AND EICAS MESSAGE. CREW RETURNED TO BLOCKS (BTB). MAINTENANCE REMOVED AND REPLACED CAPT PITOT IAW B767 A - [SDR ABXA20260221074](https://openairdocs.org/sdr/ABXA20260221074), Feb 21, 2026: RELAY. FAULTED. L AUX PITOT EICAS MSG DURING TAXI OUT, AC RETURNED TO GATE (BTB) AND MTX GROUNDED AC . MTX . REMOVED AND REPLACED L AUX PITOT IAW B767 AMM 34-11-01 OPS AND LEAK - [SDR ABXA20251122306](https://openairdocs.org/sdr/ABXA20251122306), Nov 22, 2025: SENSOR. FAULTED. RIGHT ENGINE CONTROL EICAS MESSAGE AFTER PUSHBACK FROM GATE AFTER ENGINE START, ACFT RETURNED TO GATE (BTB), AND MTX GROUNDED ACFT, MTX TROUBLESHOT & PERFORMED - [SDR ABXA20250419082](https://openairdocs.org/sdr/ABXA20250419082), Apr 19, 2025: INDICATOR. UNRELIABLE. DURING CLIMB, AIRSPEED UNRELIABLE / STUCK AT 270 KTS INDICATION OF OVERSPEED WITH FLAPS & GEAR UP AT 270 KTS. EMERGENCY DECLARED, AIR TURN BACK. (ATB) . MAINTEN - [SDR ABXA20250315057](https://openairdocs.org/sdr/ABXA20250315057), Mar 15, 2025: STARTER. MALFUNCTIONED. DURING TAXI WHILE STARTING #2 ENGINE THE ENGINE FAILED TO START, A/C RETURNED TO GATE (BTB) AND MTX GROUNDED A/C. MTX TROUBLESHOT AND FOUND STARTER HAD FAILED I - [SDR ABXA20250214037](https://openairdocs.org/sdr/ABXA20250214037), Feb 14, 2025: VALVE. MALFUNCTIONED. DURING TAXI WHILE DEICING A/C L ENGINE ANTI-ICE EICAS 5PSI L ENGINE PACK ILLUMINATED ON EICAS, A/C THEN RETURED TO THE GATE AND MTX GROUNDED A/C, MTX THEN TROUB - [SDR ABXA20250131029](https://openairdocs.org/sdr/ABXA20250131029), Jan 31, 2025: RELAY. MALFUNCTIONED. DURING TAXI CREW REPORTED AFTER STARTING L&R ENG. EEC MODE AND PROBE HEAT EICAS MESSAGE DISPLAYED , A/C RETERNED TO THE GATE (BTB) AND MTX GROUNDED A/C , FOUND - [SDR ABXA20250130027](https://openairdocs.org/sdr/ABXA20250130027), Jan 30, 2025: PROXIMITY SWITCH. MALFUNCTIONED. "ATC DECARED EMERGENCY CREW REPORTS LND GEAR MONITOR, NOSE A/G DISAGREE, AIR/GROUND DISAGREE STATUS MESSAGES DISPLAYED IN FLIGHT UPON LANDING NO AUTOBRAKES, NO - [SDR ABXA20241214256](https://openairdocs.org/sdr/ABXA20241214256), Dec 14, 2024: WARNING MESSAGE. FALSE ACTIVATION. DURING TAXI, PARKING BRAKE EICAS MSG ILLUMINATED AND PARKING BRAKE ILLUMINATED AC RETURNED TO GATE (BTB) AND MTX GROUNDED AC . MTX PERFORMED OPS CHECK OF THE PA - [SDR ABXA20241204242](https://openairdocs.org/sdr/ABXA20241204242), Dec 4, 2024: SHUTOFF VALVE. MALFUNCTIONED. DURING DE-ICE BOTH L & R PACKS & L & R ENGINE BLEEDS OFF. L ENG BLEED DID NOT DISPLAY "OFF" NOR WAS A "L ENG BLEED OFF" EICAS MSG DISPLAYED .AC RETURNED TO THE - [SDR ABXA2024118219](https://openairdocs.org/sdr/ABXA2024118219), Nov 8, 2024: GENERATOR. WARNING LIGHT. LH GEN DRIVE LIGHT ON PUSHBACK FOLLOWED QRH PROCRDURES AC RETURNED TO THE GATE AND MTX GROUNDED AC , MTX DEFERRED GEN FOR DEPARTURE AND RETURNED AC TO SERVICE . - [SDR ABXA20241008185](https://openairdocs.org/sdr/ABXA20241008185), Oct 8, 2024: UNKNOWN. ODOR. CREW REPORTS THERE WAS A STRONG BURNT RUBBER SMELL IN COCKPIT ON DECENT AND AFTER LANDING. MTX GROUNDED AC AND PERFORMED AR CONDITIONING SYSTEM OIL SMOKE /FUME - [SDR ABXA20240925179](https://openairdocs.org/sdr/ABXA20240925179), Sep 25, 2024: DRIVE ASSY. MALFUNCTIONED. WXR RADAR FAIL MULTIPLE TIMES ON CLIMB OUT. WXR SYS STATUS MSG DISPLAYED. AC PERFORMED ATB AND LANDED MTX GOUNDED AC. REMOVED AND REPLACED WXR DRIVE UNIT IAW B7 - [SDR ABXA202408275157](https://openairdocs.org/sdr/ABXA202408275157), Aug 25, 2024: PRESSURE SWITCH. MALFUNCTIONED. ON PUSH BACK C HYD PRES EICAS MSG AND CENTER HYD DISCRETE LIGHT ILLUMINATED AC RETURNED TO GATE AND MTX GROUNDED AC TROUBLE SHOT FOUND CENTER HYD PRESSURE SITCH - [SDR UIEA2024041900287](https://openairdocs.org/sdr/UIEA2024041900287), Apr 24, 2024: FRAME. CORRODED. CORROSION ON FRAME WEB AT STA 1562 BETWEEN STGR 38RH AND STGR 39RH(

CORROSION ON FRAME WEB WAS REPAIRED PER CMA-TLS 24-0135-03B. NO FURTHER DEFECTS NOTED.

- [SDR UIEA2024041900288](https://openairdocs.org/sdr/UIEA2024041900288), Apr 24, 2024: SKIN. DELAMINATED. LH HORIZONTAL STABILIZER, LH ELEVATOR, DELAMINATION ON THE OUTBOARD LOWER SKIN BETWEEN OF ELEV STA 325.109 AND ELEV STA 251.665(

DELAMINATION ON LH ELEVATOR L - [SDR UIEA2024041900289](https://openairdocs.org/sdr/UIEA2024041900289), Apr 24, 2024: FLAP TRACK. DAMAGED. LEFT WING TRAILING EDGE OUTBOARD FLAP, TRACK #2 ON INBOARD STAP AFT LOWER HOLE ELONGATED.(

FLAP TRACK #2 FITTING ASSY 1-3 WITH ELONGATED HOLES (2 EA) WERE REP - [SDR UIEA2024041900290](https://openairdocs.org/sdr/UIEA2024041900290), Apr 24, 2024: SKIN. DENTED. FOUR DENTS ON RH WING, INB AFT FLAP UPPER SKIN AT: 1) IFS 114.5 AND 7" FROM T/E 2) IFS 119.5 AND 5.5" FROM T/E 3) IFS 121.75 AND 3" FROM T/E 4) IFS 122.5 AND 5. - [SDR UIEA2024041900291](https://openairdocs.org/sdr/UIEA2024041900291), Apr 24, 2024: FLAP TRACK. CORRODED. RH WING INB FLAP, TRACK #6 ATTACHMENT BOLT HOLES WITH CORROSION.(

 

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CORROSION ON RH WING INB FLAP, TRACK #6 BOLT HOLES (2 EA) WERE REPAIRED PER - [SDR UIEA2024042000299](https://openairdocs.org/sdr/UIEA2024042000299), Apr 24, 2024: SUPPORT BEAM. CORRODED. LH WING, MAIN LANDING GEAR SUPPORT BEAM, BUSHING OUTER RACE CAVITY, WITH CORROSION.(

CORROSION ON LH MLG SUPPORT BEAM AT HOLE FOR AFT TRUNNION BUSHINGS WAS RE - [SDR UIEA2024042000300](https://openairdocs.org/sdr/UIEA2024042000300), Apr 24, 2024: SUPPORT BEAM. CORRODED. RH WING, MAIN LANDING GEAR SUPPORT BEAM, BUSHING OUTER RACE CAVITY, WITH CORROSION.(

CORROSION ON RH MLG SUPPORT BEAM AT HOLE FOR AFT TRUNNION BUSHINGS WAS RE - [SDR UIEA2024042000301](https://openairdocs.org/sdr/UIEA2024042000301), Apr 24, 2024: SHEAR WEB. CORRODED. ELECTRONIC ELECTRIC COMPARTMENT, CORROSION ON THE BEAM AT STA 266.5, ON 40RBL(

SHEAR WEB WAS REPLACED PER DWG 141T5400. NO FURTHER DEFECTS NOTED

) - [SDR UIEA2024042900323](https://openairdocs.org/sdr/UIEA2024042900323), Apr 24, 2024: PANEL. CORRODED. AFT FUSELAGE, AFT CARGO HANDLING PANEL, CUTOUT AT RH UPPER CORNER, WITH CORROSION(

CORROSION ON SECTION 46 FUSELAGE BEAR STRAP AT CUT OUT WAS REPAIRED PER CMS - [SDR UIEA2024042900324](https://openairdocs.org/sdr/UIEA2024042900324), Apr 24, 2024: TORQUE TUBE. CORRODED. RH WING INB FLAP, INB RIB TORQUE TUBE SUPPORT UPPER ATTACHMENT BOLT HOLE WITH CORROSION.(

CORROSION ON RH WING INBOARD MAIN FLAP END RIB AT TORQUE TUBE SUPPOR - [SDR UIEA2024042900325](https://openairdocs.org/sdr/UIEA2024042900325), Apr 24, 2024: PANEL. GOUGED. FUSELAGE, FWD CARGO HANDLING PANEL, LH SIDE OF CUTOUT, WITH GOUGES.(

GOUGE ON SECTION 43 FUSELAGE BEARSTRAP AT THE CUTOUT BETWEEN STA 453/478 AND STGR 23 RH W - [SDR UIEA2024042900326](https://openairdocs.org/sdr/UIEA2024042900326), Apr 24, 2024: FLAP TRACK. DAMAGED. RIGHT WING TRAILING EDGE OUTBOARD FLAP, TRACK #8 ON INBOARD STRAP AFT LOWER HOLE ELONGATED.(

(3 EA) ELONGATED HOLES, HOLE WITH GOUGE AND HOLE WITH CORROSION O - [SDR UIEA2024042900327](https://openairdocs.org/sdr/UIEA2024042900327), Apr 24, 2024: FLAP TRACK. DAMAGED. LEFT WING TRAILING EDGE OUTBOARD FLAP, TRACK #1 ON INBOARD STAP AFT LOWER HOLE ELONGATED(

TWO (2 EA) ELONGATED HOLES ON LH WING FLAP TRACK #1 FITTING ASSY 1-3 - [SDR ABXA20241121229](https://openairdocs.org/sdr/ABXA20241121229), Feb 21, 2024: APU. LOW PRESSURE. STARTED RIGHT ENGINE DURING TAXI . GOT 2 HUNG STARTS. N 2 MAX WAS 40. QRC DID NOT FIX IT(APU AIR DUCT PRESS LOW) AC RETURNED TO GATE (BTB) AND MTX GROUNDED AC . - [SDR UIEA2023080100767](https://openairdocs.org/sdr/UIEA2023080100767), Jul 27, 2023: ECU. UNKNOWN. ENGINE FAILURE ( ROLLBACK) RIGHT SIDE.(

PERFORMED TROUBLESHOOTING OF #2 ENGINE FLAMEOUT IAW B767 FIM 71-05 FT 841 TO BLOCK 4 ITEM 23 SHEET 2.

/

# 2 ENG - [SDR UIEA2023072700762](https://openairdocs.org/sdr/UIEA2023072700762), Jun 27, 2023: ECU. UNKNOWN. ENGINE FAILURE (ROLL BACK) RIGHT SIDE (IFSD)(

PERFORMED T/S OF #2 ENG FLAEMOUT IAW FIM 71-05 FT 841 TO BLOCK 4 ITEM 23 SHEET 2. #2 ENGINE REQ REPLACEMENT OF W - [SDR UIEA2023050900436](https://openairdocs.org/sdr/UIEA2023050900436), May 8, 2023: UNKNOWN. UNKNOWN. NACELLE STRUT # 1 AFT FAIRING LOWER PANEL HAS ONE SCREW MISSING AT O/B SIDE .(

INSTALLED MISSING SCREW AT NACELLE STRUT #1 AFT FAIRING O/B SIDE IAW B767 SRM 5 - [SDR UIEA2023050900437](https://openairdocs.org/sdr/UIEA2023050900437), May 8, 2023: UNKNOWN. UNKNOWN. LEFT NACELLE STRUT # 1 AFT FAIRING O/B FWD INSPECTION PANEL HAS ONE SCREW LOOSE .(

SECURED SCREW AT L/H NACELLE STRUT #1 AFT FAIRING IAW B767 SRM 51-40-02. NO - [SDR UIEA2023050900438](https://openairdocs.org/sdr/UIEA2023050900438), May 8, 2023: SEAL. UNKNOWN. LEFT WING O/B FLAP INBOARD EDGE HAS THE UPPER SEAL DAMAGED AT AFT END.(

REMOVED DAMAGED SEAL, CLEANED RETAINER LOCATED AND INSTALLED NEW SEAL AT L/H WING O/B - [SDR UIEA2023050900439](https://openairdocs.org/sdr/UIEA2023050900439), May 8, 2023: ELT. UNKNOWN. SUPERNUMERARY PORTABLE ELT AUTOMATIC RELEASE SEAL DAMAGE. P/N 1151324-1 S/N 1151324-05962 06 NOV 23(

REMOVED AND INSTALLED PORTABLE ELT AT SUPERNUMERARY POSIT - [SDR UIEA2023050900440](https://openairdocs.org/sdr/UIEA2023050900440), May 8, 2023: SNUBBER. UNKNOWN. NLG WHEEL WELL SNUBBERS BRAKE PADS WORN OUT.(

REMOVED  WORN OUT  SNUBBERS  PADS  LOCATED   DRILLED   AND  INSTALL - [SDR UIEA2023050900441](https://openairdocs.org/sdr/UIEA2023050900441), May 8, 2023: UNKNOWN. UNKNOWN. FWD E& E CREW OXYGEN NEED SERVICE TO FULL .(

SERVICED CREW OXYGEN CYLINDER @ LOWER  E&E COMPARTMENT IAW 767-300 AMM 12-15-08, AMM 35-00-00, AMM  - [SDR UIEA2023050900442](https://openairdocs.org/sdr/UIEA2023050900442), May 8, 2023: UNKNOWN. UNKNOWN. #2 ENG PNEU DUCT SUPPORT ROD BOLT MISSING 12 O'CLOCK POS FWD OF PRV .(

INSTALLED BOLT #2 ENG PNEU DUCT AT 12 O'CLOCK POS FWD OF PRV PER AMM 20-11-0

) - [SDR UIEA2023050900443](https://openairdocs.org/sdr/UIEA2023050900443), May 8, 2023: SURGE VALVE. UNKNOWN. APU SURGE VALVE PNEUMATIC DUCT ASSY RUBBER COUPLING IS DAMAGED(

REMOVED AND REPLACED APU SURGE VALVE PNEUMATIC DUCT ASSY PER AMM 44-53-01-404-010. LEAK CHECK - [SDR UIEA2023050900435](https://openairdocs.org/sdr/UIEA2023050900435), May 8, 2023: LATCH. UNKNOWN. NACELLE STRUT #1 ACCESS DOOR AFT LATCH IS NOT PROPERLY SEATED(

REMOVED AND REPLACED 4EA LATCHES AT #1 ENG NACELLE STRUT ACCESS DOORS IAW B767 SRM 51-40-02. OP - [SDR UIEA2022120601205](https://openairdocs.org/sdr/UIEA2022120601205), Dec 6, 2022: PROXIMITY SWITCH. FAULTED. LE FLAP ASSYMETRY EICAS MASSAGE WAS LE SLAT ASYM NOT FLAP. C/W FIM PROCEDURE 27-90-14 AND FOUND CODE 284 ON PSEU. REMOVED AND REPLACED LT INBD PROX SWITCH 284 I All 293: https://openairdocs.org/aircraft/N1489A/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 N1489A The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N1489A before. - [Cancelled 1996-06-25](https://openairdocs.org/deregistered/N1489A-1996-06-25): Piper PA-22, S/N 22399. Triennial form not returned. Owner: [Zumwalt Dennis L](https://openairdocs.org/faa-owner/ZUMWALT%20DENNIS%20L), [Deming, NM](https://openairdocs.org/faa-place/NM/Deming) ## Related - Other Boeing 767-31K aircraft: https://openairdocs.org/model/boeing-767-31k/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.