# N1487A: 1997 Boeing 767-31K - Status: Valid registration - Airframe: [Boeing 767-31K](https://openairdocs.org/model/boeing-767-31k) (registry code 1385192, 261 seats) - Engine: [GE CF6-80C2B7F](https://openairdocs.org/engine/ge-cf6-80c2b7f) (registry code 30114) - Data sheets: [TCDS E13NE](https://openairdocs.org/tcds/E13NE) (General Electric Company GE Aerospace) (OpenAirDocs) - Serial number: 28865 - Year built: 1997 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: October 4, 2018 - Certificate issued: December 7, 2018 - Expires: December 31, 2028 - Mode S code: A0C3B6 - 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=1487A - Page: https://openairdocs.org/aircraft/N1487A 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): 32 in force ### Matched by airframe (Boeing 767-31K) None in force. ### Matched by engine (GE CF6-80C2B7F) - [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 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 2003-02-07](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 ### 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 ## 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 N1487A. ## FAA accident and incident reports None matched to N1487A. ## Service difficulty reports (243, 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 2026F00020](https://openairdocs.org/sdr/2026F00020), Mar 3, 2026: SKIN. CRACKED. EXTERIOR FUSELAGE SKIN ONLY IS CRACKED AT ONE FASTENER HOLE LOCATED L1 DOOR CUT OUT AFT CORNER STA 335 JUST ABOVE STR 20L(VERIFIED WITH HFEC).REPAIRED EXTERIOR - [SDR UIEA2024071900692](https://openairdocs.org/sdr/UIEA2024071900692), May 18, 2024: MODULE. FAULTED. AIR TURN BACK FOR SPOILER ADVISORY MESSAGE. UPON ARRIVAL, PERFORMED MULTIPLE OPS TEST IAW AMM 27-61-00, COULD NOT DUPLICATE. PERF FIM 31-51 FT 809. R/R PCA TAKE - [SDR UIEA2024072000707](https://openairdocs.org/sdr/UIEA2024072000707), May 18, 2024: CONTROL MODULE. FAULTED. SPOILER EICAS MESSAGE. PERFORMED FIM 27-09 FT 803 & FIM 27-09 FT 808, FOUND PCA FAULTING ON SCM #3 MSG. R & R #4 SPOILER PCA IAW AMM 27-61-02. DURING OPS CHECK - [SDR UIEA2024012500027](https://openairdocs.org/sdr/UIEA2024012500027), Jan 25, 2024: LIGHT. UNKNOWN. OVERHEAD EMERGENCY LIGHTS 1 PAX PANEL BACKLIGHT INOP,(

PERFORMED OPS CHECK ON OVERHEAD BACKLIGHTING IAW AMM 33-13-00. OPS CHECK GOOD AT THIS TIME.

) - [SDR UIEA2024012300021](https://openairdocs.org/sdr/UIEA2024012300021), Jan 23, 2024: TAT PROBE. FAULTED. EICAS MESSAG "TAT PROBE" FOLOWED BY 'AUTOPILOT DISCONNEC' LNAV AND VNAV BECAME INOP(

PERFORMED T/S PER FIM 30-33 FT805, SUSPECTING TAT, RELAY K514 AND RELAY K - [SDR UIEA2023122001008](https://openairdocs.org/sdr/UIEA2023122001008), Dec 19, 2023: ELT. UNKNOWN. CHORD ON ELT NEAR ENTRANCE DOOR UNRAVELED AND CARDBOARD SPLIT OPEN. SCOTCH TAPE HOLDING CARDBOARD TOGETHER(

REMOVED PORTABLE ELT FROM GALLEY AND INSTALLED SER - [SDR UIEA2023111100937](https://openairdocs.org/sdr/UIEA2023111100937), Nov 11, 2023: UNKNOWN. UNKNOWN. RH WING PANEL 651VB BROKEN AND PORTION MISSING FROM AIRCRAFT(

TIME-LIMITED REPAIR OF PANEL 651VB INSTALLED IAW EA 6757A0030 REV 0 DVI OF REPAIR AND SURROUNDIN - [SDR UIEA2023100900899](https://openairdocs.org/sdr/UIEA2023100900899), Oct 9, 2023: PCA. UNKNOWN. ON TAKEOFF OUT OF CVG AND MHT, THERE WAS A VIBRATION THAT FELT RAPID BUT SUBTLE PTCH OSCILLATION, ALL ENGINE GUAGES WERE NORMAL.(

R/R LH ELEVATOR CENTER PCA I - [SDR UIEA2023030300200](https://openairdocs.org/sdr/UIEA2023030300200), Mar 3, 2023: FLASHLIGHT ASSY. NONE. GALLEY FLASH LIGHT INOP(

R/R FLASHLIGHT IAW AMM 25-64-00. R/R FLASHLIGHT HOLDER/BRACKET IAW SRM 51-40-02. OPS CHECK NORMAL. DMI 181380 CLOSED

) - [SDR UIEA2023020200090](https://openairdocs.org/sdr/UIEA2023020200090), Feb 23, 2023: WIRE. NONE. AFT CARGO, DIAGONAL WALL RH SIDE, UNDER PANEL, SEVERAL ELECTRICAL WIRES BROKEN(

ELECTRICAL WIRES WERE REPLACED PER SWPM 20-10-13. OPS CHECK GOOD

) - [SDR UIEA2023021700133](https://openairdocs.org/sdr/UIEA2023021700133), Feb 23, 2023: NONE. NONE. LOWER HALF OF FUSELAGE, EXTERNAL SKIN WITH LIGHTNING STRIKE EVIDENCE ON STA 522 BETWEEN STG 19 AND 20RH.(

LOWER HALF OF FUSELAGE, EXTERNAL SKIN  ON STA 5 - [SDR UIEA2023021700134](https://openairdocs.org/sdr/UIEA2023021700134), Feb 23, 2023: NONE. NONE. LOWER FUSELAGE, EXTERNAL SKIN WITH LIGHTNING STRIKE BETWEEN STA 157 AND 164.7 AT STG 21RH (3EA)(

LOWER FUSELAGE, EXTERNAL SKIN BETWEEN STA 157 AND 164.7 AT ST - [SDR UIEA2023021700135](https://openairdocs.org/sdr/UIEA2023021700135), Feb 23, 2023: NONE. NONE. LOWER FUSELAGE, EXTERNAL SKIN WITH LIGHTNING STRIKE BETWEEN STA 172.5 AT 3.700" ABOVE STG 21RH(

LOWER FUSELAGE, EXTERNAL SKIN  BETWEEN STA 172.5 AT 3.700 - [SDR UIEA2023021700136](https://openairdocs.org/sdr/UIEA2023021700136), Feb 23, 2023: NONE. NONE. LOWER FUSELAGE, EXTERNAL SKIN WITH LIGHTNING STRIKE ON STA 287 AT 9.5" ABOVE STG 21RH.(

LOWER FULSELAGE, EXTERNAL SKIN ON STA 287 AT 9.5" ABOVE STG 21RH. LIGH - [SDR UIEA2023022100161](https://openairdocs.org/sdr/UIEA2023022100161), Feb 23, 2023: NONE. NONE. DELAMINATION ON INTERNAL / EXTERNAL AREA OF LH ACCESS PANELS FROM VERTICAL STABILIZER BETWEEN FSS 118.75 TO FSS 246.653 AND FRONT SPAR TO AUXILIARY SPAR.(

REP - [SDR UIEA2023022100162](https://openairdocs.org/sdr/UIEA2023022100162), Feb 23, 2023: NONE. NONE. DELAMINATION ON EXTERNAL AREA OF RH ACCESS PANELS FROM VERTICAL STABILIZER BETWEEN FSS 118.75 TO FSS 246.653 AND FRONT SPAR TO AUXILIARY SPAR.(

REPAIRED THE A - [SDR UIEA2022062100626](https://openairdocs.org/sdr/UIEA2022062100626), Jun 20, 2022: BOTTLE. LEAKING. SUSPECT PAX O2 BOTTLE LEAKING(REMOVED AND REPLACED PAX O2 BOTTLE AMM 12-15-08, NO LEAKS NOTED) - [SDR UIEA2022042000349](https://openairdocs.org/sdr/UIEA2022042000349), Apr 20, 2022: NONE. NONE. #2 OXYGEN BOTTLE PRESSURE REGULATOR LEAKING(

REMOVED AND REPLACED #2 OXYGEN PRESSURE REGULATOR IAW AMM 35-11-03. OPS AND LEAK CHECK GOOD AT THIS TIME.PLACED ITEM ON DMI 158497 IAW MEL 35-31-01.

/

LP 1617077 ITEM 5 - REMOVED AND REPLACED L1 PO - [SDR UIEA2021112902435](https://openairdocs.org/sdr/UIEA2021112902435), Nov 27, 2021: MASK. NONE. FIRST OFFICER MASK IS NOT FLOWING O2 PROPERLY. EXTREMELY HARD TO BREATH THROUGH NEEDS TO BE REPLACED.(

R&R FO O2 MASK IAW 35-11-51

) - [SDR UIEA2021111302413](https://openairdocs.org/sdr/UIEA2021111302413), Nov 13, 2021: NONE. NONE. STATUS MSG L ENG EEC C1(

TRANSFERRED TO MDDR 156734 IAW DDG 73-21-01-05 CAT A DUE DATE 20DEC21

) - [SDR UIEA2021111202407](https://openairdocs.org/sdr/UIEA2021111202407), Nov 13, 2021: DIODE. NONE. R ENG OIL PRESS LIGHT INOP(

TRANSFERRED TO MDDR 156702 PER MEL 79-33-01-01 CAT C. DUE DATE 23NOV21

/

14NOV21 - LOG PAGE 1373448 - ITEM #4 - SCK - : REM - [SDR UIEA2021111302408](https://openairdocs.org/sdr/UIEA2021111302408), Nov 13, 2021: NONE. NONE. L ENG BLEED EICAS CAME ON 5 TIMES ON/OFF APPROACH TO LANDING(

PERFORMED BITE CHECK OF AIR SUPPLY. NO FAULTS AT THIS TIME IAW AMM 36-23-00.

) - [SDR UIEA2021111102394](https://openairdocs.org/sdr/UIEA2021111102394), Nov 10, 2021: FIRE LOOP. MALFUNCTIONED. L ENG FIRE LP 1 INTERMITTENTLY APPEARING ON STATUS PAGE. PERFORMED FIM 26-11 P/T 804 UP TO BLOCK 52. ALL RESISTANCE CHECKS WITHIN LIMITS PER TABLE A. UPON DOING - [SDR UIEA2021102402278](https://openairdocs.org/sdr/UIEA2021102402278), Oct 23, 2021: NONE. NONE. L ENG EEC C1 STATUS(

PERFORMED UP TO STEP 4 OF FIM 73-21 FAULT TREE 885. UNABLE TO PERFORM REST OF THE FIM. TRANSFERRED TO MDDR # 155587 PER DDG MEL # 73-21-0 - [SDR UIEA2021102402277](https://openairdocs.org/sdr/UIEA2021102402277), Oct 23, 2021: NONE. NONE. LEFT WEATHER RADAR FAILED WXR FAIL MSG ON EICAS(

PERFORMED WEATHER RADAR SYSTEM OPERATIONAL TEST IAW B767 AMM 34-43-00 715-026-002. OPS CKS NORMAL AT THIS TIM - [SDR UIEA2021100802208](https://openairdocs.org/sdr/UIEA2021100802208), Oct 8, 2021: FIRE DETECTOR. INTERMITTENT. INTERMITTENT LENG FIRE LOOP 1 STATUS MSG. REMOVED AND REPLACED L/H ENGINE UPPER AFT FIRE LOOP DETECTOR ELEMENT IAW AMM 26-11-02. OPS CHECK GOOD AT THIS TIME, - [SDR UIEA2021101102215](https://openairdocs.org/sdr/UIEA2021101102215), Oct 7, 2021: NONE. NONE. STATUS MESSAGE "L ENG EEC C1"(

MSG CLEARED IAW AMM 72-00-00. OPS CKD IAW 72-10-00.

) - [SDR UIEA2021100402180](https://openairdocs.org/sdr/UIEA2021100402180), Oct 2, 2021: NONE. NONE. AFT CABIN TEMP ADVISORY MSG DISPLAYED IN FLIGHT.(

PERFORMED BITE ON ZONE TEMP CONTROLLER REF FIM 21-61 FT 803, NO FAULTS PRESENT AT THIS TIME.

) - [SDR UIEA2021100202162](https://openairdocs.org/sdr/UIEA2021100202162), Oct 2, 2021: CONTROLLER. FAULT MESSAGE. AFT CABIN TEMP CAUTION MSG IN FLIGHT @FL390 CABIN ALT 7000 CABIN DIFFERENTIAL PRESS 8.4 PSI. T/S IAW FIM 21-61 FAULT TREE 803 AND AMM 21-61-03. REMOVED AND REPL - [SDR UIEA2021100102158](https://openairdocs.org/sdr/UIEA2021100102158), Sep 30, 2021: CONTROL PANEL. WARNING MESSAGE. "AFT CABIN TEMP" EICAS MESSAGE OBSERVED IN FLIGHT.(

PERF BITE OF ZONE CONTROL PANEL IAW AMM 21-61-03. NO CURRENT FAULTS NOTED. REF OPS CHECK OF AFT CABIN TEMP - [SDR UIEA2021093002148](https://openairdocs.org/sdr/UIEA2021093002148), Sep 30, 2021: CONTROLLER. FALSE INDICATION. DURING CRUISE, AFT CABIN TEMP MESSAGE PERFORMED BITE CHECK OF ZONE TEMP CONTROLLER IAW FIM 21-61 FT 803. NO DEFECTS NOTED. A/C OK FOR SERVICE. - [SDR UIEA2021092902142](https://openairdocs.org/sdr/UIEA2021092902142), Sep 29, 2021: CONTROLLER. ERRATIC. AFT CABIN TEMP EICAS MSG ABOUT 3 HOURS IN CRUISE. RAN QRH TEMP IN ZONE DROPPED A COUPLE OF DEGREES TO 21C. PERFORMED BITE TEST OF THE ZONE TEMP CONTROLLER IAW B - [SDR UIEA2021092002062](https://openairdocs.org/sdr/UIEA2021092002062), Sep 20, 2021: RADAR. INTERMITTENT. RADAR WILL NOT MAINTAIN TILT/STABLE IN AUTO MODE.(

TRANSFERED TO MDDR# 153823 MEL 34-43-01-02 CAT C.

/

20 SEP 21 - LP 1287025 ITEM 8 - AFW - OPS CHECK - [SDR UIEA2021092002060](https://openairdocs.org/sdr/UIEA2021092002060), Sep 19, 2021: AUTOTHROTTLE SYS. FALSE INDICATION. AUTO THROTTLE DISCONNECT EICAS MSG DURING CLIMB 10,000 FT FROM INTERMEDIATE LEVEL.OFF AT 290 AFTER PRESSING ALT BUTTON TO CONTINUE CLIMB VNAV TO 350.SELECTED FL - [SDR UIEA2021090801989](https://openairdocs.org/sdr/UIEA2021090801989), Sep 17, 2021: DOOR SEAL. CORRODED. BULK CARGO DOOR CUT-OUT, UPPER SEAL HAS SEVERAL AREAS OF CORROSION.(

UPON FURTHER EVAL CORROSION FOUND TO BE OUT OF LIMITS IAW B767 53-00-15-1A-1. REMOVED AND - [SDR UIEA2021091302014](https://openairdocs.org/sdr/UIEA2021091302014), Sep 17, 2021: SKIN. CRACKED. CRACK NOTED ON RH WING LOWER SURFACE STR L-6.5 MOST I/B FASTENER AT 6 O'CLOCK POSITION LOOKING UP/FWD. APPROX 1/4" LONG.(

REPAIRED CRACK AT RH WING LOWER SURF - [SDR UIEA2021091302015](https://openairdocs.org/sdr/UIEA2021091302015), Sep 17, 2021: SKIN. CRACKED. WHILE PERFORMING HFEC INSP ON PART 1-2 OF ORIGINATING TASK CARD. VISUALLY NOTED A CRACK AND CONFIRMED WITH HFEC ON THE RH WING LOWER SURFACE STR L-9.5, 22ND FAS - [SDR UIEA2021082401868](https://openairdocs.org/sdr/UIEA2021082401868), Aug 23, 2021: SENSOR. FAILED. AFT CABIN TEMP EICAS MESSAGE.(

ITEM TRANSFERRED TO DMI 152434 PER MEL 21-61-01-02. CAT C. DUE 03SEP21. PERFORMED ZONE TEMP BITE IAW FIM 21-61-00. FOUND AFT ZO - [SDR UIEA2021082301848](https://openairdocs.org/sdr/UIEA2021082301848), Aug 22, 2021: CONTROLLER. FAULTED. AFT CABIN TEMP EICAS DURING CRUISE. FOLLOWED NON NORMAL CK LIST(

PERF BITE ON ZONE TEMP CONTROLLER.IAW AMM 21-61-00. RESET CONTROLLER. MSG AND FAULT CLEARED. - [SDR UIEA2021082301850](https://openairdocs.org/sdr/UIEA2021082301850), Aug 20, 2021: WARNING MESSAGE. FALSE ACTIVATION. STATUS MSG R ENG PRV(

C/W FIM 36-10- FAULT TREE 847, OPS CHECK NORMAL.

) - [SDR UIEA2021081701818](https://openairdocs.org/sdr/UIEA2021081701818), Aug 17, 2021: TRANSCEIVER. FAULTED. R "WX SYS FAIL" AND "WXR SYS" STATUS MSG.(

TRANSFERRED TO DMI 152042 IAW MEL 34-43-01, CAT D.

/

REMOVED AND REPLACED RIGHT WEATHER RADAR TRANSCEIVER IA - [SDR UIEA2021081701817](https://openairdocs.org/sdr/UIEA2021081701817), Aug 16, 2021: APU. FAULTED. AFTER LANDING APU WOULD NOT START (3 ATTEMPTS MADE)(

APU GRND STARTED BY MAINT W/ NO FAULTS NOTED. BITE AND SELF TEST PER AMM 49-61-05. NO FAULTS NOTED.

) - [SDR UIEA2021081601809](https://openairdocs.org/sdr/UIEA2021081601809), Aug 14, 2021: APU. UNKNOWN. APU FAILED TO START ON GND(

PERFORMED BITE AND SELF TEST OF ECU IAW AMM 49-61-05.&NBSP; NO FAULTS FOUND.&NBSP; APU START 1ST ATTEMPT.&NBSP; OPS CHECK NORMAL.< - [SDR UIEA2021081301789](https://openairdocs.org/sdr/UIEA2021081301789), Aug 13, 2021: CHARGER. FAILED. APU FAILED TO START AFTER LANDING 3 ATTEMPTS(

T/S PER FIM 49-11 F/T 987, FOUND FAULT CODE 34 ON ALL LEGS. FOUND APU BATTERY CHARGER TO BE AT FAULT. REMOVED AN - [SDR UIEA2021081201772](https://openairdocs.org/sdr/UIEA2021081201772), Aug 12, 2021: WARNING MESSAGE. FALSE ACTIVATION. R ENG PRV STATUS MSG DISPLAY AFTER ENGINE START(

PERFORMED FIM 36-20-00/101 AIR SUPPLY BITE. NO FAULTS NOTED AT THIS TIME. MSG CLEARED. OK FOR SERVICE.

) - [SDR UIEA2021081201774](https://openairdocs.org/sdr/UIEA2021081201774), Aug 12, 2021: WARNING LIGHT. FALSE ACTIVATION. APU FAULT EICAS MSG DISPLAYED DURING ATTEMPTED APU START AFTER LANDING, QRH COMPLETED. FAULT LIGHT DOES NOT REMAIN DISPLAYED WITH APU SWITCH OFF.(

PERFO - [SDR UIEA2021081321768](https://openairdocs.org/sdr/UIEA2021081321768), Aug 10, 2021: ECU. DIRTY. APU FAULT ON TAXI IN(

PERFORMED APU BITE IAW AMM 49-61-05. CLEARED ECU. APU START NORMAL ON 1ST ATTEMPT. OK FOR SERVICE

) - [SDR UIEA2021080651711](https://openairdocs.org/sdr/UIEA2021080651711), Aug 4, 2021: OIL SYSTEM. LOW. APU FAULT AFTER LANDING(

PERFORMED ECU BITE IAW FIM TASK 49-11 FT 987. START ABORTED FAULT, FOUND APU OIL LOW, SERVICED APU OIL TO FULL IAW AMM 12-13-04, PERF - [SDR UIEA2021072601630](https://openairdocs.org/sdr/UIEA2021072601630), Jul 25, 2021: LINE. LEAKING. FOUND PUDDLE OF OIL IN RIGHT ENGINE COWL AND OIL DRIPPING FROM ENGINE(

FOUND&NBSP; ENGINE HYDRALIC LEAK,TIGHT AND TORQUE HYD LINE FROM PYLON TO ENG IAW AMM 71 All 243: https://openairdocs.org/aircraft/N1487A/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 CF6-80C2B7F) - [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. Lists CF6-80C2 Series - [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 N1487A The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N1487A before. - [Cancelled 2011-03-28](https://openairdocs.org/deregistered/N1487A-2011-03-28): Piper PA-22, S/N 22-396, built 1952. Sale reported, pending cancellation. Owner: [Oklahoma City, OK](https://openairdocs.org/faa-place/OK/Oklahoma%20City) ## Related - Other Boeing 767-31K aircraft: https://openairdocs.org/model/boeing-767-31k/aircraft.md - The GE CF6-80C2B7F engine: https://openairdocs.org/engine/ge-cf6-80c2b7f.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.