# N1327A: 1996 Boeing 767-37D - Status: Valid registration - Airframe: [Boeing 767-37D](https://openairdocs.org/model/boeing-767-37d) (registry code 13852D5, 375 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: 26328 - Year built: 1996 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: September 15, 2017 - Certificate issued: October 17, 2017 - Expires: October 31, 2027 - Mode S code: A085ED - Registered owner: [Msn 26328 LLC](https://openairdocs.org/faa-owner/MSN%2026328%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=1327A - Page: https://openairdocs.org/aircraft/N1327A 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 767-37D) 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 N1327A. ## FAA accident and incident reports None matched to N1327A. ## Service difficulty reports (327, 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 ABXA20260921415](https://openairdocs.org/sdr/ABXA20260921415), Sep 21, 2026: IDG. FAULTED. DURING ENGINE START AND TAXI, L ENG GEN DRIVE & DISC. CREW RETURNED TO THE GATE (BTB). MTC DEFERRED LT ENGINE IDG IAW MEL 24-00-1-1. MBCB 09/24/26. REF ITEM 2, - [SDR ABXA20260816363](https://openairdocs.org/sdr/ABXA20260816363), Aug 16, 2026: SENSE LINE. LOOSE. DURING TAXI RT ENG BLEED OFF AND RT PACK OFF EICAS MESSAGE APPEARED A/C RETURNED TO GATE(BTB) AND MTX GROUNDED ACFT AND FOUND PRVC SENSE LINE LOOSE, RESECURED L - [SDR ABXA20260814361](https://openairdocs.org/sdr/ABXA20260814361), Aug 14, 2026: START VALVE. MALFUNCTIONED. DURING TAXI OUT ATTEMPTED TO START NR 1 ENGINE, N2 ADVANCED TO 26% BUT VALVE LIGHT ON L STAYED ILLUMINATED ATTEMPTED 2ND TIME, SAME ISSUE, ACFT RETURNED TO GATE - [SDR ABXA20260808356](https://openairdocs.org/sdr/ABXA20260808356), Aug 8, 2026: A/C PACK. INOPERATIVE. DURING ENGINE START, L PACK INOP. CREW RETURNED TO THE GATE (BTB). MTC RESET L PACK PNUEMATIC SYS IAW AMM 21-00-00 NO DEFECTS NOTED AT THIS TIME L PACK OPERATIO - [SDR ABXA20260718325](https://openairdocs.org/sdr/ABXA20260718325), Jul 18, 2026: ELEC CONNECTOR. DAMAGED. ACFT REJECTED TAKE OFF DUE TO CARGO MAIN CARGO DOOR INDICATION A/C RETURNED TO GATE AND MTX GROUNDED A/C MTX T/S MAIN CARGO DOOR LIFT SYSTEM RECONNECT CANNON PL - [SDR ABXA20260714319](https://openairdocs.org/sdr/ABXA20260714319), Jul 14, 2026: STARTER. INOPERATIVE. DURING TAXI OUT WHILE STARTING RH ENGINE, RH STARTER WAS INOP. A/C RETURNED TO THE GATE (BTB) AND MX GROUNDED A/C. MTX EXERCISED RH START VALVE AND PERFORMED OP - [SDR ABXA20260611254](https://openairdocs.org/sdr/ABXA20260611254), Jun 11, 2026: CONTROLLER. DEFECTIVE. DURING TAXI, CREW RECEIVED R ENG BLEED OFF R PACK OFF NO R DUCT PRESSURE. CREW RETURNED TO THE GATE (BTB). MTX TROUBLE SHOT AND REMOVED AND REPLACED PRV CONTROL - [SDR ABXA20260516212](https://openairdocs.org/sdr/ABXA20260516212), May 16, 2026: HINGE ARM. FAILED. DURING CREW PREFLIGHT, LEFT UPPER STORAGE BIN DOOR HINGE ARM FAILED. DEFERRED LEFT OVERHEAD STORAGE BIN SHOCK BIN SHOCK STRUT IAW ABX MEL 25-28-1A. DUE TO OVERH - [SDR ABXA20260429182](https://openairdocs.org/sdr/ABXA20260429182), Apr 29, 2026: FLAP SYSTEM. FAULTED. DURING DESCENT, LE SLAT DISAGREE LIGHT ILLUMINATED AFTER SELECTING FLAPS 25. CREW EXECUTED A MISSED APPROACH. FOLLOWED QRH PROCEDURES AND LANDED WITH FLAPS 20. - [SDR ABXA202604264173](https://openairdocs.org/sdr/ABXA202604264173), Apr 24, 2026: START VALVE. FAULTED. DURING TAXI OUT WHILE STARTING NR 1 ENGINE NO ROTATION ON NR 1, START VALVE STAYED OPEN , A/C RETURNED TO THE GATE (BTB) AND MTX GROUNDED A/C AND DEFERRED NR 1 - [SDR ABXA20260423171](https://openairdocs.org/sdr/ABXA20260423171), Apr 23, 2026: FLAP SYSTEM. WARNING MESSAGE. DURING TAXI, TE FLAP DISAGREE WHEN MOVING TO FLAPS 5 ON THE AFTER START CHECKLIST. CREW RETURNED TO BLOCK (BTB). MTC PERFORMED FIM 27-51 FT 811, RESET BY PASS L - [SDR ABXA20260331142](https://openairdocs.org/sdr/ABXA20260331142), Mar 31, 2026: ELEC CONNECTOR. FAULTED. PILOT REPORTED CARGO FIRE A 4 AMBER INDICATION. RESET ELECTRICAL CONNECTOR. ON BOX. ERROR CLEARED. OPS CHK GOOD. IAW B767 AMM 26-16-00. THIS CLEARS THE DI. PLAC - [SDR ABXA20260313107](https://openairdocs.org/sdr/ABXA20260313107), Mar 13, 2026: WARNING MESSAGE. FALSE ACTIVATION. DURING APPROACH INTO MIA, LANDING CONFIG WARNING LIGHT ILLUMINATED AT 3000 FT AGL. FLAPS WERE AT 15 AND GEAR LEVER IN OFF POSITION. CAPTAIN DID A GO AROUND AND - [SDR ABXA20260206052](https://openairdocs.org/sdr/ABXA20260206052), Feb 6, 2026: A/C PACK. INOPERATIVE. DURING TAXI OUT AND AFTER START CHECKLIST, L PACK OFF EICAS DISPLAYED QRH PROCEDURE UNSUCCESSFUL. AIRCRAFT RETURNED TO BLOCKS (BTB). TRANSFERED LH PACK TO DI IA - [SDR ABXA20260116013](https://openairdocs.org/sdr/ABXA20260116013), Jan 16, 2026: FIRE LOOP. FALSE INDICATION. DURING MAINTENANCE INSPECTION, LT ENG OH LP1 EICAS MSG. PLACED ENG OH LP 1 ON DEFERRAL IAW MEL 26-11-2-1 MBCB 01/26/2026 AIRCRAFT ETOPS 120 PLACARD ROTATED. AIR - [SDR ABXA20251216342](https://openairdocs.org/sdr/ABXA20251216342), Dec 16, 2025: SMOKE DETECTOR. DEFECTIVE. DURING MAINTENANCE INSPECTION, EICAS MSG AFT CARGO DET NR 1 ILLUMINATED. DEFERRED PER MEL 26-16-1-1-1. REMOVED AND REPLACED AFT CARGO SMOKE DETECTOR NR 1 PER AM - [SDR ABXA20250823195](https://openairdocs.org/sdr/ABXA20250823195), Aug 23, 2025: SUPPORT FITTING. CORRODED. DURING THE C-6 MAINTENANCE VISIT AT HAECO GSO, CORROSION WAS FOUND ON THE LH HORIZONTAL STABILIZER LOWER BLADE SEAL SUPPORT FITTINGS. #2 FITTINGS TOTAL WERE FOU - [SDR ABXA20250823194](https://openairdocs.org/sdr/ABXA20250823194), Aug 23, 2025: SUPPORT FITTING. CORRODED. DURING THE C-6 MAINTENANCE VISIT AT HAECO GSO, CORROSION WAS FOUND ON THE LH HORIZONTAL STABILIZER LOWER BLADE SEAL SUPPORT FITTINGS. #3 FITTINGS TOTAL WERE FOU - [SDR ABXA20250823193](https://openairdocs.org/sdr/ABXA20250823193), Aug 23, 2025: SUPPORT FITTING. CORRODED. DURING THE C-6 MAINTENANCE VISIT AT HAECO GSO, CORROSION WAS FOUND ON THE LH HORIZONTAL STABILIZER LOWER BLADE SEAL SUPPORT FITTINGS. #4 FITTINGS TOTAL WERE FOU - [SDR ABXA20250823192](https://openairdocs.org/sdr/ABXA20250823192), Aug 23, 2025: SUPPORT FITTING. CORRODED. DURING THE C-6 MAINTENANCE VISIT AT HAECO GSO, CORROSION WAS FOUND ON THE LH HORIZONTAL STABILIZER LOWER BLADE SEAL SUPPORT FITTINGS. #5 FITTINGS TOTAL WERE FOU - [SDR ABXA20250823191](https://openairdocs.org/sdr/ABXA20250823191), Aug 23, 2025: SUPPORT FITTING. CORRODED. DURING THE C-6 MAINTENANCE VISIT AT HAECO GSO, CORROSION WAS FOUND ON THE LH HORIZONTAL STABILIZER LOWER BLADE SEAL SUPPORT FITTINGS.# 6 FITTINGS TOTAL WERE FOU - [SDR ABXA20250823190](https://openairdocs.org/sdr/ABXA20250823190), Aug 23, 2025: SUPPORT FITTING. CORRODED. DURING THE C-6 MAINT VISIT, CORROSION FOUND ON LT HORIZONTAL STAB LOWER BLADE SEAL SUPPORT FITTINGS. NR 7 FITTINGS TOTAL WERE FOUND TO HAVE CORROSION BETWEEN TH - [SDR ABXA20250823189](https://openairdocs.org/sdr/ABXA20250823189), Aug 23, 2025: SKIN. DAMAGED. DURING THE CURRENT C-6 HEAVY MAINTENANCE CHK, MAINT FOUND AT BS 871.5, RT FWD OVERWING EMERG EXIT DOOR HAD NICK DAMAGE ABOVE WINDOW-PLUG CUTOUT. FASTENERS REMOV - [SDR ABXA20250823188](https://openairdocs.org/sdr/ABXA20250823188), Aug 23, 2025: PANEL. DAMAGED. DURING THE C-6 MAINTENANCE CHECK, THE NR 2 ENGINE PYLON PANEL ASSEMBLY WAS FOUND TO BE DAMAGED BEYOND REPAIR. MAINTENANCE FABRICATED A NEW PANEL. ACCORDING TO B - [SDR ABXA20250823187](https://openairdocs.org/sdr/ABXA20250823187), Aug 23, 2025: DOOR FRAME. CORRODED. DURING C6 CHECK AT HACECO INSPECTION FOUND E&E DOOR CUTOUT FWD FRAME WEB STA303 HAS PUNCTURE REMOVED ANGLE SUPPORT RAIL IAW B767 SRM 51-40-02, REMOVED DAMAGE IA - [SDR ABXA20250410074](https://openairdocs.org/sdr/ABXA20250410074), Apr 11, 2025: TCAS SYSTEM. FAULTED. DURING PUSHBACK GOT TCAS EICAS MSG. A/C RETURNED TO GATE (BTB) AND MTX GROUNDED A/C, MTX DEFERRED TCAS FOR DEPARTURE IAW MEL ABX-34-45-1A. AND RETURNED A/C TO S - [SDR ABX2025F00001](https://openairdocs.org/sdr/ABX2025F00001), Apr 6, 2025: AUTOTHROTTLE SYS. WARNING MESSAGE. ON TAXI OUT, AUTO THROTTLE DISC LIGHT & AUTO THROTTLE DISC EICAS MESSAGE ILLUMINATED. A/C RETURNED TO BLOCKS (BTB). DEFERRED AUTO THROTTLE IAW MEL ABX-22-30-1. - [SDR ABXA20241012187](https://openairdocs.org/sdr/ABXA20241012187), Oct 12, 2024: ISOLATION VALVE. FAULTED. DURING TAXI R ISLN VALVE LIGHT ON, NO AIR FOR START AC RETURNED TO GATE AND MAITENANCE GROUNDED AC. MTX CYCLED RIGHT ISOLATION VALVE 3 TIMES SUCCESSFULLY PER AM - [SDR ABXA20240919177](https://openairdocs.org/sdr/ABXA20240919177), Sep 19, 2024: PRESSURE SWITCH. FAULTED. AT ROTATION ON TAKEOFF EICAS MSG C HYD SYS PRESS APPEARED AND AC PERFORMED ATB , AND AFTER LANDING MTX GROUNDED AC AND TROUBLE SHOT TO A CTR HYD PRESSURE SWITCH - [SDR UIEA2024031700155](https://openairdocs.org/sdr/UIEA2024031700155), Mar 18, 2024: TAPE. DAMAGED. COCKPIT ELT TAPE DAMAGED. PER MCC REGISTERED WITH NOAA PER ENGINEERING DEPARTMENT IAW AMM 25-63-03. DMI 204893 CLOSED. - [SDR UIEA2024031700154](https://openairdocs.org/sdr/UIEA2024031700154), Mar 17, 2024: ELT. UNKNOWN. CAPT REPORTED GALLEY ELT NOT TAPED CORRECTLY(

R/R GALLEY PORTABLE ELT IAW AMM 25-63-03 PART EFECTIVITY AIPC 25-63-52-97 ITEM 600. NO FURTHER DEFECTS NOTED. TH - [SDR UIEA2024031800156](https://openairdocs.org/sdr/UIEA2024031800156), Mar 17, 2024: SIGN. DETACHED. OBSERVED L1 EMERGENCY EXIT SIGN TO BE DISPLACED(

RE-SECURED EMERGENCY EXIT SIGN / LIGHT PER AMM 33-51-01. OPS CHCKS GOOD AT THIS TIME. 

) - [SDR UIEA2024010500006](https://openairdocs.org/sdr/UIEA2024010500006), Jan 5, 2024: GUARD. UNKNOWN. EMER LIGTHS GUARD SWITCH DOES NOT STAY CLOSED OR SNAPS CLOSED(

REMOVED AND REPLACED EMERGENCY LIGHTS GUARD PER AMM 20-11-00 AND 33-51-00-08-01B. OPS CHECKS GO - [SDR UIEA2023122101009](https://openairdocs.org/sdr/UIEA2023122101009), Dec 19, 2023: FIRST AID KIT. UNKNOWN. FOUND RED TAG MISSING ON FIRST AID KIT(

REMOVED AND REPLACED FIRST AID KIT IAW AMM 25-64-03. NO FURTHER DEFECTS NOTED

) - [SDR UIEA2023100500863](https://openairdocs.org/sdr/UIEA2023100500863), Oct 11, 2023: UNKNOWN. UNKNOWN. DELAMINATION ON PREVIOUS REPAIR AT RUD STA 106.142 RUDDER TRAILING EDGE RH.(

RUDDER TRAILING EDGE RH AT RUD STA 106.142 WAS REPAIRED IAW SRM 55-40-01-2R-1 FIG - [SDR UIEA2023100500864](https://openairdocs.org/sdr/UIEA2023100500864), Oct 11, 2023: UNKNOWN. UNKNOWN. LIGHTNING STRIKE ON FASTENER HEAD AT STA 212.5 AND BELOW RBL 15, UPPER HALF FUSELAGE EXTERIOR.(

LIGHTNING STRIKE ON FASTENER HEAD AT STA 212.5 AND BELOW RBL 1 - [SDR UIEA2023100500865](https://openairdocs.org/sdr/UIEA2023100500865), Oct 11, 2023: UNKNOWN. UNKNOWN. LIGHTNING STRIKE ON FASTENER HEAD AT STA 287 AND 3" BELOW STGR 3 OF UPPER HALF OF FUSELAGE EXTERIOR.(

LIGHTNING STRIKE ON FASTENER HEAD AT STA 287 AND 3" BELO - [SDR UIEA2023100500866](https://openairdocs.org/sdr/UIEA2023100500866), Oct 11, 2023: PCA. UNKNOWN. OUT OF LIMITS FREE PLAY ON OUTBOARD PCA OF RH ELEVATOR.(

OUTBOARD PCA OF RH ELEVATOR WAS REPLACED, ADJUSTED AND LEAK CHECK WAS SATISFACTORY IAW AMM 27-31-05-4 - [SDR UIEA2023100500867](https://openairdocs.org/sdr/UIEA2023100500867), Oct 11, 2023: PCA. UNKNOWN. OUT OF LIMITS FREE PLAY ON OUTBOARD PCA OF LH ELEVATOR.(

N/R: 00028. OUTBOARD PCA OF LH ELEVATOR. WAS REPLACED, ADJUSTED AND TIGHTENED IAW AMM 27-31-05-424-02 - [SDR UIEA2023100500868](https://openairdocs.org/sdr/UIEA2023100500868), Oct 11, 2023: PCA. UNKNOWN. OUT OF LIMITS FREE PLAY ON MIDDLE PCA OF LH ELEVATOR.(

MIDDLE PCA OF LH ELEVATOR WAS REPLACED, ADJUSTED AND TIGHTENED IAW AMM 27-31-05-424-027 & 27-31-00- - [SDR UIEA2023100500869](https://openairdocs.org/sdr/UIEA2023100500869), Oct 11, 2023: HOSE. UNKNOWN. FUSELAGE SECTION 43, AREA ABOVE CEILING AT STA 544, SMOKE DETECTOR SYSTEM, ORANGE HOSE BROKEN (1EA)(

FUSELAGE SECTION 43, AREA ABOVE CEILING AT STA 544, SMOKE - [SDR UIEA2023100500870](https://openairdocs.org/sdr/UIEA2023100500870), Oct 11, 2023: O-RING. UNKNOWN. RH WING OVERWING PORT FUEL LEAK(

RH WING OVERWING PORT O-RINGS WERE REPLACED IAW AMM TASK 28-11-04-404-019 REV 140 DATE 22 AUG 23. LEAK TEST WAS PERFORMED, NO - [SDR UIEA2023100500871](https://openairdocs.org/sdr/UIEA2023100500871), Oct 11, 2023: HOSE. UNKNOWN. FUSELAGE SECTION 43, AREA ABOVE CEILING AT STA 610, SMOKE DETECTOR SYSTEM, ORANGE HOSE BROKEN (1EA)(

FUSELAGE SECTION 43, AREA ABOVE CEILING AT STA 610, SMOKE - [SDR UIEA2023100500872](https://openairdocs.org/sdr/UIEA2023100500872), Oct 11, 2023: HOSE. UNKNOWN. FUSELAGE SECTION 43, AREA ABOVE CEILING BTW STA 654+66 AND STA 654+88, SMOKE DETECTOR SYSTEM, ORANGE HOSE BROKEN (1EA)(

FUSELAGE SECTION 43, AREA ABOVE CEILIN - [SDR UIEA2023100500873](https://openairdocs.org/sdr/UIEA2023100500873), Oct 11, 2023: HOSE. UNKNOWN. FUSELAGE SECTION 46, AREA ABOVE CEILING BTW STA 1307 AND STA 1329, SMOKE DETECTOR SYSTEM, ORANGE HOSE BROKEN (1EA)(

FUSELAGE SECTION 46, AREA ABOVE CEILING BT - [SDR UIEA2023100500874](https://openairdocs.org/sdr/UIEA2023100500874), Oct 11, 2023: HOSE. UNKNOWN. FUSELAGE SECTION 46, AREA ABOVE CEILING BTW STA 1461 AND STA 1480, SMOKE DETECTOR SYSTEM, ORANGE HOSE BROKEN (1EA)(

FUSELAGE SECTION 46, AREA ABOVE CEILING BT - [SDR UIEA2023100500875](https://openairdocs.org/sdr/UIEA2023100500875), Oct 11, 2023: HOSE. UNKNOWN. FUSELAGE SECTION 46, AREA ABOVE CEILING AT STA 1395, SMOKE DETECTOR SYSTEM, ORANGE HOSE BROKEN (1EA)(

FUSELAGE SECTION 46, AREA ABOVE CEILING AT STA 1395, SMO - [SDR UIEA2023100500876](https://openairdocs.org/sdr/UIEA2023100500876), Oct 11, 2023: COMPUTER. UNKNOWN. STABILIZER TORSION BOX. INTERNAL STRUCTURE, ELEVATOR FUEL COMPUTER BETWEEN STA 1702 AND STA 1725.5. WITH SEVERAL LINES WITH HYD LEAK.(

ELEVATOR FEEL COMPUTER - [SDR UIEA2023100500877](https://openairdocs.org/sdr/UIEA2023100500877), Oct 11, 2023: ACTUATOR. UNKNOWN. STABILIZER TORSION BOX. INTERNAL STRUCTURE BETWEEN STA 1809.5 AND STA 1832, FEEL ACTUATOR WITH EVIDENCE LEAK.(

THE FEEL ACTUATOR WAS REPLACED, WAS TIGHTENED A - [SDR UIEA2023100600878](https://openairdocs.org/sdr/UIEA2023100600878), Oct 11, 2023: UNKNOWN. UNKNOWN. FUEL LEAK ON REAR SPAR SPLICE FITTING AND BBR 97.42 AT CENTER TANK.(

FUEL LEAK ON REAR SPAR SPLICE FITTING AND BBR 97.42 AT CENTER TANK WAS REPAIRED AND THE T All 327: https://openairdocs.org/aircraft/N1327A/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 ## Related - Other Boeing 767-37D aircraft: https://openairdocs.org/model/boeing-767-37d/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.