# N1093A: 1999 Boeing 767-36N - Status: Valid registration - Airframe: [Boeing 767-36N](https://openairdocs.org/model/boeing-767-36n) (registry code 1385152, 290 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: 30111 - Year built: 1999 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: March 1, 2017 - Certificate issued: April 20, 2023 - Expires: April 30, 2030 - Mode S code: A028E5 - Registered owner: [Andromeda Leasing II LLC](https://openairdocs.org/faa-owner/ANDROMEDA%20LEASING%20II%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=1093A - Page: https://openairdocs.org/aircraft/N1093A 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 767-36N) 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 N1093A. ## FAA accident and incident reports None matched to N1093A. ## Service difficulty reports (308, 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 ABXA20261019473](https://openairdocs.org/sdr/ABXA20261019473), Oct 19, 2026: ENGINE. VIBRATION. IN THE CLIMB OUT RIGHT ENGINE VIB INCREASE TO 3.8 AT LEVEL OFF AT FL380 DECREASED BACK TO .6 A/ RETURNED TO FIELD (ATB) AND LANDED MTX GROUNDED A/C AND PERFORME - [SDR ABXA20260923432](https://openairdocs.org/sdr/ABXA20260923432), Sep 23, 2026: BEACON. INOPERATIVE. LOWER BEACON INOP A/C RETURNED TO GATE(BTB) AND MTX DEFERRED LOWER BEACON FOR DEPARTURE IAW MEL ABX-33-44-1-1A. A/C RETURNED TO SERVICE. - [SDR ABXA20260824373](https://openairdocs.org/sdr/ABXA20260824373), Aug 24, 2026: PUMP. LOW PRESSURE. DURING TAXI, LT FWD FUEL PUMP LOW PRESSURE LIGHT. ACFT RETURNED TO THE GATE (BTB). MTC DEFERRED PER MEL 28-22-1 DEACTIVATED LT FWD FUEL PUMP IAW MPM 28-22-1, PL - [SDR ABXA20260302081](https://openairdocs.org/sdr/ABXA20260302081), Mar 2, 2026: MODULE. FAULTED. C HYD PRIM 1 EICAS MESSAGE DURING PUSHBACK AND AC RETURNED TO GATE (BTB), MTX GROUNDED AC AND BEGAN TROUBLESHOOTING. PERFORMED T/S IAW FIM 29-11 FT 810. FOUND T - [SDR ABXA20260115012](https://openairdocs.org/sdr/ABXA20260115012), Jan 15, 2026: CONTROLLER. DEFECTIVE. DURING TAXIT OUT, EICAS MSG LT ENG CONTROL APPEARED AFTER TWO ENGINE STARTS. AIRCRAFT RETURNED TO BLOCKS. (BTB). REMOVED AND REPLACED LEFT ENG EEC IAW B767 AMM - [SDR ABXA20251228361](https://openairdocs.org/sdr/ABXA20251228361), Dec 28, 2025: WARNING MESSAGE. ILLUMINATED. WHEN ADVANCING THRUST LEVERS FOR TAKEOFF, "RIGHT PACK TEMP" EICAS MESSAGE APPEARED. A/C ABORTED TAKE-OFF (ATO) AND RETURNED TO GATE (BTB). MTX GROUNDED A/C, MTX - [SDR ABXA20251214340](https://openairdocs.org/sdr/ABXA20251214340), Dec 14, 2025: START VALVE. FAULTED. ON TAXI OUT, LEFT ENGINE START VALVE DISCREET LIGHT ON. AIRCRAFT RETURNED TO BLOCKS (BTB). MAINTENANCE ACTUATED START VALVE IAW B767 AMM 80-11-02 DUE TO FAILED - [SDR ABXA2025121311](https://openairdocs.org/sdr/ABXA2025121311), Dec 1, 2025: WARNING MESSAGE. FALSE ACTIVATION. DURING TAXI OUT L REV ISLN VALVE LIGHT ILLUMINATED ON GROUND A/C RETURNED TO THE GATE(BTB0 AND MTX GROUNDED A/C. MTX PERFORMED THRUST REVERSER BITE TEST AND MSG - [SDR ABXA20250506090](https://openairdocs.org/sdr/ABXA20250506090), May 6, 2025: WARNING MESSAGE. FALSE ACTIVATION. DURING TAXI, ICE DET OFF EICAS MESSGAE AFTER ENGINE START. A/C RETURNED TO GATE (BTB) AND MTX GROUNDED A/C , MTX. PERFORMED OPS CHECK AND SYSTEM CHECKED OK IAW - [SDR ABXA20250116014](https://openairdocs.org/sdr/ABXA20250116014), Jan 16, 2025: UNKNOWN. LEAKING. AFTER PUSH BACK GROUND CREW REPORTED FUEL LEAKING FROM #2 ENGINE A/C RETURNED TO THE GATE (BTB) AND MTX GROUNDED AC. MTX THEN RAN ENGINE AND PERFORMED POWERPLAN - [SDR ABXA2025011509](https://openairdocs.org/sdr/ABXA2025011509), Jan 15, 2025: PUMP. LOW PRESSURE. DURING TAXI THE CTR R FUEL PUMP EICAS MESSAGE APPEARED , AC RETURNED TO GATE(BTB) AND MTX GROUNDED AC . MTX VERIFIED LOW FUEL IN CENTER TANK. TRANSFERRED FUEL O - [SDR ABXA2025011207](https://openairdocs.org/sdr/ABXA2025011207), Jan 12, 2025: WARNING MESSAGE. FALSE ACTIVATION. DURING TAXI RH BLEED OFF AFTER START . AC RETURNED TO GATE (BTB) AND MTX GROUNDED AC . MTX RAN RH ENGINE AND RESET RT BLEED AIR IAW AMM 71-00-00 OPS CHECK GOOD - [SDR ABXA20241223270](https://openairdocs.org/sdr/ABXA20241223270), Dec 23, 2024: SHUTOFF VALVE. MALFUNCTIONED. DURING TAXI OUT , RH ENGINE BLEED VALVE OFF REGARDLESS OF THE POSITION AFTER STARTING ENGINE. AC RETURNED TO GATE(BTB) AND MTX GROUNDED AC , TROUBLE SHOT AND RE - [SDR ABXA20241220269](https://openairdocs.org/sdr/ABXA20241220269), Dec 20, 2024: WARNING MESSAGE. ILLUMINATED. DURING TAXI OUT FWD EQUIPMENT SUPPLY FAN #1 STATUS MESSAGE APPEARED AND AC RETUNED TO GATE (BTB) AND MTX GROUNDED AC , MTX DEFERRED FOR DEPARTURE IAW MEL ABX-21 - [SDR ABXA2024122239](https://openairdocs.org/sdr/ABXA2024122239), Dec 2, 2024: WARNING MESSAGE. FALSE ACTIVATION. E/E ACCESS DOOR EICAS MSG ON T/O RTF PER FLIGHT CONTROL AND MX CONTROL. EVENT OCCURED BETWEEN 700 - 1500 FEET AGL (ATB) AND MTX GROUNDED AC . MTX INSPECTED AC A - [SDR ABXA20241126235](https://openairdocs.org/sdr/ABXA20241126235), Nov 26, 2024: ANTI-ICE VALVE. FAULTED. DURING TAXI WITH BOTH ENGINES RUNNING AND ENGINE ANTI-ICE SELECTED ON WE OBSERVED THE RIGHT ENGINE ANTI-ICE VALVE LIGHT ILLUMINATED AND A RIGHT ENGINE ANTI-ICE - [SDR ABXA20241001181](https://openairdocs.org/sdr/ABXA20241001181), Oct 1, 2024: BRAKE ASSY. FIRE. AS AC TAXIED INTO GATE MTX NOTICED LH GEAR WAS SMOKING , MTX CALLED FOR FIRE RESCUE TO EXTINGUISH . AFTER ALL WAS GOOD AND BRAKES AND WHEELS COOLED MTX GROUNDED - [SDR ABXA20240910172](https://openairdocs.org/sdr/ABXA20240910172), Sep 10, 2024: PITOT TUBE. MALFUNCTIONED. DURING TAXI FOR EVAL. FLIGHT CAPTIANS PITOT HEAT EICAS MSG APPEARED AND AC RETURNED TO GATE AND MTX GROUNDED AC , AFTER TROUBLE SHOOTING FOUND HEATER COIL FOR C - [SDR UIEA2024070300573](https://openairdocs.org/sdr/UIEA2024070300573), Jul 7, 2024: REINFORCEMENT. MECHANIC ERROR. LH WING REINFORCEMENT ANGLE AT STR L-11 BETWEEN RIB 10 AND 11 WITH MIS DRILL HOLES(

MIS DRILL HOLES ON REPAIRED LH WING REINFORCEMENT ANGLE AT STR L-11 BETWEE - [SDR UIEA2024070300574](https://openairdocs.org/sdr/UIEA2024070300574), Jul 7, 2024: SKIN. DELAMINATED. DELAMINATION ON LEFT WING, INBOARD MAIN FLAP, LOWER SURFACE(

LEFT WING, INBOARD MAIN FLAP, LOWER SURFACE WAS REPAIRED IAW SRM 57-53-01-2R-1 FIG 201 SHEET 2 AN - [SDR UIEA2024070300576](https://openairdocs.org/sdr/UIEA2024070300576), Jul 7, 2024: SAMPLE PORT. CONTAMINATED. MAIN DECK SMOKE DETECTION SYSTEM SAMPLING PORTS WITH CONTAMINATION(

SMOKE DETECTION SYSTEM SAMPLING PORTS OF MAIN DECK WERE CLEANED IAW AMM 26-19-01-400-801 R - [SDR UIEA2024070400577](https://openairdocs.org/sdr/UIEA2024070400577), Jul 7, 2024: SKIN. DELAMINATED. DELAMINATION ON LEFT WING, INBOARD MAIN FLAP, LOWER SURFACE(

LEFT WING, INBOARD MAIN FLAP, LOWER SURFACE WAS REPAIRED IAW SRM 57-53-01-2R-1 FIG 201 SHEET 2 AN - [SDR UIEA2024070400578](https://openairdocs.org/sdr/UIEA2024070400578), Jul 7, 2024: ANTENNA. CORRODED. CORROSION ON UPPER FORWARD VHF ANTENNA(

REPLACEMENT OF UPPER FWD VHF ANTENNA  WAS PERFORMED IAW AMM 23-12-03- 000-801-001 AND AMM 23-12-03-400-801-001. N - [SDR UIEA2024070400579](https://openairdocs.org/sdr/UIEA2024070400579), Jul 7, 2024: FUEL TANK. LEAKING. FUEL LEAK ON LOWER SURFACE OF CENTER TANK RIGHT SIDE AT RBL 97.42(

FUEL LEAK ON LOWER SURFACE OF CENTER TANK RIGHT SIDE AT RBL 97.42 WAS REPAIRED IAW AMM 28-1 - [SDR UIEA2024070400580](https://openairdocs.org/sdr/UIEA2024070400580), Jul 7, 2024: DRIVE ASSY. LEAKING. LEFT WING POWER DRIVE UNIT ASSY LE SLAT WITH EVIDENCE OF LEAK(

LEFT WING POWER DRIVE UNIT ASSY L/E SLAT WAS REPLACED I.A.W. AMM 27-81-10-424-023 REV. 142 DATE - [SDR UIEA2024070400581](https://openairdocs.org/sdr/UIEA2024070400581), Jul 7, 2024: ACCESS PANEL. LEAKING. LH WING, ACCESS PANEL 533AB, INNER DRY BAY, ON RIB 6, WITH EVIDENCE FUEL LEAK(

LH WING, ACCESS PANEL 533AB, INNER DRY BAY, ON RIB 6, WITH EVIDENCE FUEL LEAK. - [SDR UIEA2024070400582](https://openairdocs.org/sdr/UIEA2024070400582), Jul 7, 2024: SWITCH. INOPERATIVE. ENG 1 RH T/R INOPERATIVE CDU T/R POSITION SWITCH(

ENG 1 RH T/R, CDU T/R POSITION SWITCH WAS REPLACED PER AMM 78-36-01-404-008. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2024070400583](https://openairdocs.org/sdr/UIEA2024070400583), Jul 7, 2024: SKIN. DELAMINATED. DELAMIATION ON SKIN OF VETRICAL STABILIZER 3" ABOVE FSS 1195.390 AND NEAR LEADING EDGE(

VETRICAL STABILIZER 3" ABOVE FSS 1195.390 AND NEAR LEADING EDGE WAS RE - [SDR UIEA2024070300575](https://openairdocs.org/sdr/UIEA2024070300575), Jul 3, 2024: SKIN. DELAMINATED. DELAMINATION ON RIGHT WING, SLAT NO 9, MULTIPLE DENTS ON UPPER SKIN OF TRAILING EDGE WEDGE(

 RIGHT WING, SLAT NO 9 WAS REP AIRED IAW SRM 57-43-02-2R-1 RE - [SDR UIEA2023082800799](https://openairdocs.org/sdr/UIEA2023082800799), Aug 27, 2023: LIGHT. UNKNOWN. EMER LIGHTS "UNARMED" LIGHT BROKEN(

R/R UNARMED LIGHT IAW B767 AMM 33-11-00. OPS CKS GOOD

) - [SDR UIEA2023050700410](https://openairdocs.org/sdr/UIEA2023050700410), May 7, 2023: UNKNOWN. UNKNOWN. TWO INERTIA DESCENT DEVICE REELS BROKEN #1 AND #7(

PLACED ON DEFERRAL 185160 PER MEL 25-61-01-01 CAT C DUE DATE 17MAY23

) - [SDR UIEA2023042700388](https://openairdocs.org/sdr/UIEA2023042700388), Apr 27, 2023: SPRING. UNKNOWN. TWO ESCAPE REELS FELL OUT DURING TAKE OFF. R/R HOLDING SPINGS FOR #2 AND #3 INERTIA REEL IAW SRM 51-40-02 AND AMM 25-61-00. OPS CHECK GOOD AT THIS TIME. - [SDR UIEA2023032300281](https://openairdocs.org/sdr/UIEA2023032300281), Mar 23, 2023: UNKNOWN. UNKNOWN. EXIT SIGN BY DOOR HANDLE FELL OFF(

RE-INSTALED EXIT SIGN IAW B767 AMM 25-63-00. NO FURTHER DEFECTS NOTED

) - [SDR UIEA2023031000236](https://openairdocs.org/sdr/UIEA2023031000236), Mar 10, 2023: NONE. NONE. SUSPECTED HARD LANDING(

COMPLETED PHASE 1 INSPECTION IAW B-767 AMM 05-51-01 PER MCC, NO DEFECTS NOTED AT THIS TIME.

) - [SDR UIEA2023022300178](https://openairdocs.org/sdr/UIEA2023022300178), Mar 4, 2023: NONE. NONE. DEBONDED TWO AREAS ON RH PANEL OUTER SKIN LOCATED AT FRONT SPAR AND BETWEEN FSS145.128 TO FSS 270.784 FROM VERTICAL STABILIZER.(

IT WAS REPAIRED PER SRM 55-30 - [SDR UIEA2023022300179](https://openairdocs.org/sdr/UIEA2023022300179), Mar 4, 2023: NONE. NONE. DEBONDED TWO AREAS ON LH PANEL OUTER SKIN LOCATED AT FRONT SPAR AND BETWEEN FSS145.128 TO FSS 270.784 FROM VERTICAL STABILIZER.(

IT WAS REPAIRED PER SRM 55-30 - [SDR UIEA2023022300180](https://openairdocs.org/sdr/UIEA2023022300180), Mar 4, 2023: NONE. NONE. ENGINE #1, INLET COWL LIP SKIN WAS FOUND WITH GOUGE OUT OF LIMITS AT 8 O CLOCK POSITION(

IT WAS REPAIRED PER COLLINS REPAIR FORMAT #CV23-01267-REPAIR AND BOEI - [SDR UIEA2023022300182](https://openairdocs.org/sdr/UIEA2023022300182), Mar 4, 2023: NONE. NONE. LH PYLON - UPPER SKIN - WEAR DAMAGE BETWEEN NAC STA 149.43 TO NAC STA 139.73 FOUND OUT OF LIMITS (IT WAS EXCEEDED THE MAXIMUM DEPTH).(

IT WAS REPAIRED PER BOE - [SDR UIEA2023022300183](https://openairdocs.org/sdr/UIEA2023022300183), Mar 4, 2023: NONE. NONE. BULK CARGO DOOR SURROUND STRUCTURE - LOWER SILL - EXISTING EDGE REWORK AT LIGHTENING HOLE OF FLOOR PLATE.(

IT WAS REPAIRED PER BOEING SR 4-5708956820.

) - [SDR UIEA2023022300184](https://openairdocs.org/sdr/UIEA2023022300184), Mar 4, 2023: WINDOW. NONE. FLIGHT COMPARTMENT WINDOW, LH WINDOW (#3) WITH CRACKING(

IT WAS REPLACED PER AMM 56-11-10. OPS CHECK GOOD.

) - [SDR UIEA2023022300185](https://openairdocs.org/sdr/UIEA2023022300185), Mar 4, 2023: NONE. NONE. DURING A ZONAL INSPECTION, MISSING RIVETS ON THE ANGLE ON THE FLOOR BEAM LOWER CHORD LOCATED AT STA 654+121, S-20LH AND STA 676, S-20LH.(

IN ACCORDANCE WITH I - [SDR UIEA2023022300186](https://openairdocs.org/sdr/UIEA2023022300186), Mar 4, 2023: NONE. NONE. LOOSE SHIM LOCATED IN THE HOUSING ASSY (112T1018-1) FROM FWD TRUNNION SUUPORT, LH MAIN LANDING GEAR(

REMOVED THE HOUSING ASSY (112T1018-1) TO REPLACE FILLERS - [SDR UIEA2023022300188](https://openairdocs.org/sdr/UIEA2023022300188), Mar 4, 2023: NONE. NONE. LH WING #6 L/E SLAT (P/N 114T3100-401G, S/N 000010) SKIN BIRD STRIKE DENT DAMAGE - TIME LIMIT REPAIR(

IT WAS REPAIRED IN ACCORDANCE WITH ATLAS EO 1957A609 / S - [SDR UIEA2023030200197](https://openairdocs.org/sdr/UIEA2023030200197), Mar 4, 2023: NONE. NONE. RH WING, SPOILER #9, TRAILING EDGE LOWER SURFACEÂ (OUTBOARD CORNER), CLOSE TO WSTA 616.2.(

IT WAS REPAIRED PER SRM 57-70-01-2R-1 AND SRM 51-70-04-0G-0.

) - [SDR UIEA2023030200198](https://openairdocs.org/sdr/UIEA2023030200198), Mar 4, 2023: NONE. NONE. LH MLG DOOR WITH PUNCTURE DAMAGE ON INNER SKIN AT 30 INCH FROM DOOR LEADING EDGE AND 4 INCH FROM LOWER EDGE.(

IT WAS REPAIRED BY SRM 52-80-02-2R-1 / SRM 51-70 - [SDR UIEA2022102701175](https://openairdocs.org/sdr/UIEA2022102701175), Oct 25, 2022: BATTERY PACK. NONE. EMERGENCY LIGHT RIGHT SIDE OVERHEAD COCKPIT INOP(

T/S PER FIM 33-51 F/T 803, FOUND BATTERY PACK AT FAULT, ORDERED P/N 2013-1A.  REMOVED AND REPLACED BATT - [SDR UIEA2022102701176](https://openairdocs.org/sdr/UIEA2022102701176), Oct 25, 2022: BATTERY PACK. NONE. EMERGENCY LIGHT AT L1 DOOR INOP.(

T/S PER FIM 33-51 F/T, FOUND BATTERY PACK AT FAULT, ORDEDED 2013-1A SEE ITEM M7 FOR CORRECTIVE ACTION.

/

M7 CORRECTIV - [SDR UIEA2022082600906](https://openairdocs.org/sdr/UIEA2022082600906), Aug 24, 2022: SIGN. DETACHED. DURING COCKPIT OBSERVATION, I FOUND EXIT SIGN ON LIFE RAFT GALLEY COMPUTER NEAR BUTTON BROKEN OFF.(

RESECURED EXIT SIGN IN PLACE IAW AMM 25-00-00. OPS CHECK G - [SDR UIEA2022011100011](https://openairdocs.org/sdr/UIEA2022011100011), Jan 11, 2022: NONE. NONE. UPON DOOR CLOSURE L1 PUSH BUTTON FOR ESCAPE SLIDE WAS NOT CENTERED IN PRECUT PANEL(

TRIMMED AND ADJUSTED PRECUT PANEL IAW SRM 51-70-16-06-0 PUSH BUTTON EXTEND - [SDR UIEA2021111002386](https://openairdocs.org/sdr/UIEA2021111002386), Nov 9, 2021: NONE. NONE. FO SIDE OUTLET / NO HEAT.(

PERF PACK TEMP CONTROL TEST IAW AMM 21-51-16. OPS CHECK GOOD. AIR TEMP FROM ALL FLIGHT DECK VENTS BLOWS WARM EVENLY. NO DEFECTS AT All 308: https://openairdocs.org/aircraft/N1093A/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 N1093A The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N1093A before. - [Cancelled 1989-05-01](https://openairdocs.org/deregistered/N1093A-1989-05-01): Hughes 269C, S/N 1290866. N-number assigned, not yet registered - [Cancelled 1954-01-12](https://openairdocs.org/deregistered/N1093A-1954-01-12): Piper PA-18, S/N 18-683. Owner: [Mcmurray Paul](https://openairdocs.org/faa-owner/MCMURRAY%20PAUL), [Fletcher, NC](https://openairdocs.org/faa-place/NC/Fletcher) ## Related - Other Boeing 767-36N aircraft: https://openairdocs.org/model/boeing-767-36n/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.