# N1013A: 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: 30110
- Year built: 1999
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 7, 2016
- Certificate issued: July 17, 2018
- Expires: July 31, 2028
- Mode S code: A00B2D
- 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=1013A
- Page: https://openairdocs.org/aircraft/N1013A

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 N1013A.

## FAA accident and incident reports

None matched to N1013A.

## Service difficulty reports (298, 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 ABXA20261019472](https://openairdocs.org/sdr/ABXA20261019472), Oct 19, 2026: GENERATOR. FAULTED. L GEN DRIVE DISC LIGHT FLICKERING ON PUSHBACK AFTER ENGINE STARTA/C RETURNED TO THE GATE (BTB) AND MTX GROUNDED A/C. MTX DEFERRED LH GEN FOR DEPARTURE IAW MEL A
- [SDR ABXA20260923433](https://openairdocs.org/sdr/ABXA20260923433), Sep 23, 2026: MOTOR. DEFECTIVE. DURING TAXI, LE SLAT DISAGREE. CREW RETURNED TO THE GATE (BTB). CHECKED WIRING OF ALTERNATE INBORAD SLAT DRIVE MOTOR M494 AND FOUND CB C324 POPPING DURNING ACT 
- [SDR ABXA20260801344](https://openairdocs.org/sdr/ABXA20260801344), Aug 1, 2026: CONTROLLER. MALFUNCTIONED. L ENG BLEED OFF AND L PACK OFF EICAS LIGHT AND L ENG OFF (PNEUMATIC) VALVE LIGHT AND PACK OFF OVERHEAD LIGHT. C/X MC 227 AND CYCLED L ENG BLEED VALVE. AT 85% N2
- [SDR ABXA20260731342](https://openairdocs.org/sdr/ABXA20260731342), Jul 31, 2026: ANTI-ICE VALVE. MALFUNCTIONED. LEFT ENG ANTI-ICE VALVE ON TAXI. C/W NNC 3.3 CANNOT TAKEOFF REQUIRES HIGH THRUST CYCLED ENG ANTI ICE AND EICAS/ VALVE LIGHT DISAPPEARED CALLED DISPATCH & MAINTE
- [SDR ABXA20260711313](https://openairdocs.org/sdr/ABXA20260711313), Jul 11, 2026: AUDIO PANEL. MALFUNCTIONED. DURING SERVICE CHECK FOUND CAPTAINS OXYGEN MASK MICROPHONE INOP. SWAPPED CAPTANS AUDIO PANEL WITH FIRST OBSERVERS, IAW AMM 23-12-02 OPS CHECK GOOD. AND DEFERRED
- [SDR ABXA20260625286](https://openairdocs.org/sdr/ABXA20260625286), Jun 25, 2026: PROXIMITY SWITCH. MALFUNCTIONED. ENTRY DOOR LIGHT WON'T EXSTINGUISH WHEN ENTRY DOOR IS CLOSED. MTX DEFERRED L1 DOOR INDICATION FOR DEPARTURE IAW MEL ABX-52-71-1-1 .RETURNED AC TO SERVICE ,THEN 
- [SDR ABXA20260625284](https://openairdocs.org/sdr/ABXA20260625284), Jun 25, 2026: PROXIMITY SWITCH. DEFECTIVE. DURING TAXI, STS MSG "LDG GEAR MONITOR" "MN CARGO DOOR IND". CREW RETURNED TO THE GATE (BTB). AFTER INTERROGATE PSEU MSG CODE 006 SHOWS R/R PSEU IAW AMM 32-09-0
- [SDR ABXA20260624278](https://openairdocs.org/sdr/ABXA20260624278), Jun 24, 2026: HMU. DEFECTIVE. DURING CRUISE LEFT ENG LOST PARTIAL PWR, WOULD NOT ADVANCE BEYOND 67.5 N1 AND 22 FF ON FINAL PWR APPEARED TO RESTORE. ACFT DIVERTED TO ORD AND AN EMERGENCY WAS 
- [SDR ABXA20260511194](https://openairdocs.org/sdr/ABXA20260511194), May 11, 2026: PITOT HEAD. MALFUNCTIONED. DURING TAXI OUT,LE SLAT ASYM CAUTION MSG AND LIGHT ON AFTER START CHECKLIST. SEEMS TO HAPPEN WHEN SELECTING APU OFF WHILE FLAPS ARE IN TRANSIT.A/C RETURNED TO T
- [SDR ABXA20260320122](https://openairdocs.org/sdr/ABXA20260320122), Mar 20, 2026: COWL DOOR. MISSING. DURING MAINTENANCE INSPECTION, FOUND PANEL 446AL ON #2 ENG I/B PYLON MISSING. REPLACED PANEL 446AL IAW AMM 54-53-01. THIS CLOSES DI# 71620. PLACARD REMOVED. NO 
- [SDR ABXA20260314108](https://openairdocs.org/sdr/ABXA20260314108), Mar 14, 2026: STIFFENER. CRACKED. DURING C6 CHECK, FOUND CRACKED STIFFENER ON FLOOR SUPPORT BEAM AT STA 246 AND RBL40. (BETWEEN NLG CENTER BOX AND FLIGHT DECK FLOOR STRUCTURE) (NR 0078). MAINTEN
- [SDR ABXA20260206055](https://openairdocs.org/sdr/ABXA20260206055), Feb 6, 2026: FIRE LOOP. FAULTED. DURING MAINTENANCE INSPECTION, MAIN CARGO LOOP 1 & 2 INTERMITTENT. RESTORE AIRCRAFT POWER ON IAW AMM 26-22-00. PERFORM T/S IAW FIM 26-14 FT 809. SYSTEM TEST OK.
- [SDR ABXA2026020231043](https://openairdocs.org/sdr/ABXA2026020231043), Jan 31, 2026: START VALVE. FAILED. ON TAXI OUT WHILE STARTING LEFT HAND ENGINE START VALVE DID NOT OPEN ,LEFT STARTER EICAS MESSAGE APEARED. AC RETURNED TO THE GATE AND MTX GROUNDED AC AND DEFERR
- [SDR ABXA20260129035](https://openairdocs.org/sdr/ABXA20260129035), Jan 29, 2026: START VALVE. FAULTED. ON TAXI OUT, LEFT ENGINE EICAS LEFT ENGINE START AND OVERHEAD VALVE LIGHT ILLUMINATED DURING START. ACFT RETURNED TO BLOCKS (BTB). CYCLED START VALVE AND ACCOMP
- [SDR ABXA20260127030](https://openairdocs.org/sdr/ABXA20260127030), Jan 27, 2026: WARNING MESSAGE. ILLUMINATED. DURING TAXI OUT, LEFT ENGINE EICAS, LEFT ENGINE START AND OVERHEAD VALVE LIGHT ILLUMINATED DURING START. AIRCRAFT RETURNED TO BLOCKS (BTB). MAINTENANCE DEFERRED
- [SDR ABXA20251231365](https://openairdocs.org/sdr/ABXA20251231365), Dec 31, 2025: FIRE LOOP. FALSE INDICATION. AFTER LANDING STATUS MSG "MN CARGO LOOP 2" ILLUMINATED. ACCOMPLISHED FIM 26-14 FT 809 BLOCKS 1-2-3-4-5-6 AND 7 AFTER AFOLTS TEST, NO MN CARGO LOOP 2 PRESENT. CA
- [SDR ABXA20251212331](https://openairdocs.org/sdr/ABXA20251212331), Dec 12, 2025: PCB. DEFECTIVE. RED MAIN DECK CARGO FIRE WARNING WITH ASSOCIATED LIGHTS AND MASTER CAUTION INTERMITTENTLY EVERY 5 MINS.MTX GROUNDED A/C .MTX REMOVED AND REPLACED PRINTED CIRCUI
- [SDR ABXA20251212330](https://openairdocs.org/sdr/ABXA20251212330), Dec 12, 2025: OVERHEAT LOOP. FALSE INDICATION. INTERMITENT MN CARGO LP 1 AND 2 STATUS MESSAGE W/FIRE WARNING.MTX GROUNDED A/C AND PERFORM MAIN CARGO/ENG/APU/FIRE/OVHT TEST. IAW AMM 26-14-00. OPS CHECKED NORM
- [SDR ABXA20251019274](https://openairdocs.org/sdr/ABXA20251019274), Oct 19, 2025: BATTERY. FAULTED. DURING TAXI ,APU BATTERY, NO STBY STATUS MESSAGE DISPLAYED. ADVISED BY MTC TO RETURN TO PARKING (BTB). MTX GROUNDED ACFT AND REMOVED AND REPLACED APU BATTERY IA
- [SDR ABXA20250708143](https://openairdocs.org/sdr/ABXA20250708143), Jul 8, 2025: WARNING MESSAGE. ILLUMINATED. PER MXC REQUEST VERIFY LOCK POSITION IN MCD , A/C RETURNED TO THE GATE AND GROUNDED BY MTX, MTX THEN VERIFIED LOCK RBL:33, LBL:33 +LBL:11 PREVIOUSLY INSTALLED I
- [SDR ABXA20250527106](https://openairdocs.org/sdr/ABXA20250527106), May 27, 2025: DIRECTOR. MALFUNCTIONED. AFTER TAKE-OFF, RT FLIGHT DIRECTOR DISAPPEARED TROUBLE SHOT IT AFTER 18K AND COULDN'T GET RESOLUTION SWITCHED RIGHT SIDE TO CENTER AND SGL SOURCE FD TCAS MSG AP
- [SDR ABXA20250305053](https://openairdocs.org/sdr/ABXA20250305053), Mar 5, 2025: PUMP. WARNING MESSAGE. DURING TAXI, L FWD FUEL PUMP EICAS MSG DISPLAYED AFTER ENGINE START. A/C RECTURNED TO GATE. (BTB) DEFERRED L FWD FUEL PUMP FOR DEPARTURE IAW MEL ABX-28-22-1. MT
- [SDR ABXA20241111222](https://openairdocs.org/sdr/ABXA20241111222), Nov 11, 2024: PUMP. INOPERATIVE. DURING TAXI OUT THE RIGHT HAND AFT FUEL PIMP INOP MSG APPEARED AFTER ENGINE START A/C RETURNED TO GATE (BTB) AND MTX GROUNDED A/C . MTX FOUND INCORRECT BREAKER 
- [SDR ABXA20241111221](https://openairdocs.org/sdr/ABXA20241111221), Nov 11, 2024: PUMP. WARNING MESSAGE. DURING TAXIOUT THE L FWD FUEL PUMP EICAS MSG APPEARED AND AC RETURNED TO BLOCK (BTB) AND MAINTENANCE GROUNDED AC .MTX DEFERRED LH FWD FUEL PUMP IAW MEL ABX-28-2
- [SDR ABXA20241103213](https://openairdocs.org/sdr/ABXA20241103213), Nov 3, 2024: FIRE WARNING. FALSE ACTIVATION. DURING LOADING OF AIRCRAFT MAIN DECK CARO FIRE WARNING ACTIVATED MULTIPLE TIMES.FIRE DEPARTMENT CAME AND DECLARED NO SIGNS OF FIRE OR SMOKE IN MCD, OR LOWER CAR
- [SDR ABXA20241002183](https://openairdocs.org/sdr/ABXA20241002183), Oct 2, 2024: WARNING MESSAGE. ILLUMINATED. AFTER ENGINE START L FWD FUEL PUMP EICAS ILLUMINATED DURING TAXI.AC RETURNED TO BLOCK AND MTX GROUNDED AC , DEFERRED FOR DEPARTURE .IAW MEL ABX-28-22-1 AC WAS R
- [SDR UIEA2024052300416](https://openairdocs.org/sdr/UIEA2024052300416), May 26, 2024: SHOE. WORN. NOSE LANDING GEAR BOTH BRAKE SHOES OF WHEELS UPPER GEAR WITH WEAR(<P>NOSE LANDING GEAR BRAKE SHOES OF WHEELS WERE REPLACED I.A.W. AMM 32-45-05-022-001 REV. 142 
- [SDR UIEA2024052300417](https://openairdocs.org/sdr/UIEA2024052300417), May 26, 2024: METERING VALVE. LEAKING. NOSE LANDING GEAR STEERING VALVE WITH HYDRAULIC LEAK IN THE BODY(<P>NOSE LANDING GEAR STEERING METERING VALVE WAS REPLACED IAW AMM 32-51-04-404-013 REV. 142 22-
- [SDR UIEA2024052300418](https://openairdocs.org/sdr/UIEA2024052300418), May 26, 2024: BUSHING. EXCESS PLAY. NOSE LANDING GEAR AFT DOORS BOTH WITH EXCESSIVE PLAY IN THE PIVOT POINTS(<P>NOSE LANDING GEAR AFT DOORS BOTH WITH EXCESSIVE PLAY IN THE PIVOT POINTS, BUSHINGS W
- [SDR UIEA2024052300420](https://openairdocs.org/sdr/UIEA2024052300420), May 26, 2024: BONDING JUMPER. BROKEN. MAIN LANDING GEAR WELL LH PART AFT LOWER (STA 1065 ) WITH BROKEN BONDING BUMPER ON APU FUEL DRAIN LINE(<P>MAIN LANDING GEAR WELL, LEFT REAR LOWER STA 1065 BONDI
- [SDR UIEA2024052300421](https://openairdocs.org/sdr/UIEA2024052300421), May 26, 2024: VENT. MISINSTALLED. RIGHT WING MAIN, TANK, BETWEEN RIB 19 AND RIB 18, FUEL DUCT VENT, LOCKWIRE MISSING ON BOTH NUT RETAINER(<P>RIGHT WING MAIN TANK, BETWEEN RIB 19 AND RIB 18, FUEL
- [SDR UIEA2024052300422](https://openairdocs.org/sdr/UIEA2024052300422), May 26, 2024: SKIN. DENTED. LH WING, INBOARD FLAP SURFACE LEADING EDGE AREA UPPER OUTSIDE CORNER WITH TWO DENTS.(<P>LH WING, INBOARD FLAP, MAIN FLAP WAS REPAIRED IAW SRM 57-53-01-2R-1 FIG 
- [SDR UIEA2024052300423](https://openairdocs.org/sdr/UIEA2024052300423), May 26, 2024: NONE. NONE. FAA AGING INSPECTION RH A/A PACK EXHAUST RAM AIR ACTUATOR BONDING LEAD WITH WIRES BROKEN.(<P>RH A/A PACK EXHAUST RAM AIR ACTUATOR BONDING LEAD WAS REPLACED IAW 
- [SDR UIEA2024052300424](https://openairdocs.org/sdr/UIEA2024052300424), May 26, 2024: CONTROL CABLE. ABNORMAL. SECTION 48 INTERNAL AREA, LH ELEVATOR CONTROL CABLE RUBBING WITH PULLEY BRACKET (DUE BAD INSTALLATION) LOCATED AT B. STA 1605.5 LH SIDE.(<P>SECTION 48 INTERNAL 
- [SDR UIEA2024052400437](https://openairdocs.org/sdr/UIEA2024052400437), May 26, 2024: SKIN. DELAMINATED. RH WING, INBOARD AILERON, TRAILING EDGE, RH SIDE WITH DELAMINATION(<P>RH WING, INBOARD AILERON, TRAILING EDGE, RH SIDE WAS REPAIRED IAW SRM 57-60-01-2R-1 REPAIR
- [SDR UIEA2024052800463](https://openairdocs.org/sdr/UIEA2024052800463), May 26, 2024: SKIN. DELAMINATED. RH WING, INBOARD AILERON, TRAILING EDGE, RH SIDE WITH DELAMINATION(<P>RH WING, INBOARD AILERON, TRAILING EDGE, RH SIDE WAS REPAIRED IAW SRM 57-60-01-2R-1 REPAIR
- [SDR UIEA2024052400438](https://openairdocs.org/sdr/UIEA2024052400438), May 26, 2024: SKIN. CORRODED. PYLON #1 UPPER SURFACE, CORROSION DAMAGE ON THE BUSHING OF THE INBD LUG OF FWD UPPER SPAR FITTING.(<P>REPAIR FOR CORROSION DAMAGE ON THE BUSHING OF THE INB LUG 
- [SDR UIEA2024052400439](https://openairdocs.org/sdr/UIEA2024052400439), May 26, 2024: SKIN. DENTED. RH WING, INBOARD FLAP, MAIN FLAP, AT 2" FROM TRAILING EDGE AND 6" FROM INBOARD EDGE, DENT ON UPPER SKIN(<P>RH WING, INBOARD FLAP, MAIN FLAP WAS REPAIRED IAW SRM
- [SDR UIEA2024052400440](https://openairdocs.org/sdr/UIEA2024052400440), May 26, 2024: SKIN. PUNCTURED. LH INB ELEVATOR UPPER PANEL, PUNCTURE AT ELEV STA 104.2 APPROX. AND 28" FROM T.EDGE.(<P>LH INBOARD ELEVATOR, UPPER PANEL WAS REPAIRED IAW SRM 55-20-01-2R-1 REPA
- [SDR UIEA2024052400442](https://openairdocs.org/sdr/UIEA2024052400442), May 26, 2024: SKIN. PUNCTURED. LH INB ELEVATOR UPPER PANEL, PUNCTURE AT ELEV STA 104.2 APPROX. AND 28" FROM T.EDGE.(<P>LH INBOARD ELEVATOR, UPPER PANEL WAS REPAIRED IAW SRM 55-20-01-2R-1 REPA
- [SDR UIEA2024052400441](https://openairdocs.org/sdr/UIEA2024052400441), May 26, 2024: FITTING. CORRODED. LH WING FWD LOAD PITCH FITTING, CORROSION DAMAGE ON INB FITTING.(<P>CORROSION ON INBD FITTING WAS REWORKED IAW TRE6757246, REV 1, MAY 20, 2024. LEVEL CORROSION 
- [SDR UIEA2023053000529](https://openairdocs.org/sdr/UIEA2023053000529), May 28, 2023: EVAS UNIT. UNKNOWN. CAPTAINS EVAS IS INOP(<P><SPAN>REMOVED AND REPLACED CAPTAINS EVAS AS PER 25-60-00 (AMM) OPS CHECKED NORMAL.</SPAN></P>)
- [SDR UIEA2023050800425](https://openairdocs.org/sdr/UIEA2023050800425), May 5, 2023: SMOKE GOGGLES. UNKNOWN. FIRST OBSERVERS SMOKE GOGGLES INOP(<P>TRANSFERRED TO MDDR 185104 PER MEL 25-11-02-01A CAT A DUE 17MAT23. PLACARDS INSTALLED. LOGPAGE 1773702 M3: REMOVED AND REP
- [SDR UIEA2022102601174](https://openairdocs.org/sdr/UIEA2022102601174), Oct 25, 2022: FIRST AID KIT. NONE. FIRST AID KIT NEXT TO OVHEAD BIN COMPROMISED MISSING RED SEAL.(<P>REMOVED AND REPLACED FIRST AID KIT IW B767 AMM 25-64-03.</P>)
- [SDR UIEA2022102201170](https://openairdocs.org/sdr/UIEA2022102201170), Oct 24, 2022: NONE. NONE. CORROSION DAMAGE ON RIGHT INBOARD TE FLAP TORQUE TUBE(<P>RIGHT INBOARD TE FLAP TORQUE TUBE WAS REPLACED IAW SB 767-57A0066</P>)
- [SDR UIEA2022102201169](https://openairdocs.org/sdr/UIEA2022102201169), Oct 24, 2022: NONE. NONE. THREE DENTS ON ENGINE #2 PRIMARY EXHAUST OUTER SKIN BETWEEN 6/8 O´CLOCK AND BETWEEN NAC STA 323.42/344.67(<P>WELD FILL REPAIR IAW BOEING MSG: CMA-TLS-22-0022-0
- [SDR UIEA2022102101168](https://openairdocs.org/sdr/UIEA2022102101168), Oct 24, 2022: NONE. NONE. CORROSION ON ACCESS PANEL SUPPORT FOR KEEL BEAM BETWEEN STA 889 TO STA 915.5(<P>ACCESS PANEL SUPPORT P/N 145T8629-2 WAS REPLACED PER PRODUCTION DRAWING AND SRM 
- [SDR UIEA2022102101167](https://openairdocs.org/sdr/UIEA2022102101167), Oct 24, 2022: NONE. NONE. PUNCTURE ON LH ELEVATOR LOWER SKIN AT 44 INCH OF THE INBOARD CLOUSURE RIB AND 26 INCH OF THE TRAILING EDGE.(<P>AFFECTED AREA WAS REPAIRED ON LH ELEVATOR LOWER S
- [SDR UIEA2022102101166](https://openairdocs.org/sdr/UIEA2022102101166), Oct 24, 2022: NONE. NONE. RH WING OUTBOARD FLAP ACCESS PANEL "666KT" WITH DENT AT 33 INCH FROM EXTERNAL PANEL EDGE &AMP; 25 INCH FROM FLAP TRAILING EDGE AND SECOND ONE AT 68 INCH FROM EX
- [SDR UIEA2022102101165](https://openairdocs.org/sdr/UIEA2022102101165), Oct 24, 2022: NONE. NONE. RH WING OUTBOARD FLAP ACCESS PANEL "666MT" WITH DENT AT 5 INCH FROM INTERNAL PANEL EDGE AND 25 INCH FROM FLAP TRAILING EDGE(<P>DENT WAS REPAIRED PER SRM 57-53-0

All 298: https://openairdocs.org/aircraft/N1013A/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 N1013A

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N1013A before.

- [Cancelled 2011-04-15](https://openairdocs.org/deregistered/N1013A-2011-04-15): Gustafson Harold CORBEN JR ACE, S/N JAHG1. Assigned, pending cancellation
- [Cancelled 1955-11-17](https://openairdocs.org/deregistered/N1013A-1955-11-17): Piper PA-18S, S/N 18601. Owner: [Morgan H](https://openairdocs.org/faa-owner/MORGAN%20H)

## 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

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