# N245AY: 1987 Boeing 767-201, registration cancelled 2018-03-12

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: March 12, 2018
- Status when cancelled: Registration expired, pending cancellation
- Airframe: [Boeing 767-201](https://openairdocs.org/model/boeing-767-201) (registry code 1385125)
- Engine: [GE CF6-80 series](https://openairdocs.org/engine/ge-cf6-80-series) (registry code 30025)
- Data sheets: [TCDS A1NM](https://openairdocs.org/tcds/A1NM), [TCDS E13NE](https://openairdocs.org/tcds/E13NE) (OpenAirDocs)
- Serial number: 23897
- Year built: 1987
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: May 20, 1987
- Certificate issued: April 11, 2014
- Last registry action: April 11, 2014
- Mode S code: A242A9
- Owner when cancelled: [Jet Midwest Group LLC](https://openairdocs.org/faa-owner/JET%20MIDWEST%20GROUP%20LLC)
- Location: [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington)
- Owner type: Corporation
- Owner's area on the map: 39.7236° N, 75.5412° W: Placed by OpenAirDocs at the center of ZIP code 19801, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N245AY
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=245AY
- Page: https://openairdocs.org/deregistered/N245AY-2018-03-12

From the FAA registry file of November 7, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

ADs and bulletins for the Boeing 767-201: https://openairdocs.org/model/boeing-767-201.md

## Service difficulty reports (68, newest 50)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR USAA2014022700001](https://openairdocs.org/sdr/USAA2014022700001), Feb 25, 2014: LIGHT. INOPERATIVE. GRU DURING DAILY INSPECTION FOUND AISLE EMERGENCY LIGHT AT ROW 2 A & B INOPERATIVE. R & R AISLE EMERGENCY LIGHT AT ROW 2 A & B, OPERATIONS TESTED GOOD.
- [SDR USAA2013052700001](https://openairdocs.org/sdr/USAA2013052700001), May 24, 2013: TUBE. FAILED. ENROUTE, CAPTAIN`S ADI BLURRED WITH EFI SELECTOR IN NORMAL AND STBY WITH STRONG ELECTRICAL ODOR. PULLED CIRCUIT BREAKER, ODOR DISSIPATED. REPLACED CAPTAIN`S EAD
- [SDR USAA2012111400019](https://openairdocs.org/sdr/USAA2012111400019), Nov 9, 2012: FAIRING. CRACKED. C2 CHECK - CRACK IN NR 12 SLAT END FAIRING AT WS 1046.2. REPLACED NR 12 SLAT END FAIRING AT WS 1046.2 IAW B767 SRM 51-40-05-0G, AMM 20-11-00-422-003.
- [SDR USAA2012110500017](https://openairdocs.org/sdr/USAA2012110500017), Nov 3, 2012: SUPPORT CHANNEL. CRACKED. C2 CHECK - 1 INCH CRACK IN SUPPORT CHANNEL AT BS 545, RBL 37. REPLACED SUPPORT CHANNEL AT BS 545, RBL 37 IAW B767 SRM 51-40-02-0G FIG 12 & 8, ALSO BOEING DRAWIN
- [SDR USAA2012111400018](https://openairdocs.org/sdr/USAA2012111400018), Nov 1, 2012: BULKHEAD. CRACKED. C2 CHECK - CRACK IN BS 1805.9 RIGHT BULKHEAD FORWARD OUTER CHORD AT BS 1805.9, WL 252. REPAIRED BS 1805.9 RIGHT BULKHEAD FORWARD OUTER CHORD AT BS 1805.9, WL 25
- [SDR USAA2012110200001](https://openairdocs.org/sdr/USAA2012110200001), Oct 29, 2012: LENS. BROKEN. C2 CHECK - L1 AND R1 DOOR LOWER EXIT SIGN LENS ARE BROKEN. REPLACED L1 AND R1 DOOR LOWER EXIT SIGN ASSEMBLY AND OPS CHECKED GOOD IAW B767 AMM 33-51-09-401.
- [SDR USAA2012103000017](https://openairdocs.org/sdr/USAA2012103000017), Oct 25, 2012: LATCH. INOPERATIVE. C2 CHECK - RIGHT OFF WING ESCAPE SLIDE COMPARTMENT DOOR NR 1 LATCH NEEDS REPLACED. REPLACED RIGHT OFF WING ESCAPE SLIDE COMPARTMENT DOOR NR 1 LATCH IAW B767 AMM
- [SDR USAA2012103000015](https://openairdocs.org/sdr/USAA2012103000015), Oct 25, 2012: KEEPER. DEFORMED. C2 CHECK - RIGHT OFF WING ESCAPE SLIDE COMPARTMENT DOOR KEEPER IS DEFORMED. REPLACED RIGHT OFF WING ESCAPE SLIDE COMPARTMENT DOOR KEEPER IAW B767 AMM 25-65-09-0
- [SDR USAA2012110200019](https://openairdocs.org/sdr/USAA2012110200019), Oct 18, 2012: GUSSET. CORRODED. C2 CHECK - CORROSION ON GUSSET AT RIGHT PRESSURE DECK AT BS 955, S21R. REPLACED GUSSET AT RIGHT PRESSURE DECK AT BS 955, S21R IAW B767 SRM 51-40-05-0G FIG 2 & B
- [SDR USAA2012102900010](https://openairdocs.org/sdr/USAA2012102900010), Oct 18, 2012: STIFFENER. CRACKED. C2 CHECK - CRACK ON UPPER STIFFENER OF RIGHT PRESSURE DECK AT BS 972, S21R. REPLACED UPPER STIFFENER OF RIGHT PRESSURE DECK AT BS 972, S21R IAW B767 SRM 51-40-0
- [SDR USAA2012102200007](https://openairdocs.org/sdr/USAA2012102200007), Oct 18, 2012: INDICATOR. INOPERATIVE. C2 CHECK - FORWARD ENTRY DOOR EMERGENCY ONLY FLAG DOES NOT FULLY RETRACT. REPLACED FORWARD ENTRY DOOR EMERGENCY ONLY FLAG IAW B767 AMM 20-11-00-422-003 AND ADJU
- [SDR USAA2012102900009](https://openairdocs.org/sdr/USAA2012102900009), Oct 17, 2012: TEE FITTING. CRACKED. C2 CHECK - CRACK ON T-FITTING OF FAIL SAFE STRAP AT BS 955, RBL 97. REPLACED TEE FITTING ON FAIL SAFE STRAP AT BS 955, RBL 97 IAW EA 130973.
- [SDR USAA2012110700003](https://openairdocs.org/sdr/USAA2012110700003), Oct 13, 2012: ATTACH ANGLE. CRACKED. C2 CHECK - 5 CRACKS IN CABIN FLOOR SUPPORT WEB ATTACH ANGLE CHORD BETWEEN BS 566 TO BS 588, RBL 37. REPLACED CABIN FLOOR SUPPORT WEB ATTACH ANGLE CHORD BETWEEN 
- [SDR USAA2012111400016](https://openairdocs.org/sdr/USAA2012111400016), Oct 12, 2012: TEE FITTING. CORRODED. C2 CHECK - SURFACE CORROSION ON TEE FITTING AT BS 995, RBL 92. REPLACED TEE FITTING AT BS 995, RBL 92 IAW EA 130973.
- [SDR USAA2012102900011](https://openairdocs.org/sdr/USAA2012102900011), Oct 12, 2012: ATTACH FITTING. CRACKED. C2 CHECK - CRACK ON INTERCOSTAL ANGLE CLIP AT BS 1088, LBL 22. REPLACED INTERCOSTAL ANGLE CLIP AT BS 1088, LBL 22 IAW B767 SRM 51-40-02-0G FIG 12.
- [SDR USAA2012111200005](https://openairdocs.org/sdr/USAA2012111200005), Oct 11, 2012: FITTING. CRACKED. C2 CHECK - CRACK ON STRAKLET SHEAR CLIP AT LEFT WING LES155, RIB 1. REPLACED STRAKLET SHEAR CLIP AT LEFT WING LES155, RIB 1 IAW EA 130992.
- [SDR USAA2012111200007](https://openairdocs.org/sdr/USAA2012111200007), Oct 10, 2012: BULKHEAD. CRACKED. C2 CHECK - CRACK ON OUTER FORWARD CHORD OUTBOARD FLANGE OF BS 1809.5 BULKHEAD AT S12R. REPLACED OUTER FORWARD CHORD OF BS 1809.5 BULKHEAD AT S12R IAW EA 130974 
- [SDR USAA2012101200002](https://openairdocs.org/sdr/USAA2012101200002), Oct 9, 2012: BATTERY. DISCHARGED. MCN - LEFT FORWARD FLT ATTENDANT SEAT FLASHLIGHT BATTERY IS BAD. REMOVED AND REPLACED LEFT FORWARD FLIGHT ATTENDANT SEAT FLASHLIGHT BATTERY.
- [SDR USAA2012111400017](https://openairdocs.org/sdr/USAA2012111400017), Oct 8, 2012: STRAP. CRACKED. C2 CHECK - CRACK IN RIGHT FAILSAFE STRAP AT BS 955, RBL 92. REPAIRED RIGHT FAILSAFE STRAP AT BS 955, RBL 92 IAW EA 130973.
- [SDR USAA2012111300003](https://openairdocs.org/sdr/USAA2012111300003), Oct 8, 2012: STRAP. CRACKED. C2 CHECK - CRACK ON LEFT FAIL SAFE STRAP AT BS 955, LBL 92. REPAIRED LEFT FAIL SAFE STRAP AT BS 955, LBL 92 IAW EA 130973.
- [SDR USAA2012110500008](https://openairdocs.org/sdr/USAA2012110500008), Oct 8, 2012: STRAP. CRACKED. C2 CHECK - CRACK IN STABILIZER STRAP AT BS 325, RBL 37. REPLACED STABILIZER STRAP AT BS 325, RBL 37 IAW B767 SRM 53-10-51-2R-1, FIG 201 & 51-40-02-0G PAR 4.
- [SDR USAA2012110500007](https://openairdocs.org/sdr/USAA2012110500007), Oct 8, 2012: SKIN PANEL. WORN. 2C CHECK - 1 INCH DIAMETER HOLE WORN INTO NR 1 PYLON SKIN PANEL AT NACELLE STA 361.9, NACELLE WL 130.0. REPAIRED NR 1 PYLON SKIN PANEL AT NACELLE STA 361.9, NAC
- [SDR USAA2012061900021](https://openairdocs.org/sdr/USAA2012061900021), Jun 17, 2012: PRESSURE SWITCH. FAULTY. PHL - FLT 758 EN ROUTE PHL TO ATH. LEFT ENGINE FUEL FILTER DISPLAYED. REMOVED AND REPLACED LEFT ENGINE FUEL FILTER. REMOVED AND REPLACED LEFT ENGINE FUEL FILTER
- [SDR USAA2012051400016](https://openairdocs.org/sdr/USAA2012051400016), May 13, 2012: STRIP. LOOSE. PHL - PLASTIC EMERGENCY LIGHT STRIP UNDER FWD F/A JUMPSEAT POPS OUT, NEEDS FASTENED. RE-SECURED STRIP. OK FOR SERVICE.
- [SDR USAA2012031600012](https://openairdocs.org/sdr/USAA2012031600012), Mar 15, 2012: VENT LINE. DISCONNECTED. FLT 1035. AFT THIRD OF CABIN HAD STRONG ODOR OF URINE, SAME PACKS ON OR OFF. FOUND VENT LINE DISCONNECTED AT CARGO FLOOR LEVEL, JUST FWD OF LAV TANK. RECONNECTE
- [SDR USAA2012030800024](https://openairdocs.org/sdr/USAA2012030800024), Mar 6, 2012: ATTACH FITTING. LEAKING. FLT 1072 EN ROUTE. ON GROUND, WITH APU RUNNING, A "STRONG" URINE TYPE SMELL ON AIRCRAFT, MID CABIN TO AFT. ODOR LESSENED WITH ENGINES RUNNING. IN-FLIGHT, PAX AN
- [SDR USAA2011082300025](https://openairdocs.org/sdr/USAA2011082300025), Aug 19, 2011: DOOR ACTUATOR. EXCESS PLAY. PHL FLT 759 EN ROUTE ATH TO PHL. WITH LEFT PACK IN AUTO, "INOP AND PACK OFF" LIGHT ILLUMINATED ON OVERHEAD PANEL WITH "LEFT PACK TEMP AND LEFT PACK OFF" ON EICA
- [SDR USAA20110603BB043](https://openairdocs.org/sdr/USAA20110603BB043), Jun 1, 2011: SLIDE. DEFECTIVE. CDG - THE R1 DOOR SLIDE FELL OUT OF THE COVER. THE SLIDE WOULD NOT MOUNT BACK IN PLACE. THE AIRCRAFT WAS RELEASED TO CONTINUE ON MEL. MAINTENANCE REPLACED THE R
- [SDR USAA20110516BB037](https://openairdocs.org/sdr/USAA20110516BB037), May 15, 2011: MECHANISM. DEFECTIVE. CLT - ENTRY DOOR L1 ELECTRIC DOOR OPENING WAS INOPERATIVE. MAINTENANCE REPLACED THE OVER-CENTER MECHANISM DUE TO A MISSING BEARING.
- [SDR USAA2011032191154](https://openairdocs.org/sdr/USAA2011032191154), Mar 19, 2011: TEE FITTING. CORRODED. MCN - C1 - MAJOR REPAIR - CORROSION ON KEEL BEAM CHORD SPLICE TEE AT BS 1006.5, RBL 9. REPAIRED KEEL BEAM CHORD SPLICE TEE AT BS 1006.5, RBL 9 IAW B767 SRM 53-5
- [SDR USAA2011032291169](https://openairdocs.org/sdr/USAA2011032291169), Mar 12, 2011: POWER SUPPLY. DISCONNECTED. MCN - C1 - EXTERIOR EMERGENCY LIGHTS AT R-1 DOOR & DOUBLE BANK LIGHT HEAR NOT WORKING. RECONNECTED D1122 TO POWER SUPPLY FOR EMERGENCY LIGHTS AT R-1 DOOR & DOUB
- [SDR USAA2011032291158](https://openairdocs.org/sdr/USAA2011032291158), Mar 9, 2011: BATTERY. WEAK. MCN - C1- L-1 FLIGHT ATTENDANT SEAT FLASHLIGHT WEAK. REPLACED L-1 FLIGHT ATTENDANT SEAT FLASHLIGHT BATTERY, OPS TEST GOOD.
- [SDR USAA2011032191153](https://openairdocs.org/sdr/USAA2011032191153), Mar 9, 2011: SKIN. CRACKED. MCN - C1 - MAJOR REPAIR - RIGHT OUTBOARD AILERON IS CRACKED & DELAMINATED ON LOWER LEADING EDGE OF SKIN NEAR NR 3 HINGE POINT AT WS 1030. REPAIRED RIGHT OUTBOAR
- [SDR USAA20110221BB012](https://openairdocs.org/sdr/USAA20110221BB012), Feb 20, 2011: BEARING. WORN. CLT - THE L2 DOOR LATCH MECHANISM WORKS INTERMITTENTLY (CHECK LATCH CAM). MAINTENANCE REPLACED THE BEARINGS IN THE OVERCENTER MECHANISM FOR THE L2 DOOR.
- [SDR USAA20101201BB082](https://openairdocs.org/sdr/USAA20101201BB082), Nov 29, 2010: BEARING. FAILED. FLT 811, 15 MINUTES OUT OF CUN, ODOR OF BURNING PLASTIC IN COCKPIT AND AFT GALLEY. ODOR DISAPPEARED AFTER 5 MINUTES IN COCKPIT AND NO VISABLE SMOKE ANYWHERE. AL
- [SDR USAA20100521BB032](https://openairdocs.org/sdr/USAA20100521BB032), May 20, 2010: CABLE. DISCONNECTED. R1 DOOR EVACUATION SLIDE CABLES DISCONNECTED. REPLACED R1 DOOR EVACUATION SLIDE. PASSED ALL TESTS AS REQUIRED BY MAINTENANCE MANUALS.
- [SDR USAA20100325BB019](https://openairdocs.org/sdr/USAA20100325BB019), Mar 24, 2010: SENSOR. OUT OF ADJUST. GIG - FLT 800 EN ROUTE CREW RECEIVED EICAS MESSAGE FOR L/E SLAT ASYMMETRY. THE FLAPS ONLY EXTENDED 1/2 DEGREE. THE FLIGHT DECLARED AN EMERGENCY AND PERFORMED A 
- [SDR USAA20100311BB014](https://openairdocs.org/sdr/USAA20100311BB014), Mar 9, 2010: TERMINAL BLOCK. FAULTY. CLT - THE EMERGENCY LIGHT, AIRCRAFT RIGHT, AFT OF AFT CARGO DOOR WAS INOPERATIVE. REPLACED WIRE TERMINAL STRIP ON BACK SIDE OF LIGHT ASSEMBLY.
- [SDR USAA2010022490441](https://openairdocs.org/sdr/USAA2010022490441), Feb 18, 2010: SEAT TRACK. CORRODED. BFM - C4 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN BS 676 TO BS 753, LBL 88.5. REPAIRED SEAT TRACK BETWEEN BS 676 TO BS 753, LBL 88.5 IA
- [SDR USAA2010021990416](https://openairdocs.org/sdr/USAA2010021990416), Feb 17, 2010: SILL. CORRODED. BFM - C4 - MAJOR REPAIR - CORROSION ON L-2 DOOR SILL UPPER SURFACE AT BS 1502, LBL 88.5. REPAIRED L-2 DOOR SILL UPPER CHORD AT BS 1502, LBL 88.5 IAW B767 SRM 53
- [SDR USAA2010021990415](https://openairdocs.org/sdr/USAA2010021990415), Feb 17, 2010: SEAT TRACK. CORRODED. BFM - C4 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN BS 522 TO BS 632, RBL 88.5. REPLACED SEAT TRACK BETWEEN BS 522 TO BS 632, RBL 88.5 IA
- [SDR USAA2010021990411](https://openairdocs.org/sdr/USAA2010021990411), Feb 17, 2010: SILL. CORRODED. BFM - C4 - MAJOR REPAIR - CORROSION ON L-2 DOOR SILL UPPER SURFACE AT BS 1502, LBL 88.5. REPAIRED L-2 DOOR SILL UPPER CHORD AT BS 1502, LBL 88.5 IAW B767 SRM 53
- [SDR USAA2010021990413](https://openairdocs.org/sdr/USAA2010021990413), Feb 15, 2010: FLOORBEAM. CORRODED. BFM - C4 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM UPPER CHORD AT BS 1581, LBL 28. REPAIRED FLOORBEAM UPPER CHORD AT BS 1581, LBL 28 IAW B767 SRM
- [SDR USAA2010021990414](https://openairdocs.org/sdr/USAA2010021990414), Feb 14, 2010: FLOORBEAM. CORRODED. BFM - C4 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM UPPER CHORD AT BS 1480, LBL 28. REPAIRED FLOORBEAM UPPER CHORD AT BS 1480, LBL 28 IAW B767 SRM
- [SDR USAA2010021990412](https://openairdocs.org/sdr/USAA2010021990412), Feb 9, 2010: FLOORBEAM. CORRODED. BFM - C4 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM AT BS 1502, RBL 38. REPAIRED FLOORBEAM AT BS 1502, RBL 38 IAW B767 SRM 53-00-51, 51-40-02 & 51
- [SDR USAA2010021290353](https://openairdocs.org/sdr/USAA2010021290353), Feb 9, 2010: FLOORBEAM. CORRODED. BFM - C4 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM UPPER CHORD AT BS 325, RBL 34. REPAIRED FLOORBEAM UPPER CHORD AT BS 325, RBL 34 IAW B767 SRM 5
- [SDR USAA2010021290352](https://openairdocs.org/sdr/USAA2010021290352), Feb 6, 2010: SEAT TRACK. CORRODED. BFM - C4 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN BS 632 TO BS 753. REPAIRED SEAT TRACK BETWEEN BS 632 TO BS 753 IAW B767 SRM 53-00-52.
- [SDR USAA20091110BB152](https://openairdocs.org/sdr/USAA20091110BB152), Nov 9, 2009: DOOR LATCH. OUT OF SEQUENCE. PHL - THE L1 DOOR DOES NOT LOCK IN THE OPEN POSITION. FOUND L1 DOOR TO BE OUT OF PROPER SEQUENCE. ONCE DOOR IN PROPER SEQUENCE, OPERATION WAS NORMAL.
- [SDR USAA20091105BB151](https://openairdocs.org/sdr/USAA20091105BB151), Nov 4, 2009: SOCKET. DEFECTIVE. CLT - RIGHT AFT EXIT EMERGENCY LIGHT WAS INOPERATIVE. REMOVED AND REPLACED SOCKET / REFLECTOR OF LIGHT ASSEMBLY.
- [SDR USAA20090721BB115](https://openairdocs.org/sdr/USAA20090721BB115), Jul 20, 2009: WARNING SYSTEM. MALFUNCTIONED. CLT FLT 719 EN-ROUTE PHL TO CLT. EICAS MESSAGE "GEAR DISAGREE" DISPLAYED AND GEAR AMBER LIGHT ILLUMINATED WITH GREEN GEAR DOWN LIGHTS ILLUMINATED. THE AIRCRAFT 

All 68: https://openairdocs.org/deregistered/N245AY-2018-03-12/reports.md

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