# N180AW: 1981 Boeing 737-277, registration cancelled 2004-11-15

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: November 15, 2004
- Exported to: Mexico
- Status when cancelled: Triennial form not returned
- Airframe: [Boeing 737-277](https://openairdocs.org/model/boeing-737-277) (registry code 138447D)
- Engine: [Pratt & Whitney JT8D-15](https://openairdocs.org/engine/pratt-whitney-jt8d-15) (registry code 52051)
- Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE), [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs)
- Serial number: 22647
- Year built: 1981
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 10, 1986
- Certificate issued: December 10, 1986
- Last registry action: August 4, 2003
- Mode S code: A140C1
- Owner when cancelled: [Wilmington Trust Company Trustee](https://openairdocs.org/faa-owner/WILMINGTON%20TRUST%20COMPANY%20TRUSTEE)
- Location: [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington)
- Owner type: Corporation
- Owner's area on the map: 39.7357° N, 75.5321° W: Placed by OpenAirDocs: center of Wilmington, DE, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N180AW
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=180AW
- Page: https://openairdocs.org/deregistered/N180AW-2004-11-15

From the FAA registry file of October 29, 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 737-277: https://openairdocs.org/model/boeing-737-277.md

## Service difficulty reports (101, newest 50)

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

- [SDR AWXA200300908](https://openairdocs.org/sdr/AWXA200300908), Aug 11, 2003: BATTERY. DISCHARGED. PHX - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE FORWARD LOWER CABIN EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERIES IN
- [SDR AWXA200300369](https://openairdocs.org/sdr/AWXA200300369), Apr 14, 2003: LIGHT. BROKEN. PHX - EEL - FLIGHT CREW REPORTED THE EMERGENCY ESCAPE PATH LIGHT ON SEAT ROW 9 LT WAS BROKEN. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT O
- [SDR AWXA200300288](https://openairdocs.org/sdr/AWXA200300288), Mar 3, 2003: FRAME. CRACKED. DURING C-18 CHECK A 1 INCH CRACK WAS FOUND ON BS 178 BULKHEAD SIDE FRAME WL 207, RBL 24, JUST ABOVE FLIGHT COMPARTMENT FLOOR. MAINTENANCE REMOVED CRACKED BS 178
- [SDR AWXA200300295](https://openairdocs.org/sdr/AWXA200300295), Mar 1, 2003: STIFFENER. CRACKED. LCQ - MAJOR REPAIR - DURING C-18 CHECK A 1" CRACK WAS FOUND ON VERTICAL STIFFENER AT FORWARD BULKHEAD, AFT CARGO COMPARTMENT BILGE, BS 727, RBL 6. MAINTENANCE R
- [SDR AWXA200300285](https://openairdocs.org/sdr/AWXA200300285), Mar 1, 2003: SKIN. DAMAGED. DURING C-18 CHECK 4 SMALL CREASES WERE FOUND IN FUSELAGE SKIN AT BS 450, STR 26-27 RT. MAINTENANCE CUTOUT CREASED SKIN AT BS 450, STR 26-27 RT; FABRICATED A FIL
- [SDR AWXA200300287](https://openairdocs.org/sdr/AWXA200300287), Feb 26, 2003: BULKHEAD. CRACKED. DURING C-18 CHECK 2 EACH CRACKS WERE FOUND ON BS 178 BULKHEAD WEB AT WL 190, BL 0, UNDER VOR/LOC ANTENNA MOUNT. MAINTENANCE CUTOUT CRACKED BS 178 BULKHEAD WEB A
- [SDR AWXA200300139](https://openairdocs.org/sdr/AWXA200300139), Feb 13, 2003: LIGHT. SHORTED. SMOKE IN COCKPIT - FLT 0227 - DURING TAXI TO GATE IN PHX THE GLARE SHIELD FLUORESCENT LIGHTS BEGAN TO SMOKE, SHUT LIGHTS OFF SMOKE DISSIPATED. MAINTENANCE PERFO
- [SDR AWXA200300055](https://openairdocs.org/sdr/AWXA200300055), Jan 20, 2003: WIRE. BROKEN. TUS - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 19 L/H WAS FOUND INOPERATIVE. MAINTENANCE DISCOVERED A WIRE PULLED FROM SPLICE UNDER S
- [SDR AWXA200300286](https://openairdocs.org/sdr/AWXA200300286), Jan 17, 2003: PANEL. CRACKED. LCQ - MAJOR REPAIR - DURING C-18 CHECK A 2" CRACK WAS FOUND ON KEEL BEAM PANEL BETWEEN THE L/H AND R/H WHEEL WELLS BS 600 TO 724. MAINTENANCE REMOVED EXISTING D
- [SDR AWXA200200592](https://openairdocs.org/sdr/AWXA200200592), Jul 10, 2002: BATTERY. DISCHARGED. FORWARD EMERGENCY FLASHLIGHT INOPERATIVE, PLACED IN CHARGER BACKWARDS. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CH
- [SDR AWXA200200357](https://openairdocs.org/sdr/AWXA200200357), Apr 23, 2002: BATTERY. DISCHARGED. PHX - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED LOWER FLASHLIGHT IN AFT CABIN IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BATTERIES IN THE AFT CABIN LOWER
- [SDR AWXA200200235](https://openairdocs.org/sdr/AWXA200200235), Mar 19, 2002: WIRE. BROKEN. PHX - EEL - "C" - DURING INSPECTION OF EMERGENCY ESCAPE PATH LIGHTING A BROKEN WIRE WAS FOUND AT SEAT ROW 19 L/H. MAINTENANCE REPAIRED BROKEN WIRE FOR EMERGENCY
- [SDR AWXA200200116](https://openairdocs.org/sdr/AWXA200200116), Jan 30, 2002: TEE CHORD. CRACKED. MCN - MAJOR REPAIR - "C" - DURING C-20 CHECK A 1.3" CRACK WAS FOUND ON INBOARD OF SEAT TRACK ON UPPER TEE CHORD OF LONGITUDINAL BEAM BS 727B, RBL 44, WL 208. MA
- [SDR AWXA200200118](https://openairdocs.org/sdr/AWXA200200118), Jan 23, 2002: SKIN. GOUGED. MCN - MAJOR REPAIR - "C" - DURING C-20 CHECK A GOUGE .009 TO .027 DEEP X 7" LONG WAS FOUND ON THE #1 ENGINE AFT PYLON INBOARD SIDE SKIN JUST FORWARD OF THE FLIP
- [SDR AWXA200200117](https://openairdocs.org/sdr/AWXA200200117), Jan 23, 2002: SKIN. GOUGED. MCN - MAJOR REPAIR - "C" - DURING C-20 CHECK A GOUGE .015 DEEP X 3" LONG WAS FOUND ON THE #1 ENGINE AFT PYLON INBOARD SIDE SKIN JUST AFT OF THE FLIPPER DOOR. MA
- [SDR AWXA200200114](https://openairdocs.org/sdr/AWXA200200114), Jan 23, 2002: WEB. CRACKED. MCN - MAJOR REPAIR - "C" - DURING C-20 CHECK A 1/4" CRACK WAS FOUND ON FLOOR BEAM WEB BS 714, RBL 25. MAINTENANCE TRIMMED OUT DAMAGED SECTION OF FLOOR BEAM AT B
- [SDR AWXA200200103](https://openairdocs.org/sdr/AWXA200200103), Jan 23, 2002: WEB. CRACKED. MCN - MAJOR REPAIR - "C" - DURING C-20 CHECK A CRACK WAS FOUND ON FLOOR BEAM WEB AT BS 714, RBL 25. MAINTENANCE REMOVED DAMAGED AREA OF WEB AT BS 714, RBL 25, F
- [SDR AWXA200200115](https://openairdocs.org/sdr/AWXA200200115), Jan 22, 2002: SKIN. GOUGED. MCN - MAJOR REPAIR - "C" - DURING C-20 CHECK A GOUGE WAS FOUND ON INNER SKIN AT FRAME TORQUE TUBE BOX OF THE L1 DOOR BS 305, STR 11-12, IN ADDITION TWO EXISTING
- [SDR AWXA200200102](https://openairdocs.org/sdr/AWXA200200102), Jan 21, 2002: SKIN. CRACKED. MCN - MAJOR REPAIR - "C" - DURING C-20 CHECK A CRACK WAS FOUND ON THE UPPER HINGE CUTOUT OF THE L1 DOOR AT UPPER CORNER BS 300. MAINTENANCE STOP DRILLED CRACK A
- [SDR AWXA200200080](https://openairdocs.org/sdr/AWXA200200080), Jan 21, 2002: SKIN. CRACKED. MCN - MAJOR REPAIR - "C" - DURING C-20 CHECK A CRACK WAS FOUND ON L1 DOOR UPPER HINGE CUTOUT AT UPPER CORNER BS 319.5. MAINTENANCE STOP DRILLED THE CRACK AND PE
- [SDR AWXA0001319](https://openairdocs.org/sdr/AWXA0001319), Feb 9, 2001: FITTING. CORRODED. RT HORIZ STAB REAR SPAR UPPER ATTACH FITTING CORRODED. BLENDED CORROSION IAW ER 15-5510-01027-ES2.
- [SDR AWXA0001313](https://openairdocs.org/sdr/AWXA0001313), Feb 9, 2001: FITTING. CORRODED. RT AFT VERT STAB I/B (FAILSAFE) LUG CORRODED/GOUGED ON ID AND CORRODED/GOUGED ON FWD FACE. LOCALLY BLENDED GOUGE AREAS IAW ER 15-5510-01023-JS3.
- [SDR AWXA0001312](https://openairdocs.org/sdr/AWXA0001312), Feb 9, 2001: FITTING. CORRODED. LT AFT VERT STAB I/B (FAILSAFE) LUG GOUGED IN ID AND CORRODED ON FWD FACE. LOCALLY BLENDED GOUGED AREAS OF LUG FWD SPOT FACE AREA IAW ER 15-5510-0123-JS3.
- [SDR AWXA0001323](https://openairdocs.org/sdr/AWXA0001323), Feb 9, 2001: BULKHEAD. CHAFED. NR 2 PYLON O/B STRUCTURE CHAFED AT FWD END ABOVE ENGINE. REMOVED BLKHEAD; LOCATED, DRILLED AND INSTALLED NEW BLKHEAD (P/N 65-79415-92) IAW SRM 51-30-02.
- [SDR AWXA0001322](https://openairdocs.org/sdr/AWXA0001322), Feb 9, 2001: FITTING. CORRODED. VERT STAB REAR LUGS, RT AFT O/B LUG HAS CORROSION ON ID OF BORE. REAMED LUG IAW BAC DWG 65C22124-10 AND EO 55-50-01; HFEC INDICATES NO DEFECTS NOTED.
- [SDR AWXA0001321](https://openairdocs.org/sdr/AWXA0001321), Feb 9, 2001: FITTING. GOUGED. LT HORIZ STAB REAR SPAR UPPER ATTACH LUG AFT SIDE FACE GOUGED. BLENDED GOUGE IAW ER 15-5510-01027-ES2.
- [SDR AWXA0001320](https://openairdocs.org/sdr/AWXA0001320), Feb 9, 2001: FITTING. GOUGED. LT HORIZ STAB CENTER SECTION LUGS, LT REAR, AFT SIDE OF MID LUG HAS GOUGES AND NICKS ON AFT SIDE OF LUG. BLENDED NICKS AND GOUGES IAW ER 15-5510-01027-SS4.
- [SDR AWXA0001318](https://openairdocs.org/sdr/AWXA0001318), Feb 9, 2001: FITTING. GOUGED. LT HORIZ STAB FWD SPAR UPPER ATTACH LUG FWD FACE GOUGED. BLENDED GOUGE IAW ER 15-5510-01027-ES2.
- [SDR AWXA0001317](https://openairdocs.org/sdr/AWXA0001317), Feb 9, 2001: FITTING. GOUGED. LT HORIZ STAB FWD LWR LUG HAS A GOUGE ON THE FWD SIDE OF SPOT FACE. BLENDED GOUGE IAW ER 15-5510-01027-ES2.
- [SDR AWXA0001316](https://openairdocs.org/sdr/AWXA0001316), Feb 9, 2001: FITTING. GOUGED. RT HORIZ STAB AFT SPAR MID ATTACH AFT FACE GOUGED. BLENDED GOUGE IAW ER 15-5510-01027-ES1.
- [SDR AWXA0001314](https://openairdocs.org/sdr/AWXA0001314), Feb 9, 2001: FITTING. GOUGED. RT HORIZ STAB AFT SPAR UPPER ATTACH LUG AFT FACE GOUGED. BLENDED GOUGE IAW ER 15-5510-01027-ES1.
- [SDR AWXA0001311](https://openairdocs.org/sdr/AWXA0001311), Feb 9, 2001: BEAM. CRACKED. HFEC INDICATES A 2 INCH CRACK AT I/B SIDE OF VERTICAL CHORD ON AFT SIDE OF FS 178 BLKHEAD BETWEEN WL 183 AND 185 LBL 5.7. REPAIRED I/B SIDE OF VERTICAL CHORD ON
- [SDR AWXA0001310](https://openairdocs.org/sdr/AWXA0001310), Feb 9, 2001: FLOORBEAM. CRACKED. CABIN FLOORBEAM UPPER CHORD FWD FACE HAS A CRACK IN RADIUS EXTENDING BEYOND STOP DRILL FS 526 RBL 24.75. REPAIRED FLOORBEAM UPPER CHORD IAW BOEING MESSAGE CPZ-M
- [SDR AWXA0001309](https://openairdocs.org/sdr/AWXA0001309), Feb 9, 2001: SKIN. GOUGED. GOUGED AREA ON RT AFT UPPER FUSELAGE SKIN BETWEEN STA 807 AND 827 APPROX 50 INCHES ABOVE WINDOW. REMOVED DAMAGED SKIN; FABED, TREATED FILLER AND DOUBLER; DRILLE
- [SDR AWXA0001308](https://openairdocs.org/sdr/AWXA0001308), Feb 9, 2001: BULKHEAD. CRACKED. ULTRASONIC INSPECTION REVEALED CRACK INDICATION AT FS 178 BULKHEAD WEB BENEATH STRAP AT RBL 7 TO RBL 15 WL 218. REMOVED STIFFENERS, BRACKETS AND ANGLES; LOCATED
- [SDR AWXA0001307](https://openairdocs.org/sdr/AWXA0001307), Feb 9, 2001: BULKHEAD. CRACKED. HFEC INDICATES A .200 INCH LONG CRACK EMINATING FROM FASTENER HOLE AT BLKHD FS 178 RBL 12.75 WL 234. REMOVED STIFFENERS, BRACKETS AND ANGLES; FABED, DRILLED, TR
- [SDR AWXA0001306](https://openairdocs.org/sdr/AWXA0001306), Feb 9, 2001: FLOORBEAM. CORRODED. CORROSION ON FLOOR SUPPORT FWD OF LT LAV WASTE EXIT AND FLOORBEAM AT FS 1006 FOUND TO BE OUT OF LIMITS IAW B737-200 SRM 53-10-6. REMOVED CORROSION ON SUPPORT AN
- [SDR AWXA0001305](https://openairdocs.org/sdr/AWXA0001305), Feb 8, 2001: RIB. CHAFED. AREA OF DEEP CHAFING ON VERT STAB FWD LWR END CAP RIB. REMOVED FWD LWR END CAP AND REPLACED WITH A NEW PART IAW SRM 53-10-11 AND 51-30-2.
- [SDR AWXA0001304](https://openairdocs.org/sdr/AWXA0001304), Feb 8, 2001: FLOORBEAM. CORRODED. FLOORBEAM TOP CAP AT BS 294.5 RBL 41 FOUND TO BE OUT OF LIMITS AFTER CORROSION CLEAN UP IAW SRM 53-10-01. REPAIRED FLOORBEAM UPPER CHORD IAW SRM 53-10-02 FIG 7 
- [SDR AWXA0001303](https://openairdocs.org/sdr/AWXA0001303), Feb 8, 2001: BULKHEAD. CRACKED. ULTRASONIC INSPECTION REVEALED CRACK INDICATION AT FS 178 BLKHEAD BENEATH STRAP FROM LBL 5 TO LBL 8 WL 217 IN WEB. REMOVED STIFFENERS, BRACKETS AND ANGLES AT FS
- [SDR AWXA0001302](https://openairdocs.org/sdr/AWXA0001302), Feb 8, 2001: ANGLE. CRACKED. LEFT WING O/B HINGED FLAP TRACK ATTACH ANGLE CRACKED. REMOVED ANGLE; FABED, TREATED AND PRIMED IAW SRM 51-20-1 AND 51-10-2; INSTALLED ANGLE IAW SRM 51-30-2.
- [SDR AWXA0001301](https://openairdocs.org/sdr/AWXA0001301), Feb 8, 2001: BULKHEAD. CRACKED. ULTRASONIC INSPECTION REVEALED CRACK INDICATION AT FS 178 BLKHEAD WEB BENEATH STRAP AT LBL 6 WL 230 TO 233. REMOVED STIFFENERS, BRACKETS AND ANGLES; LOCATED, DR
- [SDR AWXA0001300](https://openairdocs.org/sdr/AWXA0001300), Feb 8, 2001: FLOORBEAM. CORRODED. CORROSION ON UPPER SURFACE OF FLOORBEAM AT FS 312 RBL 8 TO RBL 10; OUT OF LIMITS IAW B737-200 SRM 53-16-1 PG 7. REPAIRED FLOORBEAM IAW B737-200 SRM 53-10-9.
- [SDR AWXA0001299](https://openairdocs.org/sdr/AWXA0001299), Feb 8, 2001: STRINGER. CORRODED. STR 27L IS CORRODED OUT OF LIMITS IAW B737-200 SRM 53-20-2, FROM FS 1016 TO FS 986. REMOVED CORRODED SECTION; FABED AND TREATED REPAIR PARTS; INSTALLED NEW SECT
- [SDR AWXA0001298](https://openairdocs.org/sdr/AWXA0001298), Feb 8, 2001: FLOORBEAM. CRACKED. UPPER CHORD, FWD FACE OF FLOORBEAM AT BS 520 HAS A CRACK EXTENDING THROUGH PREVIOUS STOP DRILL. REMOVED PREVIOUS REPAIR; CUT OUT PREVIOUS REPAIR; FABED DOUBLERS
- [SDR AWXA0000774](https://openairdocs.org/sdr/AWXA0000774), Oct 13, 2000: LIGHT. BURNED OUT. ON TAKEOFF MULTIPLE LIGHTS ILLUMINATED. TROUBLESHOT WITH MAINT CONTROL TO CONTINUE TO LAS. PUSHED WINDSHEAR INOP LIGHT EXTINGUISHED ON GROUND IN LAS. SMELLED EL
- [SDR AWXA0000446](https://openairdocs.org/sdr/AWXA0000446), Jul 7, 2000: CONTROLLER. MALFUNCTIONED. COULD NOT CONTROL PRESSURIZATION CLIMBING FROM FL 300 TO 310, O2 MASK DID NOT DEPLOY, NO EMERGENCY CALLED. NO CORRECTIVE ACTION IN SCEPTRE AT THIS TIME.
- [SDR AWXA0000373](https://openairdocs.org/sdr/AWXA0000373), Jun 6, 2000: CONTROLLER. MALFUNCTIONED. AIR TURNBACK, 1ST EVENT-- AFTER T/O, BLEEDS OFF, COULD NOT GET NR 2 ENG BLEED TO COME ON. ALSO, CABIN CLIMBING WITH THE A/C. REPLACED NR 2 BLEED AIR SHUT-OFF VA
- [SDR AWXA0000348](https://openairdocs.org/sdr/AWXA0000348), May 30, 2000: TUBE. CHAFED. NR 2 ENGINE LOST OIL QUANTITY AND PRESSURE, ENGINE SHUT DOWN. TROUBLESHOT SYS, FOUND CHAFED OIL COOLER INLET LINE. REPLACED LINE, LEAK AND OPS CHECK GOOD. RECOM
- [SDR AWXA9900498](https://openairdocs.org/sdr/AWXA9900498), Dec 27, 1999: POWER SUPPLY. INOPERATIVE. LEFT AND RIGHT FWD EMERGENCY EXIT DOOR LIGHTS AND CEILING LIGHT STARTED FLASHING AFTER 1 MINUTE. REPLACED FWD BATTERY PACK AND POWER SUPPLY, OPS CK GOOD.

All 101: https://openairdocs.org/deregistered/N180AW-2004-11-15/reports.md

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 19911124055419I](https://openairdocs.org/incident/19911124055419I), Nov 24, 1991: Boeing 737277 (N180AW), Kansas City, MO. Electrical smoke odor in cabin. Landed for maintenance. Gasper fan had failed and popped circuit breaker.

## Other aircraft with N180AW

- [Cancelled 2019-09-06](https://openairdocs.org/deregistered/N180AW-2019-09-06): Allied Drones AT28, S/N AT28-036-2.2. Registration expired, pending cancellation. Owner: [Unmanned Innovation Inc DBA](https://openairdocs.org/faa-owner/UNMANNED%20INNOVATION%20INC%20DBA), [San Francisco, CA](https://openairdocs.org/faa-place/CA/San%20Francisco)
- [Cancelled 2008-08-04](https://openairdocs.org/deregistered/N180AW-2008-08-04): Agusta AW139, S/N 41008, built 2008. Exported to Serbia. Owner: [Aero Toy Store LLC](https://openairdocs.org/faa-owner/AERO%20TOY%20STORE%20LLC), [Ft Lauderdale, FL](https://openairdocs.org/faa-place/FL/Ft%20Lauderdale)

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