# N182AW: 1981 Boeing 737-277, registration cancelled 2005-03-09

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: March 9, 2005
- 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: 22649
- Year built: 1981
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 16, 1986
- Certificate issued: December 16, 1986
- Last registry action: August 4, 2003
- Mode S code: A1482F
- 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/N182AW
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=182AW
- Page: https://openairdocs.org/deregistered/N182AW-2005-03-09

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 (167, newest 50)

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

- [SDR AWXA200401179](https://openairdocs.org/sdr/AWXA200401179), Oct 30, 2004: LIGHT. INOPERATIVE. FLIGHT CREW REPORTED R-2 DOOR EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED R-2 DOOR EMERGENCY EXIT LIGHT ASSEMBLY, OPERATIONAL CHECK W
- [SDR AWXA200401089](https://openairdocs.org/sdr/AWXA200401089), Oct 4, 2004: BRAKE. SEIZED. ABORTED TAKEOFF, FLT 0109, ON TAKEOFF, EN ROUTE WHEN APPROACHING V1 THE AIRCRAFT NOSE STARTED TO ROTATE ON ITS OWN, LOWERED NOSE AND REJECTED TAKEOFF AT 138 KTS
- [SDR AWXA200401011](https://openairdocs.org/sdr/AWXA200401011), Sep 10, 2004: PACKING. TORN. EN ROUTE, NR 1 ENG SHUTDOWN AT 27,000 FT, ATTEMPTED RESTART WITHOUT SUCCESS, DECLARED EMERGENCY & LANDED WITHOUT FURTHER EVENT. MX FOUND SEALS ON PRESS DUMP VAL
- [SDR AWXA200401022](https://openairdocs.org/sdr/AWXA200401022), Sep 8, 2004: SKIN. CRACKED. DURING 4-DAY CHECK, A 1 1/2 INCH CRACK WAS FOUND IN FUSELAGE SKIN AT BS 727A, STR 16 RT. MAINTENANCE REMOVED EXISTING REPAIR, CUTOUT DAMAGED AREA OF SKIN AT BS 
- [SDR AWXA200400886](https://openairdocs.org/sdr/AWXA200400886), Aug 13, 2004: MOTOR. BINDING. ON CLIMB-OUT OF PHX EN ROUTE FOR SJC AT APPROXIMATELY 3000 FT, FLIGHT CONTROLS SHOOK VIOLENTLY FROM SIDE TO SIDE AS IF IN SEVERE TURBULENCE. NOTICED FEEL DIFFER
- [SDR AWXA200400816](https://openairdocs.org/sdr/AWXA200400816), Jul 24, 2004: POWER SUPPLY. DISCHARGED. PHX - EEL - DURING INSPECTION THE EMERGENCY LIGHTS SEAT ROW 15 LEFT AND AFT WERE FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPL
- [SDR AWXA200400815](https://openairdocs.org/sdr/AWXA200400815), Jul 24, 2004: LIGHT. FAILED. PHX - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 9 LT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIG
- [SDR AWXA200400802](https://openairdocs.org/sdr/AWXA200400802), Jul 20, 2004: WARNING LIGHT. FALSE INDICATION. FALSE FIRE WARNING ON CLIMB OUT, AFTER SELECTING FLAPS UP RECEIVED FWD CARGO FIRE LIGHT AND FIRE BELL, DISCHARGED NR 1 CARGO FIRE BOTTLE AND LIGHT EXTINGUISHED,
- [SDR AWXA200400636](https://openairdocs.org/sdr/AWXA200400636), Jun 13, 2004: SOCKET. SHORTED. PHX - EMERGENCY LANDING - FLT 0628 - ON DESCENT INTO PHX EN ROUTE FROM OAK AT FL 120 EXPERIENCED AN ELECTRICAL BURNING ODOR FOLLOWED BY SMOKE IN COCKPIT, DONNED
- [SDR AWXA200400344](https://openairdocs.org/sdr/AWXA200400344), Apr 2, 2004: HYDRAULIC LINE. RUPTURED. SAT - AIR TURNBACK - FLT 0679 - ON CLIMBOUT OF SAT EN ROUTE FOR PHX LOST A-HYDRAULIC SYSTEM, FOLLOWED QRH AND TURNED BACK TO SAT. MAINTENANCE REMOVED AND REPLAC
- [SDR AWXA200400354](https://openairdocs.org/sdr/AWXA200400354), Mar 30, 2004: SKIN. CRACKED. PHX - MAJOR REPAIR - A .25 INCH CRACK WAS FOUND IN FUSELAGE SKIN LT SIDE AT LAP SEAM BETWEEN WINDOWS 11 & 12, BS 540, STR 14 LEFT. MAINTENANCE CUT OUT DAMAGED S
- [SDR AWXA200400179](https://openairdocs.org/sdr/AWXA200400179), Feb 14, 2004: WIRE. BROKEN. DURING INSPECTION A BROKEN WIRE WAS FOUND ON THE EMERGENCY ESCAPE PATH LIGHT SEAT ROW 17 LT. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT AS
- [SDR AWXA200301385](https://openairdocs.org/sdr/AWXA200301385), Nov 6, 2003: BRACKET. CRACKED. MCN - MAJOR REPAIR - DURING C-21 CHECK A .375 INCH CRACK WAS FOUND IN A BRACKET AT BS 334, LBL 56, WL 206. MAINTENANCE REMOVED THE CRACKED BRACKET AT BS 334, LB
- [SDR AWXA200301389](https://openairdocs.org/sdr/AWXA200301389), Nov 2, 2003: TIE CLIP. CRACKED. MCN - MAJOR REPAIR - DURING C-21 CHECK A 1 .5 INCH CRACK WAS FOUND IN TIE CLIP BS 344-350, STR 16 LT. MAINTENANCE REMOVED THE CRACKED TIE CLIP BS 344-350, STR 1
- [SDR AWXA200301369](https://openairdocs.org/sdr/AWXA200301369), Nov 2, 2003: FLOORBEAM. CORRODED. DURING C-21 CHECK CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF UPPER T-CAP REPAIR AT BS 986.5, RBL 0.5 TO RBL 45. MAINTENANCE REMOVED UPPER T-CAP REPAIR AT
- [SDR AWXA200301422](https://openairdocs.org/sdr/AWXA200301422), Oct 30, 2003: WEB. CRACKED. DURING C-21 CHECK 2 EACH CRACKS WERE FOUND ON SHEAR WEB AT BS 344, AFT OF L-1 DOOR. MAINTENANCE REMOVED DAMAGED SHEAR WEB BS 344; FABRICATED A NEW REPLACEMENT S
- [SDR AWXA200301398](https://openairdocs.org/sdr/AWXA200301398), Oct 30, 2003: CLIP. CRACKED. MCN - MAJOR REPAIR - DURING C-21 CHECK A 1.5 INCH CRACK WAS FOUND IN RADIUS OF INTERCOSTAL CLIP ANGLE BS 344, STR 16 LT. MAINTENANCE REMOVED DAMAGED INTERCOSTAL
- [SDR AWXA200301397](https://openairdocs.org/sdr/AWXA200301397), Oct 30, 2003: FRAME. CRACKED. MCN - MAJOR REPAIR - DURING C-21 CHECK A 1.125 INCH CRACK WAS FOUND IN RADIUS OF FUSELAGE FRAME CHORD, AFT OF L-1 DOOR BS 344, STR 15 LT. MAINTENANCE REMOVED DA
- [SDR AWXA200301392](https://openairdocs.org/sdr/AWXA200301392), Oct 30, 2003: ANGLE. CRACKED. MCN - MAJOR REPAIR - DURING C-21 CHECK A 1 INCH CRACK WAS FOUND IN CLIP ANGLE ON BOTTOM OF INTERCOSTAL AT STRINGER 16 LT, BS 344. MAINTENANCE REMOVED THE CRACKE
- [SDR AWXA200301391](https://openairdocs.org/sdr/AWXA200301391), Oct 30, 2003: ANGLE. CRACKED. MCN - MAJOR REPAIR - DURING C-21 CHECK A 1.125 INCH CRACK WAS FOUND IN CLIP ANGLE ON TOP OF INTERCOSTAL AT STRINGER 16 LT, BS 344. MAINTENANCE REMOVED THE CRACK
- [SDR AWXA200301390](https://openairdocs.org/sdr/AWXA200301390), Oct 30, 2003: ATTACH ANGLE. CRACKED. MCN - MAJOR REPAIR - DURING C-21 CHECK A 2.875 INCH CRACK WAS FOUND IN STRINGER 15 LT TO FRAME 344 ATTACH ANGLE. MAINTENANCE REMOVED THE CRACKED ATTACH ANGLE BS
- [SDR AWXA200301386](https://openairdocs.org/sdr/AWXA200301386), Oct 28, 2003: CLIP. CRACKED. MCN - MAJOR REPAIR - DURING C-21 CHECK A .375 INCH CRACK WAS FOUND IN FRAME ATTACH CLIP ON L-1 DOOR AFT FRAME AT NR 6 DOOR STOP BS 344, STR 16 LT. MAINTENANCE R
- [SDR AWXA200301365](https://openairdocs.org/sdr/AWXA200301365), Oct 27, 2003: FLOOR SUPPORT. CORRODED. DURING C-21 CHECK CORROSION WAS FOUND ON FLOOR SUPPORT AT BS 1003, LBL 38. MAINTENANCE REMOVED FLOOR SUPPORT FROM BS 986.5 TO BS 1006, LBL 38; FABRICATED A NEW 
- [SDR AWXA200301338](https://openairdocs.org/sdr/AWXA200301338), Oct 23, 2003: STRINGER CLIP. CRACKED. DURING C-21 CHECK A 1 INCH CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 380, STR 25 LT. MAINTENANCE REMOVED AND REPLACED STRINGER TIE CLIP AT BS 380, STR 25 LT IA
- [SDR AWXA200301399](https://openairdocs.org/sdr/AWXA200301399), Oct 22, 2003: FAIRING. CRACKED. MCN - MAJOR REPAIR - DURING C-21 CHECK A 2 INCH CRACK WAS FOUND ON NR 1 THRUST REVERSER LOWER DEFLECTOR DOOR LT FAIRING AT 2ND FASTENER HOLE FROM FORWARD END. M
- [SDR AWXA200301387](https://openairdocs.org/sdr/AWXA200301387), Oct 22, 2003: CLIP. CRACKED. MCN - MAJOR REPAIR - DURING C-21 CHECK A .375 INCH CRACK WAS FOUND IN FRAME ATTACH CLIP ON L-1 DOOR AFT FRAME AT NR 6 DOOR STOP BS 344, STR 16 LT. MAINTENANCE R
- [SDR AWXA200301370](https://openairdocs.org/sdr/AWXA200301370), Oct 22, 2003: FLOORBEAM. CORRODED. MCN - MAJOR REPAIR - DURING C-21 CHECK CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF UPPER T-CAP REPAIR AT BS 967, RBL 10 TO RBL 48. MAINTENANCE REMOVED UPP
- [SDR AWXA200301367](https://openairdocs.org/sdr/AWXA200301367), Oct 22, 2003: SPLICE. CORRODED. DURING C-21 CHECK CORROSION WAS FOUND ON LOWER SURFACE OF FLOOR ATTACH STRAP BS 771, STR 26 LT TO STR 26 RT. MAINTENANCE REMOVED DAMAGED FLOOR ATTACH STRAP BS 7
- [SDR AWXA200301364](https://openairdocs.org/sdr/AWXA200301364), Oct 22, 2003: FLOORBEAM. CORRODED. DURING C-21 CHECK CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF FLOORBEAM UPPER AFT LEG AT BS 947 FROM RBL 5 TO LBL 53. MAINTENANCE CUT OUT DAMAGED FLOORBEA
- [SDR AWXA200301342](https://openairdocs.org/sdr/AWXA200301342), Oct 22, 2003: TAIL CONE. DELAMINATED. MCN - MINOR REPAIR - DURING C-21 CHECK THE TAIL CONE WAS FOUND DELAMINATED AT LOWER CENTER 7 INCHES, 11 INCHES, & 24 INCHES FROM FORWARD END, 7.5 INCHES LT LOWE
- [SDR AWXA200301419](https://openairdocs.org/sdr/AWXA200301419), Oct 21, 2003: WEB. CRACKED. MCN - MAJOR REPAIR - DURING C-21 CHECK A 1 INCH CRACK WAS FOUND ON SHEAR WEB AT FORWARD INBOARD SIDE END OF CREASE BEAM BS 995.5, LBL 43.5. MAINTENANCE REMOVED 
- [SDR AWXA200301418](https://openairdocs.org/sdr/AWXA200301418), Oct 21, 2003: CLIP. CRACKED. MCN - MINOR REPAIR - DURING C-21 CHECK A .25 INCH CRACK WAS FOUND ON L-ANGLE CLIP AT UPPER AFT END OF NR 2 ENGINE COWLING. MAINTENANCE REMOVED CRACKED L-ANGLE C
- [SDR AWXA200301388](https://openairdocs.org/sdr/AWXA200301388), Oct 21, 2003: ANGLE. CORRODED. MCN - MAJOR REPAIR - DURING C-21 CHECK EXFOLIATION CORROSION WAS FOUND ON FORWARD CARGO COMPARTMENT FLOOR ZEE ANGLE AT BS 520, RBL 20. MAINTENANCE CUT OUT DAMAG
- [SDR AWXA200301366](https://openairdocs.org/sdr/AWXA200301366), Oct 21, 2003: WEB. CRACKED. DURING C-21 CHECK A 1 INCH CRACK WAS FOUND ON FORWARD END OF LT SHEAR WEB AT BS 995.5, LBL 43.5, AND EXFOLIATION CORROSION WAS FOUND ON LOWER SURFACE OF LT OUTB
- [SDR AWXA200301363](https://openairdocs.org/sdr/AWXA200301363), Oct 21, 2003: ANGLE. CRACKED. DURING C-21 CHECK A 1 INCH CRACK WAS FOUND ON ANGLE (CLIP) FORWARD SIDE OF BS 500B FRAME, ABOVE STR 26 LT. MAINTENANCE REMOVED CRACKED ANGLE FORWARD SIDE OF BS 
- [SDR AWXA200301343](https://openairdocs.org/sdr/AWXA200301343), Oct 21, 2003: INTERCOSTAL. CRACKED. MCN - MINOR REPAIR - DURING C-21 CHECK A .5 INCH CRACK WAS FOUND IN INTERCOSTAL AT BS 480, LBL 24. MAINTENANCE REMOVED INTERCOSTAL FROM BS 460 TO BS 480, LBL 24
- [SDR AWXA200301395](https://openairdocs.org/sdr/AWXA200301395), Oct 20, 2003: SKIN. CRACKED. MCN - MAJOR REPAIR - DURING C-21 CHECK A 1 .375 INCH CRACK WAS FOUND IN FUSELAGE SKIN AT FASTENER HOLE LOWER AFT CORNER OF L-1 DOOR, BS 344. MAINTENANCE CUTOUT 
- [SDR AWXA200301368](https://openairdocs.org/sdr/AWXA200301368), Oct 20, 2003: FRAME. CRACKED. DURING C-21 CHECK A .3125 INCH CRACK WAS FOUND ON AFT SIDE OF R-1 DOOR INBOARD OF THE 3RD AFT STOP FITTING FROM THE BOTTOM BS 327, STR 14 RT. MAINTENANCE CUT OU
- [SDR AWXA200301341](https://openairdocs.org/sdr/AWXA200301341), Oct 20, 2003: SLAT. DELAMINATED. MCN - MAJOR REPAIR - DURING C-21 CHECK THE NR 1 LEADING EDGE SLAT WAS FOUND DELAMINATED AT THE INBOARD UPPER SURFACE WS 510 TO WS 512 LT. MAINTENANCE CUT OUT DE
- [SDR AWXA200301396](https://openairdocs.org/sdr/AWXA200301396), Oct 19, 2003: SKIN. CRACKED. MCN - MAJOR REPAIR - DURING C-21 CHECK A .5 INCH CRACK WAS FOUND ON PREVIOUS REPAIR AT FASTENER HOLE OF LOWER FUSELAGE SKIN BS 454, RBL 3. MAINTENANCE TRIMMED O
- [SDR AWXA200301394](https://openairdocs.org/sdr/AWXA200301394), Oct 19, 2003: SKIN. CRACKED. MCN - MAJOR REPAIR - DURING C-21 CHECK A .75 INCH CRACK WAS FOUND IN FUSELAGE SKIN AT FASTENER HOLE ON FORWARD UPPER CORNER OF R-1 DOOR, BS 292.50. MAINTENANCE 
- [SDR AWXA200301030](https://openairdocs.org/sdr/AWXA200301030), Sep 7, 2003: CIRCUIT BREAKER. INOPERATIVE. ON APPROACH INTO PHX EN ROUTE FROM BUR AFTER LANDING GEAR EXTENSION THERE WAS NO LANDING GEAR DOWN AND LOCKED OR UNSAFE GEAR INDICATIONS, ABORTED APPROACH. FOUN
- [SDR AWXA200300995](https://openairdocs.org/sdr/AWXA200300995), Aug 27, 2003: LIGHT. BROKEN. FLIGHT CREW REPORTED THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 5 LT WAS BROKEN. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 5
- [SDR AWXA200300944](https://openairdocs.org/sdr/AWXA200300944), Aug 19, 2003: LIGHT. BROKEN. DURING 8-DAY CHECK THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 19 LT WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT AT SEAT 
- [SDR AWXA200300941](https://openairdocs.org/sdr/AWXA200300941), Aug 19, 2003: CONTROLLER. MALFUNCTIONED. ON INITIAL TAKEOFF ROLL EN ROUTE, THE CABIN CLIMB INDICATOR NEEDLE WENT TO RAPID RATE OF DESCENT OF ABOUT 4000 FPM, REJECTED TAKEOFF AND RETURNED TO GATE. MAINT
- [SDR AWXA200300812](https://openairdocs.org/sdr/AWXA200300812), Jul 18, 2003: BLEED VALVE. MALFUNCTIONED. DEN - ABORTED TAKEOFF - FLT 0640 - DURING TAKEOFF ROLL AT DEN EN ROUTE FOR PHX, A LOUD "BANG" CAME FROM THE NR 1 ENGINE, REJECTED TAKEOFF, SUSPECT COMPRESSOR ST
- [SDR AWXA200300550](https://openairdocs.org/sdr/AWXA200300550), May 16, 2003: TRANSMITTER. MALFUNCTIONED. PHX - ABORTED TAKEOFF - FLT 0445 - ON TAKEOFF ROLL AT PHX EN ROUTE FOR TUS, SETTING REDUCED FOR POWER 1.96, NR 2 ENGINE EPR DID NOT COME UP TO POWER, EPR STAGNA
- [SDR AWXA200300300](https://openairdocs.org/sdr/AWXA200300300), Mar 22, 2003: ENGINE. OUT OF TRIM. ON TAKEOFF AT PHX EN ROUTE FOR ONT WHEN SELECTING TAKEOFF POWER, TAKEOFF POWER WAS SET TO 2.11 EPR AND THE NR 2 ENGINE ONLY CAME UP TO 1.59 EPR. FURTHER ADVANCE
- [SDR AWXA200300273](https://openairdocs.org/sdr/AWXA200300273), Mar 16, 2003: BATTERY. DISCHARGED. FLIGHT CREW REPORTED THAT THE FORWARD EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY IN THE FORWARD EMERGENCY FLASHLIGHT, OP
- [SDR AWXA200300270](https://openairdocs.org/sdr/AWXA200300270), Mar 13, 2003: VANE. DAMAGED. WHEN PREPARING FOR TAKEOFF AT DFW EN ROUTE FOR PHX WHEN THROTTLES ADVANCED RECEIVED COMPRESSOR VANE FAULT. MAINTENANCE REMOVED AND REPLACED THE PRESSURE RATIO B

All 167: https://openairdocs.org/deregistered/N182AW-2005-03-09/reports.md

## FAA accident and incident reports (4)

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 20011001025579I](https://openairdocs.org/incident/20011001025579I), Oct 1, 2001: Boeing 737277 (N182AW), Wichita, KS. (-23) During takeoff roll at about 110 KTS, #2 engine oil pressure was 23 PSI. Aborted takeoff at 110 KTS and shut down #2 engine at taxi speed. Company…
- [Incident 19950818033479I](https://openairdocs.org/incident/19950818033479I), Aug 18, 1995: Boeing 737200 (N182AW), Columbus, OH, Minor damage. Rain hit windshield hard on landing obscured runway. Hydroplaned and wind gust lifted wing veered off and on runway
- [Incident 19921031048769I](https://openairdocs.org/incident/19921031048769I), Oct 31, 1992: Boeing 737277 (N182AW), Omaha, NE, Minor damage. Pilot missed assigned taxiway. Struck a light pole while attempting to turn around.
- [Incident 19890625036109I](https://openairdocs.org/incident/19890625036109I), Jun 25, 1989: Boeing 737277 (N182AW), Des Moines, IA, Minor damage. NR3 main tire lost tread on takeoff. Damaged a hydraulic system. Landed safely.

## Other aircraft with N182AW

- [Cancelled 2011-03-17](https://openairdocs.org/deregistered/N182AW-2011-03-17): Free Bird Innovations FREEBIRD CLASSIC, S/N 102. Assigned (non-type certificated), pending cancellation

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