# N183AW: 1984 Boeing 737-277, registration cancelled 2005-02-01

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: February 1, 2005
- Exported to: United Arab Emirates
- Status when cancelled: Valid registration
- 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: 22650
- Year built: 1984
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Special flight permit
- Airworthiness date: October 30, 2003
- Certificate issued: November 15, 2003
- Last registry action: June 15, 2004
- Mode S code: A14BE6
- Owner when cancelled: [Alameda Corp Trustee](https://openairdocs.org/faa-owner/ALAMEDA%20CORP%20TRUSTEE)
- Location: [San Antonio, TX](https://openairdocs.org/faa-place/TX/San%20Antonio)
- Owner type: Corporation
- Owner's area on the map: 29.5387° N, 98.4913° W: Placed by OpenAirDocs at the center of ZIP code 78216, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N183AW
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=183AW
- Page: https://openairdocs.org/deregistered/N183AW-2005-02-01

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 (129, newest 50)

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

- [SDR TSAA0171060](https://openairdocs.org/sdr/TSAA0171060), Aug 11, 2004: ENGINE. FALSE INDICATION. NON-ETOPS FLIGHT 64, HNL-ITO: ABORTED TAKEOFF DUE TO 4 THRUST LEVER SPLIT. WITH THE NR 1 LEVER FORWARD OF THE NR 2, THE NR 2 ENGINE INDICATES 2.0 EPR WHILE THE 
- [SDR AWXA200301206](https://openairdocs.org/sdr/AWXA200301206), Oct 11, 2003: PUMP. INOPERATIVE. ON CLIMB OUT OF PHX EN ROUTE FOR SJC LOST (A) SYS HYDS, TURNED BACK TO PHX & LANDED WITHOUT EVENT. MAINT R & R NR 2 EDP IAW T/C R5M29001. R & R (A) HYD SYS CASE
- [SDR AWXA200301086](https://openairdocs.org/sdr/AWXA200301086), Sep 22, 2003: WIRE. BROKEN. DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 13 LT WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE ON EMERGENCY ESCAPE PATH LIGHT AT 
- [SDR AWXA200301006](https://openairdocs.org/sdr/AWXA200301006), Sep 1, 2003: VALVE. BINDING. EN ROUTE FROM ONT TO PHX AT CRUISE RECEIVED HIGH OIL TEMPERATURE LIGHT, FOLLOWED QUICK REFERENCE HANDBOOK AND SHUTDOWN THE NO. 1 ENGINE, LANDED AT PHX WITHOUT F
- [SDR AWXA200300575](https://openairdocs.org/sdr/AWXA200300575), May 21, 2003: WIRE. BROKEN. DURING INSPECTION MAINTENANCE FOUND THE EMERGENCY ESCAPE PATH LIGHTS AT SEAT ROWS 14 AND 19 LT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAP
- [SDR AWXA200300217](https://openairdocs.org/sdr/AWXA200300217), Mar 2, 2003: INDICATOR. FAILED. ON CLIMB OUT FROM SLC EN ROUTE TO PHX THE CAPTAINS ATTITUDE DIRECTOR INDICATOR (ADI) "ATT" RED FLAG APPEARED, AND "PITCH" AND "ROLL" COMPARATOR LIGHTS ILLUMINAT
- [SDR AWXA20030021A](https://openairdocs.org/sdr/AWXA20030021A), Feb 27, 2003: TURBINE BLADES. FRACTURED. SLC - ABORTED TAKEOFF - FLT 0220 - ON TAKEOFF ROLL AT SLC EN ROUTE FOR PHX FELT STRONG VIBRATION FROM R/H SIDE OF AIRCRAFT AND IN R/H THRUST LEVER. ALL ENGINE I
- [SDR AWXA200300214](https://openairdocs.org/sdr/AWXA200300214), Feb 27, 2003: ENGINE. MALFUNCTIONED. ON TAKEOFF ROLL AT SLC EN ROUTE FOR PHX FELT STRONG VIBRATION FROM RT SIDE OF AIRCRAFT AND IN RT THRUST LEVER. ALL ENGINE INDICATIONS WERE NORMAL AT THIS POINT 
- [SDR AWXA200300099](https://openairdocs.org/sdr/AWXA200300099), Jan 31, 2003: ACTUATOR. WORN. SLC - AIR TURN BACK - ON CLIMB OUT FROM SLC EN ROUTE FOR PHX FLIGHT ATTENDANT REPORTED AN EXTREMELY LOUD NOISE AND VIBRATION IN FLOOR BOARDS OF AFT CABIN, TURNE
- [SDR AWXA200201229](https://openairdocs.org/sdr/AWXA200201229), Dec 17, 2002: WIRE. BROKEN. FLIGHT CREW REPORTED THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 16 LT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT ASSEMBL
- [SDR AWXA200201165](https://openairdocs.org/sdr/AWXA200201165), Dec 5, 2002: HYDRAULIC SYSTEM. LOW. AIR TURN BACK - FLT 0624 - SHORTLY AFTER TAKEOFF OBSERVED HYD QTY STARTING TO DROP, QUANTITY CONTINUED TO DROP TO 1.5 GALLONS. QUANTITY LEVEL WAS JUST ABOVE REF
- [SDR AWXA200200859](https://openairdocs.org/sdr/AWXA200200859), Sep 3, 2002: BATTERY PACK. DISCHARGED. PHX - EEL - DURING INSPECTION OF EMERGENCY LIGHT SYSTEM THE COCKPIT EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AT 
- [SDR AWXA200200824](https://openairdocs.org/sdr/AWXA200200824), Aug 20, 2002: WEB. CRACKED. MCN - MAJOR REPAIR - DURING C-18 CHECK A 2" CRACK WAS FOUND ON TORQUE BOX WEB AT BS 1138 L/H. MAINTENANCE CUTOUT DAMAGE AT TORQUE BOX WEB, FABRICATED A REPAIR D
- [SDR AWXA200200806](https://openairdocs.org/sdr/AWXA200200806), Aug 15, 2002: INTERCOSTAL. CRACKED. MCN - MAJOR REPAIR - DURING C-18 CHECK A .5 INCH CRACK WAS FOUND ON INTERCOSTAL IN THE AFT CARGO COMPARTMENT AT BS 800, RBL 43, WL 164. MAINTENANCE REMOVED DAMA
- [SDR AWXA200200831](https://openairdocs.org/sdr/AWXA200200831), Aug 12, 2002: FLOORBEAM. CRACKED. MCN - MAJOR REPAIR - DURING C-18 CHECK A .75 INCH CRACK WAS FOUND IN THE UPPER FLANGE OF LONGITUDINAL FLOORBEAM AT RBL 45 APPROXIMATELY 2 INCHES FROM BS 727B, W
- [SDR AWXA200200795](https://openairdocs.org/sdr/AWXA200200795), Aug 12, 2002: FRAME. CRACKED. MCN - MAJOR REPAIR - DURING C-18 CHECK A 3/4" CRACK WAS FOUND ON THE R-1 DOOR FRAME AT INBOARD LOWER END, BS 300, RBL 55. MAINTENANCE REMOVED DAMAGED SECTION OF
- [SDR AWXA200200820](https://openairdocs.org/sdr/AWXA200200820), Aug 10, 2002: WEB. CRACKED. MCN - MAJOR REPAIR - DURING C-18 CHECK HFEC INSPECTION INDICATED A 7/8" CRACK ON VERTICAL PRESSURE BEAM AT BS 663, RBL 32, WL 199. MAINTENANCE TRIMMED OUT DAMAG
- [SDR AWXA200200770](https://openairdocs.org/sdr/AWXA200200770), Aug 10, 2002: STRINGER. CORRODED. MCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND ON THE UPPER AFT END OF STRINGER 26 R/H, BS 380 (E&E COMPARTMENT). MAINTENANCE REMOVED 1 EACH STRINGE
- [SDR AWXA200200805](https://openairdocs.org/sdr/AWXA200200805), Aug 7, 2002: WEB. CRACKED. MCN - MAJOR REPAIR - DURING C-18 CHECK A .5 INCH CRACK WAS FOUND ON R-2 DOOR INTERCOSTAL WEB AT BS 954, WL 252. MAINTENANCE REMOVED 3 STRAPS AND CRACKED INTERCO
- [SDR AWXA200200803](https://openairdocs.org/sdr/AWXA200200803), Aug 6, 2002: ANGLE. CRACKED. MCN - MAJOR REPAIR - DURING C-18 CHECK A 1/2" CRACK WAS FOUND ON TOP OF CABIN FLOOR BEAM SUPPORT ANGLE BS 344, LBL 12, WL 206. MAINTENANCE REMOVED DAMAGED FLOOR
- [SDR AWXA200200823](https://openairdocs.org/sdr/AWXA200200823), Aug 5, 2002: SHEAR TIE. CORRODED. MCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND ON THE AFT CARGO PIT FLOOR FRAME ON TOP OF THE FORWARD LEG OUTBOARD SIDE, INBOARD OF STR 27 L/H, WL 1
- [SDR AWXA200200822](https://openairdocs.org/sdr/AWXA200200822), Aug 5, 2002: STRINGER. CORRODED. MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON CENTER INBOARD SIDE OF STRINGER 22 L/H, AFT OF DOME PLATE NUT AND ABOVE EMERGENCY LIGH
- [SDR AWXA200200821](https://openairdocs.org/sdr/AWXA200200821), Aug 3, 2002: SKIN. CRACKED. MCN - MAJOR REPAIR - DURING C-18 CHECK A 1/16" CRACK WAS FOUND ON EXTERNAL FUSELAGE SKIN EXTENDING FROM FASTENER HOLE AT BS 303, STR 17 R/H, WL 210. MAINTENANCE
- [SDR AWXA200200819](https://openairdocs.org/sdr/AWXA200200819), Aug 3, 2002: FLOORBEAM. CORRODED. MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION WAS FOUND ON THE UPPER SURFACE OF TEE CHORD AT BS 986, LBL 21 TO RBL 40, WL 208. MAINTENANCE BLENDED DAMAGED 
- [SDR AWXA200200765](https://openairdocs.org/sdr/AWXA200200765), Aug 3, 2002: FLOORBEAM. CORRODED. MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON THE UPPER SURFACE OF TEE CHORD BS 967, RBL 27 - 41, WL 208. MAINTENANCE BLENDED OUT CO
- [SDR AWXA200200802](https://openairdocs.org/sdr/AWXA200200802), Aug 2, 2002: FLOORBEAM. CRACKED. MCN - MAJOR REPAIR - DURING C-18 CHECK A 2.7 INCH CRACK WAS FOUND ON THE LOWER SIDE OF FLOORBEAM UPPER CHORD AT BS 663, RBL 24, WL 202; VERIFIED BY HFEC INSPECT
- [SDR AWXA200200767](https://openairdocs.org/sdr/AWXA200200767), Aug 2, 2002: STRINGER. CORRODED. MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON BOTH SIDES OF STRINGER 26 R/H BETWEEN BS 887 AND BS 927. MAINTENANCE BLENDED OUT CORRO
- [SDR AWXA200200834](https://openairdocs.org/sdr/AWXA200200834), Aug 1, 2002: FRAME. CRACKED. MCN - MAJOR REPAIR - DURING C-18 CHECK A 1/2" CRACK WAS FOUND IN THE AFT CARGO DOORWAY FORWARD DOOR CUTOUT FRAME BS 827, RBL 43, WL 164. MAINTENANCE REMOVED THE
- [SDR AWXA200200796](https://openairdocs.org/sdr/AWXA200200796), Aug 1, 2002: WEB. CRACKED. MCN - MAJOR REPAIR - DURING C-18 CHECK A .5 INCH CRACK WAS FOUND IN CLOSE OUT WEB AT BS 1005, RBL 43, CORROSION WAS ALSO FOUND ON LOWER SIDE OF SAME WEB AT RBL 
- [SDR AWXA200200768](https://openairdocs.org/sdr/AWXA200200768), Aug 1, 2002: INTERCOSTAL. CRACKED. MCN - MAJOR REPAIR - DURING C-18 CHECK A .5 INCH CRACK WAS FOUND ON INTERCOSTAL AT BS 500A, STRINGER 25 RT. MAINTENANCE REMOVED INTERCOSTAL FROM BS 500A, STRING
- [SDR AWXA200200848](https://openairdocs.org/sdr/AWXA200200848), Jul 31, 2002: WEB. CRACKED. MCN - MAJOR REPAIR - DURING C-18 CHECK A .25 INCH CRACK WAS FOUND IN THE FORWARD END OF LOWER WEB ON FORWARD CARGO DOOR BS 446, STR 23 RT. MAINTENANCE REMOVED C
- [SDR AWXA200200835](https://openairdocs.org/sdr/AWXA200200835), Jul 31, 2002: GUSSET. CRACKED. MCN - MAJOR REPAIR - DURING C-18 CHECK A 1" CRACK WAS FOUND ON GUSSET AT AFT END OF NOSE GEAR ACTUATOR SUPPORT FITTING BS 240, BL 0, WL 190. MAINTENANCE REMOVED
- [SDR AWXA200200804](https://openairdocs.org/sdr/AWXA200200804), Jul 31, 2002: SKIN. CRACKED. MCN - MAJOR REPAIR - DURING C-18 CHECK .25 INCH CRACKS WERE FOUND ON RT WING LEADING EDGE AT THE NR 6 SLAT CENTER STOP FITTING CUTOUT, WS 557. MAINTENANCE BLEND
- [SDR AWXA200200801](https://openairdocs.org/sdr/AWXA200200801), Jul 31, 2002: WEB. CRACKED. MCN - MAJOR REPAIR - DURING C-18 CHECK A 3/8" CRACK WAS FOUND ON THE NOSE LANDING GEAR ACTUATOR SUPPORT BEAM WEB EXTENDING FROM UPPER CENTER RIVET HOLE, HFEC IN
- [SDR AWXA200200791](https://openairdocs.org/sdr/AWXA200200791), Jul 31, 2002: DOOR FRAME. CRACKED. MCN - MAJOR REPAIR - DURING C-18 CHECK A .5 INCH CRACK WAS FOUND L-1 DOOR FRAME CUTOUT FORWARD LOWER STOP FITTING ATTACH PLATE WEB DOUBLER, BS 294.5, STR 16 LT.
- [SDR AWXA200200790](https://openairdocs.org/sdr/AWXA200200790), Jul 31, 2002: LONGERON. CRACKED. MCN - MAJOR REPAIR - DURING C-18 CHECK THE #1 ENGINE FIXED FAIRING LOWER END "Z" ANGLE WAS FOUND CRACKED BETWEEN 1ST AND 2ND ATTACH FITTINGS FROM THE FORWARD EN
- [SDR AWXA200200789](https://openairdocs.org/sdr/AWXA200200789), Jul 31, 2002: ANGLE. BROKEN. MCN - MAJOR REPAIR - DURING C-18 CHECK A "T" ANGLE CLIP WAS FOUND BROKEN ON INBOARD SIDE OF THE #1 ENGINE FIXED FAIRING BETWEEN 2ND AND 3RD ATTACH FITTINGS FROM
- [SDR AWXA200200788](https://openairdocs.org/sdr/AWXA200200788), Jul 31, 2002: ANGLE. BROKEN. MCN - MAJOR REPAIR - DURING C-18 CHECK A "T" ANGLE CLIP WAS FOUND BROKEN ON INBOARD SIDE OF THE #2 ENGINE FIXED FAIRING BETWEEN 2ND AND 3RD ATTACH FITTINGS FROM
- [SDR AWXA200200769](https://openairdocs.org/sdr/AWXA200200769), Jul 31, 2002: PLATE. CRACKED. MCN - MAJOR REPAIR - DURING C-18 CHECK A 1 INCH CRACK WAS FOUND ON AFT CARGO COMPARTMENT FORWARD CORNER SCUFF PLATE. MAINTENANCE PREPARED, TREATED, AND WELDED T
- [SDR AWXA200200764](https://openairdocs.org/sdr/AWXA200200764), Jul 31, 2002: SKIN. CRACKED. MCN - MAJOR REPAIR - DURING C-18 CHECK A 1/4" CRACK WAS FOUND ON L-1 DOOR INTERNAL SKIN AT THE AFT UPPER CORNER DOOR STOP ADJUSTMENT CUTOUT, BS 346. MAINTENANCE
- [SDR AWXA200200750](https://openairdocs.org/sdr/AWXA200200750), Jul 31, 2002: ANGLE. CRACKED. MCN - MAJOR REPAIR - DURING C-18 CHECK A 1" CRACK WAS FOUND ON FLOOR BEAM SUPPORT ANGLE BS 400, BL 0. MAINTENANCE REMOVED DAMAGED FLOOR BEAM SUPPORT ANGLE AT BS
- [SDR AWXA200201046](https://openairdocs.org/sdr/AWXA200201046), Jul 30, 2002: SKIN. DELAMINATED. MCN - MAJOR REPAIR - DURING C-18 CHECK THE R/H WING INBOARD FORE FLAP WAS FOUND TO HAVE DELAMINATION ON UPPER SKIN 6" INBOARD OF THE #3 FORE FLAP TRACK. MAINTEN
- [SDR AWXA200200766](https://openairdocs.org/sdr/AWXA200200766), Jul 30, 2002: SKIN. CRACKED. MCN - MAJOR REPAIR - DURING C-18 CHECK A 1/4" CRACK WAS FOUND ON R-1 DOOR EXTERNAL SKIN AT UPPER AFT CORNER OF HINGE CUTOUT, CONFIRMED BY HFEC INSPECTION. MAINT
- [SDR AWXA200200763](https://openairdocs.org/sdr/AWXA200200763), Jul 30, 2002: ATTACH ANGLE. CRACKED. MCN - MAJOR REPAIR - DURING C-18 CHECK A 1 1/2" CRACK WAS FOUND ON WEB UPPER CHORD (ATTACH ANGLE) AT FASTENER HOLES BS 500B TO BS 520, BL 0, WL 208.1. MAINTENAN
- [SDR AWXA200200619](https://openairdocs.org/sdr/AWXA200200619), Jul 15, 2002: FLASHLIGHT. DISCHARGED. FLIGHT CREW REPORTED THE EMERGENCY FLASHLIGHT AFT LT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT LT EMERGENCY FLASHLIGHT.
- [SDR AWXA200100597](https://openairdocs.org/sdr/AWXA200100597), Nov 14, 2001: STRAP. CRACKED. PHX - MAJOR REPAIR - "C" - CRACK FOUND ON FRAME RADIUS STRAP ON UPPER FLANGE ABOVE STRINGER 27R FOWARD PIT STA 492. MAINTENANCE REMOVED RADIUS STRAP FABRICATED 
- [SDR AWXA200100593](https://openairdocs.org/sdr/AWXA200100593), Nov 12, 2001: SKIN. CRACKED. PHX - MAJOR REPAIR - C - 9 CRACKS FOUND IN FUSELAGE SKIN .125 INCH LONG ORIGINATING FROM FASTENER HOLES ALONG STR 17L, STA 390 TO 415 VERIFIED BY HFEC. MAINTENA
- [SDR AWXA0002100](https://openairdocs.org/sdr/AWXA0002100), Aug 3, 2001: WEB. CRACKED. D: S-18A R/H shear beam web cracked.C: Replaced web 65-46877-82 per DWG 65-46877 - 76 INST. IAW SRM 51-10-1 page 8,9,10
- [SDR AWXA0002101](https://openairdocs.org/sdr/AWXA0002101), Aug 2, 2001: FLOOR SUPPORT. CORRODED. AFT CABIN - CORROSION ON FLOOR SUPPORT BEAMS BETWEEN STN 1000-1010 LBL 45. REPLACED BOTH FLOOR SUPPORT PER DRAW 65-46812 PART NUMBER 65-46812-87 AND 65-46812-91
- [SDR AWXA0002099](https://openairdocs.org/sdr/AWXA0002099), Aug 2, 2001: SEAT. CORRODED. D: Aft cabin R/H track F.STN.1006-1016 RBL 45 corroded.C: R/H floor track F.STN.1006-1016 RBL 45 DRAW 65C80735 - part no. 65C80735-115 and IAW SRM 51-10-1 Page 

All 129: https://openairdocs.org/deregistered/N183AW-2005-02-01/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 19891120060619I](https://openairdocs.org/incident/19891120060619I), Nov 20, 1989: Boeing 737277 (N183AW), Wichita, KS. NR2 engine oil filter bypass light on. Diverted to Wichita. Light went out on approach. No malfunction found.

## Other aircraft with N183AW

- [Cancelled 2019-09-06](https://openairdocs.org/deregistered/N183AW-2019-09-06): Allied Drones AT28, S/N AT28-037-2.2. 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)

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