# N184AW: 1987 Boeing 737-277, registration cancelled 2013-07-16

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: July 16, 2013
- Status when cancelled: Sale reported, canceled
- Airframe: [Boeing 737-277](https://openairdocs.org/model/boeing-737-277) (registry code 138447D)
- Engine: [Amateur-built UNKNOWN ENG](https://openairdocs.org/engine/amateur-built-unknown-eng) (registry code 99999)
- Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) (OpenAirDocs)
- Serial number: 22651
- Year built: 1987
- Type of aircraft: Fixed wing multi engine
- Airworthiness: Standard, normal
- Airworthiness date: February 5, 1987
- Last registry action: August 28, 2006
- Mode S code: A14F9D
- Location: [Miami, FL](https://openairdocs.org/faa-place/FL/Miami)
- Owner type: Individual
- Owner's area on the map: 25.6544° N, 80.4122° W: Placed by OpenAirDocs at the center of ZIP code 33186, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N184AW
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=184AW
- Page: https://openairdocs.org/deregistered/N184AW-2013-07-16

From the FAA registry file of October 28, 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 (134, newest 50)

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

- [SDR AWXA200400021](https://openairdocs.org/sdr/AWXA200400021), Jan 7, 2004: BEARING. SEIZED. AFTER LANDING & TAXING TO HOLD BAY, SHORTLY AFTER NR 2 ENG SHUTDOWN COCKPIT BEGAN TO DEVELOP AN ACRID ELEC BURNING ODOR FOLLOWED BY LIGHT BLUE SMOKEY HAZE. TURN
- [SDR AWXA200400024](https://openairdocs.org/sdr/AWXA200400024), Jan 4, 2004: WIRE. DAMAGED. ON CLIMBOUT, WHEN AUTOPILOT-B ENGAGED A/C BANKED HARD RT PAST 30 DEGREES. REATTEMPTED TO ENGAGE AUTOPILOT-B SAME RESULTS. AS SOON AS AUTOPILOT-B ENGAGED CONTROL
- [SDR AWXA200301095](https://openairdocs.org/sdr/AWXA200301095), Sep 23, 2003: LINE. LEAKING. DURING DECENT INTO DFW EN ROUTE FROM PHX (A) SYSTEM HYDRAULIC QUANTITY INDICATOR BEGAN SHOWING LOSS OF FLUID. FLUID LEVEL DROPPED TO APPROX .7500 OF A GAL REMAI
- [SDR AWXA200300721](https://openairdocs.org/sdr/AWXA200300721), Jun 20, 2003: PUMP. FAILED. ON DEPARTURE, LOST A-SYSTEM HYDRAULIC PRESSURE, TURNED BACK AND LANDED WITHOUT FURTHER EVENT. AIRCRAFT TOWED BACK TO GATE. MAINTENANCE FOUND THE NR 1 ENGINE DRI
- [SDR AWXA200300142](https://openairdocs.org/sdr/AWXA200300142), Feb 14, 2003: MODULE. FAILED. PHX - ABORTED TAKEOFF - FLT 0445 - ON TAKEOFF AT PHX EN ROUTE FOR TUS RECEIVED AMBER LEADING EDGE FLAP IN TRANSIT LIGHT ON FORWARD PANEL WHILE FLAPS SELECTED TO
- [SDR AWXA200201041](https://openairdocs.org/sdr/AWXA200201041), Oct 18, 2002: SIGN. BROKEN. DURING C-20 CHECK THE FORWARD SERVICE DOOR EMERGENCY EXIT SIGN WAS FOUND DAMAGED. MAINTENANCE REMOVED AND REPLACED THE FORWARD SERVICE DOOR EMERGENCY EXIT SIGN,
- [SDR AWXA200201031](https://openairdocs.org/sdr/AWXA200201031), Oct 15, 2002: DOOR FRAME. CORRODED. DURING C-20 CHECK CORROSION WAS FOUND AT THE L-1 DOOR SILL INNER CHORD UNDER DRAIN TROUGH BS 333, LBL 50. MAINTENANCE REMOVED 2 EACH ANGLES AT BS 312 AND 344, A
- [SDR AWXA200201030](https://openairdocs.org/sdr/AWXA200201030), Oct 15, 2002: STIFFENER. CRACKED. YVR - MAJOR REPAIR - DURING C-20 CHECK A 1/2" CRACK WAS FOUND ON AFT SIDE OF CABIN FLOOR BEAM INTERCOASTAL ATTACH ANGLE (STIFFENER) BS 328, LBL 47. MAINTENANCE 
- [SDR AWXA200201056](https://openairdocs.org/sdr/AWXA200201056), Oct 7, 2002: CREASE BEAM. CRACKED. DURING C-20 CHECK A 1/2 INCH CRACK WAS FOUND ON CREASE BEAM STRINGER 17 LT, BS 360 - BS 380. MAINTENANCE REMOVED WEBS BETWEEN BS 360 TO BS 400 AND BS 400 TO BS 
- [SDR AWXA200201027](https://openairdocs.org/sdr/AWXA200201027), Oct 4, 2002: SKIN. CRACKED. DURING C-20 CHECK A 1 1/2 INCH CRACK WAS FOUND ON FUSELAGE SKIN L-1 DOOR CUTOUT BELOW LOWER SCUFF PLATE, APPROXIMATELY 10 INCH FORWARD OF AFT LOWER CORNER BS 33
- [SDR AWXA200201026](https://openairdocs.org/sdr/AWXA200201026), Oct 4, 2002: FRAME. CRACKED. YVR - MAJOR REPAIR - DURING C-20 CHECK A 1/4" CRACK WAS FOUND ON FRAME AT BS 312, BETWEEN STR 5 - STR 6 L/H. MAINTENANCE STOP DRILLED CRACK AT BS 312, BETWEEN S
- [SDR AWXA200201025](https://openairdocs.org/sdr/AWXA200201025), Oct 4, 2002: ATTACH ANGLE. CRACKED. YVR - MAJOR REPAIR - DURING C-20 CHECK A 3/4" CRACK WAS FOUND ON ATTACH ANGLE AT BS 360, STR 11 L/H, JUST AFT OF L-1 DOOR. MAINTENANCE REMOVED THE DAMAGED ATTAC
- [SDR AWXA200201024](https://openairdocs.org/sdr/AWXA200201024), Oct 4, 2002: FLAP TRACK. CRACKED. DURING C-20 CHECK A 1/4 INCH CRACK WAS FOUND ON THE NR 7 FLAP TRACK AT THE INBOARD ROLLER OF UPPER TRACK, AFT END. MAINTENANCE REMOVED AND REPLACED THE DAMAGED 
- [SDR AWXA200201057](https://openairdocs.org/sdr/AWXA200201057), Oct 3, 2002: SKIN. CORRODED. YVR - MAJOR REPAIR - DURING C-20 CHECK PITTING CORROSION WAS FOUND ON THE L/H WING LOWER SKIN AT THE #2 TRAILING EDGE FLAP TRACK ATTACH POINT WS 254 L/H. MAINTE
- [SDR AWXA200201028](https://openairdocs.org/sdr/AWXA200201028), Oct 3, 2002: SKIN. CRACKED. YVR - MAJOR REPAIR - DURING C-20 CHECK A 1/4" CRACK WAS FOUND ON FUSELAGE SKIN OF R-2 DOOR UPPER HINGE CUTOUT AT FORWARD UPPER CORNER BS 957.5, WL 240. MAINTENA
- [SDR AWXA200200686](https://openairdocs.org/sdr/AWXA200200686), Jul 31, 2002: LIGHT. INOPERATIVE. LAS - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT WAS FOUND INOPERATIVE AT SEAT ROW 6 LT. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT
- [SDR AWXA200200671](https://openairdocs.org/sdr/AWXA200200671), Jul 26, 2002: TERMINAL. BROKEN. PHX - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 6 L/H WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE TERMINAL CONNECTOR A
- [SDR AWXA200200426](https://openairdocs.org/sdr/AWXA200200426), May 15, 2002: HOSE. BURST. PHX - EMERGENCY LANDING - FLT 0332 - EN ROUTE FROM SLC TO PHX THE "A" HYDRAULIC SYSTEM LOW PRESSURE LIGHT ILLUMINATED AND THEN THE GAUGE FLUCTUATED BACK AND FOR
- [SDR AWXA200200356](https://openairdocs.org/sdr/AWXA200200356), Apr 22, 2002: BATTERY. DISCHARGED. PHX - EEL - EMERGENCY ESCAPE PATH SEAT LIGHTS ON ALL SEATS EXCEPT LAST FIVE ROWS AND EMERGENCY EXIT LIGHTS AT L1 AND L2 DOOR ARE INOPERATIVE. MAINTENANCE REMOVE
- [SDR AWXA200200210](https://openairdocs.org/sdr/AWXA200200210), Mar 10, 2002: WIRE. BROKEN. PHX - EEL - "C" - EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 13 L/H INOPERATIVE. MAINTENANCE REPAIRED WIRE PULLED FROM SPLICE AT SEAT ROW 13 L/H, FUNCTIONAL CHECK 
- [SDR AWXA200200186](https://openairdocs.org/sdr/AWXA200200186), Mar 2, 2002: CHARGER. FAILED. CLIMBOUT ELEC ODOR 7000 FT, NO SMOKE. TURNED BACK. PWR REDUCED, ODOR SUBSIDED. MX ENTERED COCKPIT, SMELL SIMILAR TO BURNT RESISTOR. ALL C/B PNL LT & RT LOAD CNT
- [SDR AWXA200200121](https://openairdocs.org/sdr/AWXA200200121), Feb 9, 2002: LIGHT. INOPERATIVE. PHX - EEL - C - DURING INSPECTION EMERGENCY EXIT LIGHT ON SEAT ROW 13 LT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED SEAT LIGHT ASSEMBLY AT SEAT ROW
- [SDR AWXA200200022](https://openairdocs.org/sdr/AWXA200200022), Jan 12, 2002: WARNING SYSTEM. MALFUNCTIONED. PHX - ABORTED T/O - FLT 644 - S - UPON RELEASE OF BRAKES FLIGHT CREW RECEIVED AMBER WARNING MESSAGES FOR INBOARD AND OUTBOARD ANTI-SKID CHANNELS INOPERATIVE AND
- [SDR AWXA200100672](https://openairdocs.org/sdr/AWXA200100672), Dec 27, 2001: LIGHT. MISSING. LAS - EEL - EMERGENCY PATH LIGHT ASSEMBLY MISSING SEAT ROW 12 LT SIDE. MAINTENANCE REPLACED LIGHT ASSEMBLY AT SEAT ROW 12 LT SIDE, FUNCTIONAL CHECK WAS GOOD.
- [SDR AWXA200100599](https://openairdocs.org/sdr/AWXA200100599), Nov 27, 2001: BATTERY PACK. DISCHARGED. PHX - EEL - C - DURING ROUTINE MAINTENANCE INSPECTION FOUND R1 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY PACK AT R1 DOOR, OPERATIONAL 
- [SDR AWXA200100577](https://openairdocs.org/sdr/AWXA200100577), Nov 5, 2001: CONNECTOR. WORN. AFTER T/O, HEARD LOUD THUMP DURING GEAR RETRACTION, INDICATIONS NORM. IN FLT W/AP ENGAGED ACFT STARTED PORPOISING. AP WAS DISENGAGED, DIFFICULTY CONTROLLING PIT
- [SDR AWXA200100498](https://openairdocs.org/sdr/AWXA200100498), Sep 27, 2001: FLOORBEAM. CRACKED. YVR - C19 CK -LONGITUDINAL SEAT TRACK SUPPORT BEAM, LBL 24.5 CRACKED AT BOLT RELIEF HOLE, BS 679. MAINTENANCE MADE REPAIRS IAW AWA ER 15-5710-01269-JS1, REFEREN
- [SDR AWXA200100495](https://openairdocs.org/sdr/AWXA200100495), Sep 13, 2001: FLOORBEAM. CRACKED. YVR - C19 CK -RT OVERWING SEAT TRACK AILERON CUTOUT STRUCTURE AT RT I/B SEAT TRACK BS 658 VERT FLANGE CRACKED .3125 INCH. VISIBLE THROUGH CUTOUT UNDER STRUCTURE
- [SDR AWXA200100494](https://openairdocs.org/sdr/AWXA200100494), Sep 13, 2001: FLOORBEAM. CRACKED. YVR - C19 CK - RT OVERWING PRESSURE DECK LOWER VERT CHORD AT BS 698, RBL 24.82 CRACKED .5 INCH. MAINTENANCE TRIMMED OUT DAMAGED AREA, FABRICATED REPAIR ANGLE AN
- [SDR AWXA200100492](https://openairdocs.org/sdr/AWXA200100492), Sep 9, 2001: SKIN. CRACKED. YVR - C19 CK - L2 DOOR CUTOUT, LOWER FWD CORNER, FUSELAGE SKIN CRACKED IN 3 PLACES (1 INCH). MAINTENANCE ROUTED OUT THE CRACK IN THE FUSELAGE SKIN, DOUBLER AND 
- [SDR AWXA200100497](https://openairdocs.org/sdr/AWXA200100497), Sep 7, 2001: FLOORBEAM. CORRODED. YVR - C19 CK - FLOORBEAM AT BS 987 TOP SURFACE HAS CORROSION BETWEEN LBL 30 AND RBL 12. MAINTENANCE REMOVED PREVIOUS BEAM CAP REPAIR, FABRICATED NEW BEAM CAP AN
- [SDR AWXA200100496](https://openairdocs.org/sdr/AWXA200100496), Sep 7, 2001: FLOORBEAM. CORRODED. YVR - C19 CK - FLOORBEAM AT BS 967 HAS CORROSION BETWEEN BL 0 AND RBL 30 ON TOP SURFACE. AFTER CORROSION REMOVAL, MATERIAL LOSS BEYOND SRM LIMITS. MAINTENANCE R
- [SDR AWXA200100491](https://openairdocs.org/sdr/AWXA200100491), Sep 6, 2001: SKIN. CRACKED. YVR - C19 CK - "C" - L2 DOOR, FUSELAGE TORQUE BOX INNER SKIN 2" CRACK BS 952, BETWEEN STR 11R & 12R. MAINTENANCE FABRICATED REINFORCEMENT STRAP AND INSTALLED IA
- [SDR AWXA200100499](https://openairdocs.org/sdr/AWXA200100499), Sep 4, 2001: ANGLE. CRACKED. YVR - C19 CK - "C" - NOSE LANDING GEAR ACTUATOR UPPER ATTACH SUPPORT FITTING VERTICAL WEB CRACKS EMINATING FROM 3 RIVIT HOLES, EACH CRACK ABOUT .25". MAINTENANC
- [SDR AWXA200100493](https://openairdocs.org/sdr/AWXA200100493), Sep 4, 2001: BULKHEAD. CRACKED. YVR - C19 CK - BS 178 PRESS. BULKHEAD FWD FACE, .050 CRACK EMANATING FROM FASTENER HOLE, WL 234, RBL 5.7. MAINTENANCE REPAIRED IAW B737 SRM 53-10-11, FIG 1, DET
- [SDR AWXA200100490](https://openairdocs.org/sdr/AWXA200100490), Sep 4, 2001: CROSSBEAM. CRACKED. YVR - C19 CK - "C" - FWD CARGO DOOR LOWER CROSSBEAM WEB, TWO CRACKS FOUND, ONE ON FWD END AND ONE ON THE AFT END. BOTH CRACKS ARE .5 INCH. MAINTENANCE REPAIRED 
- [SDR AWXA0001045](https://openairdocs.org/sdr/AWXA0001045), Dec 8, 2000: FRAME. CRACKED. BS 178 WL 207 BULKHEAD L/H O/B SIDE CHORD CRACKED. CHORD REPLACED IAW SRM 51-10-01 DWG 65-16300
- [SDR AWXA0001044](https://openairdocs.org/sdr/AWXA0001044), Dec 8, 2000: INTERCOSTAL. CRACKED. STA 178 WL 207 LBL 28 LT O/B WEB CRACKED AT RIVET HOLE. WEB REPLACED IAW SRM 51-10-01 DWG 65-45833
- [SDR AWXA0001043](https://openairdocs.org/sdr/AWXA0001043), Dec 8, 2000: ATTACH ANGLE. CRACKED. RT O/B ANGLE AT STA 178 WL 195 RBL 25 CRACKED IN RADIUS. ANGLE REPLACED IAW SRM 51-10-01 DWG 65-16300
- [SDR AWXA0001042](https://openairdocs.org/sdr/AWXA0001042), Dec 8, 2000: ATTACH ANGLE. CRACKED. LEFT OUTBOARD T CHORD AT STA 178 WL 195 LBL 24.67 WAS CRACKED. ATTACHED ANGLES REPLACED IAW SRM 51-10-01 DWG 65-16300
- [SDR AWXA0001041](https://openairdocs.org/sdr/AWXA0001041), Dec 8, 2000: BULKHEAD. CRACKED. FWD PRESSURE BULKHEAD HAS TWO CRACK INDICATIONS ON WEB AT STA 178 WL 218 BEHIND STIFFENERS L&R OF BL 0. WEB CRACKS REPAIRED IAW SRM 53-10-11 FIG 1 DET. III.
- [SDR AWXA0001040](https://openairdocs.org/sdr/AWXA0001040), Dec 8, 2000: FRAME. CRACKED. STA 178 WL 200 RBL 26 SIDE CHORD CRACKED. CHORD REPLACED IAW SRM 51-10-01 DWG 65-16300
- [SDR AWXA0001039](https://openairdocs.org/sdr/AWXA0001039), Dec 8, 2000: INTERCOSTAL. CRACKED. INTERCOSTAL AT BS 178 WL 207 RBL 26 CRACKED. REPLACED WEB/INTERCOSTAL IAW SRM 51-10-01 DWG 61-45833
- [SDR AWXA0001038](https://openairdocs.org/sdr/AWXA0001038), Dec 8, 2000: FLOORBEAM. CRACKED. OUTBOARD T-CHORD AT STA 178 WL 207 IS CRACKED THROUGH AT FWD FASTENER HOLE. REPAIRED IAW SRM 51-40-4 FIG 1 DWG 65-45833
- [SDR AWXA0001037](https://openairdocs.org/sdr/AWXA0001037), Dec 8, 2000: SKIN. CRACKED. CRACK INDICATION ON FUSELAGE APPROX BS 747 STR 17R. REPAIR CARRIED OUT IAW ENG. REPAIR NO. 15-5331-00334-J51
- [SDR AWXA0001036](https://openairdocs.org/sdr/AWXA0001036), Dec 8, 2000: BRACKET. CRACKED. STA 178 GLIDE SLOPE ANTENNA SUPPORT BRACKET LOWER LT CORNER CRACKED. STOP DRILLED END OF CRACK AND REPAIRED IAW SRM 51-40-3
- [SDR AWXA0000573](https://openairdocs.org/sdr/AWXA0000573), Aug 18, 2000: SHEAR TIE. CRACKED. C-CHECK, SHEAR TIE CRACKED AT STA 887 27R - 27L. REMOVED DAMAGED PORTION OF SHEAR TIE, FABRICATED AND INSTALLED REPAIR PARTS IAW 737 SRM 53-10-4 AND SRM 53-10-4
- [SDR AWXA0000572](https://openairdocs.org/sdr/AWXA0000572), Aug 18, 2000: STRINGER CLIP. MISDRILLED. C-CHECK, LONGERON CLIP AT FS 887 LONG 27R HAS ELONGATED HOLES. REMOVED AND REPLACED CLIP IAW 737 SRM 51-30-2.
- [SDR AWXA0000571](https://openairdocs.org/sdr/AWXA0000571), Aug 18, 2000: BULKHEAD. MISDRILLED. C-CHECK, INADVERTANT 1.25 HOLES DRILLED IN BULKHEAD AT FS 727 LBL 40.5, WL 193. REPAIRED IAW ER 15-5363-00214-BA2.
- [SDR AWXA0000570](https://openairdocs.org/sdr/AWXA0000570), Aug 18, 2000: BRACKET. CRACKED. C-CHECK, LEFT FS 663.75 AFT SIDE OF FRAME PRESSURE DECK HAS CRACK. REMOVED CRACKED BRACKET, FABRICATED NEW BRACKET AND INSTALLED IAW 737 SRM 51-30-2 AND DWG 65-

All 134: https://openairdocs.org/deregistered/N184AW-2013-07-16/reports.md

## NTSB investigations (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB LAX87LA243](https://openairdocs.org/ntsb/LAX87LA243), Jun 23, 1987: Boeing 737-277 (N184AW), Los Angeles, CA, substantial damage. Probable cause: FAILURE OF THE QUALIFIED MECHANIC TO INSURE THE OPERATION OF THE AIRCRAFT BRAKES PRIOR TO TAXIING AND HIS FAILURE TO UTILIZE THE EMERGENCY BRAKE SYSTEM TO PREVENT THE COLLISION. CONTRIBUTING TO THIS…

## 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 20000212002429I](https://openairdocs.org/incident/20000212002429I), Feb 12, 2000: Boeing 737277 (N184AW), Colorado Spring, CO. (-5) The pilot reported encountering severe turbulance at 17,000 sw of cos 1226 MST. The aircraft made an uncontrolled descent to 14,000. One flight attendant…
- [Incident 19960706026609I](https://openairdocs.org/incident/19960706026609I), Jul 6, 1996: Boeing 737277 (N184AW), San Francisco, CA, Minor damage. Narrative: on landing roll at sfo, awxa flight 2605 blew both #1 and #2 MLG tires which caused damage to the inboard flaps and left gear doors. Maintenance…
- [Incident 19920520018959I](https://openairdocs.org/incident/19920520018959I), May 20, 1992: Boeing 737277 (N184AW), Des Moines, IA, Minor damage. Parts of tire cap and boost pump found on runway after departure. Landed safely. Panel not from this aircraft.
- [Accident 19870622055262A](https://openairdocs.org/incident/19870622055262A), Jun 22, 1987: Boeing 737277 (N184AW), Los Angeles, CA, Substantial damage. While holding on taxiway was struck by 747,N141UA,that a mechanic was taxiing without proper hydraulic brake system

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