N184AW, cancelled Jul 16, 2013

Service difficulty reports · 134

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

Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE n_number = 'N184AW' AND deregistration_id = 'N184AW-2013-07-16'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR AWXA200400021Bearing · seizedAFTER 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. TURNED OFF GASPER FAN & WINDOW HEAT, ODOR SUBSIDED. MAINT TROUBLESHOT, FOUND FLT DECK CABIN AIR COND FANJan 7, 2004 · N184AW · Boeing 737277 · Air Distribution FanSDR AWXA200400024Wire · damagedON 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 WHEEL STEERING INDICATED ROLL RT, AUTOPILOT-A NORMAL. MAINT TROUBLESHOT AUTOPILOT SYS, B-SYS GOEJan 4, 2004 · N184AW · Boeing 737277 · Auto Flight System WiringSDR AWXA200301095Line · leakingDURING 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 REMAINING. EMERGENCY EQUIPMENT CALLED OUT AS A PRECAUTION. MAINTENANCE FOUND THE NOSE LANDING GEAR ACTUASep 23, 2003 · N184AW · Boeing 737277 · Hydraulic System, MainSDR AWXA200300721Pump · failedON DEPARTURE, LOST A-SYSTEM HYDRAULIC PRESSURE, TURNED BACK AND LANDED WITHOUT FURTHER EVENT. AIRCRAFT TOWED BACK TO GATE. MAINTENANCE FOUND THE NR 1 ENGINE DRIVEN HYDRAULIC PUMP HAD FAILED, REMOVED AND REPLACED PUMP. A-SYSTEM HYDRAULICS FLUSHED, OPERATIONAL Jun 20, 2003 · N184AW · Boeing 737277 · Hydraulic Pump (Electric/Engine), MainSDR AWXA200300142Module · failedPHX - 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 2 UNIT; REJECTED TAKEOFF AT 50 KTS. AFTER TAXI OFF RUNWAY AND SITTING ON TAXIWAY, THE IN TRANSIT LIFeb 14, 2003 · N184AW · Boeing 737277 · Leading Edge Slat Position Indicating SystemSDR AWXA200201041Sign · brokenDURING C-20 CHECK THE FORWARD SERVICE DOOR EMERGENCY EXIT SIGN WAS FOUND DAMAGED. MAINTENANCE REMOVED AND REPLACED THE FORWARD SERVICE DOOR EMERGENCY EXIT SIGN, OPERATIONAL CHECK WAS GOOD IAW AWA T/C A1C33006.Oct 18, 2002 · N184AW · Boeing 737277 · Emergency LightingSDR AWXA200201031Door Frame · corrodedDURING 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 WEB AT BS 277 - 306, A FRAME BS 300, AND AN ANGLE BS 277 - 284 FOR ACCESS, REMOVED DAMAGED DOOR SILOct 15, 2002 · N184AW · Boeing 737277 · Fuselage Main, StructureSDR AWXA200201030Stiffener · crackedYVR - 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 REMOVED DAMAGED INTERCOASTAL ATTACH ANGLE AT BS 328, LBL 47; FABRICATED A NEW REPLACEMENT ATTACH ANGOct 15, 2002 · N184AW · Boeing 737277 · Fuselage Main, Floor BeamSDR AWXA200201056Crease Beam · crackedDURING 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 420; CUT STRINGER 17 AT BS 396; FABRICATED A REPAIR ANGLE; INSTALLED STRINGER REPAIR AND WEBS IAW B7Oct 7, 2002 · N184AW · Boeing 737277 · Fuselage Main, StructureSDR AWXA200201027Skin · crackedDURING 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 334 - 336, STR 17 LT. MAINTENANCE REMOVED EXISTING REPAIR DOUBLER, STRAP, WEB, AND COVER PLATE AT BS 3Oct 4, 2002 · N184AW · Boeing 737277 · Fuselage Main, Plate/SkinSDR AWXA200201026Frame · crackedYVR - 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 STR 5 - STR 6 L/H; PERFORMED A HFEC INSPECTION TO VERIFY CRACK WAS CONTAINED; FABRICATED A FRAME REPAOct 4, 2002 · N184AW · Boeing 737277 · Fuselage Main, FrameSDR AWXA200201025Attach Angle · crackedYVR - 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 ATTACH ANGLE AT BS 360, STR 11 L/H; FABRICATED A NEW REPLACEMENT ATTACH ANGLE; INSTALLED REPAIR PART IAW Oct 4, 2002 · N184AW · Boeing 737277 · Fuselage Miscellaneous StructureSDR AWXA200201024Flap Track · crackedDURING 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 NR 7 FLAP TRACK AT THE INBOARD ROLLER OF UPPER TRACK, AFT END IAW AWA T/C R3R27004.Oct 4, 2002 · N184AW · Boeing 737277 · Trailing Edge FlapsSDR AWXA200201057Skin · corrodedYVR - 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. MAINTENANCE PREPARED AREA AT L/H WING LOWER SKIN FLAP TRACK ATTACH POINT WS 254 L/H; REMOVED CORROSION; TROct 3, 2002 · N184AW · Boeing 737277 · Fuselage Main, Plate/SkinSDR AWXA200201028Skin · crackedYVR - 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. MAINTENANCE TRIMMED OUT R-2 DOOR UPPER HINGE CUTOUT AT FORWARD UPPER CORNER BS 957.5, WL 240 BY .040" AND PEOct 3, 2002 · N184AW · Boeing 737277 · Fuselage Main, Plate/SkinSDR AWXA200200686Light · inoperativeLAS - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT WAS FOUND INOPERATIVE AT SEAT ROW 6 LT. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 6 LT, OPERATIONAL CHECK WAS GOOD.Jul 31, 2002 · N184AW · Boeing 737277 · Emergency LightingSDR AWXA200200671Terminal · brokenPHX - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 6 L/H WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE TERMINAL CONNECTOR AT SEAT ROW 6 L/H, OPERATIONAL CHECK WAS GOOD.Jul 26, 2002 · N184AW · Boeing 737277 · Emergency LightingSDR AWXA200200426Hose · burstPHX - 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 FORTH, FLIGHT CREW DECLARED AN EMERGENCY AND LANDED SAFELY AT SCHEDULED DESTINATION. MAINTENANCE PRESSUMay 15, 2002 · N184AW · Boeing 737277 · Hydraulic Pressure IndicatorSDR AWXA200200356Battery · dischargedPHX - 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 REMOVED AND REPLACED 2 EACH EMERGENCY LIGHTING BATTERY PACKS UNDER SEATS AT ROWS 3 AND 11 LT IAW BMM 33-5Apr 22, 2002 · N184AW · Boeing 737277 · Emergency LightingSDR AWXA200200210Wire · brokenPHX - 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 WAS GOOD IAW T/C A1C33006.Mar 10, 2002 · N184AW · Boeing 737277 · Emergency LightingSDR AWXA200200186Charger · failedCLIMBOUT 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 CNTL CENTER INSP FOR DAMAGE/ELEC ODOR, NONE FOUND. CIRCUIT CARDS IN P6 PNL INSP, M560 FOUND W/ OVERMar 2, 2002 · N184AW · Boeing 737277 · Battery/Charger SystemSDR AWXA200200121Light · inoperativePHX - 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 13 LT, OPERATIONAL CHECK C/W IAW T/C A1C33009.Feb 9, 2002 · N184AW · Boeing 737277 · Emergency LightingSDR AWXA200200022Warning System · malfunctionedPHX - 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 AUTO-BRAKES, AIRCRAFT ABORTED TAKEOFF AND RETURNED TO GATE. AT GATE MAINTENANCE ISSUED A DPI, MEL Jan 12, 2002 · N184AW · Boeing 737277 · Brake Anti-Skid SectionSDR AWXA200100672Light · missingLAS - 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.Dec 27, 2001 · N184AW · Boeing 737277 · Emergency LightingSDR AWXA200100599Battery Pack · dischargedPHX - EEL - C - DURING ROUTINE MAINTENANCE INSPECTION FOUND R1 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY PACK AT R1 DOOR, OPERATIONAL CHECK GOOD.Nov 27, 2001 · N184AW · Boeing 737277 · Emergency LightingSDR AWXA200100577Connector · wornAFTER T/O, HEARD LOUD THUMP DURING GEAR RETRACTION, INDICATIONS NORM. IN FLT W/AP ENGAGED ACFT STARTED PORPOISING. AP WAS DISENGAGED, DIFFICULTY CONTROLLING PITCH ATTITUDE. DIVERTED. ON APPROACH 165 KTS BUFFETING FELT, FLAPS 15, 170 KTS. FERRIED, A COMPLETE VNov 5, 2001 · N184AW · Boeing 737277 · Autopilot Trim ServoSDR AWXA200100498Floorbeam · crackedYVR - 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, REFERENCING BOEING S/B 737-57-1139, REV 4, FIG6.Sep 27, 2001 · N184AW · Boeing 737277 · Fuselage Main, Floor BeamSDR AWXA200100495Floorbeam · crackedYVR - 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 OF CLOSED FLOOR PANEL. MAINTENANCE STOP DRILLED CRACK AND INSTALLED REPAIR IAW AWA ER 15-5710-0126Sep 13, 2001 · N184AW · Boeing 737277 · Fuselage Main, Floor BeamSDR AWXA200100494Floorbeam · crackedYVR - 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 AND INSTALLED IAW AWA ER 15-5702-01271-SS2.Sep 13, 2001 · N184AW · Boeing 737277 · Fuselage Main, Floor BeamSDR AWXA200100492Skin · crackedYVR - 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 BEARSTRAP. FABRICATED AND INSTALLED REPAIR IAW B737 SRM 53-30-3, FIG 24, PG 83.Sep 9, 2001 · N184AW · Boeing 737277 · Fuselage Main, Plate/SkinSDR AWXA200100497Floorbeam · corrodedYVR - 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 AND INSTALLED IAW B737 SRM 53-10-9, FIG 2, PG 7.Sep 7, 2001 · N184AW · Boeing 737277 · Fuselage Main, Floor BeamSDR AWXA200100496Floorbeam · corrodedYVR - 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 REMOVED DAMAGED SECTION OF FLOORBEAM TOP CAP AND REPLACED IAW B737 SRM 53-10-9, FIG 2, PG 7.Sep 7, 2001 · N184AW · Boeing 737277 · Fuselage Main, Floor BeamSDR AWXA200100491Skin · crackedYVR - C19 CK - "C" - L2 DOOR, FUSELAGE TORQUE BOX INNER SKIN 2" CRACK BS 952, BETWEEN STR 11R & 12R. MAINTENANCE FABRICATED REINFORCEMENT STRAP AND INSTALLED IAW AWA ER 15-5345-01264-TB4, REFERENCING PROCEDURES IN BOEING SB 737-53-1094.Sep 6, 2001 · N184AW · Boeing 737277 · Fuselage, Door HingeSDR AWXA200100499Angle · crackedYVR - C19 CK - "C" - NOSE LANDING GEAR ACTUATOR UPPER ATTACH SUPPORT FITTING VERTICAL WEB CRACKS EMINATING FROM 3 RIVIT HOLES, EACH CRACK ABOUT .25". MAINTENANCE REMOVED DAMAGED FITTING, FABRICATED A NEW ANGLE (FITTING) AND INSTALLED IAW BOEING INSTALLATION Sep 4, 2001 · N184AW · Boeing 737277 · Fuselage, Landing Gear Attach FittingsSDR AWXA200100493Bulkhead · crackedYVR - 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, DETAIL II, PG 5.Sep 4, 2001 · N184AW · Boeing 737277 · Fuselage Main, BulkheadSDR AWXA200100490Crossbeam · crackedYVR - 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 THE CARGO DOOR IAW AWA E.O.52-31-04, SHEETS 1 - 18.Sep 4, 2001 · N184AW · Boeing 737277 · Cargo/Baggage DoorsSDR AWXA0001045Frame · crackedBS 178 WL 207 BULKHEAD L/H O/B SIDE CHORD CRACKED. CHORD REPLACED IAW SRM 51-10-01 DWG 65-16300Dec 8, 2000 · N184AW · Boeing 737277 · Fuselage Main, FrameSDR AWXA0001044Intercostal · crackedSTA 178 WL 207 LBL 28 LT O/B WEB CRACKED AT RIVET HOLE. WEB REPLACED IAW SRM 51-10-01 DWG 65-45833Dec 8, 2000 · N184AW · Boeing 737277 · Fuselage Main, BulkheadSDR AWXA0001043Attach Angle · crackedRT O/B ANGLE AT STA 178 WL 195 RBL 25 CRACKED IN RADIUS. ANGLE REPLACED IAW SRM 51-10-01 DWG 65-16300Dec 8, 2000 · N184AW · Boeing 737277 · Fuselage Main, StructureSDR AWXA0001042Attach Angle · crackedLEFT OUTBOARD T CHORD AT STA 178 WL 195 LBL 24.67 WAS CRACKED. ATTACHED ANGLES REPLACED IAW SRM 51-10-01 DWG 65-16300Dec 8, 2000 · N184AW · Boeing 737277 · Fuselage Main, StructureSDR AWXA0001041Bulkhead · crackedFWD 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.Dec 8, 2000 · N184AW · Boeing 737277 · Fuselage Main, BulkheadSDR AWXA0001040Frame · crackedSTA 178 WL 200 RBL 26 SIDE CHORD CRACKED. CHORD REPLACED IAW SRM 51-10-01 DWG 65-16300Dec 8, 2000 · N184AW · Boeing 737277 · Fuselage Main, FrameSDR AWXA0001039Intercostal · crackedINTERCOSTAL AT BS 178 WL 207 RBL 26 CRACKED. REPLACED WEB/INTERCOSTAL IAW SRM 51-10-01 DWG 61-45833Dec 8, 2000 · N184AW · Boeing 737277 · Fuselage Main, BulkheadSDR AWXA0001038Floorbeam · crackedOUTBOARD T-CHORD AT STA 178 WL 207 IS CRACKED THROUGH AT FWD FASTENER HOLE. REPAIRED IAW SRM 51-40-4 FIG 1 DWG 65-45833Dec 8, 2000 · N184AW · Boeing 737277 · Fuselage Main, Floor BeamSDR AWXA0001037Skin · crackedCRACK INDICATION ON FUSELAGE APPROX BS 747 STR 17R. REPAIR CARRIED OUT IAW ENG. REPAIR NO. 15-5331-00334-J51Dec 8, 2000 · N184AW · Boeing 737277 · Fuselage Main, Plate/SkinSDR AWXA0001036Bracket · crackedSTA 178 GLIDE SLOPE ANTENNA SUPPORT BRACKET LOWER LT CORNER CRACKED. STOP DRILLED END OF CRACK AND REPAIRED IAW SRM 51-40-3Dec 8, 2000 · N184AW · Boeing 737277 · Fuselage Miscellaneous StructureSDR AWXA0000573Shear Tie · crackedC-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.Aug 18, 2000 · N184AW · Boeing 737277 · Fuselage Main, StructureSDR AWXA0000572Stringer Clip · misdrilledC-CHECK, LONGERON CLIP AT FS 887 LONG 27R HAS ELONGATED HOLES. REMOVED AND REPLACED CLIP IAW 737 SRM 51-30-2.Aug 18, 2000 · N184AW · Boeing 737277 · Fuselage Main, Longeron/StringerSDR AWXA0000571Bulkhead · misdrilledC-CHECK, INADVERTANT 1.25 HOLES DRILLED IN BULKHEAD AT FS 727 LBL 40.5, WL 193. REPAIRED IAW ER 15-5363-00214-BA2.Aug 18, 2000 · N184AW · Boeing 737277 · Fuselage Main, BulkheadSDR AWXA0000570Bracket · crackedC-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 65-50733.Aug 18, 2000 · N184AW · Boeing 737277 · Fuselage Miscellaneous Structure
Back to N184AW, cancelled Jul 16, 2013