N150AW

Service difficulty reports not matched to an aircraft · 145

They name N150AW, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. 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 = 'N150AW' AND registry_match IS NULL
  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 150AW0024Transducer · inoperativeAUTO THROTTLE WILL DISENGAGE AND NOT RE-ENGAGE UNTIL FLAPS RETRACTED AND ALL LIGHTS OUT. SEEMS NR 1 THROTTLE LAGS BEHIND NR 2 AFTER TOGA IS PUSHED. PLACED AUTO THROTTLE SYSTEM ON MEL 22-4. ADJUSTED NR 2 ENGINE PLA TRANSDUCER PER MM 22-31-11. OPS CHECK OK.Jul 3, 2004 · N150AW · Boeing 7373G7 · Auto Throttle SystemSDR 150AW0023Sensor · out of adjustAUTO THROTTLE WILL KICK OFF ON TAKEOFF PRIOR TO REACHING TAKE OFF THRUST. WILL NOT RE-ENGAGE UNTIL FLAPS ARE RETRACTED AND ALL LIGHTS OUT. ADJUSTED PLA SYNCHRO PER MM 22-31-11. AUTO THROTTLE BITE TEST PERFORMS NORMAL.Jun 14, 2004 · N150AW · Boeing 7373G7 · Auto Throttle SystemSDR 150AW0042Frame · crackedAPPROX .040 INCH CRACK IN FUSELAGE FRAME AT BS 400 BETWEEN STR 8 RT AND STR 9 RT. REPAIRED CRACK PER SRM 53-00-07.May 25, 2004 · N150AW · Boeing 7373G7 · Fuselage Main, FrameSDR 150AW0041Frame · crackedAPPROX .040 INCH CRACK IN FUSELAGE FRAME AT BS 500C BETWEEN STR 8 LT AND STR 9 LT. REPAIRED CRACK PER SRM 53-00-07.May 25, 2004 · N150AW · Boeing 7373G7 · Fuselage Main, FrameSDR 150AW0040Frame · crackedAPPROX .040 INCH CRACK IN FUSELAGE FRAME AT BS 663 AT STR 2 RT. REPAIRED CRACK PER SRM 53-00-07.May 25, 2004 · N150AW · Boeing 7373G7 · Fuselage Main, FrameSDR 150AW0039Frame · crackedAPPROX .040 INCH CRACK IN FUSELAGE FRAME AT BS 663 AT STR 3 RT. REPAIRED CRACK PER SRM 53-00-07.May 25, 2004 · N150AW · Boeing 7373G7 · Fuselage Main, FrameSDR 150AW0038Frame · crackedAPPROX .040 INCH CRACK IN FUSELAGE FRAME AT BS 400 BETWEEN STR 8 LT AND STR 9 LT. REPAIRED CRACK IAW SRM 53-00-07.May 25, 2004 · N150AW · Boeing 7373G7 · Fuselage Main, FrameSDR 150AW0037Frame · crackedAPPROX .040 INCH CRACK IN FUSELAGE FRAME AT BS 480 BETWEEN STR 8 LT AND STR 9 LT. REPAIRED CRACK IAW SRM 53-00-07.May 25, 2004 · N150AW · Boeing 7373G7 · Fuselage Main, FrameSDR 150AW0036Frame · crackedAPPROX .040 INCH CRACK IN FUSELAGE FRAME AT BS827 BETWEEN STR 8 RT AND STR 9 RT. REPAIRED CRACK IAW SRM 53-00-07.May 25, 2004 · N150AW · Boeing 7373G7 · Fuselage Main, FrameSDR 150AW0035Frame · crackedAPPROX .040 INCH CRACK IN FUSELAGE FRAME AT BS 727E BETWEEN STR 8 LT AND STR 9 LT. REPAIRED CRACK PER SRM 53-00-07.May 25, 2004 · N150AW · Boeing 7373G7 · Fuselage Main, FrameSDR 150AW0034Frame · crackedAPPROX .040 CRACK IN FUSELAGE FRAME AT BS 312 AT STR 6 LT. REPAIRED CRACK PER SRM 53-00-07.May 25, 2004 · N150AW · Boeing 7373G7 · Fuselage Main, FrameSDR N150AW0010Frame · crackedAPPROX .040 INCH CRACK IN FUSELAGE FRAME AT BS 480 BETWEEN STR 8 RT AND STR 9 RT. REPAIRED CRACKS PER SRM 53-00-07.May 25, 2004 · N150AW · Boeing 7373G7 · Fuselage Main, FrameSDR 150AW0027Stringer Clip · crackedSTRINGER TIE CLIP CRACKED AT STRINGER 13 RT BS 867. REPLACED STRINGER TIE CLIP PER SRM 51-10-002.May 25, 2004 · N150AW · Boeing 7373G7 · Fuselage Main, Attach FittingsSDR 150AW0029Stringer Clip · crackedSTRINGER TIE CLIP CRACKED AT STRINGER 6 RT BS 597. REPLACED STRINGER TIE CLIP IAW SRM 51-10-02.May 25, 2004 · N150AW · Boeing 7373G7 · Fuselage Main, Attach FittingsSDR 150AW0033Stringer Clip · crackedSTRINGER TIE CLIP CRACKED AT STRINGER 4 RT BS 616. REPLACED STRINGER TIE CLIP PER SRM 51-10-02.May 25, 2004 · N150AW · Boeing 7373G7 · Fuselage Main, Attach FittingsSDR 150AW0032Stringer Clip · crackedSTRINGER TIE CLIP CRACKED AT STRINGER 8 LT BS 597. REPLACED STRINGER TIE CLIP PER SRM 51-10-02.May 25, 2004 · N150AW · Boeing 7373G7 · Fuselage Main, Attach FittingsSDR 150AW0031Stringer Clip · crackedSTRINGER TIE CLIP CRACKED AT STRINGER 7 LT BS 597. REPLACED STRINGER TIE CLIP PER SRM 51-10-02.May 25, 2004 · N150AW · Boeing 7373G7 · Fuselage Main, Attach FittingsSDR 150AW0030Stringer Clip · crackedSTRINGER TIE CLIP CRACKED AT STRINGER 4 RT BS 597. REPLACED STRINGER TIE CLIP PER SRM 51-10-02.May 25, 2004 · N150AW · Boeing 7373G7 · Fuselage Main, Attach FittingsSDR 150AW0028Stringer Clip · crackedSTRINGER TIE CLIP CRACKED AT STR 18 RT BS 747. REPLACED STRINGER TIE CLIP PER SRM 51-10-02.May 25, 2004 · N150AW · Boeing 7373G7 · Fuselage Main, Attach FittingsSDR 150AW0026Stringer Clip · crackedSTRINGER TIE CLIP CRACKED AT STRINGER 16 RT BS 727E. REPLACED STRINGER TIE CLIP PER SRM 51-10-02.May 25, 2004 · N150AW · Boeing 7373G7 · Fuselage Main, Attach FittingsSDR 150AW0025Stringer Clip · crackedSTRINGER TIE CLIP CRACKED AT STRINGER 4 RT BS 727B. STRINGER TIE CLIP REPLACED IAW SRM 51-10-02.May 25, 2004 · N150AW · Boeing 7373G7 · Fuselage Main, Attach FittingsSDR N150AW0003Stringer Clip · crackedSTRINGER TIE CLIPS CRACKED AT THE FOLLOWING LOCATIONS: STRINGER 4 RT BS 727D, STRINGER TIE CLIPS REPLACED IAW SRM 51-10-02.May 25, 2004 · N150AW · Boeing 7373G7 · Fuselage Main, Attach FittingsSDR N150AW0022Keelbeam · corrodedCORROSION ON THE HORIZONTAL FLANGE OF THE KEEL BEAM AT STR 28 RT SPLICE AT BS 500C + 9.0. REPAIRED PER EA NR 53-087.May 25, 2004 · N150AW · Boeing 7373G7 · Fuselage Main, KeelSDR N150AW0021Bear Strap · corrodedCORROSION BETWEEN STRAP AND SKIN AT BS 490 AT STR 28 RT AND IMPROPER REPAIR AT STR 27 RT AT BS 476 PER AD 2002-07-10 AND SB737-53A1177. REPAIRED PER EA NR 53-090.May 25, 2004 · N150AW · Boeing 7373G7 · Fuselage Main, Plate/SkinSDR N150AW0019Pressure Panel · corrodedCORROSION AT BS 1016 AT LOWER DRAIN HOLE ON FORWARD SIDE OF THE PRESSURE PANEL. REPAIRED PER SRM 53-80-08.May 25, 2004 · N150AW · Boeing 7373G7 · Fuselage Main, BulkheadSDR N150AW0018Floorbeam · corrodedBS 1016 AT RBBL 14 CORROSION AT FLOORBOARD ATTACH HOLE. REPLACED FLOORBEAM T-CAP PER SRM 51-10-2.May 25, 2004 · N150AW · Boeing 7373G7 · Fuselage Main, Floor BeamSDR N150AW0017Angle · corrodedL-ANGLE CORRODED AT BS 1016 TOP OF FLOOR IN AFT LAVATORY AREA. REPLACED ANGLE PER SRM 51-10-2.May 25, 2004 · N150AW · Boeing 7373G7 · Fuselage Miscellaneous StructureSDR N150AW00170Angle · corrodedL-ANGLE CORRODED AT BS 1016 TOP OF FLOOR IN AFT LAVATORY AREA. REPLACED ANGLE PER SRM 51-10-2.May 25, 2004 · N150AW · Boeing 7373G7 · Fuselage Miscellaneous StructureSDR N150AW0016Skin · damagedIMPROPER REPAIR INSTALLED AT BS 887 AT STR 20 RT AND AT BS 500A AT STR 10 LT ACCORDING TO AD2002-07-10 AND SB737-53A1177. REPLACED EXISTING REPAIRS PER SRM 53-00-014 FIG 229.May 25, 2004 · N150AW · Boeing 7373G7 · Fuselage Main, Plate/SkinSDR N150AW0015Bulkhead · crackedVERTICAL STIFFENER ON THE AFT SIDE OF BS 178 BULKHEAD IS CRACKED AT LBBL 5.7 AND WL 184. REPAIRED AREA PER SRM 53-10-8.May 25, 2004 · N150AW · Boeing 7373G7 · Fuselage Main, BulkheadSDR N150AW0014Bulkhead · crackedHFEC REVEALED A CRACK INDICATION AT FASTENER AT RBBL 10.5 AND WL 234 ON THE BS 178 BULKHEAD. REPAIRED AREA PER SRM 53-10-8.May 25, 2004 · N150AW · Boeing 7373G7 · Fuselage Main, BulkheadSDR N150AW0013Bulkhead · crackedHFEC REVEALED CRACK INDICATIONS ON THE I/B SIDE OF VERTICAL STRAP ON THE BS 178 BULKHEAD AT RBBL 5.7 AND WL 201 AND THE I/B SIDE OF THE VERTICAL STRAP AT LBBL 5.7 AND WL 198.5. REPAIRED CRACKED AREAS PER SRM 53-10-8.May 25, 2004 · N150AW · Boeing 7373G7 · Fuselage Main, BulkheadSDR N150AW0012Splice · crackedSTRINGER SPLICE CRACKED AT BS 907 AT STR 4 LT AND AT STR 4 RT. REPLACED STRINGER SPLICE AT STR 4 LT AND STR 4 RT PER SRM 51-10-02.May 25, 2004 · N150AW · Boeing 7373G7 · Fuselage Main, Longeron/StringerSDR N150AW0011Frame · crackedBS 747 FRAME CRACKED AT STR 13 LT. REPAIRED PER SRM 51-70-11.May 25, 2004 · N150AW · Boeing 7373G7 · Fuselage Main, FrameSDR N150AW0009Skate Angle · wornFORWARD END OF LEFT SKATE ANGLE FOR VERTICAL DORSAL FIN IS WORN AT BS 1016. REPLACED SKATE ANGLE PER SRM 51-10-02.May 25, 2004 · N150AW · Boeing 7373G7 · Horizontal Stabilizer StructureSDR N150AW0008Bulkhead · damagedDRILL MARK ON AFT PRESSURE BULKHEAD AT RBL 37.5 AT THE MOISTURE BARRIER RETAINER. REPAIRED PER SRM 53-80-08.May 25, 2004 · N150AW · Boeing 7373G7 · Fuselage Main, BulkheadSDR N150AW0007Web · crackedCRACK AT CUTOUT IN WEB, 4 INCHES FOWRARD OF L-2 DOOR AT STR 11 LT. REPAIRED PER SRM 51-70-13.May 25, 2004 · N150AW · Boeing 7373G7 · Fuselage Miscellaneous StructureSDR N150AW0006Attach Angle · crackedFRAME SHELF ATTACH ANGLES CRACKED AT BS 294.5 AT STR 12 RT, STR 11 RT, AND AT STR 10 RT. REPLACED ANGLES PER SRM 51-10-02.May 25, 2004 · N150AW · Boeing 7373G7 · Fuselage Main, Attach FittingsSDR N150AW0005Threshold · crackedFORWARD CORNER OF THE FORWARD CARGO DOOR THRESHOLD IS CRACKED. REPAIRED PER BAC 5975.May 25, 2004 · N150AW · Boeing 7373G7 · Fuselage Miscellaneous StructureSDR N150AW0004Seat Track · crackedSTATION 727B SEAT TRACK AT RBBL 24.82 OUTBOARD FLANGE AND SEAT TRACK AT RBBL 45.57 INBOARD AND OUTBOARD FLANGES HAVE A CRACK ON THE UPPER CHORD ON THE HORIZONTAL FREE FLANGE AT THE TRANSVERSE BEAM CONNECTION POINT. REPAIRED AREAS PER EA NR 53-085.May 25, 2004 · N150AW · Boeing 7373G7 · Fuselage, Seat/Cargo Attach FittingsSDR N150AW0002Skin · damagedLEADING EDGE OF WING DAMAGED OUTBOARD END OF THE NUMBER 5 SLAT. REPAIRED PER SRM 51-70-17.May 25, 2004 · N150AW · Boeing 7373G7 · Leading Edge DevicesSDR N150AW0001Web · damagedWEB DAMAGED AFT OF R-2 DOOR. REPLACED WEB PER SRM 51-10-02.May 25, 2004 · N150AW · Boeing 7373G7 · Fuselage Miscellaneous StructureSDR AWXA200300239Proximity Sensor · damagedDURING TAKEOFF ROLL AT LAS EN ROUTE FOR OAK THE MASTER CAUTION LIGHT ILLUMINATED FOLLOWED BY NO. ENGINE AFT BOOST PUMP LIGHT, REJECTED TAKEOFF AT APPROXIMATELY 110 KTS. MAINTENANCE PERFORMED HIGH POWER ENGINE RUN, COULD NOT DUPLICATE THE NR1 ENGINE BOOST PUMP Mar 10, 2003 · N150AW · Boeing 7373G7 · Engine Thrust ReverserSDR AWXA200201199Battery · dischargedEMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THAT THE AFT EMERGENCY FLASHLIGHT BATTERY WAS DEAD. REMOVED AND REPLACED THE AFT EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD.Dec 14, 2002 · N150AW · Boeing 7373G7 · Emergency EquipmentSDR AWXA200201198Battery · dischargedEMERGENCY EQUIPMENT - DURING INSPECTION MAINTENANCE FOUND THE FORWARD GALLEY EMERGENCY FLASHLIGHT HAD A WEAK BATTERY. REMOVED AND REPLACED THE FORWARD GALLEY EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD.Dec 13, 2002 · N150AW · Boeing 7373G7 · Emergency EquipmentSDR AWXA200201196Control Switch · inoperativeAIR TURN BACK ON CLIMB OUT, EXPERIENCED RUDDER AND TRIM PROBLEMS. UNABLE TO TRIM THE RUDDER, WITH AN INDICATION OF ONLY 2 UNITS, LEFT TRIM WILL NOT MOVE. REQUIRED AILERON 20 UNITS TO THE RIGHT IN ORDER TO MAINTAIN STRAIGHT AND LEVEL FLIGHT. TURNED BACK TO AIDec 12, 2002 · N150AW · Boeing 7373G7 · Rudder Tab Control SystemSDR AWXA200201182Battery · dischargedEMERGENCY EQUIPMENT - DURING INSPECTION THE EMERGENCY FLASHLIGHT JUST ABOVE THE FORWARD FLIGHT ATTENDANT SEAT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD FLIGHT ATTENDANT STATION EMERGENCY FLASHLIGHT BATTERY; OPERATIONAL CHECK WAS GOOD.Dec 10, 2002 · N150AW · Boeing 7373G7 · Emergency EquipmentSDR AWXA200201174Mec · faultyON DESCENT CAUTION PANEL INDICATED RT ENG FAILED. COMPLETED ENG SHUTDOWN. RESTARTED NR 2 ENG. MX REMOVED NR 2 ENG FUEL FILTER & INSPECTED FILTER & HIGH PRESSURE FUEL PUMP. ENG PERF & DETERIORATION TEST, POWER TRIM CHECK, CHECKS GOOD. FUEL FILTER REPLACED.Dec 8, 2002 · N150AW · Boeing 7373G7 · Fuel Control/Turbine EnginesSDR AWXA200201154Skin · crackedMCN - MAJOR REPAIR - DURING 8-DAY CHECK A 1 1/2" CRACK WAS FOUND ON THE FUSELAGE SKIN AFT LOWER SIDE OF THE R/H WING TO BODY FAIRING AT BS 727E, STR 23 R/H. MAINTENANCE CUTOUT DAMAGED SKIN AT BS 727E, STR 23 R/H; PREFORMED A HFEC INSPECTION OF CUTOUT TO VERIFYNov 19, 2002 · N150AW · Boeing 7373G7 · Fuselage Main, Plate/SkinSDR AWXA200201153Skin · crackedMCN - MAJOR REPAIR - DURING 8-DAY CHECK A 3" LONG CRACK WAS FOUND ON THE FUSELAGE SKIN FORWARD OF THE AFT CARGO DOOR AT BS 767, STR 21 R/H. MAINTENANCE CUTOUT DAMAGED SKIN AT BS 762.5 TO BS 766.2, STR 21 R/H; PREFORMED A HFEC INSPECTION OF CUTOUT TO VERIFY NO Nov 19, 2002 · N150AW · Boeing 7373G7 · Fuselage Main, Plate/Skin
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