Boeing 737-301

Service difficulty reports · 4,797

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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 aircraft_model_key = '737301'
  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 USAA040478Angle · crackedPIT - FOUND ANGLE CRACKED .5 INCH, BS 328 BETWEEN S20L AND S21L. REMOVED CRACKED ANGLE AND MFG NEW FROM EXTRUSION PER BOEING DWG 65-54892 AND SRM 51-40-03, 53-10-07. (M)Aug 5, 2004 · N356US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA040486Bar · corrodedPIT - FOUND STABILIZER BAR CORRODED, 7 EACH 1.5 INCH DIAMETER AREAS, RSS 181 LT WING. REMOVED STABILIZER BAR AND REPLACED WITH NEW PER WORK CARD J332-11-01 STEP NR 17. (M)Aug 5, 2004 · N356US · Boeing 737301 · Horizontal Stabilizer StructureSDR USAA040483Shim · corrodedPIT - FOUND SHIM AND ANGLE CORRODED PLUS 1 INCH BY 20 INCH AREA, BL 0 FROM BS 927-947. FABRICATED NEW ANGLE AND SHIM, ASSEMBLED AND INSTALLED PER SRM 653-60-51, 51-10-1. (M)Aug 5, 2004 · N356US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAASB04104Switch · malfunctionedFLT DEPARTED WITH RT WING TO BODY OVERHEAT MEL 26-13 APPLIED. ON CLIMB-OUT, AT 8,000 FT, LT PACK TRIPPED OFF. AT 10,000 FT, CAPT ATTEMPTED TO RESET PACK 3 MORE TIMES AFTER COOLING BUT PACK WOULD NOT REMAIN ON. DECISION MADE TO RETURN TO FIELD AT MCI. FLT LAug 5, 2004 · N584US · Boeing 737301 · Cabin Cooling SystemSDR USAA040414Skin · crackedCLT - FOUND SKIN CRACKED 1.5 INCH, BS 727E S23L. INSTALLED DOUBLERS PER SRM 53-00-01 FIG 229. (M)Aug 4, 2004 · N585US · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA040504Spar · crackedPIT - FOUND LEFT WING SPAR CRACKED .09375, AFT SPAR LEFT MAIN GEAR AREA. REWORKED HOLE PER EA 78859, REAMING HOLE AND INST BUSHING. (M)Aug 3, 2004 · N356US · Boeing 737301 · Wing SparSDR USAA040487Fitting · corrodedPIT - FOUND RIGHT HORIZ STAB LUGS CORRODED 1 INCH BY 2 INCH, R-9, 11, 12, 13, 14, 15, 17, 18, 19. CLEANED FACES AND BORE IAW SRM 55-10-10, NEW BUSHINGS. (M)Aug 3, 2004 · N356US · Boeing 737301 · Horizontal Stabilizer, Attach FittingsSDR USAA040398Beam · crackedFOUND BEAM CRACKED 8 INCHES, INTERCOSTAL BETWEEN STATION 986 AND 1006 LBL 20. DEFECTIVE PART REPLACED WITH IDENT PART. (M)Aug 1, 2004 · N356US · Boeing 737301 · Fuselage Main, StructureSDR USAA040397Support · corrodedFOUND SUPPORT CORRODED 2 INCHES BY 20 INCH AREA, INTERCOSTAL AT FS 986.5-967 LBL 18. DEFECTIVE PART REPLACED WITH IDENT PART NR. (M)Aug 1, 2004 · N356US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA040410Skin · gougedPIT - FOUND LEFT OUTBOARD FOREFLAP GOUGED, .3125 INCH WIDE BY .15 INCHE DEEP BY 2.5 INCH LONG, 30 INCHES FROM OUTBOARD END OF TOP SKIN, LEFT OUTBOARD FOREFLAP. DEFECTIVE PART REPLACED WITH IDENT PART NR PER MM 27-51-37-4. (M)Jul 31, 2004 · N340US · Boeing 737301 · Trailing Edge FlapsSDR USAA040390Roller · chafedPIT - FOUND SUPPORT FLAP ROLLER CHAFED .5 INCH BY 1 INCH AREA, FT AFT FLAP NR 1 OUTBOARD ROLLER ARM. REPLACED WITH AFT FLAP PER MM 27-51-39. (M)Jul 31, 2004 · N340US · Boeing 737301 · Trailing Edge FlapsSDR USAA040498Skin · delaminatedFOUND TOP SKIN/CORE BOND WITH 2 INCHES OF DELAMINATION, NR 2 SLAT TOP OUTBOARD T/E SURFACE. INSTALLED NEW CORE SECTION, TOP DOUBLER, SEAL END PER BOEING SRM 51-70-10. (M)Jul 30, 2004 · N356US · Boeing 737301 · Leading Edge DevicesSDR USAASB04103Light · inoperativeORD - MAINTENANCE REPORTED THE LOW LEVEL EMERGENCY ESCAPE PATH LIGHT AT SEAT 7C INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LOW LEVEL EMERGENCY ESCAPE PATH LIGHT AT SEAT 7C. OPERATIONAL CHECK GOOD. (M)Jul 30, 2004 · N558AU · Boeing 737301 · Emergency LightingSDR USAA040499Skin · delaminatedPIT - FOUND TOP SKIN DENTED WITH DELAMINATION, 1.5 INCH BY .025 INCH AREA, LEFT INBOARD FOREFLAP TOP CAMBER 58 INCHES FROM OUTBOARD END. INSTALLED TOP DOUBLER WITH FILLER MATERIAL PER BOEING SRM 51-70-10. (M)Jul 29, 2004 · N356US · Boeing 737301 · Trailing Edge FlapsSDR USAA040497Skin · delaminatedPIT - FOUND TOP SKIN/CORE BOND WITH DELAMINATION, 3 INCH BY 3.5 INCH AREA, NR 2 SLAT TOP SURFACE INBOARD END. REMOVED DAMAGE, INSTALLED NEW CORE SECTION, TOP DOUBLER, SEAL END PER BOEIGN SRM 51-70-10. (M)Jul 29, 2004 · N356US · Boeing 737301 · Leading Edge DevicesSDR USAA040396Skin · delaminatedPIT - FOUND SKIN DELAMINATED, 5 INCH BY 6 INCH AREA OF DELAMINATION, OUTBOARD END OF T/E. REMOVED DAMAGED CORE MATERIAL AND REPLACED, INSTALLED DOUBLERS PER SRM 51-70-10. (M)Jul 29, 2004 · N356US · Boeing 737301 · Wing, Plate/SkinSDR USAA040395Angle · corrodedPIT - FOUND ZEE ANGLE CORRODED 3 INCH BY 20 INCH AREA, BS 727B-727C LEFT ZEE ANGLE IN AFT CARGO. CUT OUT DAMAGED SECTION AND SPLICED IN NEW PER SRM 53-60-53, FIG 204 AND TYPICAL REPAIR 53-40-1. (M)Jul 29, 2004 · N356US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA040365Skin · crackedPIT - FOUND SKIN CRACKED 2.05 INCH, FS 129 LOWER SKIN AT AFT SPAR LEFT HORIZ STAB. INSTALLED DOUBLER PER SRM 55-10-01. (M)Jul 29, 2004 · N576US · Boeing 737301 · Horizontal Stabilizer, Plate/SkinSDR USAA040500Stringer · crackedPIT - FOUND STRINGER CRACKED 1.25 INCH, STRINGER 5A LEFT BS 1138 HORIZ STABILIZER CUTOUT. SPLICED STRINGER PER TYPICAL REPAIR 53-80-04, SRM 53-00-01 FIG 221. (M)Jul 26, 2004 · N356US · Boeing 737301 · Fuselage Main, Longeron/StringerSDR USAA040362Frame · crackedPIT - FOUND FRAME CRACKED APPROX 1.025 INCH, STATION 663.75. INSTALLED REPAIR ANGLE PER EA 78568. (M)Jul 26, 2004 · N575US · Boeing 737301 · Fuselage Main, FrameSDR USAA040361Keelbeam · chafedPIT - FOUND ELONGATED HOLES AND CHAFING ON UPPER CHORD, KEELBEAM LOWER CHORD, FS 700 TO FS 727 LBBL 6.15, FOUR EACH .4375 INCH DIAMETER. BLENDED, INSTALLED FREEZE PLUGS AND DOUBLER STRAP PER EA 78037. (M)Jul 26, 2004 · N350US · Boeing 737301 · Fuselage Main, KeelSDR USAA040394Stringer · crackedFOUND STRINGER CRACKED 1.25 INCH, STRINGER 5A LEFT BS 1138 HORIZ STAB CUTOUT. SPLICED STRINGER PER TYPICAL REPAIR 53-80-04, SRM 53-00-01 FIG 221. (M)Jul 26, 2004 · N356US · Boeing 737301 · Fuselage Main, Longeron/StringerSDR USAA040393Skin · delaminatedPIT - FOUND SKIN DELAMINATED 12 INCHES BY 3 INCHES WIDE DELAMINATED, LT WING T/E FLAP, TRAILING EDGE DELAMINATED, 15 INCHES FROM INBOARD END. REMOVED SKIN AND CORE, INSTALLED NEW SECTION AND TOP DOUBLER PER BOEING SRM 51-70-10. (M)Jul 23, 2004 · N356US · Boeing 737301 · Trailing Edge FlapsSDR SWAA042095Skin · delaminatedDURING SCHEDULED SERVICE CHECK, FOUND RT WING AFT INBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED RT WING INBOARD AFT T/E FLAP PER MM.Jul 23, 2004 · N659SW · Boeing 737301 · Trailing Edge FlapsSDR USAA040392Skin · delaminatedPIT - FOUND TOP SKIN AND CORE BOND 3 INCH BY 3.5 INCH AREA DELAMINATED, NR 1 SLAT OUTBOARD T/E. REMOVED DELAMINATED, SKIN CORE 7 INSTALLED NEW AND TOP DOUBLER PER BOEING SRM 51-70-10. (M)Jul 22, 2004 · N356US · Boeing 737301 · Leading Edge DevicesSDR USAA040391Skin · delaminatedPIT- FOUND TOP SKIN/CORE BOND DELAMINATED 3 INCH BY 3 INCH AREA, NR 6 SLAT TOP SURFACE OUTBOARD T/E. REMOVED DELAMINATED SKIN, INSTALLED NEW SECTION AND DOUBLER PER BOEING SRM 51-70-10. (M)Jul 21, 2004 · N356US · Boeing 737301 · Leading Edge DevicesSDR USAASB04095Light · inoperativePIT - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT AT SEAT ROW 10, LEFT SIDE, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY AT SEAT ROW 10, LEFT SIDE. OPS CHECK GOOD. (M)Jul 21, 2004 · N584US · Boeing 737301 · Emergency LightingSDR USAA040351Stiffener · corrodedPIT - FOUND CHANNEL STIFFENER CORRODED 1 INCH BY 2 INCH AREA, BS 1016 ABOVE AND BETWEEN STRINGER 27R AND 27L. (M)Jul 21, 2004 · N590US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA040349Frame · corrodedPIT - FOUND PRESSURE FRAME CORRODED .25 INCH BY 8 INCH AREA, AFT PRESSURE BULKHEAD BS 1016 BETWEEN STRINGER 27L AND 26R. (M)Jul 21, 2004 · N590US · Boeing 737301 · Fuselage Main, BulkheadSDR USAA040350Bulkhead · corrodedPIT - FOUND AFT WEB PRESSURE BULKHEAD CORRODED .5 INCH BY .5 INCH AREA, BS 1016 ABOVE AND BETWEEN. (M)Jul 21, 2004 · N590US · Boeing 737301 · Fuselage Main, BulkheadSDR USAA040364Skin · crackedCLT - FOUND SKIN CRACKED 1 INCH LONG, FS 727D AND STRINGER 23L. INSTALLED DOUBLER PER SRM 53-00-01, FIG 229. (M)Jul 20, 2004 · N586US · Boeing 737301 · Fuselage Main, Plate/SkinSDR SWAA042059Skin · delaminatedDURING SCHEDULED SERVICE CHECK, FOUND RT WING OUTBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED RT WING OUTBOARD AFT FLAP PER MM.Jul 20, 2004 · N659SW · Boeing 737301 · Trailing Edge FlapsSDR SWAA042058Skin · crackedDURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 787, STRINGER 25L, BS 747, STRINGER 23R, CRACKED. REPAIRED SKIN PER SRM.Jul 20, 2004 · N659SW · Boeing 737301 · Fuselage Main, Plate/SkinSDR SWAA042057Skin · corrodedDURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT RIGHT KEEL BEAM BS 500C TO RT KEELBEAM BS 500D, CORRODED. REPAIRED SKIN PER EA.Jul 20, 2004 · N659SW · Boeing 737301 · Fuselage Main, Plate/SkinSDR AWXA200400797Connector · damagedDURING 4-DAY CHECK EMERGENCY ESCAPE PATH LIGHTS AT SEAT ROWS 11 THRU 17 LT WERE FOUND INOPERATIVE. MAINTENANCE REPAIRED DAMAGED PIN ON CONNECTOR FOR EMERGENCY ESCAPE PATH LIGHTS AT SEAT ROW 12 LT; OPERATIONAL CHECK WAS GOOD.Jul 20, 2004 · N324AW · Boeing 737301 · Light System WiringSDR SWAA042047Skin · crackedDURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 787, STRINGER 20L, CRACKED. REPAIRED SKIN PER SRM.Jul 17, 2004 · N659SW · Boeing 737301 · Fuselage Main, Plate/SkinSDR AWXA200400785Wire · brokenDURING 8-DAY CHECK EMERGENCY ESCAPE PATH LIGHTS AT SEAT ROWS 11 - 17 WERE FOUND INOPERATIVE. MAINTENANCE REPAIRED A BROKEN EMERGENCY ESCAPE PATH LIGHT WIRE AT SEAT ROW 11 LT, OPERATIONAL CHECK WAS GOOD.Jul 17, 2004 · N324AW · Boeing 737301 · Light System WiringSDR SWAA042014Skin · crackedDURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 787, STRINGER 20L, CRACKED. REPAIRED SKIN PER SRM.Jul 16, 2004 · N659SW · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA040346Skin · crackedCLT - FOUND SKIN CRACKED 2.75 INCH, STATION 727E, STRINGER 24R. INSTALLED DOUBLER PER SRM 53-00-01, FIG 229. (M)Jul 15, 2004 · N340US · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA040347Skin · crackedCLT - FOUND SKIN CRACKED .625 INCH, FS 727D, STRINGER 23L. INSTALLED DOUBLER PER SRM 53-00-01 FIG 229. (M)Jul 14, 2004 · N340US · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAASB04089Wire Harness · inoperativeBOS - FLT 1249 - FLIGHT DEPARTED PVD, EN ROUTE TO DCA, WITH THE NR 2 ENGINE 'A' FIRE LOOP ON MEL 26-2A. DURING CLIMB-OUT, THE NR 2 ENGINE 'B' FIRE LOOP FAULT LIGHT ILLUMINATED AND REMAINED ON. FLIGHT DIVERTED TO BOS AND LANDED WITHOUT FURTHER INCIDENT. NO EJul 11, 2004 · N574US · Boeing 737301 · Fire Protection System WiringSDR AWXA200400762Light · inoperativeDURING B2 CHECK THE EMERGENCY ESCAPE PATH LIGHTS AT SEAT ROWS 7 AND 11 LT WERE FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT ASSEMBLIES AT SEAT ROWS 7 AND 11 LT, OPERATIONAL CHECK WAS GOOD.Jul 9, 2004 · N325AW · Boeing 737301 · Emergency LightingSDR USAA040340Frame · crackedPIT - FOUND FRAME CRACKED .125 INCH, STATION 480, S8L-S9L. INSTALLED REPAIR ANGLES PER TYPICAL REPAIR 53-10-20A. (M)Jul 8, 2004 · N355US · Boeing 737301 · Fuselage Main, FrameSDR USAA040339Skin · crackedCLT - FOUND SKIN CRACKED 1.5 INCHES LONG, STATION 727D PLUS 3 AT STRINGER 23 LEFT. INSTALLED DOUBLER PER SRM 53-00-01, FIG 229. (M)Jul 7, 2004 · N573US · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAASB04086Circuit Card · inoperativeDCA - FLT 2046 - AFTER TAKEOFF FROM DCA, EN ROUTE TO BOS, CREW RECEIVED BOTH THE GREEN AND RED NOSE LANDING GEAR INDICATION LIGHTS WHEN THE GEAR HANDLE WAS PLACED IN THE UP POSITION. IN ASSOCIATION WITH QUICK REF HANDBOOK, CREW EXTENDED GEAR AND RECEIVED A NOJul 5, 2004 · N558AU · Boeing 737301 · Landing Gear Position and WarningSDR AWXA200400710Indicator · defectiveSNA - EMERGENCY LANDING - FLT 0653 - ON DESCENT INTO PHX EN ROUTE FROM SNA AIRCRAFT EXPERIENCED A FLAP LOCKOUT AND WOULD NOT EXTEND WHEN SELECTING FLAPS 1. MAINTENANCE REMOVED AND REPLACE FLAP POSITION INDICATOR PER T/C R1B27001. PERFORMED TRAILING EDGE FLAP BJul 1, 2004 · N325AW · Boeing 737301 · Trailing Flap Position Indicating SystemSDR USAASB04081Battery Pack · inoperativePIT - FOUND DURING WEEKLY CHECK, MAINTENANCE FOUND THE INTERIOR EMERGENCY LIGHTS AT SEAT ROWS 12 THROUGH 16 AND THE EXTERIOR LIGHTS AT RIGHT OVERWING EXIT AND LEFT AFT FUSELAGE, EXTINGUISH AFTER 10 SECONDS OF OPERATION. MAINTENANCE REMOVED AND REPLACED THE BAJun 27, 2004 · N586US · Boeing 737301 · Emergency LightingSDR USAASB04078Rod · damagedPHL - FLT 301 - ON CLIMB-OUT FROM PHL, EN ROUTE TO MCO, THE AIRCRAFT WOULD NOT PRESSURIZE. CREW SWITCHED ON THE ENGINE BLEEDS WITH NO HELP. QUICK REFERENCE HANDBOOK PROCEDURES WERE ACCOMPLISHED BUT THE AIRCRAFT STILL WOLD NOT PRESSURIZE. SWITCHED TO STANDBYJun 25, 2004 · N587US · Boeing 737301 · Service DoorsSDR USAASB04076Circuit Card · malfunctionedON CLIMB-OUT FROM BOS, EN ROUTE TO DCA, CREW RECEIVED A RIGHT MLG UNSAFE INDICATION WITH GEAR UP AND LOCKED. FLIGHT RETURNED TO FIEDL AT BOS AND LANDED WITHOUT FURTHER INCIDENT. CREW REPORTED RECEIVING A NORMAL GEAR INDICATION OF THREE GREEN LIGHTS WHEN EXTEJun 25, 2004 · N558AU · Boeing 737301 · Landing Gear Retraction/Extension SystemSDR USAASB04079Sprocket · failedCLT - FLT 895 - ON 10 MILE FINAL INTO CLT FROM SAV, AT 190 KNOTS, CREW REPORTED THE STABILIZER JAMMED. BOTH PILOTS' MANUALLY TRIMMED AIRCRAFT BUT COULD NOT BREAK THE JAM. AIRCRAFT LANDED AT CLT WITH FLAPS 15 PER QUICK REFERENCE HANDBOOK. MAINTENANCE REMOVEDJun 23, 2004 · N574US · Boeing 737301 · Stabilizer Position Indicating
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