N591US, cancelled Dec 29, 2008

Service difficulty reports · 82

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 = 'N591US' AND deregistration_id = 'N591US-2008-12-29'
  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 USAA2008112192099Skin · crackedPHL - RON - MAJOR REPAIR, CRACK ON FUSELAGE SKIN FORWARD OF AFT CARGO DOOR BY EXTERIOR SERVICE LIGHT BS727D +10 INCHES, S22R TO S23R. REPAIRED FUSELAGE SKIN IAW B737 SRM 53-00-01. REPAIR COMPLETED CHANGED DISCREPANCY, ADDED CORRECTIVE ACTION, PART NUMBER, SNov 14, 2008 · N591US · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA920082054Skin · crackedCLT MAJOR REPAIR NR 4370429, CRACKED FUSELAGE SKIN AT BS 727E + 18", S24R. REPAIRED FUSELAGE SKIN AT BS 727E + 18", S24R IAW B737 SRM 53-00-01 REPAIR 31.Nov 11, 2008 · N591US · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA920080950Skin · crackedCLT - MAJOR REPAIR - CRACKED FUSELAGE SKIN, BS 727E, S24L. REPAIRED FUSELAGE SKIN, BS 727E, S24L IAW B737 SRM 53-00-01 REPAIR 31.Apr 26, 2008 · N591US · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA920080774Door · out of adjustFLT 1580 - CLT - PIT - CAPTAIN ABORTED TAKEOFF DUE TO L1 ENTRY DOOR LIGHT ILLUMINATED. MX ADJUSTED FORWARD ENTRY DOOR. OPERATIONAL CHECK WAS GOOD.Apr 7, 2008 · N591US · Boeing 737301 · Passenger/Crew DoorsSDR USAA920080534Skin · crackedCLT - MAJOR REPAIR - RON - CRACKED FUSELAGE SKIN, BS 500C, S15L. REPAIRED FUSELAGE SKIN, BS 500C, S15L IAW USAIRWAYS EA 100277.Mar 2, 2008 · N591US · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA920071177Skin · delaminatedCLT - MAJOR REPAIR - C6 CHECK, LEFT WING SPOILER NUMBER 0 UPPER AND LOWER SURFACES DELAMINATED, WS 447 - WS 499. REPLACED LEFT WING SPOILER NUMBER 0, IAW B737 AMM 27-62-91.Nov 16, 2007 · N591US · Boeing 737301 · SpoilersSDR USAA920071176Skin · delaminatedCLT - MAJOR REPAIR - C6 CHECK, LEFT WING OUTBOARD AFT FLAP LOWER SURFACE DELAMINATED, WS 395. REPLACED LEFT WING OUTBOARD AFT FLAP IAW B737 AMM 27-51-39.Nov 16, 2007 · N591US · Boeing 737301 · Trailing Edge FlapsSDR USAA920071190Skin · crackedCLT - MAJOR REPAIR - C6 CHECK, CRACKED FUSELAGE SKIN, BS 460, S26R. REPAIRED FUSELAGE SKIN, BS 460, S26R IAW USAIRWAYS EA 100015.Nov 10, 2007 · N591US · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA920071189Frame · crackedCLT - MAJOR REPAIR - C6 CHECK, FORWARD CARGO DOOR CUTOUT AFT FRAME CRACKED, BS 492.4, S24R. REPAIRED FORWARD CARGO DOOR CUTOUT AFT FRAME, BS 492.4, S24R IAW USAIRWAYS EA 100014.Nov 8, 2007 · N591US · Boeing 737301 · Fuselage Main, FrameSDR SB07088Conduit · out of positionCMH FLT 1456 AFTER TAKEOFF FROM CMH, EN ROUTE TO DCA, CREW RECEIVED A RED NLG UNSAFE LIGHT UPON GEAR RETRACTION. CREW FOLLOWED QRH PROCEDURES, EXTENDED GEAR AND RECEIVED NORMAL GEAR INDICATION OF THREE GREEN LIGHTS. FLIGHT RETURNED TO FIELD AT CMH AND LANDEOct 10, 2007 · N591US · Boeing 737301 · Landing Gear Position and WarningSDR SB07076Bulb · faultyPIT - FLT 1158 EN ROUTE FROM LGA TO PIT, APPROXIMATELY 75 MILES SOUTHEAST OF PIT, CREW NOTICED THE NR 2 ENGINE OIL TEMPERATURE WAS OUT OF LIMITS. CREW FOLLOWED QUICK REFERENCE HANDBOOK PROCEDURES AND SHUT DOWN THE NR 2 ENGINE. FLIGHT LANDED AND TAXIED TO TSep 12, 2007 · N591US · Boeing 737301 · Engine Oil TemperatureSDR USAA920070822Skin · crackedCLT - MAJOR REPAIR - CRACKED FUSELAGE SKIN, BS 727D, S23R. REPAIRED FUSELAGE SKIN, BS 727D, S23R IAW USAIRWAYS TYPICAL REPAIR 53-50-03A AND B737-300 SRM 53-00-01 REPAIR 31.Sep 5, 2007 · N591US · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA200707002Skin · crackedA 1.7 INCH CRACK AT STA 500D + 5 STRINGER 15L. INSTALLED EXT FUSELAGE SKIN REPAIR PER EA 98787.Jul 10, 2007 · N591US · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA061404Skin · crackedA 49 INCHES FROM I/B END OF RIGHT O/B AFT FLAP. REMOVED DAMAGE AND INSTALLED FABRICATED REPAIR PARTS IAW SRM 51-70-10, DEFECT SIZE: .25 INCH.Dec 11, 2006 · N591US · Boeing 737301 · Trailing Edge FlapsSDR USAASB06101Socket · corrodedBOS - MAINTENANCE REPORTED THE R2 DOOR EXTERIOR EMERGENCY ESCAPE SLIDE LIGHT, IN THE FUSELAGE, WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT SOCKET DUE TO CORROSION. OPERATIONAL CHECK GOOD.Oct 19, 2006 · N591US · Boeing 737301 · Light System WiringSDR SB06090Splice · damagedCLT - ROW 5ABC EMERGENCY SEAT LIGHT INOPERATIVE. MAINTENANCE FOUND WIRE PULLED OUT OF BUTT SPLICE. REPLACED SPLICE.Sep 13, 2006 · N591US · Boeing 737301 · Light System WiringSDR SB06054Door Seal · leakingDURING CRUISE, EN ROUTE FROM PHL TO ORD, CREW REPORTED THE AUTO PRESSURE CONTROL FAILED AT FL340. CABIN ALTITUDE CLIMBED TO 10,000 FEET AND THE WARNING HORN SOUNDED. CREW ACCOMPLISHED AN EMERGENCY DESCENT TO FL240 AND SELECTED STANDBY MODE WITH BOTH PACKS INMay 23, 2006 · N591US · Boeing 737301 · Cargo/Baggage DoorsSDR USAA060651Skin · crackedFOUND SKIN CRACKED, STA 727E, STR 24L SRM REPAIR 53-00-01, DEFECT SIZE: 3".May 3, 2006 · N591US · Boeing 737301 · Fuselage Main, Plate/SkinSDR SB06045Outflow Valve · faultyDURING CRUISE, CABIN ALT ALERT WARNING HORN SOUNDED, CABIN PRESS CLIMBED. CREW INITIATED AN EMERG DESCENT. AT LOWER ALT, WAS ABLE TO GAIN CONTROL OF CABIN ALT. NO EMERG DECLARED. FLT DIVERTED, LANDED W/O INCIDENT. MX ACCOMP A/C PRESS T/S CARD J321-30-00. May 1, 2006 · N591US · Boeing 737301 · Pressure Regulator/Outflow ValveSDR SB06034Outflow Valve · sticksDURING CRUISE, EN ROUTE FROM BDL TO CLT AT FL340, CREW WAS UNABLE TO CONTROL CABIN IN AUTO, STANDBY OR MANUAL AC PRESSURIZATION MODES. CABIN STOPPED CLIMBING AT 20,000 FEET WHEREAS CREW GAINED CONTROL OF CABIN AT 14,000 FEET. FLIGHT CONTINUED TO CLT AND LANDApr 6, 2006 · N591US · Boeing 737301 · Pressure Regulator/Outflow ValveSDR SB06028Indicator · faultyON APPROACH TO YYZ FROM PHL, AS CREW SET FLAPS TO 10 UNITS, THE LEFT SIDE STOPPED AT 5 UNITS AND THE FLAPS LOCKED OUT. CAPTAIN ELECTED TO PERFORM A GO-AROUND AND REVIEW QUICK REFERENCE HANDBOOK PROCEDURES. FLAPS WERE CYCLED AND WENT TO 10 UNITS, THEN EXTENDEMar 19, 2006 · N591US · Boeing 737301 · Trailing Flap Position Indicating SystemSDR USAA051641Frame · crackedSTA 706 FRAME WEB S9L AT I/B RIVET SECURING A/C PSU SUPPORT CRACKED. REMOVED DAMAGE AND INSTALLED, FABRICATED REPAIR PARTS IAW TR 53-10-22, DEFECT SIZE: .187 INCH.Dec 23, 2005 · N591US · Boeing 737301 · Fuselage Main, FrameSDR USAA051643Skin · crackedBS 500D +2 STR 11 LT CRACKED. INSTALLED DOUBLER IAW EA 97191, DEFECT SIZE: 2.5 INCH.Dec 23, 2005 · N591US · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA051644Frame · crackedFRAME 727D LBL 4 TO RBL 4 CRACKED. REMOVED DAMAGED AREAS, FABRICATED AND INSTALLED REPAIR DOUBLERS IAW EA 97220, DEFECT SIZE: .125.Dec 23, 2005 · N591US · Boeing 737301 · Fuselage Main, FrameSDR USAA051585Beam · crackedBS 870, WL 208, RBL 60 CRACKED. EDDY INSPECTION CONFIRMS SMALL AREA OF DISPLACED METAL ON BEAM EDGE IAW SRM 53-60-13, DEFECT SIZE: .5 INCH CRACK.Dec 20, 2005 · N591US · Boeing 737301 · Fuselage Main, StructureSDR USAA051596Frame · crackedFWD SERVICE DOOR CUTOUT FWD FRAME CRACKED AT UPPER STOP FITTING LOWER O/B CORNER. REPLACED FRAME SECTION IAW SRM 51-30, DEFECT SIZE: .25 INCH LONG CRACK.Dec 20, 2005 · N591US · Boeing 737301 · Fuselage Main, FrameSDR USAA051595Frame · crackedSTA 706 FRAME WEB S9R AT I/B RIVET SECURING A/C PSU SUPPORT CRACKED. INSTALLED DOUBLER IAW TYPICAL REPAIR 53-10-22, DEFECT SIZE: .1875 INCH.Dec 20, 2005 · N591US · Boeing 737301 · Fuselage Main, FrameSDR USAA051594Frame · crackedFWD SERVICE DOOR CUTOUT FWD FRAME CRACKED AT UPPER STOP FITTING LOWER O/B CORNER. REPLACED FRAME SECTION IAW SRM 51-30, DEFECT SIZE: .25 INCH LONG CRACK.Dec 20, 2005 · N591US · Boeing 737301 · Fuselage Main, FrameSDR USAA051593Fitting · corrodedMLG SUPPORT BEAM FITTING ASSY HAS FRETTING ON FWD INBOARD AREA AT STABILIZER. REPAIRED, SMALL BLEND OUT, DEFECT SIZE: SMALL 1 INCH AREA OF CORROSION.Dec 20, 2005 · N591US · Boeing 737301 · Fuselage, Landing Gear Attach FittingsSDR USAA051561Angle · corrodedFOUND CORROSION STATION 300-359 LT "Z" ANGLE. ACCOMPLISHED "T" CAP REPAIR DEFECT SIZE: 2" BY 50".Dec 16, 2005 · N591US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA051560Floorbeam · corrodedFOUND CORROSION STATION 328 LBL45. ACCOMPLISHED "T" CAP REPAIR IAW SRM 53-10-2R-5, DEFECT SIZE: 2".Dec 16, 2005 · N591US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA051558Door Frame · crackedFOUND LOWER DOOR FRAME LOWER CORNER CRACKED. INSTALLED DOUBLER IAW EA 97192, DEFECT SIZE: FWD SERVICE DOOR HAS A 2 INCH CRACK.Dec 15, 2005 · N591US · Boeing 737301 · Fuselage Main, StructureSDR USAA051550Skin · crackedLOCATION: IB SIDE OF NR 1 ENGINE PYLON. INSTALLED DOUBLER IAW TR 54-50-07, DEFECT SIZE: .250 IN.Dec 14, 2005 · N591US · Boeing 737301 · Nacelle/Pylon, Plate/SkinSDR USAA051552Skin · crackedRSB 727E RS24, MAJOR REPAIR, CUT OUT CRACK, FABRICATED AND INSTALLED 9.5 IN X 13 IN DOUBLER IAW SRM 53-00-01 FIG 201 DEFECT SIZE: 2TDec 14, 2005 · N591US · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA051551Attach Angle · crackedLOCATION: S12L INTERCOSTAL LWR FWD ATTACH ANGLE AT LB END. MAJOR REPAIR REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-10-02 DEFECT SIZE: .375 IN.Dec 14, 2005 · N591US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA051557Wedge · damagedNR 3 LE SLAT ASSY IB TRAILING EDGE WEDGE. REMOVED DAMAGE ON THE WEDGE. DOUBLER REPAIR IAW 51-30-03 AND SRM 51-70-10 DEFECT SIZE: .6 IN X 8 IN.Dec 14, 2005 · N591US · Boeing 737301 · Leading Edge DevicesSDR USAA051495Wedge · damagedFOUND NR 4 SLAT INBD LOWER CORNER BOTTOM SKIN WORK THROUGH ON TRAILING EDGE WEDGE. MAJOR REPAIR SRM 51-70-10, DEFECT SIZE: 1".Dec 12, 2005 · N591US · Boeing 737301 · Leading Edge DevicesSDR USAA051496Skin · debondedFOUND TRAILING EDGE WEDGE TOP SKIN DISBONDED INBOARD END NUMBER 3 SLAT. MAJOR REPAIR IAW SRM 51-70-10, DEFECT SIZE: 1".Dec 12, 2005 · N591US · Boeing 737301 · Trailing Edge FlapsSDR USAA051491Floorbeam · corrodedFOUND CORRODED STA 986.5 LBL6 TO LBL43. MAJOR REPAIR REMOVED DAMAGE ON FLOORBEAM AND INSTALLED T CAP IAW TR 53-10-05, DEFECT SIZE: .5"X33".Dec 12, 2005 · N591US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA051507Wedge · delaminatedFOUND DELAMINATION INBOARD FOREFLAP TOP SKIN INBOARD END. REMOVED DAMAGE, FABRICATED AND INSTALLED DOUBLER IAW SRM 51-70-10, DEFECT SIZE: 3.5.Dec 12, 2005 · N591US · Boeing 737301 · Trailing Edge FlapsSDR USAA051489Attach Angle · crackedFOUND S15L INTERCOSTAL WEB FWD ATTACH ANGLE AT I/B END IN RADIUS. REMOVED AND REPLACED ANGLE IAW SRM 51-10-02 AND DWG NR 69-16970, DEFECT SIZE: 1/2" CRACK.Dec 9, 2005 · N591US · Boeing 737301 · Fuselage Main, Attach FittingsSDR USAA051486Intercostal · corrodedFOUND INTERCOSTAL CORRODED BETWEEN STA 967 AND STA 986, LBL 18. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-10-02, DEFECT SIZE: 1/4 INCH SPOTS OF CORROSION ON TOP AND BOTTOM OF NUTPLATE HOLES ON INTERCOSTAL 18" LEN.Dec 9, 2005 · N591US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA051474Attach Angle · crackedFOUND CRACK S15L INTERCOSTAL WEB FWD ATTACH ANGLE AT I/B END IN RADIUS. REMOVED AND REPLACED ANGLE IAW SRM 51-10-02 AND DWG 69-16970, DEFECT SIZE: 1/2" CRACK.Dec 8, 2005 · N591US · Boeing 737301 · Fuselage Main, Attach FittingsSDR USAA051475Splice · crackedFOUND SPLICE CRACKED, BS 908 AT STRINGER 5R. REMOVED AND REPLACED STRINGER SPLICE IAW SRM 50-40-02, DEFECT SIZE: 2" CRACK.Dec 8, 2005 · N591US · Boeing 737301 · Fuselage Main, Longeron/StringerSDR USAA051473Floorbeam · corrodedFOUND CORROSION STA 986.5 BELOW TO BL45. REMOVED DAMAGED FABRICATED NEW T CAP AND INSTALLED ON FLOORBEAM IAW 53-10-05, DEFECT SIZE: .5 INCH AREAS OF CORROSION AROUND CLIP NUT HOLES 38 INCHES IN LENGTH.Dec 8, 2005 · N591US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA051469Intercostal · crackedS16L INTERCOSTAL WEB STA 300 CRACKED. REPLACED WITH IDENTICAL PART, FABRICATED WEB FROM .040 INCH 7075=T6, INSTALLED PER SRM 53-10-15.Dec 6, 2005 · N591US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA051468Intercostal · corrodedBETWEEN STA 967 & STA 986 LBL 18 CORRODED. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-10-02, DEFECT SIZE: .25 INCH SPOT OF CORROSION ON TOP & BOTTOM OF NUT PLATE HOLES ON INTERCOSTAL.Dec 6, 2005 · N591US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA051463Skin · damagedLEFT RUDDER SKIN 4 FEET FROM THE BOTTOM. MAJOR REPAIR, REMOVED DAMAGED, LAYED UP AND CURED REPAIR PLYS IAW SRM 51-70-17, DEFECT SIZE: 2 X 12 INCHES.Dec 5, 2005 · N591US · Boeing 737301 · Rudder, Plate/SkinSDR USAA051452Repair · unknownFOUND COMPOSITE REPAIR LOWER SURFACEOF RT ELEVATOR, 26.5" OTBD OF INBD END 3" FWD OF THE T/E. COMPOSITE REPAIR IAW 55-40-01. DEFECT SIZE: COMPOISTE REPAIR AT LOWER SURFACE OF RT ELEVATOR, 26.5" OTBD OF INBD END 3" FWD.Dec 1, 2005 · N591US · Boeing 737301 · Elevator StructureSDR USAA051451Repair · unbondedFOUND RUDDER COMPOSITE REPAIR APROX 7.5" DIA, 24" FWD OF T/E AND 41" UP FROM BOTTOM L/E. COMPOSITE REPAIR IAW SRM 55-40-01, DEFECT SIZE: APPROX 7.5" DIA LOCATED 24" FWD OF T/E AND 41" UP FROM BOTTOM L/E. (RT SIDE)Dec 1, 2005 · N591US · Boeing 737301 · Horizontal Stabilizer Structure
Back to N591US, cancelled Dec 29, 2008