Boeing 737-4B7

Service difficulty reports · 5,757

Newest first. General aviation reporting is voluntary.

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 = '7374B7'
  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 USAA051159Flange · crackedFOUND FUSELAGE CRACKED STATION 559 STRINGER 13L. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR ANGLE IAW EA 96912, DEFECT SIZE: .7".Sep 30, 2005 · N782AU · Boeing 7374B7 · Fuselage Main, FrameSDR USAA051158Stiffener · corrodedFOUND STIFFENER CORRODED FUSELAGE STATION 336 RBL 51 TO 59. REMOVED AND REPLACED STIFFENER IAW SRM 51-40-0, DEFECT SIZE: .75 BY 5".Sep 30, 2005 · N443US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA051157Skin · wornFOUND FLAP SKIN WORN OUTBOARD MID FLAP LEADING EDGE SKIN AT WING STATION 196.8461. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-53-1, REPAIR 8 DEFECT SIZE: 3.5X.75".Sep 30, 2005 · N443US · Boeing 7374B7 · Trailing Edge FlapsSDR USAA051156Angle · corrodedLEFT TRANSITION ANGLE BS 727 - 835 FOUND CORRODED. REPLACED ANGLE IAW SRM 53-60-53, DEFECT SIZE: CORROSION IN AREA'S FROM BS 727E TO 835.Sep 30, 2005 · N782AU · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA051155Skin · delaminatedINBD END OF FLAP DELAMINATED. REMOVED DAMAGE AND REPAIRED IAW SRM 51-70-10, DEFECT SIZE: 6" BY 2".Sep 30, 2005 · N782AU · Boeing 7374B7 · Trailing Edge FlapsSDR USAA051152Angle · crackedANGLE CRACKED STA 360 AND STR 9L. FABRICATED NEW ATTACH ANGLE AND INSTALLED IAW DWG 69-48985, SRM 1-10-02, DEFECT SIZE: .50".Sep 28, 2005 · N443US · Boeing 7374B7 · Fuselage Main, Attach FittingsSDR USAA051153Clip · crackedCLIP CRACKED BS 772, RBL 20, AFT CARGO COMPARTMENT. REPLACED CLIP WITH NEW PART IAW SRM 51-10-02, DEFECT SIZE: .5".Sep 28, 2005 · N782AU · Boeing 7374B7 · Fuselage Main, Attach FittingsSDR USAA051144Stringer · crackedSTRINGER CRACKED STA 303.9, S10L. REMOVED DAMAGE, FABRICATED REPAIR DOUBLER AND INSTALLED PER EA 96914, DEFECT SIZE: .25".Sep 26, 2005 · N782AU · Boeing 7374B7 · Fuselage Main, Longeron/StringerSDR USAA051145Skin · wornWORN AREA OB FLAP LEADING EDGE AT IB END. REMOVED DAMAGE AND INSTALLED FABRICATED REPAIR PARTS IAW SRM 57-53-01 REPAIR 8 PG 204, DEFECT SIZE: 1".Sep 26, 2005 · N443US · Boeing 7374B7 · Trailing Edge FlapsSDR USAA051146Attach Angle · crackedFOUND ANGLE CRACKED, STA 967 ABOVE AFT ENTRY DOOR. REMOVED DAMAGE AND INSTALLED FABRICATED REPAIR PARTS IAW SRM 53-00-07, DEFECT SIZE: .250".Sep 26, 2005 · N443US · Boeing 7374B7 · Fuselage Main, Attach FittingsSDR USAA051147Sill · corrodedZEE ANGLE AT AFT ENTRANCE DOOR SILL AROUND NUTPLATES BETWEEN STA 967 AND 986. REMOVED DAMAGE AND REINSTALLED FABRICATED REPAIR PARTS IAW SRM 51-70-11, DEFECT SIZE: 20".Sep 26, 2005 · N443US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA051148Skin · crackedFOUND SKIN CRACKED IL I/B MID FLAP 39" FROM O/B END. REMOVED DAMAGE AND INSTALLED REPAIR PARTS IAW SRM 57-53-01, DEFECT SIZE: .25".Sep 26, 2005 · N782AU · Boeing 7374B7 · Trailing Edge FlapsSDR USAA051149Skin · crackedLT WING SKIN FWD OF FRONT SPAR O/B SIDE OF PYLON. REMOVED DAMAGED SKIN, FABRICATED AND INSTALLED REPAIR PIECES, DEFECT SIZE: 1".Sep 26, 2005 · N782AU · Boeing 7374B7 · Wing, Plate/SkinSDR USAA051150Skin · crackedNR 1 ENG PYLON, ACCESS PNL OPENING NR 5727L. REPAIR DOUBLER INSTALLED IAW TYP REP 54-30-07, DEFECT SIZE: .400".Sep 26, 2005 · N782AU · Boeing 7374B7 · Nacelle/Pylon, Plate/SkinSDR USAA051151Skate Angle · wornRIGHT SIDE BS 1016 L/E STATION 0.0. FABRICATED AND INSTALLED A NEW SKATE ANGLE IAW TYP REP 53-20-05A, DEFECT SIZE: .5" X 1.3".Sep 26, 2005 · N782AU · Boeing 7374B7 · Fuselage Main, StructureSDR SB05122Seal · missingCLT - FLT 1169 DURING CRUISE, AT FL240, THE AIRCRAFT BEGAN LOSING CABIN PRESSURIZATION WHILE OPERATING ON ONE PACK. CABIN PRESSURE COULD NOT BE STABILIZED. FLIGHT DESCENDED TO 10,000 FEET WHERE CABIN PRESSURE DROPPED TO 7,000 FEET. FLIGHT CONTINUED ONTO CSep 24, 2005 · N433US · Boeing 7374B7 · Pressure Regulator/Outflow ValveSDR SB05121Battery Pack · dischargedCLT - DURING EMERGENCY LIGHT OPERATIONAL TEST, MAINTENANCE REPORTED THE LEFT AFT OVERWING EXIT LIGHT ON THE SIDEWALL EXTINGUISHED AND WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK FOR CHARGER ASSEMBLY M1435 PER MM 33-51-51. OPERATIONAL TSep 24, 2005 · N440US · Boeing 7374B7 · Emergency LightingSDR USAA051143Skin · crackedFOUND LT WING SKIN CRACKED, FWD OF FRONT SPAR O/B SIDE OF PYLON. REMOVED DAMAGED SKIN, FABRICATED AND INSTALLED REPAIR PIECES IAW TR 57-41-023.Sep 23, 2005 · N782AU · Boeing 7374B7 · Wing, Plate/SkinSDR USAA051140Intercostal · crackedINTERCOSTAL CRACKED LBL 45 BETWEEN STA 312 AND 328. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-40-02, DEFECT SIZE: .250" CRACK.Sep 22, 2005 · N443US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA051141Intercostal · crackedINTERCOSTAL CRACKED, LBL 45 BETWEEN STA 328 AND 344. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-40-02, DEFECT SIZE: .375" CRACK.Sep 22, 2005 · N443US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA051142Frame · crackedFRAME CRACKED BS 380 JUST BELOW STR 8L. CUT OUT CRACKED AREA, INSTALLED REPAIR PER T/R 53-10-20B, DEFECT SIZE: APPROX 1 INCH CRACK.Sep 22, 2005 · N782AU · Boeing 7374B7 · Fuselage Main, FrameSDR USAA051133Skin · crackedFOUND FUSELAGE CRACKED, BS 380 JUST BELOW S-8L. CUTOUT CRACKED AREA INSTALLED REPAIR PER T/R 53-10-20B, DEFECT SIZE: 1".Sep 21, 2005 · N782AU · Boeing 7374B7 · Fuselage Main, Plate/SkinSDR USAA051134Intercostal · corrodedFOUND INTERCOSTAL CORRODED BETWEEN STATION 312 AND 328. MAJOR REPAIR IAW SRM 51-40-02, DEFECT SIZE: 3/16".Sep 21, 2005 · N443US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA051135Floorbeam · corrodedFOUND FLOORBEAM T-CAP CORRODED STATION 312 LBL 10 TO RBL 36. T-CAP REPLACED IAW SRM 53-10-51-2R-5, DEFECT SIZE: 2" X 6".Sep 21, 2005 · N443US · Boeing 7374B7 · Fuselage Main, Floor BeamSDR USAA051136Stringer Clip · crackedFOUND TIE CLIP CRACKED STA 500 G STRINGER 8R. DEFECTIVE PART REPLACED WITH IDENTICAL PART, REMOVED AND REPLACED STRINGER TIE CLIP IAW SRM 51-40-02, DEFECT SIZE: .250".Sep 21, 2005 · N443US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA051137Splice · crackedFOUND STRINGER CRACKED BS 360 STRINGER 15L. REPLACED WITH IDENTICAL PART, REMOVED AND REPLACED STRINGER SPLICE IAW SRM 51-40-02, DEFECT SIZE: .250".Sep 21, 2005 · N443US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA051138Stringer Clip · crackedFOUND TIE CLIP CRACKED, BS 500F S-8R. REPLACED WITH IDENTICAL PART, REMOVED AND REPLACED STRINGER TIE CLIP IAW SRM 51-40-02, DEFECT SIZE: .250".Sep 21, 2005 · N443US · Boeing 7374B7 · Fuselage Main, Attach FittingsSDR USAA051139Stringer Clip · crackedTIE CLIP CRACKED, STA 787L STRINGER 4L. REPLACED WITH IDENTICAL PART, REMOVED AND REPLACED STRINGER TIE CLIP IAW SRM 51-40-02, DEFECT SIZE: .025.Sep 21, 2005 · N443US · Boeing 7374B7 · Fuselage Main, Attach FittingsSDR SB05118Connector · burnedBOS - FLT822 - ON FINAL APPROACH TO BOS, THE TR2 AND TR3 CIRCUIT BREAKERS POPPED. CREW INITIATED A GO-AROUND THE FIELD AND POWERED UP THE APU. EVERYTHING WAS NORMAL FOR LANDING. UPON SECOND FINAL APPROACH, THE SAME THING HAPPENED AS WITH THE FIRST APPROACH.Sep 21, 2005 · N430US · Boeing 7374B7 · Nacelle/Pylon System WiringSDR USAA051094Splice · damagedFOUND SPLICE BS907, STRINGER S4R. REMOVED DAMAGED PARTS, AND INSTALLED NEW PARTS IAW SRM 51-10-02, DEFECT SIZE: 1/2" CRACK.Sep 20, 2005 · N782AU · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA051108Attach Fitting · corrodedFOUND CORROSION LT HORIZ STAB L5 BUSHING LUG FACE. REMOVE CORROSION AND BUSHING IAW SRM 55-10-10, DEFECT SIZE: 1" X 2" AREA OF CORROSION.Sep 20, 2005 · N782AU · Boeing 7374B7 · Horizontal Stabilizer, Attach FittingsSDR USAA051132Pressure Panel · crackedFOUND CRACK STA 665, LBL 30. FABRICATED AND INSTALLED FILLER AND DOUBLER IAW TR 53-60-04, DEFECT SIZE: 1.0" CRACK.Sep 20, 2005 · N782AU · Boeing 7374B7 · Fuselage Main, BulkheadSDR USAA051099Attach Bracket · crackedFOUND CRACK STA 500G, S28L. FAB NEW ANGLE FROM 2024-T3 .040 PER DWG 65C33472 IAW BOEING DWG 69-73527, SRM 51-10-02, DEFECT SIZE: .250" CRACK IN RADIUS.Sep 20, 2005 · N782AU · Boeing 7374B7 · Fuselage Main, Attach FittingsSDR USAA051100Stringer · crackedFOUND CRACK PRODUCTION SEAM AT STA 907 IN STR 4L. REMOVED CRACKED STRINGER SPLICE, INST NEW P/N 1122424 STR SPLICE, CLIP AND LADDER IAW SRM 51-10-02, DEFECT SIZE: PRODUCTION SEAM AT STA 907 IN STR 4L. (MARKED)Sep 20, 2005 · N782AU · Boeing 7374B7 · Fuselage Main, Longeron/StringerSDR USAA051101Web · crackedFOUND CRACK 500G, S-27R. FAB FILLER AND DOUBLER PER SRM 51-70-11, DEFECT SIZE: 0.25" CRACK IN WEB.Sep 20, 2005 · N782AU · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA051103Attach Fitting · corrodedFOUND FWD FACE OF L4 LUG FWD CLEVIS OF LT HOR STAB. REMOVED CORROSION AND INSTALLED BUSHING IAW SRM 55-10-10, DEFECT SIZE: 1" X 2" AREA OF CORROSION.Sep 20, 2005 · N782AU · Boeing 7374B7 · Horizontal Stabilizer, Attach FittingsSDR USAA051104Attach Fitting · corrodedFOUND CORROSION RT HORIZ STAB FORWARD LWR CLEVIS AFT BUSHING AFT FACE. REMOVED CORROSION AND INSTALLED BUSHING IAW SRM 55-10-10, DEFECT SIZE: 1" X 2" AREA OF CORROSION.Sep 20, 2005 · N782AU · Boeing 7374B7 · Horizontal Stabilizer, Attach FittingsSDR USAA051105Attach Fitting · corrodedFOUND CORROSION FWD FACE OF L13 HOR STAB LUG. REMOVED CORROSION AND INSTALLED BUSHING IAW SRM 55-10-10, DEFECT SIZE: 1" X 2" AREA OF CORROSION.Sep 20, 2005 · N782AU · Boeing 7374B7 · Horizontal Stabilizer, Attach FittingsSDR USAA051127Stringer · crackedFOUND FUSELAGE STR SPLICE AT STA 907 STR 4L. INSTALLED STRINGER SPLICE IAW SRM 51-40-02, DEFECT SIZE: .75" CRACK.Sep 20, 2005 · N776AU · Boeing 7374B7 · Fuselage Main, Longeron/StringerSDR USAA051107Bushing · corrodedFOUND CORROSION LT HORIZ STAB, FWD L2 LUG BUSHING. REMOVED CORROSION AND INSTALLED BUSHING IAW SRM 55-10-10, DEFECT SIZE: 1" X 2" AREA OF CORROSION.Sep 20, 2005 · N782AU · Boeing 7374B7 · Horizontal Stabilizer StructureSDR USAA051109Bushing · corrodedFOUND CORROSION LT HORIZ STAB L14 AFT BUSHING. REWORKED AREA AND INSTALLED BUSHING IAW SRM 55-10-10, DEFECT SIZE: 1" X 2" AREA OF CORROSION.Sep 20, 2005 · N782AU · Boeing 7374B7 · Horizontal Stabilizer StructureSDR USAA051128Skin · chafedFOUND CHAFING UPPER FUSELAGE EXT SKIN DBLR UNDER DORSAL FIN STA 864 BL=0. REMOVED DBLR, FILLER, SKIN AND TEAR STRIP, FABBED AND INSTALLED NEW PER EA 96859, DEFECT SIZE: 5-3/4" X 7".Sep 20, 2005 · N776AU · Boeing 7374B7 · Fuselage Main, Plate/SkinSDR USAA051129Frame · crackedFOUND CRACK STA 907 STR 1. INSTALLED FRAME ANGLE REPAIR PER SRM 53-00-07, DEFECT SIZE: 1".Sep 20, 2005 · N776AU · Boeing 7374B7 · Fuselage Main, FrameSDR USAA051130Splice · crackedFOUND CRACK FUSELAGE STRINGER SPLICE AT STA 907 STR 4R. INSTALLED STRINGER SPLICE IAW SRM 51-40-02, DEFECT SIZE: .25".Sep 20, 2005 · N776AU · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA051131Frame · damagedBS 294.5, S-17R, CUT OUT DAMAGE, FABRICATED NEW ATTACH ANGLE AND INSTALLED IAW SRM 51-70-11 TABLE 5 OF FIG NR 1, DEFECT SIZE: .5" CRACKED DOOR FRAME.Sep 20, 2005 · N782AU · Boeing 7374B7 · Fuselage Main, FrameSDR USAA051106Attach Fitting · corrodedFOUND CORROSION AFT FACE OF L6 HORIZ STAB LUG. REMOVED CORROSION AND INSTALLED BUSHING IAW SRM 55-10-10, DEFECT SIZE: 1" X 2" AREA OF CORROSION.Sep 20, 2005 · N782AU · Boeing 7374B7 · Horizontal Stabilizer StructureSDR USAA051093Stringer Clip · crackedFOUND CRACK STA 827, S4L. REMOVED DAMAGED PART, INSTALLED NEW IAW SRM 51-10-02 3.C (3), DEFECT SIZE: .125" CRACK.Sep 20, 2005 · N782AU · Boeing 7374B7 · Fuselage Main, Attach FittingsSDR USAA051095Stringer Clip · crackedFOUND TIE CLIP CRACKED AT STA 767, STR 2L. REPLACED TIE CLIP IAW SRM 51-10-02.Sep 20, 2005 · N782AU · Boeing 7374B7 · Fuselage Main, Attach FittingsSDR USAA051096Attach Bracket · crackedFOUND CRACK O/H DUCT ATTACH BRACKET AT STA 767 STR 1. FABRICATED AND INSTALLED IAW SRM 51-10-02 AND BOEING DWG 69-47869, DEFECT SIZE: 1/4" CRACK AT BRACKET.Sep 20, 2005 · N782AU · Boeing 7374B7 · Fuselage Main, Attach FittingsSDR USAA051097Frame · damagedSTA 294, S-16L AFT OF FRAME, NEW PART, INSTALLED WITH LOCK FASTENERS IAW SRM 51-10-02, DEFECT SIZE: SHEETMETAL NR 4365, WEB CRACKED (APPROX 1.5 INCHES LONG) S-161, AFT OF BS 294 FRAME.Sep 20, 2005 · N782AU · Boeing 7374B7 · Fuselage Main, Frame
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