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 USAA060133Skin · scratchedBELOW TAT PROBE AT BS 269 BETWEEN STR 18L AND 19L SCRATCHED. DAMAGE FILE ITEM IAW EA 77892A, DEFECT SIZE: 11 X .250 INCH.Jan 24, 2006 · N784AU · Boeing 7374B7 · Fuselage Main, Plate/SkinSDR USAA060141Support Angle · crackedRAM AIR INLET SUPPORT ANGLE CRACKED AT STA 540 STR 22L. FABRICATED STRAP AND RADIUS FILLERS PER TR 53-50-03, DEFECT SIZE: .5 INCH.Jan 24, 2006 · N784AU · Boeing 7374B7 · Fuselage Main, StructureSDR USAA060140Floorbeam · crackedCARGO FLOORBEAM RBL 17 STA 747 CRACKED. REPLACED FLOORBEAM IAW SRM 53-00-53, DEFECT SIZE: 1 INCH.Jan 24, 2006 · N784AU · Boeing 7374B7 · Fuselage Main, Floor BeamSDR USAA060139Shear Tie · damagedHOLE IN SHEAR TIE BETWEEN STRINGER 13R AND 14R AT BS 500C. REMOVED MIS-DRILLED LEG AND FABRICATED & INSTALLED REPAIR LEG IAW EA 97321.Jan 24, 2006 · N775AU · Boeing 7374B7 · Fuselage Internal Mounting StructureSDR USAA060138Angle · crackedSTA 277 - 291 BETWEEN 12R AND 13R CRACKED. REPLACED ANGLE IAW SRM 51-40-02, DEFECT SIZE: .5 INCH.Jan 24, 2006 · N775AU · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA060137Strap · corrodedAFT CARGO DOOR THRESHOLD STRAP CORROSION. REMOVED AND INSTALLED NEW STRAP IAW SRM 53-60-15, DEFECT SIZE: 10 INCHES.Jan 24, 2006 · N775AU · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA060134Floorbeam · corrodedFLOORBEAM STA 312 LBL 6 - RBL 1 CORROSION. REPLACED T-CAP IAW SRM 53-10-51, DEFECT SIZE: 7 X 2 INCHES.Jan 24, 2006 · N775AU · Boeing 7374B7 · Fuselage Main, Floor BeamSDR USAA060132Skin · damagedAT 22 INCHES DOWN FROM TOP EDGE OF DOOR SKIN & AFT EDGE OF DOOR SKIN DAMAGED. INSTALLED DOUBLER IAW SRM 52-00-01, DEFECT SIZE: 3 X 3 INCHES.Jan 24, 2006 · N784AU · Boeing 7374B7 · Cargo/Baggage DoorsSDR USAA060126Rib · crackedLT WING 135.5 RIB LOWER CHORD ANGLE CRACK BETWEEN S2 AND S3. FABRICATED REPAIR PARTS AS PER GIVEN EA TRIMMED TEE REPAIR FAB FILLERS IAW EA 97288, DEFECT SIZE: 2.5 INCH.Jan 23, 2006 · N775AU · Boeing 7374B7 · Wing, Rib/BulkheadSDR USAA060125Intercostal · corrodedBETWEEN STA 312 AND 328 CORROSION. REPLACED INTERCOSTAL IAW SRM 51-40-02, DEFECT SIZE: 16 X 1 INCH.Jan 23, 2006 · N775AU · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA060131Repair · not an sdrAPPROX 33 INCHES OUT FROM INBOARD END OF REMOVABLE L/E PREVIOUS REPAIR. FLUSH REPAIR IAW 55-10-01 REPAIR 2, DEFECT SIZE: 5.5 X 5.5 INCHES.Jan 23, 2006 · N784AU · Boeing 7374B7 · Aircraft StructuresSDR USAA060130Repair · not an sdrAPPROX 33 INCHES OUT FROM INBOARD END OF REMOVABLE L/E PREVIOUS REPAIR. FLUSH REPAIR IAW 55-10-01 REPAIR 2, DEFECT SIZE: 5.5 X 5.5 INCHES.Jan 23, 2006 · N784AU · Boeing 7374B7 · Aircraft StructuresSDR USAA060128Angle · crackedSTA 294 BELOW UPPER SERVICE DOOR HINGE CUTOUT CRACKED. REPLACED WITH IDENTICAL PART, REPLACED ANGLE IAW SRM 51-40-02, DEFECT SIZE: 1 INCH.Jan 23, 2006 · N775AU · Boeing 7374B7 · Fuselage, Door HingeSDR USAA060127Frame · crackedSTATION 480 FRAME WEB LEFT SIDE IS CRACKED AT THE INBOARD RIVET FOR PSU. INSTALLED DOUBLER IAW TR 53-10-20C, DEFECT SIZE: .375.Jan 23, 2006 · N775AU · Boeing 7374B7 · Fuselage Main, FrameSDR SB06009Clamp · brokenDURING CRUISE, CABIN ALTITUDE WARNING HORN SOUNDED AS CABIN WAS CLIMBING THROUGH 10,500 FEET. CREW ACCOMPLISHED QUICK REF PROCEDURES WHICH REQUIRED THEM TO DEPLOY CABIN OXYGEN MASKS. CREW TRIED SEVERAL MODES TO RECOVER CABIN WITH NO HELP. FLIGHT DIVERTED AND LJan 22, 2006 · N427US · Boeing 7374B7 · Cabin Pressure Control SystemSDR USAA060123Floorbeam · corrodedBS 967 FROM LBL 16 TO RBL 30 CORRODED. REMOVED DAMAGE AND INSTALLED FABRICATED T-CAP IAW SRM 51-20-01, DEFECT SIZE: .50 INCH.Jan 20, 2006 · N775AU · Boeing 7374B7 · Fuselage Main, Floor BeamSDR USAA060122Repair · unknownSKIN REPAIR - 60 INCHES I/B OF O/B END. UPDATED SDA, DEFECT SIZE: 60 INCHES.Jan 20, 2006 · N775AU · Boeing 7374B7 · Aircraft StructuresSDR USAA060121Frame · crackedSTA 400 BETWEEN S-8R AND S-9R CRACKED. INSTALLED DOUBLERS IAW TR 53-10-20C, DEFECT SIZE: .437 INCH.Jan 20, 2006 · N775AU · Boeing 7374B7 · Fuselage Main, FrameSDR USAA060120Rib · crackedLEFT WING WBL 135.5 RIB LOWER CHORD BETWEEN STR 2 & 3. REMOVED CRACKED SECTION IAW EA 97282, DEFECT SIZE: .875 INCH.Jan 20, 2006 · N784AU · Boeing 7374B7 · Wing, Rib/BulkheadSDR USAA060119Frame · crackedBS 400 AT PSU RAIL BETWEEN STRINGER 8 AND 9 RT. CUT OUT DAMAGED AREA. INSTALLED REPAIR DOUBLERS IAW TR 53-10-20C AND EA 97304, DEFECT SIZE: .250 INCH.Jan 20, 2006 · N784AU · Boeing 7374B7 · Fuselage Main, FrameSDR USAA060118Floorbeam · corrodedTOP OF BS 947.5 FLOORBEAM AT LBL 4 CORRODED. REPLACED T-CAP IAW TR 53-60-02, DEFECT SIZE: 1.0 INCH.Jan 20, 2006 · N775AU · Boeing 7374B7 · Fuselage Main, Floor BeamSDR USAA060117Bushing · migratedVERTICAL STAB, LEFT FWD CENTER LUG BUSHING MIGRATED. REMOVED MIGRATED BUSHING AND REPLACED WITH NEW FABRICATED BUSHING IAW EA 97296, DEFECT SIZE: .010 INCH.Jan 20, 2006 · N775AU · Boeing 7374B7 · Vertical StabilizerSDR USAA060124Support Angle · corrodedBS 994 FROM LBL 33 TO LBL 46 CORRODED. REMOVED CORROSION AND REPLACED PART IAW BOEING DWG 69-77477-1, DEFECT SIZE: 4"X1".Jan 20, 2006 · N775AU · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA060086Clevis · corrodedFOUND CORROSION VERTICAL STAB INNERSPAR BOX. REMOVED CORROSION AND INSTALLED REPAIR PARTS AS REQUIRED IAW SRM 51-20-01 BOEING DWG 65-53744 DEFECT SIZE:Jan 18, 2006 · N775AU · Boeing 7374B7 · Vertical Stabilizer, Attach FittingsSDR USAA060095Crease Beam · corrodedFOUND CORROSION VS 727-727A S -17R CREASE BEAM WEB. REMOVED CORRODED WEB, FABRICATED AND INSTALLED NEW WEB IAW SRM 53-60-13, BOEING DWG 65-46822, DEFECT SIZE: .50" BY .50".Jan 18, 2006 · N784AU · Boeing 7374B7 · Fuselage Main, StructureSDR USAA060094Crease Beam · damagedFOUND CREASE BS 953 TO BS 994 AT LT CREASE BEAM INNER CHORD. REMOVED AND REPLACED Z ANGLE IAW SRM 51-20-01, DEFECT SIZE: 40".Jan 18, 2006 · N775AU · Boeing 7374B7 · Fuselage Main, StructureSDR USAA060093Skin · crackedFOUND CRACK NR 1 ENGINE PYLON I/B SIDE AROUND ACCESS HOLE 5724. DOUBLER INSTALLED IAW TR 54-30-10, DEFECT SIZE: 1".Jan 18, 2006 · N775AU · Boeing 7374B7 · Nacelle/Pylon, Plate/SkinSDR USAA060092Repair · unknownFOUND PREVIOUS REPAIR NR 2 SLAT LOWER T/E SURFACE BELOW ACTUATOR. FABRICATED DOUBLER IAW TR 54-43-01, DEFECT SIZE: 24" BY 4".Jan 18, 2006 · N775AU · Boeing 7374B7 · Aircraft StructuresSDR USAA060091Repair · unknownFOUND PREVIOUS REPAIR UPPER I/B T/E WEDGE SURFACE. FABRICATED DOUBLER IAW TR 57-42-01, DEFECT SIZE: 3" BY 5".Jan 18, 2006 · N775AU · Boeing 7374B7 · Aircraft StructuresSDR USAA060090Repair · unknownFOUND PREVIOUS REPAIR NR 2 SLAT UPPER O/B T/E WEDGE SURFACE. FABRICATED DOUBLER IAW 57-42-02, DEFECT SIZE: 3" BY 5".Jan 18, 2006 · N775AU · Boeing 7374B7 · Aircraft StructuresSDR USAA060089Repair · unknownFOUND PREVIOUS REPAIR STA 179 BETWEEN S-16L AND S-15L. FABRICATED DOUBLER IAW EO 5300V157, DEFECT SIZE: 3" BY 5".Jan 18, 2006 · N775AU · Boeing 7374B7 · Aircraft StructuresSDR USAA060087Bushing · migratedFOUND LUG BUSHING MIGRATING VERTICAL STAB LEFT FWD CENTER LUG BUSHING. REMOVED MIGRATED BUSHING AND REPLACED WITH NEW FABRICATED BUSHING IAW EA 97296, DEFECT SIZE:Jan 18, 2006 · N775AU · Boeing 7374B7 · Vertical StabilizerSDR USAA060077Repair · unknownFOUND PREVIOUS REPAIR LWR SURFACE O/B T/E. UPDATED SDA, IAW TR 57-42-01, DEFECT SIZE: 6" BY 3".Jan 18, 2006 · N775AU · Boeing 7374B7 · Standard Practices/StructuresSDR USAA060085Clevis · corrodedFOUND VERTICAL STAB INNERSPAR BOX. REPLACED WITH IDENTICAL PART, REPLACED CLEVIS IAW BOEING DWG 65-53744 AND SRM 51-20-01, DEFECT SIZE: UNKNOWN.Jan 18, 2006 · N775AU · Boeing 7374B7 · Vertical Stabilizer, Attach FittingsSDR USAA060084Support Angle · corrodedFOUND CORROSION BS 994 FROM LBL 33 TO LBL 46. REMOVED CORROSION AND REPLACED PART IAW BOEING DWG 69-77477-1, DEFECT SIZE: 4" BY 1".Jan 18, 2006 · N775AU · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA060083Bushing · corrodedFOUND CORROSION RT MLG UPLOCK LUG BUSHING. REMOVED DAMAGE AND INSTALLED SLEEVE IAW EEA 97302 SRM 53-60-14 , DEFECT SIZE: .250.Jan 18, 2006 · N784AU · Boeing 7374B7 · Main Landing GearSDR USAA060082Repair · unknownFOUND PREVIOUS REPAIR NR 2 SLAT LOWER T/E SURFACE BELOW ACTUATOR. FABRICATED DOUBLER THAT MEASURES 24" BY 4" IAW TR 54-43-01, DEFECT SIZE: 24" BY 4".Jan 18, 2006 · N775AU · Boeing 7374B7 · Aircraft StructuresSDR USAA060081Frame · damagedFRAME RIVETS MISSING, BS 480 2" ABOVE FLOOR LEVEL. INSTALLED TWO FASTENERS IAW SRM 51-10-02, DEFECT SIZE: 2".Jan 18, 2006 · N775AU · Boeing 7374B7 · Fuselage Main, FrameSDR USAA060080Skin · crackedFOUND CRACK NR 1 ENGINE PYLON I/B SIDE AROUND ACCESS HOLE 5724. DOUBLER INSTALLED IAW TR 54-30-10, DEFECT SIZE: 1".Jan 18, 2006 · N775AU · Boeing 7374B7 · Nacelle/Pylon, Plate/SkinSDR USAA060079Repair · unknownFOUND PREVIOUS REPAIR I/B T/E WEDGE. DOUBLER INSTALLED IAW TR 57-42-03 DEFECT SIZE: 4" BY 4".Jan 18, 2006 · N775AU · Boeing 7374B7 · Aircraft StructuresSDR USAA060078Repair · unknownFOUND PREVIOUS REPAIR, UPPER T/E SURFACE. DOUBLER INSTALLED IAW TR 57-42-03 DEFECT SIZE: 4" BY 4".Jan 18, 2006 · N775AU · Boeing 7374B7 · Aircraft StructuresSDR USAA060088Clevis · corrodedFOUND CORROSION VERTICAL STAB INNERSPAR BOX. REMOVED CORROSION AND INSTALLED REPAIR PARTS IAW BOEING DWG 65-53744 AND 737/400 SRM 51-20-01 DEFECT SIZE:Jan 18, 2006 · N775AU · Boeing 7374B7 · Vertical Stabilizer, Attach FittingsSDR USAA060066Repair · unknownFOUND PREVIOUS REPAIR LE VERTICAL FIN 70" DOWN FROM TOP. MAJOR REPAIR: UPDATED SDA AS REQUIRED IAW SRM 55-30-01. DEFECT SIZE: PREVIOUS REPAIR ON VERTICAL FIN REMOVABLE L/E 70" DOWN FROM TOP END 28" BY 18" DOUBLER.Jan 17, 2006 · N775AU · Boeing 7374B7 · Aircraft StructuresSDR USAA060076Repair · unknownFOUND SLAT SKIN WITH PREVIOUS REPAIR, LWR T/E BY AUX TRACK. SDA UPDATED AS REQUIRED IAW TR 54-43-01, DEFECT SIZE: 12" BY 4".Jan 17, 2006 · N775AU · Boeing 7374B7 · Aircraft StructuresSDR USAA060056Repair · unknownFOUND SKIN WITH PREVIOUS REPAIR, BS 178 S17L. EXTERNAL DOUBLER REPAIR IAW SRM 53-30-01, DEFECT SIZE: 2" BY 7".Jan 17, 2006 · N784AU · Boeing 7374B7 · Aircraft StructuresSDR USAA060057Skin · delaminatedFOUND NR 1 SLAT DELAMINATION UPPER OTBD END OF T/E WEDGE. REMOVED DAMAGE, INSTALLED CORE AND DOUBLER IAW SRM 51-70-10, DEFECT SIZE: 4.750" BY 5.250".Jan 17, 2006 · N784AU · Boeing 7374B7 · Leading Edge DevicesSDR USAA060058Frame · crackedFOUND FRAME CRACK STA 480 FRAME AT LT PSU RAIL SUPPORT. INSTALLED REPAIR DOUBLERS IAW TR 53-10-20C, DEFECT SIZE: .25".Jan 17, 2006 · N784AU · Boeing 7374B7 · Fuselage Main, FrameSDR USAA060059Skin · delaminatedFOUND SLAT DELAMINATION RT WING NR 5 LE SLAT OUTBD END. INSTALLED DOUBLER IAW SRM 51-70-10, DEFECT SIZE: 1 INCH DELAMINATION.Jan 17, 2006 · N784AU · Boeing 7374B7 · Leading Edge DevicesSDR USAA060060Stringer Clip · crackedFOUND TIE CLIP CRACKED, BS 500C, S-21R. REMOVED AND REPLACED TIE CLIP IAW SRM 51-40-02, DEFECT SIZE: SHEETMETAL. 0350- S-21R TIE CLIP CRACKED AT BS 500C. THE CRACK MEASURES .25 INCHES.Jan 17, 2006 · N775AU · Boeing 7374B7 · Fuselage Main, Attach FittingsSDR USAA060061Support Angle · crackedFOUND CRACK STA 616, LBL 64.5. INSTALLED DOUBLER PER TYPICAL REPAIR 53-62-01 FIG 2, DEFECT SIZE: .25 CRACK, CABIN AT EMERG EXIT STA 616, LBL 64.5 SUPPORT ANGLE CRACKED.Jan 17, 2006 · N775AU · Boeing 7374B7 · Fuselage Miscellaneous Structure
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