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 USAA051290Floorbeam · corrodedFOUND FLOORBEAM CORRODED AT 328, CORROSION AROUND CLIP NUT HOLES RBL 10 TO Z-ANGLE AT FWD SER. CLEANED CORROSION ALODINED AND PRIMED EXCEPT RBL 21 (OUT OF SRM LIMITS) IAW SRM 51-10-51, TR53-15-01B, DEFECT SIZE: .500 DIA CORRODED AREAS.Nov 1, 2005 · N779AU · Boeing 7374B7 · Fuselage Main, Floor BeamSDR USAA051273Frame · corrodedFOUND FRAME CORRODED AT STATION 867 BETWEEN S27L AND S27R. REMOVED MINOR CORROSION AND THREE FASTENERS IN THE AREA. INSTALLED NEW FASTNERS IAW SRM 53-00-07, DEFECT SIZE: .4" BY .2".Oct 31, 2005 · N779AU · Boeing 7374B7 · Fuselage Main, FrameSDR USAA051270Structure · crackedUPPER CHORD CORRODED BETWEEN BS 380 AND BS400 AT BL0. REMOVED AND REPLACED UPPER CHORD IAW SRM 51-10-02 BOEING DWG 69-35365, DEFECT SIZE: 1.5".Oct 31, 2005 · N779AU · Boeing 7374B7 · Fuselage Main, StructureSDR USAA051272Angle · corrodedFOUND Z ANGLE CORRODED AT LT ENTRY DOOR. REMOVED OLD Z ANGLE AND REPLACED WITH NEW PART IAW SRM 51-20-05, DEFECT SIZE: .75" BY 8".Oct 31, 2005 · N779AU · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA051274Floorbeam · corrodedFOUND FLOORBEAM CORRODED, STATION 1016 RIGHT. REMOVED MINOR CORROSION TREATED AND PRIMED IAW SRM 53-60-01, DEFECT SIZE: 1" BY 4".Oct 31, 2005 · N779AU · Boeing 7374B7 · Fuselage Main, Floor BeamSDR USAA051279Floorbeam · corrodedFOUND FLOORBEAM CORRODED, STA 947, RTB 6 TO LBL 2. REMOVED MINOR SURFACE CORROSION, PRIMED AND PAINTED IAW SRM 53060-51, DEFECT SIZE: .25".Oct 31, 2005 · N779AU · Boeing 7374B7 · Fuselage Main, Floor BeamSDR USAA051280Floorbeam · corrodedFOUND FLOORBEAM CORRODED, STA 986.7. REMOVED MINOR SURFACE CORROSION, ALODINED, PRIMED AND PAINTED IAW SRM 53-60-51, DEFECT SIZE: 1" BY 3".Oct 31, 2005 · N779AU · Boeing 7374B7 · Fuselage Main, Floor BeamSDR SB05139Sensor · faultyDURING CRUISE, EN ROUTE FROM ROC TO CLT AT FL340, THE NR 1 ENGINE EXPERIENCED MULTIPLE COMPRESSOR STALLS WHICH LASTED APPROXIMATELY 30 SECONDS EACH. PER QUICK REFERENCE HANDBOOK, CREW REDUCED THRUST AND OPERATED AT THAT POWER THE REMAINDER OF FLIGHT. EGT REMOct 29, 2005 · N440US · Boeing 7374B7 · Fuel Controlling SystemSDR SB05137Charger · inoperativeMCO - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHTS INOPERATIVE AT SEAT ROWS 23 AND 24ABC AND AT THE AFT SERVICE DOOR EXTERIOR. MAINTENANCE REMOVED AND REPLACED THE AFT RIGHT-HAND EMERGENCY LIGHT BATTERY CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD.Oct 26, 2005 · N777AU · Boeing 7374B7 · Emergency LightingSDR USAA051243Frame · damagedFOUND DAMAGE ON FUSELAGE FRAME STA 787, BETWEEN S-8R AND S-9R. CUT OUT DAMAGE, FABRICATED FRAME DOUBLER, INSTALLED DOUBLER IAW SRM 53-10-14, DEFECT SIZE: .5 INCH CRACK IN THE FUSELAGE FRAME.Oct 25, 2005 · N779AU · Boeing 7374B7 · Fuselage Main, FrameSDR SB05134Battery Pack · dischargedCLT - DURING OPERATIONAL TEST OF EMERGENCY LIGHT SYSTEM, MAINTENANCE REPORTED THE AFT ENTRY DOOR EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT ENTRY DOOR EMERGENCY EXIT LIGHT BATTERY PACK PER MM 33-51-51. OPERATIONAL CHECK GOOD.Oct 16, 2005 · N426US · Boeing 7374B7 · Emergency LightingSDR USAA051209Frame · crackedSTA 380 BETWEEN S19L TO S22L CRACKED. REPAIRED IAW EA 96971, DEFECT SIZE: .25 INCH.Oct 14, 2005 · N443US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA051197Intercostal · crackedSTRINGER 16L AND STA 344 CRACKED. FABRICATED NEW INTERCOSTAL/WEB AND ANGLES, INSTALLED REF DWG 65-17685-47 AND SRM 53-10-04. DEFECT SIZE 1 INCH.Oct 12, 2005 · N443US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA051198Wedge · delaminatedRIGHT WING O/B AFT FLAP BEHIND NR 8 FLAP TRACK DELAMINATED. INJECTED WEDGE SPLIT WITH TWO PART ADHESIVE IN DISBOND. NO FURTHER ACTION REQUIRED IAW SRM 57-53-01, DEFECT SIZE 3 X 5 INCHES.Oct 12, 2005 · N443US · Boeing 7374B7 · Trailing Edge FlapsSDR USAA051196Stop Fitting · crackedRIGHT FWD SERVICE DOOR, AFT FRAME AT NR 4 STOP FITTING CUTOUT CRACKED. FABRICATED AND INSTALLED REPAIR DOUBLER IAW TYPICAL REPAIR 52-10-11, DEFECT SIZE: 0.625 INCH CRACK.Oct 11, 2005 · N782AU · Boeing 7374B7 · Service DoorsSDR SB05129Engine · failedPIT - FLT 391 - ON CLIMBOUT FROM PIT, AT FL140, CREW REPORTED A LOUD BANG FROM THE NR 1 ENGINE. SIMULTANEOUSLY, SMOKE FILLED THE COCKPIT, THE NR 1 ENGINE OVERTEMP LIGHT ILLUMINATED AND THE AIRCRAFT YAWED. ENGINE CAME TO AN ABRUPT STOP. CREW SECURED THE ENGIOct 11, 2005 · N778AU · Boeing 7374B7 · Engine (Turbine/Turboprop)SDR SB05125Fuse · blownCLT - MAINTENANCE REPORTED THE EMERGENCY LIGHT AT SEAT ROW 2C OVERHEAD, AT STA 346, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FUSE IN POWER SUPPLY. OPERATIONAL CHECK GOOD.Oct 7, 2005 · N780AU · Boeing 7374B7 · Emergency LightingSDR USAA051187Wedge · wornFOUND LEFT HAND INBOARD MID FLAP INBOARD END WORN. REMOVED DAMAGED FLAP WEDGE AND REINSTALLED NEW WEDGE IAW BOEING DWG 65-46486U155, FLAP WEDGE WORN DUE TO CONTACT WITH THE CONTROL ROD. DAMAGE MEASURES .5" BY 2.75".Oct 6, 2005 · N443US · Boeing 7374B7 · Trailing Edge FlapsSDR USAA051188Skin · delaminatedFOUND NR 2 SLAT T/E WEDGE O/B END DELAMINATED. REMOVED DAMAGE INSTALLED REPAIR PIECES IAW SRM 51-70-10, DEFECT SIZE: 3" X 6" DELAMINATION.Oct 6, 2005 · N443US · Boeing 7374B7 · Leading Edge DevicesSDR USAA051189Skin · delaminatedNR 2 SLAT T/E WEDGE INBOARD END DELAMINATED. REMOVED DAMAGE, INSTALLED REPAIR PIECES IAW SRM 51-70-10, DEFECT SIZE: 3" BY 5" DELAMINATION.Oct 6, 2005 · N443US · Boeing 7374B7 · Leading Edge DevicesSDR USAA051190Keelbeam · crackedFOUND CRACKED RT KEEL BEAM AT AFT SIDE OF STA 500G. FAB`D ANGLE AND INSTALLED. REMOVED AND REPLACED DAMAGED CLIP IAW SRM 51-10-02 AND BOEING DWG 69-73527, DEFECT SIZE: 1" CRACK.Oct 6, 2005 · N443US · Boeing 7374B7 · Fuselage Main, KeelSDR USAA051191Keelbeam · crackedFOUND LEFT KEEL BEAM AFT SIDE OF STA 500G. FABRICATED AND INSTALLED NEW ATTACH ANGLE. REMOVED AND REPLACED CLIP IAW SRM 51-10-02 AND BOEING DWG 69-73527, DEFECT SIZE: 1" CRACK.Oct 6, 2005 · N443US · Boeing 7374B7 · Fuselage Main, KeelSDR USAA051192Stringer Clip · crackedFOUND STRINGER CRACKED, STA 907 AND STR 4R. REMOVED DAMAGED CLIP, REPLACED WITH FABRICATED PART IAW SRM 53-00-03, DEFECT SIZE: 1 INCH CRACK.Oct 6, 2005 · N443US · Boeing 7374B7 · Fuselage Main, Attach FittingsSDR USAA051193Frame · damagedLEFT HAND SIDE AT STA 380, STR 5 DEFECT. FABRICATED FRAME REPAIR DOUBLER & INSTALLED IAW REPAIR DOCUMENT TYP. REPAIR 53-10-14 DEFECT SIZE: 1 X 1 INCH RUB AREA AT STA 380 STR 5 LT SIDE.Oct 6, 2005 · N443US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA051194Door Frame · crackedFOUND FWD SERVICE DOOR FWD CUTOUT FRAME CRACKED. REMOVED OLD DOOR WEB FRAME UPPER FRAME WEB AND NEW ANGLE AND SHIMS IAW SRM 51-10-02, DEFECT SIZE: 1/2" CRACK.Oct 6, 2005 · N443US · Boeing 7374B7 · Fuselage Main, StructureSDR USAA051195Stringer Clip · damagedFOUND ATTACH CLIP BLENDED, STATION 303.9 AT STRINGER 4L. ATTACH CLIP INSTALLED PER SRM 51-40-02, DEFECT SIZE: 1" DIA.Oct 6, 2005 · N443US · Boeing 7374B7 · Fuselage Main, Attach FittingsSDR USAA051184Frame · corrodedFOUND FRAME BOX CORRODED AT STA 847 AND STR 25. REMOVED, FABRICATED AND INSTALLED NEW BOX PANEL IAW SRM 53-60-15, DEFECT SIZE: 3" BY 5".Oct 5, 2005 · N443US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA051185Angle · corrodedFOUND ZEE ANGLE CORRODED BETWEEN STA 767 AND 787 RT SIDE. REMOVED AND REPLACED ZEE ANGLE IAW SRM 53-60-53, DEFECT SIZE: 3" BY 1".Oct 5, 2005 · N443US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA051186Stringer Clip · crackedFOUND STRINGER CLIP CRACKED, STA 907 AND STR 4R. REMOVED DAMAGED CLIP, REPLACED WITH FABRICATED PART IAW SRM 53-00-03, DEFECT SIZE: 1".Oct 5, 2005 · N443US · Boeing 7374B7 · Fuselage Main, Attach FittingsSDR USAA200510001Skin · crackedFOUND 2.25" CRACK FOUND AT BS 727F S-25L. INSTALLED DOUBLER PER SRM 53-00-01 FIG 201.Oct 4, 2005 · N441US · Boeing 7374B7 · Fuselage Main, Plate/SkinSDR USAA051179Wedge · delaminatedFOUND NR 2 SLAT T/E WEDGE INBD END DELAMINATED. REMOVED DAMAGE, INSTALLED REPAIR PIECES IAW SRM 51-70-10, DEFECT SIZE: 3" BY 5" DELAMINATION.Oct 4, 2005 · N433US · Boeing 7374B7 · Leading Edge DevicesSDR USAA051178Wedge · delaminatedFOUND NR 2 SLAT T/E WEDGE O/B END DELAMINATED. REMOVED DAMAGE, INSTALLED REPAIR PIECES IAW SRM 51-70-10, DEFECT SIZE: 3" X 6" DELAMINATION.Oct 4, 2005 · N433US · Boeing 7374B7 · Leading Edge DevicesSDR USAA051177Keelbeam · crackedFOUND LEFT KEEL BEAM AFT SIDE OF STA 500G, CRACKED. FABRICATED AND INSTALLED NEW ATTACH ANGLE IAW SRM 51-10-02 AND BOEING DWG 69-73527, DEFECT SIZE: 1" CRACK.Oct 4, 2005 · N443US · Boeing 7374B7 · Fuselage Main, KeelSDR USAA051175Keelbeam · crackedFOUND RT KEELBEAM AT AFT SIDE OF STA 500G, CRACKED. FABRICATED ANGLE AND INSTALLED IAW SRM 51-10-02 AND BOEING DWG 69-73527, DEFECT SIZE: 1" CRACK.Oct 4, 2005 · N443US · Boeing 7374B7 · Fuselage Main, KeelSDR USAA051167Web · corrodedFOUND FUSELAGE STA 793-STA 847 RBL 20, CORRODED. REMOVED AND REPLACED WITH NEW PART IAW SRM 51-10-02, DEFECT SIZE: 1.0".Oct 3, 2005 · N782AU · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA051174Wedge · damagedFOUND NUMBER 5 SLAT WEDGE TOP SURFACE 10 INCHES FROM OUTBOARD END DAMAGED. REMOVED DAMAGE, FABRICATED AND INSTALLED CORE, FABRICATED AND INSTALLED DOUBLER IAW 57-42-02, DEFECT SIZE: 6".Oct 3, 2005 · N782AU · Boeing 7374B7 · Leading Edge DevicesSDR USAA051173Clip · crackedFOUND CLIP CRACKED, STA 277 AND STR 15R. MAJOR REPAIR IAW SRM 51-10-02, DEFECT SIZE: .75".Oct 3, 2005 · N443US · Boeing 7374B7 · Fuselage Main, Attach FittingsSDR USAA051172Angle · corrodedFOUND FUSELAGE STA 290-344, CORRODED. DEFECTIVE PART REPLACED WITH IDENTICAL PART, REPLACED Z ANGLE IAW SRM 51-40-05, DEFECT SIZE: 54 BY 2".Oct 3, 2005 · N443US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA051171Stringer Clip · crackedFOUND STRINGER 11R AND STA 344, CRACKED. REMOVED AND REPLACED CLIP IAW SRM 51-40-02, DEFECT SIZE: .4".Oct 3, 2005 · N443US · Boeing 7374B7 · Fuselage Main, Attach FittingsSDR USAA051168Floorbeam · corrodedFOUND FLOORBEAM UPPER T-CAP AT CLIPNUT HOLE AT BL 0 AND STA 294 CORRODED. INSTALLED REPAIR T CAP IAW SRM 53-10-51 FIG 201, SHEETS 1-4, DEFECT SIZE: 1".Oct 3, 2005 · N443US · Boeing 7374B7 · Fuselage Main, Floor BeamSDR USAA051166Angle · corrodedFOUND AFT CARGO COMPARTMENT RT TRANSITION ANGLE AT BS 727C TO 767 CORRODED. FABRICATED AND INSTALLED A NEW TRANSITION ANGLE IAW SRM 53-60-53, DEFECT SIZE: 1" BY 28".Oct 3, 2005 · N782AU · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA051165Angle · corrodedFOUND AFT CARGO COMPARTMENT RT TRANSITION ANGLE AT BS 747 TO 767 CORRODED. FABRICATED AND INSTALLED A NEW TRANSITION ANGLE IAW SRM 53-60-53, DEFECT SIZE: 1 BY 12".Oct 3, 2005 · N782AU · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA051164Web · crackedFOUND NLG DOWNLOCK VIEWER FRAME, LT FWD EDGE CRACKED. REMOVED DAMAGED PART, INSTALL NEW PART IAW SRM 51-10-02, DEFECT SIZE: 1.00".Oct 3, 2005 · N782AU · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA051163Flange · crackedFOUND FUSELAGE STATION 559, STRINGER 13L CRACKED. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR ANGLE IAW EA 96912, DEFECT SIZE: .7".Oct 3, 2005 · N782AU · Boeing 7374B7 · Fuselage Main, FrameSDR USAA051162Stringer Splice · crackedFOUND BS 360, STRINGER SPLICE 15L, CRACKED. DEFECTIVE PART REPLACED WITH IDENTICAL PART, REMOVED AND REPLACED STRINGER SPLICE IAW SRM 51-40-02, DEFECT SIZE: .250".Oct 3, 2005 · N443US · Boeing 7374B7 · Fuselage Main, Longeron/StringerSDR USAA051169Angle · corrodedFOUND SILL Z ANGLE AT STA 294 RIGHT SIDE CORRODED. REPLACED Z ANGLE IAW SRM 51-40-05, DEFECT SIZE: 2" BY 8".Oct 3, 2005 · N443US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR SB05124Power Supply · faultyCLT - FLT892 - EN ROUTE FROM BNA TO CLT, THE FLIGHT ATTENDANT REPORTED THE FORWARD CABIN EMERGENCY LIGHTS BEGAN FLICKERING OFF AND ON. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY LIGHT POWER SUPPLY AND BATTERY PACK. OPERATIONAL CHECK GOOD.Oct 1, 2005 · N780AU · Boeing 7374B7 · Emergency LightingSDR USAA051154Floorbeam · corrodedFOUND FLOORBEAM CORRODED, STA 967 RBL 31. REMOVED DAMAGE AND INSTALLED NEW SPLICE DOUBLER AND CAP ON FLOORBEAM IAW TYPICAL REPAIR 53-10-05B, DEFECT SIZE: 1" BY 6".Sep 30, 2005 · N443US · Boeing 7374B7 · Fuselage Main, Floor BeamSDR USAA051161Frame · crackedFOUND FRAME CRACKED AT STATION 887 BETWEEN STRINGERS 8R AND 9R. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED DOUBLER IAW SRM 53-10-20B, DEFECT SIZE: .6".Sep 30, 2005 · N782AU · Boeing 7374B7 · Fuselage Main, FrameSDR USAA051160Strap · corrodedFOUND STRAP CORRODED, STA 767-STA 858, RBL 20. REMOVED DAMAGED PART, REINSTALL NEW PART W/FILLER IAW SRM 51-10-02, DEFECT SIZE: 1.0".Sep 30, 2005 · N782AU · Boeing 7374B7 · Fuselage Miscellaneous Structure
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