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 USAA010794Angle · corrodedCLT - FOUND Z-ANGLE CORRODED 2 INCH BY 53 INCH AREA, BS 947 TO 1000, AFT SERVICE DOOR. REMOVED AND REPLACED Z-ANGLE PER SRM 51-10-02. (M)Jul 10, 2001 · N440US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA010793Angle · corrodedCLT - FOUND Z-ANGLE CORRODED 2 INCH BY 40 INCH AREA, BS 947 TO 987, LBL 52 AT AFT ENTRY DOOR. REMOVED AND REPLACED Z-ANGLE PER SRM 51-10-02. (M)Jul 10, 2001 · N440US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA010792Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 2 INCH BY 18 INCH AREA, BS 947 LBL 12 TO RBL 6. DAMAGE REMOVED, REPLACED T-CAP PER TYPICAL REPAIR 53-60-02. (M)Jul 10, 2001 · N440US · Boeing 7374B7 · Fuselage Main, Floor BeamSDR USAA010789Frame · crackedCLT - FOUND FRAME CRACKED .125 INCH, BS 827, BETWEEN STRINGERS 8 AND 9R. REPAIR DOUBLER INSTALLED PER TYPICAL REPAIR 53-10-14. (M)Jul 10, 2001 · N440US · Boeing 7374B7 · Fuselage Main, StructureSDR USAA010790Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, BS 867, BETWEEN STRINGERS 8 AND 9L. REPAIR DOUBLER INSTALLED PER TYPICAL REPAIR 53-10-14. (M)Jul 10, 2001 · N440US · Boeing 7374B7 · Fuselage Structure (General)SDR USAA010791Frame · crackedCLT - FOUND FRAME CRACKED .125 INCH, BS 867, BETWEEN STRINGERS 8 AND 9R. REPAIR DOUBLER INSTALLED PER TYPICAL REPAIR 53-10-14. (M)Jul 10, 2001 · N440US · Boeing 7374B7 · Fuselage Structure (General)SDR USAA010783Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, BS 380, BETWEEN STRINGERS 8 AND 9L. REPAIR DOUBLER INSTALLED PER TYPICAL REPAIR 53-10-14. (M)Jul 10, 2001 · N440US · Boeing 7374B7 · Fuselage Main, StructureSDR USAA010784Frame · crackedCLT - FOUND FRAME CRACKED .125 INCH, BS 400, BETWEEN STRINGER 8 AND 9L. INSTALLED REPAIR DOUBLER PER TYPICAL REPAIR 53-10-14. (M)Jul 10, 2001 · N440US · Boeing 7374B7 · Fuselage Structure (General)SDR USAA010785Frame · crackedCLT - FOUND FRAME CRACKED .125 INCH, BS 500D, BETWEEN STRINGER 8 AND 9R. REPAIR DOUBLER INSTALLED PER TYPICAL REPAIR 53-10-14. (M)Jul 10, 2001 · N440US · Boeing 7374B7 · Fuselage Main, StructureSDR USAA010786Frame · crackedCLT - FOUND FRAME CRACKED .125 INCH, BS 727B, BETWEEN STRINGERS 8 AND 9R. REPAIR DOUBLER INSTALLED PER TYPICAL REPAIR 53-10-14. (M)Jul 10, 2001 · N440US · Boeing 7374B7 · Fuselage Main, StructureSDR USAA010787Frame · crackedCLT - FOUND FRAME CRACKED .125 INCH, BS 727D, BETWEEN STRINGERS 8 AND 9R. REPAIR DOUBLER INSTALLED PER TYPICAL REPAIR 53-10-14. (M)Jul 10, 2001 · N440US · Boeing 7374B7 · Fuselage Structure (General)SDR USAA010788Frame · crackedCLT - FOUND FRAME CRACKED .125 INCH, BS 787 BETWEEN STRINGERS 8 AND 9R. REPAIR DOUBLER INSTALLED PER TYPICAL REPAIR 53-10-14. (M)Jul 10, 2001 · N440US · Boeing 7374B7 · Fuselage Structure (General)SDR USAASB01196Sign · inoperativePHL - FOUND REAR EMERGENCY EXIT SIGN FOR THE R2 DOOR INOPERATIVE. MAINTENANCE REPLACED THE ASSEMBLY. (M)Jul 7, 2001 · N784AU · Boeing 7374B7 · Emergency LightingSDR USAASB01193Seal · leakingMSY - FLT 429 - EN ROUTE FROM CLT-MSY, 140 NAUTICAL MILES AWAY FROM MSY AT FL350, THE CREW REPORTED A CABIN PRESSURIZATION LOSS WITH THE CABIN ALTITUDE WARNING HORN SOUNDING. CAPTAIN DESCENDED FLIGHT TO FL130 WHERE THE CABIN STABILIZED AT CABIN ALTITUDE OF 10Jul 5, 2001 · N781AU · Boeing 7374B7 · DoorsSDR USAASB01191Charger · failedALB - DURING OPERATIONAL TEST OF EMERGENCY LIGHTS, MAINTENANCE FOUND THE FORWARD SERVICE DOOR EMERGENCY LIGHTS WENT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK (P/N 2013-1A) WITH NO HELP. REMOVED AND REPLACED THE CHARGER ASSEMBLY. SYSTEM Jul 5, 2001 · N428US · Boeing 7374B7 · Emergency LightingSDR USAA010774Pressure Panel · crackedCLT - FOUND PRESSURE WEB HAS 10 CRACKS, SMALLEST IS .150 INCH, LARGEST IS 1.7 INCH, BS 178 WL 188 TO 213, BETWEEN RBL 6.5 AND LBL 10. DAMAGE REMOVED, DOUBLER AND FILLERS INSTALLED PER EO 5300V153 AND SRM 53-10-08, FIG 211. (M)Jul 5, 2001 · N440US · Boeing 7374B7 · Fuselage Main, BulkheadSDR USAA010775Frame · crackedCLT - FOUND SIDE CHORD CRACKED TWO PLACES .9 INCH BY 1.6 INCH, BS 178, WL 207, RBL 28 AND LBL 28. DAMAGE REMOVED, SPLICED IN NEW CHORD SECTION PER EO 5300V157. (M)Jul 5, 2001 · N440US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA010782Skin · damagedCLT - FOUND STAB SKIN WITH PREVIOUSLY INSTALLED DOUBLER, 57 INCHES LONG WIDTH VARIES FROM 4 INCHES TO 5 INCHES, LEFT HORIZONTAL STABILIZER, SS 111.10 TO 166.30 AT REAR SPAR. DAMAGE REMOVED, INSTALLED DOUBLER PER EA'S 85064 AND 69880. (M)Jul 5, 2001 · N440US · Boeing 7374B7 · Horizontal Stabilizer, Plate/SkinSDR USAA010763Skin · crackedCLT - FOUND SKIN CRACKED 1.5 INCH, BS 727D, STRINGER 23R. DAMAGE REMOVED, INSTALLED REPAIR DOUBLER PER TYPICAL REPAIR 53-60-03. (M)Jun 28, 2001 · N429US · Boeing 7374B7 · Fuselage Structure (General)SDR USAASB01186Control Valve · faultyLGA - FLT 508 - EN ROUTE FROM CLT TO LGA - AT FL250, CAPTAIN REPORTED THE CABIN ALTITUDE WARNING HORN BEGAN SOUNDING. CREW DESCENDED AIRCRAFT TO FL100 AND CONTINUED ONTO LGA. MAXIMUM CABIN ALTITUDE WAS 9,5000 FEET. FLIGHT LANDED AT LGA WITHOUT FURTHER INCIDJun 27, 2001 · N432US · Boeing 7374B7 · Cabin Cooling SystemSDR USAASB01183Battery Pack · inoperativeALB - MAINTENANCE FOUND THE EMERGENCY EVACUATION LIGHTS ON SEAT ROWS 13-19, BULLNOSE LIGHT AT ROW 20 LEFT AND SIDEWALL EXIT SIGN AT ROW 12 RIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AT ROW 21 CEILING LOCATION. OPS CHECK GOOD. (M)Jun 25, 2001 · N775AU · Boeing 7374B7 · Emergency LightingSDR USAA010825Floorbeam · corrodedPIT - FOUND FLOORBEAM CORRODED 32 INCH AREA, Z-ANGLE AFT FORWARD ENTRANCE FROM FLOORBEAM. (M)Jun 24, 2001 · N439US · Boeing 7374B7 · Fuselage Main, Floor BeamSDR USAA010818Support · corrodedPIT - FOUND GALLEY SUPPORT CORRODED, 3 INCH BY 15 INCH AREA, STATION 338 RBL 47 TO RBL 62. (M)Jun 24, 2001 · N439US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA010817Strap · corrodedPIT - FOUND FLOOR SUPPORT STRAP CORRODED 16 INCHES BY 3 INCHES UPPER SURFACE, STATION 328-344. CORROSION LEVEL 1, TASK NR C53-107-02. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-40-02. (M)Jun 24, 2001 · N439US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA010816Floorbeam · corrodedPIT - FOUND T-CAP CORRODED 2 INCH BY 62 INCH AREA, BEAM 328 BETWEEN B10 AND RBL 62. SPLICED IN SECTION OF UPPER CHORD, TREATED, PRIMED, SEALED PER SRM 53-10-51. (M)Jun 24, 2001 · N439US · Boeing 7374B7 · Fuselage Main, Floor BeamSDR USAA010815Floorbeam · corrodedPIT - FOUND BEAM T-CAP CORRODED 2 INCH BY 29 INCH AREA, BEAM 312 BETWEEN LBL 10 AND RBL 19. CORROSION LEVEL 1, TASK NR C53-107-02. REPLACED SECTION OF T-CAP, TREATED AND PRIMED PER SRM 53-10-51, 51-40-02. (M)Jun 24, 2001 · N439US · Boeing 7374B7 · Fuselage Main, Floor BeamSDR USAA010813Angle · corrodedPIT - FOUND ANGLE CORRODED 1 INCH BY 30 INCH AREA, BETWEEN SERVICE DOOR FRAME THRESHOLD SUPPORT. REPLACED CORRODED SUPPORT ANGLE PER SRM 53-10-15AS. (M)Jun 24, 2001 · N439US · Boeing 7374B7 · Fuselage Main, StructureSDR USAA010819Angle · corrodedPIT - FOUND Z-ANGLE CORRODED 2 INCH BY 56 INCH AREA, BETWEEN BEAM 282 AND 338. CORROSION LEVEL 1, TASK NR C53-107-02. REPLACED Z-ANGLE, TREATED, PRIMED PER SRM 51-40-02. (M)Jun 24, 2001 · N439US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA010820Angle · corrodedPIT - FOUND SUPPORT ANGLE CORRODED 2 INCH BY 4 INCH AREA, FLOOR SUPPORT LBL 10 BETWEEN 328 AND 344. CORROSION LEVEL 1, TASK NR C53-107-02. REPLACED FLOOR SUPPORT PER SRM 51-40-02. (M)Jun 24, 2001 · N439US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA010821Floor Support · corrodedPIT - FOUND SUPPORT ANGLE CORRODED 2 INCH BY 4 INCH AREA, FLOOR SUPPORT LBL 10 BETWEEN 312 AND 328. CORROSION LEVEL 1, TASK C53-107-02. REPLACED FLOOR SUPPORT PER SRM 51-40-02. (M)Jun 24, 2001 · N439US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA010823Floorbeam · corrodedPIT - FOUND FLOORBEAM CORRODED 2 INCHES, CLIP NUT ON FLOORBEAM 328 LEFT. CORROSION LEVEL 1. SPLICED IN SECTION OF UPPER CHORD, TREATED, PRIMED, SEALED PER SRM 53-10-51, 51-40-02. (M)Jun 24, 2001 · N439US · Boeing 7374B7 · Fuselage Main, Floor BeamSDR USAA010827Floorbeam · corrodedPIT - FOUND 6 INCHES OF CORROSION AT FLOORBEAM 328 LT OUTBOARD OF LBL 45. CORROSION LEVEL 1. SPLICED IN SECTION OF UPPER CHORD, TREATED, PRIMED, SEALED PER SRM 53-10-51, 51-40-02. (M)Jun 24, 2001 · N439US · Boeing 7374B7 · Fuselage Main, Floor BeamSDR USAASB01173Battery Pack · dischargedPHL - MAINTENANCE FOUND THE EMERGENCY LIGHTS IN THE AFT SECTION OF CABIN IN SEAT ROWS 20 TO 23, 20 TO 21 OVERHEAD AND AFT EXIT DOORS SIGNS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT LEFT BATTERY PACK. OPS CHECK GOOD. (M)Jun 15, 2001 · N428US · Boeing 7374B7 · Emergency LightingSDR USAASB01168Light · inoperativeALB - PILOT REPORTED THAT THE EMERGENCY EXIT LIGHT ON SEAT 12C IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT IDENTIFIER LIGHT AT SEAT 12C. OPS CHECK GOOD. (M)Jun 7, 2001 · N437US · Boeing 7374B7 · Emergency LightingSDR USAASB01161Charger · failedBWI - MAINTENANCE FOUND THE LEFT FORWARD INTERIOR OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK (P/N 2013-1A) AND CHARGER ASSEMBLY. OPS CHECK GOOD. (M)Jun 5, 2001 · N784AU · Boeing 7374B7 · Emergency LightingSDR USAASB01158Battery Pack · dischargedBDL - MAINTENANCE FOUND THE EMERGENCY LIGHTS AT SEAT ROWS 1 AND 2 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPS CHECK GOOD. (M)Jun 4, 2001 · N780AU · Boeing 7374B7 · Emergency LightingSDR USAASB01157Power Supply · failedBDL - MAINTENANCE FOUND THE EMERGENCY LIGHTS AT SEAT ROWS 11 TO 12 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY. OPS CHECK GOOD PER MM. (M)Jun 3, 2001 · N427US · Boeing 7374B7 · Emergency LightingSDR USAASB01144Ground Wire · brokenPHL - PILOT REPORTED THAT THE FLIGHT DECK EMERGENCY LIGHT IS INOPERATIVE. MAINTENANCE FOUND A BROKEN GROUND WIRE. REPAIRED GROUND WIRE. FLIGHT DECK EMERGENCY LIGHT OPERATIONALLY CHECKS GOOD. (M)May 23, 2001 · N434US · Boeing 7374B7 · Emergency LightingSDR USAA010822Floorbeam · corrodedPIT - FOUND FLOORBEAM CORRODED 2 INCHES BY 4 INCHES, FLOORBEAM 360 LEFT. CORROSION LEVEL 1. REMOVED AREAS OF LIGHT CORROSION, TREATED, PRIMED PER SRM 53-10-15. (M)May 19, 2001 · N439US · Boeing 7374B7 · Fuselage Main, Floor BeamSDR USAASB01137Battery Pack · dischargedCLT - DURING OVERNIGHT CHECK, MAINTENANCE FOUND NUMEROUS EMERGENCY LIGHTS IN THE AFT GALLEY INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RIGHT BATTERY PACK IN THE AFT GALLEY. OPERATIONAL CHECK GOOD. (M)May 13, 2001 · N780AU · Boeing 7374B7 · Emergency LightingSDR USAASB01135Tire · separatedMCO - FLT 722 - ON CLIMB-OUT FROM MCO,CAPT REPORTED THE FWD MAIN ENTRY DOOR WAS LEAKING AND THE AIRCRAFT WOULD NOT PRESSURIZE NORMALLY. FLIGHT RETURNED TO FIELD AND LANDED 5,000 LBS OVERWEIGHT. NO EMERGENCY WAS DECLARED. MAINTENANCE REPORTED THAT THE RT OUTBOMay 11, 2001 · N445US · Boeing 7374B7 · TireSDR USAA010509Frame · crackedCLT - FOUND SIDE CHORD CRACKED .5 INCH, BS 178, WL 207 LEFT SIDE OF AC. DAMAGED AREA CUTOUT, SPLICED IN NEW CHORD SECTION PER E5300157. (M)May 7, 2001 · N426US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA010508Bulkhead · crackedCLT - FOUND BS 178 PRESSURE BULKHEAD WEB WITH CRACKS .125 INCH, .5 INCH, .8 INCH, 1 INCH AND 1.1 INCH, BS 178, FROM WL 188 TO WL 212.5, RBL 6.6 TO LBL 5. DAMAGE REMOVED, FILLERS AND REPAIR DOUBLER INSTALLED PER SRM 53-10-01, 53-10-08 AND EO 5300V153. (M)May 7, 2001 · N426US · Boeing 7374B7 · Fuselage Main, BulkheadSDR USAASB01117Light · inoperativeTPA - DURING OVERNIGHT CHECK, MAINTENANCE FOUND THE FORWARD LEFT OVERWING LIGHT STATION 607L AND THE LEFT EXIT INDICATOR STATION 612L INOPERATIVE. (M)Apr 28, 2001 · N438US · Boeing 7374B7 · Emergency LightingSDR USAA010472Bulkhead · crackedCLT - FOUND PRESSURE WEB WITH 5 CRACKS, TWO .250 INCH, TWO .150 INCH AND ONE .100 INCH, BS 178, WL 195, 198, 201.5, 206.6; LBL 5 TO RBL 7. DAMAGE CUTOUT, REPAIR DOUBLER INSTALLED PER EO 5300V153 AND EA 69566. (M)Apr 27, 2001 · N429US · Boeing 7374B7 · Fuselage Main, BulkheadSDR USAA010457Angle · crackedCLT - FOUND SIDE CHORD ANGLE WITH TWO CRACKS .625 ON LEFT, .5 ON RIGHT, BS 178, WL 207, LEFT AND RIGHT SIDE CHORD. REMOVED DAMAGED SECTIONS ON LEFT AND RIGHT SIDE, SPLICED IN NEW CHORD SECTIONS PER EO 5300V157. (M)Apr 25, 2001 · N428US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA010456Bulkhead · crackedCLT - FOUND BULKHEAD WEB WITH CRACKS RANGING IN SIZE FROM .250 INCH TO .800 INCH, BS 178, WL 188 TO 212, RBL 7 TO LBL 6.5. INSTALLED REPAIR DOUBLER PER EO 5300V153. (M)Apr 25, 2001 · N428US · Boeing 7374B7 · Fuselage Main, BulkheadSDR USAA010434Angle · crackedCLT - FOUND ANGLE CRACKED 1 INCH, BS 294.5 FUSELAGE CUTOUT FOR FORWARD GALLEY SERVICE DOOR. INSTALLED REPAIR DOUBLER PER SRM 51-70-11. (M)Apr 20, 2001 · N437US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA010433Stiffener · crackedCLT - FOUND STIFFENER CRACKED .5 INCH BS 178,WL 184, LBL 5.7. INSTALLED REPAIR KIT, EO 5300V155. (M)Apr 20, 2001 · N437US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA010432Frame · crackedCLT - FOUND SIDE CHORD CRACKED .5 INCH, BS 178, WL 207 LBL 26. CUTOUT DAMAGE, SPLICED IN REPAIR, EO 5300V157. (M)Apr 20, 2001 · N437US · Boeing 7374B7 · Fuselage Main, Frame
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