Boeing 737-3B7
Service difficulty reports · 4,722
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 = '7373B7' 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.
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 = '7373B7' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR USAA050348Hinge · crackedCLT - UNSCHED - HINGE CASTING, 1 INCH X 1 INCH CRACK, LT AFT SERVICE DOOR HINGE BOX. (K)SDR USAA050346Skin · crackedCLT - Q6 - FUSELAGE SKIN, .5 INCH CRACK, LOWER HINGE CUT-OUT FWD SERVICE DOOR. INSTALLED REPAIR DOUBLER IAW TR 52-10-13. (K)SDR USAA050344Skin · crackedCLT - Q2 - NR 5 SLAT SKIN, 38 INCH CRACK, NR 5 SLAT LE SKIN. INSTALLED REPAIR DOUBLER IAW SRM. (K)SDR USAA050343Skin · crackedCLT - Q2 - NR 5 SLAT SKIN, SEVERAL .250 INCH CRACKS, NR 5 SLAT LOWER SKIN L/E. INSTALLED REPAIR DOUBLER. (K)SDR USAA050342Wedge · wornCLT - Q2 - NR 4 SLAT, 2 INCH X 2 INCH, WEAR. NR 4 SLAT T/E WEDGE LOWER SKIN IB. ACCOMPLISHED COMPOSITE REPAIR IAW EA. (K)SDR SB0534Socket · inoperativeMCO - MAINTENANCE REPORTED THE EMERGENCY LIGHT AT SEAT 12ABC INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT SOCKET AT SEAT 12ABC. OPERATIONAL CHECK GOOD.SDR USAA050340Skin · delaminatedCLT - Q2 - NR6 SPOILER, 2 INCH X 6 INCH, DELAMINATION. NR 6 SPOILER TOP SURFACE IB, 6 INCHES FROM T/E. APPLIED COMPOSITE REPAIR IAW SRM. (K)SDR SB05037Indicator · malfunctionedALB - FLT920 - CREW RECEIVED A SPLIT FLAP INDICATION BETWEEN POSITIONS 2 AND 5, WITH GREEN LIGHT, ON DESCENT INTO ALB. NO ROLL WAS NOTICED. CREW DECLARED AN EMERGENCY AND PROCEEDED TO GO THROUGH CHECKLIST. APPROXIMATELY TEN MINUTES LATER, AS CHECKLIST WAS BSDR SB05036Pressure Switch · faultyBWI - FLT141 - EN ROUTE FROM DCA TO IND, AT FL270, WITH THE APU POWERING THE NR 2 GENERATOR BUS, THE APU LOW OIL PRESSURE LIGHT ILLUMINATED FOLLOWED BY AN APU AUTO SHUT DOWN. THE NR 2 ENGINE CSD WAS ALREADY ON MEL SO THE FLIGHT DIVERTED TO BWI AND LANDED WITHSDR SB05035Socket · inoperativeMAINTENANCE REPORTED THE EMERGENCY LIGHT AT SEAT 12ABC INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT SOCKET AT SEAT 12ABC. OPERATIONAL CHECK GOOD.SDR USAA050306Skin · crackedCLT - FOUND NR 5 SLAT WITH 4 INCH CRACK, LOWER LE SKIN NR 5. INSTALLED REPAIR DOUBLER IAW SRM 57-43-01. (M)SDR SB05033Wire · brokenPHL - MAINTENANCE REPORTED THE EMERGENCY EXIT LIGHT AT SEAT 19ABC INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRES. OPERATIONAL CHECK GOOD.SDR USAA050305Skin · crackedCLT - FOUND SKIN CRACKED 3.375 INCH STATION 883 STRINGER 25R. INSTALLED DOUBLER IAW SRM 53-00-01. (M)SDR SB05032Circuit Breaker · burnedAFTER LANDING CREW STOPPED A/C ON TAXIWAY & REPORTED TO INBOUND RAMP, FIRE & SMOKE IN COCKPIT. CREW STATED, "ON TAXI-IN, FIRE ERUPTED FROM F/O LWR C/B PNL. USED PORTABLE HALON FIRE EXTINGUISHER & EVACUATED A/C. ENG 1 & 2 & APU FIRE EXTINGUISHER BOTTLES DISCHSDR SB05030Seal · bentBWI - FLT428 - ENROUTE FROM CLT TO BWI, CREW REPORTED A LOSS OF CABIN PRESSURE AT FL270. CABIN CREW NOTED A NOISE AROUND THE FORWARD ENTRY DOOR. OXYGEN MASKS DEPLOYED. FLIGHT DESCENDED AND CONTINUED ONTO BWI WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLASDR SB05029Socket · dirtyBDL - MAINTENANCE REPORTED THE EXTERIOR EMERGENCY LIGHT AT THE L1 DOOR INOPERATIVE. MAINTENANCE CLEANED SOCKET AND RELAMPED. OPERATIONAL CHECK NORMAL.SDR SB05028Power Unit · dischargedDURING ANNUAL OPERATIONAL CHECK OF THE AFT LEFT ENTRY DOOR ESCAPE SLIDE, THE SLIDE DEPLOYED NORMALLY BUT THE SLIDE MOUNTED EMERGENCY LIGHTS FAILED TO ILLUMINATE. SLIDE OPERATIONAL CHECK FAILED. MAINTENANCE FOUND THE POWER UNIT ASSEMBLY FOR THE ESCAPE SLIDE MSDR USAA050309Skin · chafedPIT - FOUND SKIN CHAFED .013 INCH BY .011 INCH DEEP BY 20 INCHES LONG, BS 867-887 LT/RT SIDE OF SKIN UNDER DORSAL FIN. CUT AREA OUT, INSTALLED FILLER, DOUBLER AND TRIPLER AND CHAFED STRAPS PER SRM 53-60-01 FIG 201 PAGE 241. (M)SDR USAA050295Stringer · crackedPIT - FOUND STRINGER CRACKED 3 INCHES, BS 1138 S5A LEFT. TRIM OUT DAMAGE AND SPLICE IN NEW SECTION OF STRINGER PER TYPICAL REPAIR 53-80-04. (M)SDR SB05027Battery Pack · dischargedPHL - MAINTENANCE REPORTED THE EMERGENCY EXIT LIGHTS ABOVE THE AFT LEFT SERVICE DOOR AND THE AFT RIGHT SERVICE DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACKS. OPERATIONAL CHECK GOOD.SDR USAA050310Support Angle · crackedPIT - FOUND SUPPORT ANGLE CRACKED 1 INCH, TRAILING EDGE OF SUPPORT PANEL, RT WING JUST ABOVE INBOARD EDGE OF NR 5 FLAP. FABRICATED AND INSTALLED NEW SUPPORT ANGLE PER BOEING DWG 69-47542 AND SRM 57-51-02. (M)SDR USAA050287Skin · crackedCLT - FOUND EXT FUSELAGE SKIN CRACKED .5 INCH, FORWARD SERVICE DOOR LOWER HINGE CUTOUT. INSTALLED DOUBLER IAW TR 52-10-13. (M)SDR USAA050286Floorbeam · corrodedCLT - FOUND FLOORBEAM T-CAP CORRODED .5 INCH BY .5 INCH, STATION LBL 34 TO RBL 60. INSTALLED T-CAP IAW SRM 53-10-51. (M)SDR USAA050285Skin · crackedCLT - FOUND SLAT SKIN CRACKED .025 INCH, NR 6 SLAT LOWER L/E. INSTALLED DOUBLER. (M)SDR USAA050314Floor Support · corrodedPIT - FOUND FLOOR SUPPORT CORRODED 1 INCH BY 1 INCH AREA, FLOOR SUPPORT BEAM S-26R BS 787-867. CORROSION LEVEL 1, TASK C53-208-01. REMOVED AND REPLACED FLOOR SUPPORT BEAM WITH FABRICATED BEAM PER SRM 51-40-02. (M)SDR USAA050311Channel · crackedPIT - FOUND U-CHANNEL WITH 1 INCH CRACK, BS 747-767. FABRICATED AND INSTALLED NEW U-CHANNEL SUPPORT. (M)SDR USAA050284Skin · crackedCLT - FOUND SKIN CRACKED .5 INCH, BETWEEN STATIONS 360-390 E/E BAY. INSTALLED DOUBLER IAW EA 62978. (M)SDR USAA050283Floorbeam · damagedCLT - FOUND FLOORBEAM WITH HOLE .250 INCH, STATION 328 RBL 25. ACCOMPLISHED T-CAP REPAIR IAW SRM 53-10-51. (M)SDR USAA050282Floor Support · corrodedCLT - FOUND FLOOR SUPPORT CORRODED 1 INCH BY 1 INCH, AFT STATION 727D FLOOR SUPPORT ANGLE RBL 2.5. INSTALLED REPAIR DOUBLER IAW TR 53-10-06. (M)SDR USAA050257Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, STATION 827 STRINGER 9R. INSTALLED FILLER/DOUBLER IAW TR 53-10-20A. (M)SDR USAA050256Frame · crackedCLT - FOUND FRAME CRACKED .3750 INCH, STATION 887 STRINGER 9R. INSTALLED FILLER/DOUBLER IAW TR 53-10-20A. (M)SDR USAA050255Channel · corrodedCLT - FOUND U-CHANNEL WITH CORROSION ALONG ENTIRE LENGTH, FORWARD ENTRANCE DOOR SILL PLATE U-CHANNEL. REPLACED CHANNEL IAW SRM 51-10-02. (M)SDR USAA050254Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, STATION 827 STRINGER 9R. INSTALLED FILLER/DOUBLER REPAIR IAW TR 53-10-20A. (M)SDR USAA050239Frame · crackedCLT - FOUND FRAME CRACKED 1 INCH, STATION 616 WL 200 RIGHT SIDE. FABRICATED REPAIR ANGLE AND INSTALLED PER TR 53-62-01. (M)SDR USAA050238Beam · corrodedCLT - FOUND BEAM CORRODED 3 INCHES, STATION 312 RBL 20. ACCOMPLISHED REPAIR PER SRM 53-10-51. (M)SDR USAA050296Skin · crackedPIT - FOUND SKIN CRACKED 1.5 INCH, FORWARD SERVICE DOOR CUTOUT AFT LOWER CORNER. INSTALLED DOUBLER PER SRM 53-10-01. (M)SDR USAA050297Support Angle · corrodedPIT - FOUND SUPPORT ANGLE CORRODED APPROX 24 INCHES, FORWARD SERVICE DOOR FLOOR THRESHOLD SUPPORT ANGLE. REPLACED SUPPORT PER SRM 53-10-15. (M)SDR USAA050316Skin · delaminatedPIT - FOUND EXT COMPOSITE SURFACE DELAMINATED 4 INCHES LONG BY .0625 INCHE WIDE SINGLE LAYER DAMAGE, RUDDER LEFT SIDE 38 INCHES FROM BOTTOM, 13.5 INCHES FROM T/E. REMOVED DAMAGED MATERIAL, INSTALLED REPAIR PLYS, SEALED AND REFINISHED PER SRM 51-70-17 AND EA 7SDR USAA050315Skin Panel · delaminatedPIT - FOUND COMPOSITE SKIN PANEL DELAMINATED .5 INCH BY .0625 INCH SINGLE LAYER DAMAGE, LT SIDE RUDDER 57 INCHES FROM BOTTOM, 34 INCHES FROM T/E. INSTALLED REPAIR PLYS PER SRM 51-70-17 AND EA 79999. (M)SDR USAA050317Skin · delaminatedFOUND EXT COMPOSITE SURF DELAMINATED .5 INCH LONG BY .0625 INCH WIDE SINGLE LAYER DAMAGE, RUDDER LEFT SIDE 66 INCHES FROM BOTTOM, 14 INCHES FROM T/E. REMOVED DAMAGED MATERIAL, INSTALLED REPAIR PLYS, SEALED AND REFINISHED PER SRM 51-70-17, EA 79999. (M)SDR USAA050320Skin · delaminatedPIT - FOUND EXT COMPOSITE SURF WITH 1 INCH SINGLE LAYER DAMAGE DELAMINATION, RUDDER RT SIDE 41 INCHES FROM BOTTOM, 8 INCH FROM T/E. INSTALLED REPAIR PLYS, SEALED AND REFINISHED PER BOEING SRM 51-70-17, EA 79999. (M)SDR USAA050321Skin · delaminatedPIT - FOUND EXIT COMPOSITE SURF, 2 INCHES LONG BY .125 INCH WIDE SINGLE LAYER DAMAGE, RUDDER RT SIDE 57 INCH FROM BOTTOM, 10 INCH FROM T/E. INSTALLED REPAIR PLYS, SEALED, REFINISHED PER SRM 51-70-17, EA 79999. (M)SDR USAA050322Skin · delaminatedPIT - FOUND EXT COMPOSITE SURF 4 INCH LONG BY .125 INCH SINGLE LAYER DAMAGE, RUDDER RT SIDE 64 INCHES FROM BOTTOM 34 INCHES FROM T/E. INSTALLED REPAIR PLYS, SEALED AND REFINISHED PER BOEING SRM 51-70-17, EA 79999. (M)SDR USAA050323Skin · delaminatedPIT - FOUND EXT COMPOSITE SURF WITH DELAMINATION 5 INCHES LONG BY .125 INCH WIDE SINGLE LAYER DAMAGE, RUDDER RT IDE 114 INCH FROM BOTTOM 7 INCH FROM T/E. INSTALLED REPAIR PLYS, SEALED AND REFINISHED PER SRM 51-70-17, EA 79999. (M)SDR USAA050313Attach Fitting · corrodedPIT - FOUND ATTACH RING CORRODED 1 INCH BY 20 INCH AREA, ACCESS PANEL NR 7405. DEFECTIVE PART REPLACED WITH IDENT PART PER AMM 57-00-00. (M)SDR USAA050318Skin Panel · delaminatedPIT - FOUND COMPOSITE SKIN PANEL DELAMINATED .1875 INCH DIAMETER SINGER LAYER DAMAGE, RUDDER LT SIDE 70 INCHES FROM BOTTOM, 9 INCHES FROM T/E. INSTALLED REPAIR PLYS PER SRM 51-70-17, EA 79999. (M)SDR USAA050319Skin Panel · delaminatedPIT - FOUND COMPOSITE SKIN PANEL WITH DELAMINATION 3 INCH BY .0625 INCH SINGLE LAYER DAMAGE, 165 INCHES FROM BOTTOM, 13 INCHES FROM T/E RUDDER LT SIDE. INSTALLED REPAIR PLYS PER SRM 51-70-17, EA 79999. (M)SDR USAA050298Skin · chafedPIT - FOUND RIGHT OUTBOARD MID FLAP CHAFED .25 INCH BY 2 INCH BY .016 INCH, OUTBOARD 4 EDGE SURFACE. DOUBLER INSTALLED PER SRM 57-53-01 FIG 208. (M)SDR USAA050226Skin · crackedCLT - FOUND SKIN CRACKED TWO PLACES .750 INCH EACH, STATION 663 LBL 30. INSTALLED DOUBLER PER TR 53-60-04. (M)SDR USAA050235Web · corrodedPIT - FOUND WEB CORRODED 8 INCH BY 30 INCH AREA, BS 794-828, CORROSION LEVEL 1, TASK NR C53-202-01. DEFECTIVE PART REPLACED WITH IDENT PART NR PER SRM 51-40-00. (M)
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