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 USAA061241Stringer Clip · crackedBS 500A STR 16R CRACKED. REMOVED AND REPLACED TIE CLIP IAW SRM 51-10-02, DEFECT SIZE: 1 INCH.SDR PIDR2006031Skin · corrodedCORROSION IN FUSELAGE SKIN AT BS 360 AND STR 25 LT. CORROSION ON STR 25 LT BEYOND ALLOWABLE LIMITS. SPLICED A NEW PIECE OF STRINGER SECTION AND REMOVED LIGHT SURFACE CORROSION ON FUSELAGE SKIN PER EA 53-270.SDR PIDR2006028Keelbeam · corrodedCORROSION ON RIGHT KEEL BEAM (STR28RT) FROM BS 500D TO BS 540. REPAIRED AREA BY SPLICING IN A REPLACEMENT SECTION OF KEEL BEAM PER EA 53-268. PLEASE REMOVE PIDR AS THE OPERATOR DESIGNATOR IN ORDER TO IDENTIFY THE OPERATOR AS A GENERAL AVIATION OPERATOR.SDR PIDR2006027Frame · crackedFOUND CRACK IN BS 867 FRAME AT STR 13RT. REPAIRED FRAME PER SRM 53-00-07 FIG 201. PLEASE REMOVE PIDR AS THE OPERATOR DESIGNATOR IN ORDER TO IDENTIFY THE OPERATOR AS A GENERAL AVIATION OPERATOR.SDR PIDR2006029Lap Joint · crackedCRACK IN LOWER FASTENER ROW OF STR 10LT SKIN LAP AT BS 500D+10 AND VARIOUS LOCATIONS OF SCRIBE LINES AT STR 10LT LAP AREA WERE REPAIRED BY REPLACING THE SKIN LAP PER SB 737-53A1177. PLEASE REMOVE PIDR AS THE OPERATOR DESIGNATOR IN ORDER TO IDENTIFY THE OPERATSDR USAA061218Skin · crackedAT 2 INCHES FWD OF BS 727E AT S24R CRACK. INSTALLED REPAIR DOUBLER IAW EA 98168, DEFECT SIZE: 2 INCHES.SDR PIDR2006026Frame · crackedCRACK IN BS 767 FRAME AT STR 13 RT. REPAIRED PER SRM 53-00-07 FIG 201. NOTE: PLEASE REMOVE PIDR AS THE OPERATOR DESIGNATOR IN ORDER TO IDENTIFY THE OPERATOR AS A GENERAL AVIATION OPERATOR.SDR USAA061216Door Frame · crackedFWD CARGO DOOR FWD FRAME AT LOWER DOOR STOP BS 440 S23R CRACK. INSTALLED DOUBLER AND FILLERS IAW EA 98153, DEFECT SIZE: .25 INCH.SDR PIDR2006030Lap Joint · damagedSEVERAL AREAS OF SCRIBE LINE DAMAGE AT STR 14LT FROM BS 360 TO BS 540. REPAIRED AREA BY REPLACING THE SKIN LAP PER SB 737-53A1177. PLEASE REMOVE PIDR AS THE OPERATOR DESIGNATOR IN ORDER TO IDENTIFY THE OPERATOR AS A GENERAL AVIATION OPERATOR.SDR PIDR2006025Skin · damagedSTR 14 LT SKIN LAP HAS SCRIBE LINE DAMAGE IN SEVERAL PLACES FROM BS 360 TO BS 540. REPAIRED DAMAGED AREA IAW SB 737-53A1177.SDR PIDR2006024Floorbeam · damagedVERTICAL WEB OF BS 520 FLOORBEAM DAMAGED AT RBL 36. REPAIRED DAMAGED AREA IAW EA 53-273.SDR SB06097Switch · shortedCLT - FLT1770 EN ROUTE FROM MYR TO CLT, CREW REPORTED THAT BOTH THE CAPTAIN'S AND FIRST OFFICER'S FIRE WARNING LIGHTS FLASH CONSTANTLY DURING FLIGHT AND WHILE TAXING AFTER LANDING. SEEMS TO BE ASSOCIATED WITH TURBULENCE IN FLIGHT AND BUMPS ON THE TAXIWAYS ANSDR SB06096Battery Pack · dischargedMAINTENANCE REPORTED THE FIRST CLASS SEAT EMERGENCY LIGHTS DIM/INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECK GOOD.SDR PIDR2006019Floorbeam · corrodedUNDERSIDE OF BS 727D+5 FLOORBEAM IN AFT CARGO BIN IS CORRODED FROM LBL17 TO RBL8. REPAIRED AREA IAW SRM 53-00-53 FIG. 201.SDR PIDR2006020Skin · dentedEXISTING DOUBLER ON FUSELAGE AT BS 400 AND S23RT HAS A DENT. REMOVED EXISTING DOUBLER AND INSTALLED NEW IAW SRM 53-00-01 FIG. 201.SDR PIDR2006021Skin · wornFUSELAGE SKIN WORN UNDER DORSAL FIN. REPAIRED AREA IAW SB 737-55-1057.SDR PIDR2006022Floorbeam · corrodedFLOORBEAM AT BS 312 CORRODED AT NUTPLATE HOLES FROM RBL8 TO RBL32. REPLACED FLOORBEAM T-CAP IAW SRM 53-10-51.SDR USAA061192Skin · puncturedRT ELEVATOR UPPER SURFACE APPROX 19.5 INCHES FROM ROOT AND 18.0 INCHES FROM TAB TRAIL. COMPOSITE REPAIR IAW SRM 51-70-17, DEFECT SIZE: .200" X .050".SDR USAA061193Skin · crackedSTA 727D AND 727E ABOVE S-24L CRACKED. INSTALLED DOUBLER IAW EA 98091, DEFECT SIZE: 3.5 INCHES.SDR USAA061194Skin · crackedBS 951 BETWEEN S-14R AND S-15R CRACKED. INSTALLED DOUBLER IAW SRM 53-60-01 REPAIR 7, DEFECT SIZE: .25 INCH.SDR USAA061195Skate Angle · wornBS 1006 AT VERTICAL STAB HAS WEAR. REMOVED DAMAGED ANGLE, FABRICATED AND INSTALLED REPAIR ANGLE IAW TR 53-20-05A, DEFECT SIZE: 3 INCHES.SDR USAA061196Skin · wornKG WING, PYLON I/B SKATE ANGLE WING ATTACH HAS WEAR. OVERSIZED THE AFFECTED FASTENER HOLES AND REASSEMBLED WITH NEW OVERSIZED FASTENERS IAW EA 98052, DEFECT SIZE: .187 INCH.SDR USAA061187Frame · crackedBS 727D LBL 1 FRAME CRACKED. CUT OUT DAMAGE, FABRICATED FRAME DOUBLER IAW SRM 51-70-11, DEFECT SIZE: 1 INCH.SDR USAA061188Frame · crackedSTA 727, S13L, S14L S15L IN CUTOUT FRAME CRACKED. REMOVED CRACKED AREAS OF FRAME IAW EA 98040, DEFECT SIZE: .125 INCH, .500 INCH, .750 INCH.SDR USAA061189Angle · corrodedRIGHT SIDE BETWEEN BS 727-767 HAS CORROSION. PART REPLACED WITH IDENTICAL PART IAW SRM 51-10-02 LEVEL 1 C53-202-01, DEFECT SIZE: .50 INCH.SDR USAA061190Skate Angle · wornBS 1006 AT VERTICAL STAB HAS WEAR. REMOVED DAMAGED ANGLE IAW TR 53-20-05A, DEFECT SIZE: 3 INCHES.SDR USAA061177Skin · delaminatedLOWER SURFACE 10.6 IB OF THE OB END 2.0 UP FROM LOWER EDGE REMOVED DAMAGE, RECORE AND INSTALL EXT DOUBLER IAW SRM 51-70-10 DEFECT SIZE: 1.250 INCH X1.250 INCH.SDR USAA061178Wedge · delaminatedUPPER SURF OB END OF NR2 SLAT AT WEDGE. REMOVED DAMAGED CORE INSTALLED NEW CORE IAW SRM 51-70-10 DEFECT SIZE: 7.5 INCHES X 5.0 INCHES.SDR USAA061179Stiffener · corrodedSTA 727 BL0, REMOVE AND REPLACED DAMAGED PART IAW SRM 51-10-02 DEFECT SIZE: 6.0 INCH X 1.0 INCH.SDR USAA061180Wedge · debondedDEBONDED UPPER SURF IB END OF NR 2 SLAT AT WEDGE REMOVED DAMAGED CORE, RECORED AND INSTALLED DOUBLER IAW SRM 51-70-10 DEFECT SIZE: 6.0 INCHES X5.0.SDR USAA200609003Skin · crackedFOUND 1.8750 INCH LONG CRACK IN SKIN AT STA 727 LONGERON 22L. CUT OUT CRACKED AREA/HFEC/INSTALLED DOUBLER IAW SRM 53-00-01.SDR USAA061166Angle · crackedFOUND ANGLE CRACKED, STA 294 STR 12L. REMOVED DAMAGED PARTS AND INSTALLED FABRICATED PARTS IAW 65-17664 , DEFECT SIZE: 1".SDR USAA061168Skin · crackedFOUND LOWER LT WING O/B OF ENGINE FWD OF FRONT SPAR. REMOVED DAMAGE AND INSTALLED REPAIR PARTS IAW TR 57-41-02, DEFECT SIZE: 1".SDR USAA061169Skate Angle · wornFOUND WEAR ON BS 1006 LT SIDE OF VERTICAL STAB. REMOVED DAMAGED ANGLE, INSTALLED NEW ANGLE IAW TR 53-20-05A, DEFECT SIZE: 4".SDR USAA061170Skate Angle · wornFOUND WEAR BS 1020 LT SIDE OF VERTICAL STAB. REMOVED DAMAGED PART, INSTALLED FABRICATED PART IAW TR 53-20-05A, DEFECT SIZE: 3".SDR USAA061146Cover · wornRUDDER L/E LEFT SIDE FROM HINGE NR 1 LOWER TO HINGE NR 3. FABRICATED NEW HINGE COVER FROM 2024-T3 IAW SRM 55-40-01, DEFECT SIZE: 3 INCHES.SDR USAA061147Floorbeam · corrodedAROUND FASTENER HOLES ON T-CAP STA 344 WBL R 10 WBL L 19 CORROSION. REPLACED SECTION OF T-CAP IAW SRM 53-10-51 REPAIR 5 LEVEL 1 C53-107-02, DEFECT SIZE: .50 INCH.SDR USAA061142Strap · crackedBS 294-310 BETWEEN S-13L & S-14L CRACKED. REPLACED WITH IDENTICAL PART, IAW SRM 51-10-02, DEFECT SIZE: .187 INCH.SDR USAA061140Web · crackedSTA 291.5 S11R CRACKED. FABRICATED NEW WEB AND ATTACH ANGLE IAW SRM 65-45807, DEFECT SIZE: .75 INCH.SDR USAA061136Floorbeam · corrodedSTA 967 STA 986.5 RBL 18 AND LBL 18 CORROSION. REPLACED WITH IDENTICAL PART IAW SRM 51-40-02 LEVEL 1 C53-107-02, DEFECT SIZE: 1 INCH.SDR USAA061134Stringer Clip · crackedSTA 360 S11L CRACKED. REMOVED AND REPLACED CLIP IAW SRM 51-10-02, DEFECT SIZE: .175 INCH.SDR USAA061133Door Frame · crackedFWD SERVICE DOOR CUTOUT FWD FRAME CRACKED AT UPPER STOP FITTING. REPLACED FRAME 1141088, IAW SRM 51-10-02, DEFECT SIZE: .187 INCH.SDR USAA061126Strap · crackedBTM STA 312 FWD SIDE WBL 0 CRACK. REPLACED STABILIZER STRAP IAW SRM 51-10-00, DEFECT SIZE: .50 INCH.SDR USAA061125Channel · corrodedBS 500-500A BL 0 UNDER FWD CARGO FLOOR CORROSION. REMOVED CORRODED CHANNEL AND FABRICATED NEW HAT CHANNEL IAW SRM 51-10-02 LEVEL 1 C53-208-01, DEFECT SIZE: 3 X 8 INCHES.SDR USAA061121Attach Angle · crackedSTA 360R BETWEEN S13R & S14R FRAME TO SKIN ATTACH ANGLE CRACK. FABRICATED NEW ANGLE PER DWG 69-48204, DEFECT SIZE: .125 INCH.SDR USAA061104Support Fitting · corrodedFOUND CORROSION NLG W/WELL ACTUATOR SUPPORT FITTING. SCRAPPED AND REPLACED WITH NEW PER BOEING DWG, SRM 51-00 DEFECT SIZE: 0.5" BY 1.0".SDR USAA061091Frame · crackedFOUND FRAME CRACKED, STA 500A S8L S9L. REMOVED DAMAGE, INSTALLED DOUBLERS IAW SRM 53-10-20D, DEFECT SIZE: .5".SDR USAA061092Frame · crackedFOUND FRAME CRACKED, STA 480 S8R, S9R. REMOVED DAMAGE, INSTALL DOUBLERS IAW SRM 53-10-20D, DEFECT SIZE: .5".SDR USAA061093Frame · crackedFOUND FRAME CRACKED, STA 440 S8L S9L. REMOVED DAMAGE, INSTALLED DOUBLER IAW SRM 53-10-20D, DEFECT SIZE: .5".SDR USAA061094Frame · crackedFOUND FRAME CRACKED, STA 440 S8R, S9R. REMOVED DAMAGE, INSTALLED DOUBLER IAW SRM 53-10-20D, DEFECT SIZE: .5".
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