Boeing 737-2B7
Service difficulty reports · 1,360
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 = '7372B7' 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 = '7372B7' 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 USAA000902Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .125 INCH, BS 559, STRINGER 3R. REPLACED TIE CLIP PER EO 5393G227. (M)SDR USAA000901Support Bracket · crackedCLT - FOUND VERT SUPPORT CRACKED .500 INCHES, BS 520, BL 0. INSTALLED REPAIR PER EA 67536 AND SB 737-53-1120. (M)SDR USAA000900Stringer · crackedCLT - FOUND STRINGER CRACKED .25 INCH, BS 520 TO 540, STRINGER 15L AT RIVETS. INSTALLED REPAIR PER SRM 53-10-3 FIG 1. (M)SDR USAA000899Stringer · crackedCLT - FOUND STRINGER .25 INCH CRACKED, BS 520 TO 540 STRINGER 15R AT RIVETS. INSTALLED REPAIR PER SRM 53-10-3. (M)SDR USAA000898Floorbeam · corrodedCLT - FOUND T-CAP CORRODED 2 INCHES, BS 294.5 AT BL 0. FABRICATED REPAIR PER TR 53-10-04B. (M)SDR USAA000890Skin · crackedCLT - FOUND .25 INCH CRACK, FUSELAGE SKIN UPPER CORNER L1 WINDOW. INSTALLED DOUBLER PER 53-30-3. (M)SDR USAASB00180Line · rupturedTPA - FLT 2676 - AFTER TAKEOFF AND GEAR RETRACTION FROM TPA, THE LEFT MAIN LANDING GEAR UNSAFE LIGHT ILLUMINATED. CREW FOLLOWED QUICK REF HANDBOOK PROCEDURES AND SAFE GEAR INDICATIONS WERE RECEIVED. HOWEVER, CREW NOTICED THAT HYDRAULIC PRESSURE HAD DECREASEDSDR USAASB00178Csd · failedATL - FLT 2999 - ON CLIMB-OUT FROM TPA, THE NR 1 ENGINE CONSTANT SPEED DRIVE HIGH OIL TEMPERATURE LIGHT ILLUMINATED. CREW COMPLIED WITH QUICK REFERENCE HANDBOOK PROCEDURES, DISCONNECTED THE NR 1 ENGINE CSD AND STARTED THE APU. AFTER 20 MINUTES OF RUNNING THESDR USAA000881Stringer · crackedCLT - FOUND STRINGER CRACKED .125 INCH, STRINGER 15R BETWEEN STATION 520 AND 540. REMOVED AND INSTALLED NEW STRINGER SECTION PER SRM 53-10-03. (M)SDR USAA000876Floorbeam · crackedCLT - FOUND T-CAP AND WEB CRACKED 5 INCHES, UPPER T-CAP AND CHORD BS 663, BL 0. REPAIRED T-CAP AND CHORD PER EA 67418 AND TR 57-10-04. (M)SDR USAA000875Skin · corrodedCLT - FOUND SKIN CORRODED 4 INCHES, STATION 947.5 FUSELAGE DRAIN BETWEEN STRINGER 27L AND 27R. INSTALLED DOUBLER AND FILLER PER SRM 53-30-3. CORROSION LEVEL 1. (M)SDR USAA000874Frame · corrodedCLT - FOUND FRAME CORRODED 1 INCH BY 3 INCHES, BS 767 BETWEEN STRINGER 26R AND 26L, LBL 0. INSTALLED REPAIR DOUBLER PER SRM 53-10-04, FIG 11. CORROSION LEVEL 1. (M)SDR USAA000877Skin · corrodedCLT - FOUND SKIN CORRODED 3 INCHES BY 6 INCHES, BETWEEN BS 767 AND 787, BL 0 VHF ANTENNA NR 3. INSTALLED DOUBLER PER SRM 53-30-3, FIG 6. (M)SDR USAASB00171Duct · rupturedTPA - FLT 2704 - ON CLIMB-OUT FROM TPA, AT 6,000 FEET, THE NR 2 ENGINE OVERHEAT LIGHT ILLUMINATED. CREW ACCOMPLISHED QUICK REFERENCE HANDBOOK PROCEDURES. WHEN THROTTLE WAS REDUCED, LIGHT EXTINGUISHED. WHEN THROTTLE WAS ADVANCED, LIGHT ILLUMINATED AGAIN. FLISDR USAA000857Stringer · corrodedCLT - FOUND STRINGER CORRODED 7 INCHES BY 7 INCHES, STATION 922-929 UNDER STRINGER 27R. INSTALLED REPAIR DOUBLER PER SRM 53-30-3. CORROSION LEVEL 1, C53-208-01. (M)SDR USAA000853Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 3 INCHES, STATION 1006 STRINGER 20L. SPLICE AND INSTALLED DOUBLERS PER SRM 53-10-4, 51-30-1 AND 04. CORROSION LEVEL 1, C53-202-01. (M)SDR USAA000847Angle · corrodedCLT - FOUND Z-ANGLE CORRODED .250 INCH BY .250 INCH, BS 270, BL 0. REPLACED Z-ANGLE PER TR 53-20-04. (M)SDR P2EA00209Threshold · dentedMCI - FORWARD CARGO THRESHOLD HAS DENT .50 INCH IN LENGTH, 1 INCH WIDE AND .125 INCH DEEP, DO TO GROUND DAMAGE. INSPECTED DENT AT FORWARD CARGO THRESHOLD PER BOEING SRM 51-00-4 AND 53-30-1 AND FOUND TO BE WITHIN LIMITS PLACED ON WATCH ITEM W126446. (M)SDR USAA000849Pressure Panel · crackedCLT - FOUND SKIN CRACKED .5 INCH, W/W STATION 664, LBL 31 PRESSURE DECK SKIN. REPAIRED PER TR 53-60-04 FIG 1. (M)SDR USAA000843Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .25 INCH, BS 360, STRINGER 4R TIE CLIP. REPAIRED PER SRM 51-10-01. (M)SDR USAA000846Web · crackedCLT - FOUND 3 CRACKS .250 INCH, WEB UNDER SCUFF PLATE FROM STATION 807 TO 839, BL 18R. REPLACED WEB PER 51-10-1. (M)SDR USAA000845Floorbeam · crackedCLT - FOUND T-CAP CRACKED 1 INCH, STATION 520 FLOORBEAM T-CAP UPPER RADIUS, LBL 24.5. REPAIRED PER EA 67383. (M)SDR USAA000844Stringer · crackedCLT - FOUND STRINGER CRACKED .250 INCH, BS 344-360, STRINGER 15R. INSTALLED NEW STRINGER PER SRM 51-10-1, SRM 51-10-2. (M)SDR USAA000810Floorbeam · crackedCLT - FOUND T-CAP FLOORBEAM CRACKED .5 INCH, AFT SIDE STATION 520 UPPER RADIUS LBL 45.5. INSTALLED FILLERS, CHANNELS, WEB ANGLE PER EA67383. (M)SDR USAA000812Skin · crackedCLT - FOUND SKIN CRACKED 2.25 INCH, AFT LOWER CORNER FORWARD SERVICE DOOR CUTOUT. REPAIRED WITH DOUBLER AND FILLER PER SRM 53-30-3 AND 53-30-10. (M)SDR USAA000811Web · crackedCLT - FOUND WEB CRACKED 1 INCH, STATION 948, BELOW STRINGER 11L. INSTALLED REINFORCING STRAP PER TR 53-30-07A. (M)SDR P2EA000204Skin · damagedOKC - FLT BAGGAGE LOADER CONTACTED AIRCRAFT AT BS 460, NEAR STRINGER 26 RT, LENGTH 4 INCHES WIDE, .250 INCH DEPTH .040 INCHES. REPAIRED FUSELAGE SKIN SECTION AT BS 462, STRINGER 26TH PER SRM 53-31-00 AND BOEING FAX AOC-OKC-00-00114H DATED JUNE 10, 2000. (M)SDR USAASB00160Battery Pack · dischargedTPA - MAINTENANCE FOUND THE SEAT MOUNTED EMERGENCY EVACUATION LIGHTS FROM SEAT ROWS 1 THROUGH 6 INOPERATIVE AND THE EMERGENCY EXIT LIGHTS IN THE LEFT EMERGENCY EXIT ROW INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACKS AT SEAT ROW 6 AND SEAT ROWSDR USAA000807Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .25 INCH, BS 360, STRINGER 4R. FABRICATED TIE CLIP PER SRM 51-10-01. (M)SDR USAASB00158Contactor · failedCLT - FLT 2668 - EN ROUTE FROM MCO-IAD, AT FL290, THE NR 1 TRANSFER BUS CIRCUIT BREAKER POPPED. CREW RESET CIRCUIT BREAKER BUT IT POPPED AGAIN FIVE MINUTES LATER. FLIGHT DIVERTED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTESDR USAA000803Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED .250 INCH BY .250 INCH, BS 312, RBL 11-36. INSTALLED NEW T-CAP PER SRM 53-10-9. INSTALLED NEW T-CAP PER SRM 53-10-9. (M)SDR USAASB00156Battery Pack · dischargedCLE - MAINTENANCE FOUND THE EMERGENCY LIGHTS AT THE LEFT OVERWING AND BELOW THE FLAPS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AND CHARGER ASSEMBLY (P/N 60-1321-1). OPERATIONAL CHECK GOOD. (M)SDR USAA000796Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .025 INCH, STRINGER 10R AT BS 747. REPLACED TIE CLIP PER EO 393G227. (M)SDR USAA000795Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .025 INCH, STRINGER 6R AT BS 747. RE-INSTALLED TIE CLIP PER EO 393G227. (M)SDR USAA000794Tie Clip · crackedCLT - FOUND TIE CLIP .025 INCH CRACK, STRINGER 5L AT BS 685. REPLACED TIE CLIP PER SRM 51-10-1. (M)SDR USAA000793Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .025 INCH, STRINGER 11L AT BS 663. REPLACED CLIP PER SRM 51-10-1. (M)SDR USAA000792Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .5 INCH, STATION 616 RT, STRINGER 3R. REMOVED AND REPLACED WITH NWE CLIP PER SRM 51-10-01. (M)SDR USAA000791Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .250 INCH, BS 597 STRINGER 9L. REMOVED AND REPLACED WITH NEW CLIP PER SRM 51-10-1. (M)SDR USAA000790Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .5 INCH, STATION 597 RT STRINGER 9R. REMOVED AND REPLACED NEW CLIP PER SRM 51-10-01. (M)SDR USAA000789Skin · crackedCLT - FOUND SKIN CRACKED .125 INCH, STATION 380 EQUIP COOLING DUCT. INSTALLED DOUBLER PER TR 53-30-04 DWG NR 65C33930. (M)SDR USAA000788Tie Clip · crackedCLT - FOUND STRINGER TIE CLIP CRACKED .5 INCH IN 2 PLACES, STATION 380, LBL 22, LWR FRAME. REPLACED TIE CLIP PER SRM 51-10-1. (M)SDR USAA000787Angle · crackedCLT - FOUND SUPPORT ANGLE CRACKED, BS 291.5, BETWEEN STRINGER 11 AND 12R. REPAIRED PER SRM 51-10-1. (M)SDR USAA000782Floorbeam · corrodedCLT - FOUND FLOORBEAM T-CAP CORRODED 1 INCH IN 6 AREAS, BS 344 LBL 49, BL 0 FASTENER HOLES. INSTALLED NEW T-CAP PER TR 53-10-13. (M)SDR USAASB00153Flap · jammedTPA - FLT 2797 - AS AIRCRAFT WAS BEING CONFIGURED FOR FINAL APPROACH TO TPA, THE RIGHT INBOARD TRAILING EDGE FLAP BECAME JAMMED WHEN THEY WERE MOVED FROM 10-15 DEGREES. CREW ACCOMPLISHED PROCEDURES AND A GO-AROUND AND DECLARED AN EMERGENCY. FLIGHT LANDED WITSDR USAA000756Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .25 INCH, BS 787 STRINGER 10R. INSTALLED NEW TIE CLIP PER EO 5393G227. (M)SDR USAA000755Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .025 INCH, BS 727B, STRINGER 8R. INSTALLED TIE CLIP PER EO 393G227. (M)SDR USAA000754Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .025 INCH, BS 727B, STRINGER 5R. INSTALLED TIE CLIP PER EO 393G337. (M)SDR USAA000753Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .025 INCH, BS 706, STRINGER 13R. REINSTALLED TIE CLIP PER SRM 51-30-02. (M)SDR USAA000752Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .025 INCH, BS 706, STRINGER 11L. INSTALLED TIE CLIP EO 5393G227. (M)SDR USAA000751Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .025 INCH, BS 706, STRINGER 3L. REPLACED TIE CLIP PER SRM 51-30-02. (M)
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