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 USAA061348Panel · crackedSTA 685 AT KEELBEAM PANEL CRACKED. DEFECTIVE PART REPLACED WITH IDENTICAL PART, REMOVED AND REPLACED IAW BOEING DWG 65-45866, DEFECT SIZE: 2 INCHES.SDR PIDR2006046Slat · damagedLT WING LEADING EDGE AT THE OB END OF THE NR3 SLAT DAMAGED. REPAIRED DAMAGE PER SRM 51-70-11, 51-70-14, AND 51-70-16.SDR PIDR2006047Hinge · damagedRT ELEVATOR LOWER SIDE AT NR 5 HINGE HAS DAMAGE. REPAIRED IAW SRM 51-70-17 AND MFG MESSAGE NR 1-247071893 WITH FAA DOA APPROVAL FORM 8100-9.SDR USAA061334Tee Fitting · crackedLEFT WING STA 135 INTERNAL CRACKED. REMOVED DAMAGE AND INSTALLED REPAIR PARTS IAW EA 98206, DEFECT SIZE: 2 INCHES.SDR USAA061335Angle · crackedLOWER TEE ANGLE INSIDE OF RIGHT WING FUEL TANK AT WS 135 CRACKED. REMOVED DAMAGE, FABRICATED REPAIR TEE, FILLER AND DOUBLER AND INSTALLED IAW EA 98207, DEFECT SIZE: 2.0 INCH.SDR USAA061336Spar · crackedLEFT WING REAR SPAR STA 223 CRACKED. REMOVED AND REPLACED IMG BEAM SUPPORT FITTING PER EA 98203, DEFECT SIZE: .125 INCH.SDR USAA061331Door Frame · crackedFWD SERVICE DOOR FWD STUB FRAME CRACKED. REMOVED DAMAGED FRAME AND FABRICATED REPAIR PARTS AND INSTALLED NEW FRAME IAW SRM 51-20-01, DEFECT SIZE: .125 INCH.SDR USAA061332Intercostal · crackedBS 344 STR 3R CRACKED. REMOVED DAMAGED INTERCOSTAL AND FABRICATED INTERCOSTAL/WEB IAW EA 98233, DEFECT SIZE: .25 INCH.SDR USAA061320Intercostal · crackedBS 294.5 AND STR 7L CRACKED. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-10-02, DEFECT SIZE: 1 INCH.SDR USAA061325Skin · delaminatedLEFT I/B AFT FLAP O/B END LWR SIDE DELAMINATED. REMOVED DAMAGE AND INSTALLED REPAIR PARTS IAW SRM 51-70-10, DEFECT SIZE: 5.250 X 11 INCHES.SDR USAA061324Intercostal · crackedSTR 14 BETWEEN STA 277 AND STA 294.5 CRACKED. REMOVED DAMAGED INTERCOSTAL AND INSTALLED NEW PART IAW DWG 65-45807, DEFECT SIZE: .250 INCH.SDR USAA061323Spar · crackedLEFT LG REAR SPAR UPPER CHORD CRACKED. REAMED AND REWORKED FASTENER HOLE IAW EO 5702V054, DEFECT SIZE: .25 INCH.SDR USAA061321Skin · crackedFWD GALLEY DOOR INNER SKIN CRACKED. REMOVED DAMAGE AND INSTALLED FABRICATED REPAIR PARTS IAW TR 52-10-16, DEFECT SIZE: 1 INCH.SDR USAA061310Structure · crackedLEFT WING STA 135 INTERNAL CRACKED. REMOVED DAMAGE AND INSTALLED REPAIR PARTS IAW EA 98206, DEFECT SIZE: 2.5 INCHES.SDR USAA061319Skin · crackedFWD GALLEY DOOR INNER SKIN CRACKED. REMOVED DAMAGE AND INSTALLED FABRICATED REPAIR PARTS IAW TR 52-10-16, DEFECT SIZE: 1 INCH.SDR USAA061318Frame · crackedBS 291.5 BETWEEN STR 11R AND 10R CRACKED. REMOVED DAMAGE AND INSTALLED REPAIR PARTS IAW DWG 65-45807, DEFECT SIZE: 2 INCHES.SDR USAA061317Angle · corrodedSTA 312 360 AT ENTRY DOOR HAS CORROSION. DEFECTIVE PART REPLACED WITH IDENTICAL PART IAW SRM 51-10-02 LEVEL 1 C53-107-02, DEFECT SIZE: 48 INCHES.SDR USAA061316Support Angle · crackedBETWEEN STA 291.5 AND LOWER STUB FRAME FOR RIGHT SERVICE DOOR CUTOUT. FABRICATED REPAIR ANGLE AND INSTALLED IAW SRM 51-10-02, DEFECT SIZE: 1 INCH.SDR USAA061315Angle · crackedSTA 360 STR 15L ANGLE CRACKED. DEFECTIVE PART REPLACED WITH IDENTICAL PART IAW SRM 51-10-02, DEFECT SIZE: 1 INCH.SDR USAA061313Angle · corrodedSTA 312 TO 360 AT ENTRY DOOR HAS CORROSION. REMOVE AND REPLACE IAW SRM 51-10-02 LEVEL 1 C53-107-02, DEFECT SIZE: 48 INCHES.SDR USAA061312Angle · corrodedAFT CARGO RT SIDE FROM STA 747-767 HAS CORROSION. REMOVED DAMAGE AND INSTALLED FABRICATED REPAIR PARTS IAW SRM 53-30-53 LEVEL 2 C53-202-01, DEFECT SIZE: 20 INCHES.SDR USAA061311Floorbeam · corrodedSTA 344 24 INCHES FROM LEFT OF BUTT LINE -0- HAS CORROSION. INSTALLED NEW T-CAP SECTION, IAW SRM 53-10-51 FIG 201 LEVEL 1 C53-107-02, DEFECT SIZE: 1 X 1 INCH.SDR USAA061322Spar · crackedLEFT LG REAR SPAR UPPER CHORD CRACKED. REAMED AND REWORKED FASTENER HOLE IAW EO 5702V054, DEFECT SIZE: .25 INCH.SDR PIDR2006044Skin · damagedFASTENER HOLES JUST FORWARD AND ABOVE THE RIGHT FWD DOOR UPPER HINGE CUTOUT AND JUST FORWARD OF THE LOWER HINGE CUTOUT ARE CRACKED. REPAIRED SKIN AND BEAR STRAP IAW MESSAGES 1-232472835 WITH FAA DER APPROVED 8100-9 DATED NOV. 3, 2006.SDR PIDR2006045Structure · crackedFASTENER HOLES CRACKED AT THE UPPER HINGE CUTOUT AND LOWER HINGE CUTOUT OF THE LT FORWARD ENTRY DOOR. REPAIRED AREA IAW MESSAGE 1-232472835 WITH FAA DER APPROVED 8100-9 DATED NOV.3, 2006.SDR USAA061299Angle · corrodedAFT RIGHT DOOR ZEE ANGLE BETWEEN STA 917.5 TO STA 1006 CORROSION. REMOVED DAMAGED ZEE ANGLE AND REPLACED WITH NEW ANGLE IAW SRM 51-40-02 C53-107-02 LEVEL 1, DEFECT SIZE: 12 X 3 INCHES.SDR USAA061300Angle · crackedLOWER TEE ANGLE INSIDE OF RIGHT WING FUEL TANK AT WS 135. REMOVED DAMAGE, FABRICATED REPAIR TEE, FILLER AND DOUBLER INSTALLED IAW EA 98207, DEFECT SIZE: 2.0 INCHES.SDR USAA061301Floor Support · corrodedAFT CARGO RT SIDE FROM STA 747 TO 767 CORROSION. REMOVED DAMAGE AND INSTALLED FABRICATED REPAIR PARTS LEVEL 2 C53-202-01, DEFECT SIZE: 20 INCHES.SDR USAA061302Keelbeam · crackedSTA 685 AT KEEL BEAM CRACKED. REMOVED AND REPLACED DAMAGE, DEFECT SIZE: 2 INCHES.SDR USAA061303Skin · delaminatedLEFT I/B AFT FLAP O/B END LWR SIDE DELAMINATED. REMOVED DAMAGE AND INSTALLED REPAIR PARTS IAW SRM 51-70-10, DEFECT SIZE: 5.250 X 11 INCHES.SDR USAA061304Floorbeam · corrodedSTA 312 BUTT LINE 0 CORROSION. REMOVED DAMAGED SECTION OF TEE CAP AND INSTALLED REPAIR PARTS IAW SRM 53-10-51 LEVEL 2 C53-107-02, DEFECT SIZE: .25 INCH.SDR USAA061305Door Frame · crackedFWD CARGO DOOR FRAME AT STA 440 STR 24R LOWER O/B HOLE CRACKED. REMOVED DAMAGE FRAME AND INSTALLED NEW FRAME IAW DWG 6-15224, DEFECT SIZE: 1 INCH.SDR PIDR2006040Tab · separatedTRAILING EDGE OF THE RT AILERON TAB IS SEPARATED. REPAIRED MINOR DAMAGE PER SRM 51-70-16. BALANCED TAB, NO WEIGHT CHANGE.SDR USAA061292Angle · corrodedFOUND Z-ANGLES CORRODED, MAIN ENTRY DOOR SILL SUPPORT STRUCTURE. INSTALLED BLENDED MINOR SURFACE CORROSION IAW SRM 51-10-02 LEVEL 1 C53-107-01, DEFECT SIZE: 10" BY .50".SDR USAA061284Stringer · corrodedFOUND CORROSION STRINGER 28R AT BS 323 TO BS 1177. REMOVED DAMAGED AREAS OF STRINGER AND REPAIRED IAW SRM 51-10-02 LEVEL 2 C53-107-02, DEFECT SIZE: 2" BY 1".SDR USAA061283Angle · crackedFOUND CRACK LOWER T CHORD ANGLE INSIDE OF RT WING FUEL TANK AT WS 135. REMOVED DAMAGED, FABRICATED REPAIR TEE, FILLER AND DOUBLER IAW EA 98207, DEFECT SIZE: 2".SDR USAA061282Frame · crackedFOUND CRACK, BS 492.4 FWD DOOR FRAME. REMOVED CRACKED FRAME AND INSTALLED NEW FRAME IAW SRM 51-40-02, DEFECT SIZE: .25".SDR USAA061281Intercostal · corrodedFOUND INTERCOSTAL CORRODED STA 320 12" LEFT OF BUTT LINE 0. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-10-02 LEVEL 1 C53-107-02, DEFECT SIZE: .2".SDR USAA061287Angle · corrodedFOUND CORROSION AFT ENTRY DOOR SILL. REMOVED AND REPLACED ZEE ANGLE WITH NEW PART IAW SRM 51-40-03 C53-107-02, DEFECT SIZE: 20".SDR USAA061265Stringer · corrodedS28R, BS 323 TO BS 1177 CORROSION. REMOVED DAMAGE AREAS OF STRINGER AND REPAIRED IAW SRM 51-10-02 LEVEL 1 C53-107-02, DEFECT SIZE: 1 INCH.SDR USAA061276Channel · corrodedSTA 986 LBL 14 CORROSION. BLENDED MINOR SURFACE CORROSION AND TREATED IAW SRM 51-10-02 LEVEL 1 C53-107-02, DEFECT SIZE: 2 INCHES.SDR PIDR2006043Fitting · corrodedCORROSION ON THE FORWARD FACE AND INSIDE DIAMETER OF THE RT FORWARD DRAG ANGLE FITTING AT THE VERTICAL STABILIZER AFT RT ATTACH FITTING. REPLACED FITTING IAW SRM 51-40-02, 51-40-03, AND DRAWING NR 65-53744.SDR PIDR2006036Skin · crackedCRACK IN FUSELAGE SKIN AT AFT LOWER CORNER OF FORWARD SERVICE DOOR (R1). NDT CONFIRMED ADDITIONAL CRACK IN BONDED DOUBLER. REPAIRED AREA IAW SRM 53-00-01 FIG. 201 REPAIR 32 AND EA NR 53-265.SDR USAA061251Stringer Splice · crackedSTA 908 S41 CRACK. REMOVED AND REPLACED STRINGER SPLICE IAW SRM 51-10-02, DEFECT SIZE: .125 INCH.SDR USAA061255Stiffener · crackedSTA 320 CRACK. REMOVED AND REPLACED WITH PARTS IAW SRM 51-10-02, DEFECT SIZE: .375 INCH.SDR PIDR2006037Frame · crackedCRACKS IN BS663.75 FRAME AT STR 2RT AND STR 3RT. REPAIRED FRAME IAW SRM 53-00-07.SDR USAA061250Stringer Clip · crackedFOUND TIE CLIP CRACKED, S2R, STA 907. REMOVED AND REPLACED TIE CLIP IAW SRM 51-10-02, DEFECT SIZE: .125".SDR PIDR2006032Skin · corrodedCORROSION IN FUSELAGE SKIN IN AREA OF LT KEELBEAM (STR 28LT) AND RT KEELBEAM (STR 28RT)AT BS727A-4. CUT OUT FUSELAGE SKIN FOR ACCESS TO LT AND RT KEELBEAMS. REMOVED CORROSION FROM LT AND RT KEELBEAM AREAS WITHIN LIMITS OF SRM 53-60-12 FIG. 101. REPLACED CORSDR SB06103Windshield · crackedORD FLT 1623 DURING CRUISE AT FL340, EN ROUTE FROM CLT TO MSP, THE CAPTAIN'S L1 WINDSHIELD OUTER PANE CRACKED. PRESSURIZATION HELD OK. WINDOW HEAT WAS TURNED OFF AND NO FURTHER CRACKING WAS NOTED. FLIGHT DIVERTED TO ORD AND LANDED WITHOUT FURTHER INCIDENT. SDR USAASB06102Windshield · crackedPHL FLT1428 - EN ROUTE FROM RDU TO PHL, CREW REPORTED THE CAPTAINS'S NR 1 WINDOW OUTER PANE CRACKED. OBSERVED ARCING FROM THE UPPER RIGHT SIDE, THEN CRACKING. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE CAPTAIN'S WINDSHIELD
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