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 USAA991127Floorbeam · corrodedTPA - DURING CX-3 CHECK VISUAL INSPECTION, FOUND TWO CORRODED AREAS AFT CARGO COMP FIRST FLOORBEAM INSIDE DOOR. CORROSION LEVEL 1. REPLACED WITH IDENTICAL PART. (M)SDR USAA991124Frame · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .50 INCH CRACK ON SKIN AT LOWER AFT CORNER OF SERVICE DOOR CUT-OUT SKIN. INSTALLED EXTERNAL REPAIR DOUBLER PER SRM 53-10-01. (X)SDR USAA991123Skin · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .250 INCH CRACK AT FORWARD SERVICE DOOR LOWER HINGE CUT-OUT UPPER CORNER SKIN. INSTALLED EXTERNAL DOUBLER PER EA 65883. (X)SDR USAA991122Frame · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .1250 INCH CRACK AT STA 480 BETWEEN STR 8L AND STR 9L FRAME. INSTALLED REPAIR ANGLE AND FILLER PER EA 65705. (X)SDR USAA991121Frame · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .1250 INCH CRACK AT STA 907 BETWEEN STR 8L AND STR 9L FRAME. INSTALLED REPAIR ANGLE AND FILLER PER EA 65705. (X)SDR USAA991120Frame · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .1250 INCH CRAACK AT STA 927 BETWEEN STR 8R AND STA 9R FRAME. INSTALLED REPAIR ANGLE AND FILLER PER EA 65705. (X)SDR USAA991119Frame · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .1250 INCH CRACK AT STA 847 BETWEEN STR 8R AND STR 9R FRAME. INSTALLED REPAIR ANGLE AND FILLER PER EA 65705. (X)SDR USAA991118Frame · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .1250 INCH CRACK AT STA 827 BETWEEN STR 8R AND STR 9R FRAME. INSTALLED REPAIR ANGLE AND FILLER PER EA 65705. (X)SDR USAA991117Frame · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .1250 INCH CRACK AT STA 480 BETWEEN STR 8R AND STR 9R FRAME. INSTALLED REPAIR ANGLE AND FILLER PER EA 65705. (X)SDR USAA991116Floorbeam · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT BS 520, LBL 45.5 IN RADIUS FORWARD SIDE OF FLOORBEAM. INSTALLED DOUBLER, FILLER AND REPAIR ANGLES PER EA 65721 AND S/B 737-53-1120. (M)SDR USAA991115Floorbeam · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT BS 520, LBL 24.75 IN RADIUS FORWARD SIDE OF FLOORBEAM. INSTALLED DOUBLER, FILLER AND REPAIR ANGLES PER EA 65721 AND SB 737-53-1120. (M)SDR USAA991114Floorbeam · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT BS 520, RBL 45.5 IN RADIUS FORWARD SIDE OF FLOORBEAM. INSTALLED DOUBLER, FILLER AND REPAIR ANGLES PER EA 65721 AND S/B 737-57-1120. (M)SDR USAA991113Clip · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT BS 847, STRINGER 25L TIE CLIP. INSTALLED NEW STRINGER TIE CLIP PER SRM 51-10-02. (M)SDR USAA991112Clip · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT BS 727B, STRINGER 25L TIE CLIP. REPLACED WITH IDENTICAL PART PER SRM 51-10-2. (M)SDR USAA991104Clip · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT BS 827, STRINGER 25L TIE CLIP. REPLACED WITH IDENTICAL PART PER SRM 51-10-2. (M)SDR USAA991103Frame · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION 3 INCH BY 5 FT AT FORWARD FRAME OF AFT CARGO DOOR OUTBOARD OF SILL FRAME. CORROSION LEVEL 1, CORROSION TASK NR C53-202-01. REPAIRED PER BOEING 737-300 SRM 53-60-15. (M)SDR USAA991099Floorbeam · corrodedCLT - DURING Q-4 CEHCK VISUAL INSPECTION, FOUND 4 CORRODED AREAS .75 INCH BY .5 INCH EACH AT BS 312, WL 208.1, LBL 14, LBL 20, LBL 26 AND LBL 33 FLOORBEAM. CORROSION LEVEL 2. CORROSION TASK NR C53-107-02. INSTALLED NEW T-CAP, REPAIR ANGLES AND STRAPS PER SRSDR USAA991098Floorbeam · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 5 CORRODED AREAS .75 INCH BY .5 INCH EACH AT BS 312, WL 208.1, LBL 11 TO RBL 8 FLOORBEAM. CORROSION LEVEL 2, CORROSION TASK NR C53-107-02. REPAIRED T-CAP AND SPLICES PER SRM 53-10-51. (M)SDR USAA991097Creasebeam · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND SEVERAL CORRODED AREAS AT BS 290 TO BS 344, RBL 57, WL 208.1 CREASEBEAM INNER CHORD ANGLE. CORROSIN LEVEL 2, CORROSION TASK NR C53-107-02. REPAIRED Z-ANGLE PER SRM 51-30-01. (M)SDR USAA991061Floorbeam · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND SEVERAL 1 INCH BY 1 INCH CORROSION AREAS AT BS 344, WL 208.1, RBL 8 FLOORBEAM. CORROSION LEVEL 1. REPLACED T-CAP PER SRM 53-15-01A. (M)SDR USAA991060Floorbeam · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND SEVERAL .5 INCH BY .5 INCH CORROSION AREAS AT SCREW HOLES FLOORBEAM STATION 344, RBL 8 - RBL 56 UPPER CHORD. CORROSION LEVEL 1. REPLACED T-CAP PER SRM 53-15-01A. (M)SDR USAA991046Frame · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK AT STATION 400 BETWEEN STRINGER 8R AND STRINGER 9R FRAME. INSTALLED DOUBLER PER SRM 53-00-07 AND EA 65705. (M)SDR USAA991041Tie Clip · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK IN STRINGER TIE CLIP AT STATION 847 AND STRINGER 25L. INSTALLED NEW TIE CLIP PER SRM 51-10-02. (M)SDR USAA991040Floorbeam · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND NUMEROUS SPOTS OF CORROSION .5 INCH BY .5 INCH AT STATION 312, LBL 33 TO RBL 8 FLOORBEAM. CORROSION LEVEL 1. REPLACED T-CAP OF FLOORBEAM PER SRM 53-10-51. (M)SDR USAA991039Seat Track · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION 12 INCH BY .5 INCH AT BS 328 TO 340, WL 208.1, RBL 45 SEAT TRACK. CORROSION LEVEL 1, CORROSION TASK NR C53-107-02. REPLACED SEAT TRACK PER SRM 53-00-52. (M)SDR USAA991030Sill · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION WIDE SPREAD AFT CARGO DOOR SILL WEB. CORROSION LEVEL 2. CORROSION TASK NR C55-202-01. REPLACED WITH IDENTICAL PART PER SRM 51-10-02. (M)SDR USAASB99248Relay · failedPHL - FLT 346 - AFTER TAKEOFF THE CREW REPORTED THAT EVERYTIME THE STAB TRIM SWITCH WAS ACTUATED FROM EITHER YOKE, THE FIRST OFFICERS HSI HEADING FLAGS APPEARED. RELEASING THE SWITCH CAUSES THE FLAGS TO DISAPPEAR. DECISION WAS MADE TO RETURN TO FIELD AT PHL.SDR USAASB99244Mechanism · lack of lubePHL - FLT 1908 - DURING CLIMB-OUT FROM PHL, CREW NOTICED AN AIR LEAK FROM THE FORWARD MAIN ENTRY DOOR. FLIGHT RETURNED TO FIELD AT PHL AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE CLEANED AND LUBED THE FORWARD MAIN ENTRY DOOR SDR USAA991070Skin · crackedTPA - DURING CX-5 CHECK EDDY CURRENT AND VISUAL INSPECTION, FOUND A .3750 INCH CRACK IN FUSELAGE SKIN AT STA 380 AFT OF EQUIPMENT COOLING DUCT CUT-OUT. INSTALLED REPAIR DOUBLER PER TR 53-30-07 AND DRG 65C33930. (X)SDR USAASB99237Cover · leakingRIC - FLT 163 - DURING CLIMB-OUT FROM RIC, CREW REPORTED A LOUD AIR LEAK FROM THE FORWARD MAIN ENTRY DOOR. FLIGHT RETURNED TO FIELD AT RIC AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE LOWER MAIN ENTRY DOOR HINGE COVESDR USAASB99230Adc · failedPIT - FLT 1764 - EN ROUTE FROM PIT TO PWM DURING CRUISE AT FL 370, THE CAPTAIN'S ALTIMETER, AIRSPEED INDICATOR AND VSI BECAME INOPERABLE. NO CHANGE OCCURRED WITH CLIMB AND DESCENT FOR 15 MINUTES. FLIGHT RETURNED TO FIELD AT PIT AND WHILE ON DESCENT INTO PIT,SDR USAA990991Skin · crackedCLT - DURING A DAILY CHECK VISUAL INSPECTION, FOUND A 1.25 INCH CRACK AT BS 727D PLUS 2 INCH BETWEEN STRINTER 23L AND STRINGER 24L SKIN FUSELAGE. CUTOUT DAMAGE SKIN AND FABRICATED AND INSTALLED REPAIR DOUBLER PER TR 53-60-03. (M)SDR USAASB99222Seal · tornTPA - FLT 1469 - EN ROUTE FROM CLT TO TPA, ABOVE GAINESVILLE FLORIDA AT FL310, FLIGHT LOST PRESSURIZATION. THE CREW FELT A THUMP IN THE CABIN ALONG WITH A RISE IN CABIN ALTITUDE OF 4,000 FEET PER MINUTE. CREW DECLARED AN EMERGENCY AND QUICKLY DESCENDED TO 10SDR USAASB99224Wire · brokenPHL - DURING OVERNIGHT MAINTENANCE CHECK, MAINTENANCE FOUND A SECTION EMERGENCY FLOOR PATH LIGHTING THAT WOULD NOT TEST ON THE RIGHT SIDE OF THE CABIN. MAINTENANCE TROUBLESHOT AND FOUND BROKEN WIRES AT SEAT ROW 5 DEF. REPAIRED BROKEN WIRES. OPERATIONAL CHECSDR USAA990970Skin · crackedPHL - DURING RON, FOUND 1.5 INCH CRACK ON SKIN AT STATION 747 STRINGER 25R. REPAIRED WITH EXTERNAL DOUBLER PER SRM 53-00-01 FIG 202. (M)SDR USAASB99218Power Supply · inoperativeDCA - DURING WEEKLY CHECK, MAINTENANCE FOUND THE EMERGENCY LIGHTS LOCATED AT SEAT ROWS 2L, 10R AND 12L INOPERATIVE. MAINTENANCE REMOVED AND REPLACED M1136 POWER SUPPLY AT STATION 753 PER MM 33-51-00. OPERATIONAL CHECK GOOD. (M)SDR USAASB99216Computer · failedCLT - FLT 8052 - AIRCRAFT WAS FERRYING TO ABE FOR SCHEDULED SERVICE WHEN THE CAPTAIN REPORTED THE ELEVATOR FEEL DIFFERENTIAL PRESSURE LIGHT ILLUMINATED. FLIGHT DIVERTED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVSDR USAASB99215Stud · looseDFW - FLT 870 - CAPTAIN REPORTED THAT AFTER TAKEOFF FROM DFW AND CLIMBING THROUGH 17,000 FT, THE NR 1 ENGINE OIL TEMPERATURE ROSE ABOVE THE RED RADIAL. CREW SHUTDOWN THE NR 1 ENGINE, DECLARED AN EMERGENCY AND RETURNED TO FIELD AT DFW. FLIGHT LANDED WITHOUT FSDR USAA990909Frame · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .1250 INCH CRACK STA 847 FRAME AT STR 9R OVERHEAD BIN ATTACH POINT. INSTALLED FILLER AND REPAIR ANGLE PER EA 65193 AND SRM 53-00-07 FIG 202. (X)SDR USAA990908Frame · wornCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH SLIT WORN INTO FUSELAGE FRAME. BLENDED OUT DAMAGE, INSTALLED REPAIR DOUBLER PER TR 53-80-02. (X)SDR USAA990907Angle · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK LT RAM AIR INLET UPPER AFT ANGLE AT BS 520, STR21L. INSTALLED REPAIR FILLER AND DOUBLER PER TR 53-50-03. (X)SDR USAA990906Tie Clip · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A CRACK AT STRINGER TIE CLIP STA 616 AT STR 4L. REMOVED AND REPLACED PER SRM 53-00-03. (X)SDR USAA990905Frame · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK BS 726 STR 18A LT CHORD ANGLE. REMOVED AND REPLACED PER SRM 51-10-02. (X)SDR USAA990904Frame · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK BS 723 STR 18A, LT CHORD ANGLE. REMOVED AND REPLACED PER SRM 51-10-02. (X)SDR USAA990903Frame · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A ..125 INCH CRACK STATION 787 FRAME AT STRINGER 9L OVERHEAD BIN ATTACH POINT. INSTALLED DOUBLER AND REPAIR ANGLE PER EA 65193. (M)SDR USAA990902Frame · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A ..125 INCH CRACK STATION 380 BETWEEN STRINGER 8R AND 9R FRAME. INSTALLED DOUBLER PER SRM 53-30-07. (M)SDR USAA990901Splice · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STA 907 + 1/2 AT STR 4R. INSTALLED NEW STRINGER SPLICE PER SRM 51-10-00. (X)SDR USAA990900Splice · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A ..25 INCH CRACK STATION 907 PLUS 1/2 AT STRINGER 4L. INSTALLED NEW STRINGER SPLICE PER SRM 51-10-00. (M)SDR USAA990899Frame · chafedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A ..25 INCH BY 2 INCH CHAFFED AREA AT STATION 1064, BL 0 FRAME. DAMAGED BLENDED AND INSTALLED REPAIR DOUBLER PER TR 53-80-02. (M)SDR USAA990898Strap · corrodedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORROSION IN VARIOUS LOCATIONS STATION 774-855, RBL 19 STRAP. CORROSION LEVEL 1. REMOVED AND REPLACED WITH NEW STRAP PER SRM 51-10-02. (M)
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