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 USAA980503Clip · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 616 STRINGER 1R TIE CLIP. INSTALLED MODIFIED PART PER EO 5393G227 AD 93-08-04 SB 737-53-1085 R1. (M)SDR USAA980502Clip · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 807 STRINGER 9R TIE CLIP. INSTALLED MODIFIED PART PER EO 5393G227 AD 93-08-04 SB 737-53-1085 R1. (M)SDR USAASB98273Switch · failedPIT - MAINTENANCE FOUND ALL EMERGENCY LIGHTS INOP THROUGHOUT THE AIRCRAFT. MAINTENANCE FOUND THE EMERGENCY LIGHT SWITCH IN THE COCKPIT BAD. REMOVED AND REPLACED SWITCH. OPERATIONAL CHECK GOOD. (M)SDR USAA980523Skin · crackedPIT - FOUND RON, FOUND 3 INCH CRACK IN SKIN AT STATION 767 .5 INCH ABOVE STRINGER NR 20. INSTALLED DOUBLER PER SRM 53-30-03. (M)SDR USAASB98271Battery Pack · dischargedBWI - MAINTENANCE FOUND THE AFT OVERHEAD CEILING EMERGENCY EXIT LIGHT INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M)SDR USAA980495Skin · gougedLCQ - DURING PAINT VISUAL INSPECTION, FOUND A 2 INCH GOUGE STATION 388 BETWEEN STRINGER 19L AND 20L EXTERIOR SKIN. INSTALLED DOUBLER PER SRM 53-30-03 FIG 1. (M)SDR USAASB98261Switch · failedALB - MAINTENANCE FOUND THE EMERGENCY LIGHTS TESTING INTERMITTENTLY. MAINTENANCE REMOVED AND REPLACED THE S7 EMERGENCY LIGHT SWITCH AT THE P5 PANEL. OPERATIONAL CHECK GOOD PER MM 33-51-11. (M)SDR USAASB98258Supply Duct · failedLGA - FLT 1599 - FOR TAKEOFF, FLIGHT WAS CONFIGURED FOR A BLEEDS OFF TAKEOFF. WHEN CREW RECONFIGURED, A LOUD BANG WAS HEARD. AFTER A MINUTE OR TWO, THE FLIGHT ATTENDANTS REPORTED SMOKE IN THE CABIN. AN EMERGENCY WAS DECLARED. FLIGHT RETURNED TO FIELD AT LGSDR 98ZZZM890Pack Control Vlv · failedLGA - FLT 1599 - FOR TAKEOFF, FLIGHT WAS CONFIGURED FOR A BLEEDS OFF TAKEOFF. WHEN CREW RECONFIGURED, A LOUD BANG WAS HEARD. AFTER A MINUTE OR TWO, THE FLIGHT ATTENDANTS REPORTED SMOKE IN THE CABIN. AN EMERGENCY WAS DECLARED. FLIGHT RETURNED TO FIELD AT LGSDR 98ZZZM889Press Regulator · failedLGA - FLT 1599 - FOR TAKEOFF, FLIGHT WAS CONFIGURED FOR A BLEEDS OFF TAKEOFF. WHEN CREW RECONFIGURED, A LOUD BANG WAS HEARD. AFTER A MINUTE OR TWO, THE FLIGHT ATTENDANTS REPORTED SMOKE IN THE CABIN. AN EMERGENCY WAS DECLARED. FLIGHT RETURNED TO FIELD AT LGSDR 98ZZZM888Mix Chamber Duct · failedLGA - FLT 1599 - FOR TAKEOFF, FLIGHT WAS CONFIGURED FOR A BLEEDS OFF TAKEOFF. WHEN CREW RECONFIGURED, A LOUD BANG WAS HEARD. AFTER A MINUTE OR TWO, THE FLIGHT ATTENDANTS REPORTED SMOKE IN THE CABIN. AN EMERGENCY WAS DECLARED. FLIGHT RETURNED TO FIELD AT LGSDR USAA980468Angle · corrodedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION AT LWR THRESHOLD SUPPORT ZEE AREA FWD SERVICE DOOR STATION 300 TO 340 ZEE ANGLE. REPLACED WITH IDENTICAL PART PER SRM 51-10-1. (M)SDR USAA980467Frame · crackedCLT - DURING Q-1 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND A CRACK OUTBOARD FRAME CHORD BS 727 STRINGER 15L. INSTALLED DOUBLERS, FILLERS AND STRAPS PER EA 62502. (M)SDR USAA980466Angle · corrodedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND .5 INCH BY 6 INCH AREA OF CORROSION LBL 54 STATION 887 TO STATION 1016. CORROSION TASK NR C53-107-02. REPLACED WITH IDENTICAL PART PER SRM 53-10-01. (M)SDR USAA980464Floorbeam · corrodedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .5 INCH BY .5 INCH BY 24 INCH AREA OF CORROSION CLIP NUT HOLES BS 1016 BETWEEN LBL 12 AND LBL 36 FLOORBEAM UPPER CHORD. CORROSION TASK NR C53-107-02. INSTALLED DOUBLER PER SRM 53-10-9. (M)SDR USAA980463Clip · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 767 STRINGER 7R STRINGER TIE CLIP. REPAIRED PER EO 5393G227 REV 'A'. (M)SDR USAA980462Clip · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 727A STRINGER 6R STRINGER TIE CLIP. REPAIRED PER EO 5393G227 REV 'A'. (M)SDR USAA980461Clip · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 747 STRINGER 7R STRINGER TIE CLIP. REPAIRED PER EO 5393G227 REV 'A'. (M)SDR USAA980460Floorbeam · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 3 INCH CRACK BS 663 BBL .07 UPPER CHORD LONGITUDINAL FLOORBEAM. INSTALLED SPLICE ANGLES, STRAPS AND REINFORCED ANGLES PER EA 62511 AND BOEING S/B737-57-1210. (M)SDR USAA980459Web · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 2.5 INCH CRACK BS 230.5 WL 187 BL 0 RETRACT ACT FITTING SUPPORT WEB NLG. INSTALLED DOUBLER PER SRM 51-40-2 FIG 1, BOEING 737-200. (M)SDR USAA980458Floorbeam · corrodedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION AROUND SEVERAL SCREW HOLES ON FLOORBEAM STATION 947.5. CORROSION TASK NR C53-107-02. INSTALLED NEW T-CAP TO FLOORBEAM PER SRM 53-10-9. (M)SDR USAA980457Clip · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 639 STRINGER 4L STRINGER TIE CLIP. REPAIRED PER EO 5393G227 REV 'A'. (M)SDR USAA980456Floorbeam · crackedCLT - DURING Q-4 CHECK HFEC INSPECTION, FOUND A 1.5 INCH CRACK BS 520 WL 208 LBL 24 FLOORBEAM. INSTALLED REPAIR ANGLE PER EA 62449 SB 737-53-1120 REV 1 PART VI. (M)SDR USAA980455Floorbeam · crackedCLT - DURING Q-4 CHECK HFEC INSPECTION, FOUND A 1.5 INCH CRACK BS 520 WL 208 RBL 24 FLOORBEAM. INSTALLED REPAIR ANGLES PER EA 62449 SB 737-53-1120 REV 1. (M)SDR USAA980454Floorbeam · crackedCLT - DURING Q-1 CHECK HFEC INSPECTION, FOUND .25 INCH CRACK BS 520 RBL 45 FLOORBEAM 'T' CAP RADIUS. INSTALLED REPAIR ANGLES PER EA 62449 BOEING SB 737-53-1120 REV 1. (M)SDR USAA980453Floorbeam · corrodedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION AROUND CLIP NUT HOLES STATION 344 FLOORBEAM BL 0 TO LBBL 42. REPAIRED 'T' CAP SPLICED DOUBLER PER SRM 53-10-13. (M)SDR USAA980452Clip · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 807 STRINGER 10R STRINGER TIE CLIP. REPAIRED PER EO 5393G227 REV 'A'. (M)SDR USAA980451Clip · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 727B STRINGER 8R STRINGER TIE CLIP. REPAIRED PER EO 5393G227 REV 'A'. (M)SDR USAA980450Clip · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 727B STRINGER 7R STRINGER TIE CLIP. REPAIRED PER EO 5393G227 REV 'A'. (M)SDR USAA980449Clip · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 727A STRINGER 2R STRINGER TIE CLIP. REPAIRED PER EO 5393G227 REV 'A'. (M)SDR USAA980448Clip · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 727A STRINGER 2R, STRINGER TIE CLIP. REPAIRED PER EO 5393G227 REV 'A'. (M)SDR USAA980447Clip · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 747 STRINGER 7L STRINGER TIE CLIP. REPAIRED PER EO 5939G227 REV 'A'. (M)SDR USAA980446Clip · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 706 STRINGER 9L. REPAIRED PER EO 5393G227 REV 'A'. (M)SDR USAA980445Clip · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK STATION 500B STRINGER 10L STRINGER TIE CLIP. REPAIRED PER SRM 51-10-1 AND EO 5393G227 REV 'A'. (M)SDR USAA980444Clip · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STRINGER TIE CLIP STATION 616 S 1. REPAIRED PER EO 5393G227 REV 'A'. (M)SDR USAA980439Angle · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 2 INCH CRACK IN RADIUS SUPPORT BRACKET FOR NLG AT BEAM VERT FLANGE STATION 259 WL 192 ANGLE. REPLACED WITH IDENTICAL PART PER SRM 51-10-1. (M)SDR USAA980438Skin · crackedCLT - DURING Q-1 CHECK EDDY CURRENT INSPECTION, FOUND A .25 INCH CRACK LOWER FORWARD CORNER LEFT AFT ENTRY DOOR CUTOUT STATION 962 WL 208 SKIN. INSTALLED TRIPLER PER SRM 53-30-03 FIG 24. (M)SDR USAA980437Skin · dentedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 4 INCH LONG .875 INCH WIDE AND .09375 INCH DEEP DENT BETWEEN STATION 987.5 AND STATION 1006 STRINGER 17L SKIN. FABRICATED DOUBLER PER SRM 53-30-3 FIG 61. (M)SDR USA980469Floorbeam · corrodedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 1 INCH AT CLIP NUTS STATION 344 FLOORBEAM BL 0 LBL 42. CORROSION TASK NR C53-107-01. FABRICATED REPAIR PER TR 53-10-13 'T' CAP. (M)SDR USAASB98251Duct · leakingBWI - FLT 2679 - ON CLIMB-OUT PASSING 13,000 FEET, THE NR 1 ENGINE OVERHEAT LIGHT ILLUMINATED. CREW ACCOMPLISHED CHECK LIST AND WHEN THRUST LEVER WAS PULLED BACK ON NR 1 ENGINE, LIGHT EXTINGUISHED. CREW DECIDED TO RETURN TO FIELD AT BWI. FLIGHT LANDED WITHOSDR USAASB98249Switch · failedCLT - FLT 273 - AFTER TAKEOFF FROM PHL, CREW RECEIVED A RT MAIN GEAR GREEN LIGHT WHICH WOULD NOT EXTINGUISH AFTER RECYCLING THE GEAR. CREW DECIDED TO DIVERT TO CLT WHERE THE FLIGHT LANDED WITHOUT INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND SDR USAASB98246Light · inoperativeBWI - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT OVER THE MAIN ENTRY DOOR INOP. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT ASSY. OPERATIONAL CHECK GOOD. (M)SDR USAASB98243Valve · failedTPA - FLT 2636 - AFTER TAKEOFF AT 2,000 FEET AND CLIMBING, THE NR 1 ENGINE START VALVE OPEN LIGHT ILLUMINATED. CREW PERFORMED CHECK LIST PROCEDURES AND LIGHT REMAINED ON. CREW SHUT DOWN THE NR 1 ENGINE AT 5,000 FEET, DECLARED AN EMERGENCY AND RETURNED TO FIESDR USAA980408Skin · crackedTPA - DURING CX-2 CHECK VISUAL AND VERIFIED BY EDDY CURRENT INSPECTION, FOUND A .8750 INCH CRACK STA 947 BETWEEN STR 15R AND STR 16R SKIN. INSTALLED DOUBLER PER SRM 53-30-3. (X)SDR USAA980407Skin · crackedTPA - DURING CX-2 CHECK VISUAL VERIFIED BY EDDY CURRENT INSPECTION, FOUND A .75 INCH CRACK STA 312 BETWEEN STR 14L AND STR 13L SKIN. INSTALLED DOUBLER PER SRM 53-30-3. (X)SDR USAASB98214Battery Pack · dischargedCMH - PILOT REPORTED THE LEFT AFT SERVICE DOOR EMERGENCY EXIT LIGHT FLICKERS. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M)SDR USAASB98213Water Separator · contaminatedCLT - FLT 1806 - EN ROUTE FROM BNA TO PHL, 60 MILES SOUTHWEST OF CRW, F/A TOLD CAPTAIN THAT A STRONG ELECTRICAL SMELL WAS NOTED IN THE CABIN AROUND SEAT ROW 4A. CAPT DECIDED TO DIVERT TO CLT AND DECLARE AN EMERGENCY. CAPTAIN DID NOT DIVERT TO CRW OR ROA DUE SDR USAASB98205Oil Filter · failedTPA - FLT 8026 - CLIMBING THROUGH FL270, THE NR 1 ENGINE OIL TEMP STARTED RISING INTO THE YELLOW BAND. OIL PRESS WAS AT TOP OF THE GREEN BAND BUT NOT OUT OF LIMITS. OIL TEMP CONTINUED TO CLIMB AND AT FL290 HAD RISEN INTO THE RED BAND. THE NR 1 ENGINE WAS PUSDR USAA980343Skin · crackedTPA - DURING A CX-3 CHECK EDDY CURRENT, FOUND A .300 INCH CRACK AFT SERV DOOR LOWER HINGE CUTOUT OUTER SKIN STATION 951, STRINGER 14R. INSTALLED FILLER .050 2024 T-3, ALSO DOUBLER .063 2024 T-3 AND TRIPLER .063 301.5 HARD S/S PER SRM 53-30-3 PAGE 121. (M)SDR USAA980339Skin · crackedTPA - DURING CX-5 CHECK EDDY CURRENT, FOUND A .125 INCH CRACK IN OUTER SKIN AT LOWER CORNER OF AFT ENTRY DOOR, LOWER HINGE CUTOUT STATION 950.5 2.5 INCHES BELOW STRINGER 14L. ROUTED OUT CRACK AND REFINISHED AREA PER SRM 53-00-1 PAGE 102. (M)
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