N308WA, cancelled Jan 3, 2018
Service difficulty reports · 34
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
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 n_number = 'N308WA' AND deregistration_id = 'N308WA-2018-01-03' 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 n_number = 'N308WA' AND deregistration_id = 'N308WA-2018-01-03' 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 DL733060111Duct · unknownUNABLE TO MAINTAIN PRESSURIZATION WITH LT PACK AT FL 240. RT PACK CURRENTLY ON MCO. REPAIRING RT PACK. REPLACED DUCT ON RT PACK CLEARED MCO ON RT PACK A/C PRESSURIZATION CHECK NORMAL.SDR DL733060098Actuator · brokenNR 4 O/B SPOILER ACTUATOR BROKE OFF AT REAR HINGE POINT, CAUSING HINGE POINT TO BREAK AT SPOILER PANEL. REPLACED BOTH UNITS. ACTUATOR P/N 273001083.SDR DL733050524Skin · crackedCRACK FOUND IN FUSELAGE SKIN AT CHEM-MIL WHILE ACCOMP OPN 57546. CRACK REPORTED TO BE 1.5 INCH LONG, LOCATED AT FS 727E, S-24L. REPAIRED PER SRM 53-00-01, FIGURE 201. RELATED TO AD 2004-18-06, S/B 737-53A1210, & S/B 737-53-1065.SDR DL733050523Skin · crackedCRACK WAS FOUND IN THE FUSELAGE SKIN WHILE DOING OPN 57546 INSPECTIONS. REPAIRED PER SRM 53-00-01, FIGURE 201. REF AD 2004-18-06 / S/B 737-53A1210 / 737-53-1065.SDR DL733050323Outflow Valve · unserviceableAIRCRAFT WOULD NOT PRESSURIZE. FOUND AUTO FLOW CONTROL VALVE NOT CLOSING PER CABIN PRESS LEAK TEST 05-51-91-702. REPLACED VALVE PER MM 21-58-31. OP CK OK. AIRCRAFT PRESSURIZED ON GROUND PER MM.SDR DL733040746Skin · crackedA SKIN CRACK WAS FOUND ALONG THE THE MILL LINE OF THE UNDERLYING BONDED DOUBLER JUST AFT OF FS 727D AND BELOW STRINGER 23L. THE CRACK WAS REMOVED WITH A 1.5 X 2.5 INCH CUTOUT. THE CUTOUT WAS REPAIRED WITH 2 EXTERNAL ALUMINUM REPAIR DOUBLERS PER ER/A 092528-1SDR DL733030353Power Supply · inoperativeAFT CABIN EMERGENCY LIGHT INOPERATIVE, RELAMPED NO HELP R & R POWER SUPPLY LIGHT OPS NORMAL.SDR DL733030199Smoke Detector · malfunctionedRT AFT LAV SMOKE DETECTOR LIGHT AND CHIME CAME ON AND OFF IN FLT. REPLACED SMOKE DETECTOR UNITSDR DL733030147Fitting · corrodedCORROSION WAS FOUND IN THE BORES OF BOTH THE LT AND RT PRIMARY FORWARD CLEVIS LUGS. THE LHS PRIMARY FORWARD CLEVIS LUG WAS OVERSIZED TO A DIAMETER OF 1.440 INCH TO REMOVE THE CORROSION. THE RHS PRIMARY FORWARD CLEVIS LUG WAS OVERSIZED TO A DIAMETER OF 1.408 SDR DL733030146Fitting · corrodedCORROSION WAS FOUND IN THE BORES OF BOTH THE REAR SPAR LT AND RT PRIMARY AND FAIL-SAFE FIN LUGS. THE BORES WERE ENLARGED TO REMOVE CORROSION. ALSO, THE FORWARD FACE OF THE LHS PRIMARY FIN LUG WAS SPOTFACED TO REMOVE CORROSION. REPAIR BUSHINGS WERE INSTALLEDSDR DL733011754Sensor · dirtyCLIMBING THRU 4000 FT FWD CARGO LIGHT ILLUMINATED. RETURNED FOR LANDING. MAINTENANCE CONFIRMED DOOR CLOSED AND LOCKED. CLEANED FWD SENSOR OF FOREIGN SUBSTANCE, OP CHECKS GOOD.SDR DL733011450Skin · gougedFUSELAGE / SKIN / FS 907-1156 / STRG. 25L-25R : TAIL STRIKE REPAIR THE FUSELAGE SKIN SUFFERED A TAIL STRIKE ON TAKEOFF WHICH RESULTED IN MULTIPLE GOUGES, SCRAPES, AND HOLES IN THE FUSELAGE SKIN FROM FSDR DL733010136Bulkhead · crackedWHILE ACCOMPLISHING INSPECTIONS OF THE FS 178 BULKHEAD WEB A CRACK WAS FOUND AT RBL 5.7 AND WL 211. THE CRACK WAS LOCATED ABOVE AND EXISTING DOUBLER REPAIR FOR CRACKS BELOW WL 205. THE NEW CRACK WAS REMOVED WITH A 1 INCH CUTOUT AND THE EXISTING REPAIR DOUBLESDR DL733010095Frame · crackedTHE FS 178 BULKHEAD LT SIDE CHORD WAS FOUND WITH A .5 INCH VERTICAL CRACK IN THE RADIUS OF THE CHORD. A NEW SECTION OF SIDE CHORD WAS SPLICED IN PER THE REQUIREMENTS OF BAC S/B 737-53A1173 AND DOCUMENTED PER ER/A 379791-14AD.SDR DL733992265Actuator · crackedAFTER LANDING, LOST HYD SYS A GROUND PERSONNEL REPORTED LEAK RT WING AREA. FOUND NR 8 GROUND SPOILER ACT LEAKING, REPLACED SAME. .SDR DL733981852Engine · failedAT 1500 FT NR 1 ENGINE LOUD BANG AND OVERTEMP TO 930 CELSIUS. FOLLOWED BY VIBRATION WITH THROTTLE REDUCED IDLE INDICATIONS NORM FOR 4-5 MIN THEN VIBRATION IND WENT TO 3. A/C STARTED TO SHAKE. ENG SHUT DOWN. PAX REPORTED FLAMES AT TIME OF COMPRESSOR STALL TSDR DL733981773Line · rupturedLOST A-SYS HYD PRESS AND QTY JUST AFTER RAISING GEAR ON T/O. FOUND RT GEAR UP LINE TO ACT RUPTURED. REPLACED LINE, BOTH A-SYS CASE DRAIN CHECK OK. LEAK CHECKED PUMPS, CHECK OK.SDR DL733970554Battery · dischargedFWD EMERGENCY FLASHLIGHT INOPERATIVE. REPLACED BATTERY AND BULB, OPS OK.SDR DL733950388Skin · dentedDURING HMV SHOP INSPECTION, RIGHT WING NR 3 FORE FLAP WAS FOUND WITH DENTED SKIN, LOWER LEADING EDGE JUST OUTBOARD OF INBOARD ATTACH POINT. REPAIRED PER SRM 57-53-01 FIG 201.SDR DL733950213Skin · puncturedDURING HMV, FOUNG SMALL PUNCTURE AND FIBER DAMAGE IN LEFT ELEVATOR UPPER SURFACE. LOCATED 3 FEET FROM INBOARD AND 7 INCHES FROM SPAR AFT. REPAIRED ELEVATOR PUNCTURE PER SRM 55-20-01 IN REF TO 51-70-17.SDR DL733950160Attach Fitting · crackedDURING ROUTINE INSPECTION AT HMV, THE RT WING O/B AFT SUPPORT FITTING FOR THE MAIN LANDING GEAR BEAM WAS FOUND CRACKED. THE CRACKED FITTING WILL REMAIN IN SERVICE PER S/B 737-57-1216 AND WILL BE REPAIRED PER S/B REQUIREMENTS.SDR DL733950119Seat Track · corrosionAT HMV, CORROSION WAS FOUND ON SEAT TRACK HORIZONTAL FLANGE AT STA 344 LBL 20. REMOVED OLD SECTION, FABRICATED NEW SEAT TRACK AND INSTALLED SEAT TRACK PER SRM53-00-52.SDR DL733950069Floor Beam · corrodedDURING HMV, CORROSION WAS FOUND ON A FLOOR BEAM AT FS 328 AROUND FASTENER HOLES FROM LEFT TO RIGHT SIDE OF THE FUSELAGE. REPAIRS INVOLVED TREAT AND PAINT LBL49 PER PS 900-2 NR 5 AND REPAIR LBL 36 AND RT OUTBOARD END PER SRM 53-00-51 FIG 205.SDR DL733950212Le Slat · crackedAT HMV, FOUND NR 5 LEADING EDGE SLAT CRACKED ON BOTTOM ALONG FASTENERS. REPAIRED PER SRM 57-43-01 FIG 205.SDR DL733950118Floor Beam · corrosionAT HMV, CORROSION WAS FOUND ON FLOOR BEAM CAPS SECTIONS AT STA 960 TO 975 RBL 30-40. REPAIRED PER SRM 53-00-51.SDR DL733950101Floor Support · corrodedAT HMV, FOUND FLOOR SUPPORT CORRODED AT STA 960 LBL 10-30. REMOVED OLD, FABRICATED AND INSTALLED NEW SUPPORT PER SRM 51-00-00.SDR DL733950097Seat Track · corrosionAT HMV, CORROSION WAS FOUND ON SEAT TRACK UPPER SURFACES AT STA 960 ON THE OUTBOARD SIDE. REPAIRED PER SRM 53-00-52 FIG 204.SDR DL733950068Floor Beam · corrodedDURING HMV, CORROSION WAS FOUND ON FLOOR BEAM AT STA 986.5 AROUND FASTENER HOLES ON TOP FLANGE. REPAIRED PER SRM 53-00-51 PG 220.SDR DL733950076Floor Track · corrosionAT HMV, CORROSION WAS FOUND ON GALLEY FLOOR TRACK AT FLOOR BEAM 328 RT SIDE ON THE FWD END OF INBOARD TRACK. REPAIRED PER SRM 53-00-52 PG 202-205.SDR DL733950075Floor Track · corrosionAT HMV, CORROSION WAS FOUND ON GALLEY FLOOR TRACK AT FLOOR BEAM STA 328 ON OUTBOARD TRACK RIGHT HAND SIDE AT FWD END. REPLACED SEAT TRACK PER SRM 51-00-00.SDR DL733950074Floor Track · corrosionAT HMV, CORROSION WAS FOUND ON GALLEY FLOOR TRACK AT FLOOR BEAM 328 ON RT SIDE AT CENTER FWD END. REPAIRED PER SRM 53-00-52 PG 202-205.SDR DL733950073Seat Track · corrodedAT HMV, FOUND CORROSION ON LEFT OUTBOARD SEAT TRACK AT FS 344. REPAIRED PER SRM 53-00-52 PG 202-205.SDR DL733950072Floor Beam · corrosionAT HMV, CORROSION WAS FOUND ON FLOOR BEAM 'T' CAP SURFACE AT STA 294 BL0 TO OUTBOARD RBL AROUND FASTENER HOLES. REPAIRED PER ERA 300920-14.SDR DL733950071Floor Beam · corrodedDURING HMV, CORROSION WAS FOUND AT FS 312 FLOOR BEAM FASTENER HOLES AT LBL 6, CENTERLINE AND RBL 8. REPAIRED PER SRM 53-10-51 FIG 205.
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