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.

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.Feb 9, 2006 · N308WA · Boeing 737347 · Air Distribution SystemSDR 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.Feb 2, 2006 · N308WA · Boeing 737347 · Drag Control ActuatorSDR 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.Sep 6, 2005 · N308WA · Boeing 737347 · Fuselage Main, Plate/SkinSDR 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.Sep 6, 2005 · N308WA · Boeing 737347 · Fuselage Main, Plate/SkinSDR 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.Jun 13, 2005 · N308WA · Boeing 737347 · Pressure Regulator/Outflow ValveSDR 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 092528-1Aug 7, 2004 · N308WA · Boeing 737347 · Fuselage Main, Plate/SkinSDR DL733030353Power Supply · inoperativeAFT CABIN EMERGENCY LIGHT INOPERATIVE, RELAMPED NO HELP R & R POWER SUPPLY LIGHT OPS NORMAL.Apr 11, 2003 · N308WA · Boeing 737347 · Emergency LightingSDR DL733030199Smoke Detector · malfunctionedRT AFT LAV SMOKE DETECTOR LIGHT AND CHIME CAME ON AND OFF IN FLT. REPLACED SMOKE DETECTOR UNITFeb 26, 2003 · N308WA · Boeing 737347 · Smoke DetectionSDR 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 Feb 12, 2003 · N308WA · Boeing 737347 · Fuselage, Stabilizer Attach FittingsSDR 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 INSTALLEDFeb 12, 2003 · N308WA · Boeing 737347 · Vertical Stabilizer, Attach FittingsSDR 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.Nov 3, 2001 · N308WA · Boeing 737347 · Door Warning SystemSDR 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 FAug 31, 2001 · N308WA · Boeing 737347 · Fuselage Main, Plate/SkinSDR 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 DOUBLEJan 24, 2001 · N308WA · Boeing 737347 · Fuselage Main, BulkheadSDR 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.Jan 18, 2001 · N308WA · Boeing 737347 · Fuselage Main, FrameSDR DL733992265Actuator · crackedAFTER LANDING, LOST HYD SYS A GROUND PERSONNEL REPORTED LEAK RT WING AREA. FOUND NR 8 GROUND SPOILER ACT LEAKING, REPLACED SAME. .Oct 11, 1999 · N308WA · Boeing 737347 · Drag Control ActuatorSDR 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 TSep 7, 1998 · N308WA · Boeing 737347 · Engine (Turbine/Turboprop)SDR 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.Aug 27, 1998 · N308WA · Boeing 737347 · Landing Gear Retraction/Extension SystemSDR DL733970554Battery · dischargedFWD EMERGENCY FLASHLIGHT INOPERATIVE. REPLACED BATTERY AND BULB, OPS OK.Mar 25, 1997 · N308WA · Boeing 737347 · Emergency LightingSDR 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.Jan 12, 1995 · N308WA · Boeing 737347 · Trailing Edge FlapsSDR 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.Jan 10, 1995 · N308WA · Boeing 737347 · Elevator, Plate/SkinSDR 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.Jan 10, 1995 · N308WA · Boeing 737347 · Wing, Landing Gear Attach FittingsSDR 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.Jan 8, 1995 · N308WA · Boeing 737347 · Fuselage, Seat/Cargo Attach FittingsSDR 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.Jan 5, 1995 · N308WA · Boeing 737347 · Fuselage Main, Floor BeamSDR DL733950212Le Slat · crackedAT HMV, FOUND NR 5 LEADING EDGE SLAT CRACKED ON BOTTOM ALONG FASTENERS. REPAIRED PER SRM 57-43-01 FIG 205.Jan 4, 1995 · N308WA · Boeing 737347 · Leading Edge DevicesSDR 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.Jan 4, 1995 · N308WA · Boeing 737347 · Fuselage Main, Floor BeamSDR 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.Jan 4, 1995 · N308WA · Boeing 737347 · Fuselage Miscellaneous StructureSDR 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.Jan 4, 1995 · N308WA · Boeing 737347 · Fuselage, Seat/Cargo Attach FittingsSDR 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.Jan 4, 1995 · N308WA · Boeing 737347 · Fuselage Main, Floor BeamSDR 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.Jan 3, 1995 · N308WA · Boeing 737347 · Fuselage, Seat/Cargo Attach FittingsSDR 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.Jan 3, 1995 · N308WA · Boeing 737347 · Fuselage, Seat/Cargo Attach FittingsSDR 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.Jan 3, 1995 · N308WA · Boeing 737347 · Fuselage, Seat/Cargo Attach FittingsSDR DL733950073Seat Track · corrodedAT HMV, FOUND CORROSION ON LEFT OUTBOARD SEAT TRACK AT FS 344. REPAIRED PER SRM 53-00-52 PG 202-205.Jan 3, 1995 · N308WA · Boeing 737347 · Fuselage, Seat/Cargo Attach FittingsSDR 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.Jan 3, 1995 · N308WA · Boeing 737347 · Fuselage Main, Floor BeamSDR 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.Jan 3, 1995 · N308WA · Boeing 737347 · Fuselage Main, Floor Beam
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