N302WA, cancelled Jan 17, 2018
Service difficulty reports · 24
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 = 'N302WA' AND deregistration_id = 'N302WA-2018-01-17' 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 = 'N302WA' AND deregistration_id = 'N302WA-2018-01-17' 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 DL733050107Connector · damagedEMERGENCY PATH LIGHTING INOP AT 22D/E/F. FOUND ON ROUTINE MAINTENANCE INSPECTION. REPAIRED DAMAGED SIDEWALL CONNECTOR AT 22D/E/F.SDR DL733040604Odor · detectedFLIGHT ATTENDANT SMELLS BURNING ODOR IN AFT GALLEY. INSPECTED AFT GALLEY EQUIPMENT FOR DEFECTS, NONE NOTED. NO SMELL PRESENT. APPLIANCES AND LIGHTS ALL CHECK NORMAL. OK FOR SERVICE.SDR DL733040060Skin · crackedTHE FUSELAGE SKIN WAS FOUND WITH A CRACK JUST BELOW STRINGER 23R ALONG THE EDGE OF THE BONDED SKIN WAFFLE DOUBLER BETWEEN FS 727D & 727E. THE DAMAGE WAS REMOVED WITH A CUTOUT AND REPAIRED WITH 2 EXTERNAL ALUMINUM REPAIR DOUBLERS PER ER/A 386104-14, REV A.SDR DL733040007Tire · cutON L/O FOUND NR 2 MLG TIRE CUT BEYOND LIMITS. REMOVED AND REPLACED NR 2 MLG TIRE PER MM.SDR DL733030852Wire Harness · inoperativeWHILE REPOSITIONING HARNESS AT SEAT ROW 27 PINS PULLED OUT OF HARNESS AND SHORTED POWER SUPPLY. REPLACED HARNESS AT SEAT ROW 27 AND POWER SUPPLY/BATTERY PER M/M.SDR DL733020273Attach Fitting · corrodedTHE VERTICAL STABILIZER ATTACH LUGS AND THE FUSELAGE CLEVIS LUGS WERE FOUND TO BE CORRODED DURING AN INSPECTION. THE LUG BORES WERE OVERSIZED AND THE FACES SPOTFACED TO REMOVE THE CORROSION AND OVERSIZED BUSHINGS WERE INSTALLED.SDR DL733011356Safety Switch · out of adjUPON DEPARTURE ATL LDG WOULD NOT RETRACT. GEAR HANDLE WOULD ONLY RAISE TO THE OFF POSITION. ADJUSTED AND TESTED GROUND SPOILER INTERLOCK AND SAFETY SWITCHES. REF MM 27-62-51-5 AND E2-09-01-5. ALL CHECKS OK.SDR DL733010437Skin · crackedINSPECTIONS OF THE HORIZONTAL STABILIZER CUTOUT SURROUND STRUCTURE REVEALED A CRACK IN THE STRINGER 12L STRAP. ADDITIONAL TOOLING DAMAGE WAS FOUND ON THE STRINGER 12L UPPER CHORD. THE DAMAGED SECTION OF CHORD WAS REMOVED. THESTRAP WAS REPAIRED WITH A DOUSDR DL733000922Bulkhead · crackedTHE FS 178 BULKHEAD WEB WAS FOUND WITH TYPICAL FASTENER CRACKING IN THE WEB AT WL 234 AT LBL AND RBL 9. THE CRACKS ARE TYPICAL OF BAC S/B 737-53A1173. THE CRACKED AREAS OF WEB WERE TRIMMED OUT AND REPAIRED WITH ALUMINUM DOUBLERS PER B737 SRM 53-10-08, FIG 20SDR DL733000258Valve · failedHYD SYS B PRESS DROPPED TO ZERO WITH ASSOCIATED LOW PRESS LIGHTS ILLUMINATED. REPLACED B SYSTEM PRESSURE RELIEF VALVE.SDR DL733991981Control Panel · failedON DESCENT, AUTO PRESS FAIL MADE UNPRESSURIZED LANDING. REPLACED PRESS CONTROL PANEL. CKS NORMAL.SDR DL733990506Line · leakingAFTER INITIAL GEAR RETRACTION, NOSE GEAR RE-EXTENDED WITH GEAR HANDLE IN THE UP POSITION. RECYCLED GEAR HANDLE HAD NO EFFECT. NOSE GEAR REMAINED DOWN AND LOCKED. FOUND NOSE GEAR UPLOCK ACT UPPER LINE LEAKING HYD FLUID. LINE REPLACED.SDR DL733990247Skin · crackedTHE FUSELAGE SKIN AND UNDERLYING STEEL GUSSET WERE FOUND WITH A .20 INCH CRACK AT THE UPPER AFT CORNER OF THE L1 COCKPIT WINDOW CUTOUT. THE CRACK WAS ROUTED OUT AND REPAIRED WITH A STEEL DOUBLER AND ALUMINUM TRIPLER. THE REPAIR WAS ACCOMPLISHED PER ER/A 3666SDR DL733981991Wire · damagedEMERGENCY TRACK LIGHT WIRE AT SEAT ROW 25DEF FOUND DAMAGED. PERFORMED APPROVED REPAIR PER BOEING STANDARD WIRING MANUAL. SYSTEM OPERATES NORMAL.SDR DL733981006Bulkhead Web · crackedFOUR CRACKS FOUND IN THE BLKHD WEB AT FS 178. THE CRACKS ARE LOCATED AT WL 200 AND WL 188, BETWEEN LBL 5.7 AND RBL 5.7. REPAIRED PER ERA 331672-14.SDR DL733981005Bulkhead Web · corrodedAFT PRESSURE BLKHD AT FS 1016 WAS FOUND CORRODED AND CRACKED AT BL 0. REPAIRED PER ERA 331673-14.SDR DL733981004Skin · wornFUSELAGE SKIN AT THE BLADE SEAL FUSELAGE INTERFACE WAS FOUND TO HAVE AN EXISTING REPAIR (REF 5-72770-3). WEAR WAS FOUND FWD OF THE REPAIR. REPAIRED PER ERA 331664-14.SDR DL733972182Boot Seal · failedLOST ALL PRESSURIZATION AT 30000 FEET, NORMAL DUCT PRESS. NO BLEED OR PACK TRIP. FOUND RUPTURED BOOT SEAL ON APU P DOME PRESSURE DUCT. REPLACED SEAL. PRESSURIZED A/C TO 6 PSI. CKS NORMAL. NO FURTHER LEAKS FOUND.SDR DL733970233Power Supply · inoperativeWHILE PERFORMING NR 5 AD SVC CK ON SHIP 202, FOUND EMERGENCY FLOOR TRACK LIGHTING INOP FROM ROW 1 IN F/CLASS TO ROW 12 IN Y/CLASS INOP. FOUND POWER SUPPLY FOR EMERGENCY TRACK LIGHTING INOP. REPLACED PWR SUPPLY, EMERGENCY EVACUATION LIGHTS SYS OPS NML.SDR DL733961628Skin · crackedTHE SKIN AT THE COOLING DUCT CUTOUT, FS 379 BL 0, WAS FOUND CRACKED AT THE AFT EDGE OF THE CUTOUT. THE CRACK IS APPROX .5 IN LENGTH AND IS TYPICAL OF CRACKS DESCRIBED IN BACO S/B 737-53-1117 R-1. THE CRACK WILL BE STOP DRILLED AND A PERMANENT REPAIR WILL BE SDR DL733960710Ballast · smokingSIDEWALL LIGHTS ROW 23 TO 25 MOMENTARILY WENT OUT AND SMOKED. PULLED AND COLLARED C/B FOR RT SIDE, FWD TO MCO. REPLACED BALLAST AND RELAMPED, OPERATION NORMAL.SDR DL733960416Door · crackedDURING OVERHAUL, THE AFT LOWER FRAME ON THE C1 DOOR WAS DISCOVERED TO HAVE A 1.5 INCH CRACK IN THE RADIUS. IN ACCORDANCE WITH BACO S/B 737-52-1100 REV 2, THE CROSS BEAM WAS MODIFIED AND THE FRAME WAS REPLACED.SDR DL733960062Control Cable · looseGEAR DOWN 3 RED AND 3 GREEN LIGHTS. RECYCLED OK 3 GREEN, HAPPENED ON 2 APPROACHS. CORRECTED CABLE TENSION FOR LANDING GEAR ACTUATOR, GEAR SWING NORMAL.SDR DL733954382Door Frame · crackTHE AFT CARGO DOOR OPENING FORWARD FRAME WAS FOUND WITH A .5 INCH CRACK AT THE NR 5 STOP FITTING. THE FRAME IS MADE FROM A 0.071 7075-T6 CLAD MATERIAL. THIS ER/A WILL ALLOW THE USE OF THE SRM TYPICAL FORMED SECTION REPAIR.
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