N118RW, cancelled May 11, 2004
Service difficulty reports · 103
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 = 'N118RW' AND deregistration_id = 'N118RW-2004-05-11' 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 = 'N118RW' AND deregistration_id = 'N118RW-2004-05-11' 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 FL3A200200389Check Valve · inoperativeDURING CLIMB OUT, THE FLIGHT CREW NOTED AN ILLUMINATED WING/BODY OVERHEAT LIGHT WHICH WOULD NOT EXTINGUISH WHEN QUICK REFERENCE HANDBOOK ITEMS WERE ACCOMPLISHED. THE AIRCRAFT RETURNED TO THE DEPARTURE AIRPORT.MAINTENANCE REMOVED AND REPLACED THE START MANIFOLSDR F3LA200200385Hydraulic Line · damagedDURING FLIGHT, A SYSTEM HYDRAULIC QUANTITY DROPPED TO ZERO FOLLOWED BY THE FAILURE OF THE NUMBER 2 ENGINE, ENGINE DRIVEN HYDRAULIC PUMP. A SYSTEM PRESSURE REMIAINED NORMAL. ON FINAL APPROACH TO DIVERSION SITY AIRPORT, A SYSTEM PRESSURE DROPPED TO ZERO. STANSDR F3LA200200265A/C Pack · malfunctionedAIR TURN BACK. FLIGHT CREW REPORTED SMOKE IN CABIN, LT WING/BODY OVERHEAT ILLUMINATED AND RT PACK TRIPPED OFF. DECLARED AN EMERGENCY AND RETURNED TO DEN. AIRCRAFT LANDED WITHOUT INCIDENT. ON APPROACH, AILERONS WERE DIFFICULT TO MOVE AND HAD A SHUDDER BELOWSDR F3LA200200258Odor · detectedAIR TURNBACK. FLIGHT CREW REPORTED FWD LAVATORY SMOKE ALARM ACTIVATED WHILE CLIMBING THROUGH 8000 FT. PASSENGERS IN ROW 2 NOTED DISTINCT SMELL/ODOR OR SMOKE (OVEN/ELECTRICAL) DURING FLIGHT. NR 2 PACK TRIP OFF LIGHT ILLUMINATED IMMEDIATELY BEFORE SMOKE ALARMSDR F3LA200200201Overheat Loop · out of positionDURING CLIMBOUT, THE FLIGHT CREW DISCOVERED A WIND/BODY OVERHEAT LIGHT ON. QRH ITEMS ACCOMPLISHED AND LIGHT EXTINGUISHED. AIR TURNBACK ACCOMPLISHED. UPON INSPECTION BY MAINTENANCE, AFT CARGO PIT HAD TWO AREAS WHERE THE OVERHEAT DETECTOR WAS TOUCHING THE BLESDR F3LA200200152Fire Detector · false activationUPON ARRIVAL AT GATE, FLIGHT CREW REPORTED THE FIRE BELL SOUNDED AND THE NR 1 ENGINE FIRE HANDLE WAS ILLUMINATED. PULLED NR 1 FIRE HANDLE AND DISCHARGED THE LEFT BOTTLE INTO THE NR 1 ENGINE. INSPECTED NR 1 ENGINE FOR EVIDENCE OF FIRE, NONE FOUND. INSPECTED SDR F3LA200200103Cowling · crackedDURING C-3 CHECK, INSPECTION REPORTED CRACK ON AFT LOWER CORNER OF NR 2 ENGINE OUTBOARD FIXED COWL NEXT TO FIRE SEAL. FABRICATED AND INSTALLED REPAIR PER SRM 51-40-3 AND 51-30-2.SDR F3LA200200102Web · corrodedDURING C-3 CHECK, INSPECTION REPORTED AFT LAVATORY FLOOR WEB CORRODED, STA 1016, AT DRAIN TO LBL 30.SDR F3LA200200101Attach Angle · corrodedDURING C-3 CHECK, INSPECTION REPORTED CORROSION ON SIDEWALL PANEL ATTACH ANGLE AT STA 727, LBL 21 TO LBL 25.SDR F3LA200200100Attach Angle · corrodedDURING C-3 CHECK, INSPECTION REPORTED CORROSION ON SIDEWALL ATTACH ANGLE AT STA 947.5, STR 21R TO 24R. FABRICATED AND INSTALLED REPLACEMENT ANGLE PER BOEING DRAWING 65-55726 AND SRM 51-40-3.SDR F3LA200200098Clip · corrodedDURING C-3 CHECK, INSPECTION REPORTED CORROSION ON CLIP AT FWD FRAME, STA 360. FABRICATED AND INSTALLED CHANNEL TIE PER SRM 51-20-01 AND 51-30-2.SDR F3LA200200097Web · corrodedDURING C-3 CHECK, INSPECTION REPORTED VERTICAL WEB CORRODED FROM STA 352 TO STA 360. FABRICATED AND INSTALLED REPLACEMENT WEB PER SRM 51-20-01 AND 51-30-2.SDR F3LA200200096Stiffener · crackedDURING C-3 CHECK, INSPECTION REPORTED STIFFENER ANGLE CRACKED AT STA 298 - STA 304. FABRICATED AND INSTALLED REPLACEMENT CLIP PER SRM 51-10-2 AND 51-30-2.SDR F3LA200200095Threshold · crackedDURING C-3 CHECK, INSPECTION REPORTED CRACK IN RADIUS UPPER SURFACE 28 INCHES FWD OF AFT EDGE OF WEB THRESHOLD C-2 DOOR AT STR 25-R, STA 794-847. REMOVED DAMAGED AREA AND INSTALLED DOUBLER AND FILLER ON WEB PER SRM 51-40-3.SDR F3LA200200094Panel · corrodedDURING C-3 CHECK, INSPECTION REPORTED CORROSION AT SCREW HOLES ON TRANSITION PANEL AT STA 500-520. FABRICATED AND INSTALLED REPLACEMENT TRANSITION PANEL PER SRM 51-21-41.SDR F3LA200200093Web · corrodedDURING C-3 CHECK, INSPECTION REPORTED CORROSION ON WEB AT STA 797 BETWEEN STR 22-R AND 24-R. REPLACED WEB PER SRM 51-30-2 AND 51-10-1.SDR F3LA200200092Skin · crackedDURING C-3 CHECK, INSPECTION REPORTED L2 DOOR CUTOUT CRACKED AT FWD LOWER CORNER OUTER SKIN APPROXIMATELY 1 INCH FROM RIVET TO DOOR CORNER. REPAIRED DAMAGE PER SRM 53-30-3.SDR F3LA200200091Skin Panel · damagedDURING C-3 CHECK, INSPECTION REPORTED MISSED DRILLED RIVET HOLE IN FWD LT. CORNER OF AFT E&E DOOR CUTOUT AT STA. 326. FABRICATED DOUBLER, TRIPLER AND FILLER PER EA 57-737-157. TREATED AND PRIMED REPAIR PARTS PER SOPM 20-41-02. INSTALLED FASTENERS PER 51-30-SDR F3LA200200090Cowling · damagedDURING C-3 CHECK, INSPECTION REPORTED NR 1 ENGINE LT OUTBOARD COWL TOP EDGE DAMAGED BETWEEN SECOND AND LAST HINGE. REMOVED DAMAGE PER SRM 51-40-3. FABRICATED AND INSTALLED REPAIR PER SRM 51-10-2, 51-40-3 AND 51-30-2.SDR F3LA200200089Mount Bracket · corrodedDURING C-3 CHECK, INSPECTION REPORTED LT WING REAR SPAR MOUNT TEE FOR NR 4 SPOILER OUTBOARD ACTUATOR MOUNT BRACKET CORRODED. REPLACED BRACKET AND BUSHING PER SRM 51-30-5, BOEING OHM 20-50-03 AND BOEING SOPM 20-50-01.SDR F3LA200200088Beam · corrodedDURING C-3 CHECK, INSPECTION REPORTED BEAM IN FWD BULKHEAD, AFT CARGO COMPARTMENT, CORRODED AT NUT PLATE ATTACHMENT POINT FOR LOWER DUCT SHROUD BRACKETS AT LBL 20 AND WL 160. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPLACEMENT PARTS PER SRM 51-40-4.SDR F3LA200200087Angle · corrodedDURING C-3 CHECK, INSPECTION REPORTED CORROSION ON AFT CARGO COMPARTMENT PANEL ATTACH ANGLE AT STA. 727, RBL 21 TO RBL 25. FABRICATED AND INSTALLED REPLACEMENT ANGLE PER SRM 51-30-2, 51-10-2 51-30-3 AND BOEING DRAWING 65-55726.SDR F3LA200200079Beltframe · corrodedDURING C-3 CHECK, INSPECTION REPORTED CORROSION ON BELT FRAME AT STA 827, RBL 10. REMOVED DAMAGE, FABRICATED AND INSTALLED PER SRM 53-10-4.SDR F3LA200200078Frame · crackedDURING C-3 CHECK, INSPECTION REPORTED FRAME AT STA 82.7, RBL 10, CRACKED AT SHEAR TIE ATTACH FASTENERS IN AFT CARGO COMPARTMENT. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PER SRM 53-10-4.SDR F3LA200200076Stiffener · corrodedDURING C-3 CHECK, INSPECTION REPORTED CORROSION IN NUT PLATE HOLE AT STA 727, RBL 12, VERTICAL STIFFENER. CUT OUT DAMAGED AREA, FABRICATED REPLACEMENT PARTS AND INSTALLED PER EO 51-00-737-001 AND SRM 51-40-4.SDR F3LA200200075Floorbeam · corrodedDURING C-3 CHECK, INSPECTION REPORTED FLOORBEAM AT STA 967 CORRODED. FABRICATED AND INSTALLED REPLACEMENT FLOORBEAM CAP PER SRM 51-30-2.SDR F3LA200200074Floor Panel · corrodedDURING C-3 CHECK, INSPECTION REPORTED CORROSION AROUND EDGES OF AFT FLOOR PANEL IN FWD CARGO COMPARTMENT. REMOVED CORROSION AROUND EDGES OF AFT FLOOR PANEL PER SRM 51-10-06. FABRICATED AND INSTALLED REPLACEMENT RETAINER STRAP PER SRM 51-10-01, 51-10-02 AND SSDR F3LA200200073Strap · corrodedDURING C-3 CHECK, INSPECTION REPORTED AFT LAVATORY FLOOR WEB STRAP CORRODED AT STA 1006 TO STA 1016. FABRICATED AND INSTALLED REPLACEMENT WEB STRAP PER SRM 51-30-2.SDR F3LA200200071Floor Support · corrodedDURING C-3 CHECK, INSPECTION REPORTED FLOOR SUPPORT AT STA 957, LBL 16 TO LBL 42, CORRODED. FABRICATED AND INSTALLED REPLACEMENT FLOOR SUPPORT PER SRM 53-10-2 AND 51-30-2.SDR F3LA200200072Frame · corrodedDURING C-3 CHECK, INSPECTION REPORTED CORROSION ON CHORD AT STA 352, STR 28L. REPLACED DAMAGED CHORD PER SRM 51-10-2 AND SRM 51-30-2.SDR F3LA200200070Panel · corrodedDURING C-3 CHECK, INSPECTION REPORTED CORROSION ON CLOSING PANEL AROUND NUT PLATES AT STA 789, RBL 39 TO RBL 46. REPLACED CLOSING PANEL PER SRM 51-10-1.SDR F3LA200200069Panel · corrodedDURING C-3 CHECK, INSPECTION REPORTED CORROSION ON CLOSING PANEL AROUND NUT PLATE AT STA 789, RBL 27 TO RBL 34. REPLACED CLOSING PANEL PER SRM 51-10-1.SDR F3LA200200068Floorbeam · corrodedDURING C-3 CHECK, INSPECTION REPORTED TOP SURFACE OF FLOORBEAM AT STA 986 CORRODED. REPLACED FLOORBEAM CAP PER SRM 53-10-9.SDR F3LA200200067Intercostal · corrodedDURING C-3 CHECK, INSPECTION REPORTED INTERCOSTAL AT STA 986 TO STA 1006, RBL 3, CORRODED. FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL PER SRM 51-30-2 AND EA 53-737-158.SDR F3LA200200066Web · corrodedDURING C-3 CHECK, INSPECTION REPORTED WEB AT STA 996 TO STA 1016, RBL 40, NEXT TO R2 DOOR CORRODED. FABRICATED AND INSTALLED REPLACEMENT WEB PER SRM 51-30-2.SDR F3LA200200065Strap · corrodedDURING C-3 CHECK, INSPECTION REPORTED STRAP ALONG THE BOTTOM OF PRODUCTION BREAK AT STA 1016, STR 23-L TO 23-R CORRODED. REPLACED STRAP PER SRM 51-30-2 AND BOEING DRAWING 65-46568.SDR F3LA200200064Skin · crackedDURING C-3 CHECK, INSPECTION REPORTED FUSELAGE SKIN RUBBED BY BELT 2 INCHES BELOW L-1 DOOR TOP SPIGOT (INTERIOR). PERFORMED EDDY CURRENT INSPECTION OF L-1 DOOR TOP SPIGOT INTERIOR BONDED DOUBLER AND FOUND 2 CRACKS. REPAIRED DAMAGED AREA PER EA 53-737-160.SDR F3LA200200063Floorbeam · corrodedDURING C-3 CHECK, INSPECTION REPORTED FLOORBEAM AT STA 986 CORRODED AT BOTTOM SURFACE AT FASTENERS THROUGH FLOORBOARDS. ALSO SHOWS EVIDENCE OF CORROSION ON TOP OF BEAM FROM BL 0 TO RBL 54 AS VIEWED FROM BELOW. REPLACED FLOORBEAM CAP AT STA 986 PER SRM 53-10-SDR F3LA200200062Intercostal · corrodedDURING C-3 CHECK, INSPECTION REPORTED CORROSION ON INTERCOSTAL AT STA 847, BL 16-R. FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL PER BOEING DRAWING 65-47957, SRM 51-10-2 AND SRM 51-30-2.SDR F3LA200200061Intercostal · corrodedDURING C-3 CHECK, INSPECTION REPORTED INTERCOSTAL AT STA 794, STR 27-R CORRODED. FABRICATED AND REPLACED INTERCOSTAL PER SRM 51-30-2 AND 51-20-1.SDR F3LA200200060Intercostal · corrodedDURING C-3 CHECK, INSPECTION REPORTED FLOOR INTERCOSTAL IN AFT GALLEY ENTRY CORRODED STA 957, BL 16L TO BL 42L. FABRICATED AND INSTALLED REPLACEMENT FLOOR SUPPORT PER SRM 53-10-2 AND 51-30-2.SDR F3LA200200058Intercostal · corrodedDURING C-3 CHECK, INSPECTION REPORTED FLOORBEAM INTERCOSTAL CORRODED FROM STA 1006 TO STA 1016, BL 0. FABRICATED AND REPLACED INTERCOSTAL PER SRM 53-10-2 AND 51-30-2.SDR F3LA200200057Floorbeam · corrodedDURING C-3 CHECK, INSPECTION REPORTED AFT LAVATORY TRANSVERSE BEAM CORRODED AT STA 1006 TO STA 1016, LBL 6. REPLACED TRANSVERSE FRAME PER SRM 51-30-2.SDR F3LA200200056Door Frame · corrodedDURING C-3 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FWD DOOR FRAME AT STA 803, STR 24-R, CRACKED AND CORRODED. REPLACED AFT CARGO COMPARTMENT DOOR FRAME PER SRM 57-10-1 AND 51-30-2.SDR F3LA200200055Gusset · wornDURING C-3 CHECK, INSPECTION REPORTED NR 1 ENGINE RT EXHAUST COWL INSIDE FLANGE ON BOTTOM OF THIRD RIB FROM FRONT WORN. REMOVED DAMAGED GUSSET FROM NR 1 ENGINE RT EXHAUST COWL. FABRICATED AND INSTALLED REPLACEMENT GUSSET PER SRM 51-21-171 AND 51-30-2.SDR F3LA00200054Floorbeam · corrodedDURING C-3 CHECK, INSPECTION REPORTED AFT LAVATORY TRANSVERSE FLOORBEAM CORRODED AT STA 986 TO STA 1006, LBL 10. REPLACED DAMAGED TRANSVERSE FRAME TOP CAP PER SRM 51-30-2 AND 51-10-2.SDR F3LA200200053Web · corrodedDURING C-3 CHECK, INSPECTION REPORTED WEB AT STA 1016, STR 20-L, BEHIND L-2 DOOR. FABRICATED AND INSTALLED REPLACEMENT WEB PER SRM 51-30-2 AND BOEING DRAWING 65-46812.SDR F3LA200200052Floorbeam · corrodedDURING C-3 CHECK, INSPECTION REPORTED AFT FLOORBEAM AT STA 967 CORRODED ON TOP SURFACE. FABRICATED AND REPLACED FLOORBEAM CAP PER SRM 51-30-2.SDR F3LA200200051Support · corrodedDURING C-3 CHECK, INSPECTION REPORTED AFT LAVATORY SUPPORT PARTITION FRAME CORRODED AT STA 998, 14 LBL. FABRICATED AND INSTALLED REPLACEMENT FRAME SUPPORT PER SRM 51-10-2.SDR F3LA200200050Skin · corrodedDURING C-3 CHECK, INSPECTION REPORTED CORROSION ON AFT CARGO COMPARTMENT DOOR CUTOUT, LOWER FWD CORNER, AT STA 790. REPAIRED DAMAGED SECTION PER SRM 53-30-3.
Back to N118RW, cancelled May 11, 2004