N914TW, cancelled Sep 6, 2012

Service difficulty reports · 45

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 = 'N914TW' AND deregistration_id = 'N914TW-2012-09-06'
  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 ZW0A0208203B-Nut · looseDURING TAKEOFF HIGH TEMP LIGHT IN TAIL COMPARTMENT RESULT IN UNSCHEDULED LANDING/RETURN TO STL. PNEUMATIC PRESS REGULATOR RELIEF LINE LOOSE HEAT EXCHANGE VENTING TO TAIL COMPARTMENT RT HEAT EXCHANGE PERRY SEAL LEAKING. TIGHTENED B-NUT ON LT PRESS REGULATOR RAug 3, 2002 · N914TW · Doug DC982 · Pneumatic Distribution SystemSDR ZW0A0204604Connector · looseTHE EGRESS LIGHTING ROWS 7 TO 15 WERE INOPERATIVE. RESET THE CONNECTORS.Apr 23, 2002 · N914TW · Doug DC982 · Emergency LightingSDR ZW0A0204102Battery · dischargedTHE EMERGENCY EVACUATION LIGHTS IN THE CABIN WERE ILLUMINATED WITH THE SWITCH IN THE ARM POSITION. REPLACED THE BATTERIES IN THE POWER SUPPLY.Apr 5, 2002 · N914TW · Doug DC982 · Emergency LightingSDR ZW0A0203901Power SupplyDURING CLIMB AND DESCENT THE FIRST CLASS CABIN EGRESS LIGHTS ILLUMINATED. REPLACED THE POWER SUPPLY. CHECK-C 3-4-01 STL. --CLOSED--Apr 1, 2002 · N914TW · Doug DC982 · Emergency LightingSDR ZW0A0203303Frame · corrodedDURING CHECK-C MAINT THE FORMER RING AND REPAIR WERE CORRODED AT STA 1309, LONGERON 27R TO 27L. REMOVED AND INSTALLED NEW FRAME AND INSTALLED REPAIR SPLICES PER SRM 53-03, FIG 2A.Mar 14, 2002 · N914TW · Doug DC982 · Fuselage Main, FrameSDR ZW0A0203302Cargo Track · corrodedDURING CHECK-C MAINT THE LT FLOOR TRACK IN THE AFT CARGO COMPARTMENT WAS CORRODED FROM STA 1211 TO 1320. INSTALLED NEW TRACK IN CARGO COMPARTMENT, LT SIDE, AND INSTALLED SPLICE PLATE PER SRM 53-05, FIG 4G.Mar 14, 2002 · N914TW · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR ZW0A0203301Intercostal · corrodedDURING CHECK-C MAINT THE INTERCOSTAL WAS CORRODED AT STA 1308 TO 1322, BETWEEN LONGERON 27 AND 28, LT SIDE. DRILLED NEW INTERCOSTAL AND END FITTINGS AND INSTALLED PER SRM 51-30-2 AND 5, AND SPM 6-70-01.Mar 14, 2002 · N914TW · Doug DC982 · Fuselage Miscellaneous StructureSDR ZW0A0203102Floor Support · corrodedDURING CHECK-C MAINT IN AFT CABIN FOUND CORROSION ON FLOOR SUPPORT AT STA 1320, LONGERON 23L TO 23R. INSTALLED NEW FLOOR SUPPORT PER SPM 6-70-01, 4B.Mar 12, 2002 · N914TW · Doug DC982 · Fuselage Miscellaneous StructureSDR ZW0A0203104Floor Support · corrodedDURING CHECK-C MAINT FOUND CORROSION ON CAPTAINS KICKPLATE BULKHEAD AND FLOOR PANEL SUPPORT. REMOVED CORROSION PER SPM 6-80-01. FABRICATED NEW SUPPORT AND INSTALLED PER SRM 51-30-5.Mar 8, 2002 · N914TW · Doug DC982 · Fuselage Miscellaneous StructureSDR ZW0A0203103Seat Track · corrodedDURING CHECK-C MAINT FOUND PILOTS AFT INBD SEAT TRACK WAS CORRODED. REMOVED AND REPLACED TRACK PER SRM 51-01, PAGE 1, ITEM C.Mar 8, 2002 · N914TW · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR ZW0A0203106Seat Track · corrodedDURING CHECK-C MAINT FOUND CORROSION ON NUMBER 6 RH O/B SEAT TRACK, FROM STA 256 TO 313. REPLACED SECTION OF SEAT TRACK USING SEAT TRACK SPLICE AT STA 421. TRACK CHANGED FROM STA 214 TO 421, PER SRM 53-05, PAGE 104.Mar 6, 2002 · N914TW · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR ZW0A0203105Frame · corrodedDURING CHECK-C MAINT IN THE AFT CABIN AND CARGO BIN, THE FORMER RING WAS CORRODED AT STA 1271, LONGERON 27L TO 29R. INSTALLED NEW Z FRAME FROM LBL 37 TO RBL 11, PER SRM 53-02, FIG 2.Mar 6, 2002 · N914TW · Doug DC982 · Fuselage Main, FrameSDR ZW0A0202401Web · corrodedDURING CHECK-C FOUND LT AFT LAV AT STA 1338 TO 1350, STRINGER 18L TO 17L, LBL 50 TO 56, THE FLOORBEAM FRAME AT FUSELAGE SKIN AREA, WEB HAD CORROSION. REMOVED CORROSION PER SRM 51-10-3. REPLACED DAMAGED WEB SECTION PER 51-70-4. INSTALLED NEW CHORD FITTING.Feb 25, 2002 · N914TW · Doug DC982 · Fuselage Miscellaneous StructureSDR ZW0A0202402Angle · corrodedDURING CHECK-C MAINT THE LEFT SIDE MOST FORWARD CABIN DOOR JAMB, 2 ANGLES HAD CORROSION AT STA 180 TO 200. FABRICATED AND INSTALLED PER SRM 1-10-02, 1-10-03, 51-30-02, 51-14-01, AND SPM 6-10-01.Feb 20, 2002 · N914TW · Doug DC982 · Fuselage Miscellaneous StructureSDR ZW0A0202204Trunnion · crackedDURING CHECK-C MAINT IN THE LT WHEEL WELL, FOUND CRACK IN LT GEAR SUPPORT CASTING ABOVE THE LT INBOARD FLAP TRACK, AND ABOVE THE LT FLAP BUSS CABLE BRACKET. REPAIRED GEAR SUPPORT CASTING PER ARA 18090.Feb 14, 2002 · N914TW · Doug DC982 · Main Landing Gear Attach SectionSDR ZW0A0202006Bracket · crackedDURING CHECK-C MAINT THE MID CARGO DOOR BOTTOM INBOARD BRACKET WAS CRACKED, LOWER SIDE FOR AFT BOTTOM DOOR STOP. FABRICATED NEW BRACKET AND INSTALLED.Feb 13, 2002 · N914TW · Doug DC982 · Cargo/Baggage DoorsSDR ZW0A0202005Bracket · crackedDURING CHECK-C MAINT IN THE MID CARGO COMPARTMENT, THE AFT BOTTOM DOOR STOP BRACKET WAS CRACKED INSIDE THE DOOR, ON THE FWD FACE. REMOVED AND REPLACED CRACKED BRACKET WITH NEW PER SRM 51-01, AND SPM 6-70-01.Feb 13, 2002 · N914TW · Doug DC982 · Cargo/Baggage DoorsSDR ZW0A0201807Cargo Track · corrodedDURING CHECK-C MAINT IN CARGO COMPT FOUND CORROSION ON TIE DOWN TRACK AT STA 785, RT SIDE. REPLACED TRACK WITH NEW AT STA 693 TO 788 PER SPM 6-70-01.Feb 13, 2002 · N914TW · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR ZW0A0201806Tie Clip · corrodedDURING CHECK-C MAINT THE AFT CABIN STA 1338 TIE CLIP HAD CORROSION AT RBL 57 AREA. INSTALLED NEW CLIP PER SPM 6-70-01.Feb 12, 2002 · N914TW · Doug DC982 · Fuselage Miscellaneous StructureSDR ZW0A0201805Web · corrodedDURING CHECK-C MAINT THE AFT CABIN STA 1338, RBL 57, WEB HAD HEAVY CORROSION 6 INCHES BELOW FLOORBEAM RT LAV. INSTALLED FILLER DOUBLER PER SRM 51-70-4.Feb 12, 2002 · N914TW · Doug DC982 · Fuselage Miscellaneous StructureSDR ZW0A0202002Stop Fitting · crackedDURING CHECK-C MAINT IN MID CARGO COMPT THE AFT BOTTOM DOOR STOP BRACKET, INSIDE THE DOOR, IS CRACKED ON AFT SIDE. REMOVED AND REPLACED CRACKED BRACKET AND REPLACED WITH NEW PER SRM 51-01, PAGE 1.Feb 8, 2002 · N914TW · Doug DC982 · Cargo/Baggage DoorsSDR ZW0A0202001Floorbeam · corrodedDURING CHECK-C MAINT FOUND CORROSION IN RT FLOORBEAM BETWEEN STA 636 AND 693. REMOVED CORROSION PER SPM 6-80-01. INSTALLED REPAIR ANGLE AND FILLER PER SRM 53-05, FIG 20A.Feb 8, 2002 · N914TW · Doug DC982 · Fuselage Main, Floor BeamSDR ZW0A0201804Bracket · crackedDURING CHECK-C MAINT THE FORWARD CARGO COMPARTMENT DOOR HAD A SMALL BRACKET CRACKED LOCATED INSIDE THE SECOND LIGHTENING HOLE FROM THE AFT END, AT LOWER EDGE OF THE FWD CARGO COMPARTMENT DOOR. CONFIRMED WITH EDDY CURRENT. INSTALLED FITTING.Feb 7, 2002 · N914TW · Doug DC982 · Cargo/Baggage DoorsSDR ZW0A0201803Cargo Track · corrodedDURING CHECK-C MAINT IN THE AFT CARGO COMPARTMENT FOUND CORROSION ON FLOOR TRACK AT STA 1211 TO 1320, RT TRACK. REPLACED TRACK PER SPM 6-70-01-4B, AND SRM 51-30-01.Feb 7, 2002 · N914TW · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR ZW0A0201802Cargo Track · corrodedDURING CHECK-C MAINT IN THE AFT CARGO COMPARTMENT FOUND CORROSION ON THE LT TIE DOWN TRACK FROM STA 1003 TO 1231. INSTALLED NEW TIE DOWN TRACK PER SPM 6-70-01-4B, AND SRM 51-30-01.Feb 7, 2002 · N914TW · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR ZW0A0201602Keelbeam · crackedDURING CHECK-C IN LT WHEEL WELL, FOUND ANGLE CRACKED FWD OF HINGE CASTING AT KEEL BEAM. REMOVED AND REPLACED CRACKED ANGLE PER SPM 6-70-01.Feb 7, 2002 · N914TW · Doug DC982 · Fuselage Main, KeelSDR ZW0A0201601Frame · corrodedDURING CHECK-C FOUND CABIN STA 1338 LONGERON 18R, FRAME HAS CORROSION FROM FLOOR LEVEL TO 6 INCHES UP THE FWD SIDE. CORROSION WAS REMOVED PER SPM 6-80-01.Feb 7, 2002 · N914TW · Doug DC982 · Fuselage Main, FrameSDR TWAA0104605Battery Pack · dischargedTHE EMERGENCY LIGHTS CAME ON DURING FLIGHT AT ROW 5 THRU 15. REPLACED THE BATTERY PACK. CHECK-C 2-13-01 STL.Mar 10, 2001 · N914TW · Doug DC982 · Emergency LightingSDR TWAA0104603Battery Pack · disconnectedTHE EGRESS LIGHTS AT ROW 5 THRU 15 CAME ON DURING FLIGHT. ALL THE LIGHTS WENT OUT WITH THE EMERGENCY LIGHT SWITCH TURNED OFF. RECONNECTED THE BATTERY PACK AT ROW 5. CHECK-C 2-13-01 STL.Mar 10, 2001 · N914TW · Doug DC982 · Emergency LightingSDR TWAA0104604Battery · dischargedTHE EGRESS LIGHTS COME ON AT ROW 5 TO 15. REPLACED THE EMERGENCY LIGHT BATTERIES. CHECK-C 2-13-01 STL.Mar 9, 2001 · N914TW · Doug DC982 · Emergency LightingSDR TWAA0104501Battery · dischargedA SECTION OF EGRESS LIGHTING IN THE FIRST CLASS CABIN ILLUMINATED DURING TAXI AND WOULD NOT RESET. REPLACED THE BATTERIES IN THE POWER SUPPLY. CHECK-C 2-13-01 STL.Mar 8, 2001 · N914TW · Doug DC982 · Emergency LightingSDR TWAA0104403Battery Pack · dischargedTHE EGRESS LIGHTS ON CABIN FLOOR AND AT THE LEFT SIDE NUMBER 2 CABIN DOOR OCCASIONALLY ILLUMINATED IN FLIGHT. REPLACED THE BATTERY PACK. CHECK-C 2-13-01 STL.Mar 7, 2001 · N914TW · Doug DC982 · Emergency LightingSDR TWAA0104402Light · intermittentTHE FIRST SECTION OF CABIN EGRESS LIGHTS REPORTED TO INTERMITTENTLY STAY ILLUMINATED. RESET THE EMERGENCY LIGHT ARM AND CHARGE CIRCUIT BREAKER AND LIGHTS OPERATED NORMALLY. CHECK-C 2-13-01 STL.Mar 7, 2001 · N914TW · Doug DC982 · Emergency LightingSDR TWAA0100902Switch · inoperativeTHE EGRESS LIGHTING WAS INOPERATIVE FROM CABIN ROWS 5 TO 14. RECYCLED THE EMERGENCY LIGHT SWITCH. CHECK-C 2-3-00 STL.Jan 14, 2001 · N914TW · Doug DC982 · Emergency LightingSDR TWAA0017001Battery Pack · wornTHE FIRST CLASS OVERHEAD EMERGENCY LIGHT AND ONE SECTION OF COACH FLOOR EGRESS LIGHTS WERE INOPERATIVE. REPLACED THE BATTERY PACK AT ROW 3 AND THE FEEDER STRIP IN THE FIRST CLASS DIVIDER. CHECK-C 2-3-00 STL.Oct 31, 2000 · N914TW · Doug DC982 · Emergency LightingSDR TWAA0015606Compressor · fodCREW ABORTED TAKEOFF AT 65 KTS DUE TO RT ENGINE STALL WITH VIBRATION ON RT FUEL CONTROL LEVER. ENGINE WAS SHUT DOWN AND FLIGHT RETURNED TO THE GATE. COMPRESSOR HAD FAILED WITH ENGINE CASE PENETRATION, INCLUDING ONE INSTANCE OF UNCONTAINED FAILURE AT 12 O''CLOct 5, 2000 · N914TW · Doug DC982 · Turbine Engine Compressor SectionSDR TWAA9917001Vhf Radio · contaminatedTHE NUMBER 1 AND 2 VHF COMM RADIOS WERE INOPERATIVE AFTER TAKEOFF. STATIC WAS TRANSMITTED ON ANY FREQUENCY SELECTED. FLIGHT RETURNED TO STL. FOUND MOISTURE IN THE CAPTAINS AUDIO SELECTOR PANEL AND REPLACED THE PANEL. CHECK-C 2-13-99 MCI.Dec 15, 1999 · N914TW · Doug DC982 · VHF Communications SystemSDR TWAA9916901Light · inoperativeTHE CABIN EGRESS LIGHTS WERE INOPERATIVE FROM ROW 4 TO 16. FOUND FEEDER CABLE BROKEN AND SPLICED CABLE TOGETHER. CHECK-C 2-13-99 MCI.Dec 14, 1999 · N914TW · Doug DC982 · Emergency LightingSDR TWAA9906401Turbine · failedDURING TAKEOFF, THERE WAS A LOUD NOISE FROM THE NUMBER 1 ENG FOLLOWED BY HIGH EGT INDICATION. THE ENG WAS SHUT DOWN AND THE FLIGHT RETURNED TO STL. FOUND THE TURBINE HAD FAILED. REPLACED THE ENGINE. CHECK-C 2-13-99 MCI.Apr 3, 1999 · N914TW · Doug DC982 · Turbine SectionSDR TWAA9819301Coffeemaker · failedTHE NUMBER 3 GALLEY COFFEEMAKER CAUSED SPARKS. CREW PULLED CIRCUIT BREAKER. MAINT REPLACED THE COFFEEMAKER. CHECK-C 2-28-98 MCI.Dec 4, 1998 · N914TW · Doug DC982 · Buffet/GalleysSDR TWAA9812501Boost Pump · wornABOVE FL 300 COULD NOT PUMP FUEL FROM CENTER TANK. TURNED OFF LEFT TANK PUMPS AND DESCENDED IN ALTITUDE AND CENTER TANK STARTED FEEDING. RETURNED TO MCI. REPLACED BOTH CENTER TANK FUEL BOOST PUMPS. CHECK-C 2-28-98 MCI.Aug 3, 1998 · N914TW · Doug DC982 · Fuel Boost PumpSDR 96ZZZM1202Bulb · failedSFO - DURING GEAR EXTENSION RIGHT MAIN LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE. REMOVED AND REPLACED LIGHT BULB IN LIGHT ASSEMBLY. OPERATIONAL CHECK NORMAL. (M)Jul 10, 1996 · N914TW · Doug DC982 · Landing Gear Position and WarningSDR 96ZZZM46Strut Seals · failedTPA - DURING LANDING, UNABLE TO LOWER NOSE GEAR. CYCLED LANDING GEAR. NOSE STRUT SEALS REPLACED, REPACKED NOSE STRUT. CYCLED GEAR AND OPERATIONS ARE NORMAL.Dec 23, 1995 · N914TW · Doug DC982 · Nose/Tail Landing Gear Strut/AxleSDR 95ZZZX3411Blade · failedDEN - FLT 427 - DURING DESCENT, SHUT DOWN LEFT ENGINE DUE TO SPOOLED DOWN WITH INCREASING EGT. FOUND METAL PARTICLES IN TAILPIPE. CHANGED ENGINE, S/N 1205. ENGINE OPERATION CHECKED NORMAL. ENGINE TOTAL TIME: 21,594 HOURS; 10,979 CYCLES. OP-15 - 12-3-94 -Jun 22, 1995 · N914TW · Doug DC982 · Turbine Engine Compressor SectionSDR 95ZZZW339Retract Sys · req'd lubeBOS - AFTER TAKEOFF NOSE LANDING GEAR DID NOT RETRACT. CYCLED LANDING GEAR, AND NOSE LANDING GEAR RETRACTED. INSPECTED NOSE LANDING GEAR AND LUBRICATED. JACKED NOSE LANDING GEAR AND OPERATED NOSE LANDING GEAR SEVERAL TIMES AND ALL OPERATIONS WERE NORMAL.Mar 20, 1995 · N914TW · Doug DC982 · Landing Gear Retraction/Extension System
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