N240FE, cancelled Apr 25, 2013
Service difficulty reports · 39
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 = 'N240FE' AND deregistration_id = 'N240FE-2013-04-25' 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 = 'N240FE' AND deregistration_id = 'N240FE-2013-04-25' 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 08FDEA02376Aoa · damagedSTALL WARNING ACTIVATED AT ROTATION. AIRCRAFT FLYING NORMALLY. STAYED ON UNTIL CIRCUIT BREAKER PULLED. AMBER WINDSHEAR LIGHT CAME ON. REMOVED AND REPLACED AOA VANE AND SYSTEM OPS CKS NORMAL IAW 727 M/M 34-18-051-4 AND REINSTALLED S/OS HAND MIKE AND BOOM MSDR 07FDEA00541Unknown · noneDOORS, MAIN CARGO LWR AFT CORNER EXTERNAL SKIN PERMANENT REPAIR P/N 52FX1435-2. COMPLIED WITH EA 7-5230-102022 DOORS MAIN CARGO, LWR AFT CORNER EXTERNAL SKIN PERMANENT REPAIR P/N 52FX14 35-2.SDR 07FDEA00540None · noneNACELLES AND PYLONS MINOR DEVIATION TO SRM S DUCT HOUSING SKIN REPAIR. COMPLIED WITH EA 7-5410-102026 THIS ITEM CLEARED BY REPAIR PER SRM 54-10-3 FIG 4 WITH MINOR DEVIATION DOCUMENTED BY THIS EA.SDR 06FDEA1661Engine · failedATTEMPTED TAKEOFF ON 18L HAD SLIGHT COMPRESSOR STALL ON POWER APPLICATION. ABORTED TAKEOFF AND CHECKED ENGINE CONDITIONS ELECTED SECOND ATTEMPT DUE TO CROSSWINDS. ON SECOND ATTEMPT HAD ANOTHER COMPRESSOR STALL. 1ST STALL OCCURRED AT 1.5 EPR AND SECOND STALLSDR 05FDEA04109Union · leakingAFTER T/O WHEN GEAR LVR WAS RAISED TO THE UP POS THE HYD SYS (A) RESERVOIR WENT TO ZERO. THE GEAR REMAINED DOWN AND FLAPS STAYED AT 15 DEG. REMOVED AND REPLACED PACKING AND UNION FOR THE OB TE FLAP CONTROL VALVE IAW IPC REF 27-50-00-30AZZ ITEM 145. LEAK ANSDR 05FDEA00501Oil Filter · bypassingDESCENDING THROUGH 20,000 FEET, THE NR 1 LOW OIL PRESSURE/FILTER BYPASS LIGHT ILLUMINATED; ENGINE OIL PRESSURE READ 45 PSI (MATCHED NR 2 AND NR 3). SHUT DOWN NR 1 ENGINE IAW QRH PROCEDURES. NO OTHER PROBLEMS NOTED.SDR 05FDEA00047Shear Tie · damagedREPAIR SHEAR TIE AT BS 380 BETWEEN STR 14 & 15 LT TO ACCOMPLISH 9G MOD. REPAIRED PER SRM 53-10-4.SDR 05FDEA00048Shear Tie · damagedREPAIR SHEAR TIE AT BS 380 BETWEEN STR 15 & 16 LT TO ACCOMPLISH 9G BARRIER MOD.SDR 04FDEA02842Channel · corrodedFWD LWR CARGO A/C COMPT STR 27L BETWEEN F/S 720F TO 740, PROTECTIVE FINISH PEELING AND MINOR SURFACE CORROSION IN HAT CHANNEL. REMOVED CORROSION IAW SRM 51-10-6 PG 6, PARG 4. ORIG MAT .095, AFTER REWORK .075 .020 MAT LOSS, FOUND TO BE OUT OF LIMITS IAW SRMSDR 04FDEA02840Floorbeam · corrodedBFM CLOSER C/W WITH EA7-5321-82044 FUSELAGE, FLOORBEAM UPPER CORD REPAIR STA 950 AT BL 21.0 ENT BY: 497236 RPT BY: 497236 FACT 28SEP04 23:10. BFM U COMPLIED WITH EA 7-5321-82044. REMOVED CORROSION, TREATED AREA AND INSTALLED REPAIR ANGLE ENT BY: 497236 RPT SDR 04FDEA02839Support Beam · corrodedCLOSER COMPLY WITH EA NR 7-5710-82041 WINGS, LEFT MLG SUPPORT BEAM CORROSION AT FLAP TRACK MOUNT. BFM U COMPLIED WITH EA7-5710-82041 REAMED HOLE, FLAP PEENED AREA , INSTALLED REPAIR BUSHING AND WASHER ENT BY: 497236 RPT BY: 497236.SDR 04FDEA02838Beam · corrodedCOMPLY WITH EA 7-5710-82042 WINGS RIGHT MLG SUPPORT BEAM CORROSION AT FLAP TRACK MOUNT. COMPLIED WITH EA 7-5710-82042 REAMED HOLE, FLAP PEENED AND INSTALLED REPAIR BUSHING.SDR 04FDEA02837Skin · damagedCOMPLY WITH EA 7-5450-80610 PYLON STRUCTURE NR 1 ENG PYLON UPPER SKIN REPAIR. COMPLIED WITH EA 7-5450-80610, REPLACED SKIN SECTION AND INSTALLED EXT SPLICE DOUBLER.SDR 04FDEA02803Floor Support · corrodedAFT CARGO COMPT FLOOR SUPPORT BEAM CORRODED UNDER NUTPLATE STA. 1110, RBL 6. REMOVED CORROSION, MATERIAL OUT OF LIMITS IAW SRM 53-10-5 FIG.6,PG.16 AND SRM 51-10-6. REMOVED DAMAGED AREA FROM STA 1105 TO 1115 RBL, FABRICATED 4 EA ANGLES (SPLICES). REPAIR ANSDR 04FDEA02801Intercostal · crackedFWD CARGO, INTERCOSTAL IS CRACKED AT STRINGER 25L STA.624. REMOVED INTERCOSTAL IAW SRM 51-30-2. FABRICATED,TREATED AND PRIMED NEW INTERCOSTAL IAW SRM 51-20-1 FIG.6, 51-30-5 AND 51-10-2. INSTALLED IAW SRM 51-30-2. FABRICATED INTERCOSTAL USING 2024-T3 .050,SDR 04FDEA02800Stringer · corrodedNUMEROUS AREAS OF CORROSION FOUND AT FWD PIT BILGE AREA FROM STA 560 TO STA 580 AT STR 28L. REMOVED DAMAGED AREA FROM STA 550 - 590 IAW SRM 51-10-3 FIG 1 PG 4. FABBED 2EA STRINGERS FROM BAC1498-142 7075-T62, BATCH 318127, FABBED 3EA SPLICES FROM BAC1498-132 SDR 04FDEA00601O-Ring · failedA-SYSTEM HYDRAULICS FAILED IN FLIGHT. IN CRUISE FLT LVL 220, NOTICED A-SYSTEM QUANTITY DECREASING, LEAK CONTINUED TILL CHECKLIST DIRECTED A-PUMPS TO BE TURNED OFF. FOUND O-RING FAILURE AT UPPER PORT OF FLAP CONTROL VALVE. REPLACED O-RING PER 727-200 MM 20-1SDR 03FDEA01597Door · false indicationRED GEAR DOOR LIGHT ILLUMINATED AFTER GEAR RETRACTION AND HANDLE PLACED IN OFF POSITION. LIGHT EXTINGUISHED WHEN GEAR HANDLE PLACED IN UP POSITION. COMPLIED WITH ALL APPLICABLE CHECK LIST. PUT IN GEAR PINS, CYCLED GEAR DOORS, ALL INDICATIONS NORMAL, REF PERSDR 03FDEA01401Packing · leakingAFTER T/O NR 1 ENG EPR LOW WITH A HI FF AT FL200 NR 1 ENG THROTTLE LEVER 3 INCHES FWD OF NR 2 & 3 THROTTLE LEVERS W/ ALL EPR'S MATCHING & NR 1 FF GAUGE 3000 LBS/HR MORE THAN NR 2 & 3 FF GAUGES. ALL ENG INST IN GREEN. CL THRU FL230, NR 1 EPR INDIC 0 & NR 1 FFSDR 02FDEA00242Fitting · crackedBS 1185, LBL 24, WL 292 BULKHEAD TO SPAR FITTING CRACKED AT FWD HORZ FASTENER HOLE. REMOVED AND REPLACED FITTING PER SRM & MM.SDR 02FDEA00235Skin · wornN 279 FASTENERS AROUND DRAIN HOLE 11" ABOVE LH AFT NLG DOOR WORN. ** S/D ** COMINGSDR 02FDEA00234Skin · chafedMAIN E/E BAY DOOR SKIN IS CHAFED AT LEFT AFT EDGE. R&R SKIN PER SRM.SDR 02FDEA00306Frame · dentedN 697 MAIN CARGO DOOR AFT SIDE FRAME DENTED ABOVE CENTERING GUIDE RAMP. ** S/D ** COMINGSDR 02FDEA00226Door Frame · dentedMAIN CARGO DOOR AFT SIDE FRAME DENTED ABOVE CENTERING GUIDE RAMP. REMOVED AND REPLACED FRAME PER EA 7-5230-64028.SDR 02FDEA00222Skin · dentedNR 2 CARGO DOOR OUTER SKIN HAS THREE LARGE DENTS FWD OF AFT EDGE 6 INCHES FROM BOTTOM. REMOVED AND REPLACED SKIN PER EA 75230-64035.SDR 02FDEA00233Web · corrodedFWD GALLEY DOOR INTERNAL WEB ABOVE CENTER PRESSURE PANEL UPPER SURFACE OF WEB HAS CORROSION. REMOVED AND REPLACED WEB PER SRM 51-20-1, 51-10-1.SDR 00FDEA00886Controller · faulty00-365 FLT 1239/19 AIR TURN-BACK SEA. AC WILL NOT PRESSURIZE. WITH REF TO B727-200 MM 21-31-00-0 INSP AIRFRAME. RESET & PRESSURE TEST C/W CHECKS OK.SDR 00FDEA00786Switch · malfunctionedWHEN PUTTING GEAR HANDLE FROM UP TO OFF, DOOR LIGHT ILLUMINATED WITH RIGHT MAIN DOOR LIGHT ILLUMINATED ON S/O PANEL. COMPLETED RED TABS HANDLE TO OFF, LIGHT OUT. *S/D* REMOVED AND REPLACED DOOR WARN SWITCH PER MM 32-62-011-4 & OPS CK NORMAL PER MM 32-62-011SDR 98FDEA00167Fire Warn Light · malfunctionBOTH MASTER FIRE WARNING LIGHTS ILLUMINATE INTERMITTENTLY. ALL FIRE WARNING LIGHTS OFF PRIOR TO TAKEOFF. ONCE AIRBORNE APU FIRE LIGHT CAME ON STEADY. MASTER FIRE WARNING LIGHTS STARTED FLICKERING. REPLACED APU FIRE BOTTLE. FOUND CORROSION ON PLUG D-4858P SDR 98FDEA00116Fire Light · malfunctionedRED LIGHT ON IN AUXILIARY POWER UNIT FIRE HANDLE IN FLIGHT. TOOK OFF AT 0334Z AND NOTICED THE AUXILIARY POWER UNIT RED LIGHT ON AT 0400Z, FLIGHT LEVEL 310. PULLED THE HANDLE AND DISCHARGED THE AGENT. RED LIGHT REMAINED ON BUT WITH VARIATION OF INTENSITY. LSDR 97FDEA00382Bolt · jammedBEFORE TAKEOFF CHECK, ELEVATOR JAMMED PULLING AFT ON YOKE. OPENED ACCESS PANELS 9115, 9118, BOUND BOLT AT FORWARD END OF FORWARD TAB ROD ON LEFT HAND ELEVATOR POWER CONTROL UNIT WORKED LOOSE. INSTALLED BOLT, WASHERS, NUT AND SAFETY PER MAINTENANCE MANUAL 27-SDR 97FDEA00227Chord · corrodedNR 0302 005. CORROSION (C53-100-01(1)) ON MID LT NOSE CHORD BS 344-350, LBL 16, WL 170. REMOVED AND REPLACED MID LT NOSE CHORD PER BAC DWG 65-18415 AND FED-EX SRM 51-30-2.SDR 97FDEA00229Keel Beam · corrodedNR 0250 004, CORROSION (C53-113-01-1) ON KEEL BEAM AT BS 720F, RBL 7, WL 149. *S/D* REMOVED CORROSION, SPOT FACED, FLAP PEENED AND INSTALLED STRAP AT BS 720F, RBL 7, WL 149 IAW FED-EX EA 7-5310-32976.SDR 97FDEA00211Foreflap · delaminatedNR 0349 003, LEFT WING I/B UPPER SURFACE STAINLESS STEEL RUB STRIP DISBONDED. *S/D* REMOVED, REPAIRED AND INSTALLED ON LEFT WING I/B FOREFLAP, I/B UPPER SURFACE STAINLESS STEEL RUB STRIP IAW FED-EX SRM 51-40-6. FUNCTIONAL TEST LEFT WING I/B FOREFLAP OK IAW SDR 97FDEA00208Frame · damageNR 0244 002, DENT IN FRAME AT BS 720A, RBL 15, WL 155. BLENDED OUT DENT AND REPAIRED FRAME BS 720A, RBL 15, WL 155. ALL WORK ACCOMPLISHED PER FED-EX 727 SRM 51-10-2, 51-10-6, 53-10-4. FABRICATED REPAIR PART PER FED-EX SRM 53-10-4.SDR 97FDEA00207Wedge · puncturedNR 0106 001, RIGHT WING I/B MIDFLAP TRAILING EDGE WEDGE PUNCTURED ON LOWER SURFACE 25 FROM INBOARD END. *S/D* REMOVED RIGHT WING I/B AFT FLAP, REPAIRED PUNCTURE ON RIGHT WING I/B MID FLAP T/E WEDGE, INSTALLED RIGHT WING I/B AFT FLAP, REPAIR PERFORMED IAW FEDSDR 97FDEA00042Accessory Unit · failedLANDING GEAR WOULD NOT RETRACT UNLESS WE USED LATCH LEVER RELEASE. REMOVED AND REPLACED GEAR ACCESSORY UNIT IAW 32-09-121 PG 401, FUNCTIONAL TEST GOOD IAW 32-09-122 PG 501 TO 505.SDR 97FDEA00037Sensor · dirtyGEAR WOULD NOT RETRACT NORMALLY AFTER TAKEOFF. RETRACTED GEAR USING LEVER LOCK OVERRIDE. GEAR EXTENDED NORMALLY FOR LANDING. FOUND ICE ON AIR GROUND SAFETY SENSOR. CLEANED AND LUBED AS REQUIRED.SDR 95FDEA00010Accessory Unit · false warningAFTER T/O FROM MEM AT GEAR RETRACTION, THE L/MAIN GEAR RED LIGHT WOULD NOT EXTINGUISH. CHECKLIST PROCEDURE ACCOMPLISHED. ALL GREEN ALL GEAR DOOR LIGHTS AND THE NOSE AND R/MAIN RED LIGHT EXTINGUISHED. THE L/MAIN RED LIGHT STILL WOULD NOT EXTINGUISH. FLT CON
Back to N240FE, cancelled Apr 25, 2013