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.

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 MJun 22, 2008 · N240FE · Boeing 727227 · Stall Warning SystemSDR 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.Feb 22, 2007 · N240FE · Boeing 727277 · Cargo/Baggage DoorsSDR 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.Feb 22, 2007 · N240FE · Boeing 727227 · Nacelle/Pylon, Main FrameSDR 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 STALLApr 29, 2006 · N240FE · Boeing 727227 · Engine (Turbine/Turboprop)SDR 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 ANDec 3, 2005 · N240FE · Boeing 727200 · Hydraulic System, MainSDR 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.Mar 12, 2005 · N240FE · Boeing 727200 · Turbine Engine Oil SystemSDR 05FDEA00047Shear Tie · damagedREPAIR SHEAR TIE AT BS 380 BETWEEN STR 14 & 15 LT TO ACCOMPLISH 9G MOD. REPAIRED PER SRM 53-10-4.Jan 7, 2005 · N240FE · Boeing 727200 · Fuselage Main, StructureSDR 05FDEA00048Shear Tie · damagedREPAIR SHEAR TIE AT BS 380 BETWEEN STR 15 & 16 LT TO ACCOMPLISH 9G BARRIER MOD.Jan 7, 2005 · N240FE · Boeing 727200 · Fuselage Main, StructureSDR 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 SRMSep 29, 2004 · N240FE · Boeing 727277 · Fuselage Miscellaneous StructureSDR 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 Sep 28, 2004 · N240FE · Boeing 727277 · Fuselage Main, Floor BeamSDR 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.Sep 28, 2004 · N240FE · Boeing 727277 · Wing, Landing Gear Attach FittingsSDR 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.Sep 28, 2004 · N240FE · Boeing 727200 · Wing, Landing Gear Attach FittingsSDR 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.Sep 28, 2004 · N240FE · Boeing 727200 · Nacelle/Pylon, Plate/SkinSDR 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 ANSep 22, 2004 · N240FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 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,Sep 22, 2004 · N240FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 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 Sep 22, 2004 · N240FE · Boeing 727200 · Fuselage Main, Longeron/StringerSDR 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 20-1Mar 5, 2004 · N240FE · Boeing 727200 · Trailing Edge Flap Control SystemSDR 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 PERSep 20, 2003 · N240FE · Boeing 727200 · Door Warning SystemSDR 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 FFSep 1, 2003 · N240FE · Boeing 727200 · Turbine Engine Reduction GearSDR 02FDEA00242Fitting · crackedBS 1185, LBL 24, WL 292 BULKHEAD TO SPAR FITTING CRACKED AT FWD HORZ FASTENER HOLE. REMOVED AND REPLACED FITTING PER SRM & MM.Apr 9, 2002 · N240FE · Boeing 727277 · Fuselage Miscellaneous StructureSDR 02FDEA00235Skin · wornN 279 FASTENERS AROUND DRAIN HOLE 11" ABOVE LH AFT NLG DOOR WORN. ** S/D ** COMINGApr 8, 2002 · N240FE · Boeing 727277 · Fuselage Main, Plate/SkinSDR 02FDEA00234Skin · chafedMAIN E/E BAY DOOR SKIN IS CHAFED AT LEFT AFT EDGE. R&R SKIN PER SRM.Apr 6, 2002 · N240FE · Boeing 727277 · Electrical/Electronic Compartment DoorsSDR 02FDEA00306Frame · dentedN 697 MAIN CARGO DOOR AFT SIDE FRAME DENTED ABOVE CENTERING GUIDE RAMP. ** S/D ** COMINGMar 28, 2002 · N240FE · Boeing 727277 · Cargo/Baggage DoorsSDR 02FDEA00226Door Frame · dentedMAIN CARGO DOOR AFT SIDE FRAME DENTED ABOVE CENTERING GUIDE RAMP. REMOVED AND REPLACED FRAME PER EA 7-5230-64028.Mar 28, 2002 · N240FE · Boeing 727277 · Cargo/Baggage DoorsSDR 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.Mar 27, 2002 · N240FE · Boeing 727277 · Cargo/Baggage DoorsSDR 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.Mar 25, 2002 · N240FE · Boeing 727277 · Galley DoorsSDR 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.Dec 19, 2000 · N240FE · Boeing 727277 · Cabin Pressure ControllerSDR 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 32-62-011Nov 22, 2000 · N240FE · Boeing 727277 · Landing Gear Position and WarningSDR 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 Mar 10, 1998 · N240FE · Boeing 727277 · Fire DetectionSDR 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. LFeb 18, 1998 · N240FE · Boeing 727277 · Fire DetectionSDR 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-Jul 2, 1997 · N240FE · Boeing 727277 · Elevator Tab Control SystemSDR 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.Apr 10, 1997 · N240FE · Boeing 727277 · Fuselage Miscellaneous StructureSDR 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.Apr 9, 1997 · N240FE · Boeing 727277 · Fuselage Main, KeelSDR 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 Apr 1, 1997 · N240FE · Boeing 727277 · Trailing Edge FlapsSDR 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.Mar 31, 1997 · N240FE · Boeing 727277 · Fuselage Main, FrameSDR 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 FEDMar 31, 1997 · N240FE · Boeing 727277 · Trailing Edge FlapsSDR 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.Jan 12, 1997 · N240FE · Boeing 727277 · Landing Gear Position and WarningSDR 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.Jan 11, 1997 · N240FE · Boeing 727277 · Landing Gear Position and WarningSDR 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 CONJan 12, 1995 · N240FE · Boeing 727277 · Landing Gear Position and Warning
Back to N240FE, cancelled Apr 25, 2013