N418FE, cancelled Feb 18, 2016

Service difficulty reports · 29

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 = 'N418FE' AND deregistration_id = 'N418FE-2016-02-18'
  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 FDEA201204131398Valve · inoperativePASSING 10000 FT, RECEIVED ECAM ALERT ROR EXCESS CABIN ALTITUDE, ALSO OBSERVED ECAM ADVISORY FOR EXCESS CABIN VERTICAL SPEED (APPROX 3800') CLIMB. TRIED CONTROLLING WITH MANUAL PRESS CONTROL COULD NOT STOP RATE OF CLIMB. DONNED OXYGEN MASKS DESCENDED TO 1Apr 13, 2012 · N418FE · Airbus A310222 · Pressure Regulator/Outflow ValveSDR FDEA201111235007Landing Gear · malfunctionedNOSE GEAR WOULD NOT EXTEND USING NORMAL PROCEDURES, INDICATED UNLOCKED ON BOTH PRIMARY AND SECONDARY INDICATORS USED ALTERNATE PROCEDURE TO EXTEND. EMERGENCY WAS DECLARED. TROUBLESHOOTING AT THIS TIME.Nov 23, 2011 · N418FE · Airbus A310222 · Landing Gear Retraction/Extension SystemSDR FDEA201010023862Skin · corrodedRIGHT ELEVATOR UPPER SKIN AFT EDGE FOUND CORROSIN. REMOVE TOP SKIN UNTIL THE REAR SPAR. PERFORM SRM 55-21-11 CONG-1 FIG 209 WITH THE FOLLOWING PROVISIONS: INSTALLED STRAP FILLER.Oct 2, 2010 · N418FE · Airbus A310 · Elevator, Plate/SkinSDR FDEA201009093324Sleeve · out of positionADVANCING THROTTLES FOR TAKEOFF, RECEIVED A ENG 2 BLEED LEAK. FACT OPEN NR 2 ENG COWLS AND INSPECTED FOUND NO EVIDENCE OF BLEED LEAK WITH APU AIR. REMOVED RT WING L/E PANEL FOUND NO AIR LEAK AT PNEUMATIC DUCT. ALL LEAK CHECK USING APU AIR. FUTHER CHECK FOUND Sep 9, 2010 · N418FE · Airbus A310222 · Cabin Cooling SystemSDR FDEA201006222111Uplock · damagedAFTER TAKEOFF RECEIVED LANDING DOOR NOT CLOSED ECAM. CONFIRMED IT WAS THE NOSE FEAR DOOR (AMBER ON BOTH LANDING GEAR PANELS), IAW MX INSTRUCTION, RECYCLED GEAR, BOTH LIGHTS SAME ON AND ECAM RETURNED, MX WANTED GEAR RECYCLE AGAIN, BUT NOSE GEAR AREA VERY NOJun 22, 2010 · N418FE · Airbus A310222 · Landing Gear Door Retract SectionSDR 08FDEA04623Mount · corrodedAFT MOUNTING MATING SURFACE ON NR 2 ENGINE PYLON RUSTED. PERFORMED REPAIR AS PER EA NR 6-5450-125471 PART 2.Oct 30, 2008 · N418FE · Airbus A310222 · Engine Mount SectionSDR 08FDEA04624Fitting · corrodedAFT MOUNTING MATING SURFACE ON NR 1 ENGINE PYLON RUSTED. PERFORMED REPAIR AS PER EA 6-5450-125471 PART 2.Oct 30, 2008 · N418FE · Airbus A310222 · Engine Mount SectionSDR 08FDEA04465Arm · crackedEMPENNAGE, RT ELEV NR 5 HINGE ARM FOUND CRACKED/CORROSION AT UPPER END REPLACED RT ELEV NR 5 HINGE ARM AS PER AMM 55-16-45-4.Oct 21, 2008 · N418FE · Airbus A310222 · Elevator StructureSDR 08FDEA04464Skin · delaminatedLT WING, INBD FLAP TRAILING EDGE UPPER SURFACE PREVIOUS REPAIR LOCATED 44.0 INCH FROM OTBD EDGE DELAMINATED APPROX 3.0 BY 3.0 IN SIZE. REMOVED EXISTING REPAIR BY A NEW REPAIR PER SRM 57-52-12 FIG 204.Oct 21, 2008 · N418FE · Airbus A310222 · Trailing Edge FlapsSDR 08FDEA04463Skin · delaminatedRT WING, INBD FLAP TRAIL EDGE LWR SURFACE PREVIOUS REPAIR LOCATED 17.0 INCHES FROM INBD EDGE, DELAMINATED APPROX 22.0 BY 3.0 INCHES IN SIZE. REMOVED THE EXISTING REPAIR AND REPLACED BY A NEW REPAIR PER EA 6-5750-125477.Oct 21, 2008 · N418FE · Airbus A310222 · Trailing Edge FlapsSDR 08FDEA04462Skin · delaminatedLT WING, INBD FLAP TRAIL EDGE LWR SKIN PREVIOUS REPAIR LOCATED 54.5 INCHES FROM INBD EDGE DELAMINATED APPROX 3.0 BY 3.0 INCHES IN SIZE. REMOVED THE EXISTING REPAIR AND REPLACED BY A NEW REPAIR PER SRM 57-52-12 FIG 204.Oct 21, 2008 · N418FE · Airbus A310222 · Trailing Edge FlapsSDR 08FDEA04449Lug · corrodedWHILE COMPLYING WITH EO 6-5710-7-5010 CORROSION WAS FOUND ON BOTH LEFT AND RIGHT WING RIB 5 FORWARD LUG. COMPLIED WITH EA 6-5710-125482 IN THE REMOVAL OF CORROSION ON THE AFFECTED AREAS IN ACCORDANCE WITH EO 6-5710-7-5010.Oct 20, 2008 · N418FE · Airbus A310222 · Wing, Attach FittingsSDR 07FDEA02433Regulator Valve · failedENG 1 REV UNLOCK LIGHTS ILLUMINATED ON T/O ROLL LESS THAN 80KTS. ACN RELEASED FOR SERVICE PER MEL/CDL: 78-30-01-C 11JUL SFS. REMOVED AND REPLACED ENG 1 PRSOV, PERFORMED OPERATIONAL TEST, NORMAL PER MM 78-32-11-4 AND MM78-32-11-5.Jul 10, 2007 · N418FE · Airbus A310222 · Engine Thrust ReverserSDR 07FDEA02411Unknown · unknownUNLOCK LIGHTS ILLUMINATED ON T/O ROLL, LESS THAN 80KTS. RELEASED FOR SERVICE PER MEL/CDL: 78-30-01-C CATEGORY: C EXPIRATION: 20JUL07 "MEL 78-30-01-C: ENGINE (IDENTIFY 1 OR 2) NR 1 THRUST REVERSER, INOP. THRUST REVERSER IS DEACTIVATED IN FORWARD THRUST POSIJul 10, 2007 · N418FE · Airbus A310222 · Engine Thrust ReverserSDR 06FDEA04174Skin · damagedR-WING NR 4 SPOILER PANEL CENTER I/B HINGE AND O/B HINGE HAS WORN BUSHING. EXCESSIVE PLAY DURING MOVEMENT OF PANEL REMOVED AND REPLACED NR 4 RT WING SPOILER BUSHING IAW AMM 310/200 27-61-51-4 AND CMM 57-73-11. REMOVED AND REINSTALLED NR 4 RT WING SPOILER, ODec 5, 2006 · N418FE · Airbus A310222 · Drag Control SystemSDR 06FDEA04130Frame · damagedWHILE WORKING LT FS 12A DUE TO TOOLING MALFUNCTION DAMAGE TO FRAME 12A APPROX STR 29 COMPLIED WITH EA6-5310-105011.Nov 28, 2006 · N418FE · Airbus A310203 · Fuselage Main, FrameSDR 06FDEA04129Skin · unknownPREVIOUS REPAIR, RT FUSELAGE SKIN HAS EXTERNAL REPAIR DOUBLER MEASURES 8.3 IN X 5.5 IN, LOCATED AT FS 77 BETWEEN STRINGERS 52RT AND 54R REMOVED EXISTING REPAIR AND REPAIRED SKIN PER A310/200 SRM 53-10-12 FIG 217. ALSO, COMPLIED WITH FRAME 77 SHEARTIE TO FRAMENov 28, 2006 · N418FE · Airbus A310203 · Fuselage Main, Plate/SkinSDR 06FDEA04091Rib · corrodedVERTICAL STAB FRONT SPAR FWD FACE ENTIRE LENGTH OF RT VERT STAB L/E HAS CORROSION UNDER NUT PLATES AND FASTENER HOLES. REMOVED CORROSION FROM RIB12-26 RT CHORD FLANGE CHECKED AND FOUND TO BE IN LIMITS IAW A310/200 SRM'S 51-74-10, 55-31-21.Nov 22, 2006 · N418FE · Airbus A310203 · Vertical Stabilizer, Spar/RibSDR 06FDEA2855Engine · bird ingestionFELT A JULT ON T/O. SUSPECT COMPRESSOR STALL. CHECKED PER MM 72-00-00-6 03 AND FOUND BIRD STRIKE AT NR 2 ENGINE. COMPLIED ITEM 13B. NOTED NO ABNORMALITIES. ENGINE PARAMETER INDICATION OK. A/C OK FOR SERVICE.Aug 6, 2006 · N418FE · Airbus A310222 · Engine (Turbine/Turboprop)SDR 05FDEA02690Fire Loop · malfunctionedREPLACED FIRE DET ASSY (H2/H4) FOR BOTH LOOP A AND B, THIS ALSO CLEARED MEL ON "A" LOOP WRI 26-10/9082 PER MM 26-12-12-4. OPS CHECK SATIS AND PERFORMED ENG RUN PER A-310 JRH OK.Aug 26, 2005 · N418FE · Airbus A310222 · Fire DetectionSDR 04FDEA02875Fitting · crackedMOD TYPE H MOD NR C-CHECK REV NO, PS ACCOMPLISH MAINTENANCE C-CHECK NR 004. DURING C-CHECK WHILE ACCOMPLISHING EO 6-5710-7-3322 FOUND CRACK AT FWD FITTING FRAME 47, HOLE NR 41. ITEM WAS REPAIRED ON N00606 PER FEDEX EA 6-5710-77088.Oct 5, 2004 · N418FE · Airbus A310222 · Fuselage Main, StructureSDR 04FDEA00390Thrust Reverser · out of rigON TAKEOFF ROLL, JUST AFTER TOGA AND BEFORE STANDARD PWR WAS SET NR 2 THRUST REVERSER UNLOCK LIGHT ILLUMINATED ON LEFT ECAM SCREEN. ABORTED T/O COMPLIED WITH QRH, RETURNED TO GATE. MAINTENANCE PROCEDURE PERFORMED IAW MEL 78-30-01-C. MANUALLY CLOSED PRSV ANDFeb 10, 2004 · N418FE · Airbus A310 · Engine Thrust ReverserSDR 01FDEA01040Crossbeam · crackedMAIN DECK CARGO FLOOR CROSSBEAM DAMAGED AT BS 37 BETWEEN LBL 26.5 & 37.5. R&R CROSSBEAM PER SRM 53-10-15 FIG 201.Dec 7, 2001 · N418FE · Airbus A310222 · Fuselage Miscellaneous StructureSDR 00FDEA00617Floorbeam · crackedFRAME 37 AT AXIS LHS Y + 1800, .5 INCH BELOW UPPER FLANGE, FOUND CRACK .5 INCH LONG. *S/D* REMOVED AND REPLACED PER FEDEX EA 6-5100-52045 & A310 SRM SUPL MANUAL 53-10-15, FIG 201.Sep 2, 2000 · N418FE · Airbus A310222 · Fuselage Main, Floor BeamSDR 00FDEA00463Skin · dentedTHREE OFF DENTS IN FUSELAGE SKIN, RHS FWD OF BULK CARGO DOOR CUTOUT DURING C-CHECK. REPAIRED IN ACCORD WITH FEDEX EA REF EA 6-5330-49662.Jul 18, 2000 · N418FE · Airbus A310222 · Fuselage Main, Plate/SkinSDR 00FDEA00030Unknown · smoke00-17 - UPON TAXI OUT, ODOR OF SMOKE FILLED THE COCKPIT, RETURN TO RAMP. WHEN NR 2 ENGINE WAS SHUT DOWN, THE ODOR WAS GONE. PERF FAULT CONFIRM AND RESTARTED NR 2 ENGING NIL ABNLR OR ODOR OBSERVED.Jan 20, 2000 · N418FE · Airbus A310222 · Air Distribution SystemSDR 99FDEA00210Smoke Detector · failed99-129 AT 17,000 MSL, LT ECAM RED/CRC AVIONICS SMOKE NOT NOTICABLE FUMES/ODORS. REMOVED AND REPLACED 13WA SMOKE DETECTOR PER MM 26-15-12. OPS CK GOOD MM A310-26-15-00. OK FOR SERVICE.Jun 10, 1999 · N418FE · Airbus A310222 · Smoke DetectionSDR 98FDEA00120Smoke Detector · defectiveAPPROACHING LEVEL OFF AT FL 370, FWD CARGO COMPT SMOKE LIGHT AND ASSOC ECAM CAUTIONS ACTIVATED. NR 1 BOTTLE WAS DISCHARGED AND NR 2 BOTTLE WAS ACTIVATED ON APPROACH. LIGHT WENT OUT AFTER DISCHARGE. REMOVED AND REPLACED SMOKE DET A AND B, OPS CHK NORMAL. INFeb 18, 1998 · N418FE · Airbus A310222 · Fire DetectionSDR 96FDEA01238Hyd Line · leakingSTA KHH LOST GREEN HYD SYS DURING DESCENT PERFOMED ECAM ITEMS. WHEN A/C ARRIVED CK'D GREEN RSVR QTY AND FOUND LOWER THAN HAT ARC. T/S FOUND HYD FLUID LEAKING FROM LT INSIDE WING SPAR BETWEEN PYLON AND 1ST FLAP TRACK IT IS A RIDGID LINE FOR AILERON DROOP RUBBJul 11, 1996 · N418FE · Airbus A310221 · Hydraulic System, Main
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