N426FE, cancelled Jun 28, 2024

Service difficulty reports · 90

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 = 'N426FE' AND deregistration_id = 'N426FE-2024-06-28'
  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 FDEA201511093525Battery · inoperativeDURING SERVICE CHECK, FOUND ASPSU FAULTED NR 2 BATTERY REASON CODE. R & R NR 2 BATTERY ON ASPSU IAW AMM 52-73-18-04. PERFORMED BITE TEST IAW AMM 52-73-00-05, SYS CHECKED GOOD. EMER POWER SUPPLY BATTERY PN AD-3214-30 & SN 42169.Nov 9, 2015 · N426FE · Airbus A310203 · Door Warning SystemSDR FDEA201511083515Battery Pack · dischargedEMERGENCY LIGHTS WILL NOT TEST IN COURIER AREA. R & R EMER POWER SUPPLY BATTERY PACK IAW AMM 33-51-14-4. OPERATIONS CHECKED GOOD. PART NAME, EMER POWER, BATTERY PACK, PN AD-3214-30 & SN 106982.Nov 8, 2015 · N426FE · Airbus A310 · Emergency LightingSDR FDEA201310072434Engine · failedDURING CLIMBOUT, NR 1 ENGINE OVERTEMPED. HEARD A LOUD POP WITH A YAW TO THE LEFT. ALL ENG INDICATIONS WERE NORMAL EXCEPT EGT WHICH WAS 700 DEGREES HIGHER THEN NR 2 EGT, NR 1 EGT STAYED BEWTEEN 600 TO 700 DEGREES. DURING RETURN, MAX EGT 1000 FT. REMOVED ANDOct 7, 2013 · N426FE · Airbus A310203 · Engine (Turbine/Turboprop)SDR FDEA201308171919Spar · damagedRT PYLON LWR SPAR BETWEEN RIBS 6 AND 7. REPAIRED IAW EA 6-5450-117917C, PART 2. COMPLIED WITH EA 6-5450-117917C PART2. REMOVED AND INSTALLED THE REPAIR DOUBLER FOR NDT INSPECTION.Aug 17, 2013 · N426FE · Airbus A310203 · Nacelle/Pylon, Main FrameSDR FDEA201308171918Skin · corrodedLT WING ROOT CENTER WING BOX BOTTOM SKIN LWR SURFACE FOUND CORRODED BETWEEN FR44-45. REMOVED CORROSION IAW SRM 51-74-10. REPAIRED EA 6-5710-T0301458.Aug 17, 2013 · N426FE · Airbus A310203 · Fuselage Main, Plate/SkinSDR FDEA201308061782Sill · corrodedBULK CARGO DOOR SILL FOUND CORROSION SURROUNDING FASTENER HOLES BETWEEN FR 68 & 69. REPLACED SILL IAW SRM 51-40-21.Aug 6, 2013 · N426FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR FDEA201307261665Floor Support · corrodedMAIN DECK FR 14-14B, Y730, FLOOR SUPPORT CORRODED. REPAIRED FLOOR SUPPORT IAW SRM 53-12-15/201, FIG 207.Jul 26, 2013 · N426FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR FDEA201307261666Floor Support · corrodedMAIN DECK FR 12A-15A Y1456 FLOOR SUPPORT CORRODED. REPAIRED THE FLOOR SUPPORT IAW SRM 53-12-15/201, FIG 207.Jul 26, 2013 · N426FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR FDEA201301310237Buffer · bindingDURING CLIMBOUT, FLAP VANE JAMMED. HANDLE WAS AT SLATS/FLAPS POS 15/0 . SLATS/FLAPS INDICATED 15/5. FLAPS SYS 1 AND SYS 2 FAULT LIGHTS ON. SLATS/FLAPS EXTENDED NORMALLY FOR LANDING. SFCC NR 1 AND SFCC NR 2 BOTH FAULTED " LT VANE OUT ". EFCU NR 1 FAULTS MJan 31, 2013 · N426FE · Airbus A310203 · Trailing Edge Flap Control SystemSDR FDEA201301290217Switch · malfunctionedDEPARTING & DURING FLAP RETRACTION, RECEIVED AN ECAM ALERT "FLAPS VANE JAM". COMPLIED WITH QRH, CYCLED THE FLAPS, AND UNABLE TO FIX PROBLEM. RETURNED TO DEPARTURE. FOUND BOTH NR 1 & NR 2 SFCC'S FAULTED "LT VANE IN 2" ON ARRIVAL. RESET BOTH SFCC'S & RETRAJan 29, 2013 · N426FE · Airbus A310203 · Trailing Edge Flap Control SystemSDR FDEA201104221588Bracket · wornPERFORM W/C 47C0201 FOUND NLG MAIN DOOR RT SELECTOR VALVE FIXED BRACKET THREAD WORN OUT. REMOVED THE WORN OUT BRACKET, THEN INSTALLED A NEW ONE FOR REPLACEMENT IAW EA NR6-3220-150288 (LANDING GEARS, NOSE GEAR AND DOORS: SHAFT INSTALLATION, THREAD DAMAGE ON NLApr 22, 2011 · N426FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR FDEA201104201535Panel · misrepairedDOUBLER HAD TO BE REMOVED. PERFORMED FUSELAGE, PLATES AND SKIN: RT FUSE SKIN PANEL, FR54, STR 44R, REDUNDANT FASTENER, PERMANENT REPAIR DURING PERFORMED 41 X 5141 ALI STEP ID. ONE FASTENER IS COVERED BY DOUBLER IAW EA NR 6-5330-1502 81.Apr 20, 2011 · N426FE · Airbus A310203 · Fuselage Main, Plate/SkinSDR FDEA201104141484Rib · crackedREAR FUSELAGE INTERNAL FOUND 1 RIB CRACKED AT FR86 STR32R. REMOVED THE CRACKED RIB. FABRICATED A NEW RIB FOR REPLACEMENT IAW SRM 51-72-10 AND IAW DWG A53986743205.Apr 14, 2011 · N426FE · Airbus A310203 · Fuselage Main, StructureSDR FDEA201104141483Floorbeam · crackedMAIN DECK COMPT FLOOR AREA FOUND CROSSBEAM GOT A CRACK AT FR 42 LOCATION BETWEEN -Y450 AND -Y953. REMOVED THE NR 242RH. NR 242QJ, NR 242SH FLOOR PANELS FOR CROSSBEAM REPLACEMENT IAW AMM 53-10-25-4. R & R THE CROSSBEAM WITH CHECK OK FOR SERVICE IAW SRM 51-72-Apr 14, 2011 · N426FE · Airbus A310203 · Fuselage Main, Floor BeamSDR FDEA201104121445Skin · corrodedRIGHT WING UPPER SURFACE FOUND CORROSION POSITION AT O /B GROUND POINT ABOUT RIB 27-28 PERFORMED WINGS, SKIN AND PLATES: PERMANENT REPAIR REF. TO EA 6-5730-150286. PER GMM 6-2-100 CLASSIFIED MAJOR.Apr 12, 2011 · N426FE · Airbus A310203 · Wing, Plate/SkinSDR FDEA201104121444Skin · corrodedLT WING FOR SKIN GOT CORROSION AT STA 845 SURROUND GROUNDING STUD (RIB 13-14, STR7-8).Apr 12, 2011 · N426FE · Airbus A310203 · Wing, Plate/SkinSDR FDEA201104121447Crossbeam · corrodedUPPER SUPPORT CROSSBEAM GOT CORROSION AT FR86 STG R12L. REPLACED THE DAMAGED CROSSBEAM BY NEW ONE IAW SRM 51-40-21. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED MINOR.Apr 12, 2011 · N426FE · Airbus A310203 · Fuselage Main, Floor BeamSDR FDEA201104121446Floorbeam · corrodedUPPER SUPPORT STRUCTURE GOT MINOR CORROSION AT FR86 STG 12R. REMOVED THE CORRODED CROSS BEAM. FABRICATED A NEW CROSS BEAM I.A.W. DRAWING NO.: A53988624201. INSTALLED THE NEW CROSS BEAM FOR REPLACING.Apr 12, 2011 · N426FE · Airbus A310203 · Fuselage Main, Floor BeamSDR FDEA201006272203Autothrottle Sys · malfunctionedON TAKE OFF WITH ONLY NR 2 ATS OPERATIVE, THE NR 2 THROTTLE KEPT TRYING TO ADVANCE TO FIREWALL AFTER 90 KNOTS, EGT WENT UP TO 940, T/0 ABORTED AT 100 KIAS, BRAKES COOLED, AUTOTHROTTLE OFF TAKEOFF ACCOMPLISHED. PERFORMED CROSSLOAD FROM NR 1 FMC. ALSO PERFORJun 27, 2010 · N426FE · Airbus A310 · Auto Throttle SystemSDR 08FDEA04529Sequence Valve · malfunctionedUNSAFE NOSE GEAR INDICATION/MANUAL CRANK DOWN. JACK ADAPTER AND TEST BOX SHIPPED FROM LAX, T/S TO SEQUENCE VALVE AND RT NOSE GEAR ACTUATOR. BOTH REPLACED PER 32-31-16-4 AND 32-31-18-4. OPS AND LEAK CHECKS GOOD PER 32-30-158. ALSO, PERFORMED FREE FALL ACTUOct 24, 2008 · N426FE · Airbus A310203 · Landing Gear Retraction/Extension SystemSDR 08FDEA04286Frame · crackedCENTER FUSELAGE ZONE 12 REINFORCE THE UPPER FRAME BASE TO ARCH STRUCTURE AT FRAME 45 FASTENER HOLE CRACKED ON FR4AME FOOT, RIGHT SIDE. COMPLIED WITH E.A 6-5310-123911.Oct 9, 2008 · N426FE · Airbus A310203 · Wing SparSDR 08FDEA04283Frame · crackedFUSELAGE MAIN FRAME FRAME FOOT 45 RIGHT SIDE ,INSTALL 1ONE CADMIUM PLATED SHOULDERED BUSH MADE OF STAINLESS STEEL 17-4PH REQUESTED BY E.A 6-5310-123911. FABED BUSHING ON MAE TRAVELER T8/761893, INSTALLED PER E.A 6-5310-123911Oct 9, 2008 · N426FE · Airbus A310203 · Wing SparSDR 08FDEA04282Frame · crackedCENTER FUSELAGE ZONE 20 REINFORCE THE UPPER FRAME BASE TO ARCH JUNCTION AT FRAME 44 FASTENER HOLE CRACKED ON FRAME FOOT FITTING. COMPLIED WITH E.A 6-5310-123911.Oct 9, 2008 · N426FE · Airbus A310203 · Wing SparSDR 08FDEA04281Frame · crackedMAIN DECK REINFORCE UPPER FRAME BASE TO ARCHES JUNCTIONS FRAME FOOT 46 LEFT, REWORK HOLES 23, 26, 27 BY E.A 6-5310-123911. REAMED HOLES 23, 26,& 27. TO .433. BUSHINGS FABED ON TRAVELER T8/762882, BUSHINGS INSTALLED IAW E.A 6-5310-123911Oct 9, 2008 · N426FE · Airbus A310203 · Fuselage Main, FrameSDR 08FDEA04175Fitting · crackedCENTER FUSELAGE ZONE 20 - REINFORCE THE UPPER FRAME JUNCTION AT FR 46 LT FASTENERS HOLES CRACKED ON FRAME FOOT FITTING. REMOVED FRAME FOOT IAW SRM 51-40-21. RE-INSTALLED FRAME FOOT PER EA 6-5310-123911 & SRM 51-40-21, INSTALLED BUSHINGS PER EA 6-5310-123911.Oct 2, 2008 · N426FE · Airbus A310203 · Fuselage Main, FrameSDR 08FDEA04138Door Frame · corrodedLEFT AFT PAX DOOR CUTOUT LOWER AFT DOOR STOP FITTING HAS CORROSION UNDER IT. REMOVED AND REPLACED THE LT AFT PAX DOOR CUTOUT AFT FRAME IAW SRM 51-40-21. PREPPED AND PAINTED IAW AMM 51-75-10-8, PERFORMED DOOR STOP ADJUSTMENT CHECK IAW AMM 52-10-11-5 CHECKED GSep 30, 2008 · N426FE · Airbus A310203 · Fuselage Main, StructureSDR 08FDEA04014Skin · gougedLOWER FUSELAGE FWD CARGO DOOR CUTOUT FWD LOWER EDGE BELOW REPAIR DOUBLER HAS SKIN GOUGES 5 INCH LONG. BLENDED AREA FOUND TO BE WITH IN LIMITS IAW SRM 53-10-12, AND 51-73-10 FIG 201. TREATED, PRIMED AND PAINTED IAW SRM 51-21-10, AND MM 51-75-10-8.Sep 24, 2008 · N426FE · Airbus A310203 · Fuselage Main, Plate/SkinSDR 08FDEA04013Skin · damagedLOWER FUSELAGE LT FR 18 TO FR 23 BETWEEN STR 37 AND STR 39 HAS 6 LIGHTNING STRIKES. REWORKED LIGHTNING STRIKES IAW SRM 51-40-21, 51-10-30, AND 51-10-10. TREATED AND PRIMED IAW 51-21-10, PAINTED IAW MM 51-75-10.Sep 24, 2008 · N426FE · Airbus A310203 · Fuselage Main, Plate/SkinSDR 08FDEA03881Angle · crackedVERTICAL STABILIZER FWD RT LOWER CHORD ANGLE HAS A 6.5 INCH CRACK. REMOVED AND REPLACED CHORD ANGLE IAW SRM 51-40-21.Sep 15, 2008 · N426FE · Airbus A310203 · Ventral StructureSDR 08FDEA03863Attach Fitting · crackedMAIN DECK RT SIDE BETWEEN FR 13 AND FR 13 A, ATTACH ANGLE ABOVE GALLEY SIDE FITTING HAS A CRACK. REMOVED AND REPLACED FRAME FITTING BETWEEN FR13 AND 13A IAW SRM 51-40-00 AND 51-40-21.Sep 12, 2008 · N426FE · Airbus A310203 · Fuselage Main, Attach FittingsSDR 08FDEA03853Attach Fitting · corrodedVERT STAB ATTACH FITTING CORROSION L AND R SIDE. COMPLIED WITH EA 6-5536-110931 RII:680053. COMPLIED WITH EA 6-5536-110931.Sep 12, 2008 · N426FE · Airbus A310203 · Vertical Stabilizer, Attach FittingsSDR 08FDEA03759Support Angle · crackedFUSELAGE CENTER SECTION ZONE 240 RT/SIDE EMERGENCY EXIT LOWER JAMB AT FRAME 43,TOP ANGLE SUPPORT HAS CRACK. REMOVED AND INSTALLED NEW SUPPORT ANGLE IAW SRM 51-40-21.Sep 8, 2008 · N426FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR 08FDEA03758Support Angle · crackedFUSELAGE CENTER SECTION ZONE 240 LT/SIDE EMERGENCY EXIT LOWER JAMB, AT FRAME 43 TOP ANGLE SUPPORT HAS CRACK. REMOVED AND INSTALLED NEW SUPPORT ANGLE IAW SRM 51-40-21.Sep 8, 2008 · N426FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR 07FDEA01790Sensor · failedRTO AT 100KTS , NAV ADC 1 FAILURE WITH ASSOCIATED WARNINGS. SWAPPED 1 ANGLE OF ATTACK AND NR 3 ANGLE OF ATTACK, PER AMM 34-11-19-4. PERFORMED ALPHA PROBE TEST AND AFS/ LAND TEST NO FAULT OR FAILURES. PER TSM 22-00-00. R/I FROM FACT SWAP COMPONENT POSITIONMay 15, 2007 · N426FE · Airbus A310203 · Stall Warning SystemSDR 06FDEA03214Symbol Generator · failedON TAKEOFF ROLL, NR 1 EFIS SGU FAILED. BOTH PFD AND ND HAD DIAGONAL LINES ON THE CAPTAINS SIDE "MEL 34-73-01: EFIS SGU (IDENTIFY 2 OR 3) NR 3 INOP." BY LGB MX. SWAPPED NR 1 AND 3. REMOVED AND REPLACED NR 3 EFIS SGU IAW M/M 34-73-34-4. ALL OPS CHECKS NORMASep 6, 2006 · N426FE · Airbus A310203 · Integrated Flight SystemSDR 06FDEA2720Power Cable · faultyPDIS 426 30-40 0008213 28JUL06 MEM, SMOKE IN COCKPIT DUE TO OVERHEAT OF RT WINDOW HEAT COILED POWER CORD. RAM AIR VALVE OPENED AND COURIER 02 MAN OVERRIDE SELECTED ON. COURIER 02 SYSTEM RESET AND RAM AIR DOOR CLOSED. ACN RELEASED FOR SERVICE IAW MEL/CDJul 28, 2006 · N426FE · Airbus A310 · Ice/Rain Protection System WiringSDR 06FDEA1319Repair · misinstalledPREVIOUS REPAIR INSTALLED ON LT ELEVATOR STA 604/ER26 UPPER SURFACE T/E WEDGE UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION. NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. EVALUATED AND FOUND NOT TO CONFORMApr 6, 2006 · N426FE · Airbus A310203 · Trailing Edge FlapsSDR 06FDEA1270Flange · bentCOMPLY WITH AGING 9-AGING-INSP. LOWER FLANGE AFT SIDE BEND FR 60 FR 3249, - Y214. PERFORMED PART 1 OF FEDEX EA 6-5310-97865, NO CRACKS FOUND. EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MINOR.Mar 30, 2006 · N426FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR 06FDEA1249Repair · noneCOMPLY WITH AGING 9-AGING-INSP. PREVIOUS REPAIR INSTALLED AT FUSELAGE ON RT MCD SEAT TRACK BETWEEN FR 62 TO FR 63 FS 3355 TO FS 3408, AT -145. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATMar 28, 2006 · N426FE · Airbus A310203 · Standard Practices/StructuresSDR 06FDEA1248Repair · unknownCOMPLY WITH AGING 9-AGING-INSP. PREVIOUS REPAIR INSTALLED AT FUSELAGE ON RT AFT PIT CROSSBEAM AT FR 65 TO FR 65 FS 3514 TO FS 3514, AND -Y20 UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATIONMar 28, 2006 · N426FE · Airbus A310203 · Standard Practices/StructuresSDR 06FDEA1243Structure · damagedCOMPLY WITH AGING 9-AGING-INSP. PREVIOUS BLEND REPAIR 3 EACH ON RT SIDE NR 2 L/E SLAT TRAILING EDGE UNABLE TO DETERMINE APPROVED REPAIR. DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIRED PEMar 27, 2006 · N426FE · Airbus A310203 · Leading Edge DevicesSDR 06FDEA1182Repair · noneCOMPLY WITH AGING 9-AGING-INSP. PREVIOUS REPAIR INSTALLED ON FWD PIT CROSSBEAM AT FR 25 TO FR 25, FS 1711 TO FS 1711 AND Y72 TO Y72. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APMar 21, 2006 · N426FE · Airbus A310203 · Aircraft StructuresSDR 06FDEA1101Repair · unknownPREVIOUS REPAIR INSTALLED ON RIGHT HAND AFT PIT CROSSBEAM AT FR 64 TO FR 64, FS 3461 TO FS 3461 AND -Y 117. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPLAMar 15, 2006 · N426FE · Airbus A310203 · Standard Practices/StructuresSDR 06FDEA1094Repair · unknownPREVIOUS REPAIR INSTALLED ON RIGHT HAND MCD FLOORBEAM AT FR 12A TO FR 13, FS 1091 TO FS 1125 AND -YC 145.6. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIMar 15, 2006 · N426FE · Airbus A310203 · Standard Practices/StructuresSDR 06FDEA1102Repair · noneCOMPLY WITH AGING 9-AGING-INSP. PREVIOUS REPAIR INSTALLED ON RIGHT HAND AFT PIT CROSSBEAM AT FR 65 TO FR 65, FS 3514 TO FS 3514 AND Y 20. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AMar 15, 2006 · N426FE · Airbus A310203 · Aircraft StructuresSDR 06FDEA1100Repair · noneCOMPLY WITH AGING 9-AGING-INSP. PREVIOUS REPAIR INSTALLED ON RIGHT HAND MCD FLOORBEAM AT FR 37 TO FR 37, FS 2029 TO FS 2029 AND YE 57 TO YD 81. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICAMar 15, 2006 · N426FE · Airbus A310203 · Aircraft StructuresSDR 06FDEA1098Floorbeam · damagedCOMPLY WITH AGING 9-AGING-INSP. PREVIOUS REPAIR INSTALLED ON RIGHT HAND MCD FLOORBEAM AT FR 15A TO FR 16A, FS 1245 TO FS 1267 AND -YB 195.9. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATIOMar 15, 2006 · N426FE · Airbus A310203 · Fuselage Main, Floor BeamSDR 06FDEA1097Floorbeam · damagedCOMPLY WITH AGING 9-AGING-INSP. PREVIOUS REPAIR INSTALLED ON RIGHT HAND MCD FLOORBEAM AT FR 14 TO FR 14C, FS 1204 TO FS 1232 AND YB 195.9. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION Mar 15, 2006 · N426FE · Airbus A310203 · Fuselage Main, Floor BeamSDR 06FDEA1095Repair · noneCOMPLY WITH AGING 9-AGING-INSP. PREVIOUS REPAIR INSTALLED ON RIGHT HAND MCD FLOORBEAM AT FR 12A TO FR 13, FS 1091 TO FS 1128 AND YD 95.3. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AMar 15, 2006 · N426FE · Airbus A310203 · Aircraft StructuresSDR 06FDEA1093Repair · noneCOMPLY WITH AGING 9-AGING-INSP. PREVIOUS REPAIR INSTALLED ON LEFT HAND MCD SEAT TRACK AT FR 54.3 TO FR 55/58, FS 3090 TO FS 3143, AT - YD95.3. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATMar 15, 2006 · N426FE · Airbus A310203 · Aircraft Structures
Back to N426FE, cancelled Jun 28, 2024