N429FE, cancelled Mar 2, 2024

Service difficulty reports · 75

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 = 'N429FE' AND deregistration_id = 'N429FE-2024-03-02'
  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 FDEA201510293405Gearbox · lack of lubeSELECTED FLAPS 15 DEGREES AT 200 KTS. FLAPS SYS 1 & 2 FAULT LIGHTS & ON ECAM. CYCLED HANDLE WITH SAME RESULT. FOLLOWED ECAM & QRH. LANDED SLATS 30, FLAPS 0 UNEVENTFULLY & CANCELLED EMERGENCY. LUBED & SERVICED RT ANGLE GEARBOX, TORGUE LIMITER & NR 1 GEARBOOct 29, 2015 · N429FE · Airbus A310203 · Trailing Edge Flap Control SystemSDR FDEA201509042800Sensor · failedAUTO THROTTLES OFF, SET N1 TO 107% ON BOTH ENGS. THERE WAS SIGNIFICANT THRUST DIFFERENCE CAUSING YAW ON CLIMB OUT. WE GOT ECAM ENG EXCEEDENCE WARNING & REDUCED POWER. NOTICED N1 ANALOG & DIGITAL INDICATIONS DISAGREED SIGNIFICANTLY. ON ATB MANUAL THROTTLES Sep 4, 2015 · N429FE · Airbus A310203 · Auto Throttle SystemSDR FDEA201404260861Pressure Switch · malfunctionedON APPROACH WHEN WE SELECTED, SLATS EXT, GOT ECAM SLATS SYS NR 1 & NR 2 FAULT. CYCLED & SLATS EXTENDED, WHEN SELECTING FLAPS 15, GOT FLAP SYS NR 1 & NR 2 FAULT. CYCLED WITH NO HELP. LANDED WITH 0 FLAPS. CYCLED FLAPS SEVERAL TIMES WITH NO HELP. TROUBLESHOApr 26, 2014 · N429FE · Airbus A310203 · Trailing Edge Flap Control SystemSDR FDEA201402110305Relay · burnedFIRST OFFICER`S TAT PROBE, FAULT LIGHT ON AT FL300, ECAM MONITOR. 5 MINS LATER SMELL OF ELEC ORIGIN, NO VISUAL SMOKE, ODOR GONE AFTER LANDING. FOUND DET SENSOR TEMP IN 107 VU PANEL WITH BURN HOLE IN TOP OF RELAY. WHILE CHANGING RELAY DET BASE SCREWS FELL OFFeb 11, 2014 · N429FE · Airbus A310 · Pitot/Static Anti-Ice SystemSDR FDEA201311102720Tee Fitting · crackedCENTER WING REAR SPAR INTERNAL ANGLE LOWER SKIN TEE FITTING RT SIDE FOUND CRACKED. REPAIRED IAW EA 6-5710-T0303521.Nov 10, 2013 · N429FE · Airbus A310203 · Fuselage Main, Attach FittingsSDR FDEA201311102719Tee Fitting · crackedCENTER WING REAR SPAR INTERNAL ANGLE LOWER SKIN TEE FITTING LEFT FOUND CRACKED. REPAIRED IAW EA 6-5710-T0303521.Nov 10, 2013 · N429FE · Airbus A310203 · Fuselage Main, FrameSDR FDEA201311052688Fitting · crackedFRAME 40 RT UPPER CORNER FITTING FOUND CRACKED. COMPLIED WITH EA 6-5710-0303103.Nov 5, 2013 · N429FE · Airbus A310203 · Fuselage Main, Attach FittingsSDR FDEA201311052687Fitting · crackedFRAME 40 LT UPPER CORNER FITTING FOUND CRACKED. COMPLIED WITH EA 6-5710-T0303103.Nov 5, 2013 · N429FE · Airbus A310203 · Fuselage Main, Attach FittingsSDR FDEA201311052686Fitting · crackedFUSELAGE CENTER BOX FRAME 45 RT UPPER FRAME BASE-TO-ARCH JUNCTION FOUND CRACK AT HOLE H22 COMPLIED WITH EA 6-5310-T0303124.Nov 5, 2013 · N429FE · Airbus A310203 · Fuselage Main, Attach FittingsSDR FDEA201311052685Fitting · crackedFUSELAGE CENTER BOX FRAME 44 RT UPPER FRAME BASE-TO-ARCH JUNCTION FOUND CRACKS AT H5 & H13. R & R THE SUPPORT FITTING IAW SRM 51-40-21 & EA 6-5310-T0303124.Nov 5, 2013 · N429FE · Airbus A310203 · Fuselage Main, Attach FittingsSDR FDEA201311052684Fitting · crackedFUSELAGE CENTER BOX FRAME 43 RT UPPER FRAME BASE-TO-ARCH JUNCTION FOUND CRACK AT HOLE H2. R & R NEW SUPPORT FITTING IAW SRM 51-40-21 & EA 6-5310-T0303124.Nov 5, 2013 · N429FE · Airbus A310203 · Fuselage Main, Attach FittingsSDR FDEA201311052683Fitting · crackedFUSELAGE CENTER BOX FRAME 45, LT UPPER FRAME BASE-TO-ARCH JUNCTION FOUND CRACK AT HOLE H22 COMPLIED WITH EA 6-5310-T0303124.Nov 5, 2013 · N429FE · Airbus A310203 · Fuselage Main, Attach FittingsSDR FDEA201311042676Fitting · crackedFUSELAGE CENTER BOX FRAME 43, LT UPPER FRAME BASE-TO-ARCH JUNCTION FOUND CRACKED. R & R SUPPORT FITTING SRM 51-40-21 & EA 6-5310-T0303124.Nov 4, 2013 · N429FE · Airbus A310203 · Fuselage Main, StructureSDR FDEA201311042677Support Fitting · crackedFUSELAGE CENTER BOX, FRAME 44 LT UPPER FRAME SUPPORT FITTING FOUND CRACKED. R & R NEW SUPPORT FITTING IAW SRM 51-40-21 & EA 6-5310-T0303124.Nov 4, 2013 · N429FE · Airbus A310203 · Fuselage Main, Attach FittingsSDR FDEA201310312659Skin · crackedFUSELAGE SKIN UNDER PICKUP ANGLE AT FRAME 40 LT, FASTER HOLE 14 FOUND CRACKED. REPAIRED IAW EA 6-5310-T0303309.Oct 31, 2013 · N429FE · Airbus A310203 · Fuselage Main, Plate/SkinSDR FDEA201310202557Seat Track · corrodedMAIN DECK FRAMES 47-48 -Y953, SEAT TRACK CORRODED. SPLICE REPAIRED SEAT TRACK IAW EA 6-5315-T0303255 & SRM 53-10-16.Oct 20, 2013 · N429FE · Airbus A310203 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201310182549Floor Support · corrodedMAIN DECK FR 12A-14 Y770, FLOOR SUPPORT CORRODED REPLACED THE CORRODED FLOOR SUPPORT IAW SRM 51-40-21.Oct 18, 2013 · N429FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR FDEA201212134295Warning Light · false activationAPPROX 10 MINUTES INTO FLIGHT, ECAM "HYD GREEN RSVR LO LEVEL" QUANTITY INDICATED. TURNED PUMPS OFF IAW ECAM. FOLLOWED QRH PROCEDURES TO EXTEND LANDING GEAR. LANDING UNEVENTFUL. CLEANED WHEEL WELL AND SERVICED GREEN SYS. HYD TO MIDDLE OF THE HAT AMM 12-12-Dec 13, 2012 · N429FE · Airbus A310203 · Hydraulic System, MainSDR FDEA201207152579Skin · crackedLT WING FIXED L/E INBD CUT OUT FOR SHUTTER DOOR NR 1 TOP EXTERNAL SKIN CRACKED 1.25" APPROXIMATELY. REPAIRED SKIN IAW SRM 51-40-21 DWGS A57246236, A57246240 AND EA 6-5740.Jul 15, 2012 · N429FE · Airbus A310203 · Wing, Plate/SkinSDR FDEA201108253484Skin · crackedEVIDENCE OF FUSELAGE SKIN CRACK UNDER LAV SERVICE DOOR. REPAIRED IAW RDAS ISSUE A AND EA 6-5330-154038 PARTS 1 AND 2.Aug 25, 2011 · N429FE · Airbus A310203 · Fuselage Main, Plate/SkinSDR FDEA201106032104Fitting · crackedTWO LOWER HOLES WERE FOUND INDICATION AT LT & RT SIDE OF FR43A. REMOVED LT AND RT FRAME FITTINGS. OVERSIZED LT RIB LOWER HOLE TO 0.402" DIA. PERFORMED NDI INSPECTION ON ALL SEPERATED STRUCTURE AND FOUND THE CRACK IS ONLY ON THE FRAME FITTING. FABRICATED CRJun 3, 2011 · N429FE · Airbus A310203 · Fuselage Main, Attach FittingsSDR FDEA201106022095Angle · crackedANGLE FOUND CRACKED. REMOVED ANGLE, OVERSIZED HOLES TO 0.199". PERFORMED NDI INSPECTION ON ALL SEPERATED STRUCTURE AND FOUND CRACK ONLY ON ANGLE. FABRICATED ANGLE PER DRAWING A53812589200. INSTALLED ANGLE IAW SRM 51-40-21. THE REPAIR CLASSIFIED AS MAJORJun 2, 2011 · N429FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR FDEA201106012072Tube · crackedMAIN DECK COMPT LT LOWER SIDEWALL AREA FOUND SMOKE DETECTOR SNIFFER TUBE BROKEN AT 2EA PLACES, LOCATION BETWEEN FR 40/41 AND FR 45. IAW AMM 26-19-09 REOVED THE SNIFFER TUBE AT FR 40/41 LT. COMPLIED WITH E.A. 6-2610-149004. REPAIR CLASSIFIED AS MINOR PER GMJun 1, 2011 · N429FE · Airbus A310203 · Smoke DetectionSDR FDEA201106012073Floorbeam · crackedCENTER MAIN DECK COMPARTMENT FLOOR AREA BETWEEN R2 AND R3 SEAT TRACK FOUND 5 EA CROSSBEAM ASSY CRACKED AREA FROM FR40/411 TO FR45/-Y450 AND -Y953. R & R CENTER MAIN DECK SOMPARTMENT FR40 / 41 TO FR45 / -Y953 5 EA CROSS BEAMS IAW AMM20-21-12. THE REPAIR CLASJun 1, 2011 · N429FE · Airbus A310203 · Fuselage Main, Floor BeamSDR FDEA201105302029Panel · debonded1EA DISBONDED AREA (2" X 3") WAS FOUND AT 321AL PANEL R/H SIDE. ( 14" FROM LEADING EDGE AND 20" FROM BOTTOM EDGE.) CLEANED & EVALUATED THE DISBONDED AREA 3"X2.5". REINFORCED REPAIR THE AREA WITH THE RESIN COMPOUND AND FIBERGLASS CLOTH REFER TO A310 SRM 55-May 30, 2011 · N429FE · Airbus A310203 · Vertical Stabilizer, Plate/SkinSDR FDEA201105302028Panel · debonded1EA DISBONDED ARE WAS FOUND AT LT SIDE INTERIOR ARE (11" X 17") OF 324AT PANEL. ( 1.9" FROM LEADING EDGE AND 1.5" FROM BOTTOM EDGE.) CLEANED & EVALUATED THE DISBONDED AREA 11" X 17". REINFORCED REPAIR THE AREA WITH THE RESIN COMPOUND AND FIBERGLASS CLOTH IAWMay 30, 2011 · N429FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR FDEA201105302027Panel · debonded1EA DISBONDED AREA (2.5" X 1.8") WAS FOUND AT 322BL PANEL L/H SIDE. (6" FROM LEADING EDGE, 27" FROM BOTTOM EDGE.) CLEANED & EVALUATED THE DIMENSION OF THE DISBONDED AREA 9" X 8.5". REINFORCED REPAIR THE AREA WITH THE RESIN COMPOUND AND FIBERGLASS CLOTH REFMay 30, 2011 · N429FE · Airbus A310203 · Vertical Stabilizer, Plate/SkinSDR FDEA201105302030Floor Panel · crackedCARGO COMPARTMENT 162HF FLOOR PANEL GOT IMPACT DAMAGED. FABRICATED A NEW FLOOR PANEL FOR REPLACING IAW DRAWING 17A53279962 & SRM 53-10-20 AND MCG IRM 9701 REVISION G.May 30, 2011 · N429FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201105251978Rib · crackedREMOVE HINGE SUPPORT RIB, FOUND ANOTHER SIDE RIB MATING SURFACE GOT CRACK AT RIB 20, 19 INCH. REMOVED THE CRACKED BOX RIB IAW SRM 51-40-21. FABRICATED RIB MATERIAL 7075-T7651 IAW DWG A57247040. TRANSFERED DRILL THE FASTENER'S HOLE AND ASSEMBLED RIB IAW SRM 5May 25, 2011 · N429FE · Airbus A310203 · Wing, Rib/BulkheadSDR FDEA201105251980Duct · chafedENG 2, LT T/R COWL INNER DUCT AFT EDGE GOT CHAFING ATTACH TO CORE COWL AREA UPPER SIDE.May 25, 2011 · N429FE · Airbus A310203 · Engine Thrust ReverserSDR FDEA201105221929Rib · crackedLT WING T/E BOX RIB LOWER CORNER BOTH SIDE GOT CRACKS BETWEEN NR 5 AND NR 6 SPOILER. REMOVED THE CRACKED BOX RIBS IAW SRM 51-40-21. REPLACED THE RIBS WITH NEW PARTS BY FASTENERS IAW SRM 51-72-10 AND 51-40-21. THE REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.May 22, 2011 · N429FE · Airbus A310203 · Wing, Rib/BulkheadSDR FDEA201105181861Skin · corrodedFWD CARGO COMPARTMENT BILGE SKIN AREA AROUND MAIN HOLE SKIN GOT CORROSION BETWEEN FR38.1 AND FR38.2 POSITION. REMOVED THE CORROSION AREA. MEASURED THE DIMENSION 2.5"L X 2.2"W X 0.078"D OVER LIMIT REF. TO SRM 53-14-12. REPAIRED THE DAMAGE AREA WITH DOUBLER ANDMay 18, 2011 · N429FE · Airbus A310203 · Fuselage Main, Plate/SkinSDR FDEA201105121806Rib · crackedRIGHT WING NR 5 SPOILER O/B HINGE SUPPORT RIB CRACKED. REMOVED CRACKED BOX RIB IAW SRM 51-40-21. FABRICATED RIB IAW DWG A57247040. TRANSFERRED HOLES AND ASSEMBLED RIB IAW SRM 51-40-21. WET INSTALLED SUPPORT RIB IAW A310 SRM 51-40-21 AND 51-72-10. THE REPAIMay 12, 2011 · N429FE · Airbus A310203 · Wing, Rib/BulkheadSDR FDEA201105091781Wedge · damagedRT WING T/E INBD FLAP T/E DAMAGED ABOUT 5" X 20" BETWEEN RIB 18 AND 21. REMOVED FLAP T/E WEDGE. REPLACED WITH NEW T/E WEDGE PER E.A. 6-5750-149005. 3. PAINT TOUCHED-UP. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.May 9, 2011 · N429FE · Airbus A310203 · Trailing Edge FlapsSDR FDEA201105061766Fitting · crackedFWD CARGO COMPARTMENT DOOR SILL AREA FITTING CRACKED ABOVE NR 6 LATCH FITTING. REMOVED THE CRACKED FITTING. INSTALLED THE NEW FITTING FOR REPLACING IAW SRM 51-72-10.May 6, 2011 · N429FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR FDEA201105061767Seat Track · chafedAFT MAIN DECK COMPARTMENT FOUND L4 LONGITUDINAL SEAT TRACK FLANGE GOT A EXCESS CHAFED MARK LOCATION AT FR79 AND Y1447.8 POSITION. REMOVED THE DAMAGE SEAT TRACK. FABRICATED NEW SEAT TRACK REF. TO DRAWING NR A53279232. INSTALLED NEW TRACK WITH FASTENER REF. TMay 6, 2011 · N429FE · Airbus A310203 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200910273682Slat System · failed2 ND REPEAT: ON APPROACH SLATS WOULD NOT EXTEND (STUCK), RAN QRH AND LANDED WITH 0/40 SLATS FLAPS W/OUT INCIDENT. LANDED AT ABOUT 140 KIAS. SFCC'S 1 & 2 INDICATE JAM. NO OTHER FAULTS. EVIDENCE OF LEAK AT INBD SLAT JACKSCREW. EXTENDED SLATS WITHOUT FAULTS ANOct 27, 2009 · N429FE · Airbus A310203 · Leading Edge Slat Control SystemSDR FDEA200910233685Slat System · stuckON APPROACH, SLATS WOULD NOT EXTEND (STUCK), RAN QRH AND LANDED WITH 0/40 SLATS FLAPS W/OUT INCIDENT. LANDED AT ABOUT 140 KIAS. MOCC UPDATE SFCC'S 1 AND 2 INDICATE JAM. NO OTHER FAULTS. EVIDENCE OF LEAK AT INBD SLAT JACKSCREW. EXTENDED SLATS WITHOUT FAULTOct 23, 2009 · N429FE · Airbus A310203 · Leading Edge Slat Control SystemSDR FDEA200910233684Slat System · stuckON APPROACH, SLATS WOULD NOT EXTEND (STUCK), RAN QRH AND LANDED WITH 0/40 SLATS FLAPS W/OUT INCIDENT. LANDED AT ABOUT 140 KIAS. SFCC'S 1 AND 2 INDICATE JAM. NO OTHER FAULTS. EVIDENCE OF LEAK AT INBD SLAT JACKSCREW. EXTENDED SLATS WITHOUT FAULTS AND FOUND Oct 23, 2009 · N429FE · Airbus A310203 · Leading Edge Slat Control SystemSDR FDEA200910233683Slat System · failed2 ND REPEAT: ON APPROACH SLATS WOULD NOT EXTEND (STUCK), RAN QRH AND LANDED WITH 0/40 SLATS FLAPS W/OUT INCIDENT. LANDED AT ABOUT 140 KIAS. SFCC'S 1 & 2 INDICATE JAM. NO OTHER FAULTS. EVIDENCE OF LEAK AT INBD SLAT JACKSCREW. EXTENDED SLATS WITHOUT FAULTS ANOct 23, 2009 · N429FE · Airbus A310203 · Leading Edge Slat Control SystemSDR FDEA200910233681Limiter · failed2 ND REPEAT: ON APPROACH SLATS WOULD NOT EXTEND (STUCK), RAN QRH AND LANDED WITH 0/40 SLATS FLAPS W/OUT INCIDENT. LANDED AT ABOUT 140 KIAS. SFCC'S 1 & 2 INDICATE JAM. NO OTHER FAULTS. EVIDENCE OF LEAK AT INBD SLAT JACKSCREW. EXTENDED SLATS WITHOUT FAULTS ANOct 23, 2009 · N429FE · Airbus A310203 · Leading Edge Slat Control SystemSDR FDEA200910223680Jackscrew · lack of lubeSLATS SYS 1 & 2 FAULTED ON APPROACH, RECYCLED, LANDED SLATS 0/FLAPS 40. NO FAULTS ON SFCC NR 1 OR 2, RAN END ENGINE'S OPS. CHK SLATS 0 TO 30 THREE TIMES NO FAULTS NOTED. FOUND BOTH SYSTEM TORQUE LIMITERS ACTIVATED. RESET SAME. IAW TSM 27-80-02 BEGAN CHECKINGOct 22, 2009 · N429FE · Airbus A310203 · Leading Edge Slat Control SystemSDR FDEA200910223679Slat System · faultedSLATS FAULTED SYSTEMS 1 & 2 ON APPROACH CYCLED PER QRH NO HELP RAN QRH AND LANDED SLATS 0 FLAPS 40 T/S PER TSM 27-80-00 NO HARD FAULTS NOTED. RAN NR 1 & 2 ENGINES PER JRH CH 5. CYCLED FLAPS & SLATS SEVERAL TIMES. ALL INDICATIONS NORMAL. NO FAULTS NOTED OOct 22, 2009 · N429FE · Airbus A310203 · Leading Edge Slat Control SystemSDR FDEA200905241776Heater · smokeSMOKE/FUMES FROM BEHIND F/O SLIDING WINDOW. SECURED R WINDOW HEAT. SMOKE/FUMES STOPPED. FOUND WIRES AT COPILOTS SLIDING WINDOW BURNED AND MELTED WHERE WIRES ENTER BETWEEN THE WINDOW AND THE WINDOW MECHANISM COVER. PARTS REQUIRED ARE CLAMP P/N NSA5516-09V May 24, 2009 · N429FE · Airbus A310203 · Windshield/Door Rain/Ice RemovalSDR FDEA200905241775Coalescer Bag · dirtyFAINT SMELL OF ELECTRICAL FUMES. TRANSIENT THEN DISSIPATED. RAN PACKS WITH APU AIR AND NOTICED SLIGHT INDUSTRIAL KIND OF SMELL. CONTINUING T/S. REMOVED BOTH COALESCER BAGS AND FOUND VERY DIRTY. REPLACED PER MM 21-51-16-3. OPERATED BOTH ENGINES PER JRH (May 24, 2009 · N429FE · Airbus A310203 · Humidity Control SystemSDR FDEA200902060466Uplock · failedAFTER TAKE OFF NOSE GEAR DOOR AMBER LIGHT REMAINED ILLUMINATED. NOSE GEAR DOOR NOT CLOSED ECAM. HEAVY BUFFET AND VIBRATION. SPEED NEVER EXCEEDED 210 KTS. RETURN TO MKE. UPLOCK FOUND BROKEN SPRINGS IN NOSE GEAR DOOR UPLOCK ASSY, WHICH WOULD NOT ALLOW DOOR Feb 6, 2009 · N429FE · Airbus A310203 · Landing Gear Door Retract SectionSDR FDEA200901090106Filter · dirtyNR 2 ENG FUEL FILTER CLOG LIGHT & ECAM INDICATION ON CLIMB-OUT PASSING 2000 FT. POWER REDUCED & ECAM INDICATIONS WENT AWAY. TRIED ADVANCING THROTTLE AGAIN & ECAM INDICATIONS BACK ON. REMOVED & INSPECTED NR 2 ENGINE FUEL FILTER FOR CONTAMINATION. FOUND SMJan 9, 2009 · N429FE · Airbus A310203 · Engine Fuel DistributionSDR FDEA200812135137Door Frame · corrodedL1 DOOR LT UPPER FWD FAIL/SAFE RING RADIUS BOTH LAYERS SHOW EXFOLIATION CORROSION INDICATIONS AFTER EDDY CURRENT INSPECTION, UNABLE TO VERIFY ULTRASONICALLY 1 SQ INCH AREA. REMOVED LEVEL 1 CORROSION AND REPAIRED DAMAGED AREA AT L-1 DOOR UPPER FWD CORNER FDec 13, 2008 · N429FE · Airbus A310203 · Fuselage Main, StructureSDR FDEA200812065100Fitting · gougedAFT CARGO DOOR NR 2 DOOR LOCK FITTING HAS 1 GOUGE ON OTBD MOUNT AND 2 GOUGES ON INBD MOUNT REMOVED AND REPLACED AFT CARGO DOOR FITTING AT FR 60A IAW A310 SRM 51-40-21.Dec 6, 2008 · N429FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR FDEA200812065099Web · corrodedFRAME 1 FWD FACE AT RADOME ACCESS HAS 4 EA AREAS OF SKIN CORROSION, APPROX 7 SQ INCHES REMOVED LEVEL 1 CORROSION AND INSTALLED REPAIR DOUBLER ON WEB FLANGE AT FRAME 1 IAW FEDEX EA 6-5310-124171, RELEASE DATE 12 NOVEMBER, 2008.Dec 6, 2008 · N429FE · Airbus A310203 · Fuselage Miscellaneous Structure
Back to N429FE, cancelled Mar 2, 2024