# Service difficulty reports: N454FE

A list on [N454FE](https://openairdocs.org/aircraft/N454FE.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 2 · 57 reports

- [SDR FDEA201412184149](https://openairdocs.org/sdr/FDEA201412184149.md): Panel · damaged · Dec 18, 2014 · N454FE · Airbus A310222 · Wing Main, Frame Structure
  > ON ARRIVAL LT WING TE DAMAGE FOUND. R & R THE LT WING OTBD TE PANEL IAW SRM 57-51-12.
- [SDR FDEA201312243034](https://openairdocs.org/sdr/FDEA201312243034.md): Plate · worn · Dec 24, 2013 · N454FE · Airbus A310222 · Engine Thrust Reverser
  > NR 2 ENG OTBD T/R COWL UPPER MID-SECTION INNER FACE FOUND ONE EACH PLATE WORN BY SPRING SEAL. ACCOMPLISHED THE WORK IAW EA 6-5410-T0208220.
- [SDR FDEA201312243033](https://openairdocs.org/sdr/FDEA201312243033.md): Frame · corroded · Dec 24, 2013 · N454FE · Airbus A310222 · Fuselage Main, Frame
  > FORWARD CARGO COMPARTMENT BILGE FRAME FOUND CORROSION AT FR 39, STRINGER 51R POSITION. CORROSION AREA CUT OUT & REINFORCED WITH REPAIR PART & FITTING TO INSTALLED IAW SRM 53-15-17. THE REPAIR CATEGORY B IAW 53-15-17-2-003-00.
- [SDR FDEA201211103930](https://openairdocs.org/sdr/FDEA201211103930.md): Windshield · cracked · Nov 10, 2012 · N454FE · Airbus A310222 · Flight Compartment Windows
  > IN CRUISE FL340, CAPTAIN'S WINDOW CRACKED IN TWO PLACES. CAPTAINS WINDOW HEAT FAULTED SHORTLY AFTER CRACK APPEARED. TURNED OFF WINDOW HEAT, NO FURTHER CRACKING. R & R CAPTAIN'S WINDSHIELD IAW MM 56-11-11-04.
- [SDR FDEA201208092925](https://openairdocs.org/sdr/FDEA201208092925.md): Hinge Fitting · gouged · Aug 9, 2012 · N454FE · Airbus A310222 · Fuselage, Landing Gear Attach Fittings
  > RIGHT NLG AFT DOOR UPPER FWD HINGE FITTING HAS.2500" X.5" GOUGE FROM CONTACT WITH DOOR CONTROL ROD (ON AFT FACE OF HINGE FITTING) R & R RT NLG AFT DOOR UPPER FWD HINGE FITTING IAW SRM 51-72-10. REMOVED AND REINSTALLED FLOOR PANEL 122 PF IAW AMM 53-10-27-04.
- [SDR FDEA201208092923](https://openairdocs.org/sdr/FDEA201208092923.md): Hinge Fitting · gouged · Aug 9, 2012 · N454FE · Airbus A310222 · Fuselage, Landing Gear Attach Fittings
  > LT NLG AFT DOOR UPPER FWD HINGE FITTING HAS.2500" X.5" GOUGE FROM CONTACT WITH DOOR CONTROL ROD (ON AFT FACE OF HINGE FITTING) R & R LT NLG AFT DOOR UPPER FWD HINGE FITTING IAW A310 SRM 51-72-10. REMOVED AND REINSTALLED FLOOR PANEL 121PF IAW A310-200 AMM 53
- [SDR FDEA201205302015](https://openairdocs.org/sdr/FDEA201205302015.md): Pressure Switch · failed · May 30, 2012 · N454FE · Airbus A310222 · Engine Fuel/Oil Cooler
  > NR 2 FUEL FLITER CLOG WOULD NOT GO AWAY AFTER QRH PROCEDURE. FOLLOWED ECAM AND QRH. DECLARED PRECAUTIONARY EMERGENCY. NR 2 ENG REMAINED AT IDLE REMAINDER OF FLIGHT. REF TSM 73-30-10, AMM 73-34-00-00, AMM 73-34-11-04, AND AMM 73-12-03-04: FOUND LIGHT STAYE
- [SDR FDEA201202130564](https://openairdocs.org/sdr/FDEA201202130564.md): Coupling · leaking · Feb 13, 2012 · N454FE · Airbus A310222 · Hydraulic System, Main
  > AFTER STARTING THE ENGINES DURING PUSHBACK THE COCKPIT FILLED WITH A LIGHT SMOKE WITH EYES AND THROAT BURNING. THERE WERE NO COCKPIT INDICATIONS OF ANY FIRE OR SMOKE. SMOKE STARTED TO DISSAPATE QUICKLY, DONNED OXYGEN MASKS. FOUND HYDRAULIC FLUID PUDDLED A
- [SDR FDEA201112215409](https://openairdocs.org/sdr/FDEA201112215409.md): Line · leaking · Dec 21, 2011 · N454FE · Airbus A310222 · Hydraulic System, Main
  > BLUE SYS HYD QUANTITY DECREASED IN FLIGHT SLOWLY UNTIL REACHED LO LEVEL WARNING, SECURED PUMP IAW ECAM AND QUANTITY STOPPED DECREASING, PRESSURE REMAINED ABOVE 3000 PSI UNTIL PUMP TURNED OFF. FOUND RETURN LINE TO BLUE MANIFOLD INSTALLATION SERVO CONTROL AC
- [SDR FDEA201111305082](https://openairdocs.org/sdr/FDEA201111305082.md): Signal Cond Unit · failed · Nov 30, 2011 · N454FE · Airbus A310222 · Engine Oil Pressure
  > DURING T/O AT TYS AT 90 KNOTS - ECAM AND ENG 1 LIGHT - OIL HI PRESS - ILLUMINATED. CREW REJECTED T/O - LIGHT WENT OUT IMMEDIATLY. COMPLETED RTO CK LIST & QRH FOR OIL HI PRESS (NR 1 ENG) - ALL INDICATIONS WERE NORMAL. ALLOWED BRAKES TO COOL - THEN RAN UP E
- [SDR FDEA201106162300](https://openairdocs.org/sdr/FDEA201106162300.md): Skin · delaminated · Jun 16, 2011 · N454FE · Airbus A310222 · Elevator, Plate/Skin
  > AFTER SKIN REMOVED FOR REPAIR, FOUND FURTHER DELAMINATION APPROX. 8 SQ". REPAIRED RT ELEVATOR LOWER SURFACE EXISTING REPAIR DELAMINATED IAW SRM 55-21-11 PAR.5J PGS 257-262 AT RIB -14.
- [SDR FDEA201106162297](https://openairdocs.org/sdr/FDEA201106162297.md): Bracket · damaged · Jun 16, 2011 · N454FE · Airbus A310222 · Nacelle/Pylon, Attach Fittings
  > NR 1 ENGINE, NR 2 HYD SUCTION LINE HAS EXCESSIVE PLAY AT WING ATTACH POINT INSIDE NR 1 PYLON. LEFT WING, REWORKED HOLES 1,2,3,AND 4. R & R SUPPORT BRACKET BUSHING. REPAIR HOLES AND INSTALLED, NDT SKIN AND HOLES FOR CRACKS, NO CRACKS FOUND IAW EA 6-5720-14561
- [SDR FDEA201106162296](https://openairdocs.org/sdr/FDEA201106162296.md): Skin · chafed · Jun 16, 2011 · N454FE · Airbus A310222 · Wing, Plate/Skin
  > RIGHT WING AFT SPAR ABOVE PYLON HYD LINE JAM NUT, LOOSE. REWORKED OVERSIZE HOLE IAW E-5720-145615. REWORKED AND INSTALLED NEW SUPPORT BRACKET BUSHING. REPAIRED HOLE IN BOTTOM WING SKIN IAW EA 6-5720-145615, NDT NR 2 PYLON SKIN AND HOLES FOR CRACKS-NO CRACK F
- [SDR FDEA201106162295](https://openairdocs.org/sdr/FDEA201106162295.md): Skin · corroded · Jun 16, 2011 · N454FE · Airbus A310222 · Wing, Plate/Skin
  > LEFT WING TOP SKIN HAS CORROSION AT REAR SPAR FASTENER, 6" OTBD OF RIB-4. LT WING CORROSION REMOVED BY BLENDING, NDT INSPECTED (NIL FINDINGS), NEW OVERSIZE TAPERLOCK FASTENERS INSTALLED AND SURFACE PROTECTION RESTORED. REF EA 6-5730- 145610.
- [SDR FDEA201105031744](https://openairdocs.org/sdr/FDEA201105031744.md): Skin · delaminated · May 3, 2011 · N454FE · Airbus A310222 · Elevator, Plate/Skin
  > AFTER SKIN REMOVAL FOR REPAIR, FOUND FURTHER DELAMINATION APPROX 8 SQ IN. REPAIRED RT ELEVATOR LOWER SURFACE IAW SRM 55-21-11, PAR 5J, PGS 257-262 AT RIB 14 AND EA 6-5520-145618.
- [SDR FDEA201105031745](https://openairdocs.org/sdr/FDEA201105031745.md): Skin · corroded · May 3, 2011 · N454FE · Airbus A310222 · Elevator, Plate/Skin
  > LT ELEVATOR LOWER SURFACE AT RIB 9 HAS 6 SQ IN TOTAL AREA OF CORROSION. REPAIRED LT ELEVATOR LOWER SURFACE AT RIB 9 IAW SRM 55-21-11, PARA I, PGS 247-252 REF EA 6-5520-145621.
- [SDR FDEA201105031743](https://openairdocs.org/sdr/FDEA201105031743.md): Skin · corroded · May 3, 2011 · N454FE · Airbus A310222 · Elevator, Plate/Skin
  > RT ELEVATOR UPPER SURFACE AT RIB 17 HAS 2 SQ IN OF CORROSION. REMOVED LEVEL 1 CORROSION. REPAIRED RT ELEVATOR UPPER SURFACE IAW SRM 55-21-11, PARA 5L PAGES 257-262. AND REFERENCE E.A. 6-5520-145618.
- [SDR FDEA201105031742](https://openairdocs.org/sdr/FDEA201105031742.md): Skin · corroded · May 3, 2011 · N454FE · Airbus A310222 · Elevator, Plate/Skin
  > RT ELEVATOR LOWER SURFACE OTBD OF RIB 14 HAS 4 SQ IN OF CORROSION. REMOVED LEVEL 1 CORROSION. REPAIRED RIGHT HAND ELEVATOR LOWER SURFACE IAW SRM 55-21-11,PARA 5I, DOUBLER REPAIR AT RIB 14 OF ELEVATOR. REFERENCE E.A. 6- 5520-145618.
- [SDR FDEA201105031741](https://openairdocs.org/sdr/FDEA201105031741.md): Skin · corroded · May 3, 2011 · N454FE · Airbus A310222 · Elevator, Plate/Skin
  > LOWER SURFACE LT ELEVATOR AT RIB 96 SQ IN CORROSION.
- [SDR FDEA200903241027](https://openairdocs.org/sdr/FDEA200903241027.md): Transmitter · malfunctioned · Mar 24, 2009 · N454FE · Airbus A310222 · Engine Oil Indicating System
  > ENG 1 AFTER START, AMBER ECAM HIGH OIL PRESSURE IND (64PSI), MOMENTARILY ON TAKEOFF ROLL AMBER ECAM-HIGH OIL PRESSURE, RTO. HIGH OIL PRESS (64PSI). LOWER OIL PRESSURE NR 1 (90C). REPLACED NR 1 ENG OIL PRESSURE TRANSMITTER PER MM 79-33-11-04 AND NR 1 FWC PER
- [SDR FDEA200903241026](https://openairdocs.org/sdr/FDEA200903241026.md): Computer · malfunctioned · Mar 24, 2009 · N454FE · Airbus A310222 · Engine Oil Indicating System
  > ENG 1 AFTER START, AMBER ECAM HI OIL PRESSURE IND (64 PSI), MOMENTARILY ON TAKEOFF ROLL AMBER ECAM-HI OIL PRESSURE, RTO. HI OIL PRESS (64PSI). LOWER OIL PRESSURE NR 1 (90C) REPLACED NR 1ENG OIL PRESSURE TRANSMITTER PER MM 79-33-11-04 AND NR 1FWC PER MM31-53
- [SDR FDEA200903220999](https://openairdocs.org/sdr/FDEA200903220999.md): Signal Cond Unit · malfunctioned · Mar 22, 2009 · N454FE · Airbus A310222 · Engine Oil Temperature
  > REJECTED TAKEOFF. NR 1 ENGINE HIGH OIL PRESSURE WARNING LIGHT ILLUMINATED ON TAKEOFF ROLL APPROXIMATELY 85KTS. INDICATION DEFERRED PER MEL 79-33-01-02. REMOVED AND REPLACED NR 1 ENG OIL SIGNAL CONDITIONER P ER MM 79-33-31-4, PERFORMED OPERATIONAL TEST OF
- [SDR FDEA200901080081](https://openairdocs.org/sdr/FDEA200901080081.md): Frame · corroded · Jan 8, 2009 · N454FE · Airbus A310322 · Fuselage Main, Frame
  > AFT CARGO DOOR CUTOUT FRAME 59A CORROSION AT LOWER END OF DOOR FRAME. PERFORMED REPAIR PER SRM 53-17 FIG 201 AND 202A AND EA NR 6-5320-125509.
- [SDR 08FDEA02075](https://openairdocs.org/sdr/08FDEA02075.md): Regulator · failed · Jun 1, 2008 · N454FE · Airbus A310222 · Pressure Regulator/Outflow Valve
  > DURING CLIMB-OUT WITH NR 1 REG DEFERRED, LOST NR 2 REG. USED MANUAL PRESSURIZATION FOR THE REST OF FLIGHT. ACN RELEASED FOR SERVICE PER MEL/CDL: 21-31-04-01-A. DEACTIVATED IN CLOSED POSITION. ENSURE CAB DIF PRESS IS ZERO PRIOR TO OPENING ANY DOOR." SWAPP
- [SDR 07FDEA02562](https://openairdocs.org/sdr/07FDEA02562.md): Autopilot Sys · unknown · Jul 20, 2007 · N454FE · Airbus A310222 · Autopilot System
  > CLOSE R AP 1 AND 2 DO NOT ENGAGE. MTP FAULT REVIEW FOUND FCC 1/ FCC 2/FCU/TORQUE LIMIT RESET A/P 1 AND 2 BOTH FCC AND FCU. PERFORMED AFS/LAND ENGAGE TEST AS PER AMM 22-10-00-5 BOTH A/P CAN BE ENGAGED. A/C RETURNED TO SERVICE. MTP FAULT REVIEW FOUND FCC1/FC
- [SDR 07FDEA02366](https://openairdocs.org/sdr/07FDEA02366.md): Unknown · warning light · Jul 3, 2007 · N454FE · Airbus A310222 · Door Warning System
  > FWD CARGO DOOR UNLOCK INDICATION NUMEROUS TIMES AFTER TAKEOFF. ACN RELEASED FOR SERVICE PER MEL/CDL: 52-71-01, CATEGORY: C EXPIRATION: 13JUL07.
- [SDR 06FDEA04333](https://openairdocs.org/sdr/06FDEA04333.md): Bulkhead · corroded · Dec 28, 2006 · N454FE · Airbus A310222 · Fuselage Main, Bulkhead
  > FUSE AFT PRESSURE BULKHEAD LOWER RIM FWD SIDE FR 80/82 FROM STR 50L TO STR 51L. CORROSION REPAIRED IAW FEDEX EA6-5310-106280.
- [SDR 06FDEA04332](https://openairdocs.org/sdr/06FDEA04332.md): Bearing · frozen · Dec 28, 2006 · N454FE · Airbus A310222 · Rudder Control System
  > A FROZEN BEARING EXIST AT LT NR 3 RUDDER HINGE ARM COMPLIED WITH FEDEX EA6-5540-106279.
- [SDR 06FDEA04312](https://openairdocs.org/sdr/06FDEA04312.md): Seat Track · damaged · Dec 26, 2006 · N454FE · Airbus A310222 · Fuselage, Seat/Cargo Attach Fittings
  > DUMMY TRACK FS 54 TO 54.2 LT NR 5 HAS SLOTTED HOLE ATTACHMENT POINT HAS WEAR MEASURING.051 IN. REMOVED AND INSTALLED FLOORBOARD IAW A310/200 AMM 53-10-254. ROUTED TO B/S FOR REPAIR IAW A310/200 SCP53-15-16. INSTALLED DUMMY TRACK IAW A310/200 SRM 53-15-18.
- [SDR 06FDEA04311](https://openairdocs.org/sdr/06FDEA04311.md): Hinge · corroded · Dec 26, 2006 · N454FE · Airbus A310222 · Elevator Structure
  > RT ELEVATOR T/E AT AT 4 HINGE ARM HAS LIGHT CORROSION TOP AND BOTTOM AS MARKED REPAIRED CORROSION ON RT, ELEVATOR AT NR 4 HINGE ON CORNER SKIN IAW A310/200 SRM 51-74-10 PARAGRAPH 6A. REPAIRED DAMAGED SKIN ON UPPER SKIN IAW EA6-5520-106303.
- [SDR 06FDEA04307](https://openairdocs.org/sdr/06FDEA04307.md): Skin · misrepaired · Dec 22, 2006 · N454FE · Airbus A310322 · Fuselage Main, Plate/Skin
  > PREVIOUS REPAIR, FUSELAGE SKIN RT SIDE HAS EXTERNAL REPAIR DOUBLE BETWEEN FR 54.1 TO 54.2, BETWEEN STR 38 RT TO STR 40 RT, MEASURES 6.3" BY 6.2" PREVIOUSLY INSTALLED REPAIR LOCATED AT RT SIDE FUSELAGE SKIN BETWEEN FRAMES 54.1- 54.2 STRINGERS 38 TO 40 RT DETERM
- [SDR 06FDEA04306](https://openairdocs.org/sdr/06FDEA04306.md): Seat Track · broken · Dec 22, 2006 · N454FE · Airbus A310222 · Fuselage, Seat/Cargo Attach Fittings
  > MDCC SEAT TRACK R1 AT FR 38.1 HAS (1) BROKEN SCALLOP AND (1) BENT SCALLOP. REMOVED AND INSTALLED REPAIR SEAT TRACK IAW A310-200 SRM 53-10-16 PB 201 FIG 208.
- [SDR 06FDEA04304](https://openairdocs.org/sdr/06FDEA04304.md): Seat Track · gouged · Dec 22, 2006 · N454FE · Airbus A310222 · Fuselage, Seat/Cargo Attach Fittings
  > MDCC SEAT TRACK L4 FR 54.2 - 58 GOUGED REMOVED AND REINSTALLED 4EA FLOORBOARDS IAW A310-200 SRM 53-10-25-4. REMOVED AND INSTALLED NEW SEAT TRACK IAW A310-200 DWG 16R532H1414. FABBED NEW SEATRACK PER A310-200 DWG 16R532H1414. REMOVED AND REINSTALLED 4 EA SEA
- [SDR 06FDEA04302](https://openairdocs.org/sdr/06FDEA04302.md): Hinge Fitting · corroded · Dec 22, 2006 · N454FE · Airbus A310222 · Rudder Miscellaneous Structure
  > CORROSION EXIST AT VERT STAB REAR SPAR NR 3 RUDDER ATTACHMENT HINGE FITTING COMPLIED WITH EA NR 6-5540-106300. RUDDER RIB 12 AND 13 ATTACH FITTINGS CORROSION. MAJOR REPAIR IAW FED EX GMM 6-2-100.
- [SDR 06FDEA04301](https://openairdocs.org/sdr/06FDEA04301.md): Hinge Fitting · corroded · Dec 22, 2006 · N454FE · Airbus A310322 · Rudder Miscellaneous Structure
  > VERT STAB REAR SPAR NR 2 RUDDER ATTACHMENT HINGE FITTING HAS CORROSION. COMPLIED WITH EA NR 6-5540-106300 RUDDER RIB 12 AND 13 ATTACH FITTINGS CORROSION. MAJOR REPAIR IAW FED EX GMM 6-2-100.
- [SDR 06FDEA04300](https://openairdocs.org/sdr/06FDEA04300.md): Skin · delaminated · Dec 22, 2006 · N454FE · Airbus A310322 · Wing, Plate/Skin
  > RT WING, INBD FLAP, LWR EXT SKIN AT MID T/E, (1)EA AREA OF DELAMINATION APPROX 6" * 6" DIA. REPAIRED (1EA) AREA OF DELAMINATION ON RT WING I/B FLAP LOWER SKIN IAW A310-200 SRM 57-52-12 FIG 204. THE REPAIR IS FOUND TO BE MAJOR IAW FED EX GMM 6-2-100.
- [SDR 06FDEA2068](https://openairdocs.org/sdr/06FDEA2068.md): Regulator · malfunctioned · May 30, 2006 · N454FE · Airbus A310222 · Engine Thrust Reverser
  > ENGINE NR 1 REV UNLK ILLUMINATED ON TAKEOFF ROLL, REJECTED TAKEOFF, WHEN THROTTLES PULLED TO IDLE REV UNLK LIGHT ENGINE NR 1 EXTINGUISHED. REJECTED TAKEOFF AT APPROX 6O KTS. REMOVED AND REPLACED NR 1 ENGINE PRESSURE REGULATING AND SHUTOFF VALVE AS PER AMM 78
- [SDR 06FDEA2064](https://openairdocs.org/sdr/06FDEA2064.md): Switch · faulty · May 29, 2006 · N454FE · Airbus A310222 · Engine Thrust Reverser
  > ENGINE NR 1 REV UNLK ILLUMINATED ON TAKEOFF ROLL. REJECTED TAKEOFF APPROX 40 KTS REV UNLK LIGHT EXTINGUISHED WHEN THROTTLES PULLED TO IDLE. REMOVED AND REPLACED NR 1 ENGINE STOW SWITCH S303 AND PERFORMED RIGGING PER A310 AMM 78-31-00-5. OPS CHK COMPLETED.
- [SDR 05FDEA04016](https://openairdocs.org/sdr/05FDEA04016.md): Regulator · malfunctioned · Nov 29, 2005 · N454FE · Airbus A310 · Engine Oil Quantity
  > NR 2 ENGINE INDICATED HIGH OIL PRESSURE, THEN FOLLOWED QRH & MONITORED PARAMETERS. OIL PRESS. WENT TO 20-32 PSI (LOW) FOLLOWED QRH AND SHUTDOWN ENGINE. DECLARED EMERGENCY AND LANDED RWY 32L. HIGH OIL PRESS. WAS 100, LOW OIL PRESS. WAS 22. PRESSURE VARIED
- [SDR 05FDEA00036](https://openairdocs.org/sdr/05FDEA00036.md): Rib · corroded · Jan 6, 2005 · N454FE · Airbus A310222 · Wing, Rib/Bulkhead
  > ACCOMPLISH MAINTENANCE C-CHECK, NON-ROUTINE, LT WING - CORROSION FOUND ON UPPER SURFACE STA 1659 RIB 27 TO STA 1713 RIB 28 INTERSECTION WITH STRINGER 12. REPAIRED IAW FAX REF 942-034715/005/2004 DATED 12/27/2004 AND FEDEX EA 6-5710-81827. PERFORMED NDT INSP
- [SDR 05FDEA00035](https://openairdocs.org/sdr/05FDEA00035.md): Skin · dented · Jan 6, 2005 · N454FE · Airbus A310222 · Wing, Plate/Skin
  > ACCOMPLISH MAINTENANCE C-CHECK, NON-ROUTINE, RT WING - DENTS AND DEBONDS AT LOWER SKIN SURFACE OF T/E OF FLAP INBOARD. REPAIRED IAW AIRBUS REF: 001-57-01-2005-A1B AND IAW EA 6-5750-81828. PAINTED IAW SRM 51-75-10-8.
- [SDR 05FDEA00039](https://openairdocs.org/sdr/05FDEA00039.md): Skin · corroded · Jan 6, 2005 · N454FE · Airbus A310 · Wing, Plate/Skin
  > RT WING - CORROSION FOUND ON UPPER SURFACE STA 1659 RIB 27 TO STA 1713 RIB 28 INTERSECTION WITH STRINGER 12. CORROSION REMOVED AND REPAIRED IAW EA 6-5710-81827.
- [SDR 05FDEA00038](https://openairdocs.org/sdr/05FDEA00038.md): Skin · corroded · Jan 6, 2005 · N454FE · Airbus A310 · Fuselage Main, Plate/Skin
  > RT WING CORROSION FOUND ON UPPER SURFACE STA 813 RIB 13 TO STA 874 RIB 14 INTERSECTION WITH STRINGER 7. CORROSION REMOVED AND REPAIRED IAW EA 6-5710-81827.
- [SDR 05FDEA00034](https://openairdocs.org/sdr/05FDEA00034.md): Fairing · cracked · Jan 6, 2005 · N454FE · Airbus A310 · Nacelle/Pylon, Main Frame
  > NR 2 PYLON, AFTER FIXED FAIRING WITH CRACK AT LT. REMOVED IAW AMM 54-55-00. REPAIRED IAW FEDEX EA 6-5480-81822. INSTALED IAW AMM 54-55-00.
- [SDR 05FDEA00033](https://openairdocs.org/sdr/05FDEA00033.md): Skin · damaged · Jan 6, 2005 · N454FE · Airbus A310 · Trailing Edge Flaps
  > NON-ROUTINE NR N00380. RT WING REPAIR ON INBD FLAP LWR SURFACE T/E. VERIFIED THAT THE EXISTING REPAIR WAS PERFORMED IAW FEDEX EA 6-5710-63790.
- [SDR 05FDEA00029](https://openairdocs.org/sdr/05FDEA00029.md): Skin · damaged · Jan 6, 2005 · N454FE · Airbus A310222 · Fuselage Main, Plate/Skin
  > COMPLY WITH AGING 9-AGING-INSPECTION. NON-ROUTINE, FUSELAGE - REPAIR AT APPROX FS 69 STR 50 RT. *S/D* VERIFIED THAT THE EXISTING REPAIR WAS PERFORMED IAW SRM 53-10-12, FIG 225.
- [SDR 05FDEA00027](https://openairdocs.org/sdr/05FDEA00027.md): Skin · damaged · Jan 6, 2005 · N454FE · Airbus A310 · Fuselage Main, Plate/Skin
  > FUSELAGE REPAIR AT APROX. FS 1 STR 56 LT. VERIFIED THAT THE EXISTING REPAIR WAS PERFORMED IAW FEDEX EA 6-5310-81826.
- [SDR 05FDEA00026](https://openairdocs.org/sdr/05FDEA00026.md): Skin · damaged · Jan 6, 2005 · N454FE · Airbus A310 · Fuselage Main, Plate/Skin
  > FUSELAGE - REPAIR AT APROX. FS 63 STR 42 RT. REPAIRED IAW SRM 53-17-12, FIG 203.
- [SDR 05FDEA00037](https://openairdocs.org/sdr/05FDEA00037.md): Skin · corroded · Jan 6, 2005 · N454FE · Airbus A310222 · Wing, Plate/Skin
  > ACCOMPLISH MAINTENANCE C-CHECK, ORIGINAL PLAN DATE WAS ENTERED ON: 23JUL04. NON-ROUTINE LT WING - CORROSION FOUND ON UPPER SURFACE STA 813 RIB 13 TO STA 874 RIB 14 INTERSECTION WITH STRINGER 7. REPAIRED IAW FAX REF 942-034715/005/2004 DATED 12/27/2004 AND FE
- [SDR 04FDEA01815](https://openairdocs.org/sdr/04FDEA01815.md): Engine · failed · Jun 20, 2004 · N454FE · Airbus A310222 · Engine (Turbine/Turboprop)
  > UNRECOVERABLE STALL ENG NR 2 DURING T/O AT 500 FT ATB. EGT WAS RAISING TO 670 DEG C, EGT LIGHT ON, PULLED BACK THE THROTTLE TO PREVENT FURTHER EGT INCREASE. FLAME NOTED BY ATC. AS PER MTSI 72-00/3790 REMOVED AND REPLACED NR 2 ENG VANE AND BLEED CONTROL PE

Next page: https://openairdocs.org/aircraft/N454FE/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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 = 'N454FE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N454FE/reports

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