# N811FD: 1988 Airbus Industrie A310-324, registration cancelled 2024-03-02

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: March 2, 2024
- Status when cancelled: Valid registration
- Airframe: [Airbus Industrie A310-324](https://openairdocs.org/model/airbus-industrie-a310-324) (registry code 3930318)
- Engine: [Pratt & Whitney PW4152](https://openairdocs.org/engine/pratt-whitney-pw4152) (registry code 51668)
- Data sheets: [TCDS A35EU](https://openairdocs.org/tcds/A35EU), [TCDS E24NE](https://openairdocs.org/tcds/E24NE) (OpenAirDocs)
- Serial number: 457
- Year built: 1988
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 28, 2006
- Certificate issued: April 13, 2005
- Last registry action: October 20, 2023
- Mode S code: AB0D94
- Owner when cancelled: [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP)
- Location: [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis)
- Owner type: Corporation
- Owner's area on the map: 35.0351° N, 89.9272° W: Placed by OpenAirDocs at the center of ZIP code 38118, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N811FD
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=811FD
- Page: https://openairdocs.org/deregistered/N811FD-2024-03-02

From the FAA registry file of November 3, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

ADs and bulletins for the Airbus Industrie A310-324: https://openairdocs.org/model/airbus-industrie-a310-324.md

## Service difficulty reports (123, newest 50)

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

- [SDR FDEA201903010528](https://openairdocs.org/sdr/FDEA201903010528), Mar 1, 2019: LINKAGE. BROKEN. PDIS 811 32-30 4584 01MAR19 GRR DURING LANDING GEAR RETRACTION. L/G RETRACTION FAULT. THE LEFT GEAR DOOR AMBER LIGHT WAS LIT AND THE RED UNLOCKED LIGHT WAS LIT.
- [SDR FDEA201901030010](https://openairdocs.org/sdr/FDEA201901030010), Jan 3, 2019: ACTUATOR. MALFUNCTIONED. AT FL340 GOT YELLOW SYS HYD RESERVOIR ECAM WITH CONFIRMED LOW QTY. EMER RTN TO MEM. COMPLETED INSTALL OF #4 LH SPOILER ACTUATOR REFERENCE AIRBUS A310-300 AMM 27
- [SDR FDEA2018121863510](https://openairdocs.org/sdr/FDEA2018121863510), Dec 16, 2018: CIRCUIT BREAKER. BURNED. 811 24-50 4376 15DEC18 MEM FACT LOGPAGES:3011783 DURING APPROACH PHASE, RECEIVED "BUS 2 FAIL". COMPLIED WITH QRH. FOUND HEAT DAMAGE ON C/B 2XN. R&R'D C/B 2XN PA
- [SDR FDEA201709182589](https://openairdocs.org/sdr/FDEA201709182589), Sep 18, 2017: STIFFENER. CORRODED. LOWER SKIN STIFFENER CORRODED BETWEEN FRAMES 43 & 46, Y1456. COMPLIED WITH EA6-5710-T0335320 P1. MAJOR REPAIR IAW GMM6-2-100.
- [SDR FDEA201709132525](https://openairdocs.org/sdr/FDEA201709132525), Sep 13, 2017: STIFFENER. CORRODED. LOWER SKIN STIFFENER CORRODED,BETWEEN FRAMES 43 AND 47, Y-1456. COMPLIED WITH EA 6-5710-T0335320 P1. MAJOR REPAIR IAW GMM6-2-100.
- [SDR FDEA201709072463](https://openairdocs.org/sdr/FDEA201709072463), Sep 7, 2017: STRINGER. DAMAGED. AFT CABIN UNDERFLOOR COMPT FR74-FR75, S45R STRINGER 1EA FASTENER HOLE DAMAGED. AFT CABIN UNDERFLOOR COMPT FR74-FR75,S-45R STRINGER 1EA FASTENER HOLE DAMAGED. RE
- [SDR FDEA201708282387](https://openairdocs.org/sdr/FDEA201708282387), Aug 28, 2017: SPAR. CRACKED. LEFT REAR SPAR INTERNAL ANGLE NR 1 HOLE FOUND CRACKED DURING AN NDT INSPECTION. REPAIRED IAW EA 6-5710-T0335292 P1. MAJOR REPAIR IAW GMM 6-2-100.
- [SDR FDEA201708282385](https://openairdocs.org/sdr/FDEA201708282385), Aug 28, 2017: SPAR. CRACKED. LEFT REAR SPAR INTERNAL ANGLE NR 4 HOLE FOUND CRACKED DURING AN NDT INSPECTION. REPAIRED IAW EA 6-5710-T0335292 P1. MAJOR REPAIR IAW GMM 6-2-100.
- [SDR FDEA201708282384](https://openairdocs.org/sdr/FDEA201708282384), Aug 28, 2017: SPAR. CRACKED. LEFT REAR SPAR INTERNAL ANGLE NR 10 HOLE FOUND CRACKED DURING AN NDT INSPECTION. REPAIRED IAW EA 6-5710-T0335292 P1. MAJOR REPAIR IAW GMM 6-2-100.
- [SDR FDEA201708282383](https://openairdocs.org/sdr/FDEA201708282383), Aug 28, 2017: SPAR. CRACKED. LEFT REAR SPAR INTERNAL ANGLE NR 52 HOLE FOUND CRACKED DURING AN NDT INSPECTION. REPAIRED IAW EA 6-5710-T0335292 P1. MAJOR REPAIR IAW GMM 6-2-100.
- [SDR FDEA201708282382](https://openairdocs.org/sdr/FDEA201708282382), Aug 28, 2017: SPAR. CRACKED. LEFT REAR SPAR INTERNAL ANGLE NR 60 HOLE FOUND CRACKED DURING AN NDT INSPECTION. REPAIRED IAW EA:6-5710-T0335292 P1. MAJOR REPAIR IAW GMM 6-2-100.
- [SDR FDEA201708282381](https://openairdocs.org/sdr/FDEA201708282381), Aug 28, 2017: SPAR. CRACKED. LEFT REAR SPAR INTERNAL ANGLE NR 62 HOLE FOUND CRACKED DURING AN NDT INSPECTION. REPAIRED IAW EA 6-5710-T0335292 P1. MAJOR REPAIR IAW GMM 6-2-100.
- [SDR FDEA201708282380](https://openairdocs.org/sdr/FDEA201708282380), Aug 28, 2017: SPAR. CRACKED. RIGHT REAR SPAR INTERNAL ANGLE NR 2 HOLE FOUND CRACKED DURING AN NDT INSPECTION. REPAIRED IAW EA 6-5710-T0335292 P1. MAJOR REPAIR IAW GMM 6-2-100.
- [SDR FDEA201708282379](https://openairdocs.org/sdr/FDEA201708282379), Aug 28, 2017: SPAR. CRACKED. RIGHT REAR SPAR INTERNAL ANGLE NR 8 HOLE FOUND CRACKED DURING AN NDT INSPECTION. REPAIRED IAW EA:6-5710-T0335292 P1. MAJOR REPAIR IAW GMM 6-2-100.
- [SDR FDEA201708282378](https://openairdocs.org/sdr/FDEA201708282378), Aug 28, 2017: SPAR. CRACKED. RIGHT REAR SPAR INTERNAL ANGLE, NR 14 HOLE FOUND CRACKED DURING AN NDT INSPECTION. REPAIRED IAW EA:6-5710-T0335292 P1. MAJOR REPAIR IAW GMM 6-2-100.
- [SDR FDEA201708282377](https://openairdocs.org/sdr/FDEA201708282377), Aug 28, 2017: FRAME ANGLE. CRACKED. RIGHT REAR FRAME INTERNAL ANGLE NR 23 HOLE, NDT INSPECTION FOUND A CRACK. REPAIRED IAW EA:6-5710-T0335292 P1. MAJOR REPAIR IAW GMM 6-2-100.
- [SDR FDEA201703180949](https://openairdocs.org/sdr/FDEA201703180949), Mar 18, 2017: AOA. MALFUNCTIONED. DURING CLIMB THRU FL 340, PROBES & STAT ALPHA CONTROL CIRCUIT BREAKER TRIPPED. MULTIPLE PROBE HT FAILS. FOLLOWED ECAM & QRH PROCEDURES. ATS LEVER TRIPPED OFF IN
- [SDR FDEA201701050043](https://openairdocs.org/sdr/FDEA201701050043), Jan 5, 2017: LIMIT SWITCH. FAILED. WHILE TROUBLE SHOOTING R1 DOOR ARMING PROBLEM, SLIDE TRIED TO DEPLOY. REMOVED AND REPLACED RI DOOR LIMIT SWITCH 14WN AND TESTED IAW AMM 52-73-13-04-09.
- [SDR FDEA201701050045](https://openairdocs.org/sdr/FDEA201701050045), Jan 5, 2017: SWITCH. MALFUNCTIONED. R1 SLIDE INDICATOR WAS BLINKING ON & OFF AT BLOCK IN PRIOR TO DISARMING. R & R THE R1 DOOR LIMIT SWITCH 14WN.
- [SDR FDEA201701050044](https://openairdocs.org/sdr/FDEA201701050044), Jan 5, 2017: SLIDE. UNKNOWN. DURING TROUBLESHOOTING OF THE R1 DOOR ARMING PROBLEM, THE SLIDE TRIED TO DEPLOY. COMPLIED WITH R1 SLIDE REMOVAL ONLY IAW EA 6-5210-T0330666 PART 1.
- [SDR FDEA201612314582](https://openairdocs.org/sdr/FDEA201612314582), Dec 31, 2016: RELAY. FAILED. R1 SLIDE INDICATION FLASHES CONTINUOUSLY WHEN SLIDE IS ARMED ON RIGHT ECAM. RELEASED FOR SERVICE PER MEL 52-30-04. REMOVED AND REPLACED RELAYS 9ES AND 10ES REF 
- [SDR FDEA201612034317](https://openairdocs.org/sdr/FDEA201612034317), Dec 3, 2016: LIMIT SWITCH. INOPERATIVE. AFTER PARKING, THE R1 DOOR SLIDE INDICATION WAS FLASHING. R & R THE DOOR LIMIT SWITCH IAW AMM 52-73-13-04-09 OPS CHECKED GOOD IAW 73-13-05-09.
- [SDR FDEA201611274258](https://openairdocs.org/sdr/FDEA201611274258), Nov 27, 2016: BATTERY PACK. INOPERATIVE. DURING LANDING, SLIDE INDICATION ON ECAM FOR R1 WAS FLASHING. REMOVED AND REPLACED ASPU BATTERY NR 1 IAW AMM 52-73-18-04, ASPU BITE CHECKED GOOD. SLIDE INDICATI
- [SDR FDEA201611224197](https://openairdocs.org/sdr/FDEA201611224197), Nov 22, 2016: BOTTLE. LOW PRESSURE. R1 DOOR SLIDE ARMED INDICATION FLASHING WHILE TAXING IN AFTER LANDING. RT DOOR DAMPER AND EMERGENCY OPERATING CYLINDER PRESSURE FOUND TO BE LOW. SERVICED CYLIND
- [SDR FDEA201610263703](https://openairdocs.org/sdr/FDEA201610263703), Oct 26, 2016: RELAY. FAILED. AT FL 370 , THE NR 2 LEFT INNER PUMP FAULTED. PUMP FAULTED AND STRONG ACRED ODOR IN THE COCKPIT AND THE AVIONICS COMPARTMENT, ON DESCENT THE REMAINING THREE INN
- [SDR FDEA201601050025](https://openairdocs.org/sdr/FDEA201601050025), Jan 5, 2016: SELECTOR VALVE. MALFUNCTIONED. AFTER TAKEOFF, LG RETRACTION FAULT SYS NR 1, GEAR REMAINED DOWN. RETURNED FOR LAND. CANNOT OPEN THE LT LG DOOR ON GND. RT LG DOOR OPENED OK ON GND. R&R LG NORMA
- [SDR FDEA201507072165](https://openairdocs.org/sdr/FDEA201507072165), Jul 7, 2015: HYDRAULIC LINE. LEAKING. EN-ROUTE, GREEN HYD LEVEL DECREASING SLOWLY. DESCENDING THRU FL 150, ECAM WARNING, HYD LEVEL LO, RAN QRH. LEAK FOUND AT LT MAIN GEAR FLEX HOSE PN 00624AE711082-
- [SDR FDEA201505061396](https://openairdocs.org/sdr/FDEA201505061396), May 6, 2015: SKIN. CRACKED. RIGHT WING ROOT REAR SPAR BOTTOM SKIN FOUND ONE EACH FASTENER HEAD POPPED OUT. REMOVED THE HEAD POPPED OUT FASTENER IAW SRM 51-40-21. CARRIED OUT ROTOTEST INSPE
- [SDR FDEA201504291321](https://openairdocs.org/sdr/FDEA201504291321), Apr 29, 2015: FAIRING. CRACKED. RIGHT WING TIP FENCE FAIRING RIB CRACKED, WY495. REPLACED THE CRACKED RIB OF RT WING TIP FENCE FAIRING AT WY 501 IAW SRM 51-40-21.
- [SDR FDEA201504291320](https://openairdocs.org/sdr/FDEA201504291320), Apr 29, 2015: RIB. CRACKED. RIGHT WING TIP FENCE FAIRING AROUND FASTENER HOLES CRACKED AT WY501. REPLACED IAW SRM 51-40-21.
- [SDR FDEA201504291319](https://openairdocs.org/sdr/FDEA201504291319), Apr 29, 2015: FRAME. CORRODED. AV COMPARTMENT FOUND FRAME 17 CORRODED BETWEEN STRINGER 42 & 43L. BLENDED OUT THE CORROSION IAW SRM 51-74-10 & EA 6-5310-T0317322 P1.
- [SDR FDEA201504291318](https://openairdocs.org/sdr/FDEA201504291318), Apr 29, 2015: FRAME. NICKED. MDCC LT FRAME 34 SURFACE FOUND NICK BETWEEN STRINGER 12LT & 22LT. BLEND OUT & SMOOTHED THE NICK AREA IAW SRM51-73-10. APPLIED ALODINE IAW SRM 51-21-10. NO CRACK
- [SDR FDEA201504161242](https://openairdocs.org/sdr/FDEA201504161242), Apr 16, 2015: DOOR FRAME. CRACKED. FORWARD CARGO DOOR ACTUATOR ATTACH FITTING. SDI FOUND CRACK WITH A HFEC INSPECTION. REMOVED THE FWD CARGO DOOR IAW AMM 52-31-11-04. REPLACED THE CRACKED FRAME O
- [SDR FDEA201504161241](https://openairdocs.org/sdr/FDEA201504161241), Apr 16, 2015: FITTING. CRACKED. AFT CARGO COMPARTMENT DOOR ACTUATOR FITTINGS. FOUND CRACK WITH A HFEC INSPECTION. REPLACED THE CRACKED FRAME OF AFT CARGO DOOR AT FRAME 61A IAW SRM 51-40-21. IN
- [SDR FDEA201504141229](https://openairdocs.org/sdr/FDEA201504141229), Apr 14, 2015: CROSSBEAM. CORRODED. AFT CARGO CROSSBEAM RT SIDE FITTING, CORRODED AT FRAME 62. REPLACED THE RT SIDE CORRODED FITTING, CROSSBEAM, IAW SRM 51-40-21.
- [SDR FDEA201406251546](https://openairdocs.org/sdr/FDEA201406251546), Jun 25, 2014: WINDSHIELD. CRACKED. CAPTAIN`S COCKPIT WINDOW CRACKED AT FLIGHT LEVEL 340, ARCING BEGAN IMMEDIATELY. NORMAL QRH PROCEDURES STOPPED THE ARCING. REMAINDER OF FLIGHT NORMAL. R & R CAPT
- [SDR FDEA201405211114](https://openairdocs.org/sdr/FDEA201405211114), May 21, 2014: ENGINE. STALLED. NR 1 ENGINE HAD A SUSPECTED STALL ON ROLLOUT. TOWER REPORTED LT ENGINE ON FIRE. STOWED THRUST REVERSERS BY 60 KIAS & STOPPED ACFT, SHUTDOWN ENGINE, NO OTHER FIR
- [SDR FDEA201403130495](https://openairdocs.org/sdr/FDEA201403130495), Mar 13, 2014: SMOKE DETECTOR. MALFUNCTIONED. IAW WRI 26-22 8151 FWD CARGO COMPARTMENT DET INDICATION. AGENT 1 DISCH, NO SECONDARY INDICATION, NO SMOKE INDICATION IN THE COCKPIT. TESTED BOTH SMOKE DET OK & 
- [SDR FDEA201310162517](https://openairdocs.org/sdr/FDEA201310162517), Oct 16, 2013: SKIN. DENTED. FUSELAGE SKIN DENTED ON BELLY FWD OF FRAME 4. REPAIRED DENT IAW EA 6-5330-T0302970A.
- [SDR FDEA201308191952](https://openairdocs.org/sdr/FDEA201308191952), Aug 19, 2013: JACKSCREW. WORN. AFTER TAKEOFF DURING FLAP RETRACTION, RECIEVED A WARNING BELL AND FLAP SYS 1, FLAP SYS 2FAULT. FLAPS WERE STUCK BETWEEN 15-20, CYCLED HANDLE AND DID NOT CLEAR R
- [SDR FDEA201308151902](https://openairdocs.org/sdr/FDEA201308151902), Aug 15, 2013: UNKNOWN. UNKNOWN. ON APPROACH, FLAPS SYS 1 AND 2 FAULTED. RECYCLED FLAPS, RETRACTED BUT ON EXTENSION STOPPED AT APPOX 18. RAN QRH AND ON FINAL WITH FLAP HANDLE EXTENSION TO 30/40
- [SDR FDEA201308011728](https://openairdocs.org/sdr/FDEA201308011728), Aug 1, 2013: COMPUTER. FAILED. DURING TAKEOFF ROLL, APPROX 10 SECONDS INTO ROLL, ATS LEVER TRIPPED OFF. ENGINE NR 2 EPR MODE FAULTED, ENGINE NR 2, N1 MODE, ATS OFF ON ECAM. CLEARED RUNWAY. RE
- [SDR FDEA201305070933](https://openairdocs.org/sdr/FDEA201305070933), May 7, 2013: WIRE. DAMAGED. WHEN SETTING TAKEOFF POWER, NR 1 ENGINE REVERSE UNLOCK LIGHT ILLUMINATED. DURING REACTIVATION OF NR 1 THRUST REVERSER, FOUND WIRE CHAFING IN WIRING BUNDLE 21W40
- [SDR FDEA201304090756](https://openairdocs.org/sdr/FDEA201304090756), Apr 9, 2013: LIMIT SWITCH. FAILED. CLIMBING THROUGH 5,100 METERS RECEIVED ECAM ALERT. FORWARD CARGO DOOR UNLOCK, PROCEEDED ACCORDING WITH ECAMS SET LANDING ELEVATION AT 10,000 ALERT WENT AWAY AND
- [SDR FDEA201111305081](https://openairdocs.org/sdr/FDEA201111305081), Nov 30, 2011: CONTROLLER. INOPERATIVE. ACFT CABIN PRESS CLIMB ABOVE 10000. REQUESTED LOWER ALTITUDE FROM ATC. BRIEFING WITH FLIGHT CREW, NO WARNING MESSAGE DISPLAYED ON ECAM. PERFORMED CPC 1 AND CPC 
- [SDR FDEA201110214611](https://openairdocs.org/sdr/FDEA201110214611), Oct 21, 2011: BATTERY. INOPERATIVE. R1 DOOR WILL NOT ARM. R & R THE EMERGENCY POWER SUPPLY BATTERY NR 1 AND NR 2, AND THE AUTO STANDBY UNIT IAW AMM 52-73-18-04-0, AND PERFORMED THE TEST IAW AMM 52
- [SDR FDEA201108103196](https://openairdocs.org/sdr/FDEA201108103196), Aug 10, 2011: INDICATOR. FAILED. AT ALTITUDE CABIN PRESSURE INDICATED 20460 AND COMMANDED DESCENT. DONED MASKS AND DESECNDED TO 10K, DIVERTED. CABIN PRESS INDICATIONS DELTA P XX (ORANGE) V/S= 2
- [SDR FDEA201108103195](https://openairdocs.org/sdr/FDEA201108103195), Aug 10, 2011: CONTROLLER. FAILED. AT ALTITUDE CABIN PRESSURE INDICATED 20460 AND COMMANDED DESCENT. DONED MASKS AND DESCENDED TO 10K, DIVERTED. CABIN PRESS INDICATIONS DELTA P XX (ORANGE) V/S= 2
- [SDR FDEA201009303819](https://openairdocs.org/sdr/FDEA201009303819), Sep 30, 2010: FILTER. LEAKING. DURING DESCENT RECEIVED ECAM GREEN HYD SYS LOW LEVEL WARNING. HYD QTY ON OVERHEAD PANEL INDICATED ZERO. CONSULTED THE QRH AND MANUALLY EXTENDED THE LANDING GEAR
- [SDR FDEA201009303821](https://openairdocs.org/sdr/FDEA201009303821), Sep 30, 2010: FILTER. LEAKING. DURING DESCENT RECEIVED ECAM GREEN HYD SYS LOW LEVEL WARNING. HYD QUANTITY ON OVERHEAD PANEL INDICATED ZERO. CONSULTED THE QRH AND MANUALLY EXTENDED THE LANDING

All 123: https://openairdocs.org/deregistered/N811FD-2024-03-02/reports.md

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