# N446FE: 1983 Airbus Industrie A310-222, registration cancelled 2013-07-29

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: July 29, 2013
- Status when cancelled: First renewal notice
- Airframe: [Airbus Industrie A310-222](https://openairdocs.org/model/airbus-industrie-a310-222) (registry code 3930315)
- Engine: [Pratt & Whitney JT9D series](https://openairdocs.org/engine/pratt-whitney-jt9d-series) (registry code 52054)
- Data sheets: [TCDS A35EU](https://openairdocs.org/tcds/A35EU) (OpenAirDocs)
- Serial number: 224
- Year built: 1983
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 4, 1996
- Certificate issued: February 14, 1996
- Last registry action: November 19, 2010
- Mode S code: A56169
- Owner when cancelled: [Federal Express Corporation](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORPORATION)
- 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/N446FE
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=446FE
- Page: https://openairdocs.org/deregistered/N446FE-2013-07-29

From the FAA registry file of October 29, 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 A310-222: https://openairdocs.org/model/airbus-industrie-a310-222.md

## Service difficulty reports (97, newest 50)

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

- [SDR FDEA201002150424](https://openairdocs.org/sdr/FDEA201002150424), Feb 15, 2010: TRANSMITTER. MALFUNCTIONED. AFTER TOGA POWER SET ON T/O, GOT A NR 1 ENG HIGH OIL PRESS LIGHT. REJECTED T/O. ALSO DURING START THE NR 1 ENG HIGH OIL PRESSURE LIGHT CAME ON FOR 1 MIN. GROUND
- [SDR FDEA200911244202](https://openairdocs.org/sdr/FDEA200911244202), Nov 24, 2009: SWITCH. MALFUNCTIONED. ON APPROACH, NO NOSE GEAR INDICATION ON NR 1 SYS (FRONT PANEL) NR 2 SYS (OVERHEAD PANEL) GOOD, DID A GO AROUND AND ON DOWNWIND, NOSE GEAR LIGHT CAME BACK AND IN
- [SDR 07FDEA04248](https://openairdocs.org/sdr/07FDEA04248), Sep 24, 2007: SPAR. FAILED. LEFT HORIZONTAL STAB ON UPPER REAR SPAR BETWEEN RIBS 4/5 REPAIR STRAP IN WRONG MATERIAL TYPE. REMOVE AND REPLACE AS REQUIRED REMOVED STRAP IAW A310-200 FX SRM 5
- [SDR 07FDEA04251](https://openairdocs.org/sdr/07FDEA04251), Sep 24, 2007: SPAR. DAMAGED. LEFT HORIZONTAL STAB ON UPPER REAR SPAR BETWEEN RIBS 10 AND 11 REPAIR STRAP REQUIRES REMOVAL FOR MATERIAL TYPE VERIFICATION REMOVED STRAP IAW A310-200 SRM 55-11
- [SDR 07FDEA04247](https://openairdocs.org/sdr/07FDEA04247), Sep 24, 2007: SPAR. DAMAGED. RIGHT HORIZONTAL STAB ON UPPER REAR SPAR BETWEEN RIBS 9 AND 10 REPAIR STRAP REQUIRES REMOVAL FOR MATERIAL TYPE VERIFICATION REMOVED STRAP REF A310-200 SRM 51-40
- [SDR 07FDEA03758](https://openairdocs.org/sdr/07FDEA03758), Sep 14, 2007: STRINGER SPLICE. MISREPAIRED. STGR SPLICE REPAIR BETWEEN FRAME 72/73 ON STGR 56R REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA VISU
- [SDR 07FDEA03783](https://openairdocs.org/sdr/07FDEA03783), Sep 14, 2007: STRAP. MISINSTALLED. LEFT HORIZ STAB ON UPPER REAR SPAR BETWEEN RIBS 5 AND 8 REPAIR STRAP REQUIRES REMOVAL FOR MATERIAL TYPE VERIFICATION REMOVED DOUBLER STRAP DUE INCORRECT MATL IN
- [SDR 07FDEA03788](https://openairdocs.org/sdr/07FDEA03788), Sep 14, 2007: FRAME. CRACKED. FRAME CRACKED IN FASTENER HOLE AT FRAME 43A LOWER HOLE COMMON TO CRUCIFORM FITTING LT SIDE SEE JOB CARD 41X5271ALI FROM CABIN SIDE 1ST LAYER RUNNING IN THE 5 O`
- [SDR 07FDEA03786](https://openairdocs.org/sdr/07FDEA03786), Sep 14, 2007: FRAME. CRACKED. FRAME CRACKED IN FASTENER HOLE AT FRAME 42A LOWER HOLE COMMON TO CRICIFORM FITTING SEE JOB CARD 41 BY 5271ALI. RT SIDE FROM CABIN SIDE THE FIRST LAYER RUNNING I
- [SDR 07FDEA03753](https://openairdocs.org/sdr/07FDEA03753), Sep 14, 2007: STRAP. CRACKED. LT FWD PAX/CREW DOOR CUTOUT, HFEC INSPECTION INDICATES CRACK/CORROSION IN 5 LOCATIONS ALONG EDGE OF LOWER CORNER STRAPS AS FOLLOWS; (1) FWD LOWER CORNER- ONE 1/
- [SDR 07FDEA03749](https://openairdocs.org/sdr/07FDEA03749), Sep 14, 2007: STRAP. CRACKED. AREA IS RT FWD PAX/CREW DOOR CUTOUT. 1 1/8 INCH CRACK WITH POSSIBLE EXFOLIATION CORROSION EXISTS ALONG TOP EDGE OF FWD CORNER STRAP, BEGINNING APPROX 1 1/8 INCH
- [SDR 07FDEA03727](https://openairdocs.org/sdr/07FDEA03727), Sep 14, 2007: STRAP. CRACKED. AREA IS RT FWD PAX/CREW DOOR CUTOUT, 3 5/8 INCH CRACK WITH POSSIBLE EXFOLIATION CORROSION EXISTS ALONG TOP EDGE OF AFT CORNER STRAP, BEGINNING 1" FROM FWD EDGE 
- [SDR 07FDEA03131](https://openairdocs.org/sdr/07FDEA03131), Aug 26, 2007: SEAT TRACK. SHEARED. MAIN CABIN RIGHT SEAT TRACK Y-1959 AT FRAME 47 LUGS ARE BROKE OUT.
- [SDR 07FDEA03053](https://openairdocs.org/sdr/07FDEA03053), Aug 22, 2007: SEAT TRACK. DAMAGED. MAIN CABIN RT SEAT TRACK NR Y-1456 AT FRAME C63 LUGS BROKEN OUT. 09-11-07 REMOVED DAMAGED SECTION OF SEAT TRACK IAW A310 SRM 53-10-16. INSTALLED NEW SECTION OF 
- [SDR 07FDEA02155](https://openairdocs.org/sdr/07FDEA02155), Jun 16, 2007: CONTROLLER. FAILED. ON CLIMB-OUT, AIRCRAFT DID NOT PRESSURIZE. BOTH FWD AND AFT REG NR 2 VALVES WERE STUCK FULL OPEN AND SHOWING AMBER ON THE ECAM. DUPLICATED PROBLEM AT GATE, REPL
- [SDR 06FDEA04328](https://openairdocs.org/sdr/06FDEA04328), Dec 27, 2006: SWITCH. FAILED. NR 2 ENG REV UNLK LIGHT AND ECAM WARNING CAME ON AT FL 360, STAYED ON AFTER LANDING AND SHUTDOWN. REPEAT GRIP, FOUND THE MASTER ACTUATOR SECONDARY LOCK SWITCH R
- [SDR 06FDEA2559](https://openairdocs.org/sdr/06FDEA2559), Jul 13, 2006: ENGINE. UNKNOWN. ON INITIAL POWER-UP FOR TAKEOFF NUMBER 2 ENG WAS VERY SLOW TO ACCELERATE. TERMINATED THE TAKEOFF AT APPROXIMATELY 20 KTS AND CLEARED THE RUNWAY. TAXI'D BACK TO 
- [SDR 05FDEA01850](https://openairdocs.org/sdr/05FDEA01850), Jul 7, 2005: WIRE. BROKEN. ABORTED TAKEOFF DUE TO ENG NR 2 FAILED TO STABILIZE AT 40 PERCENT POWER, WITH NR 1 ENG THROTTLE SET NORMALLY TO PRODUCE 40 PERCENT N1 THE NR 2 THROTTLE WAS THRE
- [SDR 05FDEA01044](https://openairdocs.org/sdr/05FDEA01044), Apr 17, 2005: TERMINAL BLOCK. LOOSE. ON CLIMB-OUT, NOTICED NR 2 EGT NEEDLE/ANALOGUE GAUGE FLUCTATING-RECEIVED ECAM FOR NR 2 ENG OVERLIMITS. PULLED POWER BACK. GAUGE STABILIZED THEN STARTED TO FLUCT
- [SDR 05FDEA00998](https://openairdocs.org/sdr/05FDEA00998), Apr 14, 2005: ARM. GOUGED. NR 7 RUDDER HINGE ATTACHMENT BRACE ( A-FRAME) HAS GOUGE MARKS AND WEAR MARKS AT ATTACHMENT BOLT. REMOVED AND REPLACED NR 7 HINGE ARM IAW A310-200 AMM 55-36-47-4
- [SDR 05FDEA00603](https://openairdocs.org/sdr/05FDEA00603), Mar 18, 2005: STRUCTURE. CORRODED. CORROSION FOUND UNDER THE NR 9 LATCH ROLLER FOR FWD CARGO DOOR. COMPLIED WITH EA 6-5310-86132.
- [SDR 05FDEA00602](https://openairdocs.org/sdr/05FDEA00602), Mar 18, 2005: SKIN. CRACKED. LEFT WING T/E BOTTOM SKIN HAS INDICATION OF CRACK ON I/B CORNER SIDE CUTOUT PANEL 581AB AS MARKED. COMPLIED WITH EA 6-5710-86028.
- [SDR 05FDEA00574](https://openairdocs.org/sdr/05FDEA00574), Mar 16, 2005: SKIN. CORRODED. CORR B/T STR 34-35 FROM FS 39 AFT APPROX 8 IN LT REF N00850. COMPLIED WITH EA 6-5315-86078.
- [SDR 05FDEA00493](https://openairdocs.org/sdr/05FDEA00493), Mar 10, 2005: FLOOR SUPPORT. CORRODED. BULK PIT FLOOR SUPPORT AT FR67 FROM 12 INCHES TO LT CTR TO 36 INCHES TO LT OF CTR, 4EA AREAS OF CORROSION EXTENDING UNDER FASTENER HEADS AS MARKED. REMOVED AND 
- [SDR 05FDEA00492](https://openairdocs.org/sdr/05FDEA00492), Mar 10, 2005: RIB. DAMAGED. UPON REMOVAL OF EXISTING REPAIR ON N/R N00817 ON RT ELEVATOR INBOARD T/E LWR SURFACE FOUND 2EA AREAS OF CORROSION .5 X .5 INCH 1 ON INBOARD SIDE OF REPAIR, 1 ON
- [SDR 05FDEA00439](https://openairdocs.org/sdr/05FDEA00439), Mar 8, 2005: PANEL. DAMAGED. RT WING PANEL 650JB HAS 4 EA ELONGATED REF N00522. REPAIRED PANEL 650JB IAW EA 6-5710-86051.
- [SDR 05FDEA00425](https://openairdocs.org/sdr/05FDEA00425), Mar 8, 2005: RIB. CRACKED. RT WING 4 IN IB OF RIB 30 L/E AREA AFT PANEL LANDING IS CRACKED REF N00636. REMOVED AND REPLACED LANDING IAW SRM 51-40-21 AND 51-72-10 AND DRW A57243955.
- [SDR 05FDEA00447](https://openairdocs.org/sdr/05FDEA00447), Mar 8, 2005: SKIN. CORRODED. BULK PIT UNDER FLOOR AREA FS 69 STR 48 LT HAS AN AREA THAT EXTEND 2 INCHES FWD OF FS 69 OF CORROSION EXTENDING UNDER SHEAR TIE. REMOVED SHEAR TIE AND STRINGER S
- [SDR 05FDEA00477](https://openairdocs.org/sdr/05FDEA00477), Mar 8, 2005: SKIN. CORRODED. BULK PIT UNDER FLOOR AREA FR69 STG48L HAS AN AREA THAT EXTEND 2" FWD OF FR 69 OF CORROSION EXTENDING UNDER SHEAR TIE. REMOVED SHEAR TIE AND STRINGER SECTION IAW
- [SDR 05FDEA00453](https://openairdocs.org/sdr/05FDEA00453), Mar 8, 2005: ANGLE. CORRODED. THS ACTUATOR STRUCTURAL HOUSING HAS APPROX 12 INCH OF CORROSION (10 EA. AREAS). REMOVED CORROSION IN 10 EA AREAS ON THS ACTUATOR STRUCTURAL HOUSING. ALL AREAS W
- [SDR 05FDEA00452](https://openairdocs.org/sdr/05FDEA00452), Mar 8, 2005: SHEAR TIE. CORRODED. BULK PIT UNDER FLOOR STG 55L FROM FS 65 TO FS 66 HAS CORROSION AND CORROSION. EXTENDS BETWEEN SPLICE ANGLE AND STG AND UNDER SHEAR TIE AT FS 66. REMOVED CORROSI
- [SDR 05FDEA00451](https://openairdocs.org/sdr/05FDEA00451), Mar 8, 2005: FLOORBEAM. CORRODED. AFT PIT FLOOR FS 66 10 INCH TO RT OF CTR HAS A 5 INCH BY 2 INCH AREA OF CORROSION. REMOVED CORROSION PER A310-200 SRM 51-74-10. CORROSION OUT OF LIMITS PER SRM 
- [SDR 05FDEA00450](https://openairdocs.org/sdr/05FDEA00450), Mar 8, 2005: SKIN. CORRODED. AFT PIT UNDER FLOOR 16 INCH FWD OF FS 54.1, STG 47R HAS CORROSION. REMOVED CORROSION IAW A310-200 SRM 51-74-10. AREA WAS OUT OF LIMITS IAW A310-200 SRM 53-10-00
- [SDR 05FDEA00449](https://openairdocs.org/sdr/05FDEA00449), Mar 8, 2005: SHEAR TIE. CORRODED. BULK PIT UNDER FLOOR STG 53R FROM 1 INCH FWD OF 66 TO FR 67 HAS CORROSION EXTENDING UNDER SHEAR TIE AT FR 66 AND EXTENDING UNDER FASTENERS IN SEVERAL AREAS. REM
- [SDR 05FDEA00448](https://openairdocs.org/sdr/05FDEA00448), Mar 8, 2005: STRUCTURE. CORRODED. AFT PIT UNDER FLOOR FROM 12 INCH FWD OF FS 59 TO 3 INCHES FWD OF FS 59 STG44L HAS CORROSION. REMOVED CORROSION IAW A310-200 SRM 51-74-10. THE AREA WAS FOUND OUT
- [SDR 05FDEA00443](https://openairdocs.org/sdr/05FDEA00443), Mar 8, 2005: FLAP TRACK. CORRODED. RT WING FLAP O/B UPPER SURFACE AT NR 3 FLAP TRACK AND NR 4 FLAP TRACK HAS 2 EA AREAS OF NOTED CORROSION REF N00771. REMOVED CORR IAW SRM 51-74-10, FOUND IN LIMI
- [SDR 05FDEA00442](https://openairdocs.org/sdr/05FDEA00442), Mar 8, 2005: SKIN. PUNCTURED. RT WING I/B FLAP UPPER SURFACE 3.9 IN FROM T/E AND 30 IN FROM I/B END SKIN PUNCTURED REF N00914. REPAIRED FLAP IAW SRM 57-52-12 FIG 4D.
- [SDR 05FDEA00441](https://openairdocs.org/sdr/05FDEA00441), Mar 8, 2005: ATTACH FITTING. CORRODED. VERTICAL STAB UPPER EDGE LEFT AND RIGHT FORE TO AFT HAS CORROSION AROUND CAP ATTACH FASTENER HOLES REF N00734. REMOVED AND REPLACED RT CHORD IAW SRM 51-40-21 AN
- [SDR 05FDEA00440](https://openairdocs.org/sdr/05FDEA00440), Mar 8, 2005: DOUBLER. DAMAGED. REPAIR ON RT ELEVATOR I/B T/E LOWER SURFACE REQUIRES EVALUATION REF N00817. REMOVED EXISTING REPAIR AND INSTALLED CORRECT REPAIR IAW SRM 55-21-11 CONF 1 FIG 203
- [SDR 05FDEA00438](https://openairdocs.org/sdr/05FDEA00438), Mar 8, 2005: PANEL. DAMAGED. RT WING PANEL 650KB HAS 4 EA ELONGATED HOLES REF N00521. REPAIRED PANEL IAW EA 6-5710-86051.
- [SDR 05FDEA00437](https://openairdocs.org/sdr/05FDEA00437), Mar 8, 2005: PANEL. DAMAGED. LT WING PANEL 550HB HAS 2 EA ELONGATED HOLES REF N00520. REPAIRED HOLES IAW EA 6-5710-85051.
- [SDR 05FDEA00436](https://openairdocs.org/sdr/05FDEA00436), Mar 8, 2005: PANEL. DAMAGED. RT WING PANEL 650HB HAS 3 EA ELONGATED HOLES REF N00523. REPAIRED PANEL 650HB IAW EA 6-5710-86051.
- [SDR 05FDEA00426](https://openairdocs.org/sdr/05FDEA00426), Mar 8, 2005: RIB. CRACKED. RT WING L/E UPPER SIDE OF PANEL LANDING, LANDING FOR PANEL HAS 2 EA CRACKS AT 11 IN I/B OF RIB 14 AND 11 IN O/B OF RIB 14 REF N00631. REMOVED AND REPLACED PANEL
- [SDR 05FDEA00424](https://openairdocs.org/sdr/05FDEA00424), Mar 8, 2005: DOOR. DAMAGED. NOSE LANDING GEAR DOORS HAS STRUCTURAL DAMAGE REF N00748. REPAIRED RT GEAR DOORS IAW SRM 52-82-11 C1 FIG 201.
- [SDR 05FDEA00423](https://openairdocs.org/sdr/05FDEA00423), Mar 8, 2005: SKIN. CRACKED. RT WING T/E SKIN HAS A .4 CRACK ON IB CORNER OF CUTOUT FOR PANEL 681 AB REF N00265. REPAIRED SKIN IAW EA 6-5710-86028.
- [SDR 05FDEA00422](https://openairdocs.org/sdr/05FDEA00422), Mar 8, 2005: SKIN. DAMAGED. REPAIR FUSELAGE AT LT ELEVATOR T/E AFT FROM OB END HAS NO DATA REF N00806. REMOVED AND INSTALLED CORRECT REPAIR IAW EA 6-5100-87090 REF A310 SRM 55-21-11, REPAI
- [SDR 05FDEA00421](https://openairdocs.org/sdr/05FDEA00421), Mar 8, 2005: SEAT TRACK. CORRODED. NR 4 SEAT TRACK LT OF CENTER FROM FS 16 TO FS 18 HAS CORROSION REF N00519. REMOVED AND REPLACED SEAT TRACK FROM FS 16 TO FS 18 IAW SRM 51-40-21 AND EA 6-5310-86
- [SDR 05FDEA00420](https://openairdocs.org/sdr/05FDEA00420), Mar 8, 2005: SEAT TRACK. CORRODED. MDC NR 4 SEAT TRACK RT OF CENTER AT FR19 ON I/B SPLICE HAS CORROSION ON UPPER SURFACE. REMOVED AND REPLACED SPLICE ANGLE AT FR19 IAW SRM 51-40-21.
- [SDR 05FDEA00419](https://openairdocs.org/sdr/05FDEA00419), Mar 8, 2005: PLATE. CORRODED. BULK CARGO DOOR CUTOUT ON LWR FWD TOP EDGE OF SCUFF PLATE SURFACE CORROSION. REMOVED SCUFF PLATE AND REMOVED CORROSION IAW SRM 51-74-10 FOUND IN LIMITS IAW SRM 
- [SDR 05FDEA00418](https://openairdocs.org/sdr/05FDEA00418), Mar 8, 2005: PANEL. CRACKED. UPON REMOVAL OF LANDING AT RT WING HINGE PANEL ON L/E FOUND PANEL LANDING CRACKED REF N00915. REMOVED AND REPLACED PANEL LANDING IAW SRM 51-40-21 AND DRW A572-4

All 97: https://openairdocs.org/deregistered/N446FE-2013-07-29/reports.md

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20030820023929I](https://openairdocs.org/incident/20030820023929I), Aug 20, 2003: Airbus A310222 (N446FE), Columbus, OH, Minor damage. (-23) While enroute right side sliding window heat power cord caught fire. Switch was turned off and fire was extinguished. Landed klck. The maintenance action…

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