# N716FD: Airbus A300 B4-622, registration cancelled 2024-06-27

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: June 27, 2024
- Status when cancelled: Valid registration
- Airframe: [Airbus A300 B4-622](https://openairdocs.org/model/airbus-a300-b4-622) (registry code 3940012)
- Data sheets: [TCDS A35EU](https://openairdocs.org/tcds/A35EU) (OpenAirDocs)
- Serial number: 358
- Type of aircraft: Fixed wing multi engine
- Certificate issued: August 1, 2002
- Last registry action: April 21, 2023
- Mode S code: A992D8
- 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/N716FD
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=716FD
- Page: https://openairdocs.org/deregistered/N716FD-2024-06-27

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 A300 B4-622: https://openairdocs.org/model/airbus-a300-b4-622.md

## Service difficulty reports (110, newest 50)

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

- [SDR FDEA201403120490](https://openairdocs.org/sdr/FDEA201403120490), Mar 12, 2014: SMOKE DETECTOR. FALSE INDICATION. RECEIVED AVIONICS SMOKE WARNING AT CRUISE ALTITUDE. AFTER INITIAL STEADY WARNING THE WARNING BECAME INTERMITTENT. NO SIGN OF SMOKE THROUGH THE SNIFFER.
- [SDR FDEA201402270411](https://openairdocs.org/sdr/FDEA201402270411), Feb 27, 2014: PANEL. CRACKED. RIGHT WING CENTER WING BOX REAR SPAR & BOTTOM PANEL WITH A CRACK SIGNAL. REAMED THE INTERNAL FITTING ONLY STEP BY STEP 0.4 MM PER SRM 51-40-44 AND COMPLIED WITH
- [SDR FDEA201402270410](https://openairdocs.org/sdr/FDEA201402270410), Feb 27, 2014: PANEL. CRACKED. LEFT WING CENTER WING BOX REAR SPAR & BOTTOM PANEL WITH A CRACK SIGNAL. REAMED THE CRACKED LAYERS FROM INTERNAL TO EXTERNAL PER SRM 51-40-44 AND COMPLIED WITH E
- [SDR FDEA201402270409](https://openairdocs.org/sdr/FDEA201402270409), Feb 27, 2014: PANEL. CRACKED. LEFT WING CENTER WING BOX REAR SPAR & BOTTOM PANEL WITH A CRACK SIGNAL. REAMED THE PICK-UP ANGLE AND LOWER KEEL BEAM ONLY STEP BY STEP 0.4MM PER SRM 51-40-44 AN
- [SDR FDEA201402270408](https://openairdocs.org/sdr/FDEA201402270408), Feb 27, 2014: STRUCTURE. CRACKED. CENTER WING BOX REAR SPAR & BOTTOM PANEL CRACKED. REPAIRED IAW EA6-5710-T0306021 PT1. MAJOR REPAIR IAW GMM6-2-100.
- [SDR FDEA201402270407](https://openairdocs.org/sdr/FDEA201402270407), Feb 27, 2014: FRAME. CRACKED. LEFT WING CTR WING BOX REAR SPAR & BOTTOM PANEL CRACKED. REPAIRED IAW EA 6-5710-T0306021 PT1. MAJOR REPAIR IAW GMM6-2-100
- [SDR FDEA201402240393](https://openairdocs.org/sdr/FDEA201402240393), Feb 24, 2014: SKIN. WORN. RIGHT WING, RIBS 7 - 8 LOWER SKIN WORN. REPAIRED IAW EA 6-5730-T0305940 PART1. MAJOR REPAIR IAW GMM6-2-100.
- [SDR FDEA201402240392](https://openairdocs.org/sdr/FDEA201402240392), Feb 24, 2014: SKIN. WORN. LEFT WING RIB 7 - 8 LOWER SKIN WORN. REPAIRED IAW DWG R57150532 AND INSTALLED BUSHINGS IAW DWG R57150532. MAJOR REPAIR IAW GMM6-2-100.
- [SDR FDEA201402240390](https://openairdocs.org/sdr/FDEA201402240390), Feb 24, 2014: SKIN. CRACKED. NOSE LANDING GEAR WW RT AFT LOWER CUTOUT SKIN ONE EACH HOLE FOUND CRACKED. REPAIRED IAW EA 6-5330-T0305901 PART1. MAJOR REPAIR IAW GMM6-2-100.
- [SDR FDEA201402240389](https://openairdocs.org/sdr/FDEA201402240389), Feb 24, 2014: FRAME. CRACKED. JUNCTION BETWEEN CTR WING BOX & CRUCIFORM FITTING, FOUND FRAME 43 CRACKED. REPAIRED IAW EA 6-5710-T0305954 PART 1. MAJOR REPAIR IAW GMM 6-2-100.
- [SDR FDEA201402240388](https://openairdocs.org/sdr/FDEA201402240388), Feb 24, 2014: FRAME. CRACKED. JUNCTION BETWEEN CTR WING BOX & CRUCIFORM FITTING, FOUND FRAME 42 CRACKED. REPAIRED IAW EA6-5710-T0305954 PART 1. MAJOR REPAIR IAW GMM 6-2-100
- [SDR FDEA201402240387](https://openairdocs.org/sdr/FDEA201402240387), Feb 24, 2014: FRAME. CRACKED. JUNCTION BETWEEN CENTER WING BOX & CRUCIFORM FITTING, FOUND FRAME 41 CRACKED. REPAIRED EA 6-5710-T0305954. MAJOR REPAIR IAW GMM 6-2-100
- [SDR FDEA201402210380](https://openairdocs.org/sdr/FDEA201402210380), Feb 21, 2014: FRAME. CRACKED. MAIN DECK CARGO FRAME 52 FOUND CRACKED FROM FASTERNER HOLE AT STRINGER 27L. REAMED THROUGH ALL LAYERS TO REMOVE CRACK AND COMPLIED WITH EA 6-5310-T0305807 PT1. 
- [SDR FDEA201402170343](https://openairdocs.org/sdr/FDEA201402170343), Feb 17, 2014: DOOR FRAME. CORRODED. AFT CARGO DOOR FWD CUTOUT FRAME CORRODED AT FR 59A BETWEEN STRINGER 42R - STRINGER 43R. REMOVED CORROSION IAW A300-600 SRM51-74-10 & REPAIR IAW EA6-5310-T030587
- [SDR FDEA201402140318](https://openairdocs.org/sdr/FDEA201402140318), Feb 14, 2014: SKIN. CRACKED. SKIN, FRAME 54, STRINGER 36 & 44, FOUND WITH A CRACK SIGNAL. REPAIRED IAW EA 6-5330-T0305912A PT1. MAJOR REPAIR IAW GMM 6-2-100.
- [SDR FDEA201402140317](https://openairdocs.org/sdr/FDEA201402140317), Feb 14, 2014: SKIN. CRACKED. SKIN AT FRAME 54, STRINGER 36 & 44, SHOWS A CRACK SIGNAL AT BUTT JOINT. REPAIRED IAW EA 6-5330-T0305912A PT1. MAJOR REPAIR IAW GMM 6-2-100
- [SDR FDEA201402130313](https://openairdocs.org/sdr/FDEA201402130313), Feb 13, 2014: SKIN. DENTED. LEFT WING OTBD SIDE CENTER FLAP LOWER SKIN FOUND A DENTED BETWEEN RIB 9 - 10. FABRICATED REPAIR DOUBLER IAW SRM 57-50-00/201 FIG205 AND INSTALLED IAW SRM 57-50-
- [SDR FDEA201402030238](https://openairdocs.org/sdr/FDEA201402030238), Feb 3, 2014: SUPPORT ANGLE. GOUGED. AFT CARGO COMPARTMENT FRAME 60 CROSS FLOOR BEAM LOWER SUPPORT ANGLE WITH TWO EACH DEEP GOUGES AT ABOUT Y 1470 LOCATION. REMOVED THE DAMAGE ANGLE PER A300-600 SR
- [SDR FDEA201402030242](https://openairdocs.org/sdr/FDEA201402030242), Feb 3, 2014: SUPPORT FITTING. CRACKED. AFT CARGO COMPARTMENT FRAME 63 CROSS FLOOR BEAM LOWER SUPPORT FITTING WITH A CRACK AT ABOUT Y 1470, LOCATION CRACK LENGTH 0.35 INCHES. REMOVED THE DAMAGED FITTI
- [SDR FDEA201402030240](https://openairdocs.org/sdr/FDEA201402030240), Feb 3, 2014: SUPPORT FITTING. CRACKED. AFT CARGO COMPARTMENT FRAME 60 CROSS FLOOR BEAM LOWER SUPPORT FITTING WITH A CRACK AT ABOUT Y 1470, LOCATION CRACK LENGTH 0.3 INCHES. REMOVED THE DAMAGED FITTIN
- [SDR FDEA201402020233](https://openairdocs.org/sdr/FDEA201402020233), Feb 2, 2014: STRINGER. CORRODED. AFT CARGO FRAME 60 - 61, STRINGER 46R, STRINGER CORRODED. REPLACED THE CORRODED STRINGER WITH A NEW ONE PER A300-600 SRM51-40-21 AT AFT CARGO FR58-FR65, S-46R L
- [SDR FDEA201402020234](https://openairdocs.org/sdr/FDEA201402020234), Feb 2, 2014: STRINGER. CRACKED. AFT CARGO COMPARTMENT STRINGER 47RT, STRINGER CRACK AT FRAME 59 LOCATION. REPAIRED THE DAMAGED STRINGER PER A300-600 SRM53-10-14 PARA 4 A FIG201 AT AFT CARGO CO
- [SDR FDEA201402020236](https://openairdocs.org/sdr/FDEA201402020236), Feb 2, 2014: FITTING. CRACKED. AFT CARGO COMPARTMENT FRAME 63A LOWER FRAME FITTING CRACK BETWEEN STRINGER 44R - STRINGER 46R. REMOVED THE DAMAGED FITTING PER A300-600SRM51-40-21. INSTALLED TH
- [SDR FDEA201402020235](https://openairdocs.org/sdr/FDEA201402020235), Feb 2, 2014: SUPPORT BEAM. CRACKED. BULK CARGO COMPARTMENT Y 525 LONGITUDINAL SUPPORT BEAM FOUND CRACK BETWEEN FRAME 65 - FRAME 66. REMOVED THE CRACK SUPPORT BEAM PER A300-600 SRM51-40-21. INSTALL
- [SDR FDEA201401290214](https://openairdocs.org/sdr/FDEA201401290214), Jan 29, 2014: SKIN. CORRODED. FORWARD CARGO BAY DOOR CUTOUT FITTING CORRODED BETWEEN FRAMES 23 - 24, STRINGERS 49R - 54L. CORROSION REMOVED AND FOUND OUT OF LIMITS. REPAIRED IAW SRM 53-13-12
- [SDR FDEA201401270203](https://openairdocs.org/sdr/FDEA201401270203), Jan 27, 2014: ROLLER TRACK. CRACKED. AFT CARGO BAY DOOR SILL AREA ROLLER TRACK LOWER SURFACE FOUND CRACKED AT FRAME 63A. CRACK LENGTH 1.5 INCHES. REPLACED IAW SRM 51-40-21 & DWG A25772929. MAJOR RE
- [SDR FDEA201401240189](https://openairdocs.org/sdr/FDEA201401240189), Jan 24, 2014: FLOOR SUPPORT. CORRODED. MAIN DECK CARGO FLOOR SUPPORT CORRODED BETWEEN FRAMES 13 - 13A,Y D TO E. REMOVED FLOOR SUPPORT IAW SRM 51-40-21. INSTALLED NEW FLOOR SUPPORT IAW SRM 51-40-21
- [SDR FDEA201401210148](https://openairdocs.org/sdr/FDEA201401210148), Jan 21, 2014: FLOORBEAM. CORRODED. BULK CARGO BAY FRAME 66 FLOORBEAM CORRODED. REMOVED FLOORBEAM IAW SRM 51-40-21. INSTALLED NEW FLOORBEAM IAW SRM 51-72-10. MAJOR REPAIR IAW GMM 6-2-100.
- [SDR FDEA201401170125](https://openairdocs.org/sdr/FDEA201401170125), Jan 17, 2014: SILL. CORRODED. AFT CARGO DOOR SILL CORRODED. REMOVED AND REPLACED DOOR SILL IAW SRM 53-17-18/201 2.
- [SDR FDEA201201110100](https://openairdocs.org/sdr/FDEA201201110100), Jan 11, 2012: BATTERY. INOPERATIVE. DURING SERVICE CHECK, FOUND COURIER COMPARTMENT INTERIOR EMERGENCY LIGHTS, TEST FUNCTION INOPERATIVE. REPLACED EMERGENCY POWER SUPPLY BATTERY IAW MM 33-51-14-04
- [SDR FDEA201112065175](https://openairdocs.org/sdr/FDEA201112065175), Dec 6, 2011: CYLINDER. FAILED. AFTER TAKE-OFF, DURING GEAR RETRACTION, AMBER LIGHT DOOR OPEN ON FORWARD PANEL AND UPPER PANEL, VIBRATIONS AFTER LEVEL-OFF AT FL330, AND LOWER ALTITUDES UNTIL L
- [SDR FDEA201112065172](https://openairdocs.org/sdr/FDEA201112065172), Dec 6, 2011: WARNING LIGHT. FALSE ACTIVATION. AFTER TAKEOFF AND DURING GEAR RETRACTION, AN AMBER NOSE DOOR LIGHT ILLUMINATED ON FORWARD PANEL AND OVERHEAD PANEL. LIGHTS WENT OUT ON TAXI IN. TROUBLESHOT IAW 
- [SDR FDEA201107012530](https://openairdocs.org/sdr/FDEA201107012530), Jul 1, 2011: SKIN. DAMAGED. UPON REMOVAL OF SKIRT ANGLE ON NR 2 PYLON INBD SIDE, 2 EA DOUBLE DRILLED HOLES, 1 HOLE WITHIN .1 OF ANOTHER HOLE. REPAIRED HOLES IAW TD 70548824/012/2011, ISSUE
- [SDR FDEA201106222385](https://openairdocs.org/sdr/FDEA201106222385), Jun 22, 2011: ROLLER TRACK. CORRODED. L1 ROLLER TRAY IN FWD CARGO COMPT BETWEEN FRAMES 29 AND 30 HAS 2 EA AREAS OF CORROSION ON OTBD FLANGE BLENDED CORROSION IAW SRM 517-74-10 AND FOUND CORROSION TO
- [SDR FDEA201106172324](https://openairdocs.org/sdr/FDEA201106172324), Jun 17, 2011: SKIN. MISREPAIRED. FLUSH REPAIR LOCATED ON LT WING CENTER FLAP UPPER T/E SKIN BETWEEN RIBS 22 TO 24 & AFT OF REAR SPAR IS NOT A VALID REPAIR. REMOVED FLUSH REPAIR AND REPAIRED SKI
- [SDR FDEA201106172319](https://openairdocs.org/sdr/FDEA201106172319), Jun 17, 2011: SKIN. GOUGED. RT HORIZONTAL STAB L/E PANEL 341CB HAS SEVERAL SMALL GOUGES AND NICKS ON L/E FROM INBD TO OTBD END. SMOOTHED AND BLENDED 4 AREAS OF L/E AREA. NR 1 AND 4 ARE WIT
- [SDR FDEA201106162294](https://openairdocs.org/sdr/FDEA201106162294), Jun 16, 2011: ROLLER TRACK. CORRODED. CARGO ROLLER TRAY IN FWD CARGO COMPT. LT CENTER CORRODED AT FRAMES 23 AND 18 AFTER CORROSION REMOVAL, ROLLER TRAY FOUND TO BE OUT OF LIMITS IAW SRM 53-10-15, PG
- [SDR FDEA201106112208](https://openairdocs.org/sdr/FDEA201106112208), Jun 11, 2011: SKIN. CORRODED. 8 SQ IN OF FUSELAGE INTERNAL SKIN CORROSION ON FWD CARGO AFT BILGE BETWEEN STR 55 AND STR 54R FWD OF FR 38.2. REMOVED CORROSION IAW SRM 51-74-10. FOUND AREA OUT
- [SDR FDEA201106092176](https://openairdocs.org/sdr/FDEA201106092176), Jun 9, 2011: ROLLER TRACK. CORRODED. ROLLER TRAY 2L INBD FLANGE HAS CORROSION BETWEEN FRAMES 34 AND 35 IN FWD CARGO COMPT. REMOVED LEVEL 1 CORROSION. REMOVED DAMAGED SECTION OF ROLLER TRACK IN FWD 
- [SDR FDEA201106092177](https://openairdocs.org/sdr/FDEA201106092177), Jun 9, 2011: ROLLER TRACK. CORRODED. ROLLER TRACK 2R BETWEEN FRAMES 29 AND 30 CORRODED IN FWD CARGO COMPT. AFTER REMOVAL OF LEVEL 1 CORROSION, TRACK WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-10-15 P
- [SDR FDEA201106092179](https://openairdocs.org/sdr/FDEA201106092179), Jun 9, 2011: ROLLER TRACK. DAMAGED. FWD CARGO COMPT. ROLLER TRAY R1 HAS DOUBLE DRILLED HOLE BETWEEN FRAME 35 AND 36 REMOVED AND REPLACED ROLLER TRACK SECTION IAW SRM 53-10-15 PG 211/212.
- [SDR FDEA201106082159](https://openairdocs.org/sdr/FDEA201106082159), Jun 8, 2011: FLOOR SUPPORT. CORRODED. UPON REMOVAL OF ROLLER TRAY ON N01207 IN FWD CARGO COMPT BETWEEN FR 35 AND 36, FOUND CORROSION ON TOP OF FLOOR SUPPORT AT FRAME 35. REPAIRED FLOOR SUPPORT AT FR
- [SDR FDEA201106062135](https://openairdocs.org/sdr/FDEA201106062135), Jun 6, 2011: FRAME. CORRODED. AFT PRESSURE BULKHEAD BOTTOM FWD SIDE AT FR 80/82 CIRCUMFERENTIAL STRAP CORRODED 7 IN LENGTH X 4 IN WIDTH BETWEEN STR 54R TO 56R. REMOVED CIRCUMFERENTIAL STRAP 
- [SDR FDEA201105191879](https://openairdocs.org/sdr/FDEA201105191879), May 19, 2011: ROLLER TRACK. MISREPAIRED. EXISTING ROLLER TRACK REPAIR HAS INCORRECT ANGLES SHAPE AND THICKNESS AND MS20470D6 RIVETS INSTALLED FROM BOTTOM SURFACE UP AND NO COUNTERSUNK RIVETS AT OUTER F
- [SDR FDEA201105191881](https://openairdocs.org/sdr/FDEA201105191881), May 19, 2011: STRINGER. MISREPAIRED. STRINGER 53L BETWEEN FRAMES 63 TO 64 EXISTING REPAIR SPLICE ANGLE HAS INCORRECT MATERIAL THICKNESS INSTALLED REMOVED AND REPLACED EXISTING REPAIR SPLICE ON STRI
- [SDR FDEA201105191880](https://openairdocs.org/sdr/FDEA201105191880), May 19, 2011: STRINGER. MISINSTALLED. STRINGER 52L BETWEEN FRAMES 63 TO 64 REPAIR SPLICE ANGLE HAS INCORRECT MATERIAL THICKNESS INSTALLED REMOVED AND REPLACED REPAIR SPLICE ANGLE ON STRINGER 52L/H B
- [SDR FDEA201105181872](https://openairdocs.org/sdr/FDEA201105181872), May 18, 2011: STRINGER SPLICE. FAILED. STRINGER 44 RT SPLICE ANGLE BETWEEN FRAMES 38.2 TO 39 HAS INCORRECT THICKNESS INSTALLED REMOVED AND REPLACED STRINGER 44RH SPLICE ANGLE BETWEEN FRAME 38.2 TO 39
- [SDR FDEA201105171857](https://openairdocs.org/sdr/FDEA201105171857), May 17, 2011: SEAT TRACK. MISREPAIRED. PREVIOUS REPAIR LOCATED INCORRECTLY BETWEEN FRAMES 60 AND 61 OTBD SIDE AT SEAT TRACK 2R -Y450. REMOVED AND REPLACED SEAT TRACK 2R -Y450 FROM FRAME 58 TO 62 WITH
- [SDR FDEA201105121832](https://openairdocs.org/sdr/FDEA201105121832), May 12, 2011: SKIN. PUNCTURED. LT ELEVATOR UPPER SURFACE AT STA 253/ RIB NR 8 UPPER SKIN HAS A HOLE PUNCTURE APPROX 0.25 IN. LONG THROUGH INTO HONEYCOMB. REPAIRED LT ELEVATOR UPPER SURFACE IA
- [SDR FDEA201009163501](https://openairdocs.org/sdr/FDEA201009163501), Sep 16, 2010: ENGINE. FAILED. NR 2 ENG CATASTROPHIC FAILURE. (DURING CRUISE, ECON, COST INDEX 55) MC1 U IAW POWERPLANT ENGINEER THIS ENGINE IS APPROVED FOR ENGINE CHANGE. NR 2 ENGINE CHANGED

All 110: https://openairdocs.org/deregistered/N716FD-2024-06-27/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 20050813025579I](https://openairdocs.org/incident/20050813025579I), Aug 13, 2005: Airbus A300B4622 (N716FD), Syracuse, NY. (-23) On 8/13/2005 at 22:54 edst an Airbus A-300 operated by fdea (flt 1685) while at cruise "got ecam #1 oil filter clog." The crew followed ecam and idled…

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