# N611FE: 1993 Mcdonnell Douglas MD-11F, registration cancelled 2012-07-16

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: July 16, 2012
- Status when cancelled: First renewal notice
- Airframe: [Mcdonnell Douglas MD-11F](https://openairdocs.org/model/mcdonnell-douglas-md-11f) (registry code 3023600)
- Engine: [GE CJ610-8&9](https://openairdocs.org/engine/ge-cj610-8-9) (registry code 30014)
- Data sheets: [TCDS A22WE](https://openairdocs.org/tcds/A22WE) (OpenAirDocs)
- Serial number: 48604
- Year built: 1993
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: September 10, 1993
- Certificate issued: September 29, 1993
- Last registry action: October 21, 2008
- Mode S code: A7F2F7
- Owner when cancelled: [Wilmington Trust Company Trustee](https://openairdocs.org/faa-owner/WILMINGTON%20TRUST%20COMPANY%20TRUSTEE)
- Location: [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington)
- Owner type: Corporation
- Owner's area on the map: 39.7357° N, 75.5321° W: Placed by OpenAirDocs: center of Wilmington, DE, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N611FE
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=611FE
- Page: https://openairdocs.org/deregistered/N611FE-2012-07-16

From the FAA registry file of October 28, 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 Mcdonnell Douglas MD-11F: https://openairdocs.org/model/mcdonnell-douglas-md-11f.md

## Service difficulty reports (9)

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

- [SDR 08FDEA01662](https://openairdocs.org/sdr/08FDEA01662), Apr 29, 2008: SEAT TRACK. CORRODED. MAIN CARGO COMPT CENTER SEAT TRACK IS CORRODED ON THE BOTTOM AT FRAME 78. SPLICED IN A NEW SEAT TRACK SECTION IAW SRM 53-10-16; FIG 208.
- [SDR 97FDEA00309](https://openairdocs.org/sdr/97FDEA00309), May 25, 1997: HYDRAULIC LINE. FAILED. 97-0096, ONE HOUR AND 30 MINUTES INTO FLIGHT, GOT HYDRAULIC 1 OFF ALERT. SYSTEM QUANTITY SHOWS 2.6 AFTER 3.5 HOURS OF FLIGHT. GOT LEVEL 2 HYDRAULIC 1 FAIL ALERT
- [SDR 97FDEA00064](https://openairdocs.org/sdr/97FDEA00064), Jan 22, 1997: FIRE DETECTOR. MALFUNCTIONED. PASSING 11,000 GOT NR 1 ENG FIRE WARNING, AURAL AND BELL. DID NOT HAVE LIGHT IN HANDLE OR ANY OTHER INDICATION OF FIRE, EGT NORMAL. NO RISE IN EGT, SHUTDOWN AND
- [SDR 96FDEA01709](https://openairdocs.org/sdr/96FDEA01709), Dec 27, 1996: BULKHEAD FITTING. CRACKED. THE CENTER LANDING GEAR WHEEL WELL AREA HAS A CRACK AT THE RT BULKHEAD AND DRAG LINK VERTICAL SUPPORT FITTING AT STA 1453 AT X = - 31.50 CRACK MEASURES 13 AT LO
- [SDR 96FDEA01702](https://openairdocs.org/sdr/96FDEA01702), Dec 15, 1996: TUBE. BROKEN. DURING CRUISE, NR 3 HYDRAULIC SYSTEM FAILED (LOSS OF FLUID). PUMPS WERE TURNED OFF WITH 2.4 GALLONS REMAINING. REPLACED RT PUMP. CASE DRAIN REPLACED. P/N 224-94
- [SDR 96FDEA01541](https://openairdocs.org/sdr/96FDEA01541), Sep 27, 1996: ENGINE. FAILED. ENGINE FAILED INSPECTION PER EA 1-7220-31511 INSP OF FIRST STAGE BOOSTER VANES.
- [SDR 95FDEA01458](https://openairdocs.org/sdr/95FDEA01458), Sep 26, 1995: BRAKE ASSY. DAMAGE. REFERENCE NR 7015 - DURING REPLACEMENT OF WORN TIRE AND WHEEL ASSY ON POS NR 3, FOUND ROTORS ON BRAKE ASSY DAMAGED. ROTORS NR 3, 4 AND 5 ARE DELAMINATED. STATOR
- [SDR 95FDEA00008](https://openairdocs.org/sdr/95FDEA00008), Jan 8, 1995: CONNECTOR. CONTAMINATED. NRT - LANDING GEAR AURAL WARNING CAME ON AT 1500 FT ON CLIMB-OUT GEAR AND FLAP POSITIONS CONFIRMED UP NORMAL WARNING OFF WHEN GEAR WAS LOWERED FOR LANDING. FOUN
- [SDR 95FDEA00007](https://openairdocs.org/sdr/95FDEA00007), Jan 8, 1995: TRANSMITTER. MALFUNCTION. NRT - CONTINUOUS LANDING GEAR AURAL ALERT AT 1500 FT ON CLIMBOUT. GEAR UP INDICATIONS NORMAL, RECYCLED GEAR NO EFFECT, CONFIRMED GEAR/FLAPS UP ON CONFIG PAGE DU

## NTSB investigations (2)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB DCA97MA055](https://openairdocs.org/ntsb/DCA97MA055), Jul 31, 1997: McDonnell Douglas MD-11 (N611FE), Newark, NJ, destroyed. Probable cause: The captain's overcontrol of the airplane during the landing and his failure to execute a go-around from a destabilized flare. Contributing to the accident was the captain's concern with touching…
- [NTSB ANC95FA008](https://openairdocs.org/ntsb/ANC95FA008), Nov 4, 1994: Mcdonnell Douglas MD-11/F (N611FE), Anchorage, AK, substantial damage. Probable cause: THE FLIGHT CREW'S IMPROPER RECOVERY FROM A BOUNCED LANDING. FACTORS ASSOCIATED WITH THE ACCIDENT ARE THE FIRST OFFICER'S LACK OF FAMILIARITY WITH THE AIRPLANE, HIS FAILURE TO STABILIZE THE APPROACH,…

## FAA accident and incident reports (2)

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.

- [Accident 19970731020129A](https://openairdocs.org/incident/19970731020129A), Jul 31, 1997: Doug MD11F (N611FE), Newark, NJ, Destroyed. Aircraft bounced on landing, skidded down runway, came to rest inverted, caught fire, burned.
- [Accident 19941104040729A](https://openairdocs.org/incident/19941104040729A), Nov 4, 1994: Doug MD11F (N611FE), Anchorage, AK, Substantial damage. Landed hard. Bounced. Tail hit runway. Damaged aft fuselage. Unstabilized approach and improper shock servicing.

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