# N326FE: 1984 Mcdonnell-Douglas DC-10-30, registration cancelled 2021-07-03

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: July 3, 2021
- Status when cancelled: Registration expired, pending cancellation
- Airframe: [Mcdonnell-Douglas DC-10-30](https://openairdocs.org/model/mcdonnell-douglas-dc-10-30) (registry code 3023501)
- Engine: [GE CF6-50 series](https://openairdocs.org/engine/ge-cf6-50-series) (registry code 30018)
- Data sheets: [TCDS A22WE](https://openairdocs.org/tcds/A22WE), [TCDS E23EA](https://openairdocs.org/tcds/E23EA) (OpenAirDocs)
- Serial number: 47813
- Year built: 1984
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 5, 1997
- Certificate issued: July 28, 2008
- Last registry action: October 16, 2017
- Mode S code: A3851C
- Owner when cancelled: [Logistic Air Inc](https://openairdocs.org/faa-owner/LOGISTIC%20AIR%20INC)
- Location: [Fernley, NV](https://openairdocs.org/faa-place/NV/Fernley)
- Owner type: Corporation
- Owner's area on the map: 39.6708° N, 119.0064° W: Placed by OpenAirDocs at the center of ZIP code 89408, within about 12 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N326FE
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=326FE
- Page: https://openairdocs.org/deregistered/N326FE-2021-07-03

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 Mcdonnell-Douglas DC-10-30: https://openairdocs.org/model/mcdonnell-douglas-dc-10-30.md

## Service difficulty reports (16)

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

- [SDR 05FDEA03476](https://openairdocs.org/sdr/05FDEA03476), Oct 21, 2005: FLAP SYSTEM. MALFUNCTIONED. UPON CONFIG, A/C ROLLED LEFT REQ 3/4 DEFLECTION TO RIGHT TO HOLD A/C LEVEL. A/C WAS CONTROLLABLE TO TOUCHDOWN. ON POST FLIGHT WALK AROUND, DISCOVERED THAT THE M
- [SDR 04FDEA02464](https://openairdocs.org/sdr/04FDEA02464), Aug 13, 2004: HINGE BRACKET. DAMAGED. C/W WITH EA 8-5740-78234 WING LT OTBD FLAP OUTBD HINGE BRACKET, ACT MOUNT HOLES REPAIR P/N ARC0503. COMPLIED WITH EA 8-5740-78234 TO INCLUDE REV A WINGS LT OUTB
- [SDR 04FDEA02286](https://openairdocs.org/sdr/04FDEA02286), Jul 29, 2004: SUPPORT. CRACKED. R-1 AFT UPPER CHAIN GUARD BRACKET CRACKED. REMOVED AND REPLACED CHAIN GUARD BRACKET AND CHAIN GUARD IAW MM 52-11-09 AT MAE.
- [SDR 04FDEA02166](https://openairdocs.org/sdr/04FDEA02166), Jul 23, 2004: INTERCOSTAL. CORRODED. NOSE GEAR WHEEL WELL FWD PRESSURE BULKHEAD ACCESS DOOR 115AZ INSIDE BOTTOM CORRODED. REMOVED AND REPLACED INTERCOSTALS IAW SRM 51-31-01 AND SRM 51-35-01 ON N/R 
- [SDR 04FDEA02151](https://openairdocs.org/sdr/04FDEA02151), Jul 22, 2004: RIB. CRACKED. LEFT WING I/B LEADING EDGE ACCESS PANEL 516FE RIB WITH CRACK. REMOVED AND REPLACED STIFFENER IAW SRM 51-35-01.
- [SDR 04FDEA02150](https://openairdocs.org/sdr/04FDEA02150), Jul 22, 2004: RIB. CRACKED. RIGHT WING I/B LEADING EDGE ACCESS PANEL 616ET SEVERAL RIBS CRACKED. REMOVED CRACKED RIBS AND REPLACED WITH NEW RIBS IAW SRM 51-31-01. PAINTED IAW SRM 51-23-01.
- [SDR 04FDEA02149](https://openairdocs.org/sdr/04FDEA02149), Jul 22, 2004: FRAME. CRACKED. NR 2 ENGINE RIGHT CORE COWL FORTH RIB AFT CRACKED JUST ABOVE ACCESS DOOR. REMOVED DOUBLER IAW SRM 51-31-01. RECEIVED FROM WELD SHOP CORE COWLING FRAME WELDED BY
- [SDR 04FDEA02144](https://openairdocs.org/sdr/04FDEA02144), Jul 21, 2004: FITTING. CORRODED. COMPLY WITH EA 8-5750-79540; WINGS OUTBOARD FLAP, FLAP SPINDLE CARRIAGE SUPPORT FITTING CORROSION REPAIR, P/N ARC2177. COMPLIED WITH EA 8-5750-79540, WINGS OUTB
- [SDR 04FDEA02101](https://openairdocs.org/sdr/04FDEA02101), Jul 17, 2004: PLATE. CORRODED. FUSELAGE RT BASE PLATE INBOARD FLAP SUPPORT SURFACE CORROSION REPAIR P/N ANB7170-2. COMPLIED WITH EA 8-5310-80573.
- [SDR 04FDEA02100](https://openairdocs.org/sdr/04FDEA02100), Jul 17, 2004: FITTING. CORRODED. C/W EA 8-5720-79541 WINGS INBOARD FLAP SIDE LOAD SUPPORT FITTING CORROSION REPAIR P/N ANB7434. COMPLIED WITH EA 8-5720-79541.
- [SDR 04FDEA02086](https://openairdocs.org/sdr/04FDEA02086), Jul 15, 2004: HINGE. CORRODED. C/W EA 8-5740-80575 WINGS RT INBD FLAP OUTBD HINGE UPPER HOLE LUG CORROSION REPAIR P/N ARC0154-2. COMPLIED WITH EA 8-5740-80575.
- [SDR 04FDEA02084](https://openairdocs.org/sdr/04FDEA02084), Jul 15, 2004: FITTING. CORRODED. RIGHT MAIN GEAR DOOR FWD UPPER H-11 BOLT POSITION NR 1 PER DWG ARC2859 HAS GOUGES AND CORROSION. REMOVED FITTING AND FOUND TO BE OUT OF LIMITS. INSTALLED NEW FI
- [SDR 04FDEA02083](https://openairdocs.org/sdr/04FDEA02083), Jul 15, 2004: FITTING. GOUGED. NOSE WHEEL WELL RT OVERHEAD FLIGHT BRAKE FITTING HAS GOUGED AREAS. REMOVED AND REPLACED FITTING IAW DC10-30 M/M 32-42-02-7.
- [SDR 04FDEA02082](https://openairdocs.org/sdr/04FDEA02082), Jul 15, 2004: FITTING. GOUGED. NOSE WHEEL WELL LT OVERHEAD FLIGHT BRAKE FITTING HAS GOUGED AREAS. REMOVED AND REPLACED FITTING IAW DC-10-30 M/M 32-42-02-7.
- [SDR 04FDEA02070](https://openairdocs.org/sdr/04FDEA02070), Jul 13, 2004: VANE. GOUGED. COMPLY WITH EA 8-5710-79550 WINGS REWORK OF GOUGE IN OUTBD FLAP VANE SUPPORT RIB ARB1860-3. COMPLIED WITH EA 8-5710-79550 WINGS REWORK OF GOUGE IN OUTBD FLAP VA
- [SDR 04FDEA02041](https://openairdocs.org/sdr/04FDEA02041), Jul 10, 2004: LATCH. BENT. NR 3 ENG LEFT T/R UPPER LATCH ROD IS BENT. REMOVED AND REPLACED UPPER LATCH ROD IAW MM 78-32-19 AND 20-50-02 AT MAE.

## 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 20051020030999I](https://openairdocs.org/incident/20051020030999I), Oct 20, 2005: Doug DC1030 (N326FE), Minneapolis, MN, Minor damage. (-23) During approach, a 5-foot section of the left inboard flap vane separated from the aircraft, it was discovered missing during the post flight inspection.

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