# N605GC: 1974 Mcdonnell Douglas DC-10-30F, registration cancelled 2016-12-13

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: December 13, 2016
- Status when cancelled: First renewal notice
- Airframe: [Mcdonnell Douglas DC-10-30F](https://openairdocs.org/model/mcdonnell-douglas-dc-10-30f) (registry code 3023504)
- Engine: [GE CF34 series](https://openairdocs.org/engine/ge-cf34-series) (registry code 30015)
- Data sheets: [TCDS A22WE](https://openairdocs.org/tcds/A22WE) (OpenAirDocs)
- Serial number: 47925
- Year built: 1974
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 9, 1996
- Certificate issued: April 13, 2011
- Last registry action: November 25, 2013
- Mode S code: A7DA6B
- Owner when cancelled: [International Trading Co Of Yukon Inc](https://openairdocs.org/faa-owner/INTERNATIONAL%20TRADING%20CO%20OF%20YUKON%20INC)
- Location: [Oklahoma City, OK](https://openairdocs.org/faa-place/OK/Oklahoma%20City)
- Owner type: Non-citizen corporation
- Owner's area on the map: 35.5813° N, 97.5737° W: Placed by OpenAirDocs at the center of ZIP code 73120, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N605GC
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=605GC
- Page: https://openairdocs.org/deregistered/N605GC-2016-12-13

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-10-30F: https://openairdocs.org/model/mcdonnell-douglas-dc-10-30f.md

## Service difficulty reports (11)

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

- [SDR G6OA071](https://openairdocs.org/sdr/G6OA071), Jul 22, 2003: BOLT. WORN. AIRCRAFT PERFORMED AN AIR RETURN SAFELY DUE TO UNABLE TO PRESSURIZE AFTER TAKE OFF. DURING TROUBLESHOOTINGFOUND GROUND SENSE ROD LOOSE. R/R UPPER BOLT PER MM 32
- [SDR G6OA059](https://openairdocs.org/sdr/G6OA059), Jan 11, 2002: BELLCRANK. WORN. ELEVATOR CONTROL CHECK DOWNWARD MOVEMENT BINDING DURING NOSE DOWN MOVEMENT. FOUND BENT AND WORN BELLCRANK ASSEMBLIES ON LEFT INBOARD ELEVATOR ACTUATOR. REMOVED 
- [SDR G6OA060](https://openairdocs.org/sdr/G6OA060), Jan 11, 2002: BRACKET. WORN. FOUND ELEVATOR CONTROL CHECK DOWNWARD MOVEMENT BINDING DURING NOSE DOWN MOVEMENT. FOUND BENT AND WORN BRACKET ASSEMBLIES ON LEFT INBOARD ELEVATOR. REMOVED AND R
- [SDR G60A040](https://openairdocs.org/sdr/G60A040), Dec 7, 1999: SEAL. LEAKING. CABIN ALTITUDE COULD NOT BE CONTROLLED IN AUTO, SEMI-AUTO, STANDBY, OR MANUAL POSITION. PERFORMED RAPID DEPRESSURIZATION/EMERGENCY DESCENT TO 11,000 FT, DUMPED 
- [SDR GTOAA036](https://openairdocs.org/sdr/GTOAA036), Sep 29, 1999: BATTERY. DISCHARGED. EMERGENCY LIGHT TEST DOES NOT COME ON WITH TEST. REMOVED AND REPLACED EMERGENCY BATTERY IAW MM 24-24-00. OPS CHECKED GOOD. (M)
- [SDR G6OA043](https://openairdocs.org/sdr/G6OA043), Feb 9, 1999: BOLT. LOOSE. NR 1 ENGINE FORWARD MOUNT TRUSS FITTING TO PYLON, HAS SIX LOOSE PYLON BOX BOLTS ON LOWER FORWARD SIDE, AND THREE HI-LOCKS ON LOWER FORWARD SHOWS EVIDENCE OF SPI
- [SDR G60A044](https://openairdocs.org/sdr/G60A044), Feb 9, 1999: BOLT. LOOSE. NR 3 ENGINE FORWARD MOUNT TRUSS FITTING TO PYLON LOWER FORWARD SIDE ATTACH BOLTS LOOSE. INSPECTED FORWARD MOUNT TRUSS FITTINGS AS PER DRAWING AVB 7011 '2' AND P
- [SDR G6OA024](https://openairdocs.org/sdr/G6OA024), Jul 1, 1998: CONNECTOR. LOOSE. THE FLIGHT CREW REPORTED THE NR 2 ENGINE PNEUMATIC MANIFOLD FAILURE LIGHT ILLUMINATED. ACCOMPLISHED EMERGENCY PROCEDURES PER AOM VOL 1. GROUND MAINTENANCE TROUB
- [SDR G6OA006](https://openairdocs.org/sdr/G6OA006), Feb 3, 1997: COMPUTER. MALFUNCTIONED. GVA - AFTER TAKEOFF, CREW REPORTED STALL SPEED WARNING ACCOMPANIED BY AUTO SLAT EXTENSION. CREW ACCOMPLISHED IRREGULAR PROCEDURES AND PULLED AUTO SLAT EXTEND CI
- [SDR G6OA005](https://openairdocs.org/sdr/G6OA005), Jan 28, 1997: GARLOC SEAL. DAMAGED. GVA - APPROXIMATELY 90 MINUTES AFTER TAKEOFF, CREW REPORTED LOSS OF NR 1 ENGINE OIL QUANTITY AND OIL PRESSURE FLUCTUATION OF 30-40 PSIG. ENGINE NR 1 WAS SHUT DO
- [SDR G60A004](https://openairdocs.org/sdr/G60A004), Dec 24, 1996: TR MOUNT. BROKE. NR 3 ENGINE THRUST REVERSER RHS CENTER BALL ACTUATOR ASSEMBLY FAILED TO RETRACT AFTER LANDING. THE BALL SCREW ACTUATOR MOUNT BRACKET BROKE OFF AND DAMAGED THE L

## 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.

- [Incident 20041226032429I](https://openairdocs.org/incident/20041226032429I), Dec 26, 2004: Doug DC1030F (N605GC), Miami, FL, Minor damage. (-23) "Industrial incident-no intent to fly" aircraft was being serviced with fuel. The fuel truck was positioned under the wing. During the servicing the…
- [Incident 20041011027469I](https://openairdocs.org/incident/20041011027469I), Oct 11, 2004: Doug DC1030F (N605GC), Miami, FL, Minor damage. (-23) During walk around found a hole in the side of the right forward fuselage near cargo door. Found paint from aircraft on loader that was loading the…

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.