# N323FE: 1979 Mcdonnell-Douglas DC-10-30, registration cancelled 2012-07-23

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: July 23, 2012
- Status when cancelled: First renewal notice
- 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: 47811
- Year built: 1979
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: February 25, 1997
- Certificate issued: October 1, 2008
- Last registry action: October 1, 2008
- Mode S code: A379F7
- Owner when cancelled: [Project Orbis International Inc](https://openairdocs.org/faa-owner/PROJECT%20ORBIS%20INTERNATIONAL%20INC)
- Location: [New York, NY](https://openairdocs.org/faa-place/NY/New%20York)
- Owner type: Corporation
- Owner's area on the map: 40.7553° N, 73.9927° W: Placed by OpenAirDocs at the center of ZIP code 10018, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N323FE
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=323FE
- Page: https://openairdocs.org/deregistered/N323FE-2012-07-23

From the FAA registry file of October 31, 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 (31)

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

- [SDR 04FDEA03390](https://openairdocs.org/sdr/04FDEA03390), Dec 7, 2004: SEAL. FAILED. NR 3 PNEU MANIFOLD FAILURE LIGHT ILLUMINATED INTERMITTENTLY SHORTLY AFTER T/O (NR 3 PNEU SUPPLY ON DUE TO WING ANTI-ICE REQUIRED FOR T/O). PHASE IS ACCOMPLISHED
- [SDR 04FDEA02023](https://openairdocs.org/sdr/04FDEA02023), Jul 7, 2004: SKIN. DENTED. RIGHT HAND LOWER FUSELAGE SKIN EXTERNAL REPAIR DOUBLER DENTED AT STA 1019 BETWEEN L-36R AND L-37R. DENT FOUND TO BE OUT OF LIMITS IAW DC10 SRM 53-20-00 VOL 2. F
- [SDR 04FDEA02017](https://openairdocs.org/sdr/04FDEA02017), Jul 7, 2004: WEDGE. DENTED. RIGHT HAND OUTBOARD FLAP NR 2 TRAILING EDGE STATION 556 HAS DENT OUT OF LIMITS. FABRICATED SKIN ASSEMBLY IAW DAC DWG ARC 1953 AND INSTALLED SKIN IAW DC10 SRM 51
- [SDR 04FDEA01934](https://openairdocs.org/sdr/04FDEA01934), Jul 3, 2004: SPAR. DAMAGED. RIGHT HAND WING STATION XW255.000, LOWER SPAR BEAM OUTBOARD HOLE "C" ON PAGE 9 OF 18 OF EO 8-5750-7-5001 PART 2, HOLE HAS TOOLING DAMAGE. REAMED HOLE TO FINAL S
- [SDR 04FDEA01919](https://openairdocs.org/sdr/04FDEA01919), Jul 3, 2004: SKIN. CRACKED. NR 3 ENG PYLON CRACK RIGHT SIDE STA YN 320 ABOVE CORE COWL. TRIMMED OUT CRACK IAW DC10 SRM 54-00-01VOL 2, FABBED DOUBLER & FILLER IAW DC10 SRM 54-00-01 VOL 1, I
- [SDR 04FDEA01918](https://openairdocs.org/sdr/04FDEA01918), Jul 3, 2004: VANE. DAMAGED. LEFT HAND INBOARD FLAP VANE, LOWER SKIN DAMAGED AT OUTBOARD STOP. REMOVED AND INSTALLED OVERHAULED VANE AT LEFT HAND INBOARD FLAP IAW FEDEX WORKCARD E-8-5750-7-
- [SDR 04FDEA01920](https://openairdocs.org/sdr/04FDEA01920), Jul 3, 2004: FLOORBEAM. CRACKED. FWD CARGO PIT FLOORBEAM AT BS 652 IS CRACKED. CUT OUT DAMAGE, FABRICATED REPAIR PARTS LOCATED AND DRILLED IAW DC10 SRM 53-00-01 VOL 1. ALODINED AND PRIMED IAW D
- [SDR 04FDEA01921](https://openairdocs.org/sdr/04FDEA01921), Jul 3, 2004: ANGLE. CRACKED. ZONE 316 FORWARD UPPER BULKHEAD ANGLE IS CRACKED AT STATION 2164 BULKHEAD TO FUSELAGE SKIN ATTACH ANGLE AT RBL 8. PERFORMED DYE PEN CHECK, FOUND 1 INCH CRACK, R
- [SDR 04FDEA01922](https://openairdocs.org/sdr/04FDEA01922), Jul 3, 2004: RIB. CRACKED. RIGHT HAND INBOARD FLAP, INBOARD TRACK UPPER FAIRING, FORWARD RIB CRACKED. REMOVED CRACKED RIB IAW DC10 SRM 51-35-01 VOL 2. FABRICATED NEW RIB IAW DAC DWG ARC 2
- [SDR 04FDEA01923](https://openairdocs.org/sdr/04FDEA01923), Jul 3, 2004: SKIN. CRACKED. RIGHT HAND INBOARD FLAP, INBOARD, AFT HOIST POINT, SKIN CRACKED/DAMAGED. REMOVED TRAILING EDGE WEDGE, FABRICATED REPAIR DOUBLER IAW DC10 SRM 51-21-01 VOLUME 2. 
- [SDR 04FDEA01924](https://openairdocs.org/sdr/04FDEA01924), Jul 3, 2004: SKIN. DENTED. RIGHT HAND WING INBOARD AILERON - INBOARD EDGE OF LOWER SKIN SURFACE DENTED. REMOVED DAMAGE AND FABRICATED REPAIR DOUBLER IAW DC10 SRM 57-00-01 VOLUME 1. INSTAL
- [SDR 04FDEA01925](https://openairdocs.org/sdr/04FDEA01925), Jul 3, 2004: SKIN. DENTED. RIGHT HAND WING INBOARD AILERON UPPER SKIN SURFACE HAS NUMEROUSE DENTS. CHECKED LIMITS ON 58 DENTS, 54 DENTS WITHIN LIMITS, 4 DENTS EXCEEDED SRM LIMITS IAW DC10
- [SDR 04FDEA01926](https://openairdocs.org/sdr/04FDEA01926), Jul 3, 2004: TRACK. CHAFED. RIGHT WING LOWER SURFACE, LEADING EDGE DIRECTLY INBOARD OF NR 9 SLAT DRIVE TRACK IS CHAFED. BLENDED AREA, FOUND TO BE OUT OF LIMITS IAW DC10 SRM 57-55-01 FIGURE
- [SDR 04FDEA01927](https://openairdocs.org/sdr/04FDEA01927), Jul 3, 2004: SKIN. GOUGED. RIGHT HAND WING LOWER SURFACE, LEADING EDGE ADJACENT TO NR 8 SLAT IS GOUGED. BLENDED GOUGE IAW DC10 SRM 57-00-01 VOL I, FABRICATED AND INSTALLED DOUBLER IAW DC1
- [SDR 04FDEA01928](https://openairdocs.org/sdr/04FDEA01928), Jul 3, 2004: ANGLE. CRACKED. LEFT HAND OUTBOARD FLAP, OUTBOARD SUPPORT FITTING, FAIRING ATTACH STRUCTURE LOWER, INBOARD L-ANGLE BRACKET IS CRACKED. REMOVED L-ANGLE BRACKET IAW DC10 SRM 51-3
- [SDR 04FDEA01929](https://openairdocs.org/sdr/04FDEA01929), Jul 3, 2004: SKIN. DENTED. RIGHT HAND OUTBOARD ELEVATOR HAS NUMEROUS DENTS ON UPPER SURFACE. CHECKED DENTS HIGHEST READING 97887.111, DENT FOUND TO BE OUT OF LIMITS IAW DC10 SRM 51-80-01.
- [SDR 04FDEA01930](https://openairdocs.org/sdr/04FDEA01930), Jul 3, 2004: FLOORBEAM. CRACKED. FLOORBEAM CRACKED UNDER CENTER ROLLER TRAY AT ATTACH POINT STATION 840 LBL 2. FABRICATED AND INSTALLED REPAIR COMPONENTS IAW DC10 SRM 53-00-01 VOL I, 53-00-01 V
- [SDR 04FDEA01931](https://openairdocs.org/sdr/04FDEA01931), Jul 3, 2004: FLOORBEAM. CRACKED. FORWARD CARGO PIT FLOORBEAM AT FUSELAGE STATION 652 IS CRACKED. FABRICATED AND INSTALLED REPAIR PARTS IAW DC10 SRM 53-12-01 VOL 3, 53-00-01 VOL I AND 51-21-01 V
- [SDR 04FDEA01932](https://openairdocs.org/sdr/04FDEA01932), Jul 3, 2004: SHEAR TIE. CORRODED. CORROSION AND FLAKING PAINT AND PRIMER AT STATION 1821, LONGERON 51L-51R. REMOVED CORROSION IAW DC10 SRM 51-21-01 VOL 2, FOUND TO BE OUT OF LIMITS IAW DC10 SRM 
- [SDR 04FDEA01933](https://openairdocs.org/sdr/04FDEA01933), Jul 3, 2004: FLOORBEAM. CRACKED. FORWARD CARGO PIT FLOORBEAM AT FUSELAGE STATION 775 IS CRACKED. REMOVED CENTER ROLLER TRAY FOR ACCESS. FABRICATED REPAIR FILLER ANGLE, REPAIR ANGLE AND CUT OUT 
- [SDR 04FDEA01935](https://openairdocs.org/sdr/04FDEA01935), Jul 3, 2004: SPAR. DAMAGED. RT WING STATION XW255.000, LOWER SPAR BEAM OUTBOARD HOLE "C" ON PAGE 9 OF 18 OF EO 8-5750-7-5001 PART 2, HOLE HAS TOOLING DAMAGE. REAMED HOLE TO FINAL SIZE OF 1
- [SDR 04FDEA01917](https://openairdocs.org/sdr/04FDEA01917), Jul 3, 2004: VANE. DELAMINATED. RIGHT HAND INBOARD FLAP VANE, UPPER SKIN HAS MULTIPLE AREA OF DENTS AND DELAMINATION. REMOVED AND REPLACED WITH OVERHAULED VANE RIGHT HAND INBOARD FLAP VANE IAW
- [SDR 04FDEA01896](https://openairdocs.org/sdr/04FDEA01896), Jun 30, 2004: WEDGE. DENTED. RIGHT HAND OUTBOARD FLAP HAS DENT OUT OF LIMITS AT STATION 478 INBOARD END. REMOVE WEDGE IAW DC10 SRM 51-40-2 VOL 2. REMOVE WEDGE SKIN IAW DC10 SRM 51-40-2 VOL 
- [SDR 04FDEA01895](https://openairdocs.org/sdr/04FDEA01895), Jun 30, 2004: WEDGE. DENTED. RT OUTBOARD FLAP NR 2 TRAILING EDGE WEDGE STATION 556 HAS DENT OUT OF LIMITS. FABRICATED SKIN ASSEMBLY IAW DAC DWG ARC 1953 AND INSTALLED SKIN ASSEMBLY IAW DC10
- [SDR 04FDEA01894](https://openairdocs.org/sdr/04FDEA01894), Jun 30, 2004: BRACKET. BROKEN. RIGHT HAND OUTBOARD FLAP INBOARD HINGE HAS A BROKEN BRACKET PART NUMBER ARC 2149-25. DISASSEMBLED HINGE PANEL STRUCTURE IAW DC10 SRM 51-35-01 VOL 2. REMOVED BRO
- [SDR 04FDEA01893](https://openairdocs.org/sdr/04FDEA01893), Jun 30, 2004: RUB STRIP. CORRODED. LEFT WING FUEL PANEL 536DD LANDING RUB STRIP HAS CORROSION AND PITTING LOWER WING. REMOVED CORRODED RUB STRIP IAW DC10 SRM 51-35-01 VOL 2. FOUND LANDING CORRODE
- [SDR 04FDEA01892](https://openairdocs.org/sdr/04FDEA01892), Jun 30, 2004: WIRE HARNESS. ARCED. RT WING INSIDE NR 3 FUEL TANK THRU ACCESS PANEL NR 634 AT FUEL PROBE WIRE HARNESS HAS CUT WIRE WITH EVIDENCE OF ARCING, LOCATED JUST BELOW ACCESS PANEL. REMOVED
- [SDR 04FDEA01891](https://openairdocs.org/sdr/04FDEA01891), Jun 30, 2004: SKIN. DENTED. RIGHT HAND LOWER FUSELAGE SKIN EXTERNAL REPAIR DOUBLER IS DENTED AT FS 1019 BETWEEN L-36R AND L-37R. DENT FOUND TO BE OUT OF LIMITS IAW DC10 SRM 53-20-00 VOL I 
- [SDR 04FDEA01890](https://openairdocs.org/sdr/04FDEA01890), Jun 30, 2004: FRAME. CORRODED. AREA AFT OF AFT CARGO COMPARTMENT BILGE HAS AREA OF CORROSION, FS 1971, RBL 8 TO LBL 4. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW DC10 SRM 51-21-01 VO
- [SDR 04FDEA01889](https://openairdocs.org/sdr/04FDEA01889), Jun 30, 2004: FRAME. CORRODED. AREA AFT OF AFT CARGO COMPARTMENT BILGE HAS AREA OF CORROSION, FS 1971, RBL 8 TO LBL 4. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW DC10 SRM 51-21-01 VO
- [SDR 03FDEA01049](https://openairdocs.org/sdr/03FDEA01049), Jul 5, 2003: BULB. BURNED OUT. UPON LOWERING LANDING GEAR, RECEIVED NO GREEN INDICATION ON EITHER F/O'S PANEL OR S/O PANEL. COMPLETED GO AROUND. TESTED LIGHTS, NO TEST ON GREEN LIGHTS. REPLAC

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