# N322FE: 1975 Mcdonnell Douglas DC-10-30F, registration cancelled 2006-05-04 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: May 4, 2006 - Exported to: Brazil - Status when cancelled: Valid registration - Airframe: [Mcdonnell Douglas DC-10-30F](https://openairdocs.org/model/mcdonnell-douglas-dc-10-30f) (registry code 3023504) - 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: 47908 - Year built: 1975 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: October 30, 1992 - Certificate issued: July 19, 2004 - Last registry action: July 19, 2004 - Mode S code: A37640 - Owner when cancelled: [Sky Lease I Inc](https://openairdocs.org/faa-owner/SKY%20LEASE%20I%20INC) - Location: [Miami, FL](https://openairdocs.org/faa-place/FL/Miami) - Owner type: Corporation - Owner's area on the map: 25.8361° N, 80.4200° W: Placed by OpenAirDocs at the center of ZIP code 33178, within about 4 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N322FE - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=322FE - Page: https://openairdocs.org/deregistered/N322FE-2006-05-04 From the FAA registry file of November 12, 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 (19) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR 2004F00236](https://openairdocs.org/sdr/2004F00236), Aug 14, 2004: FUSE LINK. SHEARED. RT OB SLAT RETAINER MECHANISM MECHANICAL FUSE SHEARED. (REFERENCE MM 27-83-08 PAGE 202 FIGURE 201) REFERENCE NON-ROUTINE 39546. - [SDR 2004F00237](https://openairdocs.org/sdr/2004F00237), Aug 14, 2004: SLEEVE. CRACKED. NR 3 ENGINE IB THRUST REVERSER EXTRUDED TORQUE RING, AT THE LEADING EDGE OF TRANSLATING SLEEVE, CRACKED AROUND FASTENER HOLE AT 10 O'CLOCK (REVERSER DEPLOYED). - [SDR 2004FA0000678](https://openairdocs.org/sdr/2004FA0000678), Aug 6, 2004: FUSE PIN. SHEARED. RT WING OB SLAT CONTROL MECHANISM HAS ANTI-DROOP FUSE PIN SHEARED. REFERENCE NON-ROUTINE 39501. - [SDR 2004FA0000679](https://openairdocs.org/sdr/2004FA0000679), Aug 6, 2004: ATTACH FITTING. CORRODED. LOWER AFT WING TO CENTER BOX ATTACH SKATE FITTING IS EXFOLIATED, LT WHEEL WELL, FUSELAGE STATION 1366 TO 1381. REFERENCE NON-ROUTINE NR 39431. - [SDR 01FDEA00218](https://openairdocs.org/sdr/01FDEA00218), Mar 20, 2001: PIN. DEFECTIVE. NOSE GEAR DID NOT RETRACT ON T/O. REMOVED AND REPLACED NOSE GEAR PIN. AC OK TO CONTINUE. - [SDR 00FDEA00400](https://openairdocs.org/sdr/00FDEA00400), Jun 20, 2000: STIFFENER. CORRODED. SNRM 0327 LOWER AUX FUEL TANK AFT BULKHEAD, LT MOST VERTICAL STIFFNER FOUND WITH CORROSION. R&R PER 51-31-01, 21-11-06-2. - [SDR 00FDEA00399](https://openairdocs.org/sdr/00FDEA00399), Jun 20, 2000: SUPPORT BRACKET. CRACKED. SNRM 0338 RT WING PANEL SUPPORT FOR PANEL NR 618GB WAS CRACKED, LOCATED APPROX 4 INCHES OB OF SLAT DRIVE MECH ACCESS PANEL. R&R PER SRM 51-31-01. - [SDR 00FDEA00403](https://openairdocs.org/sdr/00FDEA00403), Jun 19, 2000: SKIN. CRACKED. SNRM 0196 LT WING OB FLAP UPPER SKIN SURFACE FOUND CRACKED APPROX 3 5/32 INCHES. R&R PER SRM 51-31-01, 57-10-00, 57-52-02. - [SDR 00FDEA00402](https://openairdocs.org/sdr/00FDEA00402), Jun 19, 2000: SKIN. CRACKED. SNRM 0198 LT WING IB FLAP UPPER SKIN FOUND PATCH REPAIR CRACKED APPOX 6 INCHES. R&R PER CMM 57-52-01. - [SDR 00FDEA00401](https://openairdocs.org/sdr/00FDEA00401), Jun 19, 2000: SKIN. CRACKED. SNRM 0222 LT WING L/E LOWER ACCESS PANEL CUTOUT NR 526AB FWD SIDE FOUND CRACKED. R&R PER SRM 51-31-01. - [SDR 00FDEA00398](https://openairdocs.org/sdr/00FDEA00398), Jun 19, 2000: CHANNEL. CORRODED. SNRM 0252 AFT FUSELAGE WATER TANK BAY STA 1996, FUSELAGE FRAME AFT LWR CHANNEL TOP SURFACE CORRODED, LONGERON 50 RT TO LT. R&R CHANNEL & STRAP PER SRM 53-30-00 - [SDR 98FDEA00413](https://openairdocs.org/sdr/98FDEA00413), Jun 20, 1998: FIRE BOTTLE. DISCHARGED. ENGINE NR 2, NR 1 BOTTLE LOW PRESSURE LIGHT ILLUMINATING JUST PRIOR TO DEPARTURE. FOUND NR 1 BOTTLE OF APU FIRE EXTINGUISHER SYSTEM HAD DISCHARGED THRU APU PORT - [SDR 98FDEA00250](https://openairdocs.org/sdr/98FDEA00250), Apr 5, 1998: SLIDER. BROKEN. SHORT FINAL, LEFT AFT CARGO DOOR LIGHT ON F/E PANEL ILLUM FOLLOWED BY IMMEDIATE PRESSURE DROP IN CABIN. ACFT WAS ALREADY CONFIGURED FOR LANDING, LANDED SUCCESSF - [SDR 96FDEA01489](https://openairdocs.org/sdr/96FDEA01489), Sep 16, 1996: HI-LOCK COLLARS. MISSING. SNRM NR 0352, VERTICAL STABILIZER ALL COLLARS MISSING FROM HI-LOCKS BETWEEN AFT H-11 BOLTS THAT ATTACH UPPER VERICAL STABILIZER TO LOWER VERTICAL STABILER. REF - [SDR 96FDEA01490](https://openairdocs.org/sdr/96FDEA01490), Sep 14, 1996: TENSION STRAP. CRACKED. SMRM NR 00506, RT WING, O/B FLAP I/B HINGE O/B SIDE TENSION STRAP IS CRACKED AT THE LOWER BOLT HOLE LOWER FLANGE. *S/D* REMOVED AND REPLACED TENSION STRAP BRACK - [SDR 96FDEA01435](https://openairdocs.org/sdr/96FDEA01435), Sep 4, 1996: V-PANEL. MISSING. UPON WALK AROUND, FOUND THE V-PANEL ON NR 3 ENGINE PYLON RIPPED AWAY. INSTALLED V-PANEL ON PYLON FARING. ALSO, REPAIRED DAMAGED PYLON FARING HONEYCOMB PANEL OUT - [SDR 95FDEA01428](https://openairdocs.org/sdr/95FDEA01428), Sep 26, 1995: DUCT. FAILED. DURING T/O ROLL, NR 1 ENG N1 IND DROPPED APPROX 10 PERCENT. ADJUSTED THROTTLE TO MATCH N2 AND FUEL FLOW, NO CHANGE NOTED IN N1, EGT IND 910 DEGREES, APPROX 50 D - [SDR 95FDEA00214](https://openairdocs.org/sdr/95FDEA00214), Mar 10, 1995: FIRE WARNING. MALFUNCTIONED. THE APU FIRE LIGHT ILLUMINATED INTERMITTENTLY DURING FLIGHT. IT ALSO ILLUMINATED DURING TAKEOFF OUT OF MEM. FOUND APU FIRE LIGHT ASSY RETAINER PIN MISALIGNED, R - [SDR 95FDEA00005](https://openairdocs.org/sdr/95FDEA00005), Jan 7, 1995: DUCT. FAILED. ENG FIRE IN NR 2 ENG SHORTLY AFTER ROTATION. OBSERVED EGT REACHED 899 DEG. MEMORY ITEMS ACCOMP, CKLT PROCED COMPLIED WITH, RETURNED TO OAK FOR UNEVENTFUL LANDIN --- 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, except the copies of manufacturers’ service documents, which belong to their rights holders.