# N13067: 1974 Mcdonnell-Douglas DC-10-30, registration cancelled 2005-04-27

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: April 27, 2005
- Status when cancelled: Valid registration
- 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: 47866
- Year built: 1974
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 27, 1985
- Certificate issued: December 28, 2000
- Last registry action: April 27, 2005
- Mode S code: A07E7B
- Owner when cancelled: [Wells Fargo Bank Northwest Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20BANK%20NORTHWEST%20NA%20TRUSTEE)
- Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City)
- Owner type: Corporation
- Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N13067
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=13067
- Page: https://openairdocs.org/deregistered/N13067-2005-04-27

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 (62, newest 50)

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

- [SDR CALA0000846](https://openairdocs.org/sdr/CALA0000846), Jun 8, 2000: WEB. CRACKED. INSPECTION FOUND A 3 INCH CRACK ON VERTICAL WEB IN AFT CARGO COMPARTMENT AT STA 1841 ABOVE LONGERON 43-44, LBL 65. THE CRACKED AREA WAS TRIMMED OUT AND REINFORC
- [SDR CALA0000845](https://openairdocs.org/sdr/CALA0000845), Jun 8, 2000: CHANNEL. CRACKED. THE FORWARD CARGO COMPARTMENT LEFT LOWER SIDEWALL Z-CHANNEL FORWARD OF LOAD BAR HAD A 12 INCH CRACK AND PUNCTURE ON LT LOWER SIDEWALL TRIM PLATE. AN INTERIM REP
- [SDR CALA0000844](https://openairdocs.org/sdr/CALA0000844), Jun 7, 2000: INTERCOSTAL. CORRODED. INSPECTION FOUND INTERCOSTAL CORRODED IN CENTER CARGO COMPARTMENT AT STA 1740, LONGERON 45R. THE CORRODED AREA WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 53
- [SDR CALA0000843](https://openairdocs.org/sdr/CALA0000843), Jun 7, 2000: FITTING. CORRODED. INSPECTION FOUND FORWARD CARGO DOOR JAMB FORWARD FITTING CORRODED. THE FITTING WAS REMOVED AND A NEW FITTING WAS INSTALLED IAW SRM 53-50-00, FIGURE 1, 51-21-01,
- [SDR CALA0000837](https://openairdocs.org/sdr/CALA0000837), Jun 7, 2000: STRINGER. CRACKED. INSPECTION FOUND STRINGERS NR 4, 5, AND 7 CRACKED IN RT MAIN GEAR WHEEL WELL AT O/B LOWER WALL AFT OF OUTER DOOR CUTOUT. THE CRACKS WERE 1, 4, AND 5 INCHES LONG
- [SDR CALA0000836](https://openairdocs.org/sdr/CALA0000836), Jun 7, 2000: ANGLE. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN ANGLE ON OUTER DOOR CUTOUT AFT SIDE FORWARD EDGE, LT MLG WHEEL WELL. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW 
- [SDR CALA0000835](https://openairdocs.org/sdr/CALA0000835), Jun 7, 2000: SKIN. CORRODED. INSPECTION FOUND EXTERNAL FUSELAGE SKIN CORRODED AT STA 900 BETWEEN LONGERON 37L AND 38L. THE CORRODED AREA OF SKIN WAS TRIMMED OUT. THE AREA WAS REINFORCED WIT
- [SDR CALA0000834](https://openairdocs.org/sdr/CALA0000834), Jun 7, 2000: SKIN. CRACKED. INSPECTION FOUND A 6 INCH CRACK IN LT WING LOWER SURFACE ON I/B CORNER OF FUELING BAY DOOR CUTOUT. THE AREA WAS REINFORCED WITH A DOUBLER USING RIVETS IAW SRM 5
- [SDR CALA0000814](https://openairdocs.org/sdr/CALA0000814), Jun 2, 2000: LIGHT. INOPERATIVE. INSPECTION FOUND CABIN EMERGENCY LIGHT ASSEMBLY AT SEAT 9B INOPERATIVE. THE LIGHT ASSEMBLY WAS REPLACED AND OPERATION CHECKED GOOD IAW MM 33-50-00.
- [SDR CALA9901719](https://openairdocs.org/sdr/CALA9901719), Dec 23, 1999: OVEN. INOPERATIVE. SMOKE BEGAN COMING OUT OF THE AFT GALLEY OVEN CONTROL PANEL WHILE EN ROUTE TO EWR. THE SMOKE STOPPED WHEN OVEN WAS TURNED OFF. THE FLIGHT CONTINUED WITHOUT FURT
- [SDR CALA9901498](https://openairdocs.org/sdr/CALA9901498), Nov 14, 1999: WIRE. BROKEN. INSPECTION FOUND FORWARD EMERGENCY LIGHT AT SEAT 2KL INOPERATIVE. INSPECTION REPAIRED BROKEN WIRE AT SEAT 2KL AND OPERATION CHECKED GOOD.
- [SDR CALA9900779](https://openairdocs.org/sdr/CALA9900779), Jul 5, 1999: ANGLE. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN FUSELAGE SKIN ATTACH ANGLE AT STA 1120, STRINGER 33-34R. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-31-01
- [SDR CALA9900778](https://openairdocs.org/sdr/CALA9900778), Jul 5, 1999: SUPPORT. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN FLOOR SUPPORT IN FORWARD CARGO AREA AT STA 899, RBL 45-65. THE FLOOR SUPPORT WAS REMOVED AND A NEW ONE WAS INSTALLED IAW SRM 
- [SDR CALA9900777](https://openairdocs.org/sdr/CALA9900777), Jul 5, 1999: SUPPORT. CRACKED. INSPECTION FOUND A 2 INCH CRACK IN FLOOR SUPPORT IN FORWARD CARGO AREA AT STA 755 BETWEEN RBL 65 AND 85. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INS
- [SDR CALA9900776](https://openairdocs.org/sdr/CALA9900776), Jul 5, 1999: LINER. TORN. INSPECTION FOUND A 2 INCH TEAR ON VERTICAL WALL IN CENTER CARGO COMPARTMENT AT STA 1841, RBL 10. THE TORN AREA WAS TRIMMED OUT AND REINFORCED WITH DOUBLER IAW S
- [SDR CALA9900775](https://openairdocs.org/sdr/CALA9900775), Jul 5, 1999: FRAME. CRACKED. INSPECTION FOUND A 2 INCH CRACK IN FRAME OF CENTER CARGO COMPARTMENT VERTICAL WALL AT STA 1841, RBL 20. THE CRACKED AREA WAS TRIMMED OUT AND REINFORCED WITH DOU
- [SDR CALA9900774](https://openairdocs.org/sdr/CALA9900774), Jul 5, 1999: SUPPORT. CORRODED. INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED BETWEEN STA 1920 AND 2007, LBL 55. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-31-01.
- [SDR CALA9900773](https://openairdocs.org/sdr/CALA9900773), Jul 5, 1999: SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT CORRODED UNDER LAV/GALLEY FLOOR AREA AT STA 420 BETWEEN BL 0 TO LBL 27. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTA
- [SDR CALA9900772](https://openairdocs.org/sdr/CALA9900772), Jul 5, 1999: SKIN. CRACKED. INSPECTION FOUND A 1 INCH CRACK WITH SHEARED RIVETS IN RT WING NR 2 LEADING EDGE SLAT INBOARD SKIN. THE CRACKED AREA WAS TRIMMED OUT AND REINFORCED WITH DOUBLER
- [SDR CALA9900771](https://openairdocs.org/sdr/CALA9900771), Jul 5, 1999: ANGLE. CRACKED. INSPECTION FOUND TWO VERTICAL STIFFENER ANGLES ON LT WHEEL WELL AFT SIDE WEB CRACKED. THE CRACKS WERE .5 INCH LONG. THE TWO ANGLES WERE REMOVED AND NEW ANGLES W
- [SDR CALA9900770](https://openairdocs.org/sdr/CALA9900770), Jul 4, 1999: ANGLE. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN STIFFENER VERTICAL ANGLE AT RT MLG WHEEL WELL REAR BULKHEAD LOWER O/B CORNER JOINT TO LONGERON TO BULKHEAD. THE ANGLE WAS REM
- [SDR CALA9900759](https://openairdocs.org/sdr/CALA9900759), Jun 30, 1999: STRINGER. CORRODED. INSPECTION FOUND FRAME CORRODED IN LOWER LOBE AFT CARGO BILGE AREA AT STA 1851 BETWEEN STRINGER 51L AND 51R WITH CORROSION ON STRINGERS 52L AND 51L. THE CORRODE
- [SDR CALA9900736](https://openairdocs.org/sdr/CALA9900736), Jun 28, 1999: STRINGER. CORRODED. INSPECTION FOUND STRINGER 50 CORRODED BETWEEN STA 1851 AND 1868. THE CORRODED SECTION WAS REMOVED, A NEW SECTION OF STRINGER WAS INSTALLED WITH REINFORCEMENT IA
- [SDR CALA9900735](https://openairdocs.org/sdr/CALA9900735), Jun 28, 1999: FRAME. CORRODED. INSPECTION FOUND CORROSION ON BOTH LOWER SIDES OF FRAME AT STA 1741 AND 1761 BETWEEN STRINGER 47L AND 50R. THE CORRODED AREAS WERE REMOVED, NEW ANGLES WERE INST
- [SDR CALA9900734](https://openairdocs.org/sdr/CALA9900734), Jun 28, 1999: WALL. TORN. INSPECTION FOUND TEARS ON VERTICAL WALL IN CENTER CARGO COMPARTMENT AT STA 1841 BETWEEN LBL 40 & 60. THE TORN AREAS WERE TRIMMED OUT AND DEBURRED. REINFORCED AR
- [SDR CALA9900733](https://openairdocs.org/sdr/CALA9900733), Jun 28, 1999: ANGLE. CRACKED. INSPECTION FOUND A 2 INCH CRACK ON VERTICAL ANGLE IN CENTER CARGO COMPARTMENT AT STA 1841, LBL 10. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 5
- [SDR CALA9900715](https://openairdocs.org/sdr/CALA9900715), Jun 22, 1999: SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT UNDER LAV/GALLEY AREA CORRODED AT STA 755-899, LBL 44. THE CORRODED FLOOR SUPPORT SECTION WAS REMOVED AND A NEW SECTION WAS INSTA
- [SDR CALA9801941](https://openairdocs.org/sdr/CALA9801941), Oct 11, 1998: APU. LEAKING. OIL SMELL IN COCKPIT. APU INTERNAL OIL LEAK CONFIRMED. CLEANED AIRCRAFT PACKS. PLACARD APU PER MEL.
- [SDR CALA9800900](https://openairdocs.org/sdr/CALA9800900), May 24, 1998: COMPUTER. INOPERATIVE. THE CAPTAIN'S STICK SHAKER ACTIVATED, THE SLAT DISAGREE LIGHT ILLUMINATED, AND SLAT RESET ILLUMINATED DURING TAKEOFF FROM IAH. CONFIRMED SLAT RETRACTION PER CHE
- [SDR CALA9800810](https://openairdocs.org/sdr/CALA9800810), May 7, 1998: WIRE. BROKEN. NUMBER 3 ENGINE NUMBER 1 AGENT FIRE BOTTLE LOW PRESSURE SWITCH FAILED. WIRE FOUND BROKEN AT EARTH POINT 6015D. WIRE RETERMINATED WITH A NEW TAG PER MM20-00-00.
- [SDR CALA9800789](https://openairdocs.org/sdr/CALA9800789), May 6, 1998: WIRE. BROKEN. CARGO FIRE BOTTLE NR 2 LOW PRESSURE SWITCH ELECTRICAL CONNECTOR WIRE FOUND BROKEN. WIRE W277B24 FOUND BROKEN AT PIN B OF CONECTOR P1-2189. NEW PIN FITTED AND TE
- [SDR CALA9800788](https://openairdocs.org/sdr/CALA9800788), May 6, 1998: FIRE BOTTLE. DAMAGED. NUMBER 2 ENGINE AND APU FIRE BOTTLE LOW PRESSURE CONNECTOR P1-1264 SOCKET B FOUND PUSHED BACK. ELECTRICAL CONNECTOR REPLACED PER MM 20-00-00.
- [SDR CALA9800787](https://openairdocs.org/sdr/CALA9800787), May 6, 1998: CARTRIDGE. OPEN CIRCUIT. NUMBER 1 ENGINE FIRE BOTTLE AGENT ONE FILAMENT A NOT LIGHTING ON TEST BOX DURING TEST. CARTRIDGE FOUND U/S. INSTALLED NEW CARTRIDGE.
- [SDR CALA9700636](https://openairdocs.org/sdr/CALA9700636), May 3, 1997: COMPRESSOR. DAMAGED. THE NR 3 ENGINE EXPERIENCED COMPRESSOR STALLS WHILE ENROUTE. THE AIRCRAFT WAS RETURNED TO LGW. THE NR 3 ENGINE WAS REMOVED AND REPLACED. THE ENGINE WAS RUN AND 
- [SDR CALA9700666](https://openairdocs.org/sdr/CALA9700666), Apr 25, 1997: LONGERON. CORRODED. DIP NR 017105 WAS COMPLIED WITH BY INSTALLING A PERMANENT REPAIR AT LONGERON 46L, STA 1811. THE OLD REPAIR WAS REMOVED. A PERMANENT REPAIR WAS FABRICATED AND IN
- [SDR CALA9700665](https://openairdocs.org/sdr/CALA9700665), Apr 25, 1997: SKIN. CRACKED. INSPECTION FOUND A 1 CRACK IN SKIN WITH CORROSION AT FASTENER ON RIGHT HAND SIDE OF NR 2 ENGINE COWL, STA 2120 UPPER SURFACE AT BASE OF VERTICAL STABILIZER. THE
- [SDR CALA9700664](https://openairdocs.org/sdr/CALA9700664), Apr 25, 1997: SKIN. CORRODED. INSPECTION FOUND FUSELAGE SKIN CORRODED BELOW CENTER PIT DOOR AT STA 1681-1701, L48L TO L48R. THE CORRODED AREA OF SKIN WAS CUT OUT IAW SRM 53-20-00. SKIN FILLE
- [SDR CALA9700662](https://openairdocs.org/sdr/CALA9700662), Apr 25, 1997: LONGERON. CORRODED. INSPECTION FOUND LONGERON 50L CORRODED AT BS 1708. THE CORRODED SECTION WAS CUTOUT. A LONGERON AND SPLICE WERE FABRICATED AND INSTALLED IAW SRM 53-10-00, FIGURE
- [SDR CALA9700661](https://openairdocs.org/sdr/CALA9700661), Apr 25, 1997: LONGERON. CORRODED. INSPECTION FOUND LONGERON 51R CORRODED AT STA 1708. THE CORRODED AREA WAS CUTOUT. A LONGERON AND SPLICE WERE FABRICATED AND INSTALLED IAW SRM 53-10-00, FIGURE 1
- [SDR CALA9700660](https://openairdocs.org/sdr/CALA9700660), Apr 25, 1997: PANEL. CRACKED. INSPECTION FOUND NR 3 ENGINE ACCESS PANEL 487 FRAME CRACKED AT ATTACHMENT HOLE, A BROKEN NUTPLATE, AND CORROSION AT MATING SURFACE. THE CRACK WAS 1 INCH LONG. T
- [SDR CALA9700659](https://openairdocs.org/sdr/CALA9700659), Apr 25, 1997: ANGLE. CRACKED. INSPECTION FOUND A 5.5 INCH CRACK IN LT WING INBOARD ATTACH ANGLE AT WS XCW 118. THE ANGLE WAS REMOVED IAW SRM 51-33-01. A NEW ANGLE WAS FABRICATED AND INSTALLE
- [SDR CALA9700658](https://openairdocs.org/sdr/CALA9700658), Apr 25, 1997: SKIN. BUCKLED. INSPECTION FOUND FUSELAGE SKIN BUCKLED AT STA 335 JUST UNDER PILOT'S SLIDING WINDOW. THE AREA WAS REFORMED TO WITHIN LIMITS IAW SRM 53-20-00. A FINGER DOUBLER W
- [SDR CALA9700657](https://openairdocs.org/sdr/CALA9700657), Apr 25, 1997: SHEAR TIE. CORRODED. INSPECTION FOUND FRAME SHEAR TIE CORRODED AT STA 1721, BETWEEN LONGERON 49L AND 47L. THE CORRODED SECTION OF SHEAR TIE WAS REMOVED AND A NEW SHEAR TIE SECTION W
- [SDR CALA9700656](https://openairdocs.org/sdr/CALA9700656), Apr 25, 1997: SHEAR TIE. CORRODED. INSPECTION FOUND FRAME SHEAR TIE CORRODED AT STA 1821, BETWEEN LONGERON 48L AND 49L. THE CORRODED SECTION OF SHEAR TIE WAS REMOVED AND A NEW SHEAR TIE WAS INSTA
- [SDR CALA9700655](https://openairdocs.org/sdr/CALA9700655), Apr 25, 1997: SKIN. DENTED. INSPECTION FOUND FIVE DENTS IN UPPER SKIN OF RT DETACHABLE ELEVATOR. THE DENTED SKIN WAS REMOVED IAW SRM 55-00-01, FIG. 1, VOL I AND 55-00-01, FIG. 2, VOL I. RE
- [SDR CALA9700654](https://openairdocs.org/sdr/CALA9700654), Apr 25, 1997: ANGLE. CRACKED. INSPECTION FOUND A 2 CRACK IN FORMED ANGLE AT FUSELAGE SKIN, STA 1421, LONGERON 31L TO 32L, AT LT WING INBOARD TOP FILLET AREA. THE ANGLE WAS REMOVED. A REPAIR 
- [SDR CALA9601725](https://openairdocs.org/sdr/CALA9601725), Dec 3, 1996: CONTROL CABLE. BROKEN. THE AIRCRAFT ARRIVED IN EWR WITH THE RT MLG DOOR HANGING DOWN. MAINTENANCE FOUND THE RT MLG DOOR FOLLOW-UP CABLE BROKEN. THE CABLE WAS REMOVED AND REPLACED AND 
- [SDR CAL960217](https://openairdocs.org/sdr/CAL960217), Jan 28, 1996: LONGERON. CORRODED. KUL - INSPECTION FOUND CORROSION ON LONGERON 31L AT STATION 1405. THE CORROSION WAS REMOVED AND A DOUBLE ANGLE REPAIR WAS INSTALLED IAW ECRA 5310-03217 AND SRM 
- [SDR CAL960216](https://openairdocs.org/sdr/CAL960216), Jan 28, 1996: LONGERON. CORRODED. KUL - INSPECTION FOUND LONGERON 30L CORRODED AT STATION 1436. THE LONGERON WAS REPAIRED IAW ECRA 5310-03218 AND SRM 53-14-01. (M)
- [SDR CAL960219](https://openairdocs.org/sdr/CAL960219), Jan 26, 1996: STIFFENER. CORRODED. KUL - INSPECTION FOUND LATERAL STIFFENER CORRODED AT FS 1841 RBL 42 AND LBL 28. THE LATERAL STIFFENERS WERE REPLACED IAW SRM 53-16-01. (M)

All 62: https://openairdocs.org/deregistered/N13067-2005-04-27/reports.md

## 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 19970625023839I](https://openairdocs.org/incident/19970625023839I), Jun 25, 1997: Doug DC1030 (N13067), Houston, TX, Minor damage. Landing turned off high speed taxiway. ATC advised make next turn. Ran off taxiway. Gear inspected for side load.

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