# N37077: Mcdonnell-Douglas DC-10-30, registration cancelled 2005-11-04 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: November 4, 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: 46981 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: January 23, 1997 - Certificate issued: September 17, 1996 - Last registry action: November 6, 2002 - Mode S code: A43738 - 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/N37077 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=37077 - Page: https://openairdocs.org/deregistered/N37077-2005-11-04 From the FAA registry file of November 3, 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 (42) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR CALA0100048](https://openairdocs.org/sdr/CALA0100048), Jan 19, 2001: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED IN PASSENGER CABIN AT STA 495, LT SIDE. A NEW FLOORBEAM WAS INSTALLED IAW SRM 51-31-01. - [SDR CALA0100047](https://openairdocs.org/sdr/CALA0100047), Jan 19, 2001: FLOOR SUPPORT. CORRODED. INSPECTION FOUND TRANSVERSAL SUPPORT UNDER FLOOR PANEL 244AF IN MID PASSENGER CABIN CORRODED AT STA 816. REPLACED SUPPORT IAW SRM 51-31-01. - [SDR CALA0100036](https://openairdocs.org/sdr/CALA0100036), Jan 16, 2001: FRAME. CRACKED. INSPECTION FOUND A 0.8 INCH CRACK IN FRAME AT STA 1841 IN CENTER CARGO AREA. REPAIRED IAW SRM 53-00-01, FIGURE 4, SHEET 2. - [SDR CALA0100035](https://openairdocs.org/sdr/CALA0100035), Jan 16, 2001: FLOOR SUPPORT. CORRODED. INSPECTION FOUND LEFT O/B GALLEY FLOOR SUPPORT CORRODED IN MID PASSENGER CABIN, STA 824 - 840. THE SUPPORT WAS REPLACED IAW SRM 51-31-01. - [SDR CALA0100034](https://openairdocs.org/sdr/CALA0100034), Jan 16, 2001: FLOOR SUPPORT. CORRODED. INSPECTION FOUND AFT PASSENGER CABIN RT SUPPORT IN CENTER LAV CORRODED. THE SUPPORT WAS REPLACED IAW SRM 51-31-01. - [SDR CALA0100033](https://openairdocs.org/sdr/CALA0100033), Jan 16, 2001: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AT LT MID PASSENGER CABIN, STA 857 - 899. A NEW FLOORBEAM WAS INSTALLED IAW SRM 51-31-01. - [SDR CALA0100028](https://openairdocs.org/sdr/CALA0100028), Jan 15, 2001: FRAME. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN CENTER CARGO FRAME AT STA 1841. REPAIRED IAW SRM 53-00-01, FIGURE 4, SHEET 2. - [SDR CALA0100027](https://openairdocs.org/sdr/CALA0100027), Jan 15, 2001: BRACKET. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN RT WING I/B BRACKET AT I/B SIDE PANEL. A NEW BRACKET WAS INSTALLED IAW ECRA 5730-01741. - [SDR CALA9900100](https://openairdocs.org/sdr/CALA9900100), Feb 1, 1999: ELEVATOR. DAMAGED. INSPECTION FOUND IMPACT DAMAGE TO RT ELEVATOR TIP CAUSED BY HANGAR DOOR. A NEW ELEVATOR WAS INSTALLED IAW MM 27-30-09, PAGE 401. ELEVATOR OPERATION CHECKED GOOD - [SDR CALA9900099](https://openairdocs.org/sdr/CALA9900099), Jan 31, 1999: SKIN. CRACKED. INSPECTION FOUND A 2 INCH CRACK IN RT WING LEADING EDGE DROOP PANEL UPPER SKIN. TWO RIBS WERE REMOVED AND REPLACED. THE SKIN WAS REINFORCED WITH DOUBLER AND INS - [SDR CALA9900098](https://openairdocs.org/sdr/CALA9900098), Jan 30, 1999: RIB. CRACKED. INSPECTION FOUND A .25 INCH CRACK IN NR 1 SLAT RIB. THE RIB WAS REMOVED AND REPLACED IAW SRM 51-31-01. - [SDR CALA9900090](https://openairdocs.org/sdr/CALA9900090), Jan 27, 1999: SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT CORRODED IN MAIN DECK AT STA 1871 NEAR LAV E. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 53-70-00, 51- - [SDR CALA9800101](https://openairdocs.org/sdr/CALA9800101), Jan 24, 1998: HYD PUMP. LEAKING. THE HYDRAULIC SYSTEM 3 ELEVATOR OFF LIGHT CAME ON JUST PRIOR TO LANDING AT LGW. THE ELEVATOR FEEL CHANNEL LIGHT CAME ON AFTER LANDING. THE AIRCRAFT HAD LOST FLU - [SDR CALA9700336](https://openairdocs.org/sdr/CALA9700336), Mar 12, 1997: RELAY. INOPERATIVE. THE GROUND REFUEL POWER, FUEL TANK FILL VALVE, AND BATTERY BUS SENSING CIRCUIT BREAKERS POPPED WHILE EN ROUTE FROM FCO TO EWR. THE BATTERY BUS OFF LIGHT ILLUMIN - [SDR CALA9700105](https://openairdocs.org/sdr/CALA9700105), Jan 15, 1997: SKIN. CRACKED. INSPECTION FOUND RT DOOR ACCESS CUTOUT SKIN CRACKED AT STA 1308.5 AND STA 1255. BOTH CRACKS WERE 1 INCH LONG. DOUBLERS WERE INSTALLED IAW SRM 53-00-01, FIGURE 4 - [SDR CALA9700104](https://openairdocs.org/sdr/CALA9700104), Jan 9, 1997: SUPPORT. CORRODED. INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT BS 1986 LBL 27. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-21-01, 51-31-01 AND 53-60-01 FIGURE 1. - [SDR CALA9700161](https://openairdocs.org/sdr/CALA9700161), Jan 3, 1997: SUPPORT. CORRODED. INSPECTION FOUND T-ANGLE FLOOR SUPPORT CORRODED IN FORWARD CARGO COMPARTMENT AT STA 1099, RBL 20. THE CORRODED AREA WAS CUT OUT, REPAIR ANGLES WERE FABRICATED A - [SDR CALA9700162](https://openairdocs.org/sdr/CALA9700162), Dec 18, 1996: HINGE ANGLE. CRACKED. INSPECTION FOUND A 5.5 INCH CRACK IN UPPER RADIUS OF LOWER AFT FAIRING 535JL INBOARD HINGE AT OUTBOARD LT FLAP INBOARD FACE. THE FAIRING WAS REMOVED AND THE COR - [SDR CALA9700106](https://openairdocs.org/sdr/CALA9700106), Dec 18, 1996: SLAT. GOUGED. INSPECTION FOUND RT NR 6 SLAT CHAFED AND GOUGED AT INBOARD END, 12 INCHES UP FROM L/E TIP. THE SLAT WAS REPAIRED IAW ECRA 5750-02573. - [SDR CALA9700107](https://openairdocs.org/sdr/CALA9700107), Dec 8, 1996: SUPPORT. CORRODED. INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT STA 472 LBL 54. A FLOOR SUPPORT REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-00-01, 51-21-01, 51-31-01, 51-35 - [SDR CALA9601868](https://openairdocs.org/sdr/CALA9601868), Nov 29, 1996: SKIN. CORRODED. INSPECTION FOUND FUSELAGE SKIN CORRODED STA 1509-1521, XCW 25 TO XCW -25. SKIN DOUBLERS WERE FABRICATED AND INSTALLED IAW ECRA 5330-02465 AND SRM 51-31-01. - [SDR CALA9601870](https://openairdocs.org/sdr/CALA9601870), Nov 27, 1996: DOUBLER. CRACKED. INSPECTION FOUND BOTH INBOARD AND OUTBOARD FORWARD UPPER ATTACH DOUBLERS OF NR 3 PYLON AFT FAIRING 489AL CRACKED THROUGH. THE CRACKED DOUBLERS WERE REMOVED IAW - [SDR CALA9601852](https://openairdocs.org/sdr/CALA9601852), Nov 14, 1996: SUPPORT. CORRODED. INSPECTION FOUND THE UPPER HORIZONTAL SURFACE OF FORWARD END FLOOR SUPPORT CORRODED AT STA 1900, RBL 57. THE CORRODED SECTION WAS REMOVED, A NEW SECTION WAS SPL - [SDR CALA9601869](https://openairdocs.org/sdr/CALA9601869), Nov 11, 1996: SKIN. CRACKED. INSPECTION FOUND A .50 INCH CRACK ON LT AND RT CORNERS OF NR 3 ENGINE PYLON FORWARD END. THE CRACKED AREAS WERE CUT OUT. TWO EACH DOUBLERS, FILLERS, AND TRIPLER - [SDR CALA9601866](https://openairdocs.org/sdr/CALA9601866), Nov 5, 1996: SKIN. DENTED. INSPECTION FOUND THE RT WING NR 4 SLAT DENTED AT XORS 480. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-10-00, FIGURE 12. - [SDR CALA9601865](https://openairdocs.org/sdr/CALA9601865), Nov 5, 1996: SKIN. GOUGED. INSPECTION FOUND FUSELAGE SKIN GOUGED IN TWO PLACES AT STRINGER 48R, B.S. 1581 AND 1585. THE GOUGES WERE REMOVED IAW SRM 53-00-01, FIGURE 1. TWO DOUBLERS, FILLE - [SDR CALA9601854](https://openairdocs.org/sdr/CALA9601854), Oct 21, 1996: SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT CORRODED AT BS 1986, LBL 27. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-21-01, 51-31-01 AND 53-60-01, FIGURE 1. - [SDR CALA9601853](https://openairdocs.org/sdr/CALA9601853), Oct 21, 1996: SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT CORRODED AROUND FLOOR PANEL ATTACH HOLES FROM BS 1986 TO 2007, RBL 27. A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 5 - [SDR CALA9601851](https://openairdocs.org/sdr/CALA9601851), Oct 21, 1996: SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT CORRODED AT BS 1963, LBL 27. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-21-01, 51-31-01 AND 53-60-01, FIGURE 1. - [SDR CALA9601848](https://openairdocs.org/sdr/CALA9601848), Oct 21, 1996: SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT CORRODED AT BS 1882, LBL 36. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-21-01, 51-31-01 AND 53-60-01, FIGURE 1. - [SDR CALA9601856](https://openairdocs.org/sdr/CALA9601856), Oct 20, 1996: SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 457, RBL 29. A NEW SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-21-01, 51-35-01 AND 53-11-01, FIGURE 1A. - [SDR CALA9601874](https://openairdocs.org/sdr/CALA9601874), Oct 19, 1996: SKIN. CRACKED. THE LT WING FIXED LEADING EDGE SKIN HAD A 2.5 INCH CRACK FROM LOWER EDGE RUNNING FORWARD AT APPROXIMATELY XORS 810. THE CRACKED AREA WAS REMOVED. DOUBLER, FILLE - [SDR CALA9601873](https://openairdocs.org/sdr/CALA9601873), Oct 19, 1996: SKIN. DENTED. INSPECTION FOUND LT WING NR 1 LEADING EDGE SLAT DENTED ON LEADING EDGE NOSE STARTING 30 INCHES OUTBOARD OF XFS 145. THE DENTED AREA WAS CUT OUT AND DOUBLERS WER - [SDR CALA9601864](https://openairdocs.org/sdr/CALA9601864), Oct 19, 1996: SKIN. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN INNER SKIN AT RT DOOR CUT-OUT SURROUNDING FRAME STRUCTURE, STA 1308.5, AT CABIN FLOOR. THE SKIN WAS REPAIRED BY FABRICATING A - [SDR CALA9601863](https://openairdocs.org/sdr/CALA9601863), Oct 19, 1996: SKIN. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN INNER SKIN AT RT DOOR CUT-OUT SURROUNDING FRAME STRUCTURE, STA 1255, AT CABIN FLOOR. THE CRACK WAS STOP DRILLED. A DOUBLER WA - [SDR CALA9700163](https://openairdocs.org/sdr/CALA9700163), Oct 18, 1996: CLIP. CORRODED. INSPECTION FOUND CLIP FROM RT WHEEL WELL PRESSURE PANEL TO FRAME CORRODED ON UPPER FORWARD FACE OF FLANGE AT STA 1501, SIX INCHES BELOW CABIN FLOOR. A NEW CLIP - [SDR CALA9601855](https://openairdocs.org/sdr/CALA9601855), Oct 15, 1996: SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 472, LBL 54. TWO ANGLES, FILLER AND A FLOOR SUPPORT WERE FABRICATED AND INSTALLED IAW SRM 51-31-01, 51-21-01, 51- - [SDR CALA9601871](https://openairdocs.org/sdr/CALA9601871), Oct 13, 1996: HINGED PANEL. CRACKED. INSPECTION FOUND A .50 INCH CRACK AROUND FASTENER OF LT HORIZONTAL STABILIZER LOWER TRAILING EDGE HINGED PANEL AT STA XE 158. THE AREA WAS REPAIRED IAW SRM 51-7 - [SDR CALA9601872](https://openairdocs.org/sdr/CALA9601872), Oct 12, 1996: BLKHD STIFFENER. CORRODED. INSPECTION FOUND CORROSION AROUND LOWER BOLT HOLE OF T-SHAPED VERTICAL STIFFENER AT CENTER WHEELWELL AFT FACE OF FORWARD BULKHEAD, XCW -15.0. THE STIFFENER WAS - [SDR CALA9601867](https://openairdocs.org/sdr/CALA9601867), Oct 10, 1996: FRAME. CORRODED. THE RT CENTER MLG DOOR AFT FRAME WAS FOUND CORRODED. THE AFT FRAME WAS REMOVED AND REPLACED IAW SRM'S 51-35-01 AND 51-35-02. - [SDR CALA9601850](https://openairdocs.org/sdr/CALA9601850), Oct 10, 1996: SKIN. CORRODED. INSPECTION FOUND FUSELAGE SKIN CORRODED AT BS 1009 TO 1029, STRINGER 52. THE CORRODED AREA WAS CUT OUT. REPAIR DOUBLERS, FINGER DOUBLERS AND FILLER WERE INSTALL - [SDR CALA9601849](https://openairdocs.org/sdr/CALA9601849), Oct 10, 1996: SKIN. CORRODED. INSPECTION FOUND CORROSION ON FUSELAGE SKIN AT BS 1049 TO 1069, STRINGER 52. THE CORRODED AREA WAS REMOVED. REPAIR DOUBLERS, FINGER DOUBLER AND FILLER WERE INST ## Other aircraft with N37077 - [Cancelled 1947-10-14](https://openairdocs.org/deregistered/N37077-1947-10-14): Luscombe 8A, S/N 1738, built 1941. Owner: [Wilbanks J D](https://openairdocs.org/faa-owner/WILBANKS%20J%20D), [Spearman, TX](https://openairdocs.org/faa-place/TX/Spearman) - [Cancelled (date not recorded)](https://openairdocs.org/deregistered/N37077-undated): Boeing-Vertol CH-47(352), S/N MA034 --- 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.