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Aircraft record

N997ZDouglas DC-9-32

DeregisteredUnclaimedSource: FAA, updated Oct 17, 2026

This N-number isn't registered right now. Below is its last known registration, canceled Aug 24, 2001.

Safety record in brief:No NTSB accidents or incidents since 1982No ADs since 1998 matched52 service difficulty reports

Registration
Deregistered
Last based in
Salt Lake City, UT
owner city / state
Owners
1
since 1997
NTSB events
None
since 1982
ADs may apply
0
confirm with A&P
Service reports
52
since 1995

Registration

FAA Aircraft Registry · Oct 17, 2026
Last registered owner
Wells Fargo Bank Northwest NA Trustee
Owner type
Corporation
City, state
Salt Lake City, UT
Certificate issued
Aug 22, 1997
Canceled
Aug 24, 2001

We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.

Airframe & engine

FAA Registry + type data

Airframe

Manufacturer
Douglas
Model
DC-9-32
Serial number
47029
Aircraft type
Fixed wing multi engine
Category
Land
Certification
Type Certificated
Seats
85
Engines
2
Max takeoff weight
20,000 and over lb
Mode S code
ADEEE3

Engine

Type
Turbo-jet

Total time and engine hours aren't public. They appear here once the owner adds logbooks.

Ownership history

Ownership history from FAA records
  1. 1997 – 2001Wells Fargo Bank Northwest NA TrusteeSalt Lake City, UT

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 17, 2026 · SDRs · Oct 16, 2026

NTSB events (0)

No NTSB accidents or incidents found for this airframe since 1982.

ADs published since 1998 that may apply (0)

These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.

No ADs published since 1998 matched this airframe or engine model.

AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.

Service Difficulty Reports (52)

Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.

  • Landing gear · actuator · wornJan 7, 2000

    CREW WAS UNABLE TO EXTEND THE NOSE LANDING GEAR DURING APPROACH TO MLI WAS NECESSARY TO USE MANUAL NOSE GEAR EXTENSION. FOUND PROBLEM WAS THE NOSE LANDING GEAR BUNGEE CYLINDER. MAINTENANCE FERRIED THE AIRCRAFT TO STL FOR REPLACEMENT. CHECK-C 8-28-99 STL.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · longeron · crackedAug 27, 1999

    DURING CHECK-C MAINT, LONGERON 2L WAS FOUND CRACKED AT THE END CAP STA 1076, ONE INCH LONG. REPAIRED PER SRM 53-02, FIG 8 AND 18.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · longeron · crackedAug 27, 1999

    DURING CHECK-C MAINT, LONGERON 2R WAS FOUND CRACKED AT END CAP STA 1076, A ONE INCH CRACK. REPAIRED PER SRM 53-02, FIG 8 AND 18.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reports
  • Fuselage · skin · corrodedApr 14, 1998

    MCI - DURING OP 15 MAINTENANCE CHECK, FOUND FUSELAGE SKIN BENEATH DOOR THRESHOLD HAD CORROSION AT STATION 916 TO 945, L29R TO L27R. REPAIRED AS PER ARA 15272 AND STD PRACTICES. (M)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Wings · rib · wornApr 3, 1998

    MCI - DURING OP 15 MAINTENANCE CHECK, FOUND HOLE WORN THROUGH FLAP RIBS AT RT WING INBOARD AND OUTBOARD FLEX JOINT BOTTOM SIDE. REPLACED END RIBS PER SRM 51-01 AND TWA STD PRACTICE. (M)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · bulkhead angle · crackedApr 3, 1998

    DURING OP 15 MAINTENANCE CHECK, FOUND FUSELAGE TO BULKHEAD ATTACH ANGLE CRACKED BETWEEN LONG 15L AND 16L. REPLACED ANGLE PER SRM 51-01, PAGE 1 ITEM C, AND TWA STD PRACTICE. (M)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · support · crackedMar 31, 1998

    MCI - DURING OP 15 MAINTENANCE CHECK, FOUND CABIN CHAIR AND FLOORBEAM SUPPORT CRACKED AT STATION 680, LBL 22 IN. REPLACED PART PER SRM 51-01-01 AND STANDARD PRACTICES. (M)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · intercostal · crackedMar 30, 1998

    MCI - DURING OP 15 MAINTENANCE CHECK, FOUND FS 1043 LBL 10.5 INCH INTERCOSTAL CRACKED ON LWR FLANGE, LEFT SIDE OF TAIL SKID CASTING. REPAIRED AND REINSTALLED PER SRM 53-01, FIG 2 PAGE 10. (M)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · skin · damagedMar 30, 1998

    MCI - DURING OP 15 MAINTENANCE CHECK, FOUND TEMPORARY REPAIR ON OUTER FUSELAGE SKIN AT STA 965, LONGERONS 13 AND 14L. REPAIRED PER SRM 53-04, FIG 32, AND TWA STD PRACTICES. (X)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · rivets · failedMar 27, 1998

    MCI - DURING OP 15 MAINTENANCE CHECK, FOUND LONGERON 26L WITH A RIVET POPPED AT FS 354. REMOVED AND REPLACED RIVETS AS REQUIRED PER SRM 51-30-02. (M)

    From FAA Service Difficulty Reports; matched by N-number and serial number.

Showing the 10 most recent of 52 reports.

Sources

  • FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 17, 2026
  • NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
  • FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 17, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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