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Aircraft record

N970AX1970 Douglas DC-9-41

DeregisteredUnclaimedSource: FAA, updated Oct 18, 2026

This N-number isn't registered right now. Below is its last known registration, canceled Nov 18, 2009.

Safety record in brief:No NTSB accidents or incidents since 1982No ADs since 1998 matched58 service difficulty reports

Registration
Deregistered
Last based in
Guthrie, OK
owner city / state
Owners
1
on record
NTSB events
None
since 1982
ADs may apply
0
confirm with A&P
Service reports
58
since 1995

Registration

FAA Aircraft Registry · Oct 18, 2026
Last registered owner
Stewart Industries International LLC
Owner type
Corporation
City, state
Guthrie, OK
Canceled
Nov 18, 2009
Airworthiness
Standard · Transport
Airworthiness date
Feb 26, 1993

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-9-41
Year
1970
Serial number
47494
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
AD83BB

Engine

Make and model
P & W Jt8d Series
Type
Turbo-jet
Power
7,700 lb thrust

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

Ownership history

Ownership history from FAA records
  1. until 2009Stewart Industries International LLCGuthrie, OK

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 18, 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 (58)

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.

  • Lights · power supply · defectiveSep 9, 2008

    EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY POWER SUPPLY IAW DC9 MM CHAPTER 33.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Engine · engine · failedJun 24, 2007

    NR 1 ENGINE, 1ST STAGE TURBINE HAD SEVERAL BLADES WITH CRACKED LEADING EDGE TIPS. ALSO SEVERAL BLADES HAD MOLTEN METAL ON TIPS. OUT OF SERVICABLE LIMITS IAW JT8D MM 72-50-00-210-002. REMOVED AND REPLACED NR 1 ENGINE IAW DC9 MM ON JOB CARD 9090010.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Electrical power · charger · defectiveJun 13, 2007

    WHILE STARTING APU, NOTICED NOISE AND SMOKE EMITTING FROM BATTERY CHARGER. REPLACED BATTERY CHARGER IAW DC9 MM 24-30-02-2-0001. ALSO, REPLACED BOTH AIRCRAFT BATTERIES AND BATTERY TEMPERATURE SENSOR IAW DC9 MM 24-30-01-0-0001.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reports
  • Fuselage · seat track · corrodedJan 3, 2007

    FLOOR TRACK CORRODED AT STA 224 - 232, RIGHT BUTT LINE 54. REMOVED AND REPLACED TRACK IAW DC9 SRM 51-30-1.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · bulkhead · crackedJan 2, 2007

    AFT PRESSURE BULKHEAD LEFT LOWER CORNER WAS CRACKED. REPAIRED AREA IAW DC9 REA D953-55282MR.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Stabilizers · fitting · crackedDec 28, 2006

    HORIZONTAL STABILIZER REAR SPAR FITTING WAS CRACKED AT SCREW HOLES FOR P/N: 5910405-3 COVER PLATE. REMOVED AND REPLACED REAR SPAR FITTING IAW DC9 SRM 51-30-1.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Doors · skin · crackedDec 28, 2006

    LEFT MAIN ENTRY DOOR CORNER CRACKED ON INTERIOR WEB CUTOUT. REPAIRED MAIN ENTRY DOOR INNER SKIN/WEB IAW DC9 SRM 52-42-0 AND 52-01.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Stabilizers · skin · damagedDec 27, 2006

    RIGHT ELEVATOR UPPER SKIN HAD HEAVY STATIC DISCHARGE DAMAGE 3 FEET FROM TIP. REPAIRED AREA IAW DC9 SRM 51-70-6.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · pan · corrodedJan 7, 2005

    AFT LOWER CARGO DOOR CUTOUT LOWER PAN CORRODED AND FORWARD LOWER CORNER OF PAN BULGED WITH 3 RIVETS THROUGH THE SKIN POPPED. REMOVED DOOR PAN / SCUFF PLATE / WEB. REMOVED AND REPLACED -45 DOUBLER. CLEANED CORROSION ON DOOR PAN AND RE-INSTALLED DOOR PAN / WEB / SCUFF PLATE IAW DC-9 SRM 51-10-3…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Doors · fitting · crackedJan 6, 2005

    UPPER AFT STOP TEE FITTING CRACKED FORWARD LOWER CARGO DOOR. REPLACED FITTING IAW DC-9 SRM 51-30-1, 51-30-2 AND 51-30-4.

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

Showing the 10 most recent of 58 reports.

Sources

  • FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 18, 2026
  • NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
  • FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 18, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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