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Aircraft record

N935L1974 Douglas DC-9-41

DeregisteredUnclaimedSource: FAA, updated Oct 17, 2026

This N-number isn't registered right now. Below is its last known registration, canceled Aug 27, 2008.

Safety record in brief:No NTSB accidents or incidents since 1982No ADs since 1998 matched19 service difficulty reports

Registration
Deregistered
Last based in
Lake Zurich, IL
owner city / state
Owners
1
since 1999
NTSB events
None
since 1982
ADs may apply
0
confirm with A&P
Service reports
19
since 1995

Registration

FAA Aircraft Registry · Oct 17, 2026
Last registered owner
Jet Capital LLC
Owner type
Corporation
City, state
Lake Zurich, IL
Certificate issued
Jul 15, 1999
Canceled
Aug 27, 2008
Airworthiness
Standard · Transport
Airworthiness date
Nov 22, 1983

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
1974
Serial number
47603
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
ACF936

Engine

Make and model
P & W Jt8d-15
Type
Turbo-jet
Power
15,500 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. 1999 – 2008Jet Capital LLCLake Zurich, IL

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 (19)

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 · inopNov 17, 1999

    THE FWD SECTION OF COACH CABIN EGRESS LIGHTING WAS INOPERATIVE. REPLACED THE POWER SUPPLY FOR ROWS 8 THRU 14. CHECK-C 9-28-98 STL.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Flight controls · motor · failedAug 16, 1999

    LONGITUDINAL TRIM CONTROL WHEEL AND SUITCASE HANDLES INOP. REMOVED AND REPLACED LONGITUDINAL PRIMARY TRIM MOTOR TWA STK NR 80374. OPERATIONAL CHECK WAS NORMAL. CHECK C 9-28-98 STL.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Lights · battery pack · dischargedFeb 2, 1999

    JUST PRIOR TO DEPARTURE FOUND FLOOR EGRESS LIGHTS AT ROW 15 TO 19 REMAINED ON. REPLACED THE BATTERY PACK. CHECK-C 9-28-98 STL.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reports
  • Air conditioning and pressurization · valve · wornSep 1, 1998

    CREW REPORTED SLOW PRESSURIZATION LOSS IN FLIGHT. REGAINED CABIN PRESSURIZATION IN DESCENT FROM BETWEEN 11000 AND 16000 FT. FLIGHT RETURNED TO STL. REPLACED RT PACK FLOW CONTROL VALVE, 2022014-2, AND PRESS RATIO SHUT OFF VALVE, 392714-1-1. CHECK-C 6-24-97 STL.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Air conditioning and pressurization · fan · malfunctionedJun 14, 1998

    STL - FLT 598 - AFATER TAKEOFF, THE RT PACK FILLED CABIN WITH SMOKE. THE PACK FAN WAS WORKING. RAN BOTH ENGINES AND RT PACK AND PACK FAN. NO SMOKE NOTED. GROUND CHECKS NORMAL. CHECK-C 3-23-98 MCI. (X)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Lights · power supply · inoperativeDec 13, 1997

    STL - FLT 689 - DURING CRUISE, L1 AND R1 DOOR EMERGENCY LIGHTS CAME ON. NO FLOOR LIGHTS. REPLACED POWER SUPPLY AND BATTERIES FOR L1 AND R1 EMERGENCY LIGHTS. MFG P/N 58222-2 POWER SUPPLY. OP-15 06-24-97 STL. (X)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · seat track · corrosionAug 14, 1997

    STL - REPLACED NR 4 SEAT TRACK FROM STA 200 TO STA 256 DUE TO CORROSION. (X)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · floorbeam · crackedAug 14, 1997

    STL - REPAIRED 3 INCH CRACK IN FLOORBEAM AT STATION 237 BY PULLEY BRACKET. (M)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · trap panel · crackedAug 14, 1997

    STL - RIGHT TRAP PANEL HAS CRACK IN PREVIOUS REPAIR. REMOVED AND REPLACED ENTIRE TRAP PANEL. (M)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Hydraulic power · pump · failedApr 25, 1997

    STL - FLT 563 - DURING CRUISE LOST RIGHT HYDRAULIC PRESSURE DUE TO WORN RIGHT ENGINE DRIVEN HYDRAULIC PUMP, MFG P/N 314195, MANUFACTURED BY VICKERS INC. OPERATIONAL CHECK NORMAL. (M)

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

Showing the 10 most recent of 19 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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