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Aircraft record

N632CTMcdonnell Douglas Aircraft Co MD 83

DeregisteredUnclaimedSource: FAA, updated Oct 19, 2026

This N-number isn't registered right now. Below is its last known registration, canceled Oct 6, 2017.

Safety record in brief:No NTSB accidents or incidents since 1982No ADs since 1998 matched22 service difficulty reports

Registration
Deregistered
Last based in
Wilmington, DE
owner city / state
Owners
1
since 2011
NTSB events
None
since 1982
ADs may apply
0
confirm with A&P
Service reports
22
since 1995

Registration

FAA Aircraft Registry · Oct 19, 2026
Last registered owner
Jet Midwest Group LLC
Owner type
Corporation
City, state
Wilmington, DE
Certificate issued
Mar 15, 2011
Canceled
Oct 6, 2017

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
Mcdonnell Douglas Aircraft Co
Model
MD 83
Serial number
49632
Aircraft type
Fixed wing multi engine
Category
Land
Certification
Type Certificated
Seats
155
Engines
2
Max takeoff weight
20,000 and over lb
Mode S code
A8456E

Engine

Type
Turbo-fan

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

Ownership history

Ownership history from FAA records
  1. 2011 – 2017Jet Midwest Group LLCWilmington, DE

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 19, 2026 · SDRs · Oct 16, 2026

NTSB events (0)

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

Accident history for this model

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 (22)

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.

  • Engine air · controller · malfunctionedJun 18, 2009

    THRUST SET FOR TAKEOFF, LT AND RT ENGINE EPR 2.08 LT ENG N1 98 PERCENT RT ENG N1 98.7 PERCENT, LT AND RT ENGINE EGT WITHIN LIMITS. ABOUT 100 KTS A STRONG DECELERATION WAS FELT, RT ENGINE EPR DROPPED TO 1.78, AFT CREW REPORTED A LOUD BANG FROM RT ENGINE. AMM 72-00-04 PAGE 112 ACCOMPLISHED. BLEED…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Indicating and recording systems · warning system · false activationDec 4, 2007

    DURING ROLL T/O FLAPS CONFIGURATION ALARM SOUNDS WITH THE FLAPS T/O SELECTOR IN TO POSITION AT 60 KTS. IAW AMM 27-53-01 PAG 201. FLAPS WARNING SWITCH CHECK AND TEST WERE EFECTUATED. FAULT NOT DUPLICATED.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Hydraulic power · packing · brokenOct 16, 2007

    DURING APP AT BOG, R HYD QTY DROPPED TO 1 QT WITH THE SYSTEMS PRESSURIZED. THERE WAS NOT R HYD QTY ANNU ON THE EOAP. (THIS CAUSES EMERGENCY LANDING) SEVERE HYD LEAK FOUND AT FWD OUTLET LINE FITTING OF MOTOR OPERATED DUAL SHUTOFF VALVE. DURING INSPECTION FITTING PACKING WAS FOUND BROKEN AND THE…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reports
  • Electrical power · electrical sys · multiple failSep 24, 2007

    DURING TAKEOFF ROLL, HAD AN ELECTRICAL FAILURE: TAKEOFF WAS ABBORTED AT 90 KNOTS. THE FLIGHT GUIDANCE STATUS AND MAINT PNL C/B G 25 WAS TRIPPED. THE AC BUSS PHASE B C/B WAS ALSO TRIPPED. ART WAS ACCURATED. IAW AMM 24-20-00/201 GCU`S WERE CHECKED AND RESET AND IAW WDM 24-23-00 CIRCUIT WAS CHECKED…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Landing gear · pin · installedJun 2, 2007

    AFTER TAKEOFF LEFT AND RIGHT AND GEAR DOOR OPEN LIGHTS REMAIN ON. ABNORMAL CHECK LIST CARRIED OUT AND RETURNED. LANDING EXTEND AND ALL INDICATION WERE NORMAL. NORMAL LANDING CARRIED OUT SKBO. GEAR LOCK PINS WERE FOUND INSTALLED ON BOTH MAIN LANDING GEAR. IAW TASK CARD 0003 AV NUMERAL 1D WERE…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Electrical power · control unit · failedMay 14, 2006

    DURING CLIMB AT FLIGHT LEVEL 210 AC CROSS DURING CLIMB AT FLIGHT LEVEL 210 AC CROSS TIE LOCK OUT LIGHT TURNED ON WITH NO ADDITIONAL LIGHTS IN THE EOAP. FLIGHT ATTENDANTS REPORTED STRONG ELECTRICAL ODOR. FOUND BURNT GCU APU IN ACCORDANCE TO AMM 24-20-07 PAG 401, GCU APU AND RT ENGINE GCU WERE…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuel · pump · failedJan 11, 2006

    DURING FLIGHT, CENTER TANK FAILS TO FEED. INFLIGHT ABNORMAL CHECKLIST ACCOMPLISHED. PERFORMED TROUBLESHOOTIING AS PER AMM 28-20-07 AND CONFIRMED THAT AFTER CENTRAL FUEL TANK AC PUMP IS FAULT. TRANSFERED TO DMI 648 AS PER MEL 28-2 CATEGORY C. MAINTENACE PROCEDURE ACCOMPLISHED DMI 648: AS PER AMM…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Electrical power · csd · failedApr 20, 2005

    DURING RT ENG START, RT GEN FREQ 396 CPS & GEN CAME ON LINE AT 50 PERCENT N2. REPORTED TO TECH. DURING TAKEOFF ROLL, RT GEN TRIPPED, RESET UNSUCCESFULL. RT CSD OIL TEMP BEGAN RISING UNTIL OFF SCALE, WITH GEN OFF, FOLLOWED CHKLST, CSD DISCONNECTED. THROUGH FL 280, APU OIL TEMP HIGH ANNUNCIATION…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Landing gear · transducer · malfunctionedNov 22, 2004

    TWO REJECTED TAKEOFF WAS PERFORMED DUE WHEEL NOT TURNING COMES ON APPROX 90 KNOTS. REPLACED TRANSDUCER IN MLG RT POSITION NR 3 AND NR 4 IAW AMM:32-43-02 PAG 201 PN OFF:4062575, S/N:OFF:627, S/N ON:5325A POS NR 3.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Landing gear · landing gear · out of rigOct 10, 2004

    TAKE-OFF WAS ABORTED DUE TO STRONG VIBRATION OA THE NOSE GEAR, IT HAPPENED ABOVE 100 KTS. IAW AMM 32-21-03 PAGE 403. IN NLG WAS PERFORMED CHECK AND RIGGING IN NOSE GEAR UPPER LINKAGE TORQUE TUBE.

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

Showing the 10 most recent of 22 reports.

Sources

  • FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 19, 2026
  • NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
  • FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 19, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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