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Aircraft record

N583AN1993 Mcdonnell 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 Sep 5, 2013.

Safety record in brief:No NTSB accidents or incidents since 1982No ADs since 1998 matched34 service difficulty reports

Registration
Deregistered
Last based in
Salt Lake City, UT
owner city / state
Owners
1
since 2011
NTSB events
None
since 1982
ADs may apply
0
confirm with A&P
Service reports
34
since 1995

Registration

FAA Aircraft Registry · Oct 19, 2026
Last registered owner
Bank Of Utah Trustee
Owner type
Corporation
City, state
Salt Lake City, UT
Certificate issued
Jan 19, 2011
Canceled
Sep 5, 2013
Airworthiness
Standard · Transport
Airworthiness date
Aug 3, 2000

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
Year
1993
Serial number
53183
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
A7811A

Engine

Make and model
P & W Jt8d Series
Type
Turbo-fan
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. 2011 – 2013Bank Of Utah TrusteeSalt Lake City, UT

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 (34)

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.

  • Indicating and recording systems · display · inoperativeSep 1, 2008

    AIR TURN BACK, AFTER LIFT OFF CAPT AND F/O PRIMARY DISPLAY AND NAV DISPLAY WENT BLANK, AIRSPEED INDICATOR, ALTIMETER SHOWED FLAGS. GONE AHRS DISPLAYED. CAPT`S VSI AND CAPT`S RMI SHOW HDG FLAG AND VSI AND RA FLAGS. FTR AND RTS WERE ACCOMPLISHED AT BOTH DFGC SHOWED GO IAW AMM 22-01-05, PAG 204.…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Indicating and recording systems · warning light · multiple indSep 20, 2007

    DURING TAKEOFF RUN AT 80 KNOTS "AUTO SPOILER FAIL" ANNUNCIATION CAME ON. AT 95 KNOTS SLAT "DISAG" LIGHT ILLUMINATED SLAT "TO" LIGHT WENT OFF AND "TO" WARNING SOUND: "SLATS" TO WAS DISCONTINUED IAW AMM 27-81-00 PAGE 109 WAS PERFORMED T/S; TO AUTO SPOILER SYSTEM AND AUTO SLAT SYSTEM T/O…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Engine · engine · damagedJun 2, 2007

    AT TO ABOUT 11000 FT, A BIRD IMPACT OCCURRED ON THE LEFT ENGINE, PARAMETER DROP 1.4 EPR THEN ALL PARAMETERS CAME BACK TO NORMAL. IN ACCORDANCE WITH EWO 83-72-7309 LT ENGINE WAS REPLACED IAW AMM 71-00-00 PAGE 501 WAS PERFORMED ADJUSTMENT/TEST AND CONDITIONS ARE SATISFACTORY FOR OPTIMUM OPERATION.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reports
  • Doors · switch · malfunctionedMay 1, 2007

    MID CARGO DOOR OPEN ANNUNCIATION HAD BEEN ON IN FLIGHT. (EMERGENCY LANDING WAS PERFORMED) IAW AMM 52-31-00 PAG 601 PERFORMED CHECK MID CARGO DOOR SWITCH. NORMAL OPERATION.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Hydraulic power · pump · failedOct 23, 2006

    DURING CLIMB, RT HYDRAULIC PRESSURE DROPPED TO (0) PSI AND QUANTITY GOES UP TO 19 QTY. IAW AMM 29-10-14/201 THE FILTER WERE CHECKED AND BLED AND SYSTEM AND CHECKED HYD LEVEL IAW AMM 12-13-01. THE RT ENGINE DRIVEN HYD PUMP WAS DEFERED TO DMI 849 IAW MEL 29-5 CAT (C), AND DOWN GRADE CAT II, NOT CAT…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Engine indicating · transmitter · malfunctionedSep 24, 2006

    PILOT REPORT: DURING TAKE OFF ROLL AT 80 KTS RT EPR INDICATIONS SHOWED 1.6 AND NORMAL EPR WAS 2.03 THE OTHER ENGINE PARAMETERS WERE NORMAL, BECAUSE OF THIS, A REJECTED TAKE OFF WAS PERFORMED. IAW AMM 77-11-02/201 THE RT EPR TRANSMITER WAS REMOVED AND REPLACED BY OTHER ONE, ENGINES WERE RUN UP IAW…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Engine fuel and control · fuel control · out of trimApr 28, 2006

    DURING T/O, A DIFFERENCE BETWEEN LT AND RT OF EPR 0.5 PERCENT. DURING FLIGHT AT FL 320 MACH 076 LT EPR 1.98 AND RT EPR 1.82. THEN USING ENG ANTI ICE AUTO THROTTLE DISCONNECT AND LT EPR 1.28 & RT EPR 1.72. WITH THIS PROBLEM IS UNABLE TO FLY IN IT CONDITIONS IN ACCORDANCE WITH AMM 71-00-00 PAGE 501.…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Doors · switch · malfunctionedMar 30, 2006

    AFTER TAKEOFF, TAIL CONE UNSAFE ANNUNCIATION ILLUMINATED. IN ACCORDANCE WITH AMM 52-70-11 PAGE 201-202. THE TAIL CONE EXTERNAL WARNING SWITCH WAS REPLACED AND AMM 53-53-00 PAGE 501 ADJUSTMENT/ TEST TAILCONE WAS PERFORMED SWITCH PART NUMBER H20-28B.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Hydraulic power · pump · inoperativeMar 18, 2006

    DURING CLIMB, RIGHT HYD PRESS (R HYD PRESS) ANNUNCIATION CAME ON. RIGHT HYD PRESS DROPPED TO ZERO. RT ENGINE DRIVEN PUMP IS INOP. IN ACCORDING WITH AMM 29-10-05 ENGINE DRIVEN HYDRAULIC PUMP WAS REPLACED.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Flight controls · unknown · unknownJan 28, 2006

    DURING ROLLING TAKEOFF AUTOSPOILER ALARM CAME ON TAKE OFF WAS DISCONTINUED AT 80 KTS AND RETURN TO GATE. NOTE: AUTOBRAKE WAS ARM TO, THE AURAL ALARM CAME ON WITH NO ANNUN ON THE EOAP. IAW AMM 05-57-00 PAG 601 HIGH ENERGY STOP/MAIN LANDING GEAR WHEELS TIRES AND BRAKES CHECK WAS DONE. IAW AMM…

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

Showing the 10 most recent of 34 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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