Owner type
Corporation
Serial number
49950
Year built
1991
Type
Fixed wing multi engine
Engine
Turbo-fan
Airworthiness
Standard, transport
Airworthiness date
August 23, 2019
Certificate issued
January 4, 2022
Expires
January 31, 2029
Mode S code
AB569D

From the FAA registry file of October 24, 2026.

On this page

Airworthiness directives that may apply · 23

Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.

1970In forceSuperseded2026
ADs by the year they took effect: 36 ADs
19704
19771
19881
19921
19951
19961
19972
19981
19994
20002
20011
20024
20031
20054
20063
20101
20112
20151
20211
See all 36 ADs

Information bulletins that may apply · 2

Advisory, not mandatory.

NTSB investigations

No NTSB investigations matched to N83GFMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Mcdonnell Douglas MD 83 aircraft

FAA incident reports

No FAA accident or incident reports matched to N83GFMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Mcdonnell Douglas MD 83 aircraft

Service difficulty reports · 1

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

Reports on N83GF not matched to an aircraft · 1

They name N83GF, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

STCs that may be installed · 11

Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.

Engine · Pratt & Whitney JT8D-219

STC SE482CHInstallation of Tube Processing Corporation (TPC) JT8D-200 Anti-Ice tube assemblies Part Numbers 2026-TP, 2027-TP, 2028-TP and 2029-TP and support brackets Part Number 2060-TP, 2061-TP, 2062-TP and 2063-TPUnited Technologies Corporation, Pratt & Whitney DivisionSTC SE01944LAInstallation of a JET Engineering, Ltd. Turbine Exhaust Cone Mixer (TECM).Jet Engineering LTDSTC SE02128ATInstallation of a replacement ring manufactured by Praxair as part of the Praxair Second Stage Turbine inner air seal ring assembly.PAS Technologies IncSTC SE00429ATIncorporate an alternate gear box stud installation.Jet Avion CorporationSTC SE2117SOInstallation of an oil tank safety cap adapter which prevents loss of oil in the event of loss or damage to the oil filler cap.Jet Avion CorporationSTC SE01650SEInstallation of Aviation Fleet Solutions MD-80 heavy weight noise abatement systemAviation FLeet Solutions LLCSTC SE2930SOInstallation of an alternate gearbox cover seal utilizing an aluminum retainer .040-inch thick with a molded-in-place elastomeric seal contoured to fit the main housing/cover flange interface.Parker O-Seal DivisionSTC SE1683GLInstallation of Rexnord O-Ring face seal P/N's 1-1337-701, 1-1633-701, 1-1738-701, and/or1-2233-701.Rexnord, IncSTC SE86WEReplace the airoils on P&WA P/Ns 495051, 478351, 583751, 653851, 653951, 572451, 583351, 653751, 653151, 676951, 728951, 709951, 710751, 627751, 737271, 578551, 738271, 747171, 792871, 786471, 583751, 777971, 780591, 782571, 793181, 799771, 794481, 794491 , 798781, and 799191.Chromizing CompanySTC SE557NEInstallation of oil tank shuttle valve.Stockbridge William DSTC SE1930SOInstallation of power control shaft bushing.Cook Airtomic Division