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N939AX

Cancelled 2017

Deregistered aircraft · 1969 Mcdonnell Douglas DC-9-32 · Pratt & Whitney JT8D series

Open in FAA registry

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Cancelled: July 20, 2017
Status when cancelled: Registration expired, pending cancellation
Serial number: 47201
Year built: 1969
Type: Fixed wing multi engine
Engine: Turbo-jet
Airworthiness: Standard, transport
Airworthiness date: May 20, 1989
Certificate issued: October 15, 2008
Last registry action: October 15, 2008
Mode S code: AD072E
Owner when cancelled: Dhl Network Operations (USA) Inc
Location: Plantation, FL
Owner type: Corporation

Airframe modelMcdonnell Douglas DC-9-32TCDS A6WE · ADs, bulletins and aircraft registered now Engine modelPratt & Whitney JT8D seriesTurbo-jet

From the FAA registry file of October 28, 2026, cancelled registrations. Owners’ street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

FAA incident reports · 1

FAA accident and incident reports matched to this aircraft by N939AX and the event date: up to this one’s cancellation.

Incident 19921104051539IForced/Precautionary Landing · Peoria, ILAircraft struck a deer on liftoff. Returned. Lanlded safely.Nov 4, 1992 · Minor damage

Service difficulty reports · 106

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

SDR ABXA080083Relay · defectiveCENTER PRIMARY TRIM CIRCUIT BREAKER TRIPPED DURING TRIM SETTING. FOUND UP TRIM RELAY BURNT AT TERMINALS A1 & A2. REPLACED NOSE UP PRIMARY TRIM RELAY AND TERMINALS A1 & A2. OPS CHECK GOOD IAW DC9 AMM 27-40-04-5-0002.Feb 26, 2008 · N939AX · Doug DC932 · Stabilizer Control System SDR ABXA070105Floorbeam · crackedFLOORBEAM CRACKED TO LIGHTENING HOLE APPROXIMATELY STA 175, BUTT LINE 0. REPAIRED AREA IAW REA D953-55576MR.Apr 2, 2007 · N939AX · Doug DC932 · Fuselage Main, Floor Beam SDR ABXA070103Frame · crackedAFT RIGHT MAIN FRAME HAD CRACK AT FORWARD AND AFT FLANGES, MUST BE REPLACED PER NEA 53400102-002-30. REMOVED AND REPLACED RIGHT MAIN FRAME IAW DC9 EA 53400326-001-2. CRACK LENGTHS WERE 1" AND 1 1/4".Mar 16, 2007 · N939AX · Doug DC932 · Fuselage Main, Frame

See all 106 reports