N139WA

Cancelled 2010

Deregistered aircraft · 1980 Mcdonnell-Douglas DC-10-30 · GE CF6-50 series

Cancelled
July 15, 2010
Status when cancelled
Valid registration
Serial number
46583
Year built
1980
Type
Fixed wing multi engine
Engine
Turbo-fan
Airworthiness
Standard, transport
Airworthiness date
May 31, 1992
Certificate issued
February 6, 2007
Last registry action
March 24, 2009
Mode S code
A09E95
Owner type
Corporation

From the FAA registry file of October 29, 2026, cancelled registrations. Owners’ street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

NTSB investigations · 1

Matched to this aircraft by N139WA and the event date: up to this one’s cancellation.

FAA incident reports · 1

FAA accident and incident reports matched to this aircraft by N139WA and the event date: up to this one’s cancellation.

Service difficulty reports · 5

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

SDR WRLA2009118Fluid · leakingEDDP-KBWI ON LANDING AIRCRAFT BOUNCED A BIT ON BOTH MAINS AND BECAME SLIGHTLY AIRBORNE AGAIN AT WHICH TIME, THE GROUND SPOILERS DEPLOYED CAUSING A RAPID DESCENT AND SUBSEQUENT HARD IMPACT, WHICH CAUSED ANOTHER TRIP INTO THE AIR. AT SOME POINT THE SPOILERS CYCMay 6, 2009 · N139WA · Doug DC1030 · Hydraulic System, MainSDR WRLA2008088Skin · corrodedDURING C1 INSPECTION FOUND FASTENER HOLE CORRODED AT STA 2160 BETWEEN LONGERON 13R - 14R. REAMED HOLE TO REMOVE DAMAGE, EDDY CURRENT INSPECTION ACCOMPLISHED. MFG AND INSTALLED BUSHINGS AND REPAIR DOUBLER, TREAT, PRIME, SEAL AND PAINT IAW ENGINEERING REPAIR. Aug 27, 2008 · N139WA · Doug DC1030 · Fuselage Main, Plate/SkinSDR WRLA2008089Skin · corrodedDURING C1 INSPECTION FOUND FASTENER HOLE CORRODED AT STA 2160 BETWEEN LONGERON 13L-14L. REAMED HOLE TO REMOVE DAMAGE, EDDY CURRENT INSPECTION ACCOMPLISHED, MFG AND INSTALLED BUSHINGS AND REPAIR DOUBLER, TREAT, PRIME, SEAL AND PAINT IAW ENGINEERING REPAIR. (KAug 27, 2008 · N139WA · Doug DC1030 · Fuselage Main, Plate/SkinSDR WRL2008F00010Skin · corrodedDURING C1 INSPECTION FOUND FASTENER HOLE CORRODED AT STA 2160 BETWEEN LONGERON 13L - 14L. REAMED HOLE TO REMOVE DAMAGE, EDDY CURRENT INSPECTION ACCOMPLISHED, MFG AND INSTALLED BUSHINGS AND REPAIR DOUBLER, TREAT, PRIME, SEAL AND PAINT IAW ENGINEERING REPAIR. Aug 27, 2008 · N139WA · Doug DC1030 · Fuselage Main, Plate/SkinSDR WRLA2008072Bolt · shearedDURING C-CHECK INSPECTION FOUND 1 BOLT SHEARED AND RUSTED, AND 1 BOLT RUSTED AT RT WING ROOT FUSELAGE ANGLE. FUSELAGE STA 1371. REAMED HOLES, EDDY CURRENT INSPECTION ACCOMPLISHED, MFG AND INSTALLED TAPERED WASHERS, TREAT, PRIME, SEAL AND PAINT IAW ENGINEERINAug 26, 2008 · N139WA · Doug DC10 · Fuselage Miscellaneous Structure