N94246

Cancelled 2004

Deregistered aircraft · 1948 Convair 600-240D · Rolls-Royce DART-542 series

Cancelled
March 8, 2004
Status when cancelled
Valid registration
Serial number
102
Year built
1948
Type
Fixed wing multi engine
Engine
Turbo-prop
Airworthiness
Standard, transport
Airworthiness date
March 21, 1966
Certificate issued
August 13, 2001
Last registry action
August 13, 2001
Mode S code
AD1799
Owner when cancelled
J&R Aircraft Leasing LLC
Location
Columbus, IN
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.

FAA incident reports · 2

FAA accident and incident reports matched to this aircraft by N94246 and the event date: up to this one’s cancellation.

Service difficulty reports · 7

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

SDR GAIA9936Rod · disconnectedFLT 485 - AFTER DEPARTURE FROM CVG, RIGHT ENGINE TEMP STARTED TO RISE AFTER CLIMB POWER WAS SET, TRIMMER MOTOR HAD NO EFFECT ON TEMP, POWER WAS REDUCED TO KEEP TEMPS IN LIMITS. FLIGHT CREW DECLARED AN EMERGENCY AND RETURNED TO CVG AND MADE AN UNEVENTFUL LANDIMar 8, 1999 · N94246 · Cvac 600240D · Power LeverSDR GAIA9908Wire · shortedKHA - FLT 176 - AFTER DEPARTURE FROM CLE APPROX 10 MINUTES INTO FLIGHT, CREW SMELLED STRONG ELECTRICAL ODOR. FLIGHT CREW NOTIFIED ATC DELARED AN EMERGENCY AND RETURNED TO CLE AND MADE AN UNEVENTFUL LANDING. A CLOSE INSPECTION OF THE EXTERNAL POWER WIRING SYSJan 29, 1999 · N94246 · Cvac 600240D · Electrical Power System WiringSDR GAIA2297Stiffener · crackedDURING C-CHECK INSPECTION, A CRACK WAS FOUND IN THE VERTICAL STIFFENER FOR THE LEFT AFT WING SPAR AT STATION 1. TRACOR FURNISHED KHA THE ORIGINAL 240-1610740C DRAWINGS TO MANUFACTURE THE REPLACEMENT PARTS. THE NEW VERTICAL STIFFENER WAS INSTALLED IAW THE GD Apr 21, 1997 · N94246 · Cvac 600240D · Wing Miscellaneous StructureSDR GAIA2197Spar Rail · corrodedTAT - DURING C-CHECK INSPECTION, FOUND CORROSION AT UPPER LT TOP AFT WING SPAR RAIL AT FUSELAGE WING FITTINGS. CORROSION DAMAGE SUBMITTED TO TRACOR COM JET/ CONVAIR FOR EVAULATION. THE ABOVE AREAS WERE FOUND TO BE IN LIMITS IAW TRACOR MSG NR 505-97-WLD-058 DApr 21, 1997 · N94246 · Cvac 600240D · Wing SparSDR GAIA2097Bulkhead · crackedDURING C-CHECK INSPECTION, A ONE INCH CRACK WAS FOUND IN RIGHT FUSELAGE STATION 766.63 HORIZONTAL STABILIZER ATTACH POINT BULKHEAD. THE BULKHEAD WAS REPAIRED IAW TRACOR MSG NR 505-97-WLD-047 DATED 2-26-97 TFS/ASD FAA DER APPROVED. (M)Apr 21, 1997 · N94246 · Cvac 600240D · Fuselage Main, BulkheadSDR GAIA1997Skin · crackedDURING C-CHECK INSPECTION, THREE SMALL CRACKS WERE FOUND IN THE LOWER RIGHT WING SKIN AT STATION 9 INCHES FORWARD OF REAR SPAR. THE WING WAS REPAIRED IAW TRACOR MSG NR 505-97WLD-059 DATED 3-17-97 FAA DER APPROVED. (M)Apr 21, 1997 · N94246 · Cvac 600240D · Wing, Plate/SkinSDR GAIA9523Retract Mech · out of adjustDURING TRAINING FLIGHT, A SIMULATED LANDING APPROACH PROCEDURE WAS INITIATED. THE LT MLG DID NOT INDICATE DOWN AND LOCKED CONDITION. THE FLIGHT CREW FOLLOWED EMERGENCY PROCEDURES, NOTIFIED ATC OF THE EMERGENCY, AND MADE AN UNEVENTFUL LANDING. INSPECTION REVJan 31, 1996 · N94246 · Cvac 600240D · Landing Gear Retraction/Extension System

Other aircraft with N94246 · 1

The FAA can assign a mark to another aircraft once a registration is cancelled. N94246 is registered now to the first aircraft listed.