Service difficulty report · Wire · Lear 35A

Difficulty date
November 4, 2003
Submitted
November 4, 2003
Operation
General aviation
Aircraft
N44TT
Make and model
Lear 35A
Aircraft serial
211
Aircraft time
13,735 hours, 13,829 cycles
Engine
Garrtt TFE73122B
Engine time
13,243 hours, 12,287 cycles
Part
Wire
Condition
Loose
Location
Nr 2 Engine
Part time
13,735 hours, 13,829 cycles
Stage of operation
NR
How discovered
9
Nature of condition
O
Precautionary procedure
O

As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.

What was found

AC WAS TAKING OFF WHEN RT FUEL COMPUTER LIGHT CAME ON AT APPROX 100 KNOTS. PILOT ABORTED TAKE OFF. DURING TAXI BACK TO FBO NR 3 AND NR 4 MLG WHEEL FUSIBLE PLUGS BLEW DUE TO OVERHEATED BRAKES. MECH INSTALLED A SPARE WHEEL AND TIRE ASSY ON RT MLG SO THAT AC COULD BE MOVED OFF OF TAXIWAY. MAINT WAS DISPATCHED TO DETERMINE CAUSE OF ENG COMPUTER PROBLEM, CHANGE NR 3, NR 4 BRAKES, WHEEL AND TIRE ASSEMBLIES. MAINT DETERMINED THAT FUEL COMPUTER LIGHT WAS CAUSED BY LOOSE WIRE TO RT ENGINE PT2 PROBE CONNECTOR LOCATED AT NAC.STA. 188.5 NAC. BL 100.0. NO ANTI-SKID MALFUNCTION WAS NOTED. AC RETURNED WITH NO FURTHER INCIDENTS.

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