Service difficulty report · Connector · Airbus A300*

Difficulty date
July 31, 2004
Submitted
August 3, 2004
Operation
Air carrier
Aircraft
N664FE
Make and model
Airbus A300*
Aircraft serial
768
Aircraft time
12,950 hours, 6,887 cycles
Engine
Ge CF680
Part
Connector
Condition
Damaged
Location
Nr 2 Engine
Stage of operation
TO
How discovered
C
Nature of condition
J
Precautionary procedure
C

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

What was found

ON TAKE OFF ROLL APPROX 60 KTS ECAM MOMENTARALY CAME ON. NR 2 ENG REV PRESSURIZED- INDICATION WENT OUT ABOUT 100 KTS AND CONTINUED NORMAL TAKE OFF. APPROX 800 AGL INDICATION RETURNED TO ECAM AND STAYED ON. PROCEDURE WAS FOLLOWED TO PULL NR 2 THROTTLE TO IDLE AND NOT USE IT FOR THRUST. FACT 31JUL04 16:27 ROC R ON INITIAL MEL PROCEDURES FOR NR 2 ENGINE THRUST REVERSER. BELIEVED ENGINE WAS PRE SB GE 78-1086 UPON FURTHER INSPECTION FOUND TO BE POST SB GE 78-1086 REMOVED AND STOWED SOLENOID AND PRESSURE SWITCH CONNECTORS AND SOWED IAW MEL PROCEDURE 78-30-01-A, OK FOR SERVICE. ENT BY: 034759 RPT BY: 034759