Service difficulty report · Comp Blade · Airbus A310222

Difficulty date
April 18, 1998
Submitted
March 26, 2000
Operation
Air carrier
Aircraft
N417FE
Make and model
Airbus A310222
Aircraft serial
333
Engine
Pwa JT9D7R4E
Part
Comp Blade
Part number
804541
Condition
Damaged
Location
Nr 1 Engine
Stage of operation
CL
Nature of condition
E, J
Precautionary procedure
A

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

What was found

98-0110 - STA-DFW - AFTER ROTATION AND DURING CLIMB, EXPERIENCED A SEVERE VIBRATION FROM NR 1 ENG. WHEN POWER PULLED BACK BELOW 1.2 EPR, VIBRATION WOULD STOP, NO ABNORMAL READING NOTED ON VIBRATION METER. NOTICED NEED FOR RUDDER TRIM DURING CLIMB. REMOVED NR 1 ENG NOSE COWL, FAN BLADES, FRONT CASE PER M/M 71-11-00, 72,23-00, 72-10-00 SEE LOG 01039388 FOR NOSE COWL INSTALLATION. INSTALLED FRONT FAN CASE PER JTPD-7R4 SEC 72-33-00 RUB WEAR CHECKED OK AFTER RUN PW INSPECT XC374 EVM ON ENG RUN 0.4 RAN ENG PER JRH INSTALLED FAN BLADES PER PW SEC 72-31-00.

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