What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
During climb the LH engine was not
Producing full power. Between low
Teens up to 10000 our climb rate was
About 500FPM. Initial engine numbers
On climb LH 1.98 epr 73 N1 380 EGT 85 N2
3500PPH. RH 1.91 epr 89 N1 470 EGT 92 N2
5700PPH.
Initial descent power idle lower
Altitude level flight
1.18 .99 Epr 1.31 1.33
38 N1 40 N1 N1 58 71
300 270 EGT 350 350
64 N2 66 N2 N2 78 84
900PPM 900PPH ff 2500
3500
Corrective action: replaced PT2 flex line in pylon with new line.
Ref amm 77-00-00 & 77-11-01
Tightened fitting iat amm s/p 20-30-02.
Leak check good iaw taskcard
77-071-002.
As the FAA filed it
DURING CLIMB THE LH ENGINE WAS NOT
PRODUCING FULL POWER. BETWEEN LOW
TEENS UP TO 10000 OUR CLIMB RATE WAS
ABOUT 500FPM. INITIAL ENGINE NUMBERS
ON CLIMB LH 1.98 EPR 73 N1 380 EGT 85 N2
3500PPH. RH 1.91 EPR 89 N1 470 EGT 92 N2
5700PPH.
INITIAL DESCENT POWER IDLE LOWER
ALTITUDE LEVEL FLIGHT
1.18 .99 EPR 1.31 1.33
38 N1 40 N1 N1 58 71
300 270 EGT 350 350
64 N2 66 N2 N2 78 84
900PPM 900PPH FF 2500
3500
CORRECTIVE ACTION: REPLACED PT2 FLEX LINE IN PYLON WITH NEW LINE.
REF AMM 77-00-00 & 77-11-01
TIGHTENED FITTING IAT AMM S/P 20-30-02.
LEAK CHECK GOOD IAW TASKCARD
77-071-002.
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