boeing 767 engine cf6-80c2 - part 1
TRANSCRIPT
By Ccoyure Tito
(P61)
PURPOSE
LOCATION
CHARACTERISTICS
REMOVAL & INSTALLATION
CAUTION: DURING REMOVAL
& INSTALLATION, DO NOT
LEAVE TOOLS OR OTHER
OBJECTS IN AIR INLET
CAUTION: ADJUST
SLING TO TAKE ONLY
WEIGHT OF INLET
COWL
PURPOSE
LOCATION
CHARACTERISTICS
OPERATIONS & LIMITATIONS
REMOVAL & INSTALLATION
WARNING: ENSURE THAT HOLD- OPEN ROD IS FULLY
EXTENDED AND LOCKED. RED BAND & “UNLOCKED”
CAUTION: DO NOT ALLOW FAN COWL
PANEL TO SLAM CLOSED
WARNING: ADEQUATELY
SUPPORT FAN COWL
PANEL DURING
HANDLING. WEIGH
APROX. 50 KG EACH
CAUTION: RAISING OR
LOWERING AFTER REMOVAL
MAY DAMAGE UPPER COWL
SEAL. LIFT PANEL OUTWARD
FROM STRUT HINGE
ADJUSTMENT
TEST- Force req. to close latches
CAUTION: DO NOT USE
OVER 100 POUNDS (445 N)
FORCE TO PUSH LATCH
HANDLE CLOSED.
CAUTION: DO NOT ROTATE KEEPER
EYEBOLT TO ADJUST LATCH TENSIONGAP: .06 A 0.18”
CLOSING FORCE: 0.5 A 2.5”
RELIEF VALVE: 4350 – 4500 PSIG
CORE CORE PANEL WEIGH APROX 41 KG
LPC
ROTORQTY
1 38
2 62
3 71
4 80
5 71
CDP: COMPRESSOR
DISCHARGE PRESSURE
SIGNAL TO THE MEC ↓
(80)
(74)
STG 2 HPT NOZZLE:
24 SEGMENTS WITH 2
VANES EACH
LPT
ROTORQTY
1 118
2 124
3 88
4 88
5 98
