BOEING 767 ENGINE CF6-80C2 - part 1

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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

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