Cabin Left Side; Fuselage - Front - Bell BHT-206L3-FM-1 LongRanger-III Flight Manual

BHT-206L3-FM-1
DOT APPROVED
a. Nodal beam - Condition and
security of elastomeric
bearings, elastomeric strap,
and fore and aft restraint
damper.
I
b. Transmission oil filter bypass
button - Ensure not extended.
c. Main driveshaft forward
coupling - Condition and
evidence of grease leakage.
Check paint strip for evidence
of overheat indicated by brown
color.
d. Cockpit indicator pressure
lines - Condition and security.
e. Access door - Secured.
2-14. FUSELAGE - CABIN LEFT
SIDE
1. Main rotor hub and yoke -
Condition.
2. Main rotor blade doublers and
skin - Condition.
3. Pitch horn trunnion bearing -
Wear and security.
4. Main rotor pitch links -
Condition and security of
attachment bolts and locking
hardware.
6. Swashplate assembly -
Condition, security of attached
controls, and boot condition.
6. Control linkages to swashplate -
Condition, security of attachment
bolts and locking hardware.
7. Forward fairing and access door
- Secured.
6. Cabin doors and hinge pins -
Condition and security.
9. Windows - Condition and
security.
2-8 Rev. 4
10. Hydraulic reservoir - Check
fluid level.
11. Landing gear - Condition and
ground handling wheel
removed.
12.
Forward and aft crosstube
fairings - Secured, condition
and aligned.
13. Left static port - Condition.
2-15. FUSELAGE - FRONT
1. Exterior surfaces - Condition.
2. Windshield - Condition and
cleanliness.
3.
Battery and vent lines -
Condition and security.
4. HOUR METER circuit breaker -
In.
5.
FUEL BOOST LEFT circuit
breaker - In.
6. Battery access door - Secured.
7. Pitot tube - Cover removed,
clear of obstruction.
6. External power door - Condition
and security.
NOTE
APU should be 500 amperes or
less to reduce risk of starter
damage from overheating.
9. Landing light glass - Condition.
10. Antennas - Condition and
security.
11. Main rotor blade - Condition.
12. External power - Check BAT
switch OFF and APU connected
as desired.