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Pilot's Handling Notes for the Stinson 108-3 Voyager
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This Franklin 6A4-165-B3 engine has manual mixture controls, manually applied carb heat controls, no supercharger and no airscrew controls. Rated and sea level take off output is 150hp. However at 2800 RPM 165 hp are available for emergency (go around) use at sea level.

CAUTION - MINIMUM altitude for full throttle cruising is 5000 feet.

CAUTION - Restrain RPM < 2800 AT ALL TIMES

WARNING - Structural failure may occur > 126 MIAS

WARNING - Structural failure will occur > 158 MIAS

WARNING - This aircraft has very fragile flaps, Structural failure may occur > 88 MIAS with any flap deployed.

CAUTION - Manually applied pitot heat available, but no structural or airscrew de-icing available.

WARNING - THIS AIRCRAFT IS *NOT* CERTIFICATED FOR USE IN KNOWN ICING.

This aircraft is loaded by default with the maximum fuel load of 300 pounds and a payload of 780 pounds. 24 pounds of fuel are unusable by design.

Design cruise altitude is 5000 QNH.

This aircraft has rudder trim to counter torque and p-factor. FS9 users with no rudder pedals are however advised to minimise all relevant factors in the realism screen before flight.

FS9 users with no real world experience of leaning aero engines are advised to ignore the next instruction and set automixture = ON in the realism screen before flight.

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Take Off:

AUTOMIXTURE = OFF (in FS9 realism options)

FLAP = STAGE 1

CARB HEAT = COLD

TRIM = 13% POSITIVE

LINE UP

BRAKES = ON

THROTTLE = FULL

RPM > 2200

BRAKES = OFF

YOKE = FULL FORWARD to raise tail

65 MIAS = ROTATE

ACCELERATE = 80 MIAS

CLEAR OF OBSTACLES

FLAP = UP

ACCELERATE = 95 MIAS

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Climb power:

FULL THROTTLE subject to

MINIMUM 500 VSI

ELSE 2600 RPM cruise climb

95 MIAS

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Max Cruise (*FL50 and above*):

FULL THROTTLE subject to

MAX 125 MIAS

MAX 2800 RPM

Plan 65 PPH

Note: Yields 110 KTAS at FL50

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Econ Cruise: (All levels)

2500 RPM

Below FL50 plan 55 PPH

Above FL50 plan 50 PPH

Note: Yields 94 KTAS at most levels

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Descent:

RPM ideally 2500

MAX 126 MIAS

IF RPM < 2500 & OAT < 5C CARB HEAT = HOT

Plan 55 PPH

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Approach Circuit and Landing:

2500 RPM

OAT < 5C CARB HEAT = HOT


Late Downwind:

RPM < 2500

REDUCE = 85 MIAS


Base Leg:

85 MIAS


Short final:

85 MIAS

In time to achieve Vref

FLAP = STAGE 1

FLAP = STAGE 2

CARB HEAT = COLD


Vref = Cross airfield boundary @ 70 MIAS

WHEN TAIL SETTLES - YOKE FULL AFT

FLAP = UP

BRAKES - as required

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