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4. NORMAL PROCEDURES
There is no change in to the normal procedures.
5. PERFORMANCE
The range with 30 minute reserve fuel is reduced by approximately 19% with the 20.5 US gallon fuel tank installed in place of the 24.5 US gallon tank.
6. WEIGHT AND BALANCE
Lever arm of fuel in the 20.5 US gallon tank: 30.08 in (0.764 m)
7. DESCRIPTION OF THE AIRPLANE AND ITS SYSTEMS
7.10. Fuel System
A 20.5 US Gal total / 20.5 US Gal usable fuel tank replaces the standard 24.5 US Gal total /
24.0 US Gal usable fuel tank. There are no other changes to the fuel system.
7.10.5. Fuel Dipstick
A fuel dipstick P/N 22-2550-18-00, is supplied with all aircraft with the 20 US gallon fuel tank installed. This dipstick permits direct measurement of the fuel level during the pre-flight check.
8. HANDLING, PREVENTATIVE AND CORRECTIVE MAINTENANCE
There is no change in handling, preventative or corrective maintenance with the 20 US gallon fuel tank installed.
INTENTIONALLY LEFT BLANK
CHAPTER 9
SUPPLEMENT 10
Reversed Instrument Panel
1.
GENERAL S10-2
2.
OPERATING LIMITATIONS S10-2
3.
EMERGENCY PROCEDURES S10-2
4.
NORMAL PROCEDURES S10-2
5.
PERFORMANCE S10-2
6.
WEIGHT AND BALANCE S10-2
7.
DESCRIPTION OF THE AIRPLANE AND ITS SYSTEMS S10-3
8.
HANDLING, PREVENTATIVE AND CORRECTIVE MAINTENANCE S10-3
1. GENERAL
This supplement addresses the optional installation of the navigation and powerplant instruments in a reversed configuration. The navigational instruments are located on the right hand side of the instrument panel. The powerplant instruments are located on the left hand side of the panel. Only portions of the flight manual affected by this installation are included in this supplement.
2. OPERATING LIMITATIONS
There is no change in the operating limitations.
3. EMERGENCY PROCEDURES
There is no change in to the emergency procedures.
4. NORMAL PROCEDURES
There is no change in to the normal procedures.
5. PERFORMANCE
There is no change in the performance of the aircraft.
6. WEIGHT AND BALANCE
The weight and balance of the aircraft is not affected.
7. DESCRIPTION OF THE AIRPLANE AND ITS SYSTEMS
7.4.
Instrument Panel
8.
HANDLING, PREVENTATIVE AND CORRECTIVE MAINTENANCE
Description Description Description Description
1 -- 13 Vertical Speed Ind. 25 -- 37 Fuel Quantity Ind.
2 Clock/OAT 14 CDI 26 -- 38 EGT Indicator
3 Magnetic Compass 15 Air Vent 27 -- 39 CHT Indicator
4 Trim Position Display 16 Switch Panel 28 -- 40 Circuit Breakers
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