ALTITUDE LIMITATION
The maximum flight altitude is 25,000 MSL with a working oxygen
system and 14,000 MSL without oxygen available. This is to ensure
backup oxygen is available in the event of pressurization system
failure.
POWERPLANT OPERATING LIMITATIONS
Operating limitations for the TSIO-550E engine in this aircraft are
listed below. In addition, the data and limits shown are for new
specification engines and do not reflect any degradation due to age or
number and quality of overhauls.
Rated max continuous BHP
350 HP @ 2700
RPM
Recommended Max.cruising BHP
262 HP @ 2500
RPM
Max continuous manifold pressure
38.5” Hg.
Cylinder Head Temperatures - °F
Normal flight operation max temperature
420°F
Maximum allowable
460°F
Turbine Inlet Temperature - °F
Maximum allowable
1750
1850 for
30 sec
Oil Temperatures - °F
Maximum
240
Minimum for take-off
100
Cruise
160-200
Oil Pressure - PSI
Normal operation at 75
o
F – 240
o
F
30-60
Idle, Minimum
10
Max Allowable (cold oil)
100
Fuel Pressure (Unmetered p.s.i.g.)
Idle (700 RPM)
7.0 - 9.0
Takeoff
32 - 34
Fuel Flow (GPH)
Takeoff
41.7 – 43.4
Содержание ES-P
Страница 10: ...Basic Airframe Dimensions ...
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Страница 82: ...CARE AND CLEANING 10 EXTERIOR PAINTED SURFACES 11 ENGINE 11 RECOMMENDED SERVICING 12 ...
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Страница 95: ...SECTION 9 SUPPLEMENTS TABLE OF CONTENTS ALTITUDE REGULATIONS 2 ALTITUDE REACTION 2 ...
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Страница 120: ...WORK PERFORMED ...
Страница 122: ...Idle cut off Static rpm Idle mixture Check engine for oil leaks ...