Section 5 Flashcards
CAUTION ang. Icing
Flying into known icing conditions is not approved.
WARNING ang. Inverted flight
Inverted flight is limited to 10 seconds due to engine oil system design.
Maximum crosswind component for take-off and landing is?
Maximum crosswind component for take-off and landing on a dry runway is 30 knots.
Conditions resulting in unusable fuel is?
Unuseable fuel
o Flaps up, prolonged power-on dive , 154 knots IAS
with less than 75% max. continuos power.
o Flaps down, prolonged low power dive, 100 knots
IAS with less than 60% max. continuos power.
RPM operating range
2200 - 2700 RPM normal operating range
2700 RPM maximum RPM
Oil pressure range
60 - 85 PSI normal operating range
25 - 60 and 85 - 100 PSI caution range
25 PSI minimum for engine idling
100 PSI maximum for engine start and warm-up
Oil temp
50 - 120 C normal operating range
120 C maximum
Cylinder head temp.
105 - 120 C normal operating range
225 - 245 C caution range
245 C maximum
T17 maximum landing weight?
1140 kg
Normal category weight, maneuvers and G’s?
NORMAL CATEGORY
The aircraft is in normal category when the AUW is less than 1200 kg and when the CG is not behind 30% of MAC and within approved CG-envelope.
In this category the aircraft is limited to the following maneuvers:
1. Any maneuver used in normal flight
2. Stalls (except whip stall, hammer stall)
3. Lazy eights, chandelles, and steep turns with angle of bank not exceeding 60°.
The limiting load factors “G” are 4.4 positive and 2.2. negative.
Utility category I weight, maneuvers and G’s?
UTILITY CATEGORY I
The aircraft is in utility category I when the AUW is less than 1125 kg. and when the CG is not behind 27.5% MAC and within approved CG-envelope.
Maneuvers:
- Any maneuver used in normal category
- Erect stall
- Spins
- Lazy eights, chandelles and steep turns with angle of bank exceeding 60°.
The limiting load factors “G” are 4.8 positive and 2.4 negative.
Utility category II weight, maneuvers and G’s?
UTILITY CATEGORY II
In case of the AUW being less than 1000 kg and the CG not behind 27.5% MAC and within approved CG-envelope utility category II in addition permits the following maneuvers:
- Any maneuvers used in utility category I. - Rolling
- Looping
- Half roll (Split-S)
- Top roll (Immelmann)
The limiting load factors “G” are 5.4 positive and 2.7 negative.
Aerobatic category weight, maneuvers and G’s?
AEROBATIC CATEGORY
The aircraft is in this category when the AUW is less than 900 kg. and the CG is not behind 27.5% MAC and within approved CG-envelope.
In the aerobatic category, the aircraft is limited to the same maneuvers as in utility categories I and II. The limiting load factors “G” are 6.0 positive and 3.0 negative.
The maximum permissible load in the rear compartment?
The maximum permissible load in the rear compartment is either one person + 50 kg or a total of 100 kg luggage. Provided that the load is placed on a special cargo floorboard, the maximum load can be raised to 150 kg.
Vne (Never exceed)
196 knots (Do not exceed this speed in any operation.)
