ORLI
Č
AN M-8 EAGLE
PILOT'S OPERATING
REVISION NO. 05
DATE OF ISSUE: MAY 02,
LIMITATIONS
PAGE
OF
32
42
6.11. APPROVED MANEUVERS
M-8 Eagle airplane is approved to perform the following maneuvers:
•
steep turns up to bank angle of 60°
•
climbing and diving up to 30° from horizontal plane
•
normal flight maneuvers
6.12. MANEUVERING LOAD FACTORS
Flaps up:
Maximum positive load factor in the center of gravity: +4.0
g Maximum negative load factor in the center of gravity:
-2.0 g
Flaps down:
Maximum positive load factor in the center of gravity: +2.0
g Maximum negative load factor in the center of gravity:
-0.0 g
LOAD FACTOR
(N)
1.0
1.15
1.4
2.0
ATTITUDE
CONFIGURATION
0°
30°
45°
60°
Flaps
not
extend
ed
Km/
h
(Kts
)
80
(43)
83
(45)
95
(51)
113
(61)
Flaps
30°
extend
ed
Km/
h
(Kts
)
70
(38)
72
(39)
83
(45)
99
(53)
ATTENTION!
THE DATA FOR BANK ANGLES 45° AND 60° ARE
CALCULATED VALUES, THEY HAVE NOT BEEN VERIFIED
BY A TEST FLIGHT.
Summary of Contents for M-8 EAGLE 2022
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