Prefect limitations Aug 21 Flashcards
VMO (Max Operating Speed)
238
MMO (Max operating Mach Number
0.45MN
V LOE (Max speed landing gear oppression extend)
182
V LE (Max speed landing gear extend)
182
VO (Aerobatic) (Max manoeuvre speed up to 1440kg AUM)
164
VO (Utility) (Max manoeuvre speed 1440 to 1515 kg AUM)
143
VFE - T/O (Max speed flaps extended at take off position)
151
V LOR (Max speed landing gear operation retract)
137
VFE (Max speed flaps extended beyond take off position)
114
Power lever must not be retarded below __ during flight
Flight Idle
Max airspeed to apply reverse thrust during landing
80
Min airspeed for use of Reverse thrust during landing
40
Take off and landing cross wind component limitations
1) Take off and landing ___
2) maximum crosswind for break release take off __
3) flaps should be up in crosswinds grater than __
25
20
20
Recommended cruise airspeed during severe turbulence?
140-180
Max opening speed of the canopy in flight
110
Max speed with canopy open in flight
120
Max take off AUM
1515
Max landing AUM
1515
Max aerobatics AUM
1440
Max zero fuel AUM
1370
Min flying AUM
1170
Max baggage compartment Mass
50kg
Pitch attitude limitations, when fuel tank selector in emergency transfer
Max nose up ___
Max nose down ___
15
10
Aerobatic (<1440kg) max G limits
-4 to +6
Utility (<1515) G limits
-1.7 to +4.4
Flaps down max positive G
Flaps down min G
+3.8
0
Max OAT on the ground
+38c
Max OAT
ISA + 23c
Min OAT
-54c
Reduced power - OAT operating limitation minimum
ISA - 15c
OAT <4c in visible rain or moisture
P/S Heat - On
Comp intake - Both
What must fuel contain when OAT is below 4c
FSII
Min battery voltage for engine start
24v
Max transient TRQ (10 Seconds)
115%
Max T/O Power TRQ (5 min at T/O) cumulative per sortie
111%
Max continuous TRQ
92%
Max engine start TOT
927c (10 seconds over 810c)
Max transient TOT
899c (6 seconds over 810c)
Max T/O power TOT
810 (5 min at T/O, cumulative per sortie)
Max continuous TOT
752c
Taxi and landing might limitation
OAT > +38c =
Max 40 minutes (min 30 mins cool time)
Max transient limit (Propeller RPM)
2233 N2 (15 seconds max above 2130 N2)
Max continuous speed of propeller RPM
2132
Max static ground ops propeller RPM
1850 N2
N2 must not be allowed to stabilise within the ___
N2 speed avoidance range
The N2 speed avoidance range is
Stabilised for longer than 1 second between 1523 and 1786 RPM with more than 20% TRQ
Speed avoidance range applied in both
Forward and reverse thrust
Accumulated time spent in the N2 speed avoidance range must be recorded in __
The engine logbook
Gas generator RPM
Max transient N1
Max continuous N1
106% N1 (max 15 sec >105%)
105% N1
Oil pressure Max transient (cold weather / engine start)
150 PSI
Oil Pressure max
130 PSI
Oil pressure min at an N1 greater than 94%
120
105 (Beta)
Oil pressure min at N1 85% to 94%
90 PSI 75 PSI (Beta)
Oil pressure N1 <85%
50 PSI 35 PSI (Beta)
Oil temperature max limit at TRQ <40%
107c
Oil temperature Max transient TRQ >40% (5min)
107c
Oil temperature at max continuous TRQ >40%
82c
Min oil temperature
0c
Min oil temperature before starting
-40c
Total Fuel Capacity
282.7kg
LH collector tank capacity
16.8kg
Unusable fuel left wing
6.3kg
Unusable fuel right wing
1.4kg
Usable fuel
275kg
Max tank asymmetry
45.3kg
Max fuel in each wing for aerobatics
115kg
Max fuel pressure
25 PSI
Min fuel pressure
12 PSI
