P&M QUIK-GTR Manual, ref. QUIK-GTR Man 1.0.doc
Page 28
4. OPERATING LIMITATIONS
4.1. GENERAL LIMITATIONS
The P&M Aviation Quik-GTR must be operated in compliance with the following limitations:
The aircraft is to be flown only in daytime visual meterological conditions ( VMC).
The minimum instrumentation required to operate the aircraft: ASI, altimeter, tachometer (RPM), oil
temp & oil pressure and CHT.
When flown solo, the aircraft must be flown from the
front seat only
.
The aircraft must be flown such as to maintain positive n
ormal acceleration (positive ‘g’) at all times.
The aircraft must not be flown in negative ‘g’.
Do not pitch nose up or nose down more than 45° from the horizontal.
Do not exceed more than 60° of bank.
ALL aerobatic manoeuvres including whipstalls, wingovers, tailslides, loops, rolls and spins are
prohibited.
GENERAL LIMITATIONS - ALL MODELS
Max. Empty weight (Subject to approved
equipment fit)
583lb (632.5
with parachute
fit)
265kg (287.5
with parachute
fit)
Min. empty weight
484lb
220kg
Max. take off weight
990lb
450kg
Min. take off weight
605lb
275kg
Min. total occupant weight
121lb
55kg
Max. front seat weight
242lb
110kg
Max. number of occupants
2
2
Max. passenger weight
242lb
110kg
Max. useable fuel 65L tank
99lb
45kg
63.6Ltr
Manoeuvring airspeed (Va)
90mph
144kph
78kn
Max. load factor at Va
+4
+4
Vne
120mph
192kph
104kn
Max. load factor @ Vne
+4
+4
Max. wind operating conditions
23mph
37kph
20kn
Cross wind limits
Taxiing
23mph
37kph
20kn
Take off
12mph
20kph
10kn
Landing
12mph
20kph
10kn
It is extremely dangerous to attempt to fly
outside the designated Flight Envelope, or
outside any of the limitations detailed below.
WARNING
!
HIGH WINDS & CROSS WIND LANDINGS
AND TAKE-OFFS: the figures shown above
were demonstrated by experienced factory test
pilots. Lower limits apply for pilots of average
ability. Low hour and student pilots must
adhere to the cross wind limits set out in
Section 8.1.
WARNING
!
Содержание QUIK-GTR
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