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SECTION 2
Aircraft Operating Instructions Edge XT 912
LIMITATIONS
January 2014
Issue 2.4
Page 26
2.7 Placards
The placards on the aircraft are designed to provide information regarding general aircraft limitations and
other details for the safe operation of the aircraft. Listed on the following pages are details of the placards
fitted to the aircraft.
2.7.1 Flight Limitations Placard
Location
The flight limitation placards are located on the dash either side of the
mast brace. Engine limitations placard option of metric 107599 or
imperial 107600
Series
Edge XT Series
Table 9 Section 2. Flight Limitations Placards
62mm
7
2
m
m
PART No.107600
CONTINUOUS
CYLINDER HEAD TEMP
USEABLE FUEL
FUEL TANK CAPACITY
MAX TAKEOFF WEIGHT
WEIGHT OF
OCCUPANTS
ENGINE LIMITATIONS
ROTAX 912 UL
LOADING LIMITATIONS
-
SEE AIRCRAFT OPERATING
INSTRUCTIONS SECT 6.3.4 FOR FUEL LOAD LIMITATIONS.
FLY SOLO FROM FRONT SEAT ONLY
EMPTY WEIGHT
5 MINUTES MAX
ENGINE
RPM
MAX
EGT
5800 rpm
5500 rpm
300 Deg F
17.7 USGal
18.5 USGal
120 Deg F
285 Deg F
1560 Deg F
1620 Deg F
102 psi
12 psi
OIL PRESSURE
MIN
MIN
MAX
MAX
OIL TEMPERATURE
440lbs
121lbs
992lbs
62mm
7
2
m
m
PART No.107599
CONTINUOUS
CYLINDER HEAD TEMP
USEABLE FUEL
FUEL TANK CAPACITY
MAX TAKEOFF WEIGHT
WEIGHT OF
OCCUPANTS
ENGINE LIMITATIONS
ROTAX 912 UL
LOADING LIMITATIONS
- SEE AIRCRAFT OPERATING
INSTRUCTIONS SECT 6.3.3 FOR FUEL LOAD LIMITATIONS.
FLY SOLO FROM FRONT SEAT ONLY
EMPTY WEIGHT
5 MINUTES MAX
ENGINE
RPM
MAX
EGT
5800 rpm
5500 rpm
150 Deg C
67 Litres
70 Litres
50 Deg C
140 Deg C
850 Deg C
880 Deg C
7 bar
0.8 bar
OIL PRESSURE
MIN
MIN
MAX
MAX
OIL TEMPERATURE
200kg
55kg
450kg
62mm
7
2
m
m
PART No.107596
FLIGHT LIMITATIONS
WARNINGS
DO NOT PITCH NOSE DOWN OR NOSE UP
MORE THAN 45 DEGREES FROM HORIZONTAL.
DO NOT EXCEED 60 DEGREES OF BANK.
NO NEGATIVE G.
NO AEROBATIC MANOEUVRES.
NO INTENTIONAL SPINS.
NO WHIPSTALLS.
NO STALLED SPIRAL DESCENTS.
APPROVED FOR DAY VISUAL METEOROLOGICAL
CONDITIONS ONLY.
NO SMOKING.
ALWAYS PREFLIGHT AIRCRAFT.
ENSURE MAST LOCKED IN POSITION BEFORE
STARTING ENGINE.
OPERATE IN ACCORDANCE WITH LIMITATIONS
AND PROCEDURES DETAILED IN THE
AIRCRAFT OPERATING INSTRUCTIONS.