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ASG 32 EL Flight Manual

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Flight Manual
Speed
Maximum
Flap Extended
V
FE
speeds
Maximum Winch-
V
W
launching speed
Maximum Aero-
V
T
towing speed
Maximum Sustainer
assisted aerotowing
V
TA
speed
Maximum Landing
Gear Operating
V
LO
speed
Maximum speed with
V
PE
propeller extended
Maximum speed for
extending and re-
V
PO
tracting the propel-
max
ler
Minimum speed for
extending and re-
V
PO
tracting the propel-
min
ler
Issue:
15.09.2017
Revision:
TN 12 30.10.21 PA
IAS
1 – 2 – 3 – 4
270 km/h
146 kts
168 mph
5 – 6
180 km/h
97 kts
111 mph
L
150km/h
81 kts
93 mph
140 km/h,
75 kts
87 mph
180 km/h
97 kts
111 mph
180 km/h
97 kts
111 mph
180 km/h
97 kts
111 mph
180 km/h
97 kts
111 mph
120 km/h
64 kts
74 mph
95 km/h,
51 kts,
59 mph
PA
Flight Manual
Remarks
Do not exceed these speeds
with the flap in position of
the given numbers.
Do not exceed this speed
during winch- or autotow
launching
Do not exceed this speed
during aerotowing.
Do not exceed this speed
during sustainer assisted
aerotowing.
Do not extend or retract the
landing gear above this
speed.
Do not exceed this speed
with the engine extended
Do not extend or retract the
retractable powerplant out-
side of this speed range
Appr.
2.1

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Summary of Contents for ASG 32 EL

  • Page 1 Flight Manual Flight Manual Speed Remarks 1 – 2 – 3 – 4 270 km/h 146 kts 168 mph 5 – 6 Maximum Do not exceed these speeds 180 km/h Flap Extended with the flap in position of 97 kts speeds the given numbers.
  • Page 2 Winch and Autotow launches are approved using the tow-re- lease below the rear seat. The ASG 32 El is not approved for take-off by sole means of its own power. Winch and Autotow launches have to be performed with the en- gine retracted.

  • Page 3: Limitations Placards

    Flight Manual Flight Manual 2.15 Limitations Placards This placard is fixed to the right-hand cockpit sidewall and contains the most important mass (weight) and speed limitations. (The original placard is to be enlarged by 130%) This placard is to be glued below the data placard: This placard is to be glued near the data placard: This placard is to be glued near the data placard: This placard is to be glued near the data placard:...
  • Page 4 Flight Manual Flight Manual Emergency Retraction of the Power-plant The following emergency retraction procedure can be applied, if the ex- tended power-plant should fail and the additional drag is a serious danger for the further flight. A still sound 12V power supply of the power-plant is required for this.
  • Page 5 Flight Manual Flight Manual Ground run WARNING Perform ground run with rigged aircraft only! CAUTION The freestream during flight is necessary for the proper air cooling of the propulsion like it is the case during normal operation as sus- tainer. The motor overheats after about 10 minutes ground run with a power setting of 100% and 20°C (68°F) outside air temperature.
  • Page 7 Flight Manual Flight Manual Sustainer assisted aerotow The electric propulsion can be used to assist the aerotow, e.g. in case of short or wet airfields. WARNING The sustainer assisted aerotow is only permissible, if the aerotow would be also possible without the assistance of the gliders sus- tainer.
  • Page 8 Flight Manual Flight Manual CHECKLIST: Sustainer assisted aerotow Power-plant main switch: ON (power-plant instrument on) Power lever: EXTEND (until the noticeable stop position) Observe correct extension process in the mirror, blue message „PRESS Starter Button“ appears, propeller holds in vertical position Pre take-off check Trim: NEUTRAL...
  • Page 9 Flight Manual Flight Manual CAUTION In case of a motor failure at the sailplane, a decrease in climb rate of the tow up to 1.5 m/s (300 ft/min) has to be taken into account. If necessary, the emergency retraction of the power-plant as per page 3.8 could be applied to improve this situation.
  • Page 10 Maintenance Manual Maintenance Manual This placard must be en- larged by 141%. This placard is af- fixed below the Data and Loading placard (21). Issue: 01.04.2017 Revision: TN 12 30.10.21 PA...