SECTION 2.
ASSEMBLING & DISASSEMBLING,
SYSTEMS DESCRIPTION
TECHNICAL SERVICE MANUAL
SZD-54-2
„Perkoz”
page 2.30
Allstar PZL Glider Sp. z o.o.
Doc No. 542.4.02
Issue II
April 2014
Revision
corrected
2.15. Front instrument panel
Flight instrument installation diagram on front instrument panel is presented
in Fig. 2
‒16. (example configuration with typical equipment).
Legend to Fig. 2
‒16.
1 - Instrument panel
2 - Instrument panel casing
3 - Static pressure vent
4 - Air intake and total air pressure vent
5 - T-pipe
6 - Static air pressure conduit
7 - Total air pressure conduit
8 - Electrical turn indicator
9 - Airspeed indicator
10 - Variometer
11 - Accelerometer
12 - Altimeter
13 - Compass
14 - Variometer compensator (standard option)
15 -
Variometer’s compensating vessel
16 - Dehydrator
17 - Instrument panel suspension
18 - Turn indicator switch
19 - Total energy probe
„K-1” (alternative option) or blind slot
20 - Total energy probe
„K-1” conduit
21 - Flexible ventilation conduit
22 - Inlet throat of ventilation installation
23 - Throttle lever of ventilation conduit
24 - Vent pull rod
25 - Vent pull rod handle
26 - Pipe cross
27 - Nut
28 - SP3 stall warning device switch
29 - Bank indicator
30 - Fuses
31 - Transceiver
32 - Reducing connector