TM 1-1520-240-10
2-9-4
of travel. At PARK, the wipers stop and reposition against the
inside windshield frame.
2-9-10. Map and Data Case.
The map and data case is in the passageway. It holds
manuals, maps and other data.
2-9-11. Cockpit Rearview Mirror.
A rearview mirror is installed on the right center wind-
shield support to enable the pilot to observe the cargo
compartment.
2-9-12. Spare Lamp Stowage Box.
The spare lamp stowage box is in the cockpit on top of
the No. 1 PDP. Spare lamps are provided for the instru-
ment post lights, instrument light shields, dome lights,
cabin and ramp lights, and nacelle work lights.
2-9-13. Cockpit Utility Receptacles.
Two 28-volt DC utility receptacles are in the cockpit, one
on No. 1 PDP and one on No. 2 PDP. Each receptacle is
labeled UTIL RCPT 28V DC. Power to operate the copilot
receptacle is supplied by the No. 1 DC bus through the
UTILITY COPLT circuit breaker on the No. 1 PDP. Power
to operate the pilot receptacle is supplied by the No. 2 DC
bus through the UTILITY RCPT PILOT circuit breaker on
the No. 2 PDP.
2-9-14. AC Cabin Utility Receptacles.
A 115 volt, single-phased 400 Hz AC utility receptacle
and a 200 volt 3-phase 400 Hz AC utility receptacle are
on each side of the cabin at sta 320. The receptacles are
accessible after the acoustical access cover and the re-
ceptacle dust cap are removed. Power to operate the 115
volt receptacles is supplied by the No. 1 and No. 2 AC
buses through the LH and RH UTIL RCPT circuit break-
ers on the No. 1 and No. 2 PDP. Power to operate the 200
volt receptacles is supplied by the No. 1 and No. 2 AC
busses through the LH and RH CABIN AC RCPT
3-phase circuit breakers on the No. 1 and No. 2 PDP.
2-9-15. DC Cabin Utility Receptacles.
Four 28-volt DC utility receptacles with three outlets are
on the sidewalls of the cargo compartment. Power to
operate the left cabin utility receptacles is supplied by the
No. 1 DC bus through the UTILITY LH FWD and LH AFT
circuit breakers on the No. 1 PDP. Power to operate the
right cabin utility receptacles is supplied by the No. 2 DC
bus through the UTILITY RCPT RH AFT and RH FWD
circuit breakers on the No. 2 PDP.
2-9-16. Ash Trays.
Three ash trays may be installed in the cockpit, one for
each pilot and one for the troop commander.
2-9-17. Compass Correction Card Holder.
The magnetic compass correction card holder is at-
tached to the left side of the magnetic compass. The card
contains the necessary deviation values which are ap-
plied to the indicated reading.
2-9-18. Pilot Assist Straps.
Two assist straps are attached to the center window
frame of the cockpit structure to provide the pilots with a
hand hold while getting into the seats. The assist straps
can be positioned flat against the structure after use.
