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Vol. 1 01--30--15
AIRPLANE GENERAL
Flight Compartment REV 3, May 03/05
Flight Crew Operating Manual
CSP C--013--067
1. REINFORCED FLIGHT COMPARTMENT DOOR <1226>
A. General
The reinforced flight compartment door is installed to enhance aircraft security. The
door is used to protect the flight crew from ballistic threat and to prevent unauthorized
access to the flight compartment. The door is made from Nomex core panels
sandwiched in the middle with a bullet proof insert.
The door consists of:
(1) Slide latch
(2) Deadbolt assembly with key lock
(3) Two quick--release hinge pins
(4) Two decompression panels release latches
(5) Cabin viewer
(6) Strap handles
B. Operation
The slide latch is used to latch and unlatch the door
The deadbolt assembly is used securely lock the door. To lock or unlock the door from
inside the flight compartment, the deadbolt knob is manually rotated to engage the
deadbolt pin into the flight compartment bulkhead. A key is required to lock or unlock
the door from the passenger compartment.
The door is hinged to the galley bulkhead. The door opens towards the passenger
compartment and can be held open with a door retainer on the galley wall. The two
quick--release pins are used to remove the door from inside the flight compartment and
the strap handles are used to lift the door out of the way.
The bullet proof viewer has two lenses to increase the magnification for field of view.
The decompression panels are hinged on the door and held closed by the pressure
release latches. When the pressure differential between the passenger compartment
and the flight compartment exceeds a preset limit, the latches release to allow both
panels to open. This is done to equalize the pressure between the two compartment.
At any time during the flight, if one of the required flight crew leaves the flight
compartment, another crew member must replace him/her in the flight compartment to
ensure that the required crew member is not locked out of the flight compartment.
Vol. 1 01--30--16
AIRPLANE GENERAL
Flight Compartment REV 3, May 03/05
Flight Crew Operating Manual
CSP C--013--067
Reinforced Flight Compartment Door
Figure 01---30---15
HINGE ASSEMBLY
COCKPIT DOOR
HINGE ASSEMBLY
UPPER
DECOMPRESSION
PANEL
LOWER
DECOMPRESSION
PANEL
MAIN
DEADBOLT
LATCH
DEADBOLT
ASSEMBLY
VIEWER
(PEEPHOLE
ASSEMBLY)
POCKET
ENCLOSURE
A
B A
Vol. 1 01--30--17
AIRPLANE GENERAL
Flight Compartment REV 3, May 03/05
Flight Crew Operating Manual
CSP C--013--067
C. Evacuation
If the latch has failed or if the door has jammed, the following steps are used to remove
the door in an emergency
WARNING
The lower door hinge pin must be released before the
upper hinge pin. Failure to do so could result in the
door suddenly coming disengaged from the hinges
causing injury to persons.
From inside the flight compartment:
(1) Unlock and lift lower hinge pin.
(2) Unlock and pull down upper hinge pin.
(3) Remove the door by forcibly pushing it out at the hinge side.
(4) Rotate door clockwise and stow against the galley.
From the passenger compartment:
In the event that the flight crew becomes trapped in the flight compartment or becomes
incapacitated, it has been demonstrated that rescue personnel can remove the door
using normally available, non-powered, hand carried, rescue tools (e. g. , crowbar, axe,
etc.).
Vol. 1 01--30--18
AIRPLANE GENERAL
Flight Compartment REV 3, May 03/05
Flight Crew Operating Manual
CSP C--013--067
Reinforced Flight Compartment Door --- Placards
Figure 01---30---16
B
PRESSURE
RELEASE
LATCH
UPPER HINGE
HANDLE
RETRACTABLE
BOLTS
LATCH
DEADBOLT
NAMEPLATE
STRAP
HANDLE
STRAP
HANDLE
LOWER HINGE
HANDLE PRESSURE
RELEASE
LATCH
Vol. 1 04--00--1
AUXILIARY POWER UNIT
Table of Contents REV 3, May 03/05
Flight Crew Operating Manual
CSP C--013--067
CHAPTER 4 ---AUXILIARY POWER UNIT
Page
TABLE OF CONTENTS 04--00
Table of Contents 04--00--1
INTRODUCTION 04--10
Introduction 04--10--1
APU POWER PLANT 04--20
APU Power Plant 04--20--1
Engine 04--20--1
Gearbox 04--20--1
SYSTEMS 04--30
Systems 04--30--1
Lubrication 04--30--1
Fuel 04--30--1
Ignition and Starting 04--30--1
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