Equipment & Furnishings¶
Equipment & Furnishings: 1 COCKPIT PLAN¶
Equipment & Furnishings: 1.1 General¶
(Applies: 1096;1126) For comfort, convenience, and safety the cockpit could have various furnishings.
4 WINDSHIELD SUN VISOR GRIP HANDLE CHART HOLDER CUP HOLDER ASHTRAY CHECK LIST STOWAGE CAPTAIN BRIEFCASE STOWAGE OBSERVER BRIEFCASE STOWAGE WINDSHIELD SUN VISOR GRIP HANDLE CHART HOLDER CUP HOLDER ASHTRAY CHECK LIST STOWAGE F/O BRIEFCASE STOWAGE CREW MANUALS AND DOCUMENTS STOWAGE WINDSHIELD SUN VISOR OBSERVER FOLDING FOOTREST CAPTAIN STATION FIRST OFFICIER STATION
(Applies: 1054;1124;1142-1283) For comfort, convenience, and safety the cockpit could have various furnishings.
C WINDSHIELD SUN VISOR GRIP HANDLE CHART HOLDER CUP HOLDER ASHTRAY CHECK LIST STOWAGE CAPTAIN BRIEFCASE STOWAGE OBSERVER BRIEFCASE STOWAGE WINDSHIELD SUN VISOR GRIP HANDLE CHART HOLDER CUP HOLDER ASHTRAY CHECK LIST STOWAGE F/O BRIEFCASE STOWAGE CREW MANUALS AND DOCUMENTS STOWAGE WINDSHIELD SUN VISOR OBSERVER FOLDING FOOTREST CAPTAIN STATION FIRST OFFICIER STATION ELECTRONIC FLIGHT BAG SUPPORT ELECTRONIC FLIGHT BAG SUPPORT
Equipment & Furnishings: 1.2 Seats¶
1 - CENTER PEDESTAL 2 - F/O SEAT 3 - RH SIDE CONSOLE 4 - OBSERVER SEAT 5 - LH SIDE CONSOLE 6 - CAPTAIN SEAT ELECTRONIC RACK ELECTRIC RACK A B C 1 2 3 4 5 6
- Fig. 1 : Cockpit Seats - CAPT and F/O seats are each mounted on a base secured to the floor on each side of the center pedestal. The flight crew can adjust them along the three axis for individual comfort. The flight crew can also adjust folding armrests. The observer seat is behind the pedestal and between electronic and electric racks. When not in use, the observer seat can be stowed:
- Facing the electronic rack (position A).
- In the cargo compartment, allowing the observer to move in the cabin (position B) or transversely along the electronic rack (position C). Safety pins enable the observer seat to be removed backward in order to help emergency evacuation in case of jamming. The three seats include full harness with an inertial reel and locking handle for the shoulder harness. Note Carefully and slowly handle shoulder harnesses. When unfastened too quickly they may damage panels behind the seats.
Equipment & Furnishings: 1.3 Seat Position Sight Gauge¶
- Fig. 1 : Cockpit Shadow -
- Fig. 2 : Seats Position Sight Gauge - Seat position sight gauge must be used for proper setting of the vertical and longitudinal position of the seat. It permits to the flight crew a correct view of instrument panels as well as runway environment, especially when flying low visibility instrument approaches. This indicator includes three colored balls. Center ball is red and is horizontally shifted compared with the other two white balls. For proper seat position, the red ball obscures the respective white ball.
Equipment & Furnishings: 1.4 Captain-First Officer Seats¶
(Applies: 1054-1142;1237-1283)
RECLINE CONTROL HORIZONTAL ADJUSTMENT CONTROL VERTICAL ADJUSTMENT CONTROL INERTIAL REEL LOCKING CONTROL ARMREST ADJUSTMENT CONTROL LUMBAR IN/OUT CONTROL LUMBAR UP/DOWN THIGH SUPPORT CONTROL CONTROL - Fig. 1 : Captain-First Officer Seats -
(Applies: 1160)
2 RECLINE CONTROL HORIZONTAL ADJUSTMENT CONTROL VERTICAL ADJUSTMENT CONTROL INERTIAL REEL LOCKING CONTROL ARMREST ADJUSTMENT CONTROL LUMBAR IN/OUT CONTROL LUMBAR UP/DOWN THIGH SUPPORT CONTROL CONTROL NEW PLACARD - Fig. 1 : Captain-First Officer Seats - A placard at level of the horizontal control handle is added. This new placard has been developed in order to confirm the correct locking of the seats (Pilot and Copilot) by quick visual check. Seat correctly locked
Seat incorrectly locked
3
Equipment & Furnishings: 1.5 Observer Seat¶
DOUBLE HINGE HANDLES BUNGEE BUNGEE SEAT LOCKING CONTROL LIFE VEST STOWAGE
- Fig. 1 : Observer Seat -
Equipment & Furnishings: 1.6 Cockpit Philosophy¶
The pushbuttons displays status and failure indications. Dark cockpit concept applies: lights are off during normal continuous operation. The light comes on to indicate a failure or an abnormal condition. The failure alert appears on the pushbutton that must be operated for corrective action. The following pushbuttons or switchs are circled in amber to help the flight crew to find them in case of smoke (fluorescent painting): - BTC - DC SVCE/UTLY BUS - ACW GEN 1 - ACW GEN 2 - EXHAUST MODE - OVBD VALVE selector - RECIRC FAN 1 - RECIRC FAN 2 - FLOW PB POSITION BASIC FUNCTION IN (PUSHED) ON, AUTO, NORM OUT (RELEASED) OFF, MAN, ALTN, SHUT COLOR INDICATION No light except flow bars Normal basic operation BLUE/CYAN Selection of temporarily required systems GREEN Proper functioning of the system WHITE System selected off AMBER Caution indication RED Warning indication
Equipment & Furnishings: 2 COCKPIT DOOR SECURITY SYSTEM¶
Equipment & Furnishings: 2.1 DESCRIPTION¶
Equipment & Furnishings: 2.1.1 Cockpit Door Description¶
The door has an electromagnetic locking system controlled by the flight crew. In normal conditions, after closing the door, it remains locked. In case of a loss of electrical power, the manual bolt can lock the door.
The flight crew must unlock the locking system in order to open the door. After an entry request reception, the flight crew can authorize entry by unlocking the door. Then it remains closed until it is pulled open. When the flight crew does not respond to a request for entry, then the cabin crew could press the EMER pb in order to unlock the door. The EMER pb is on the Door Call panel installed on cargo compartment side. The door is bulletproof, intrusion resistant, and fully compliant with the rapid decompression requirements. The door provides protection against fire, heat release and smoke in the cabin. If the door jams, the flight crew can remove the right door panel. In this case, the flight crew uses the quick release hinges which are only accessible from the cockpit.
Equipment & Furnishings: 2.1.2 Cockpit Door Locking System Description¶
The Cockpit Door Locking System (CDLS) enables the crew to electrically lock and unlock the cockpit door. The system mainly includes: - A Door Call panel on the cargo compartment side - A Cockpit Door control panel with a toggle switch and a buzzer - A CDLS sw behind the first officer seat - A Cockpit Door Control Unit (CDCU) in the forward avionics bay. The Door Call panel enables the cabin crew to request access to the cockpit. There are two different access request modes: - Routine - Emergency. The toggle switch enables the flight crew to lock or unlock the cockpit door. Thus the flight crew can permit or not access to the cockpit. The buzzer sounds in the cockpit for a minimum of 2 s (duration of pushbutton activation + 2 s) in order to indicate a routine access request. It sounds continuously in the case of an emergency access procedure. The CDLS sw enables the crew to switch ON or OFF the system at the beginning or at the end of the flight. Thus it helps maintenance tasks and ground operations. The CDCU is the system controller responsible for: - Locking and unlocking the electromagnetic locks, on flight crew action - Alert annunciation to indicate failure of the electromagnetic locks - Activation of the access request buzzer - Turning on the Door Call panel light.
Equipment & Furnishings: 2.1.3 Video Cabin Surveillance¶
(Applies: 1096-1283) The Video Surveillance System includes: - A monitor at the right of the First Officer The monitor has: o A knob for On/Off selection and tune brightness. The knob label is OFF DIM o A pushbutton for camera selection. The pushbutton label is CAM SEL. - Camera 1 : Black and white video camera at the left of the cockpit door. It displays the person that requests access to the cockpit - Camera 2 : Black and white video camera on the cargo ceiling. It displays the back of the person that requests access to the cockpit - Camera 3 : Color video camera on the cargo/cabin door. It displays the cabin. 1 2 3
CAMSEL PUSHBUTTON ON/OFF KNOB
Equipment & Furnishings: 2.2 CONTROLS¶
Equipment & Furnishings: 2.2.1 Door Call Panel¶
The Door Call panel enables the cabin crew to request cockpit access to the flight crew.
OPEN DENIED CALL EMER OPEN DENIED CALL EMER OPEN DENIED CALL EMER OPEN DENIED CALL EMER 1 3 2 4 1 OPEN OPEN Green light comes on when the flight crew unlock the door. It also comes on when the door automatically unlocks (during 10 s) following an emergency access request (no flight action during 30 s after the emergency request). Then the cabin crew can open the door panel. OPEN Green light flashes when the cabin crew requests an emergency access. The buzzer sounds continuously until the flight crew opens the door, or denies the access.
2 DENIED DENIED light comes on when the flight crew does not authorize access. The door remains locked. If no flight crew action occurs, the light remains turned on for 3 min. During this time the Door Call panel is inhibited. 3 CALL CALL pb-sw sounds the buzzer in the cockpit for at least 2 s. 4 EMER EMER pb-sw enables the cabin crew to initiate an emergency request access procedure when the flight crew does not respond. The buzzer will sound continuously in the cockpit and the OPEN green light on the Door Call panel will flash. A turning plate protects it in order to prevent inadvertent activation.
Equipment & Furnishings: 2.2.2 Cockpit Door Control Panel¶
A toggle sw, on the center pedestal, controls the locking system of the door.
OPEN CLOSE DENY 811 VU COCKPIT DOOR 3 2 1 FAULT OPEN
1 Toggle Switch OPEN position: Enables the cabin crew to open the cockpit door. The flight crew must pull and maintain the switch in the open position until the cabin crew opens the right door panel. To open the left door panel, move the handle on the cockpit side and pull the left panel aft. CLOSE position: Locks the door. Emergency access is available for the cabin crew. DENY position: Locks the door and inhibits for 3 min the Emergency access, buzzer, and Door Call panel. Note - If the flight crew does not use the DENY position for 3 min, then the cabin crew is able to request routine or emergency access - The OPEN position overrides and resets any previous selection - In case of an electrical supply failure, the cockpit door automatically unlocks. 2 Fault/Open Indication OPEN light ON: The door is not closed, or not locked. OPEN light flashes: The cabin crew starts an emergency access procedure. If there is no reaction from the flight crew, the door will unlock after 30 s. FAULT: Indicates a system failure. 3 Buzzer Buzzer sounds: For 2 s after the cabin crew requests an access through the CALL pb on the Door Call panel or Continuously when the cabin crew starts an emergency access procedure.
Equipment & Furnishings: 2.2.3 Cockpit Door Locking System ON-OFF Control¶
The CKPT DOOR LKG SYS ON/OFF sw is behind the First Officer seat. CKPT DOOR LKG SYS ON OFF
ON/OFF Control Switch ON: The cockpit door locking system is operative OFF: The cockpit door locking system is inoperative and unlocks the door. The cabin crew can pull the door right panel in order to open it. To open the door left panel, it is necessary to move the handle on the cockpit side and pull the left panel. If the aircraft power is available, the FAULT light on the Cockpit Door Control panel comes on.
Equipment & Furnishings: 2.3 ELECTRICAL SUPPLY¶
Equipment & Furnishings: 2.3.01 Electrical Supply¶
(Applies: 1054) EQUIPMENT DC BUS SUPPLY (C/B) AC BUS SUPPLY (C/B) Cockpit Door Locking System (On center pedestal Cockpit Door panel) DC BUS 2 (on lateral panel C/B DOORS/CDCU & LATCHES SUPPLY) NIL Cockpit Door Fault Light (On center pedestal Cockpit Door panel) DC ESS BUS (on lateral panel C/B DOORS/CDCU FAULT) NIL Door Call Panel (In cargo compartment side) DC ESS BUS (on lateral panel C/B DOORS/CDCU FAULT) NIL
(Applies: 1096-1283) EQUIPMENT DC BUS SUPPLY (C/B) AC BUS SUPPLY (C/B) Cockpit Door Locking System (On center pedestal Cockpit Door panel) DC BUS 2 (on lateral panel C/B DOORS/CDCU & LATCHES SUPPLY) NIL Cockpit Door Fault Light (On center pedestal Cockpit Door panel) DC ESS BUS (on lateral panel C/B DOORS/CDCU FAULT) NIL VIDEO CABIN SURVEILLANCE: Monitor and Camera 1/ 2/3 DC BUS 2 (on lateral panel C/B DOORS/COMPT LT & SERVICING/ VIDEO DOOR) NIL Door Call Panel (In cargo compartment side) DC ESS BUS (on lateral panel C/B DOORS/CDCU FAULT) NIL
Equipment & Furnishings: 1 GENERAL¶
Equipment & Furnishings: 1.1 Introduction¶
The aircraft has fire fighting, oxygen, and first aid equipment. They are put all over the cabin and easily available for use in case of emergency. The emergency lighting system provides aircraft lighting when all other electrical power sources are no longer available.
Equipment & Furnishings: 1.2 Cockpit¶
Each crewmember station has: - Life vest - Smoke goggles - Quick donning oxygen mask supplied with gaseous oxygen from one rechargeable bottle - Flashlights. A portable fire extinguisher and a crash axe are at the bottom on the electrical rack. Depending on versions, a Protective Breathing Equipment (PBE) is behind the captain seat and is available for crewmember use. One plug type hatch in the cockpit ceiling is provided as an emergency exit for the cockpit crew. One escape rope is in a compartment on top of the electric rack near the exit. Steps are provided for hatch access in the corridor on right side. Protective gloves are behind the captain seat.
Equipment & Furnishings: 1.3 Cabin¶
The emergency equipment is put all over the cabin and stowed adjacent to the two cabin crew stations. It contains: - Portable fire extinguishers - Protective Breathing Equipments (PBE) - First aid kits - Crash axe (as required by regulations) - Life vests (stowed under each passenger seat and at the cabin crew stations) - Oxygen supply for passengers - Portable oxygen bottle for cabin crew - Flashlights - Manual Release Tool (MRT) to open the oxygen modules (if installed) - Protective gloves (if installed) - Megaphone.
V
Equipment & Furnishings: 1.4 Flashlight¶
_8ac4fdd3-ff58-4e2a-ad0c-7f6a676ea55f NEW 13 DEC 2023 1054-1096; 1237-1283 1) Description The LED flashlight is power supplied by batteries (Refer to Schematics for flashlight location). 1 4
5 2 3 - Fig. 1 : LED Flashlight - 1 Light Pushbutton Pb pressed in The flashlight switches on. Pb pressed again The flashlight switches off. 2 Battery Status Test Pushbutton Pb pressed in Tests the flashlight battery. When the pushbutton is pressed, the test light (3) comes on. The color of the test light indicates the battery charge.
V 3 Test Light GREEN light Battery charge is good. RED light Battery needs to be changed. 4 Lens Assembly and LED 5 Battery Caps
Equipment & Furnishings: 1.5 Schematics¶
The following diagrams are defined as a typical layout of the emergency equipment in the aircraft. Depending on the aircraft version and the options installed, ATR operators are responsible for the customization of these diagrams.
() LIFE VEST MRT (MANUAL RELEASE TOOL) () DEPENDING ON VERSION - Fig. 1 : Emergency Equipment -
LIFE VEST LIFE VEST EQUIPMENT () LIFE VESTS PROTECTIVE GLOVES ESCAPE ROPE () DEPENDING ON VERSION
Equipment & Furnishings: 01 Location of the Tail Prop¶
On ground during passengers boarding/disembarkation, the tail prop must be installed on the tail skid to avoid aircraft being tipped over. - Fig. 1 : Tail Prop - Note When not used, the tail prop stowage is in the rear unpressurized area of the aircraft (beyond the aft bulkhead.)