212-MM-CH26 Fire Protection
212-MM-CH26 Fire Protection
TABLE OF CONTENTS
FIRE PROTECTION
FIRE DETECTION
FIRE EXTINGUISHERS
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FIGURES
Figure Page
Number Title Number
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FIRE PROTECTION
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FIRE DETECTION
26-2. ENGINE FIRE DETECTION 2. Disconnect electrical connectors (10 and 11,
Figure 26-1).
Engine compartment fire detection consists of two
heat sensing elements and two flexible cable 3. Remove screw (9) from clamp (8). Remove
assemblies for each power section of the engine. A screws from six remaining clamps in same manner.
press-to-test switch is provided to test the system.
Pressing the FIRE EXT PRESS TO TEST switch Refer to BHT-ALL-SPM for specifications.
places a low resistance across each of the fire sensing
elements to simulate a fire/overheat condition. If NUMBER NOMENCLATURE
sensing elements are operating properly, both FIRE 1
C-405 Lockwire
PULL and FIRE 2 PULL handles will illuminate.
26-3. ENGINE UPPER FIRE DETECTION 1. Verify all electrical power is removed from
SENSING ELEMENTS helicopter.
The upper fire detection sensing elements are 2. Position sensing element (2, Figure 26-1) on
mounted on the underside of the upper engine cowling upper cowl as shown in View A.
(Figure 26-1).
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z
DETECTION SENSING ELEMENTS. SMOKE DETECTION SYSTEM.
NOTE
The baggage compartment smoke detector is
a closed assembly housing solid-state
Maintenance procedures are the electronic components and a light sensitive
same for both left and right sensing detector. The detector (4, figure 26-2) is
figure 26-2
elements. located in the forward end of the baggage
compartment roof. A protective screen is
La)
installed over the detector to provide
0.m
26-8. Removal. protection from items stowed in the
compartment. The instant smoke reduces
E
1. Verify all electrical power removed from light transmission in the baggage com-
helicopter. partment 30 to 35% below that of clear air,
-s-
-'Q3
the detector causes the BAGGAGE FIRE
2. Disconnect electrical connectors (14 and
r..
Chapter 96
26-10. Installation. information.
26-14. Removal.
helicopter.
1. Remove all electrical power from
2. Position sensing element in clamps (12,
gy=m
Cam.
helicopter.
figure 26-1).
figure 26-1
2. Open baggage compartment door (9,
3. Install retaining screws (13) in clamps. figure 26-2).
_':
figure 26-2
4. Connect electrical connectors (14 and 3. Remove screws (7) and screen (6).
15).
4. Disconnect electrical connector (5).
5. Perform operational check (paragraph 26-
paragraph 26-
11).
11 5. Remove screws (3) and washers (2).
Remove smoke detector (4).
26-11. Operational check.
26-15. Inspection.
Perform operational ch eck after any
°>0
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BHT-212-MM
I)
I I
li
I I
Lj-
SENSING ELEMENT ON
LEFT ENGINE POWER
SECTION TOP COWL
(VIEW LOOKING DOWN)
VIEW A 212-M-26-1-1
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SENSING ELEMENT ON
LEFT ENGINE POWER
SECTION FIREWALL
(VIEW LOOKING FORWARD)
VIEW B
3``
2. Sensing element (left engine power section top cowl) 1 0. Electrical connector
3. Flex cable 1 1. Electrical connector
4. Upper engine cowling 1 2. Clamp (eight required)
5. Engine cowl top panel 1 3. Screw
6. Sensing element (left power section firewall) 1 4. Electrical connector
coin.
1 5. Electrical connector
8. Clamp (seven required)
212-M-26-1-2
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((DD
4. Install screen (6) with screws (7) and
washers (8). detection system (Chapter 96).
Chapter 96
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1. Decal
2. Thin aluminum washer
3. Screw
4. Smoke detector
5. Electrical connector
6. Protective screen
7. Screw
8. Thin steel washer
9. Baggage compartment door
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FIRE EXTINGUISHERS
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portable, cabin mounted fire extinguishers. THE FIRE EXTINGUISHER
CONTAINERS ARE PRESSURIZED
AND EQUIPPED WITH PYRO-
26-19. ENGINE COMPARTMENT FIRE TECHNIC CARTRIDGES. ANY
EXTINGUISHERS. TIME CONNECTING WIRES ARE
DISCONNECTED, SHORTING
The two engine compartment fire
0-0--
0
0
>10
FIGURE 26-4
tubing to allow either container to be INSTALLED TO PREVENT
Z
discharged into either power section INADVERTANT DETONATION.
compartment (figure 26-3). Therefore, in the
figure 26-3
cao+,
0<z
Z
to extinguish a fire, the second (reserve)
O-0
0)0
Chapters 96 98
CONNECTORS ONE AT A TIME
AND INSTALL JUMPER WIRE
NOTE (SHORTING PLUG) AT VACANT
ACC
same.
REINSTALLATION IN PROPER
LOCATION.
Z
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RESERVE MAIN
FIRE EXT FIRE EXT
CONTAINER CONTAINER
(LEFT) (RIGHT)
LEFT RIGHT
POWER POWER
SECTION SECTION
MANIFOLD MANIFOLD
F
PRESS TO TEST I
FIRE 1 PULL R FIRE 2 PULL
E
MAIN E
X
OFF T
RESERVE
LEFT POWER SECTION RIGHT POWER SECTION
BLEED AIR VALVE BLEED AIR VALVE
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BHT-212-MM-3
1. Verify that all the electrical power is removed from structural integrity is acceptable without repair. If
the helicopter and that the helicopter is properly damage is such that loss of the structural integrity is
grounded. suspected, the container shall be replaced.
2. Open the engine cowling to gain access to the 2. Inspect the temperature/pressure correction
extinguisher bottles. decal for security and legibility.
6. Install the loose end of the jumper wire (45) on 5. Replace or recharge the container if empty.
the terminal (31) with the nut (34).
10. Install the loose end of the jumper wire (46) on Refer to BHT-ALL-SPM for specifications.
the terminal (40) with the nut (38).
NUMBER NOMENCLATURE
11. Disconnect the tube (3) from the discharge
C-405 Lockwire
outlet (5).
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3. Replace the container temperature/pressure (4) Install the jumper wire (45) on the
table decal if illegible or otherwise unserviceable. terminal (35) and install the nut (37).
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(11) To remove the cartridges (4 and 30) from (2) Open the engine cowling to gain access
the housing assemblies (4A and 30A), unscrew the to the fire extinguisher containers.
cartridge while holding the hexagonal head of the
housing assemblies, to prevent accidental discharge. (3) Remove the nut (37). Tag and remove
Discard the seal. the electrical wire (36) from the terminal (35).
(12) Install the new seal on the cartridges (4 (4) Install the jumper wire (45) on the
and 30). Install the cartridges in the housing terminal (35) and install the nut (37).
assemblies (4A and 30A). Hold the hexagonal head of
the housing assemblies with a wrench while tightening (5) Install the loose end of the jumper wire
the cartridges to prevent excessive torque on the (45, Detail B) on the terminal (31) with the nut (34).
housing assemblies. Torque the cartridges 70 to The jumper wire must remain connected at all times
80 inch-pounds (7.91 to 9.04 Nm). when the cartridge (30) is disconnected from the
helicopter wiring.
(13) Install lockwire (C-405) on the housing
(6) Remove the nut (41) and the electrical
assemblies (4A and 30A) and the cartridges (4 and
wire (43) with the electrical terminal nipple (42). Tag
30).
the electrical wire.
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6. Install the tube (3) on the discharge outlet (5). 2. Disconnect the hose (20, Figure 26-4) from the
nipple (50).
7. Install the tube (18) on the discharge outlet (29).
3. Remove the screws (47), washers (48), and
nuts (49).
26-26. INSPECTION
REFER TO THE WIRING DIAGRAM
(FIGURE 26-6) PRIOR TO CONNECTING Inspect the indicator discs on both containers for a
THE WIRE S TO THE CARTRIDGES . missing red indicator, secure installation, and obvious
MAKE SURE THAT THE WIRES ARE damage. A missing red disc indicates that the
INSTALLED ON THE CORRECT container may have discharged through the fill and
TERMINALS. thermal relief fitting.
The maintenance procedures for both discharge Two hand-held, portable fire extinguishers are
indicator discs are identical. installed in the quick release brackets at the locations
illustrated in Figure 26-5. These extinguishers are
filled with bromochlorodifluoromethane or equivalent
extinguishing agent.
WARNING
NOTE
MAKE SURE THAT NO POWER IS Maintenance procedures for both the fire
APPLIED TO THE HELICOPTER extinguishers and the brackets are
ELECTRICAL SYSTEMS AND THAT THE identical.
HELICOPTER IS PROPERLY
GROUNDED WHILE PERFORMING 26-29. REMOVAL
MAINTENANCE ON THE FIRE
EXTINGUISHER SYSTEM. 1. Release the clamp (7, Figure 26-5) and remove
the fire extinguisher.
26-25. REMOVAL
2. Remove the bolts (8), thin aluminum washer (9),
1. Remove all electrical power from the helicopter. bracket (11), and aluminum washers (10).
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3. Inspect the bracket and the attaching hardware 2. Install the bolt (8) and the thin aluminum washers
for obvious damage and security of the installation and (9). Tighten the bolts.
serviceability.
3. Open the retaining clamp (7) and position the fire
26-31. REPAIR extinguisher in the bracket. Close the retaining clamp.
1. Recharge the fire extinguisher, as required, at a 4. Verify that the bracket is securely installed in the
facility equipped and authorized to service helicopter and the fire extinguisher is securely
bromochlorodifluoromethane type extinguishers. installed in the retaining bracket.
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