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WARNING
Exercise care in rescue operations to
prevent inadvertently firing the ejection
seat.
EJECTION CONTROL
HANDLES
EJECTION
CONTROL
HANDLE
SECONDARY EJECTION CONTROL
DISCONNECT PULLEY AND CABLE
ASSEMBLY
SECONDARY
EJECTION
CONTROL
HANDLE
MK 1 MOD 0 ROCKET
CATAPULT (RAPEC)
FACE CURTAIN EJECTION
CONTROL HANDLE
EJECTION CONTROL
PULLEY MECHANISM
CATAPULT FIRING CONTROL CABLE
2-12
TO 00-105E-9
Figure 2-14. ACES II Escape Ejection Seat Showing Methods of Safetying for the A-10, B-1, B-2, F-15,
F-22A and F-117. F-16 safety pin is installed at aft bottom of Ground Safety Lever. (See Chapter 8)
Figure 2-13. Martin-Baker Ejection Seat Drogue Gun
DROGUE GUN
WITHDRAWAL LINE
SHACKLE (PISTON
ATTACHED TO LINE)
INTERNAL
PISTON
GUN
BARREL
DROGUE
GUN
SAFETY
PIN
TRIP ROD
(DO NOT TRIP OR PULL)
EJECTION
CONTROL
HANDLES
GROUND SAFETY
LEVER (LT ARM
REST ONLY)
SAFETY PIN
(INBOARD INSTALLATION, PIN DOES
NOT PROTRUDE THROUGH EJECTION
HANDLE AND SEAT HOUSING
2-13
SAFETY
PIN, F-16
ONLY
TO 00-105E-9
SAFETY PIN
FOR FACE CURTAIN
EJECTION HANDLE
SAFETY PIN FOR
CATAPULT FIRING
MECHANISM
INTERDICTOR
SAFETY PIN
ASSEMBLY
(INSTALLED
THROUGH
CATAPULT
SEAR)
FIRING
MECHANISM
CATAPULT SEAR
(DO NOT DISLODGE!
FIRING MECHANISM
WILL FIRE AND IGNITE
CATAPULT AND EJECT SEAT!
7/32 7/32
1 1/2
INITIATOR
SAFETY PIN
LOCATION
DROGUE
GUN
FIRING
MECHANISM
LINKAGE
FACE CURTAIN
EJECTION HANDLES
(SAFETY PIN IS
INSTALLED AT CENTER
HANDLE ASSEMBLY)
Figure 2-15. Martin-Baker Ejection Seat Showing Disarming Safety Pins and Red Flag
2-14
WARNING
SEE CLOSER
VIEWS OF
DANGER AREAS
WARNING
DO NOT PULL OR
HIT DROGUE GUN
LINKAGE, GUN
WILL FIRE PISTON!
EJECTION
HANDLE
“D” RING
ROTATE RED
FLAG UP TO SAFE
“D” RING AND
DISARM SEAT
NOTE:
For those seats not using gas to ignite the rocket
pack (under seat bucket), a safety pin is installed
in the rocket pack, forward right side at firing
mechanism safety cover. Cover is a fiberglass boot.
TO 00-105E-9
Using a power
rescue saw, cut
along line (canopy
frame) until plastic
can be grasped
If plastic can and broken.
not be broken
free, continue
cutting with
power rescue
saw around
canopy.
EJECTION
SEAT
FIRING
MECHANISM
Watch for fragmentation and jagged
edges. Edges are very sharp. Fragmentation
characteristics differ in type
and construction of acrylic plastic.
WARNING
Figure 2-16. Forcible Entry into
Plastic Canopies
Figure 2-17. Forcible Entry into a
Plastic Canopy
Figure 2-18. Forcible Entry into a Plastic
Canopy Exposed to Fire Conditions
NOTE:
Lines denote area cut and the plastic was then
grasped and broken free. Note the large section
removed and the absence of shattering.
NOTE:
Lines denote area cut and the plastic was then
grasped and broken free. Note large section
removed.
2-15
TO 00-105E-9
2-16
2-50. AIRCRAFT HOT WHEEL AND BRAKES.
2-51. Aircraft hot wheel and brakes pose serious considerations
for Fire Protection personnel. These considerations
are: (1) Danger Zones are areas where exploding
wheel, brake and tire assemblies can injure personnel,
(2) Safe Zones are areas of approach to the
wheels, brakes and tires if a fire is present and requires
immediate suppression, and (3) Heat Dissipation times
before the wheel and brake assemblies can be safely
approached if there has been no fire or damage. (Aircraft
tires use fuse plugs designed to melt at a given
temperature and relieve tire air pressure.)
The following is general information that is common to
most aircraft:
2-52. Danger Zones. Avoid inflated main landing gear
tire side area within 300 feet. (See Figure 2-19.)
2-53. Safe Zones. Approach wheel/brake and tire assemblies
from the front or rear of assemblies at a 45
degree angle. Munitions loaded on the aircraft must
also be taken into consideration when determining the
proper approach.
2-54. Heat Dissipation. After aircraft has stopped, wait
30 minutes for the heat in wheel and brake assemblies
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