MARTIN-BAKER MK-GRUEA-7 EJECTION SEAT
LOWER EJECTION HANDLE
SURVIVAL KIT
COMMAND SEQUENCED EJECTION
EJECTION SEQUENCE BELOW 13,000 ± 1,500 FEET
Figure 1-2.--Ejection sequence above 13,000 ± 1,500 feet.
SEPARATION OF PARACHUTE FROM CREWMEMBERS
ROCKET MOTOR INITIATOR
MAIN BEAM ASSEMBLY
Figure 1-7.--Top latch mechanism.
Figure 1-8.--Time-release mechanism.
Figure 1-9.--Personnel parachute and upper restraint harness.
ANSWERS TO REVIEW QUESTIONS
Figure 2-1.--Forward ejection seat, RH view (SJU-17(V)2/A).
Figure 2-2.--Forward ejection seat, LH view (SJU-17(V)2/A).
GENERAL DESCRIPTION
Figure 2-4.--Catapult assembly, forward seat (SJU-17(V)2/A).
Figure 2-5.--Interference devices, forward and aft seats (SJU-17(V)2/A).
Figure 2-6.--Ejection gun initiator JAU-56/A and catapult manifold valve.
Figure 2-7.--Operation of the top latch assembly.
Figure 2-8.--Drogue deployment catapult.
Figure 2-9.--Drogue deployed.
Figure 2-10.--Parachute deployment rocket motor MK 122 MOD 0.
Figure 2-11.--Electronic sequencer.
Figure 2-12.--Pitot assembly, right hand.
Figure 2-14.--Multipurpose initiator, left hand.
Figure 2-15.--Barostatic release unit.
Figure 2-16.--Shoulder harness reel.
Figure 2-17.--Shoulder harness control system (SJU-17(V)1/A, 2/A and 9/A).
Figure 2-18.--Interference devices, seat bucket to main beams for the forward and aft seats (SJU-17(V)2/A).
Figure 2-19.--Underseat rocket motor mounting bolt sizes (SJU-17(V)2/A).
Figure 2-21.--Seat height actuator (SJU-17(V)3/A and 4/A).
Figure 2-22.--Operating controls (SJU-17(V)1/A, 2/A, and 9/A).
Shoulder Harness Control System
Figure 2-24.--Parachute assembly (SJU-17(V)2/A and 5/A).
Figure 2-25.--Seat survival kit, top view.
Rigid Platform
EJECTION SEQUENCE
Figure 2-29. RH ballistic manifold (SJU-17(V)2/A thru 5/A).
Figure 2-30. LH ballistic manifold (SJU-17(V)2/A thru 5/A).
Figure 2-31.--Underseat rocket motor MK 123 MOD 0 (SJU-17(V)2/A, 3/A, and 5/A).
Figure 2-33.--Ejection sequence (sheet 1 of 2).
Figure 2-33.--Ejection sequence (sheet 2 of 2).
Table 2-1.--Sequencer Timings
ALL SPEEDS/HIGH ALTITUDE
ANSWERS TO REVIEW QUESTIONS
CANOPY SYSTEMS
Figure 3-1.--Canopy pneumatic system components.
CANOPY PNEUMATIC RESERVOIR
LOCK ACTUATOR CHECK VALVE
AUXILIARY OPENING MODE
Figure 3-2.--Canopy inflatable seal system.
Figure 3-3.--Canopy inflatable seal (removed).
Figure 3-5.--Canopy emergency jettison system components.
Figure 3-6.--External canopy jettison initiator.
Explosive Manifolds
COMPONENT DESCRIPTION
Figure 3-9.--External canopy and hatch jettison initiator.
Figure 3-10.--Internal canopy and hatch jettison initiator.
Shielded Mild-Detonating Cord One-Way Transfer
ANSWERS TO REVIEW QUESTIONS
ANSWERS TO REVIEW QUESTIONS - Continued
EXPLOSIVES HANDLING PERSONNEL QUALIFICATION AND CERTIFICATION PROGRAM
Figure 4-1.--Ordnance certification format.
Arm/De-Arm
Table 4-1.--Certification Levels
INITIAL BOARD MEMBER CERTIFICATION
OJT DOCUMENTATION TRANSFERS
Figure 4-2.--Ordnance certification training format.
BOARD MEMBERSHIP
BOARD MEMBER RESPONSIBILITIES
ANSWERS TO REVIEW QUESTIONS
UTILITY SYSTEMS
Figure 5-1. - Bleed air leak sensing element loop schematic diagram
Engine Start Port Leak Detector
Figure 5-2.--Wing leading edge anti-icing cross section.
Figure 5-3.--Anti-icing modulating valve.
OPERATION
Figure 5-5.--Engine bleed air and anti-icing control panels.
Figure 5-6. - P-3 wing anti-icing system schematic.
WINDSHIELD ANTI-ICE/RAIN REMOVAL SYSTEM
Figure 5-8.--Anti-ice/rain removal air control regulating
WINDSHIELD-WASHING SYSTEM
Windshield Switch
Figure 5-12.--Anti-g system.
Anti-G System Filter
Vent Suit Temperature Valve
Manual Mode
Figure 5-18.--Radar liquid cooling system.
FIRE-EXTINGUISHING SYSTEM
Figure 5-22.--P-3 Engine fire extinguishing system.
Container Assembly
OPERATION
Figure 5-25.--Waveguide pressurization system.
Figure 5-26.--Waveguide pressurization system component locator.
Missile Cold Air Modulating Valve
Figure 5-28.--Missile fairing.
Figure 5-30.--Missile cooling system component locator.
Coolant Fluid Expansion Tank
Figure 5-31.--Missile cooling system.
MAINTENANCE SAFETY PRECAUTIONS
ANSWERS TO REVIEW QUESTIONS
ANSWERS TO REVIEW QUESTIONS - Continued
ANSWERS TO REVIEW QUESTIONS - Continued
AIR-CONDITIONING AND PRESSURIZATION SYSTEMS
ATMOSPHERIC CONSIDERATIONS
Figure 6-1.--EDC view from left.
Figure 6-2.--AMP installation.
Figure 6-3.--P-3 air-conditioning system schematic diagram.
Figure 6-5.--Dual check valve, water separator, and ice-limiting sensor.
Figure 6-6.--Temperature control system components.
Temperature Control System Selector-Indicator
Pressure Ratio Limiter Assembly
Figure 6-8.--Selector-indicator.
Figure 6-9.--Air cycle cooling schematic diagram.
Automatic Mode
SYSTEM OPERATION
COMPONENTS
Figure 6-12.--Cabin pressurization components.
Cabin Air Pressure Sensing Filter
Figure 6-14.--Electrical symbols.
Troubleshooting
Troubleshooting - Continued
ANSWERS TO REVIEW QUESTIONS
ANSWERS TO REVIEW QUESTIONS - Continued
OXYGEN SYSTEMS
EFFECTS OF LACK OF OXYGEN
EFFECTS OF LACK OF OXYGEN - Continued
HANDLING/SAFETY PRECAUTIONS
Figure 7-2.--Self-opening oxygen cylinder valve.
Figure 7-3.--Oxygen system check valves.
TYPICAL GASEOUS OXYGEN SYSTEMS
Portable Oxygen Systems
Table 7-1.--Gaseous Oxygen System Troubleshooting
SAFETY PRECAUTIONS
SYSTEM COMPONENTS
Pressure Control Valve
Heat Exchanger
Composite Quick-Disconnect Coupling
AIRCRAFT-MOUNTED OXYGEN REGULATORS
Figure 7-16.--MD regulator operational drawing.
Table 7-2.--Gaseous Oxygen System Troubleshooting
Figure 7-17.--Liquid oxygen converter operation.
Fill Sequence
ONBOARD OXYGEN GENERATING SYSTEM
SYSTEM COMPONENTS
SYSTEM OPERATION
ANSWERS TO REVIEW QUESTIONS
SAFETY PRECAUTIONS
STORAGE TANK PRESSURE GAUGE
Figure 8-2.--Liquid oxygen servicing trailer controls and indicators.
FILL-DRAIN LINE SHUTOFF VALVE
Figure 8-4.--Operating instructions for TMU-70/M.
Table 8-1.--Periodic Inspection
TRANSFER
System Servicing
CONTAMINATION CONTROL
Components
Figure 8-5.--Type No-2 gaseous oxygen servicing trailer.
Loading Cylinders
OXYGEN SERVICING UNIT A/U26U-1A
Figure 8-7.--Oxygen servicing unit A/U26U-1A.
Figure 8-8.--Oxygen servicing unit A/U26U-1A.
Figure 8-9.--Gaseous oxygen module.
Figure 8-10.--Gaseous nitrogen module.
Figure 8-11.--Oxygen/nitrogen interface/servicing equipment.
Figure 8-12.--Air/nitrogen boost pump drive and oxygen servicing flow schematic.
Table 8-2.--Servicing Controls and Indicators
NITROGEN RECHARGING
ANSWERS TO REVIEW QUESTIONS
GLOSSARY
GLOSSARY - Continued
REFERENCES
REFERENCES - Continued
LOWER EJECTION HANDLE
SURVIVAL KIT
COMMAND SEQUENCED EJECTION
EJECTION SEQUENCE BELOW 13,000 ± 1,500 FEET
Figure 1-2.--Ejection sequence above 13,000 ± 1,500 feet.
SEPARATION OF PARACHUTE FROM CREWMEMBERS
ROCKET MOTOR INITIATOR
MAIN BEAM ASSEMBLY
Figure 1-7.--Top latch mechanism.
Figure 1-8.--Time-release mechanism.
Figure 1-9.--Personnel parachute and upper restraint harness.
ANSWERS TO REVIEW QUESTIONS
Figure 2-1.--Forward ejection seat, RH view (SJU-17(V)2/A).
Figure 2-2.--Forward ejection seat, LH view (SJU-17(V)2/A).
GENERAL DESCRIPTION
Figure 2-4.--Catapult assembly, forward seat (SJU-17(V)2/A).
Figure 2-5.--Interference devices, forward and aft seats (SJU-17(V)2/A).
Figure 2-6.--Ejection gun initiator JAU-56/A and catapult manifold valve.
Figure 2-7.--Operation of the top latch assembly.
Figure 2-8.--Drogue deployment catapult.
Figure 2-9.--Drogue deployed.
Figure 2-10.--Parachute deployment rocket motor MK 122 MOD 0.
Figure 2-11.--Electronic sequencer.
Figure 2-12.--Pitot assembly, right hand.
Figure 2-14.--Multipurpose initiator, left hand.
Figure 2-15.--Barostatic release unit.
Figure 2-16.--Shoulder harness reel.
Figure 2-17.--Shoulder harness control system (SJU-17(V)1/A, 2/A and 9/A).
Figure 2-18.--Interference devices, seat bucket to main beams for the forward and aft seats (SJU-17(V)2/A).
Figure 2-19.--Underseat rocket motor mounting bolt sizes (SJU-17(V)2/A).
Figure 2-21.--Seat height actuator (SJU-17(V)3/A and 4/A).
Figure 2-22.--Operating controls (SJU-17(V)1/A, 2/A, and 9/A).
Shoulder Harness Control System
Figure 2-24.--Parachute assembly (SJU-17(V)2/A and 5/A).
Figure 2-25.--Seat survival kit, top view.
Rigid Platform
EJECTION SEQUENCE
Figure 2-29. RH ballistic manifold (SJU-17(V)2/A thru 5/A).
Figure 2-30. LH ballistic manifold (SJU-17(V)2/A thru 5/A).
Figure 2-31.--Underseat rocket motor MK 123 MOD 0 (SJU-17(V)2/A, 3/A, and 5/A).
Figure 2-33.--Ejection sequence (sheet 1 of 2).
Figure 2-33.--Ejection sequence (sheet 2 of 2).
Table 2-1.--Sequencer Timings
ALL SPEEDS/HIGH ALTITUDE
ANSWERS TO REVIEW QUESTIONS
CANOPY SYSTEMS
Figure 3-1.--Canopy pneumatic system components.
CANOPY PNEUMATIC RESERVOIR
LOCK ACTUATOR CHECK VALVE
AUXILIARY OPENING MODE
Figure 3-2.--Canopy inflatable seal system.
Figure 3-3.--Canopy inflatable seal (removed).
Figure 3-5.--Canopy emergency jettison system components.
Figure 3-6.--External canopy jettison initiator.
Explosive Manifolds
COMPONENT DESCRIPTION
Figure 3-9.--External canopy and hatch jettison initiator.
Figure 3-10.--Internal canopy and hatch jettison initiator.
Shielded Mild-Detonating Cord One-Way Transfer
ANSWERS TO REVIEW QUESTIONS
ANSWERS TO REVIEW QUESTIONS - Continued
EXPLOSIVES HANDLING PERSONNEL QUALIFICATION AND CERTIFICATION PROGRAM
Figure 4-1.--Ordnance certification format.
Arm/De-Arm
Table 4-1.--Certification Levels
INITIAL BOARD MEMBER CERTIFICATION
OJT DOCUMENTATION TRANSFERS
Figure 4-2.--Ordnance certification training format.
BOARD MEMBERSHIP
BOARD MEMBER RESPONSIBILITIES
ANSWERS TO REVIEW QUESTIONS
UTILITY SYSTEMS
Figure 5-1. - Bleed air leak sensing element loop schematic diagram
Engine Start Port Leak Detector
Figure 5-2.--Wing leading edge anti-icing cross section.
Figure 5-3.--Anti-icing modulating valve.
OPERATION
Figure 5-5.--Engine bleed air and anti-icing control panels.
Figure 5-6. - P-3 wing anti-icing system schematic.
WINDSHIELD ANTI-ICE/RAIN REMOVAL SYSTEM
Figure 5-8.--Anti-ice/rain removal air control regulating
WINDSHIELD-WASHING SYSTEM
Windshield Switch
Figure 5-12.--Anti-g system.
Anti-G System Filter
Vent Suit Temperature Valve
Manual Mode
Figure 5-18.--Radar liquid cooling system.
FIRE-EXTINGUISHING SYSTEM
Figure 5-22.--P-3 Engine fire extinguishing system.
Container Assembly
OPERATION
Figure 5-25.--Waveguide pressurization system.
Figure 5-26.--Waveguide pressurization system component locator.
Missile Cold Air Modulating Valve
Figure 5-28.--Missile fairing.
Figure 5-30.--Missile cooling system component locator.
Coolant Fluid Expansion Tank
Figure 5-31.--Missile cooling system.
MAINTENANCE SAFETY PRECAUTIONS
ANSWERS TO REVIEW QUESTIONS
ANSWERS TO REVIEW QUESTIONS - Continued
ANSWERS TO REVIEW QUESTIONS - Continued
AIR-CONDITIONING AND PRESSURIZATION SYSTEMS
ATMOSPHERIC CONSIDERATIONS
Figure 6-1.--EDC view from left.
Figure 6-2.--AMP installation.
Figure 6-3.--P-3 air-conditioning system schematic diagram.
Figure 6-5.--Dual check valve, water separator, and ice-limiting sensor.
Figure 6-6.--Temperature control system components.
Temperature Control System Selector-Indicator
Pressure Ratio Limiter Assembly
Figure 6-8.--Selector-indicator.
Figure 6-9.--Air cycle cooling schematic diagram.
Automatic Mode
SYSTEM OPERATION
COMPONENTS
Figure 6-12.--Cabin pressurization components.
Cabin Air Pressure Sensing Filter
Figure 6-14.--Electrical symbols.
Troubleshooting
Troubleshooting - Continued
ANSWERS TO REVIEW QUESTIONS
ANSWERS TO REVIEW QUESTIONS - Continued
OXYGEN SYSTEMS
EFFECTS OF LACK OF OXYGEN
EFFECTS OF LACK OF OXYGEN - Continued
HANDLING/SAFETY PRECAUTIONS
Figure 7-2.--Self-opening oxygen cylinder valve.
Figure 7-3.--Oxygen system check valves.
TYPICAL GASEOUS OXYGEN SYSTEMS
Portable Oxygen Systems
Table 7-1.--Gaseous Oxygen System Troubleshooting
SAFETY PRECAUTIONS
SYSTEM COMPONENTS
Pressure Control Valve
Heat Exchanger
Composite Quick-Disconnect Coupling
AIRCRAFT-MOUNTED OXYGEN REGULATORS
Figure 7-16.--MD regulator operational drawing.
Table 7-2.--Gaseous Oxygen System Troubleshooting
Figure 7-17.--Liquid oxygen converter operation.
Fill Sequence
ONBOARD OXYGEN GENERATING SYSTEM
SYSTEM COMPONENTS
SYSTEM OPERATION
ANSWERS TO REVIEW QUESTIONS
SAFETY PRECAUTIONS
STORAGE TANK PRESSURE GAUGE
Figure 8-2.--Liquid oxygen servicing trailer controls and indicators.
FILL-DRAIN LINE SHUTOFF VALVE
Figure 8-4.--Operating instructions for TMU-70/M.
Table 8-1.--Periodic Inspection
TRANSFER
System Servicing
CONTAMINATION CONTROL
Components
Figure 8-5.--Type No-2 gaseous oxygen servicing trailer.
Loading Cylinders
OXYGEN SERVICING UNIT A/U26U-1A
Figure 8-7.--Oxygen servicing unit A/U26U-1A.
Figure 8-8.--Oxygen servicing unit A/U26U-1A.
Figure 8-9.--Gaseous oxygen module.
Figure 8-10.--Gaseous nitrogen module.
Figure 8-11.--Oxygen/nitrogen interface/servicing equipment.
Figure 8-12.--Air/nitrogen boost pump drive and oxygen servicing flow schematic.
Table 8-2.--Servicing Controls and Indicators
NITROGEN RECHARGING
ANSWERS TO REVIEW QUESTIONS
GLOSSARY
GLOSSARY - Continued
REFERENCES
REFERENCES - Continued