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FOR REFERENCE USE ONLY
Emergency Responder Familiarization TrainingF-35 LIGHTNING II
2
F-35 Program InformationNON EXPORT CONTROLLED INFORMATION – RELEASABLE TO FOREIGN PERSONS
Important Notice: A hard copy of this document may not be the document currently in effect. The current version is always the version on the Lockheed Martin network.
Doc. No: 2YZA00666 Rev-BDate: Mar-18-2010
Course Outline
IntroductionAircraft Hazards
Ingress/Egress and Life Support SystemsCockpit Entry and Pilot Removal Procedures
Aircraft Hot Wheels and BrakesMiscellaneous Information for Situational Awareness
ReviewQuestions
Introduction
3
F-35 Program InformationNON EXPORT CONTROLLED INFORMATION – RELEASABLE TO FOREIGN PERSONS
Important Notice: A hard copy of this document may not be the document currently in effect. The current version is always the version on the Lockheed Martin network.
Doc. No: 2YZA00666 Rev-BDate: Mar-18-2010
WARNINGS
Engine inlet area is ingestion hazard while engine is operating. Personnel must not go into engine inlet hazard area. Personnel must use caution when near engine inlet hazard area. Failure to comply can result in injury or death to personnel and/or damage to aircraft and/or equipment.
Very high noise level can occur. Personnel must wear hearing protection. Failure to comply can result in injury to personnel.
Wheels/tires can blowout. Personnel must not go near wheels if there is possible hot brake condition. Failure to comply can result in injury or death to personnel.
Tire can blowout. Personnel must stay fwd or aft of tire at all times. Failure to comply can result in injury or death to personnel.
FOR REFERENCE USE ONLY
7
F-35 Program InformationNON EXPORT CONTROLLED INFORMATION – RELEASABLE TO FOREIGN PERSONS
Important Notice: A hard copy of this document may not be the document currently in effect. The current version is always the version on the Lockheed Martin network.
Doc. No: 2YZA00666 Rev-BDate: Mar-18-2010
F-35A Lightning II Conventional Take-Off and Landing (CTOL) Aircraft
General Aircraft DescriptionIntroduction
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F-35 Program InformationNON EXPORT CONTROLLED INFORMATION – RELEASABLE TO FOREIGN PERSONS
Important Notice: A hard copy of this document may not be the document currently in effect. The current version is always the version on the Lockheed Martin network.
Doc. No: 2YZA00666 Rev-BDate: Mar-18-2010
Aircraft hazards include the following:• Airframe Hazards• Noise Hazards• In-Wash and Out-Wash Hazards• Aircraft Material Hazards
Aircraft Hazards
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F-35 Program InformationNON EXPORT CONTROLLED INFORMATION – RELEASABLE TO FOREIGN PERSONS
Important Notice: A hard copy of this document may not be the document currently in effect. The current version is always the version on the Lockheed Martin network.
Doc. No: 2YZA00666 Rev-BDate: Mar-18-2010
• Sharp edges• Operating hinged areas• Caution zones
The following are airframe hazards to be aware of:
Airframe HazardsAircraft Hazards
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F-35 Program InformationNON EXPORT CONTROLLED INFORMATION – RELEASABLE TO FOREIGN PERSONS
Important Notice: A hard copy of this document may not be the document currently in effect. The current version is always the version on the Lockheed Martin network.
Doc. No: 2YZA00666 Rev-BDate: Mar-18-2010
Airframe HazardsAircraft Hazards
11
F-35 Program InformationNON EXPORT CONTROLLED INFORMATION – RELEASABLE TO FOREIGN PERSONS
Important Notice: A hard copy of this document may not be the document currently in effect. The current version is always the version on the Lockheed Martin network.
Doc. No: 2YZA00666 Rev-BDate: Mar-18-2010
Airframe HazardsAircraft Hazards
12
F-35 Program InformationNON EXPORT CONTROLLED INFORMATION – RELEASABLE TO FOREIGN PERSONS
Important Notice: A hard copy of this document may not be the document currently in effect. The current version is always the version on the Lockheed Martin network.
Doc. No: 2YZA00666 Rev-BDate: Mar-18-2010
Inlet forces may cause ingestion hazards for personnel operating within 14 feet forward to 5 foot aft and 18 feet across the intake area.
In-Wash Out-Wash HazardsAircraft Hazards
3 FT FWD
1 FT AFT
Hot Exhaust from IPP (Left AFT side of ACFT)
15 FT AFT
IPP EXHAUST DANGER AREA
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F-35 Program InformationNON EXPORT CONTROLLED INFORMATION – RELEASABLE TO FOREIGN PERSONS
Important Notice: A hard copy of this document may not be the document currently in effect. The current version is always the version on the Lockheed Martin network.
Doc. No: 2YZA00666 Rev-BDate: Mar-18-2010
Aircraft materials that pose a recognized risk to personnel after a dynamic incident. These materials include:•Composite Material Hazards•Pressure Vessels •Batteries•Explosives•Radiation
Aircraft Material HazardsAircraft Hazards
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F-35 Program InformationNON EXPORT CONTROLLED INFORMATION – RELEASABLE TO FOREIGN PERSONS
Important Notice: A hard copy of this document may not be the document currently in effect. The current version is always the version on the Lockheed Martin network.
Doc. No: 2YZA00666 Rev-BDate: Mar-18-2010
Exterior Skin – Composite Materials (Epoxy or Bismaleimide Resins) • Inhalation and Skin Contact Risk • Wear Full Respirators and Coveralls • Prevent Dust Inhalation or Skin Contact during Post Crash Handling • Spray with wax based substance to prevent further dust and shard
generation.
Aircraft Material HazardsAircraft Hazards
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F-35 Program InformationNON EXPORT CONTROLLED INFORMATION – RELEASABLE TO FOREIGN PERSONS
Important Notice: A hard copy of this document may not be the document currently in effect. The current version is always the version on the Lockheed Martin network.
Doc. No: 2YZA00666 Rev-BDate: Mar-18-2010
Landing Gear • Exterior Wheel Surfaces contain Cadmium Plate • Inhalation Risk • Wear Full Respirators and Coveralls • Prevent any dust inhalation or skin contact during post crash
handling
Aircraft Material HazardsAircraft Hazards
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F-35 Program InformationNON EXPORT CONTROLLED INFORMATION – RELEASABLE TO FOREIGN PERSONS
Important Notice: A hard copy of this document may not be the document currently in effect. The current version is always the version on the Lockheed Martin network.
Doc. No: 2YZA00666 Rev-BDate: Mar-18-2010
Explosives
Transparency Removal System (TRS)– Flexible Linear Shaped Charge (FLSC)– Rapid Deflagrating Cord Transfer Lines (RDCTL)
Aircraft Material HazardsAircraft Hazards
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F-35 Program InformationNON EXPORT CONTROLLED INFORMATION – RELEASABLE TO FOREIGN PERSONS
Important Notice: A hard copy of this document may not be the document currently in effect. The current version is always the version on the Lockheed Martin network.
Doc. No: 2YZA00666 Rev-BDate: Mar-18-2010
Electro Optical Targeting System (EOTS) (if installed)– Extensive Use of Beryllium Alloys– Laser Assembly Contains Small Radioactive Source
» Inhalation and dermal contact risk» Wear full respirators and coveralls» Prevent any dust inhalation or skin contact during post crash
handling
Aircraft Material HazardsAircraft Hazards
Radiation
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F-35 Program InformationNON EXPORT CONTROLLED INFORMATION – RELEASABLE TO FOREIGN PERSONS
Important Notice: A hard copy of this document may not be the document currently in effect. The current version is always the version on the Lockheed Martin network.
Doc. No: 2YZA00666 Rev-BDate: Mar-18-2010
Update Graphic ???
300 ft.45°45°
300 ft.45° 45°
• Explosion Hazard• Safe approach
Cautionzone
Cautionzone
Cautionzone
Cautionzone
• Safety Concerns
10-15 deg
10-15 deg
10-15 deg
10-15 deg
Hot Wheels and BrakesAircraft Hazards
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F-35 Program InformationNON EXPORT CONTROLLED INFORMATION – RELEASABLE TO FOREIGN PERSONS
Important Notice: A hard copy of this document may not be the document currently in effect. The current version is always the version on the Lockheed Martin network.
Doc. No: 2YZA00666 Rev-BDate: Mar-18-2010
Transparency Removal System (TRS)Ingress/Egress & Life Support Systems
Rapid Deflagration Cord Transfer Line (RDCTL) example.
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F-35 Program InformationNON EXPORT CONTROLLED INFORMATION – RELEASABLE TO FOREIGN PERSONS
Important Notice: A hard copy of this document may not be the document currently in effect. The current version is always the version on the Lockheed Martin network.
Doc. No: 2YZA00666 Rev-BDate: Mar-18-2010
Transparency Removal System
WARNING: Do not cut within 3 inches of the edge of the transparency. Cutting of RDCTRLs may inadvertently activate TRS detonation.
Rapid Deflagration Cord Transfer Lines (RDCTLs)
Flexible Linear Shaped Charge (FLSC)
Ingress/Egress & Life Support Systems
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F-35 Program InformationNON EXPORT CONTROLLED INFORMATION – RELEASABLE TO FOREIGN PERSONS
Important Notice: A hard copy of this document may not be the document currently in effect. The current version is always the version on the Lockheed Martin network.
Doc. No: 2YZA00666 Rev-BDate: Mar-18-2010
Canopy CuttingIngress/Egress & Life Support Systems
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F-35 Program InformationNON EXPORT CONTROLLED INFORMATION – RELEASABLE TO FOREIGN PERSONS
Important Notice: A hard copy of this document may not be the document currently in effect. The current version is always the version on the Lockheed Martin network.
Doc. No: 2YZA00666 Rev-BDate: Mar-18-2010
Transparency Removal System (TRS)Ingress/Egress & Life Support Systems
24
F-35 Program InformationNON EXPORT CONTROLLED INFORMATION – RELEASABLE TO FOREIGN PERSONS
Important Notice: A hard copy of this document may not be the document currently in effect. The current version is always the version on the Lockheed Martin network.
Doc. No: 2YZA00666 Rev-BDate: Mar-18-2010
Arm/Safe/Egress (ASE) Handle
HMD Quick Disconnect
Quick Release Buckle (QRB)
Ejection Handle
Simplified Combined Harness
Parachute Container
Canopy Penetrators
Services Connection
Package (SCP)
Seat Bucket Assembly
Ejection Seat SystemIngress/Egress & Life Support Systems
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F-35 Program InformationNON EXPORT CONTROLLED INFORMATION – RELEASABLE TO FOREIGN PERSONS
Important Notice: A hard copy of this document may not be the document currently in effect. The current version is always the version on the Lockheed Martin network.
Doc. No: 2YZA00666 Rev-BDate: Mar-18-2010
Thermal Batteries
Drogue Container
Back-Up Oxygen Supply (BOS)
Sequencer
Neck Protection Device Bottle
Seat Rail and Tilt Mechanism
Ejection Seat SystemIngress/Egress & Life Support Systems
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F-35 Program InformationNON EXPORT CONTROLLED INFORMATION – RELEASABLE TO FOREIGN PERSONS
Important Notice: A hard copy of this document may not be the document currently in effect. The current version is always the version on the Lockheed Martin network.
Doc. No: 2YZA00666 Rev-BDate: Mar-18-2010
Seat Restraint System consists of:– Simplified Combined Harness– Passive Leg Restraint System– Active Arm Restraint System– Personal Services Connections
Ejection Seat SystemIngress/Egress & Life Support Systems
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F-35 Program InformationNON EXPORT CONTROLLED INFORMATION – RELEASABLE TO FOREIGN PERSONS
Important Notice: A hard copy of this document may not be the document currently in effect. The current version is always the version on the Lockheed Martin network.
Doc. No: 2YZA00666 Rev-BDate: Mar-18-2010
Simplified Combined Harness– Parachute– Seat restraints
Quick Release Box
Ejection Seat SystemIngress/Egress & Life Support Systems
28
F-35 Program InformationNON EXPORT CONTROLLED INFORMATION – RELEASABLE TO FOREIGN PERSONS
Important Notice: A hard copy of this document may not be the document currently in effect. The current version is always the version on the Lockheed Martin network.
Doc. No: 2YZA00666 Rev-BDate: Mar-18-2010
Pulls arms in to prevent flailing
Arm Restraint routing
Automatic release when QRB is
rotated
Active Arm Restraint System
Ejection Seat SystemIngress/Egress & Life Support Systems
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F-35 Program InformationNON EXPORT CONTROLLED INFORMATION – RELEASABLE TO FOREIGN PERSONS
Important Notice: A hard copy of this document may not be the document currently in effect. The current version is always the version on the Lockheed Martin network.
Doc. No: 2YZA00666 Rev-BDate: Mar-18-2010
Leg Restraint Lines
Passive Leg Restraint System (PLRS)– Purpose– Action free
ingress/egress– Stowage– Kevlar cords
Ejection Seat SystemIngress/Egress & Life Support Systems
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F-35 Program InformationNON EXPORT CONTROLLED INFORMATION – RELEASABLE TO FOREIGN PERSONS
Important Notice: A hard copy of this document may not be the document currently in effect. The current version is always the version on the Lockheed Martin network.
Doc. No: 2YZA00666 Rev-BDate: Mar-18-2010
Pilot Interface Connector (PIC)– Purpose– Location– Operation
Pilot’s Oxygen
Manual Release Handle and Button. Automatically disconnects when seat ASE Handle is rotated aft to the “Egress” position.
Pilot’s Communication
Pilot’s Anti-G
Ejection Seat SystemIngress/Egress & Life Support Systems
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F-35 Program InformationNON EXPORT CONTROLLED INFORMATION – RELEASABLE TO FOREIGN PERSONS
Important Notice: A hard copy of this document may not be the document currently in effect. The current version is always the version on the Lockheed Martin network.
Doc. No: 2YZA00666 Rev-BDate: Mar-18-2010
Helmet Quick Disconnect/Connect (QDC) fitting– Manual connect
point for helmet display electronics
– Automatically disconnects with ASE Handle
Ejection Seat SystemIngress/Egress & Life Support Systems
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F-35 Program InformationNON EXPORT CONTROLLED INFORMATION – RELEASABLE TO FOREIGN PERSONS
Important Notice: A hard copy of this document may not be the document currently in effect. The current version is always the version on the Lockheed Martin network.
Doc. No: 2YZA00666 Rev-BDate: Mar-18-2010
Arm/Safe/Egress (ASE) Handle
Seat ARMED
ASE Handle can be rotated to SAFE without pressing button.
Seat EGRESS
Thumb button pressed to rotate handle from SAFE to EGRESS
Seat SAFE
ASE Handle is locked with safety pin & streamer
Depress Thumb Button to rotate handle from SAFE to the ARMED
position or to the EGRESS position
Ejection Seat SystemIngress/Egress & Life Support Systems
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F-35 Program InformationNON EXPORT CONTROLLED INFORMATION – RELEASABLE TO FOREIGN PERSONS
Important Notice: A hard copy of this document may not be the document currently in effect. The current version is always the version on the Lockheed Martin network.
Doc. No: 2YZA00666 Rev-BDate: Mar-18-2010
Ejection Seat System Hazards– Un-commanded / inadvertent initiation– Seat movement injuries– Unspent cartridges – post ejection
Ejection Seat SystemIngress/Egress & Life Support Systems
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F-35 Program InformationNON EXPORT CONTROLLED INFORMATION – RELEASABLE TO FOREIGN PERSONS
Important Notice: A hard copy of this document may not be the document currently in effect. The current version is always the version on the Lockheed Martin network.
Doc. No: 2YZA00666 Rev-BDate: Mar-18-2010
Fuel Tank Locations
Situational Awareness
35
F-35 Program InformationNON EXPORT CONTROLLED INFORMATION – RELEASABLE TO FOREIGN PERSONS
Important Notice: A hard copy of this document may not be the document currently in effect. The current version is always the version on the Lockheed Martin network.
Doc. No: 2YZA00666 Rev-BDate: Mar-18-2010
Any successful rescue operation involves expeditious entry to the cockpit area and removal of the pilot from the aircraft.
Rescue personnel shall be familiar with the systems and procedures described in the following slides to ensure quick and safe recovery of the pilot.
Cockpit Entry & Pilot Removal Procedures
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F-35 Program InformationNON EXPORT CONTROLLED INFORMATION – RELEASABLE TO FOREIGN PERSONS
Important Notice: A hard copy of this document may not be the document currently in effect. The current version is always the version on the Lockheed Martin network.
Doc. No: 2YZA00666 Rev-BDate: Mar-18-2010
The following slides present a recommended sequence to assure the successful cockpit entry, securing of the engine, pilot extraction and evacuation by first-responders during a mishap scenario.
Cockpit Entry & Pilot Removal Procedures
37
F-35 Program InformationNON EXPORT CONTROLLED INFORMATION – RELEASABLE TO FOREIGN PERSONS
Important Notice: A hard copy of this document may not be the document currently in effect. The current version is always the version on the Lockheed Martin network.
Doc. No: 2YZA00666 Rev-BDate: Mar-18-2010
The preferred approach path to the aircraft by rescue personnel should be towards the aircraft port side forward fuselage. This section of the aircraft contains the canopy locking and operating mechanisms and will allow for the most obstruction free route for pilot removal from the cockpit.
Preferred Approach PathCockpit Entry & Pilot Removal Procedures
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F-35 Program InformationNON EXPORT CONTROLLED INFORMATION – RELEASABLE TO FOREIGN PERSONS
Important Notice: A hard copy of this document may not be the document currently in effect. The current version is always the version on the Lockheed Martin network.
Doc. No: 2YZA00666 Rev-BDate: Mar-18-2010
Cockpit entry is normally accomplished utilizing the boarding ladder. However, use of the boarding ladder during rescue operations may not be advisable due to restrictions to mobility, balance, and leverage of rescue personnel. Rescue crews accessing the cockpit from ground level will require some form of ladder or boarding platform.
Cockpit Entry & Pilot Removal ProceduresCockpit Entry
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F-35 Program InformationNON EXPORT CONTROLLED INFORMATION – RELEASABLE TO FOREIGN PERSONS
Important Notice: A hard copy of this document may not be the document currently in effect. The current version is always the version on the Lockheed Martin network.
Doc. No: 2YZA00666 Rev-BDate: Mar-18-2010
WARNING: Do not cut within 3 inches of the edge of the transparency. Cutting of RDCTRLs may inadvertently activate TRS detonation.
WARNING: For a pilot initiated TRS activation, maintain a 300ft safety radius.
If pilot is incapacitated, canopy is locked and normal or manual means of entering cockpit are unavailable – canopy cutting may be required.
Cockpit Entry-Emergency Canopy OperationCockpit Entry & Pilot Removal Procedures
40
F-35 Program InformationNON EXPORT CONTROLLED INFORMATION – RELEASABLE TO FOREIGN PERSONS
Important Notice: A hard copy of this document may not be the document currently in effect. The current version is always the version on the Lockheed Martin network.
Doc. No: 2YZA00666 Rev-BDate: Mar-18-2010
Engine Bay Access for Ground Fire Extinguishing
Engine Bay Ventilation Inlet/Screen
Apply fire retardant– Down intakes and
Through engine bay ventilation inlet/screen
Situational Awareness
41
F-35 Program InformationNON EXPORT CONTROLLED INFORMATION – RELEASABLE TO FOREIGN PERSONS
Important Notice: A hard copy of this document may not be the document currently in effect. The current version is always the version on the Lockheed Martin network.
Doc. No: 2YZA00666 Rev-BDate: Mar-18-2010
Situational Awareness
42
F-35 Program InformationNON EXPORT CONTROLLED INFORMATION – RELEASABLE TO FOREIGN PERSONS
Important Notice: A hard copy of this document may not be the document currently in effect. The current version is always the version on the Lockheed Martin network.
Doc. No: 2YZA00666 Rev-BDate: Mar-18-2010
• Pilot recovery is #1• No pilot, No injuries - “Go Defensive”• Composite Fibers• Canopy hazards• Ejection system hazards
Takeaways
43
F-35 Program InformationNON EXPORT CONTROLLED INFORMATION – RELEASABLE TO FOREIGN PERSONS
Important Notice: A hard copy of this document may not be the document currently in effect. The current version is always the version on the Lockheed Martin network.
Doc. No: 2YZA00666 Rev-BDate: Mar-18-2010
Notes
• No matter where the plane goes down, FD and Security Forces will respond (SMEs)
• Minimum cordon area - 300 feet• Unknown weapons - evacuation 4000 feet• Bottom line - Life/Security of the aircraft!
44
F-35 Program InformationNON EXPORT CONTROLLED INFORMATION – RELEASABLE TO FOREIGN PERSONS
Important Notice: A hard copy of this document may not be the document currently in effect. The current version is always the version on the Lockheed Martin network.
Doc. No: 2YZA00666 Rev-BDate: Mar-18-2010
Questions?
