Emergency Responder Familiarization Training F-35 …

FOR REFERENCE USE ONLY

Emergency Responder Familiarization TrainingF-35 LIGHTNING II

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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

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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

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F-35A Lightning II Conventional Take-Off and Landing (CTOL) Aircraft

General Aircraft DescriptionIntroduction

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Aircraft hazards include the following:• Airframe Hazards• Noise Hazards• In-Wash and Out-Wash Hazards• Aircraft Material Hazards

Aircraft Hazards

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• Sharp edges• Operating hinged areas• Caution zones

The following are airframe hazards to be aware of:

Airframe HazardsAircraft Hazards

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Airframe HazardsAircraft Hazards

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Airframe HazardsAircraft Hazards

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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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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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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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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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Explosives

Transparency Removal System (TRS)– Flexible Linear Shaped Charge (FLSC)– Rapid Deflagrating Cord Transfer Lines (RDCTL)

Aircraft Material HazardsAircraft Hazards

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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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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

20

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Transparency Removal System (TRS)Ingress/Egress & Life Support Systems

Rapid Deflagration Cord Transfer Line (RDCTL) example.

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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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Canopy CuttingIngress/Egress & Life Support Systems

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Transparency Removal System (TRS)Ingress/Egress & Life Support Systems

24

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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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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

26

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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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Simplified Combined Harness– Parachute– Seat restraints

Quick Release Box

Ejection Seat SystemIngress/Egress & Life Support Systems

28

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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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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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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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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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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

33

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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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Fuel Tank Locations

Situational Awareness

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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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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

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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

38

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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

39

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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

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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

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Situational Awareness

42

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• Pilot recovery is #1• No pilot, No injuries - “Go Defensive”• Composite Fibers• Canopy hazards• Ejection system hazards

Takeaways

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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

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Doc. No: 2YZA00666 Rev-BDate: Mar-18-2010

Questions?