Mk.1 to Mk.9
      Mk.10
      Mk.11
      Mk.12
      Mk.14
      Mk.15
      Mk.16 high-speed
      Mk.16 low-speed
      RetroFit / Upgrades

Overview

The JPATS (Joint Primary Aircraft Training System) is designed to train students in basic flying skills, and is common to the U.S. Air Force and Navy. The US16LA-1/2 lightweight ejection seat is designed for training aircraft. It optimises the pilot field of view, improves comfort and pilot efficiency, and provides increased reliability and maintainability. With the Mk.16 lightweight low speed seat, ejection performance is optimised throughout the escape envelope, from zero height at zero velocity in a near level attitude through to 370 knots. It is designed to accomodate a very wide, size and weight range, including female aircrew. 

Specifications


Specifications
US16LA - JPATS
 
 
Operating ceiling
50 000+ ft (15,250 m) (aircraft limit 31 000 ft)
Minimum height/speed
Zero/zero in near level attitude
Crew boarding mass range
62.3 to 123.0 kg
Crew size range
JPATS multi-variate body size cases 1 to 7
Maximum Speed for ejection
600 KIAS (aircraft limit 316 KIAS)
Parachute type
GQ Type 5000
Parachute deployment
Cartridge initiated
Auxiliary parachute
22 in.
Drogue parachute
5 ft
Drogue deployment
Cartridge initiated and deployed
Harness type
Combined, torso
Ejection seat operation type
Ejection guns and underseat rocket motor
Ejection gun
Twin
Ejection initiation
Handle on seat pan initiates gas operated seat
 
firing system
Automatic back-up unit
No, manual override
Electronic sequencer
No
Barostatic time-release unit
Yes + g-restrictor, cartridge initiated
Timers
Time delays in sequencing system
Seat adjustment
Up/down actuator operated 28 Vdc
Arm restraints
No
Leg restraints
Yes, two garters
Oxygen supply
Bottled emergency oxygen
Personal survival pack (PSP)
Yes + automatic deployment
Aircrew services
Connection to emergency oxygen supply
Command ejection
Yes, via Interseat Sequencing System
Canopy jettison
No
Canopy fracturing system
Yes
Interseat Sequencing System (ISS)
Yes

How it works

Seat firing handle pulled causing seat initiation cartridge to fire
Interseat sequencing system initiated initiated
Harness retraction unit operated
Primary cartridge fires, bottom latches engage, top latches disengage seat
   rises up rails
- Canopy fracturing MDC initiated
- Aircraft services disconnected
- Leg restraint lines draw back and restrain aircrew’s legs
- Secondary cartridges fire as seat rises

Multi-purpose initiators fire
- Underseat rocket motor fires
- Leg restraint lines become taut and rivets shear, freeing lines from floor brackets
- Emergency oxygen supplied to aircrew
- Barostatic time-release unit (BTRU) mechanism set to operate when altitude 
  and g-load conditions are satisfactory
- Manual override handle lock released
- Drogue and bridle deployed, stabilise and decrease velocity of seat

Barostatic time release unit (BTRU) monitors the altitude and g-load conditions
Above 15 000 ft
- Seat falls, stabilised by drogue
- Emergency oxygen supply continues

Below 15 000 ft but above 8000 ft
 - Seat falls, stabilised by drogue
 - Emergency oxygen supply continues
 - G-restrictor prevents operation of time-release mechanism until g-load
    is satisfactory

Below 8000 ft
 - Time-release mechanism operates, cartridge fires (If BTRU fails manual
    deployment also available by pulling manual override handle)
 - Cartridge of headbox deployment unit fires
 - Parachute container (headbox) deploys
 - Drogue bridle released
 - Sear of time-delay unit (TDU) operated

After delay, TDU fires
- Upper and lower harness to seat locks released
- Leg restraint lines released
Parachute container (headbox) separates from main parachute and is pulled clear by auxiliary parachute
Sticker straps momentarily hold aircrew in seat
Main parachute develops, lifts aircrew and survival pack from seat and pulls sticker clips from clips causing aircrew and seat to diverge
Aircrew and survival pack (attached to aircrew) separate from seat
Pulling survival pack from seat causes automatic deployment unit (ADU) cartridge to fire (if seat to AUTO)
- If set to MANUAL aircrew pulls handle to manually deploy
ADU operates, lowers survival pack on drop line below aircrew
Personal locator beacon operates, automatic liferaft inflation unit (ALIU) armed
Normal parachute descent follows

Variants

No variants available

US16LA -  T-6
                     US16LA T-6