T-6B

*1. PCL - OFF; or STARTER switch - AUTO/RESET

*1. PCL-Off

*2. Firewall Shutoff Handle- Pull

*3. Emergency Ground Egress- As Required

*1. ISS mode selector - SOLO

*2. Ejection seat pin - Install (BOTH)

*3. PARKING BRAKE - As required

*4. Canopy - Open

• IF CANOPY CANNOT BE OPENED OR SITUATION REQUIRES
• RIGHT SIDE EGRESS:
• *5. CFS handle - Rotate and pull (BOTH)

• *6. Upper fittings, lower fittings, and leg restraint garters - Release
• (BOTH)

*7. BAT, GEN, and AUX BAT switches - OFF

*8. Evacuate aircraft

*1. PCL - IDLE

*2. BRAKES - AS REQUIRED

*1. AIRSPEED - 110 KNOTS (MINIMUM)

*2. PCL - AS REQUIRED

*3. EMER LDG GR HANDLE - PULL (AS REQUIRED)

*4. Flaps - As required

*1. ZOOM/GLIDE - 125 KNOTS (MINIMUM)

*2. PCL - OFF

*3. INTERCEPT ELP

*4. Airstart - Attempt if warranted

IF CONDITIONS DO NOT WARRANT AN AIRSTART:

*5. FIREWALL SHUTOFF handle - Pull

*6. Execute Forced Landing or Eject

*1. PCL - OFF

*2. STARTER SWITCH - AUTO/RESET

*3. PCL - IDLE, ABOVE 13% N1

*4. Engine instruments - Monitors ITT, N1, and oil pressure

IF AIRSTART IS UNSUCCESSFUL:

*5. PCL - OFF

*6. FIREWALL SHUTOFF handle - Pull

*7. Execute Forced Landing or Eject

*1. PCL - MID RANGE

*2. PMU SWITCH - OFF

*3. PROP SYS CIRCUIT BREAKER (left front console) - PULL,

IF NP STABLE BELOW 40%

• *4. PCL - As required
• IF POWER IS SUFFICIENT FOR CONTINUED FLIGHT:

• *5. PEL - Execute
• IF POWER IS INSUFFICIENT TO COMPLETE PEL:

*6. PROP SYS circuit breaker - Reset, as required

*7. PCL - OFF

*8. FIREWALL SHUTOFF handle - Pull

*9. Execute Forced Landing or Eject

*1. PCL - Slowly retard below stall threshold

*2. DEFOG switch - ON

*3. PCL - Slowly advance (as required)

IF POWER IS SUFFICIENT FOR CONTINUED FLIGHT:

*4. PEL - Execute

IF POWER IS INSUFFICIENT TO COMPLETE PEL:

*5. PCL - OFF

*6. FIREWALL SHUTOFF handle - Pull

*7. Execute Forced Landing or Eject

*1. PCL - IDLE

*2. CONTROLS - NEUTRAL

*3. ALTITUDE - CHECK

*4. Recover from unusual attitude

IF FIRE IS CONFIRMED:

*1. PCL - OFF

*2. FIREWALL SHUTOFF HANDLE - PULL

IF FIRE IS EXTINGUISHED:

*3. Forced Landing - Execute

IF FIRE DOES NOT EXTINGUISH OR FORCED LANDING IS IMPRACTICAL:

• *4. Eject (BOTH)
• IF FIRE IS NOT CONFIRMED:

*5. PEL - Execute

*1. PCL - Minimum necessary to intercept ELP; avoid unnecessary PCL movements

*2. PEL - Execute

IF ONLY AMBER OIL PX CAUTION ILLUMINATES:

*1. Terminate maneuver

*2. Check oil pressure; if oil pressure is normal, continue operations

• IF RED OIL PX WARNING ILLUMINATES AND/OR AMBER OIL
• PX CAUTION REMAINS ILLUMINATED FOR 5 SECONDS:

• *3. PCL - Minimum necessary to intercept ELP; avoid unnecessary
• PCL movements

*4. PEL - Execute

*1. PEL - Execute

*1. PCL - Advance

*1. GREEN RING - PULL (AS REQUIRED)

*1. EJECTION HANDLE - PULL (BOTH)

*1. Airspeed - 125 KIAS prior to extending landing gear

*2. EMER LDG GR handle - Pull (as required)

*3. Airspeed - 120 KIAS minimum until intercepting final; 110 KIAS minimum on final

*4. Flaps - As required

*1. Turn to nearest suitable field

*2. Climb or accelerate to intercept ELP

*3. Gear, flaps, speed brake - UP

1. Hydraulic pressure – Check

2. Electrical systems – Check

3. Fuel quantity/balance – Check

4. OBOGS – Check flow indicator for normal operation (BOTH)

5. Engine instruments – Check

6. Pressurization – Check

1. Loose items – Stowed (BOTH)

• 2. Engine instruments – Check
• (Verify caution and warning messages are extinguished)

3. Fuel balance – Check less than 50 pounds

1. DEFOG switch – OFF

2. Engine instruments – Check

3. Gear – DOWN (press down firmly) (BOTH) (Check three green annunciators illuminated)

• 4. Brakes – Check, as required
• (Verify positive pressure by actuating toe brakes.)

5. Flaps – As required (BOTH)

6. Speed brake – Verify retracted

An emergency shall be declared and a landing accomplished at the nearest suitable landing area considering the severity of the emergency, weather conditions, field facilities, ambient lighting, and command guidance.

Emergency conditions are less urgent and, although the mission is to be terminated, the degree of the emergency is such that an immediate landing may not be necessary.

Inverted stalls

Inverted spins

Aggravated spins past two turns

Spins with PCL above idle

Spins with landing gear, flaps, or speed brake extended

Spins with PMU off

Spins below 10,000 feet pressure altitude

Spins above 22,000 feet pressure altitude

Abrupt cross-controlled (snap) maneuvers

Aerobatic maneuvers, spins, or stalls with a fuel imbalance greater than 50 pounds between wings

Tail slides

Clean +7.0 to -3.5 G's

Gear and flaps extended +2.5 to 0.0 G's

• Clean +4.7 to -1.0 G's
• Gear and flaps extended +2.0 to 0.0 G’s
• For uncoordinated rolling maneuvers initiated at -1 G, the maximum bank angle change is 180 degrees.

Maximum ramp weight - 6950 pounds

• Maximum takeoff weight - 6900 pounds
• Maximum landing weight - 6900 pounds

Maximum zero fuel weight - 5850 pounds

Maximum weight in baggage compartment - 80 pounds

Maximum crosswind component for dry runway - 25 knots.

Maximum crosswind component for wet runway - 10 knots.

Maximum crosswind component for icy runway - 5 knots.

Maximum tailwind component for takeoff - 10 knots.

Starter duty cycle (start attempts and/or engine motoring) is limited to four 20-second cycles as follows:

First - Motor 20 seconds then, 30-second cooling period.

Second - Motor 20 seconds then, 2-minute cooling period.

Third - Motor 20 seconds then, 5-minute cooling period.

Fourth - Motor 20 seconds then, 30-minute cooling period.

Sustained propeller operation on the ground between 62 and 80% NP is prohibited to prevent damage from ground resonance.

• 1. PFD – Check (BOTH)
• 2. Altimeters – Set (BOTH)
• 3. DEFOG switch – As required
• 4. MASTER ARM switch – As required
• 5. Vent control lever – As required

• 1. OBOGS – Check flow indicator for normal operation
• (BOTH)
• 2. DEFOG switch – As required
• 3. Vent control lever – As required
• 4. Pressurization system – Check
• NOTE
• If readings other than 3.6±0.2 psi are
• encountered at or above 18,069 feet MSL,
• notify maintenance after landing.

With canopy defog ON, expect an increase inITT of up to 40 °C for a given PCL setting.Cockpit noise will also increase. Performancewill decrease with defog on. A DUCTTEMP indication is likely at climb or cruisepower with canopy defog ON and cockpittemperature controller set to AUTO orMANUAL HOT. Refer to EnvironmentalSystems Duct Overtemp procedure in SectionIII.

• 1. EICAS display – Check (BOTH)
• 2. PROBES ANTI-ICE switch – ON
• 3. Transponder – Mode to ALT
• 4. Landing/taxi light – ON
• 5. Nose wheel steering – Off

• 131 (20 sec) (8)
• 8. Torque at 131% is a materials limit above which damage to the engine may occur. Torque above 102% is indicative of a system malfunction

• Max/TO 820
• IDLE 750
• Start 1000 (5 sec)
• Transient 870 (20 sec)

• Max/ TO 104
• IDLE: 60 Min (ground)/ 67 Min (flight)
• Transient 104

• TO/MAX 100
• Transient 102 (20 sec) 110 (3)
• 3. Permissible at any power setting for completion of in-flight emergency.

• TO/MAX 90-120
• IDLE 90 minimum
• START 200
• Transient 40-130(5)
• 5. Operation in this range permitted only during aerobatics or spins, and 15 to 40 psi for 5 seconds with PCL at IDLE.

• TO/Max 10 to105
• Idle 10 to 105 (flight), -40 to 105 (ground)
• Start -40 minimum
• Transient 106-110 (10 minutes, ground ops only below 20% torque)

Zoom capability at 200 knots will vary from 603 to 915 feet of altitude gained. Zoom capability at 250 knots will vary from 1180 to 1576 feet of altitude gained.