S-92

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What are the buses powered by the #1 DC Converter?

#1 DC PRIMARY BATTERY UTILITY BATTERY HOLDUP

What AFCS mode can be coupled below 50 KIAS?

Radar Altimeter

When odes the Hydraulic Backup Isolation Valve automatically open and close?

Start: Closed >15% Ng, WOW; Open > 50% Nr Shutdown: Open < 15% Ng on last operating Engine; Closed: at 80% Nr and System is Normal then 50% Nr closes

Main Gearbox (MGB) Temperature Limits:

0-120 C-Continuous 120-130 C-Precatutionary 130 C-Maximum

Dual Engine TQ Limits:

100% Max Continuous* (86% >100 KIAS) 100% 30 min* 100% 5 min Takeoff* 120% 10-second Transient* *FADEC Controlled Limit Value

Max Starting TGT:

1000 degrees C

Maximum Baggage Load to Rear Ramp:

1000 lbs

OEI Ng Limits:

102.4% Max Continuous 102.9% OEI 2-min 103.7% 30 second Transient* *FADEC Controlled Limit Value

Ng Overspeed Protection comes on at:____

108.5% Ng

Main Rotor Speed Limits - POWER ON:

110% - Maximum 106-110% - Precautionary 104-106% - Normal Dual Engine 100-106% - Normal OEI 95-104% - Precautionary Dual Engine 95-100% - Precautionary Range OEI 95% - Minimum 90% - Transient Minimum OEI 80% - Transient at Touchdown During OEI Landing

Main Rotor Speed Limits - POWER OFF:

110% - Maximum 95% - Minimum, "LOW ROTOR" aural alert sounds 80% - Transient

360 Hovering Turn in Less Than ____ seconds are Prohibited.

12 seconds

Max Airspeed One or Both SAS Inop:

120 knots

Max Airspeed with Hyd Boost Inop:

120 knots

Max Airspeed with one Pri-Flight Servo Inop:

120 knots

Max OEI Airspeed:

120 knots

Vne Power OFF:

120 knots (If Vne power ON is less than 120, the lower Vne shall apply for power off as well)

OEI TQ Limits:

120% Max Continuous* 120% OEI 2-min* 141% 30 second Transient* 156% 5-second Transient *FADEC Controlled Limit Value

Engine Oil Temperature Limits:

132 C - Max Continuous 132-149 C - 15 minute 149 C - Max Allowable

Max enroute density altitude:

15,000 feet Density Altitude

Max Airspeed with APU Operating:

150 knots

Minimum Operating Weight:

16,200 lbs

Max Airspeed with Landing Gear Down/Transient:

165 knots

Vne Power ON:

165 knots

Maximum Self Capacity:

300 lbs

Max Airspeed for Rearward/Tailwind Hover:

35 knots

Max Airspeed for Sideward/Crosswind Flight:

35 knots

CAT A Takeoffs and Landings are limited to ____knots of crosswind component or less.

35 kts

Max Groundspeed for Brake Application:

35 kts

Max Groundspeed for Taxi Operations:

35 kts

Main Gearbox (MGB) Pressure Limits:

35 psi - Minimum 45-70 psi - Continuous 70-130 psi - Precautionary 130 psi - Maximum

Avoid prolonged operations in Np/Nr ranges:

36%-49% 56%-67%

Max Airspeed with Emergency Flotation System Armed:

80 knots

Max Airspeed Activation L/G Blowdown:

90 knots

Dual Engine TGT (T4.5) Limits:

935 C Max Continuous 988 C 30 min 995 C 5 min Takeoff* 1003 C 12-second Transient *FADEC Controlled Limit Value

Fuel Anti-Icing Additives are Required at Temperatures below:

-20 degrees C

What is the ambient Temperature Range?

-40C to ISA+35C

What sub-modes are available from the PFD display?

-Full -Arc -Hover -Comp -CATA

Where are the only two circuit breakers not available to the pilots from the cockpit?

1) 7.5 amp in nose compartment 2) 4 amp inside the external power door

What is Required Equipment For Flight?

1. APU 2. Two DCU 3. Four MFDs configured as follows: a. PFD mode both outboard displays b. EICAS mode on one inboard 4. AFCS a. Day.Night, VFR PSAS/AP1 or PSAS2/AP2, cyclic trim release b. IFR-PSAS1 and PSAS2, AP1 & AP2, cyclic trim & Rudder trim 5. Two Primary AC Gen (IFR) 6. All Standby Instruments (IFR) 7. The applicable operator's manual.

Slope Limitations:

10 degrees-Nose Up/Down 13 degrees- Left/Right side slope

Coupled flight below _____feet AGL will be in VMC.

100 feet AGL

Do not apply engine power above ground idle until ENG Oil Pressure is below:

100 psi

Day or night VFR with certain PSAS and/or AP components inop:

165 kts Vne = PSAS1 and PSAS2, AP1 or AP2, ATT Mode, cyclic and rudder trim 165 kts Vne = PSAS1 and PSAS2, AP1 and/or AP2, SAS Mode, cyclic and rudder trim 120 kts Vne = PSAS1 or PSAS2, AP1 and AP2, ATT Mode, cyclic and rudder trim 120kts Vne = PSAS1/AP! or PSAS2/AP2, SAS Mode, functional cyclic trim release

Height to top of TR disk:

17 feet, 11 inches

Maximum Seating of ____ Passengers.

19

Starter Motoring Limits at ALL Ambient Temperatures:

2 min - Motoring 5 min - OFF 2 min - Motoring 30 min - OFF for cooling Repeat Cycle

Mimimum Flight Crew:

2 pilots

Landing Gear Dimension:

20'4" Length (Nose to Main) 10'5" Width (Main to Main)

Engine Oil Pressure:

20-30 psi = Min Idle 30-100 psi = Continuos 100-120 psi = Max (5 min) 5 psi = Max Fluctuation

Above 120 KIAS minimum AGL altitude for coupled operations:

200 feet AGL

When coupled below _____ feet AGL the pilot will monitor the flight controls and take action in the event of an excessive rate of descent.

200 feet AGL

Max T/O Gross Weight (Internal Load):

26,500 lbs

Max T/O Gross Weight (External Load):

28,300 lbs

Maximum Tie-Down Ring Limit is:

5,700 lbs per ring

Max Airspeed after inadvertent Float Deployment:

50 KIAS - Climb 55 KIAS - Level Flight 60 KIAS - Decent/Auto

Below 120 KIAS minimum AGL altitude for coupled operations:

50 feet AGL

What is the total capacity of the aircraft FUEL system?

5119 lbs (764 gal)- Pressure Refuel 4770 lbs (712 gal)-Gravity Refuel 32 lbs (4.8 gal)-Un-useable Fuel

Main Rotor Dimensions:

56 feet, 4 inches

How many DC buses are there? List them:

6 DC buses #1 DC PRIMARY DC ESSENTIAL BATTERY BATTERY UTILITY BATTERY HOLDUP #2 DC PRIMARY

Max Groundspeed for Takeoff/Landing:

65 kts (50 kts Temporary Restriction due to improper heat treating of the gear locking claws during manufacture by 3rd party vendor)

Total Length:

68 feet, 6 inches

Max Allowable Cabin Floor Loading:

75 lbs/sq ft or 200 lbs/sq ft(heavy duty floors)

TGT OEI:

988 C - Max Continuous (MCP Limiter) 1006 C - 2 min (2-minute Limiter) 1049 C - 30 sec (30-second Limiter)

OEI TGT (T4.5) Limits:

988 C Max Continuous 1006 C OEI 2-min* 1049 C 30 second Transient* *FADEC Controlled Limit Value

Ng Dual Engine Limits:

99.9% - Max Continuous 101.5% -30 min 102.9% - 5 min Takeoff (Limiter) 103.7% - 12 second Transient

Dual Engine Ng Limits:

99.9% Max Continuous 101.5% 30 min 102.9% 5 min Takeoff* 103.7% 12-second Transient *FADEC Controlled Limit Value

Back-To-Back Starter Limits:

Ambient Temperatures > +15C 2 consecutive starts 5 min-OFF (cooling) 2 consecutive starts 30 min-OFF (cooling) Repeat Cycle Ambient Temperatures </= +15C 4 consecutive starts 15 min-OFF (cooling) 4 consecutive starts 30 min-OFF (cooling) Repeat Cycle

Limits with Low Fuel Light(s) Illuminated:

Avoid steady state pitch attitudes in excess of 10 degrees nose up and lower than 5 degrees nose down.

What Systems are driven by the #2 hydraulic pump?

Boost #2 SAS Actuators #2 Main Rotor Servos #2 Tail Rotor Servo

When can you operate CROSS FEED?

Category A: Emergencies Only Category B: Cruise Flight Only

Rotor Brake Limits:

Engines Operating limited to 1 or both engines at IDLE Both Engines must be OFF before applying Rotor Brake 40% Nr or below for NORMAL application 105% Nr or below (Both Engines OFF) for EMERGENCY application

This aircraft is Certified IAW:

FAA Part 29, CAT-A and CAT-B

Pre-Heat must be used for all starts when:

OAT is -25C or below > 1 hour

Aerobatic Maneuvers Are:

Prohibited

Practice Touchdown Autorotations are:

Prohibited

What is the Caution associate with the weather radar system operations?

The weather radar has a WOW override that forces the system into standby when the aircraft is on the ground. Unless STBY or OFF are selected, the weather radar will radiate as soon as the helicopter lifts to a hover. If an active radar mode is selected, ensure all people are at least 100 feet away from the forward 270 degree arc of the aircraft prior to takeoff.

When the APU as the sole source of AC Power in flight results in Auto Shed of:

WARM1 Air W-Windshield Anti-Ice (Pilot's side recoverable) A-Anti-Vibration Control (AVC) R-Rotor Ice Protection System (RIPS) M1-Mats, #1 Engine Inlet Anti-Ice Mat Air- Air Conditioner(s)


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