RFM

Question 1

max take off and landing weight

Answer 1

11700lbs

Question 2

VNE

Answer 2

155

Question 3

VNE power off

Answer 3

136

Question 4

Maximum airspeed for main landing gear down or in transit (SOP?)

Answer 4

130 KIAS 110KIAS

Question 5

Maximum airspeed for windshield wiper operation

Answer 5

141 KIAS

Question 6

Maximum groundspeed for landing, takeoff, or taxi

Answer 6

54 knots

Question 7

Maximum groundspeed for brake application

Answer 7

34 knots

Question 8

ALTITUDE LIMITS
Takeoff and landing

Answer 8

Category A: 5,000 feet density altitude

Question 9

ALTITUDE LIMITS
Enroute

Answer 9

15,000 feet density altitude.

Question 10

AMBIENT TEMPERATURE LIMITS

Answer 10

-34°C to ISA plus 37°C not to exceed 49°C

Question 11

360° hovering turn in less than

Answer 11

12 seconds prohibited

Question 12

Flight in known icing conditions is?

Answer 12

prohibited

Question 13

Maximum airspeed for sideward flight or crosswind hover is

Answer 13

35 knots

Question 14

Maximum airspeed for rearward flight or tailwind hover is

Answer 14

35 knots

Question 15

With usable fuel per tank indicating 80 lbs or less, avoid sustained nose-down pitch attitudes in excess of?

Answer 15

5° nose low

Question 16

Fuel cross-feed operations limited to:

Answer 16

Category A - emergency operation only

Question 17

Operation vs. allowable wind limited to ____ knots sideward and rearward flight

Answer 17

35

Question 18

IFR lateral CG limits are ___ inches left or right

Answer 18

3.5

Question 19

Flight director shall not be coupled below ___ KIAS

Answer 19

60

Question 20

The Pulselite System should not be operated

Answer 20

in the clouds at night or on the
ground while in close proximity to other aircraft.

Question 21

EFIS stands for

Answer 21

electrical flight Instrument Limits

Question 22

Maximum airspeed for inflation of the emergency flotation gear

Answer 22

75 KIAS Landing gear must be down before float inflation

Question 23

Maximum airspeed with emergency flotation gear inflated

Answer 23

75 KIAS

Question 24

Maximum water contact speed with emergency flotation system inflated is

Answer 24

33 knots

Question 25

Maximum demonstrated airspeed for sideward flight or crosswind hover

Answer 25

20 knots

Question 26

Maximum pressure altitude with emergency flotation gear inflated is

Answer 26

5,000 feet

Question 27

ENGINE TORQUE LIMITS: 5-Minute takeoff and maximum continuous limit, dual-engine

Answer 27

104% Torque

Question 28

ENGINE TORQUE LIMITS: 30-Second limit, single engine

Answer 28

135% Torque

Question 29

ENGINE TORQUE LIMITS: 2-Minute limit, single engine

Answer 29

127% Torque

Question 30

ENGINE TORQUE LIMITS: Maximum Continuous, single engine

Answer 30

115% Torque

Question 31

ENGINE TORQUE LIMITS: Maximum transient 20 seconds

Answer 31

160% Torque

Question 32

N1 (GAS PRODUCER) SPEED LIMITS

Answer 32

TWO ENGINE OPERATION: 100.0% N1 – 5-Minute takeoff power limit, dual engine Deleted 97.8% N1 - Maximum continuous power, dual engine OEI OPERATION: 103.9% N1 - 30-Second power, single engine 100.5% N1 - 2-Minute power, single engine 99.4% N1 - Maximum continuous power, single engine TRANSITIONAL OPERATION, GROUND TO FLIGHT IDLE: 53-62% N1 - Avoid prolonged operation in this range. TRANSITIONAL OPERATION, ROTOR RUNUP OR SHUTDOWN: 87.0-90.5% N2 - Avoid prolonged operation in this range.

Question 33

N2 (POWER TURBINE) SPEED LIMITS

Answer 33

Maximum, power-on or off: 108.5% N2 Minimum, power off: 90.5% N2 Transient Maximum, power-on: 109% N2 for 20 seconds Transient Maximum, power-off: 115% N2 for 20 seconds Transient Minimum: 68% N2 for 20 seconds while executing an OEI landing

Question 34

T5 (POWER TURBINE) INLET TEMPERATURE LIMITS Steady State Limits

Answer 34

TWO ENGINE OPERATION: 930°C - 5-Minute takeoff power limit, dual engine 893°C - Maximum continuous power, dual engine OEI OPERATION: 996°C - 30-Second power, single engine 944°C - 2-Minute power, single engine 926°C - Maximum continuous power, single engine

Question 35

T5 (POWER TURBINE) INLET TEMPERATURE LIMITS Starting and Shutdown

Answer 35

750°C - no time limitation 750°C to 840°C - limited to 10 seconds

Question 36

DIGITAL ENGINE CONTROL UNIT (DECU) LIMITS

Answer 36

Before takeoff, the following DECU conditions must be met: 1. Both engine DECUs must be free of all faults, Total, Degraded, and Minor, as read on the IIDS display. 2. Both throttles must be in the FLY po sition with pilo t’s and copilot’s blue ENG CONTROL lights out.

Question 37

ENGINE BARRIER FILTER LIMITS

Answer 37

Engine operations with the barrier filters not in stalled is prohibited. 1. With PWR ASSURANCE advisory light on the IIDS and the CHECK condition light on the BARRIER FILTER panel latched prior to or during flight (between 3 and 5 segment lights): Normal operations are permitted if; a ground or in-flight Power Assurance check is performed and the power and T5 margin results for both engines are at least zero. Maintenance shall be performed prior to the next day's flight. 2. With CHECK BAR FILT caution light on the IIDS and the MAINT condition light on the BARRIER FILTER panel latched prior to flight (between 6 and 8 segment lights): Maintenance shall be performed prior to flight. 3. With CHECK BAR FILT caution light on the IIDS and CAUT cond ition light on the BA RRIER FILTER panel latched prior to flight (9 or 10 segment lights): Maintenance shall be performed prior to flight. 4. A power assurance check must be p erformed when a ne w, cleaned, or used filter element is installed.

Question 38

ENGINE OIL TEMPERATURE LIMITS

Answer 38

Maximum: 115°C (239°F)

Question 39

ENGINE OIL PRESSURE LIMITS

Answer 39

In Flight: Precautionary 87 to 142 PSI with Oil Temp < 4ºC Normal 29 to 87 PSI Precautionary 24 to 29 PSI Minimum 24 PSI, only at N1 less than 85% Ground Idle: Minimum 10 PSI

Question 40

TRANSMISSION LIMITS

Answer 40

Operation above 104% torque on one engine (200% total torque), 100.0% N1, or 930°C T5 is reserved for actual emergencies, inadvertent transient excursions, or, as artificially biased indications, with the OEI training provision.

Question 41

TORQUE LIMITS Dual-Engine Operation

Answer 41

100% Torque per engine – 5-Minute takeoff and maximum continuous limit NOTE Takeoff torque may exceed 100% on one engine to a maximum of 104% provided that the torque on the other engine is less than 96% and the sum of the individual torque values does not exceed 200%. 115% Torque per engine – 10-Second transient

Question 42

TORQUE LIMITS OEI Operation

Answer 42

136% Torque - 2 1/2-Minute limit 128% Torque - Maximum Continuous 150% - 5-Second transient

Question 43

TRANSMISSION OIL TEMPERATURE LIMITS

Answer 43

Maximum: 135°C Minimum: -20°C

Question 44

TRANSMISSION OIL PRESSURE LIMITS

Answer 44

Maximum: 120 PSI Minimum: 20 PSI

Question 45

ROTOR LIMITS POWER OFF

Answer 45

Maximum: 115% Nr Minimum: 91% Nr Transient (Minimum): 74% Nr Transient (Minimum): 68% Nr at touchdown while executing an autorotative landing Transient (Maximum): 121% Nr

Question 46

ROTOR LIMITS POWER ON

Answer 46

Maximum: 108% Nr; except 109% transient operation for 20 seconds Minimum: 106% Nr (dual-engine operation) Minimum: 100% Nr (one engine inoperative) Transient: 91% Nr Transient 68% at touchdown while executing an OEI landing One engine operation up to best rate of climb speed, 100% to 108% Nr One engine operation above best rate of climb speed, 106% Nr to 108% Nr

Question 47

TCAS

Answer 47

TRAFFIC COLLISION AVOIDANCE SYSTEM

Question 48

SOP landing