Differences Training

Question 1

Max Gross Weight

Answer 1

B4: 5350lbs
T2: 5512 lbs

Question 2

Max Continuous Torque

Answer 2

B4: 92.7& @ IAS > 40kts
T2: 81.3%

Question 3

Power affected by CG

Answer 3

B4: none
T2: window of differing Vne based on CG

Question 4

Engine temp start limits

Answer 4

B4: 750C Max continuous, 865C max transient 10 sec
T2: 750 Max continuous, 840C max transient 10 sec

Question 5

Max Continuous Power on FLI

Answer 5

B4: 9.6 to 10
T2: 8.2 to 10

Question 6

Torque limits above 40kts

Answer 6

B4: 92.7 %
T2: 81.3%

Question 7

Max takeoff power Delta Ng/N1

Answer 7

B4: 0% +1% for 5 seconds
T2: 0% +1% for 20 seconds

Question 8

Normal operation Nf/N2

Answer 8

B4: 349 - 418 RPM Nf
T2: 367 - 413 N2

Question 9

Transient Max Nf/N2

Answer 9

B4: 450 RPM for 5 seconds
T2: 440 RPM for 20 seconds

Question 10

Max Continuous Operation T4/TOT

Answer 10

B4: 849
T2: 905

Question 11

Max Takeoff Operation T4/TOT

Answer 11

B4: 915 (941 20 seconds)
T2: 949 (981 20 seconds)

Question 12

Engine Oil Press Max

Answer 12

B4: 9.8 bar
T2: limits vary with N1

Question 13

Max Engine Oil Temp

Answer 13

B4: 115C
T2: 117C

Question 14

Hover Wind Limit

Answer 14

B4: None
T2: OAT > 35C, I/OGE, relative wind 045-135, 5kts or greater, limited to 5 minutes

Question 15

GPS Systems

Answer 15

B4: G430
T2: 650/750

Question 16

EP: Relight in flight

Answer 16

1. Start selector - OFF
2. (T2 GENE - OFF)
3. Fuel Pump - ON
4. Start selector - ON
   - B4: relight Ng < 17%
   - T2: relight N1< 10%
5. (T2 GENE - ON)
6. Fuel pump - OFF

Question 17

EP: Smoke in Cabin, source not ident

Answer 17

B4: lists out each items to turn off/on
T2: Battery switch has an emergency shed function

Question 18

Torquemeter failure Ng/N1 table

Answer 18

Different numbers given in the table for Ng/N1 number to comply with in the event of a Torquemeter failure

Question 19

EP: Engine Fire

Answer 19

T2: included Battery - OFF after landing/crank if fire was on start

Question 20

EP: (GOV) yellow light

Answer 20

T2: adds Caution: failure of minor FADEC function can lead to constant Nr of 394

Question 21

EP: Loss of Hyd Press

Answer 21

B4: both servo circuits have the same HYD light
T2: each servo circuit has their own light, HYD 1 or HYD 2

Question 22

EP: Fuel Filter

Answer 22

T2: breaks down the clogging into 2 levels
Level 1: flashing light on idle or shutdown
Level 2: continuous light in flight

Question 23

T2 Instrument Lighting Circuit
(INST LIGHT) yellow light

Answer 23

One or both inst lighting circuits inop

CONTINUE FLIGHT
Note - dome light can be used for additional panel lighting

Question 24

T2 - (P2 OVHT) yellow light

Answer 24

Temp in heating ducts >90C

1. Temp button - press off
2. Check P2 and P2S on VEMD
3. Check light after one minute
   - light off CONTINUE FLIGHT
   - light on - close valve - CONTINUE FLIGHT - BUT if extermal vis is degraded LAND AS SOON AS POSSIBLE

Question 25

T2 (AVCS OFF/FAIL) LIGHT

Answer 25

Enviro system light

Question 26

Doors

Answer 26

T2
- now has sliding doors on both sides
- more sturdy
- indicator window for each door

Question 27

Pitot Heat

Answer 27

B4: push button in cockpit, rated for continuous use
T2: switch now in baggage compartment on “auto - on”

Question 28

Electrical Switches

Answer 28

B4: Battery, Direct Battery, Master Switch
T2: combinded all 3 into one switch

Question 29

T2 Emer Shed Switch

Answer 29

These items will remain on:
- Nr/N2 indicator
- map and dome lights
- FADEC engine start/stop switch
- intercom system
- transponder
- com1/nav/gps1
- instrumetn lighting circuit 2

Question 30

Vibration Mitigation

Answer 30

B4: 2 weights attached to bottom frame
T2: Active Vibration Control System (AVCS)

Question 31

Fuel Tank

Answer 31

B4: Crash resistant
T2: Crash Worthy

Question 32

Engine

Answer 32

B4: Arriel 2B1
T2: Arriel 2D

Question 33

FADEC

Answer 33

B4: FADEC
T2: EECU