Reading...
Play button
Play button
Use LEFT and RIGHT arrow keys to navigate between flashcards;
Use UP and DOWN arrow keys to flip the card;
H to show hint;
A reads text to speech;
41 Cards in this Set
- Front
- Back
|
MTOW
Min. Weight Max ceiling |
MTOW--3780 lb
Min Weight--2284 lb Ceiling: 20,000 |
|
|
Fuel:
Gallons Endurance Range gph |
107.3 Gallons
3+15 395nm 33 gph |
|
|
Engine type
MAX t/o power (shp) Continuous (shp) weight of engine |
Turbomeca Arrius 2f
MTO power 504 shp MC power 449 shp 262 lb |
|
|
NR
Max Caution Normal Caution Minimum Rotor Brake |
NR RPM
Max 447 Caution 415-447 Normal 390-415 Caution 340-390 Minimum 340 Rotor Brake 150 |
|
|
FLI-Values
Max Continuous Takeoff Power Range Max Takeoff Rating Max Transient Rating |
FLI-Values
Max Continuous 9.6 Takeoff Power Range 9.6-10 Max Takeoff Rating 10 Max Transient Rating 10.8 (5 seconds) |
|
|
p2 bleeds prohibited?
|
above the max continuous rating (Ng or T4)
|
|
|
Main Transmission Limits (torque)
MCR takeoff with IAS < Vy max takeoff max transient |
Main Transmission Limits (torque)
MCR 97% takeoff with IAS < Vy 97-103% max takeoff 103% max transient 110% |
|
|
Starter Limits
|
no more than 3 consecutive failed starts.
After third attempt wait 30 minutes. |
|
|
Nf
Minimum Caution Normal Max Continuous Transient |
Nf
Minimum 365 Caution 365-373 Normal 373-422 Max Continuous 422 Transient 447 |
|
|
Ng
minimum stabilized max continuous takeoff range max takeoff max transient |
Ng
minimum stabilized 63% max continuous -1.5% takeoff range -1.5-0% max takeoff 0% max transient +2.6% |
|
|
T4
Starting --Max Continuous --Transient Flight --Max Continuous --Takeoff range --Takeoff transient --Max Transient |
T4
Starting --Max Continuous 800 C --Transient 870 C 010 sec Flight --Max Continuous 830 C --Takeoff range 830-870 C --Takeoff transient 870 C --Max Transient 900 C 5 sec |
|
|
Oil Temp
--Caution Range --Max Oil PSI --Min --Max |
Oil Temp
--Caution Range -10c -- 10c --Max 110c Oil PSI --Min 1.7 bar Ng > 70% --Max 15 bar |
|
|
Electrical System
--Battery --Generator --Max Voltage --Max Current --Continuous Transient |
Electrical System
--Battery 15ah Nicad battery --Generator 28 vdc generator --Max Voltage 31.5v --Max Current 150A --Continuous Transient 240A transient 2 minutes |
|
|
Hydraulics
--how much PSI (bar) --how many servos |
Hydraulics
--how much PSI (bar) 37 bar 536psi --how many servos 3 main servos |
|
|
Battery Temperature
--caution --max |
Battery Temperature
--caution 60C --max 71C |
|
|
When is prist required?
|
Prist < -15C
|
|
|
Cabin or bag compartment load?
--lb/spft Useful load |
Cabin or bag compartment load?
--62.5 lb/sqft Useful load--970lb |
|
|
Engine Oil Capacity
|
3-4.9 liters
|
|
|
Temperature limit for AC use
Performanc adjustment for AC use |
Temp limit for AC use:
ISA + 35C or 50C reduce hover perfomanc in section 5 by 20 Kg. VEMD doesn't take into account use of AC. Reduce climb 20 fpm. |
|
|
Vne
--power on --power off |
Vne
--power on 150 (-3kt/1000 PA) --power off 120 (-3kt/1000 PA) |
|
|
Flight is Forbidden (4)
|
1. Aerobatic Maneuvers
2. Flight in Freezing Rain 3. Flight in Icing conditions 4. In flight, intentionally shutting off VEMD |
|
|
Minimum Aircraft Temp
Maximum Aircraft Temp |
Min Temp -30 C
Max Temp ISA +35 limited to 50 C |
|
|
Slopes
--Nose up --Nose down --Side |
Slopes degrees
--Nose up 10 --Nose down 06 --Side 08 |
|
|
Hydraulics Capacity
Total Resevoir Pump PSI/bar Over PSI/bar Low PSI/bar |
Hydraulics Capacity
Total .58 gal Resevoir .48-.58 gal Pump 536.5 PSI 37bar Over 797.5PSI 55bar Low 362PSI 25bar |
|
|
Cool down at idle?
|
60 seconds
|
|
|
Dimensions:
Length Rotor skids Clearance: Height--Rotor Height--Tail cockpit tail |
Dimensions:
Length 37.79 ft Rotor 32.81 ft skids 6.79 ft Clearance: Height--Rotor 10.10 ft Height--Tail 11.15 ft cockpit 1.84 ft tail 2.06 ft |
|
|
VEMD definition
|
Vehicle
Engine Multifunction Display |
|
|
FLI
|
First
Limit Indicator |
|
|
LACU
|
Lighting
Ancillary Control Unit |
|
|
Main Rotor Head type
|
Spheriflex head
Fully Articulated |
|
|
Main Gear Box (SHP)
|
402 shp
|
|
|
LACU description
|
LACU- Comprises all the electrical control and monitoring units of the main, optional and lighting systems.
|
|
|
CWP
|
CWP--warning and caution panel
|
|
|
When does a gong sound?
|
generated each time a red warning appears on the cwp
|
|
|
ASU definition/description
|
ASU--Ancillary System Unit. Processes all audible warning, some visual warnings, and some specific electrical signals.
|
|
|
PCB1 (3)
|
PCB1
1. processing of engine fire visual warning 2. generation of min Nr or max Nr audible warning. 3. processing of audible warnings |
|
|
PCB2 (2)
|
PCB2
1. starting time delay 2. processing of visual alarm for ENG CHIP |
|
|
FLI
1. What's displayed? 2. When does the VEMD switch to FLI? 3. How to display 3 parameters on VEMD? |
1. Ng, T4, torque...all on one gauge
2. 60% Ng 3. Press scroll to change to 3 parameters |
|
|
Time delay for start.
|
If a problem occurs during start-up a time delay relay gives the pilot 5-7 seconds to return twist grip to stop position.
|
|
|
Start button slide (4)
|
1. Starter
2. Starting valve 3. Spark plugs energized 4. twist grip unlocked |
|
|
definitions
N1 or Ng N2 or Nf or Np t4 Nr bar Hp or PA |
definitions
N1 or Ng Gas producer turbine N2 or Nf or Np Free turbine or free power turbine T4 TOT/Egt station 4.5 Nr Rotor Speed bar Barometric pressure Hp or PA pressure altitude |
