EC130 B4 Limitations Flashcards
Warning
An operating procedure or practice, which if not correctly followed, could result in personal injury or loss of life.
Caution
An operating procedure or practice which, if not strictly observed, could result in damage/destruction to helicopter parts or equipment.
The following are forbidden:
Aerobatic maneuvers
Engine starting with snow/ice around intake
Flight in falling snow without sand filter
Flight in freezing rain or icing conditions
In flight use of twist grip control (except training and emergency)
Intentional VEMD shutoff in flight
Weight Limits
Max weight 5350 lbs
Min weight 3307 lbs
CG limits
Longitudinal weight dependent. See chart.
Lateral 3.94 inches both left and right
Power on and off Vne
Power on: 155 kt at Hp=0 (less 3 kt per 1000’)
Power off: 125 kt at Hp=0 (less 3 kt per 1000’)
Vne with doors off
70 kt - LH sliding door operating in flight
80 kt - LH sliding door open-locked
110 kt - LH sliding door removed
90 kt - LH sliding door removed or locked and RH, LH, or both doors removed
Maximum Operating Altitude in Flight
Hp = 17000’
(With crash resistant fuel tanks)
Temperature Limits
Min temp: -20 deg c
Max temp: ISA +35 deg c or max 50 deg c
Landing and Rotor Stopping Limitations on Slope
6 degrees nose up
6 degrees nose down
8 degrees sideways
Maneuvering limitations load factor
Don’t exceed load factor that makes the “LIMIT” light come on
Main Rotor Limitations
170 rpm: Rotor brake max speed
320 rpm: Min power off
320-375 rpm: Caution range
375-405 rpm: Normal operating range
405-430 rpm: Caution range
430 rpm: Max power off
Aural warnings:
Low: Under 360 rpm
High: Over 410 rpm
First Limitation Instrument
9.6 = Max continuous
9.6-10 = Takeoff power
10 = Max takeoff
10.4 = Max transient
Torque Limitations
92.7% Max continuous
92.7%-100% Takeoff power below 40 kt
100% Max takeoff
104% Max transient (5 seconds)
Engine Limitations (Nf)
Arriel 2B1
349 rpm: Minimum
349-418 rpm: Normal operating range
418 rpm: Max continuous
450 rpm: Max transient limit (5 seconds)
Ng Limitations
Ng 67% : Min stabilized speed
Delta Ng -4% : Max continuous
Delta Ng -4% to 0% : Takeoff power
Delta. Ng 0% : Max takeoff
Delta Ng +1% : Max transient (5 seconds)
100% Ng = 52110 rpm
T4 Starting Limitations
750 deg C = Max continuous
865 deg C = Max transient (10 seconds)
T4 Flight Limitations
849 deg C = Max continuous
849 to 915 deg C = Takeoff power
915 deg C = Max takeoff
941 deg C = Max transient (20 seconds)
Engine Oil Temperature Limitations
-10 C to 0 C : Caution range (minimum 0 C before power application)
115 C : Max temperature
Engine Oil Pressure Limitations
1.1 bar : Min pressure
1.1 to 2 bar : Caution range
6 to 9.8 bar : Caution range
9.8 bar : Max pressure
Electrical Circuit Limitations
31.5 V : Max voltage
150 A : Max current
Baggage compartment load limitations
RH cargo: 287 lbs
LH cargo: 342 lbs
Both limit (62.5 lb/sq ft)
Rear cargo: 176 lbs (30 lb/sq ft)
Cabin Floor Load Limitations
Max distributed load of 62.5 lb/sq ft
Rear cabin floor: 1091 lbs
Forward left cabin floor: 893 lbs
Starter/Generator Limitations
(Starter time is the time between starter selector “ON” and engine igniting)
To prevent starter overheating:
30 seconds ON
60 seconds OFF
30 seconds ON
60 seconds OFF
30 seconds ON
30 MINUTES OFF
Headsets
Minimum of two in helicopter:
One worn by pilot (required for audio warnings)
One spare
Fuel capacity (with crash resistant tanks)
144 US Gal
Minimum Voltage before Start
22V
What does Hydraulic Manifold Do?
Directs
Regulates
Monitors
Filters
How to conduct power check
- Raise collective to above 9 on FLI
- Note Ng value
- Push button on collective twice
- Check for “good” result
To view power check later:
- Turn off VEMD screens
- Turn on screen 2 then immediately hold [Scroll] + [Reset] until “release keys” is displayed
TOPS Limitations
> 500’ AGL
30 deg bank, 10 deg pitch
No thrill ride, aerobatic, NOE
Inadvertent IMC procedure
- Get on instruments
- Level aircraft, safe airspeed
- Climb to MEF for area (8500’)
- Las Vegas approach 119.4
- Confess
- Declare urgent
- Position, Altitude, Fuel on board, Souls on board, Nature of emergency
- Comply with instructions
Time between rotor brake applications
5 minutes
P2 air bleed limitations
Off for starting and stopping engine
Off for using power above MCP
Off for engine power check
Vy
70kt at 0Hp (-1kt/1000’)