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B3 2B1 > B3 2B1 > Flashcards

B3 2B1 Flashcards

Learn EP's and Limits of B3 2B1 (48 cards)

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1
Q

Max Gross Wt

A

5225

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2
Q

Hyd pressure

A

35+-1 Bar

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3
Q

When does HYD Light come on

A

20+-5 Bar

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4
Q

Tail Rotor Control Failure

A

Airspeed …70 Kts
Yaw Servo Hyd Switch…..Shutoff
Hyd Test….Engage
LASA Practicable…Shallow Approach/ Run on Landing

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5
Q

ENGINE FAILURE (CRUISE)

A

AUTOROTATE…….A/S (65 KIAS)

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6
Q

ENGINE FIRE / DURING START

A
  1. STARTING SELECTOR … OFF
  2. FUEL SHUTOFF …. CLOSE
  3. ROTOR BRAKE (As Necessary) … ENGAGE
  4. FUEL PUMP…. OFF
  5. CRANK SWITCH …. ENGAGE (For 10 sec)
  6. MASTER SWITCH ………… OFF
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7
Q

ENGINE FIRE (IN FLIGHT)

A
  1. AUTOROTATE …. A/S (65 KIAS)
  2. FUEL SHUTOFF … CLOSE
  3. MASTER SWITCH (If There Is A Burning Smell) … OFF
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8
Q

TAIL ROTOR DRIVE FAILURE (HOVER IGE)

A
  1. TWIST GRIP … IDLE

2. LAND … MAINTAIN LEVEL ATTITUDE

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9
Q

TAIL ROTOR DRIVE FAILURE (HOVER OGE)

A
  1. COLLECTIVE … REDUCE (As Required)
  2. AIRSPEED … INCREASE
  3. LASA POSSIBLE
  4. AUTOROTATE / ENGINE SHUTDOWN … MIN TOUCHDOWN SPEED
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10
Q

TAIL ROTOR DRIVE FAILURE (IN FLIGHT)

A
  1. COLLECTIVE … REDUCE (As Required)
  2. AIRSPEED … ADJUST (To Minimize Left Yaw)
  3. LASA POSSIBLE
  4. AUTOROTATE / ENGINE SHUTDOWN …… MIN TOUCHDOWN SPEED
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11
Q

TAIL ROTOR CONTROL FAILURE

A
  1. AIRSPEED …SET 70 KIAS / Level Flight
  2. YAW SERVO HYD SWITCH (collective)… OFF
  3. HYD. TEST …. ENGAGE
  4. LASA PRACTICABLE .. SHALLOW APP/RUN-ON LDG
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12
Q

HIGH ENGINE OIL TEMPERATURE (IN FLIGHT)

A
  1. AIRSPEED ….. 80 KIAS

IF THE TEMPERATURE DECREASES BELOW THE REDLINE

  1. LASA PRACTICABLE
    IF THE TEMPERATURE REMAINS ABOVE THE REDLINE
  2. LASA POSSIBLE
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13
Q

ENG P LIGHT

A
  1. POWER….REDUCE

IF ENGINE OIL PRESSURE IS LOW OR ZERO:

  1. AUTOROTATE / ENGINE SHUTDOWN
    IF ENGINE OIL PRESSURE IS NORMAL:
  2. LASA POSSIBLE
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14
Q

LOW ENGINE OIL PRESSURE (GAUGE)

A
  1. WARN/FIRE TEST … CHECK ENG P LIGHT

IF ENG P LIGHT IS OFF WHEN TESTED:

  1. AUTOROTATE / ENGINE SHUTDOWN
    IF ENG P LIGHT IS ON WHEN TESTED:
  2. LASA POSSIBLE
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15
Q

HYDR + SERVO + LIMIT (LH CIRCUIT FAIL)

A

LASA PRACTICABLE

FOR ALL CASES, NORMAL APPROACH AND LANDING

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16
Q

HYDR + SERVO + STIFF PEDALS (RH CIRCUIT FAIL)

A

LASA PRACTICABLE

FOR ALL CASES, NORMAL APPROACH AND LANDING

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17
Q

SERVO LIGHT

A

CONTINUE FLIGHT, RETURN TO BASE

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18
Q

LIMIT LIGHT

A
  1. COLLECTIVE – REDUCE
  2. CYCLIC – REDUCE SPEED OR LOAD FACTOR
  3. CONTINUE FLIGHT
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19
Q

YAW SERVO-CONTROL SLIDE-VALVE SEIZURE (IN FLIGHT)

A
  1. AIRSPEED … ADJUST (40-60 KIAS)
  2. YAW SERVO HYDRAULIC SWITCH (Collective)…OFF
  3. LASA PRACTICABLE … NORMAL APPROACH
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20
Q

YAW SERVO-CONTROL SLIDE-VALVE SEIZURE (HOVER)

Study These Flashcards
A 
If yaw control is maintained:
LASA POSSIBLE
If yaw control is NOT maintained:
1. HYDRAULIC PRESSURE SWITCH (Collective) ...... OFF
2. LASA POSSIBLE
21
Q

M.G.B P. LIGHT

Study These Flashcards
A
  1. POWER …. REDUCE

2. LASA POSSIBLE

22
Q

M.G.B T. LIGHT

Study These Flashcards
A
  1. POWER … REDUCE

2. LASA POSSIBLE

23
Q

MGB CHIP LIGHT

Study These Flashcards
A
  1. POWER … REDUCE

2. LASA POSSIBLE

24
Q

ENG CHIP LIGHT

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A

LASA POSSIBLE

25
TGB CHIP LIGHT
LASA POSSIBLE
26
FUEL FILTER LIGHT (EITHER)
1. POWER ... REDUCE | 2. LASA POSSIBLE
27
FUEL P LIGHT
1. POWER ... REDUCE 2. FUEL PUMP ... ON 3. LASA POSSIBLE
28
GOV. LIGHT [RED]
1. FLIGHT PARAMETERS ... CHECK 2. MAINTAIN NG > 80% WITH PA < 20,000 FEET. 3. LASA PRACTICABLE
29
GOV. LIGHT [AMBER] (STEADY)
1. AVOID ABRUPT POWER VARIATIONS 2. IAS ... MAINTAIN BELOW VNE Power Off 3. LASA PRACTICABLE
30
VEMD SINGLE SCREEN FAILURE
FAILED SCREEN ...OFF
31
VEMD DUAL SCREEN FAILURE
1. POWER ... ADJUST (100 KIAS Max) | 2. LAND WITHOUT HOVERING
32
NR INDICATOR FAILURE
1. POWER ... MAINTAIN TORQUE >10 2. Nf ... MONITOR 3. LASA POSSIBLE
33
When does Engine Oil Light illuminate?
<1.1 bar
34
How many volts should you see before starting engine
22V min
34
NG Limits
Max Continuous 97.1% ΔNg-4% Take-Off range ... ΔNg-4% to ΔNg0% Max Take-Off (5 Minutes) ... 101.1% ΔNg0% Transient (< 5 sec) ...102.3% ΔNg+1% CAUTION: P2 bleed is prohibited at power settings beyond MCP.
34
Oil Temp Switch activates the thermal swtich at what temp?
on at 77 ̊C off at 68 ̊C
35
TQ Limits
Max Continuous - A/S > 40 kts...92.7% Take-Off - A/S < 40 kts 100% Transient - 104% for 5 sec
35
T4 Limits
Max for Engine Starting ... 750ºC Max Transient for Starting ... 865ºC for 10 Sec Max Continuous ... 849ºC Take-Off ... 915ºC
36
Engine Oil Temp Limit
-10ºC to 0ºC Caution Range Minimum oil temp before power application: 0ºC Max Temp ...115ºC
37
Engine Oil Pressure
1.1 Bar (16psi) ... Min pressure (NG>70%) 1.1 - 2 Bar (16-29 psi) .. Caution Range 6 - 9.8 Bar (87-142 psi) .. Caution Range 9.8 Bar (142 psi) ... Max Pressure
38
Ammeter & Voltmeter
Max Current .......... 180A | Max Voltage .......... 31.5V
39
Airspeed Limits
VNE Power Off - 125 kts at 0 PA, -3 kts per 1000ft | VNE Power On - 155 kts at 0 PA, -3 kts per 1000ft
40
Rotor Brake Limits
100 rpm recommended for application of Rotor Brake Max Nr for application ... 170 rpm Minimum time between 2 consecutive braking's : 5 min
42
Slope Limits
Nose Down ... 6º Nose up ...... 10º Lateral ......... 8º
42
Max A/S for running landings
excluding emergencies ... 40kts
43
NR Limits
``` Power On: Normal .... 375 - 405 Horn continuous when < 360 Intermittent when > 410 Minimum Power Off .... 320 Max rpm Power Off .... 430 ```
45
NF Limits
Minimum ... 349 rpm Normal ... 349-418 rpm Max Continuous .. 418 Max Transient ... 450 rpm (5 sec)
47
DOOR Caution Light
A/S ... Reduce (70 kts Max) | LASA Practicable ..... Low decent rate, shallow approach

B3 2B1 (1 decks)

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