EC130B4 Random Questions Flashcards

Further info for study for Ec130B4 checride (60 cards)

1
Q

OVERALL LENGTH

from tip of rotor to tail

A

41.47’

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2
Q

ROTOR DIAMETER

A

35.07’

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3
Q

WHAT TYPE OF ENGINE

A

Turbomeca Arriel 2B1

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4
Q

MAST TILT

A

2 degrees forward to level cabin in cruise flight

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5
Q

TURBOMECA ARRIEL 2B1 Power Rating

A

847 SHP

(through reduction derated to)

747 SHP (MTOP)

728 SHP (MCP)

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6
Q

Vy USED FOR TAKE OFF, LAND, APPROACH AND EMERGENCY MANUEVERS

A

70 Knots - 1/1000’

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7
Q

AUTOROTATION FLARE HEIGHT

A

70 Feet

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8
Q

VEMD ENGINE CHECK PROCEDURES

A

Scroll to Engine Performance Check (EPC) page

Hold settings for 30 seconds and read results on the following page

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9
Q

SCU

A

System Control Unit

To tell you which button on the console is engaged before applying power, because the buttons do not stay depressed

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10
Q

VEMD

(stands for)

A

Vehicle and Engine Mangment Display

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11
Q

WHAT VEMD SCREENS ARE AVAILABLE UNDER FLIGHT MODE?

A
  • Engine
  • Vehicle
  • Flight Report
  • HIGE
  • HOGE
  • Engine Power Check
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12
Q

WHEN IS THE FLIGHT REPORT PAGE DISPLAYED?

A

On engine shutdown when NR is below 70 rpm

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13
Q

HOW MANY CHIP DETECTORS ARE ON THE ENGINE?

A

3

1 electrical

2 magnetic

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14
Q

HOW MANY FUEL PUMPS ARE THERE?

A

3

1 start pump .5 bar

1 low pressure pump 10 bar

1 high pressure pump 40 bar

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15
Q

WHAT PART DOES THE OIL FILTER HAVE TO DO WITH THE FUEL SYSTEM?

A

Heats the fuel so anti ice additive is not needed

(anti ice, Prist, only needed if below -20c)

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16
Q

FADEC

(STANDS FOR)

A

Full Authority Digital Engine Control

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17
Q

WHAT DOES THE FADEC DO?

A
  • Automatic engine starting, preventing T4 exceedences
  • Proportional power turbine speed control with rotor noise reduction feature
  • Protection against engine surge and flame out
  • Bleed valve monitoring
  • Protection against NG and T4 overlimits
  • Engine Power Check (EPC)
  • NG and NF cycle counting
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18
Q

HOW IS FUEL FLOW DETERMINED AND ADJUSTED?

A

By the FADEC

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19
Q

WHAT DOES THE DUAL STAGE STEPPED MOTOR DO?

A

Provides fuel flow modulation by driving a metering valve in the engine’s ‘hydro-mechanical unit’

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20
Q

HOW IS THE FADEC SUPPLIED POWER?

A

2 channel gas generator driven independent alternator

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21
Q

FADEC SYSTEM FAILURES 3 LEVELS

A

LEVEL 1 - FLASHING YELLOW GOV LIGHT

Flashing at idle or during starting or shut down: Governor redundancy failure, no impact on governing
function.
. Start-up procedure: abort, report to Maintenance Manual
. Autorotation training: cancel training, return to base.

LEVEL 2 - SOLID YELLOW GOV LIGHT

Permanently lighted :
Governing function degraded.
1. Collective - AVOID abrupt power changes.
2. IAS - MAINTAIN below VNE power off
LAND AS SOON AS PRACTICABLE
On ground : do not start the engine.

LEVEL 3 - RED GOV LIGHT (Total FADEC failure, metering valve frozen. EBCAU has taken over

IN FLIGHT:
1. Flight parameters - CHECK
Emergency mode automatically self-engages. GOV (yellow) illuminates.

2. Collective pitch…………….. AVOID abrupt changes

Maintain Ng > 80% Hp < 20000 ft
Maintain Ng > 85% Hp ≥ 20000 ft

LAND AS SOON AS PRACTICABLE
Approach and Landing : Make a powered approach. Avoid steep angle.

After touch down, shut-down :
Collective pitch - SLOWLY down to low pitch
Starting selector - OFF

NOTE

This failure can also results in loss of ΔNg and torque parameters on the VEMD.

• DURING ENGINE STARTING :
Starting selector - OFF position immediately

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22
Q

DESCRIBE THE 3 ANCILLARY SYSTEMS

(PCB’s under the rear right passenger seat)

A

PCB1 - Fire warning lights, Aural NR warning horns, Gong

PCB2 - ENG chip, MGP chip, TGB chip caution lights, NR/NF signals, BATT TEMP warning light and processes VEMD electrical supply

PCB3 - EBCAU backup unit

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23
Q

WHAT IS THE NAME OF THE SHROUDED TAIL ROTOR SYSTEM?

A

FENESTRON

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24
Q

HOW MANY BLADES MAKE UP THE FENESTRON?

A

10

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25
WHAT INDICATION WILL A PILOT HAVE OF THE LANDING OR TAXI LIGHT ARE ON?
26
WILL THE AIRCRAFT START WITH THE ROTOR BRAKE OUT OF THE LOCKED POSITION?
NO
27
IS THE OVERHEAD FUEL CUT-OFF LEVER SAFETEY WIRED?
No, a plastic cover protects it
28
HOW MANY HYDRAULIC PUMPS?
2 ## Footnote Left hand gear driven for upper portion of servos Right hand belt driven for lower portion of servos
29
DO THE HYDRAULIC PUMPS USE SEPARATE RESERVOIRS?
YES
30
WHAT IS THE PURPOSE OF THE ROTARY DISTRIBUTION VALVE?
If one of the systems fails, the two valves move as an independent unit and supply pressurized fluid and return
31
IN THE EVENT OF HYDRAULIC FAILURE HOW DO THE HYD ACCUMULATORS HELP?
There are NO accumulators
32
WHAT DOES THE INST 1 SWITCH DO ON THE LIGHTING CONSOLE?
Instrument panel lighting control
33
WHAT DOES THE INST 2 SWITCH DO ON THE LIGHTING CONSOLE?
Console and overhead lighting panel
34
WHAT DOES THE DAY SETTING DO?
VEMD and CWP lights are set to normal brightness
35
WHAT DOES NIGHT 1 AND 2 SWITCH DO?
VEMD and CWP lights are dimmed accordingly #2 shuts off compass light
36
DIRECT BATTERY SUPPLIES POWER TO WHAT?
* Transponder * NR/NF instrument * Instrument lighting * Reading and dome lights * Emergency floatation gear
37
WHEN DOES GEN TAKE OVER POWER PRODUCTION
When it produces .5 volt above battery
38
FAN OPERATION TEMP
On at 77c Off at 68c
39
TR SHAFT SPEED
6000 RPM
40
WHY IS THE GPS CRITICAL TO THE FADEC?
It provides a clock for FADEC exceedences or failures
41
What does B on a page of the RFM mean?
It is FAA approved
42
Which sections of the RFM are FAA approved, or complimentary?
Sec 1-5 and 9 are FAA approved Sec 6,7,8,10,11 Complimentary
43
UPDATES - REVISIONS
* WHITE - NORMAL * YELLOW - INTERMEDIATE
44
DIFFERENCE BETWEEN SBT and SLT
SBT (Service Bulletin) Due to an incident or event SLT (Service Letter) Information
45
4.3.1 ENGINE PRESTART CHECK
- Seats and control pedals - ADJUSTED. - Seat belts - FASTENED. NOTE: Copilot seat belts shall be fastened in all cases. Rotor brake - RELEASED, fully forward. Fuel shut-off lever - FORWARD, plastic guard condition. Twist grip - IDLE detent. [EMER SW] (if fitted) - ON, LOCK-WIRED. Starting selector - OFF. [SCU TEST] (if fitted) - COMPLETE. [BAT/EPU] - ON. [DCT BAT] - ON. [GENE] - ON. ICS and GPS nav.system (if fitted) - ON. Lighting circuits 1 and 2 test - COMPLETE. (night flight intended). Electrical mirror (if fitted) - SET to avoid dazzling (night flight). [W/LT TST] - COMPLETE. [FIRE TST] - COMPLETE. [SERVO TST] - SERVO lit when depressed. CWP lights - CHECK : ---With battery power ................ GENE PITOT ENG P FUEL P HORN MGB P SERVO HYDR TWT GRP ---With EPU power.....................Same light as above + BATT VEMD - _3-data page DISPLAYED,_ _Vehicle page DISPLAYED,_ _Battery voltage 22 V,_ _Bleed valve open flag DISPLAYED._ Control pedals - _Freedom, then NEUTRAL_ Cyclic pitch - _Center, Friction adjusted_ Collective pitch - _LOCKED_ Heating, demisting, air conditioning (if fitted) - _0FF_
46
Engine Start Checklist
CWP - check GOV [Fuel P] - ON [A/Col LT] - ON \*\*\*After 30 Seconds Starting selector - ON position Enigine paramaters - Check \*Ng increase, \*T4 remains below its limits, \*Rotor is turning at Ng\>25%, \*Engine Oil pressure increases. \*\*\*When Ng \>67% CWP - CHECK \*ENG P \*MGB P \*HYDR \*SERVO [PITOTS] - ON & light out [FUEL P] - OFF & light out [SERVO TST] - Light on when depressed Starting selector gaurd - SET All necessary systems - ON, TESTED (Master avionics switch, lights, etc.) NOTE 1 In strong wind apply little cyclic into wind. NOTE 2 If the starting procedure has to be aborted, return the starting selector to OFF, switch off thc fuel pump and the generator. NOTE 3 At Ng \>60 % the VEMD upper sercen automatically switches to FLI display. EPU - DISCONNECT, make sure EPU door is closed and locked. CWP - CHECK , GENE light and BATT light. NOTE Unless otherwise specified in applicable operational rules, one pilot should be at the controls as soon as the rotors turn until flight ends and the rotors are fully stopped.
47
RUN-UP CHECK
1. Twist grip ..............FLIGHT detent. • When NR ≥ 340 rpm 2. [HORN] .................ON, HORN CHECK aural warning : . ON for NR ≤ 360 rpm and . OFF for NR \> 360 rpm. 3. NR indication ......CHECK in lower green range. 4. Check ....................warning lights voltage and current, Eng oil press
48
BEFORE TAKEOFF CHECKLIST
Doors.................................................... CLOSED or OPEN LOCKED (left sliding door). 2. Cyclic and collective frictions ............ AS REQUIRED. 3. Landing light ........................................ AS REQUIRED. 4. Temperatures and pressures................. NORMAL RANGE. 5. Warning panel ...................................... All lights OFF. 6. Collective pitch .................................... UNLOCK. NOTE Adjust collective and cyclic friction so that friction forces are felt by the pilot when moving the flight controls.
49
ENG & ROTOR SHUTDOWN
1. Cyclic stick............................................................... NEUTRAL. 2. Collective pitch ........................................................ LOCK. 3. Twist grip ................................................................. IDLE detent. 4. Engine oil cooling .................................................... WAIT for 30 sec. 5. [PITOT] or [PITOTS], [HORN], Landing light.......... OFF. 6. Non-required systems, [MASTER AVIONICS] or [AVIONIC] ......................... OFF. 7. Starting selector........................................................ OFF position. 8. [GEN] or [GENE]...................................................... OFF. • For NR ≤ 140 rpm. Normal NR, 170 rpm. Maximum NR (in strong wind operations). 9. Rotor brake............................................................... APPLY. • When rotor is stopped : 10. GPS navigation system (if fitted)....OFF. 11. [A/COL LT]........................................ OFF. • BEFORE LEAVING HELICOPTER 12. VEMD .............................................. CHECK for Flight Report page data : . Operating time (counted from Ng \> 60 % until Ng \< 50 %). . Ng and Nf cycles ........................ CHECK (written in white characters and above 0). . Advisory messages of FAILURE or OVERLIMIT DETECTED . 13. VEMD .............................................. CHECK bleed valve open flag displayed. 14. [DIRECT BATT.] or [DCT BAT], [EXT PWR BATT.] or [BAT/EPU]...... OFF. 15. Pitot, air intake and exhaust covers, blade socks as required.
50
DCT BATT consumers
1. Tpndr 2. NR/Nf 3. Inst Lights #2 4. Reading/Dome lights 5. Start Selector switch 1. FLIGHT/IDLE selection 2. COM/NAV 1 (GNS430) 3. ICS ENG & FADEC self supplied Standby Horizon self batt
51
PGCH Manuvering limits
30° bank 10° pitch 2000 FPM 300 AGL 120 kts in descent
52
Name of Vibration Reduction Devices
Cabin Resonators & Anti-Vibration Assembly or Device
53
Blade Root Parts
Sleeves Thrust Bearing (spherical) Star Flex/Star Arm Frequency Adaptor
54
IIMC Procedure
1. Unsusual Attitude recovery (Bank, Pitch, Power) 2. 90 kts (7 on FLI) 3. Climb to MEF (8500 msl, Max Elevation Figure) 4. Call LAS Vegas App 119.4 5. Confess 6. Comply
55
SFRA Route limits, freq & configuration
1/2 mile route line 5000' MSL +/- 300' (or \< 1 min) 121.95 Anti-collision & Stobe all times. Landing lights, pulsating lights in the vicinity of Supai Village, the Dragon Corridor, Split Intersection or in a VFR holding area. Inoperative Okay if MEL allows.
56
What does the Articulated Coupling do?
1. Absorbs overrunning torque 2. Fwd Mount for ENG 3. Allows small misalignments 4. Ensures equal distance MGB to ENG
57
MRGB
2 stage reduction - spiral bevel and epicyclic 3 modules - oil, bevel, epicyclic
58
Explain Hydraulics
Dual Body, rotary type Left upper limit (red, fwd, gear) Right lower belt
59
VEMD Mx pg
OFF 1 OFF 2 OFF 2 SCROLL & RESET (hold) Release
60
Fuel Amounts
146.8 Total 144 Usable