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AS332 L/L1 - Craig
ITR/Refreasher AS332L/L1 Questions - Good luck
| Question | Answer |
|---|---|
| D-Value | 18.70 mtr |
| Max load takeoff with internal loads | 8600 kg |
| Max takeoff external load | 9350 kg |
| How many persons can the AS332L/L1 can carry? | 24 |
| Min approved takeoff weight? | 4500 kg |
| Power On: NR Range | NR 92,5-103.8 % |
| Max wheel braking speed | 30 kts |
| Max taxi speed | 40 kts |
| Max VNE power OFF AS332L1 | 145 kts |
| Min speed IMC with both lanes of the AP working | L = 65 knots & L1 = 40 knots |
| Max temp for operations | ISO + 35* (Limited to 50*c) |
| Max weight in the aft baggage compartment lower shelf | 250 kg |
| Max weight in the tail boom | 55 kg |
| Max nose-up & lateral for takeoff & landing | 12* / 8* |
| Collective pitch for AP loss of a single roll/pitch/roll lane? | 15,5* collective pitch |
| What is the problem associated with taxing with the nose gear castoring | Breaking the locking pin |
| The main rotor blades must be restrained to the helicopters fitting if the wind is over ... | 25 kts |
| When parked, the aircraft is kept stationary by | The Park Brake |
| Max towing speed | 10 kp/h |
| Rotor Diameter | 15,58 meter |
| Main rotor is angled forward by | 5* |
| The heater/vent blower for the cabin is located | Overhead consol cockpit |
| Flight controls: The short term (fast & small) deviations are executed by | Servo valves |
| Power Off: Max Continuous NR | 109,5% |
| Max VNE power ON | 167 kts <8350 kg. & 150 kts >8350 kg. |
| Max rotor speed for rotor brake application | 45 % NR |
| Max angle of bank | 40* 7800-8350 kg & 30* >8350 kg. |
| Flight Controls: Long term deviations are executed by | Beeper trim |
| How many servos directly move the swashplate | 3 |
| Electric AP heating must be ON for OAT below | 0* |
| Which of the components provides attitude reference for the AP Module | VG1 & VG2 |
| The AP can be disengaged from | Either cyclic sticks and the APCP |
| Additional 3 or 4 axis mode be engaged via the | Coupler |
| Which mode will automatically be engaged at the end of a couple ILS approach | RAD.ALT |
| Where is the Vtoss for the AS332L1 displayed in the cockpit | Not calculated - must be calculated from the RFM |
| While a standard SFIM 155 autopilot test is being conducted, what is seen? | Red dash dot |
| If Lane 2 of the SFIM 155 AP fails | Lane 1 takes over |
| When using altitude (ALT) coupling, how are changes in altitude done? | ALT must be disengaged to change altitude, then reengaged |
| What causes the red AP.HT light on the warning-caution panel to illuminate | Overheating or failure of the AP electric heating system (temp >120*c) |
| What selection should be made on the TEAM TB45 to have ICS (voice)? | ICS selected "Normal" |
| VHF Com No.2 antenna is normally located | Bottom of the aircrafts nose RH side |
| What makes a amber TRANSFER light on the AC electric power supply panel illuminated | Short 1XP1 or 2XP1 |
| The 115/26V AC transformer is connected to | AC bus 1XP1 |
| An amber alternator light will illuminate | Alternator INOP |
| The standard rating of the two alternators are | 20-30 kWA (30-40 kWA is optional) |
| Which TRU will normally charge the main battery | No. 2 |
| The battery + light illuminates - what's the problem | Short circuit PP2 |
| Red BAT.T warning light on the Central Warning Panel illuminates when temperature is over ... | 70*c |
| Which system light is triggered on the Central Warning Panel, if a failure in the electrical system occures | ELEC |
| Emergency battery supplies | DC Priority / Em. light / Ord. light / Standby bar |
| Inflight: DC power is normally provided by the | TRU´s |
| What causes the RED DC warning light to illuminate on Central Warning Panel | Failure of DC supply from both TRU 1 & 2 |
| What happens when the main battery fails? | BAT isolates |
| If the + contractor for the battery illuminates | No PP2 connected |
| How is the emergency flotation gear activated? | On either collective or pedestal panel |
| The pressure bottle in the emergency flotation system is normally pressurized with | Helium |
| Fire in engine No. 1 indications are | Alarm / Audio / Fire 1 or 2 / FSOL illuminates |
| What are the indications of cargo fire? | Smoke + Warning Cargo Fire |
| Yellow light on the engine fire extinguisher panel indicates | That a bottle has been discharged |
| What will be the indications if the fuel quantity in the RH or LH group drops below 71 kg (90 liters) | Warning Fuel Low light |
| What may cause the FUEL light on the Central Warning Panel to illuminate | Pressure drop / Filter / Level high-low |
| Where are the LH and RH fuel booster pumps located | In each longitude (feeder) tanks |
| When the transfer switch on the fuel panel is selected ON, the fuel ... | Fuel transfer - left or right |
| Where is the pressure refueling adapter located | Right sponson |
| What will happen if the RH hydraulic system fluid level in the reservoir droops below 2 liters | RH tail rotor shut off valve closes |
| What does the illumination of the RH.P message on the hydraulic sub panel, HYD warning light and WARN repeater lights indicate? | RH hydraulic system has less that 80 bar |
| When the auxiliary hydraulic is selected OFF position, the indication will be | No green + pressure 0 |
| The electrical auxiliary hydraulic pump is supplied with hydraulic fluid from the ... | LH reservoir |
| Normal operating hydraulic pressure for RH and LH system is | Pump 170-175 |
| The wheel brakes, rotor brake, landing gear, autopilot servos and optional equipment are supplied hydraulics by what system | LH reservoir |
| Which HYD system is used for normal landing gear extension/retraction | LH reservoir relieved by the AUX system |
| How are the windshield wipers activated in manual mode | By pressing the button on the collective. |
| When triggered, pressing the red ALARM repeater lights will ... | Extinguish the light. |
| The aural warnings for Low and High NR thresholds PWR OFF are: | Low 92,5% & High 109,5% |
| What information does the BARAN air data unit supplying the autopilot with | ALT & IAS |
| The two VG gyros are controlled from the | Overhead panel |
| Where is the Radar Altimeter (RAD.ALT) information displayed | On radar altimeters |
| The pilot and co-pilot doors can be jettisoned from | The inside or outside |
| The main rotor NR is monitored utilizing | Phonic wheel MGB flare housing |
| The 105 bar position of the rotor brake is used for | High wind start |
| The main gearbox pump and emergency pump are monitored by ... | Pressure gauges |
| The MGB is attached to the structure by | 3 suspender bars + BBQ plate |
| What brings on the MGB.C light on | Pump out or cooler fan fail |
| The MGB.T light illuminates when the temperature exceeds | 145*c |
| RED MGB.P warning light on Central Warning Panel illuminates when gearbox oil pressure is below | 1 bar |
| Tail gear box is lubricated by | Splash |
| Maximum NG AEO Take-off power is limited to __ min. | 5 min |
| Maximum NR OEI Contingency power can be used for__ min. | 2,5 min |
| Engine compressors can be washed by introducing water | LH side |
| OEI TQ ratings are | MGB TQ 66 % Unlimited / 69% 2:30 min. / 74% 20 sec. |
| The bleed valve offset is controlled by | Collective switch |
| The DC power busses PP2-PP3, are in flight supplied with power from the | The Transformer rectifiers (TRUs) |
| Max takeoff weight without external load is | 8600 kg |
| Min approved weight | 4500 kg |
| Max Emergency NR Power ON | NR 109,5% |
| Max wheel braking speed is | 30 kts |
| Max ground taxing speed is (landing) | 40 kts |
| The max VNE Power ON is | 167 knots <8350 kg & 150 knots >8350 kg. |
| The max VNE Power OFF AS332L1 | 145 kts. |
| Max angle of bank | 40* <8350 kg. & 30* >8350 kg. |
| A GOV1 or GOV2 light means | Governing system redundancy has failed on the respective engine |
| The engine compressor can be washed by introducing water | Through washing connectors on LH side of the fuselage |
| When starting with Rotor Brake applied, max NG is | 70% on aircraft with 21/105 bar rotor brake unit |
| Max NR for rotor brake application | 45% |
| When landing on sloping ground, what limits apply | 12* nose up & 8* lateral |
| The MGB T light illuminates when the temp exceeds | 145*c |
| What is the max temp for operations | OAT ISA +35*c (+50*c) |
| The tail gear box is lubricated by | Splash lubricated |
| What causes the red AP.HT light on the CWP illuminate | AP Heating failure |
| A Yellow light on the Engine Fire extinguisher panel indicates | A discharged fire extinguisher bottle |
| What problem is associated with taxing with the gear pastoring lock ON | May break the pastoring lock pin |
| MIN speed in IMC with both lanes of the AP working is | L1 = 40 knots & L = 65 knots |
| Max speed IMC with one lane of AP working | IAS at 15,5 degrees collective pitch |
| Illumination of the amber HIGH (up pointing arrow) light on the fuel management panel indicates | All tanks are full |
| What happens when "Auto Transfer" on the fuel panel is selected ON | Fuel transfer to standard fuel tanks is initiated and terminated automatically |
| An amber A.PUMP message indicates that | There has been a short circuit in the auxiliary pump electrical supply |
| The electrical auxiliary hydraulic pump is supplied with hydraulic fluid from the | LH hydraulic reservoir |
| From what hydraulic system and how many bar pressure does the autopilot unit need to function | LH hydraulic system and needs 70 bar min. |
| What is the result if the temperature sensor in the centre windshield heating system fails? | The centre windshield heating is lost |
| What will be the result if the temp sensor in LH windshield heating system fails | LH windshield heating system goes auto to OFF |
| How are the LH and RH windshield wipers operated | By a start/stop button located on both collective handles |
| In manual mode, how long does the windshield wipers run? | Runs as long as the collective push-button is pressed |
| The rotor brake system has 3 setting: | Safety / Normal / High wind |
| Does both the MGB standby and main pumps suck oil from the same level? | Yes |
| The amber MGB.T. function message illuminates when the gearbox temp is above? | 145*c |
| Tail gear box is lubricated by | Splash lubrication |
| The fuel filter is monitored in the cockpit by ... | A FUEL light on the CWP and FUEL FILT message on the fuel panel |
| The main rotor blades must be restrained to the helicopter fittings if wind exceeds | 25 knots |
| The aircraft, when parked, is kept stationary by | The parking brake & wheel chocks if available |
| What is the maximum speed for towing the AS332L/L1 | 10 kp/h |
| The rotor diameter | 15.58 meter |
| The main rotor is angled forward by | 5 degrees |
| The heating/ventilation blower for the cabin is located | On top of the cockpit section |
| The short term control (fast and small) deviations are executed by | The servo valves |
| The long term collective control deviations (large) are executed by | The PTA (Parallel Trim Actuator) |
| How many servos directly move the swashplate | 3 |
| What do the PTA (Parallel Trim Actuators) do? | Executes collective commands from the autopilot |
| What are the PTA (Parallel Trim Actuators) functions? | Electrically powered, fitted to the collective channel and have 100% authority |
| What is the purpose of the autopilot with NAV coupling | Stabilization and guidance |
| Which component provides attitude reference for the AP Module | VG1 & VG2 |
| The AP can be disengaged | From the APCP (Autopilot Pilot Control Panel) |
| The AP hydraulics can be disengaged from | Either collective handle |
| When is the Go Around mode available | With the SFIM CDV 85/155 Flight Director Coupler |
| Additional 3 or 4 axis mode coupling can be engaged via | The Coupler Control Unit |
| Which mode will automatically be engaged at the end of a coupled ILS approach | ALT (Radio altitude level height) |
| How do we change ALT when using altitude (ALT) coupling | The ALT modes needs to be disengaged to change altitude |
| Where is the Vtoss displayed in the cockpit | It's not, it needs calculating before flight |
| When are AP additional upper modes available | With the additional SFIM CDV 85 Flight Director Couple |
| While a standard SFIM 155 autopilot test is being conducted what is seen | A red DOT flashes during the test |
| How can the Turbulence mode (TURB) can be selected? | By moving a switch on the AFCP from NORM to TURB |
| If lane 2 of the SFIM 155 autopilot fails ... | Lane 1 automatically takes control |
| What causes the red AP.HT light warning-caution panel to illuminate | Failure of the autopilot heating system |
| When is the ICE voice activated on the TEAM TB45 ICS (intercom system) | The ICS is voice activated only when the power switch is selected to NORMAL |
| VHF Com No. 2 antenna is normally located | On the bottom structure forward of the nose landing gear, right hand side |
| What makes the Amber TRANSFER light on the AC electric power supply panel to illuminate | A short on either Alternator (AC) Bus 1XP1 or Bus 2XP1 |
| The 115/26V AC transformers is connected to what bus | Alternator (AC) Bus 1XP1 |
| An amber alternator light will illuminate | When the respective alternator is disconnected |
| The standard rating of the two alternators are | 20 -30 kVA |
| When does the + contactor light for the battery illuminate? | When the battery is disconnected from the Primary Bus bar |
| Which TRU will normally charge the main battery | TRU 1 and 2 via PP3 and PP2 (bus tie closed) |
| What does it mean if the battery + light illuminates | DC electric short circuit on PP2 |
| The red BAT.T warning light on the CWP illuminates when | The battery temp exceeds 70*c |
| Which system light is triggered on the CWP, if a failure in the electrical system occurs | ELEC |
| The Essential Safety Consumers - emergency battery supplies | DC protection boards / Ordinance light / Emergency exits / Emergency cabin lighting / Standby artificial horizon |
| In flight, the DC power is provides from | The transformer rectifiers (TRU´s) that gets it's power from Alternator 2 (AC) |
| What causes the red DC warning light to illuminate on the CWP | If both TRU´s fail to operate |
| What happens when the main battery fails | WARN & ELEC illuminates on the CWP and the + contactor lights illuminate on the overhead elec panel. Battery is isolated +/- contactor |
| Inflation of the emergency floatation gear can be carried out by | When armed; Press the button on either collective sticks or on the control panel located in the pedestal. |
| The emergency flotation system pressure bottles is normally pressurized with | Helium |
| Fire in engine No.1 is indicated by | Flashing ALARM repeater lights / FIRE 1 on CWP / Aural tone / Light in affected fuel shut off lever. Light in the two affected fire extinguishing push buttons will illuminate |
| Cargo fire indications | C-FIRE and SMOKE caution light on CWP (detected more than 20% smoke temp reaches 80*c) |
| A yellow light on the engine fire extinguisher panel indicates | A empty fire extinguisher bottle |
| What will be the indications if the fuel quantity in the RH or LH group drops below 71 kg (90 liters) | WARN repeater light / FUEL caution light on CWP / RED LOW level light (down pointing arrow) on fuel management panel illuminates |
| What may cause the FUEL light on the CWP to illuminate | Low fuel level / Low fuel pressure / Fuel filter clogging |
| Where are the LH & RH fuel system booster pumps located | Two in each longitude (feeder) tanks |
| What happens when the transfer switch on the fuel panel is selected ON | Fuel starts transferring from one longitude tank towards the other longitude tank, depending on the switch direction |
| Where is the pressure refueling adapter located | Aft of the RH sponson |
| What will happen if the RH hydraulic system fluid level in the reservoir drops below 2 liters | The WARN, HYD cautions light and RH.LEV message on the hydraulic panel illuminates, and the RH cylinder of the tail servo is isolated. |
| Illumination of the RH.P message the hydraulic sub panel, HYD warning light and the WARN repeater lights indicates | That the RH hydraulic system pressure is less than 80 bar |
| When the auxiliary hydraulic pump is selected to OFF position, the indication will be ... | No green light in the switch and the AUX pressure will be 0 |
| The electrical auxiliary hydraulic pump is supplied with hydraulic fluid from the ... | Bottom of the LH hydraulic reservoir |
| The normal operating hydraulic pressure is | 170-175 bar |
| What HYD system supplies the wheel brakes, rotor brake, landing gear, autopilot servos and optional equipment? | The LH hydraulic system |
| In manual mode, how long does the windshield wipers runs for? | Runs as long as the collective push-button is pressed |
| What is your action when getting a red ALARM repeater light? | You should cancelled the light after verifying the malfunction |
| The Aural warnings for Low and High NR thresholds are | Low 92,5% & High 109,5% |
| What happens with the HYD system during normal landing gear extension/retraction? | The aux pump starts automatically in case of a pressure drop in the LH hydraulic system |
| What information does the BARAN air data unit supplying the autopilot with | Altitude and speed data |
| The two VG gyros are controlled from the ... | Gyroscope Unit Control Panel in the overhead panel |
| Where is the Radio Altimeter (RAD.ALT) information displayed | On the radar altimeters |
| The pilot and co-pilot doors can be jettisoned | From the inside or outside |
| The main rotor NR is monitored utilizing | A phonic wheel and sensors on the gearbox flared housing |
| The 105 bar position of the rotor brake is used for | High wind starts |
| The main gearbox pump and emergency pump are monitored by | Separate pressure gauges |
| The MGB is attached to the structure by | 3 suspension bars and a flexible mounting plate (barbecue plate) |
| What brings on the MGB.C (or MGB.COOL dependent on the MOD state) light | A main cooling system failure; MGB Pump failure and thereby bypassing oil cooler. |
| The MGB.T light illuminates when the temperature exceeds | 145* degrees C |
| The red MGB.P warning light on the CWP illuminates when gearbox oil pressure is below ... | 0.4 bar (or 1 bar depending on MOD state) |
| Tail rotor gearbox is lubricated by | Splash lubrication |
| AEO max takeoff power rating is limited to (MTOP) __ min | 5 minutes |
| OEI max contingency power can be used for | 2 min 30 sec |
| The engine compressors can be washed by introducing water | Through washing connectors on the LH side of the fuselage |
| In OEI operations, the 3 power ratings are | 1) Max Continuous 2) Max Intermediate 3) Continuous ratings |
| A GOV1 or GOV2 light means | Governing system redundancy has failed on the respective engine |
| The bleed valve offset is controlled by | Buttons on the pilot and co-pilot´s collective levers |
| The AS332L/L1 can carry ___ people | 24 (crew & pax) |
| AS332L1 max takeoff weight with internal loads | 8600 kg |
| Minimum approved takeoff weight | 4500 kg |
| POWER OFF: Max Continuous NR % is | NR 109,5% |
| POWER ON: NR Range % is | NR range 92,5 - 103,8% |
| Max wheel braking speed is | 30 knots |
| Max taxing speed is | 40 knots |
| Max VNE Power ON | 167 knots <8350 kg. |
| Max rotor speed for rotor brake application | 45% NR |
| Max angle of bank is | 40* for >7800 kg. & 30* for >8350 kg. |
| Minimum speed in IMC with both lanes of the AP working is | L1 = 40 knots & L = 65 knots |
| Max temperature for operations | OAT ISA + 35*c - Limited to 50*c |
| Max weight permitted in the aft baggage compartment lower shelf | 250 kg. |
| Max weight permitted in the tail boom baggage compartment | 55 kg |
| Max nose-up/lateral slope for takeoff and landings | 12* nose-up & 8* lateral |
| AP; loss of a single roll, pitch or roll lane - max collective pitch? | Max 15,5* collective pitch |
| What problem is associated with taxing with the gear castoring lock ON | Risk of breaking the lock pin |
| The main rotor blades must be retained to the helicopter fittings if the wind exceeds | 25 knots |
| Long term control deviations are executed by the | Beeper trim valves |
| The electric AP heating must be ON for outside temperatures of | 0*c and below |
| What is the maximum allowable Pressure Altitude with Booster pumps inoperative | 10.000´ |
| VNE Power ON L/L1 | 167 knots <8350 kg. / 150 knots >8350 kg |
| Vno | VNE - 10 knots |
| Max airspeed for flight with sliding doors open | 150 knots |
| What are the NR thresholds for Aural Warnings (NRmin-NRmax) | 92,5% & 109,5% |
| Max taxi speed | 40 knots |
| Max brake speed | 30 knots |
| Slope gradient for shutdown | Nose-up 10* & lateral 5* |
| Engine starts are prohibited without Rotor Brake ON, when wind velocity exceeds | 30 knots |
| What happens when operating the Emergency Cut Off Gangbar | It cuts off Alternator 1 & 2 plus the main battery (+) |
| Max airspeed for operating the landing light | 110 knots |
| Max airspeed with the floats armed Power ON/OFF | Power On 135 knots / Power Off 110 knots |
| Aircraft Engine type & effect | Turbomeca Makila 1A1 1400 kW |
| Size of the cabin door | 1,35 x 1,35 meters |
| What is the clearance under the helicopter | Normal 0.43 meter / Kneeling 0.25 meter |
| What is the clearance under the tail rotor | 1.90 meter |
| What is the clearance under the tail skid | 1.12 meter |
| What's the max speed limit when opening the plug doors? | 55 kts |
| Pitch limits Cruise/Climbing/Max pitch travel stop | Climbing 17.5* / Cruise <8350 kg. 16.5* & Cruise >8350 kg. 16.0* / Max pitch travel stop at 19* |
| Max MGB TQ Limits OEI | 66% No Limit - 69% 2:30 min. (Maximum) - 74% 20 sec. (Transient) |
| Max MGB TQ Limits AEO | 81% No Limit (Max continuous) - 100% 5 min (Maximum) |
| Max NG misalignment between two engines is ... | 1.5% (500 RPM) |
| T4 Limit AEO Take-off rating (5 min) | 795* |
| T4 Limit AEO Max Continuous (Unlimited) | 735* |
| T4 Limit OEI Max Contingency (2:30 min) | 830* |
| T4 Limit OEI Intermediate Contingency (Unlimited) | 785* |
| T4 Starting Unlimited | 750* |
| T4 Starting Transient <25 sec | 780* |
| T4 Starting Maximum Transient <5 sec | 800* |
| T4 Starting Absolute Maximum Transient <2 sec | 810* |
| Engine Intake shall not be ON temperature over ... | + 10* |
| What 3 lights are canceled (disappear) by pressing the WARN buttons? | HYD / FUEL / FIRE Detection System |
| What triggers the landing gear (up) warning buzzer | Below 60 knots & 300´ |
| What 3 aural warnings are there? | Gear / Fire / NR |
| AS332L1 primary electric power is generated by? | Two AC Alternators- 3-phase 20-30 kVA 115 VAC-200 VAC/400 Hz alternators |
| The two Transformers Rectifiers (TRU) generate what voltage? | 28 VDC from alternator #2 |
| Can DC ground power (GPU) be used for engine starting? | No, the engines must be started from the battery or AC |
| The alternators (AC) are driven by the | MGB |
| Alternator (AC) No. 1 (LH) supplies | Aircraft (AC) transformers power system (1XP1) |
| Alternator (AC) No. 2 (RH) supplies | Aircraft (DC) power system via the transformer-rectifiers (TRU) (1XP2) |
| The main battery type/amp? | 24V DC 43 amp NICAD Battery (PP1 Battery Bus & PP2 Essential Bus) |
| Fuel Low Level light comes ON at what level | 71 kg. / 90 l. |
| Does the GPU DC charge the battery? | No |
| Gang-Bar (Emergency Cut-Off) isolates | Alternator 1 & 2 / Battery + / External Power |
| General Cut-Off isolates | Both Alternators (AC) / Main Battery + / Engine Ventilation flaps / Engine Fuel Shutoff levers. |
| Low Fuel Level could be caused by | Low Fuel / Jet pump fail / Both Booster pumps fail / Flap tank valve jammed open |
| The two AC transformers generate what voltage? | 26 VAC from alternator #1 |
| Is the emergency battery AC or DC and what is the voltage & amp? | 24VDC 4Ah |
| How many fuel tanks are standard? | 3LH + 3RH = 6 total |
| What is the standard fuel quantity with 6 tanks? | 1.613 kg. / 2.043 liters |
| How many emergency exits do the aircraft have? | 15 Em. Exits = 12 windows (including the sliding doors) + 2 cockpit doors + optional rear hatch. |
| How many door micro-switches are there? | 11 Micro-switches = 4 on each sliding door + 1 one each cockpit door + 1 on the hatch. |
| At what NG does the 1) starter disengage and 2) the starter sequence stop? | 45% & 65% NG |
| Are there any communication between the engines? | No |
| How many degrees C is the T4 temperature starter datum? | 650*c |
| At what % does the DIFF.NG light come on? | 7.5% NG splitt between the two engines. |
| At what NF % does the engine automatically shutdown due to an overspeed? | 120% |
| At what % does the Bleed Air P1 valve close with & without Bleed Air Offset? | 85% with out & 95.5% with Offset |
| The 5 stages of the engine throttle? | A) Engine Shutdown B) Automatic Starter Detent C) Fast Reduction Detent D) Flight Detent E) Manual Governing Range |
| When does the THROT indicator light go out during a start | When both control levers are in the FLIGHT detent, |
| How long can you crank the engine | Max 15 seconds |
| The Governor has 3 NF channels, how many can it loose before the engine shuts down | The engine will automatically shut down if the Governor looses 2 of the 3 channels. |
| Below what oil pressure (bar) does the ENG P1 or P2 come on | Below 1.7 bar |
| After a inflight flame-out, can you restart an engine with a steady OVSP | Yes, this is the correct status of the OVSP light before a normal start. It's a flashing OVSP light that indicates a real overspeed and the engine should not be restarted. Auto shut down with flashing OVSP light is because NF >120 or shaft failure. |
| How many electric heating mats do each engine air intake have | 2 per engine intake and each 115 VAC/400 Hz |
| How many fire detectors are installed for each engine | 6 bimetallic strip detectors are installed in each engine compartment bay. |
| What do the Fuel Shut-off levers control | It shuts off the fuel shut-off valve and the engine compartment ventilation flap. |
| What does the General Cut-out Control | Both engines ventilation compartment flaps, both fuel shut-off valves and the electric power alternators (AC), the battery +/- contractors. |
| What is the NR Range power ON | 92.5-103.8 % |
| Minimum & maximum NR range power ON including Max Emergency | 92.5-109.5 % |
| Describe the different RFM Vol 1 Sections 1-5 | 1) General 2) Limitations 3) Emergency Procedures 4) Normal Procedures 5.1) Performance Data |
| Describe the different RFM Vol 2 Sections 5-9 | 5.2) Additional Performance Data 6) Weight & Balance 7) Systems 8) Servicing 9) Operational Info |
| What are PINK revisions in the RFM | Conditional Revisions |
| What are YELLOW revisions in the RFM | Rush Revisions |
| What is on the PP1 circuit Essential Safety Consumers | Essential Safety Consumers - Battery ON/OFF (Fire Ext/Utility light/Dingy etc) |
| What is on the PP2 circuit Safety Consumers | Safety Consumers - Battery ON (ENG Gov/ENG NG/Fire Detect/Fire Ext./Fuel Boost/Transponder/ICS) |
| The MGB contains how many liters with oil? | 21,4 liters |
| What is the minimum oil level the MGB main pump has to have to function | 8 liters |
| What is the minimum oil level (liters) required for the MGB standby pump to function | 0 liters - no lower limit |
| The MGB cooler has a minimum oil pressure level requirement of __ to function | 3 bar |
| Where does the rotor brake get it's hydraulic fluid? | LH reservoir |
| There is two type of rotor braking? | Static (rotor stop for the start) & Dynamic (rotor stop after flight) |
| How long can you run the engine with a static rotor brake ON | Max 5 min. |
| What is the procedure if you have used the rotor brake twice within 5 min. | Must wait 15 min before using the rotor brake again including 10 min with rotor turning. |
| How many engines can you start with the rotor brake on | Only 1 |
| What is the pressure and flow rate of the main hydraulic pumps? | 175 bar & 27 l/min |
| What is the normal volume in liters for the hydraulic reservoir? | 8 liters |
| In addition to the normal 8 liter volume in the LH hydraulic reservoir; there are 3 other volume limits, 4, 2 and 0 liters. What factor do they have? | 4 l. level that triggers LH.LEV light and tail rotor shut off valve / 2 l. main pump oil level / 0 l. Aux Pump oil level. |
| Why would you get the hydraulic LH.P & RH.P warning light | Hyd. pressure below 80 bar. |
| What happens when the LH Hydraulic drops below 80 bar? | You get the LH.P light and the AUX pump starts. |
| The Aux. Pump is electrically driven, but what are the pressure ranges | Low pressure on battery; 80-100 bar / In flight or on GPU; 110 - 140 bar |
| What happens if the hydraulic oil goes below the 6 l. level in the LH system | Not able to use the emergency hand pump for the landing gear. |
| How long can the Aux. pump run with a pressure below 80 bar | 6 sec. before automatically shutting down |
| When would you get the RH.L light | Hydraulic oil level under 2 liter in the RH system |
| How long will the Aux. pump run with full oil reservoir | Max 10 sec. |
| Sponson tanks feed fuel into which tank? | Longitudinal (feeder) tanks |
| How many brake application/release cycles does the brake accumulator hold before the accumulator needs recharging | 20 application/release |
| What is the procedure after hard braking | Minimum 5 min with gear down before retracting |
| The landing gear "L/G SIG" means | Loss of 28 VDC supply to indicating sensors (cockpit indications) |
| The landing gear "L/G CONT" means | Loss of 28 VDC supply to control the solenoid valves (electrical control) |
| Three successive operations of the starter are permitted, followed by ___ min cooling down periode. | 20 min. |
| When does the landing gear warning light LG come on. | 1) When below 60 IAS & 2) with the buzzer 60 IAS + <300` |
| Max temperature IGB & TGB (tail gear box) | 120*c |
| Max wind for high wind starts | 65 knots from +/- 20* of nose |
| Max demonstrated cross/tail-wind limitation | 35 knots |
| When do you turn on AP heating 1) Hot P2 Air Heat 2) Electric Heating | 1) Hot P2 air heating below 15*c & 2) Electric heating below 0*c |
| At what IAS does the function HDG Hold convert to Coordinated Turns | 40 knots IAS |
| Which DG provides the autopilot YAW channel with gyro magnetic heading data | DG2 |
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