ATR 72-600 Limites y sistemas

Maximum operating altitude. 20.000 ft. 25.000 ft. 30.000 ft. 15.000 ft.

Do not operate cargo door with a cross wind component of more than ________knots. 10. 40. 45. 20.

Maximum weight on ramp. 23.000 KG. 23.750 KG. 28.000 KG. 21.000 KG.

Maximum TOW. 23.000 KG. 23.750 KG. 21.000 KG. 20.000 KG.

Maximum MLW. 22.150 KG. 23.000 KG. 21.000 KG. 20.000 LB.

Maximum ZFW. 21.000 KG. 20.000 LB. 23.000 KG. 25.000 KG.

VMO. 250 KT. 150 KT. 150 MACH. 320 KT.

MMO. 250 KT. 0.55 MACH. 55 MACH. 500 K/H.

Maximum operating maneuvering speed VA. 180 KT. 175 KT. 85 KT. 150 KT.

Maximum flaps extended operating speed / Flaps 15. 185 KT. 85 KT. 150 KT. 250 KT.

Maximum flaps extended operating speed / Flaps 30. 150 KT. 185 KT. 165 KT. 160 KT.

VLE. 185 KT. 85 KT. 75 KT. 135 KT.

VLO during extension. 170 KT. 185 KT. 190 KT. 150 KT.

VLO during retraction. 160 KT. 170 KT. 185 KT. 180 KT.

Maximum rough air speed VRA. 180 KT. 190 KT. 170 KT. 125 KT.

Maximum wipers operating speed VWO. 160 KT. No limit. 140 KT. 120 KT.

Starter: ____starts with a ____ minute ____ seconds maximum combined starter running time, followed by ____ minutes off. 3, 1, 30, 4. 2, 2, 30, 5. 1, 1, 30, 4. 1, 2, 25, 5.

REFUELING: Maximum pressure. 50 psi. 60 psi. 25 psi. 500 psi.

USABLE FUEL: Each tank. 2.500 KG. 5.000 KG. 2.5 LT. 25.000 KG.

Tail wind limit: _____kias. 15. 20. 45. 30.

OEB (_______). Operations Engineering Bulletins. Operational Equitment Base. Max Wing Bank Operation. Electrical Bulletins Ops.

The MASTER MEL is more restrictive than the MEL. FALSE. TRUE.

Dark means?. Normal Operation. OFF. Warning. Ready.

Time after DENY to answer (cockpit door). 3 minutes. 2 minutes. 5 minutes. No time.

COCKPIT DOOR: After pressing the button EMERGENCY, how time for the door to open automatically?. 1 minute. 3 minutes. 30 seconds. 20 seconds.

How many doors?. 7. 5. 8. 9.

which systems connected to the battery can discharge it? CRE. C. R. E.

Emergency EXITS. windows (2), service door, main door, emergency hatch. windows (4), documents hatch, main door, emergency hatch, cargo door. windows (4), main door, pilots windows, back hatch, cargo door. window, landing gear hole, bath door, pilots hatch, main door.

LIGHTS: choose the light that corresponds DC/WILD. DC. WILD.

EXIT Light. DC source, 6 volt battery and 10 minutes of durance. It recharges with sunlight and 15 minutes of durance. Wild source, 12 volt battery and 10 minutes of durance. The main battery of the plane turns on the EXIT lights.

MPC (multi propose computer) consist of ______and_______. Copi voice recorder and FMA. FDAU and DMU. Pafeda and CRE. DCTSS and TPS.

CVR (cockpit voice recorder) record with the help of RCAU. TRUE. FALSE.

SSFDR record the crew communication. TRUE. FALSE.

The recording of the CVR (Cockpit voice recorder) stops when. The aircraft touchdown. Brake handle-parking. The pilot switch off. Company stops.

How much time save the cockpit voice recorder?. 30 minutes. 25 hours. 50 minutes.

CDS (Control Display System) integrated by: DISPLAY UNITS.

FWS (Flight Warning System) Identification phases: Information, identification, isolate. Identification, detection, check list. Detection, crew control, isolate. Information, identification, Emergency memory items, check list.

TAT. Total air temperature. Time arrival TCP. Tends animal treatment on board. Crew incapacitation.

FWS (Flight Warning System) When occurs fails, the procedure is... C. I. S. C. L. R.

FWS (Flight Warning System) audible alarms. Single shine. Stall. Repetitive shine. Too low. Siren alarm. High alarm. Fire alarm. Pull up. Don´t sink. Bank angle.

Which are the categories of the MEL. A, B, C and D. 1, 2, 3 and 4. B, C, Z and S. Low, high, medium, delicate.

MEL: Specify the time of each category. A. B. C. D.

The CDL doesn´t have times, the reparations should do always when the items are not more than two and one ATA. TRUE. FALSE.

SPS. Support Power Single Engine. Single Performance Sofware. Secure Performance Speed. Operational Security Program.

The rack that handles the electronic is the one behind the chair of the commander. TRUE. FALSE.

COCKPIT PHILOSOPHY. AMBER. RED. WHITE. BLUE. GREEN.

IMA. Integrated Modular Avionics. Cockpit Door System. Instrumental Avionics Avoidanse. Integrity Manual Aplicate.

The CACs are two cabinets that store 6 IMA cards each one. TRUE. FALSE.

The DU2 and DU4 store Flight Managment aplication and Radio Managment Application. TRUE. FALSE.

The McDU is directly connected to. McDU.

The IESI gives us the following information. Altitude, air speed, attitude, barometric pressure, VHF 1 radio communication, VOR/ILS 1 radio navigation. Air speed, actual time UTC, Airport Elevation and QNH. Bank angle, Air speed, barometric pressure, VHF 2 radio communication, VOR. Stall, pitch, AP, attitude, altitude, airspeed, VOR, ILS, communication 1 and 2.

Emergency Audio Cancel reactivates when. If you re-energize. bad wheather conditions. After MFC 1B/2B reset. High bank angle. After pressing ECL pb. Low bank angle. After presing T.O configuration test. Low Battery less than 5v.

What is the take off configuration test?. It is a test that verifies the required configuration before takeoff. It is a test of the landing gear that must be done on the first flight of the day. It is a test that verifies the appropriate wind conditions to make T.O. It is a test of the landing gear that verifies the hydraulic pressure so that the train climbs without problems after the takeoff procedure.

A limiter that below 180 knots leaves the movement free and above 185 knots limits the free movement of the rudder. Spoilers. TLU. FWS. Stall Alert. GPWS.

A lever that blocks the ailerons and the elevator to prevent wind gusts from causing damage to these surfaces. Gust Lock. ATPCS. Flaps. Brake Handle.

Two minutes after takeoff the pusher is disabled. TRUE. FALSE.

Below 500 feet the pusher is inhibited. TRUE. FALSE.

What are the pusher and the stick shaker. System installed on the chairs to ergonomically adjust the position of the crew. Alert system to awaken the crew when they are tired. Warning system when the aircraft in flight is almost in stall condition. Part of the autopilot system that alerts when it will be disconnected. They make part of the elements of service to passengers to prepare fruit smoothies.

The butterfly valves or bleed valves of the pneumatic system. Electrically controlled pneumatically operated. Electrically operated mechanically controlled. Electrically controlled hydraulically operated. Pneumatically controlled automatically operated.

ISOLATION: The bleed valve is automatically close when.

FIRE PROTECTION SYSTEM /Pulled Fire Handle. P. A. F. E. D. A.

Airplane’s engine. PT6a 67R. M301 wallter. PW 127 N. M601 Walter.

RTO SHP MOTOR. 2750 SHP-reverse take off for 10 minutes (100% NP). 3000 SHP-reverse take off for 20 minutes (100% NP). 2500 SHP- reverse take off 10 minutes (50% NP). 2000 SHP- reverse take off 15.5 minutes (100% NP).

SHP MOTOR MTC. 2500 SHP-MCT-(90.9% NP). 2475 SHP-MCT -(100%NP). 3000 SHP-MCT-(89.9%NP). 2500 SHP-MCT (89.9%NP).

SHP MOTOR TAKE OFF. 2475 SHP T.O- 5 minutes (90%NP). 2500 SHP T.O- 10 minutes (100%NP). 2400 SHP T.O- 5 minutes (89.9 NP). 3000 SHP T.O-10 minuetes (100 HP).

SHP MOTOR CLIMB. 2192 SHP Climb (82 % NP). 2200 SHP Climb (90.8% NP). 2500 SHP Climb (100% NP). 3000 SHP Climb (90.0%NP).

SHP MOTOR CRUISE. 2132 SHP cruise (82% NP). 2000 SHP cruise (90% NP). 5000 SHP cruise (100% NP). 2300 SHP cruise (90.9% NP).

What are the functions of the MFC?. Monitors, controls, authorizes the operation of aircraft systems. Monitors the doors test. Monitors the engine parameters. Links all the DUs.

In a total failure of electrical power of the plane, what are the last dispay that I am going to lose?. DU2 DU4 and IESI. D2 D4. DU1 DU3. DU1 DU2 and security cameras.

what systems are tested with the take off configuration?. TAKE OFF CONFIGURATION TEST.

What are te reasons of the threshold stall modifications?. Activating level two of anti-ice or when the system detects ice conditions. Visible moisture. Level three of anti ice. The airplane detects.

The valves are automatically closed when the bleed duct OVHT 274 C grades, bleed duct leak 153 C grades, Over pressure, ENG fire handle, ENG flame out after take off (uptrim signal), propeller brake ON (left blled valve only), during the ENG start up procedure (is inhibited by 30 s), due to lack of air flow closes due to spring effect. TRUE. FALSE.

When the dump function is available?. When the pressurization system is in automatic mode. When a hard landing occurs. When there is an air leak in the cabin. When the autopilot is disengaged.

What ADC sends information for the automatic pressurization of the plane?. ADC1. ADC1 and ADC2. ADC2. ACW.

These are the conditions for the HYD AUX PUMP to work automatically. P. A. G. O.

FMS adjust order. 1. 2. 3. 4. 5. 6.

Emergency Equipment. Flash lights. Life jacket. Googles. Thermal blanket. Oxy Mask. water bottle. Extinguisher halon. PBE. Ipad. Crash axe.

Conditions to use the icing anti/de system. Ground: OAT <5 grades, snow and water puddle. If the passenger ask for it. Flight: TAT <7 grades visible humidity, clouds, haze, rain, ice cristals. Ground: TAT <2 grades. If the crew is cold. Flight: If the ATC inform icing conditions.

HYD blue/green pumps operation. GREEN. BLUE.

How much time takes the HYD aux pump ante fuel pump after push the button?. 30s. 3s. 15s. 20s.

at what speed the anti skid is available. 10 kt. 5 kt. 20 kt. 10 km.

at what speeds the anti skid test is performed?. In flight test: 3 s/ On ground test 6s. In flight test: 2 s/ On ground test 4s. In flight test: 3 s/ On ground test 2s. In flight test: 7 s/ On ground test 10s.

MAX speed on ground. 150 kt. 165 kt. 175 kt. 180 kt.

Operation grades of NOSE WHEEL STEARING with switch (on). +/-30. +/-60. +/-360. +/-180.

Operation grades of NOSE WHEEL STEARING with switch (off). +/- 91. +/-80. +/-65. 75.

Wheel fusibles melt temp grades. 177. 190. 200. 300.

Brake Tem hot grades. >150. 177. <200. >350.

How many grades of movement of the ailerons spoilers are activated?. 2.5. 5.2. 1.2. 2.05.

Order of activation/ STALL. 1. 2.

ICE AND RAIN PROTECTION. Permanent. Anti icing (electric). De icing (pneumatic).

At what time the RUN pump goes off, after the NH 45?. 30s. 20s. 35s. 1min.

Oil tank storage. 4.4 lt. 1 gl. 3 lt. 5 lt.

Which means the N in the engine reference PW 127 N?. United States registration. Has Boost. It refers to the model of the motor shaft. it is the physical form of the engine.

The power MGT in position T.O can only be used by. 5 min. 10 min. 30 min. 1 h.

The RAPM of the power lever has a limitation. Two ENG 10 min/ one ENG 5 m. Two ENG 05 min/ one ENG 5 m. Two ENG 1 h/ one ENG 30 m. NO LIMITATION.

AUTO IGNITION. N. A. C. E.

The low pitch is?. It is a protection that the blades have so that it goes to the back and gives changes in the blade. When the airplane is going down. A fail. An ítem BEFORE TAKE OFF CHECK LIST.

A.F.U. Auto fix Unit. Automatic Flight Unit. Auto Feather Unit. Simpson character.

PIU. Propeller Interface unit. Performance Limitation unit. Propeller Indication unit. Power Indication Display unit.

TCAS-INHIBIT. 1100 ft climb/ 900ft descent. 500 ft climb/ on land. NO LIMIT. 200 ft after landing/ 100 before land.

EEC (Electronic ENG Control). EEC TAKE DATA FROM.

The PACKS are located in the bay of the main train. LEFT PACK cabin and cockpit air conditioning RIGHT PACK cabin air conditioning. LEFT PACK cabin and cockpit air conditioning RIGHT PACK cabin air conditioning and cellar. LEFT PACK cabin and cockpit air conditioning and lavarory RIGHT PACK cabin air conditioning. These two feed the entire plane including bathrooms and aircraft cellars.

MAIN BATT. 24 V / Ni-Cd / 43 Ah. 12 V / HALON / 45 Ah. 34 V / Ni-Cd / 45 Ah. 18 V / Ni-Cd / 43 Ah.

Do you use the MAIN BATT for?. MAIN BATT.

Do you use the EMER BATT for?. EMERGENCY BATT.

EMER BATT. 24 V / Ni-Cd / 17 Ah. 28 V / Ni-Cd / 43 Ah. 18 V / HALON / 17 Ah. 24 V / Ni-Cd / 34 Ah.

ATPCS ARM CONDITIONS (UPTRIM/AUTOFEATHER) / ON GROUND. ATPCS / GROUND.

ATPCS ARM CONDITIONS (JUST AUTOFEATHER) / IN FLIGHT. ATPCS/FLIGHT.

FIRE. DETECTION. EXTENTION.

Which includes the fuel system?. 1 Electric pump/1 Jet pump in each tank. 2 Electric pump/2 Jet pump in each tank. 1 fuel pump, 1 main tank av gas 100/130. 3 scavation pump and 4 Electic.

TOTAL FUEL. 5000 kg. 2500 kg. 10000kg. 4000kg.

Max unbalance fuel. 730 kg. 2500 kg each tank. 520 kg. 220 lt.