Term
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Definition
1st attempt = Wait 1 Minute
2nd attempt = Wait 1 Minute
3rd attempt = Wait 15 Minutes
4th attempt = Wait 1 Minute
5th attempt = Wait 1 Minute
6th attempt = Wait 60 Minutes |
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Term
| Fire-Extinguishing Agent? |
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Definition
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Term
| Fire Bottle Gauge Pressure |
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Definition
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Term
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Definition
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Term
| Temperature (Operating Limitations) |
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Definition
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Term
| Max TO/Landing Altitude (PA) |
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Definition
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Term
| Max Depth of Water or Slush on the Runway |
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Definition
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Term
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Definition
| with the Cabin Pressurized |
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Term
Thrust Reversers are operated by
(Aeronca) |
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Definition
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Term
| Thrust Reversers are only opereated |
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Definition
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Term
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Definition
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Term
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Definition
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Term
| TR's are "Prohibited" for |
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Definition
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Term
| EMER STOW Inoperative until? |
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Definition
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Term
| What Surfaces are TR's to be used on? |
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Definition
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Term
| Do not Deploy the Drag Chute where? |
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Definition
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Term
| Max Deploy Speed for the Drag Chute? |
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Definition
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Term
| Max Demonstrated Crosswind for Drag Chute |
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Definition
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Term
The nose compartment of the LJ35 contains?
(5 ITEMS) |
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Definition
1.Radar
2.Radios
3.Emergency Oxygen Bottles
4.Emergency Battery
5.Alcohol Tank |
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Term
| A Red DOOR warning light illuminates when the cabin door latching pins are not? |
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Definition
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Term
| A Red DOOR warning light illuminates when the lower door hooking mechanism has not? |
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Definition
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Term
| The only recommended cleaning solutions for the aircraft windshield are? |
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Definition
Water and Mild Detergent or
Aliphatic Naptha Type II (grease remover) IPTM 5A-8 |
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Term
| The overall height of the LJ35 Tail is? |
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Definition
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Term
| The primary danger areas around the aircraft are? (3 ITEMS) |
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Definition
1.Radar emissions (30 Feet) IPTM 5A-14
2.Engine inlet suction (12 Feet)
3.Exhaust plume (40 Feet) |
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Term
| Emergency equipment on the LJ35 consists of? (4 ITEMS) |
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Definition
1.Life Vests
2.First Aid Kit
3.Emergency Tool Kit
4.Emergency Hatchet |
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Term
| All life vests and CO2 cartridges are inspected ________ for condition and cartridge charge. |
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Definition
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Term
| The name of the engines that power the LJ35 is? |
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Definition
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Term
| The two spools in the engine are? |
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Definition
Low Pressure (N1)
High Pressure (N2) |
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Term
| The primary engine indicators that provide engine speed are the? |
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Definition
Fan Speed (N1)
Turbine Speed (N2) |
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Term
| The transfer gear case, which powers the accessory gear case, is driven by the high-pressure spool through a? |
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Definition
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Term
| In the engine's oil lubrication system, an extended _______ located on the right side of the accessory gear case indicates a blockage of the oil filter. |
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Definition
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Term
| The oil pressure gage requires _______ power for operation. |
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Definition
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Term
| Ultimate overspeed protection of 109% N1 and 110% N2 is provided by? |
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Definition
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Term
| With the fuel computer in MANUAL mode, the engine responds slower to ______ movement. |
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Definition
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Term
| The surge bleed valve system, controlled by the fuel computer, is designed to prevent __________ by bleeding low pressure compressor air into the fan duct. |
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Definition
| Compressor Stalls (surges) |
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Term
| With a failed fuel computer or when in MANUAL mode, the surge bleed valve stays? |
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Definition
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Term
| On aircraft equipped with Aeronca thrust reversers, ________ is used for thrust reverser operation. |
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Definition
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Term
| Nacelle inlet lip and fuel computer Pt2/Tt2 heat is provided when the _______ switches are ON. |
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Definition
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Term
| Ignition is active during the start cycle or can be selected manually when the ______ switch is on. |
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Definition
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Term
| During start, DC voltage is reduced to approximately ____ for the first 1.5 seconds to prevent starter torque from breaking the _________. |
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Definition
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Term
| The purpose of cross-start protection is to prevent the opening of a __________ due to the high starter current demand. |
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Definition
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Term
| To ensure continuous operation if the fuel filter clogs, a filter bypass valve ______ to deliver fuel directly to the high-pressure pump. |
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Definition
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Term
| If the bypass valve opens, a __________ on the pump protrudes. |
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Definition
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Term
| Increased fuel scheduling for engine starts is provided by the ____________. |
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Definition
| Starter Pressure Regulator (SPR) switch |
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Term
| Engine synchronization allows the right engine N1 or N2 to be slaved to the _____. |
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Definition
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Term
| An ENG SYNC light illuminates on the glareshield when the engine synchronizer switch is in SYNC and the nose landing gear is ____________. |
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Definition
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Term
| During takeoff and landing, the engine synchronization syetem must be ______ to prevent the possibility of power loss during engine failure. |
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Definition
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Term
| Engine oil level should be checked within ______ after shutdown (preferably within ______ ). |
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Definition
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Term
| The illumination of the red LO OIL PRESS or optional L/R OIL light signals an oil pressure of _________ or lower. |
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Definition
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Term
| With the Aeronca Thrust Reversers installed, the emergency stow system is inoperative with the thrust levers in ______ or above _______. |
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Definition
| CUTOFF or above 70% power angle |
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Term
| The Aeronca Thrust Reversers are armed when the _______ indicates the aircraft is on the ground and the thrust levers are retarded to the __________. |
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Definition
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Term
| Describe how to perform the Aeronca Thrust Reverser Test. |
|
Definition
Press Test Button
-Opens Bleed Valves
-Illuminates the Bleed Valve light |
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Term
| When pulling the engine fire T-handle, the following valves close: |
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Definition
-Main Fuel Firewall Shutoff
-Hydaulic Firewall Shutoff
-Bleed Air Shutoff and Pressure Regulatory valve |
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Term
| The three main components of the fire detection system are? |
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Definition
1. Fire Control Units
2. 3 Sensing Elements/Assemblies (Loops)
3. 2 FIRE PULL/ENG PULL T-handles |
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Term
| The two bottles in the aft compartment contain a fire-extinguishing agent known as? |
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Definition
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Term
| Full discharge of the bottle occurs in? |
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Definition
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Term
| A thermal discharge can be identified by the absence of the _____ indicator disk under the left nacelle pylon. |
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Definition
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Term
| If one fire bottle has been discharged the second bottle is available to? |
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Definition
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Term
| The portable fire extinguisher is available for use in the ________ and ______ compartments and location varies by aircraft. |
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Definition
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Term
| If a bottle is discharged into a nacelle, a _________ manual discharge indicator disk under the left nacelle is ejected. |
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Definition
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Term
| Because Halon is ________, engine or nacelle cleaning is not required after discharge. |
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Definition
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Term
| An illuminated-ARMED light does not _____ fire bottle discharge readiness. |
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Definition
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Term
| Describe how to perform the Fire Detect System Test. |
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Definition
-Rotary Test Switch
-Push Button
-Both T-handles should Flash |
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Term
| All fueling operations for the aircraft are accomplished through the fuel filler ports in the? |
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Definition
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Term
| The tip tanks hold approximately _______ pounds of kerosene each. |
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Definition
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Term
| The tip tanks supply fuel to the wing tanks via a ________ installed in the bottom of each tip tank. |
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Definition
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Term
| Fuel in the upper portion of the tip tank gravity flows into the wing tanks through a _________. |
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Definition
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Term
| ________ in the aft end of the tip tanks permit the fuel to be jettisoned. |
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Definition
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Term
| A ________ and a ________ are installed in each wing tank sump. |
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Definition
| Jet Pump and Standby Pump |
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Term
| A ________ in the left wings root area connects the left and right wing tanks and allows fuel transfer between the wing tanks. |
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Definition
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Term
| Two pressure relief valves between the wings prevent over-pressurization during crossflow operations by opening at a pressure of _______ PSID. |
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Definition
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Term
| Both wing tanks hold _______ pounds of kerosene. |
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Definition
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Term
| The wing tanks are vented to the _______ which are vented overboard. |
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Definition
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Term
| The ram air fuel vent system ensures _______ internal tank pressure in flight, preventing possible tank collapse. |
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Definition
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Term
| The fuselage tank holds ______ pounds of kerosene (LJ35) and _______ pounds (Lear 36). |
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Definition
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Term
| A _______ in the bottom of the fuselage tank transfers fuel between the fuselage tank and the wings. |
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Definition
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Term
| A jet pump has _________ and operates on the venturi principle. |
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Definition
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Term
| The ______ switch controls the motive flow valve. |
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Definition
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Term
| A red FUEL PRESS annunciator illuminates if the fuel pressure to the associated engine drops below _________. |
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Definition
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Term
| The Standby pump is a submerged type used for ________,__________,and __________. |
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Definition
Fuel Crossflow
Fuselage Fill Operation
Engine Starting |
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Term
| The standby pump is a standby in the event a __________ should fail. |
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Definition
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Term
| A switch connected to the bypass illuminates the FUEL FILTER annunciator (amber) when a pressure differential indicates either __________ is being bypassed. |
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Definition
| Main Fuel Line Fuel Filter |
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Term
| The quantity indicated on the gage is compensated for fuel temperature, but can be in error as much as ________ pounds in each position; therefore, the most accurate reading is obtained in the ______ position. |
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Definition
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Term
| Moving the XFER-FILL switch to XFER opens the _________ valve and _______ valve. |
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Definition
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Term
| Switching the XFER-FILL switch To XFER turns on the ________ and disables the _________. |
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Definition
Transfer Pumps
Standby Pumps |
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Term
| The _______ illuminates when the fuselage tank is empty and there is no pressure being sensed in the transfer line. |
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Definition
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Term
| Moving the XFER switch to off closes the _______ and _______ valves and turns the _________ off. |
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Definition
Transfer and Crossflow Valves
Transfer Pump |
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Term
| Fuel is transferred from the wings to the fuselage tank by placing the XFER/FILL switch to the ________ position. |
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Definition
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Term
| When the fuselage tank is full, a float switch causes the green FULL light to illuminate and closes the ________ and _______ valves. |
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Definition
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Term
| When the fuselage tank is full, a float switch causes the green FULL light to illuminate and turns off the _________. |
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Definition
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Term
| There is a _________ maximum differential (imbalance) allowed between the tanks when refueling. |
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Definition
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Term
| The LOW FUEL annunciator (RED) illuminates when a float switch in either wing indicates a fuel level below ________ pounds. |
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Definition
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Term
| Describe how to perform the Standby Pump Check. |
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Definition
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