C—a new section of spar should be s

C—a new section of spar should be spliced in or the spar replaced entirely.
C—neutral line.
C—2.
C—aids in getting full penetration of the metal and prevents local distortion.
B—so that the airplane will have a nose-heavy tendency.
C—to manufacturer's specifications.
A—each aileron to have a greater up travel (from the streamlined position) than down travel.
C---2, 3. 4, 6, 7. 8.
A—the main hydraulic system.
C—Selector.
C—low accumulator air preload.
C—Pump drive coupling shear section.
B—sequence valve.
B—rotary motion.
C—inlet of the main system pump.
C—too low or no preload in the accumulator.
A—front spar.
A—pulley misalignment.
A—with the aileron in the NEUTRAL position.
C—Expander-tube type.
C—reduce the pressure and release the brakes rapidly
A—collapsed and fluid added at the filler opening.
B—prevent oil from escaping.
B—restrict flow in one direction and allow free flow in the other.
A—O-ring seal.
C—Prevent high pressure from extruding the seal between the moving and stationary part.
A—mineral base oil.
B—fluid pressure into useful work.
C—shear pin.
C—hand pump outport check valve.
A—exhausted or dumped, usually overboard.
C—quickly connecting and disconnecting hydraulic lines without loss of fluid or entrance of air into the
system.
B—Ambient air.
C—impedance.
A—volts.
B—rectifiers.
A—Total resistance will be smaller than the smallest resistor.
A—The hydrometer reading does not require a temperature correction if the electrolyte temperature
is 80ºF.
C—constant voltage and varying current.
A—toward the end of the charging cycle.
C—only No. 2 is true.
B—both No. 1 and No. 2^are true.
A—crew, usable fuel, passengers, and cargo.
A—neither No. 1 nor No. 2 is true.
C—authorized weight of the aircraft and its contents.
C—more restricted than for airplanes.
C—AN-818-8.
C—10 percent of the wall thickness.
A—Eddy current inspection.
C—Clad aluminum alloy.
C—contracts in length and expands in diameter.
C—52-1/2 inches.
A—appear in the heel of a bend in the tube.
B—ls carrying a substance which may be dangerous to personnel.
C—It may be used with steels which have been heat treated for stressed applications.
A—reveal all possible defects.
C—was not thoroughly washed before developer was applied.
B—Intergranular.
C—subject to rotation.
B—for engine cooling purposes.
C—a person should be in the cockpit to operate brakes.

C—Kerosene has a higher heat energy per unit volume than gasoline.
C—hard starting.
A—improper heat treatment.
B—To prevent scratching.
A— 1.63 x 10 to the fourth power.
C—hydraulic lock.
A—nitriding.
C—Better scavenging and cooling characteristics.
C—-slight drop in RPM.
A—excessively enriching the fuel/air mixture,
C—spark plug condition.
B—should be performed parallel to the length of the blade using smooth contours to minimize
stress points.
B—fails to reach idle RPM.
A—Labyrinth and/or carbon rubbing.
B—Turbine inlet temperature.
C—decrease the air velocity and prevent swirling.
A—allow the turbine wheel to cool before the case contracts around it.
B—an increased fuel flow indication on the gauge.
B—thermocouple system.
B—Direct current, series-wound motor.
B—Fuel line for oil dilution system.
A—is greater than the capacity of the oil supply pump.
C—extended cylinder skirts.
C—pump and the internal oil system.
B—where the contact points open.
B—Advance the spark and decrease its intensity.
A—180 apart.
C—high-heat intensity.
C—Distributors.
C—A high-energy spark is required for ignition.
A—an open ground lead in the magneto.
A—A high-tension harness tester.
A—2,3,4.
B—activation of a flyweight cutout switch.
A—float needle valve is worn or otherwise not seated properly.
B—rich at high altitudes.
B—Incomplete fuel vaporization.
B—When the boost pump pressure is greater than fuel pump pressure.
B—provide bleed air for aircraft pneumatic systems.

ผลลัพธ์ (อังกฤษ) 2:

C-a New section of spar should be spliced ​​in or the spar replaced entirely.
C-Neutral line.
C-2.
C-AIDS in getting full Penetration of the Metal and prevents local distortion.
B-so that the Airplane Will have a. Nose-Heavy tendency.
C-to manufacturer's Specifications.
A-each aileron to have a Greater travel up (from the streamlined position) than down travel.
C --- 2, 3. 4, 6, 7. 8.
A-the. Main Hydraulic System.
C-Selector.
C-low accumulator Air Preload.
C-Pump Drive coupling shear section.
B-Sequence Valve.
B-Rotary Motion.
C-Inlet of the Main System Pump.
C-Too low or no Preload in. the accumulator.
A-Front spar.
A-pulley misalignment.
A-with the aileron in the NEUTRAL position.
C-Expander-tube Type.
C-Reduce the pressure and release the brakes rapidly
A-collapsed and Fluid added at the Filler opening. .
B-Prevent Oil from escaping.
B-restrict flow in one direction and Allow free flow in the Other.
A-O-Ring Seal.
C-Prevent High pressure from extruding the Seal between the Moving and stationary Part.
A-Mineral Base. Oil.
B-Fluid pressure Into useful Work.
C-shear pin.
C-Hand Pump outport Check Valve.
A-Exhausted or dumped, usually overboard.
C-Quickly connecting and Disconnecting Hydraulic Lines Without Loss of Fluid or Entrance of Air Into the.
System.
B-Ambient Air.
C-impedance.
A-volts.
B-rectifiers.
A-Total resistance Will be smaller than the Smallest Resistor.
A-The Hydrometer reading does not Require a Temperature Correction if the electrolyte Temperature
is 80ºF.
C. Voltage and current varying -constant.
A-charging toward the End of the Cycle.
C-only No. 2 is true.
B No. 1 and No. 2 ^-both are true.
A-crew, usable fuel, passengers, and. Cargo.
A No. 1 nor No. 2-neither is true.
C-Authorized weight of the Aircraft and its contents.
C-more restricted than for airplanes.
C-AN-818-8.
C-10 percent of the Wall thickness. .
A-Inspection Eddy current.
C-Clad aluminum Alloy.
C-contracts in Length and Diameter Expands in.
C-52-1 / 2 inches.
A-appear in the heel of a Bend in the tube.
B-LS carrying a. substance which May be Dangerous to Personnel.
C-It May be used with steels which have been heat treated for stressed Applications.
A-Reveal all possible defects.
C-was not thoroughly washed before Developer was Applied.
B-intergranular.
C-subject. to Rotation.
B-Engine for cooling purposes.
C-a person should be in the Cockpit to operate brakes. C-UNIT Kerosene has a higher heat per volume than Gasoline Energy. C-Starting hard. A heat-Treatment improper. B-. to Prevent scratching. A- 1.63 x 10 to the Fourth Power. C-Lock Hydraulic. A-Nitridation. C-Better scavenging and cooling characteristics. C - slight Drop in RPM. A-excessively enriching the fuel / Air mixture, C. -spark plug condition. B-should be performed parallel to the Length of the blade using Smooth contours to minimize stress points. B-fails to reach Idle RPM. A-Labyrinth and / or carbon Rubbing. B-Turbine Inlet Temperature. C-. decrease the Air Velocity and Prevent swirling. A-Allow the turbine wheel to cool before the Case contracts Around it. B-an Increased fuel flow indication on the gauge. B-thermocouple System. B-Direct current, Series-Wound Motor. B. Oil -Fuel line for dilution System. A-is Greater than the capacity of the Oil Supply Pump. C-Extended Cylinder skirts. C-Oil Pump System and the internal. B-open where the Contact points. B-Advance and the Spark. Intensity its decrease. A-180 Apart. C-High-Intensity heat. C-Distributors. C-A High-Energy Spark is required for ignition. A an open-Ground Lead in the magneto. A-A High-Tension harness. Tester. A-2,3,4. B-Activation Switch cutout of a flyweight. A-float Needle Valve is worn or otherwise not properly seated. B-rich at High altitudes. B-Incomplete fuel vaporization. When the B-Boost. Pump Pump pressure is Greater than fuel pressure. B-Air Bleed provide for pneumatic Aircraft Systems.