Test
Piper Seminole: PA-44-180
Preguntas del test (101)
1Wing area
- A183.8 square feet
- B182.8 square feet
- C183.6 square feet
- D182.6 square feet
2Wing span
- A38 ft. 8 in
- B36 ft. 8 in
- C38 ft. 7 in
- D36 ft. 7 in
3Wing tip
- A2 ft 1.20 in
- B2 ft 1.18 in
- C3 ft 1.20 in
- D3 ft 1.16 in
4Width
- A27 ft 7.20 in
- B25 ft 7.18 in
- C28 ft 7.20 in
- D26 ft 7.18 in
5Height
- A8 ft 6 in
- B6 ft 8 in
- C7 ft 6 in
- D8 ft 7 in
6Elevator height
- A10 ft
- B11 ft
- C12 ft
- D9 ft
7Minimum turning radius
- A33 ft
- B32 ft
- C34 ft
- D36 ft
8Propeller Manufacturer
- AHartzell
- BHeartzel
- CMcCauley
- DAirmaster
9Propeller Max Diameter
- A74 in
- B72 in
- C75 in
- D77 in
10Propeller Min Diameter
- A72 in
- B71 in
- C74 in
- D75 in
11Left Propeller Model No
- AHC-C2Y (K,R) – 2CEUF
- BFC 7666 A - 2R
- CHC-C2Y (K,R) – 2CLEUF
- DHC-C2Y (K,R) – 2CUEF
- EHC-C2Y (K,R) – 2CLUEF
12Right Propeller Model No.
- AHC-C2Y (K,R) – 2CLEUF
- BFJC 7666 A – 2R
- CHC-C2Y (K,R) – 2CEUF
- DFC 7666 A - 2R
13Engine Manufacturer
- ALycoming
- BLycuming
- CCummins
- DRolls-Royce
14Engine MAX HP
- A180 HP
- B190 HP
- C170 HP
- D200 HP
15Engine Max Speed
- A2700 rpm
- B2800 rpm
- C2750 rpm
- D2600 rpm
16Engine Model No. (Left)
- AO-360-E1A6D
- BO-370-E1A6D
- CO-360-E1A5D
- DLO-360-E1A6D
17Engine Model No. (Right)
- ALO-360-E1A6D
- BO-360-E1A6D
- CO-360-E1A0D
- DLO-360-E10D
18Engine Type
- AFour cylinder, direct-drive
- Bhorizontally opposed, air-cooled
- CSix cylinder, direct-drive
- Dhorizontally opposed, air-cooled, fuel injected
19Oil Quantity
- A6 QTS (max), 4 QTS (min)
- B7 QTS (max), 5 QTS (min)
- C5 QTS (max), 3 QTS (min)
- D8 QTS (max), 6 QTS (min)
20Recommended Fuel
- A100LL (BLUE)
- B100/130 (minimum grade)
- CJet Fuel
- DG100UL
21Total Fuel
- A110 US GAL, 55 GAL per tank
- B100 US GAL, 50 GAL per tank
- C120 US GAL, 60 GAL per tank
- D90 US GAL, 45 GAL per tank
22Usable Fuel
- A110 GAL, 55 GAL per tank
- B108 GAL, 54 GAL per tank
- C120 GAL, 60 GAL per tank
- D106 GAL, 53 GAL per tank
23Unusable Fuel
- A2 GAL
- B1 GAL
- C3 GAL
- D4 GAL
24Fuel Consumption
- A26 GPH, 13 GPH per engine
- B28 GPH, 14 GPH per engine
- C30 GPH, 15 GPH per engine
- D24 GPH, 12 GPH per engine
25Battery
- A12 V | 35 amp/hr
- B12 V | 60 amp/hr
- C14 V | 60 amp/hr
- D14 V | 35 amp/hr
26MAX GROSS WEIGHT
- A3800 LBS
- B3900 LBS
- C4800 LBS
- D2800 LBS
27Max Take-off weight
- A3800 LBS
- B4800 LBS
- C3816 LBS
- D3000 LBS
28Max Ramp weight
- A3816 LBS
- B3800 LBS
- C3815 LBS
- D3850 LBS
29Max Landing weight
- A3800 LBS
- B3870 LBS
- C3100 LBS
- D3300 LBS
30Baggage Area and weight capacity
- A24 cu. Ft, 200 LBS
- B25 cu. Ft, 180 LBS
- C24 cu. Ft, 300 LBS
- D26 cu. Ft, 200 LBS
31Wing Loading
- A21.1 lbs/sq. ft.
- B21.2 lbs/sq. ft.
- C22.1 lbs/sq. ft.
- D23.1 lbs/sq. ft.
32Power Loading
- A10.56 lbs/hp
- B10.55 lbs/hp
- C11.55 lbs/hp
- D20.55 lbs/hp
33Maneuvering Speed 3800lbs (VA)
- A135 KIAS
- B136 KIAS
- C145 KIAS
- D112 KIAS
34Maneuvering Speed 2700lbs (VA)
- A112 KIAS
- B120 KIAS
- C135 KIAS
- D113 KIAS
35Never Exceed Speed (VNE)
- A202 KIAS
- B203 KIAS
- C169 KIAS
- D205 KIAS
36Maximum Structural Cruising Speed (VNO)
- A169 KIAS
- B179 KIAS
- C202 KIAS
- D160 KIAS
37Maximum Flaps Extended Speed (VFE)
- A111 KIAS
- B110 KIAS
- C131 KIAS
- D101 KIAS
38Maximum Gear Extended Speed (VLE)
- A140 KIAS
- B160 KIAS
- C150 KIAS
- D142 KIAS
39Maximum Landing Gear Extending Speed (VLO)
- A140 KIAS
- B150 KIAS
- C180 KIAS
- D110 KIAS
40Maximum Landing Gear Retracting Speed (VLO)
- A102 KIAS
- B109 KCAS
- C109 KIAS
- D101 KIAS
41Air Minimum Control Speed (VMCA)
- A55 KIAS
- B56 KIAS
- C57 KIAS
- D66 KIAS
42Decision Speed (V1)
- A56 KIAS
- B55 KIAS
- C54 KIAS
- D57 KIAS
43VYSE
- A88 KIAS
- B98 KIAS
- C80 KIAS
- D85 KIAS
44Rotation Speed (VR)
- A70 (short field)
- B75 (normal)
- C80 (loaded)
- D60 (short field)
- E70 (normal)
- F90 (loaded)
45Best Angle of Climb Speed (VX)
- A83
- B82
- C81
- D75
46Best Rate of Climb Speed (VY)
- A88
- B90
- C81
- D85
47Stall Speed (VS0)
- A55
- B57
- C60
- D61
48Stall Speed (VS1)
- A57
- B55
- C60
- D58
49Maximum Demonstrated Crosswind
- A17 KTS
- B15 KTS
- C12 KTS
- D18 KTS
50White Arc (Flap Operating Range)
- A55-111 kts
- B50-110 kts
- C65-111 kts
- D50-111 kts
51Green Arc (Normal Operating Range)
- A57-169
- B58-170
- C57-110
- D55-169
52Yellow Arc (Caution Range)
- A169-202
- B170-201
- C169-201
- D170-202
53Red Radial Line (VNE)
- A202
- B201
- C222
- D212
54Red Radial Line (One Engine Inop., air min. control speed)
- A56
- B55
- C51
- D53
55Blue Radial Line (One Engine Inop., best rate of climb speed)
- A88
- B90
- C70
- D67
56Engine Maximum Rotation Speed (RPM)
- A2700
- B2600
- C2500
- D2650
57Maximum Manifold Pressure
- AFULL THROTTLE
- B15" MP
- C24" MP
- D20" MP
58Maximum Cylinder Head Temperature (CHT)
- A500° F
- B550° F
- C600° F
- D540° F
59Maximum Oil Temperature
- A245° F
- B255° F
- C260° F
- D215° F
60FUEL PRESSURE: Normal Operating Range (Green Arc)
- A0.5-8 psi
- B0.5-9 psi
- C0.8-8 psi
- D1.5-8 psi
61TACHOMETER: Green Arc (Normal Operating Range)
- A500-2700rpm
- B500-2800rpm
- C600-2700rpm
- D100-2700rpm
62OIL TEMPERATURE: Green Arc (Normal Operating Range)
- A75°-245° F
- B75°-255° F
- C85°-245° F
- D75°-245° C
63OIL PRESSURE: Green Arc (LEFT ENGINE)
- A55-90psi
- B60-90psi
- C15-60psi
- D25-60psi
64OIL PRESSURE: Green Arc (RIGHT ENGINE)
- A60-90psi
- B55-90psi
- C90-100psi
- D90-115psi
65OIL PRESSURE: Yellow Arc (Caution/Idle) [LEFT ENGINE]
- A55-90psi
- B15-60ps
- C90-115psi
- D90-100psi
66OIL PRESSURE: Yellow Arc (Caution/Idle) [RIGHT ENGINE]
- A90-100psi
- B25-60psi
- C55-90psi
- D60-90psi
67OIL PRESSURE: Yellow Arc (Warm-up/Taxi/Takeoff) [LEFT ENGINE]
- A90-115psi
- B15-60psi
- C25-60psi
- D90-100psi
68OIL PRESSURE: Yellow Arc (Warm-up/Taxi/Takeoff) [RIGHT ENGINE]
- A90-100psi
- B25-60psi
- C90-115psi
- D15-60psi
69CYLINDER HEAD TEMPERATURE
Green Arc- A200°-435° F
- B200°-500° F
- C200°-435° C
- D200-435 K
70CYLINDER HEAD TEMPERATURE
Red Line (maximum)- A500° F
- B500 K
- C500° C
- D435° F
71The nose gear must not exceed a turning angle of how many degrees when towed?
- A30°
- B20°
- C33°
- D31°
72What is the maximum allowable
RPM drop when checking the
feathering of the propeller?- A175rpm
- B200rpm
- C150rpm
- D100rpm
73What is the first instrument you
should check after starting the
engine?- AOIL PRESSURE GAUGE
- BCYLINDER HEAD TEMPERATURE
- COIL TEMPERATURE
- DFUEL PRESSURE
74What type of fuel system is
normally used to supply fuel to
the engine of the PA-44-180?- AEngine-driven fuel pumps
- BFuel Injected
- CGravity Fed
75What is the normal enroute or
cruise climb speed of the PA-44-180?- A105 kts
- B200 kts
- C100 kts
- D110 kts
76Normal operating range of the
vacuum system- A4.8-5.2 in. Hg.
- B5-6.2 in. Hg.
- C4.6-5.2 in. Hg.
- D4.8-5.8 in. Hg.
77How many voltage regulators are
equipped in the PA-44-180 to maintain
effective load sharing in their electrical
system?- A2
- B1
- C3
- D4
78Squat switch locations for stall warning system and landing gear
- Aleft wing and left main gear
- Bright wing and right main gear
- Cright wing and left main gear
- Dleft wing and right main gear
79The squat switch has two functions on the Piper Seminole when it is on ground
- ARemoves power from the hydraulic pump
- BDeactivates the stall warning
- CActivates pitot heat
- DGives power to the hydraulic pump
80If hydraulic pressure is lost, the landing gear
- Awill free fall down
- Bwill remain retracted
- Cwill get stuck mid extension
- Dwill explode
81Emergency landing gear extension is limited to
- A100 kts
- B200 kts
- C110 kts
- D90 kts
82The Seminole is equipped with brakes on:
- AMain landing gear
- BNose landing gear
- CNose and main landing gear
83How many blades does the propeller of each engine has?
- A2
- B1
- C3
- D4
84This is the capability of a propeller to change the blade angle:
- AControllable Pitch
- BConstant Speed
- CFull Feathering
85How many alternators is the Piper Seminole equipped with?
- A2, one on each engine
- B1 on left engine
- C1 on the right engine
- Dnone
86This is the capability of the propeller blades to align with the relative wind to decrease drag:
- AFull Feathering
- BConstant Speed
- CControllable Pitch
87The Seminole is equipped with this type of flap system
- AManual
- BPneumatic
- CHydraulic
- DElectrical
88The landing gear on the Seminole is:
- AHydraulically actuated, electrically operated
- BManually operated
- CElectrically operated
- DElectrically actuated, hydraulically operated
89The propeller governor constantly varies oil pressure into the propeller hub to change the propeller blade pitch. This is known as:
- AConstant Speed
- BFull Feathering
- CControllable Pitch
90The Piper Seminole has the following wing flaps positions:
- A0
- B10
- C20
- D25
- E30
- F35
- G40
91Pitot tube and static port are combined together and located on the:
- ALeft wing
- BRight wing
- CNose
- DTail
92Regardless of the propeller lever position, what will happen when oil pressure is lost?
- APropeller will feather if the RPM are above 950
- BPropeller will not feather.
- CPropeller will feather regardless of the RPM
- DPropeller will feather if the RPM are below 950
93The stall warning horn is activated by two lift detectors on the leading
edge of the left wing, outboard of the engine nacelle. The inboard detector
activates the horn when the flaps are in the- A0 and 10
- B25 and 40
- C25
- D10
94The stall warning horn is activated by two lift detectors on the leading
edge of the left wing, the outboard activates the horn when the flaps are in positions- A10 and 0
- B25 and 40
- C10
- D25
95The landing gear warning system will be activated under any of the following conditions:
- AGear not locked down with throttle below 15" MP
- BGear not locked down with wing flaps selected from 25 - 40 degrees
- CGear handle up position when on ground
- DAirspeed is below 88 KIAS and the gear is up
- ERPMs drop below 2300 and the landing gear is up
96Alternator
- A14 V | 60 amp/hr
- B14 V | 35 amp/hr
- C12 V | 60 amp/hr
- D12 V | 35 amp/hr
97Safe Speed for intentional engine failure
- A82 kts
- B83 kts
- C81 kts
- D84 kts
98OIL PRESSURE: Red Line (Minimum) [left engine]
- A15psi
- B20psi
- C21psi
- D22psi
99OIL PRESSURE: Red Line (Minimum) [right engine]
- A25psi
- B23psi
- C21psi
- D26psi
100OIL PRESSURE: Red Line (Maximum) [left engine]
- A115psi
- B215psi
- C105psi
- D110psi
101OIL PRESSURE: Red Line (Maximum) [right engine]
- A110psi
- B100psi
- C105psi
- D102psi
Información
- Descripción
- Specifications
- Autor
- Sean Furio
- Idioma
- English
- Visitas
- 137
- Etiquetas
- Valoración
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