tiredofshoveling
Well-Known Member
answers to atp seminole supplement.
can anyone add to or improve my answers? would be apprecitated.
tos
1. Recite the V speeds. See Page 16
2. What is the maximum demonstrated crosswind component? 17 Knots
3. Describe the Seminole PA-44-180 engine. LHAND
a. 4
b. Lycoming
c. 180 hp @2700 rpm
d. Carburetor
e. Normally Aspirated
f. rotates to the left
g. horizontally opposed
h. engine driven magnetos
i. 4-6 Quart (79) 6-8 Quart (00)
4. Describe the propeller system.
a. Hartzell
b Lowers pitch
c. Blue, Black indirectly
d. Prop Governor
e. Feathers Prop
f. Feathers Prop
g. Rpm is set, prop pitch auto adjusts via governor to rpm set
h. Via engine oil @ various Pressures
i. prop blade aligned with the relative wind
j. Not if Rpm less than 950
k. Prevent feathering below 950
l.Prevent feathering below 950 on engine shutdown
5.Prop lever DRPM, lower airspeed/throttle to maintain < 2700 rpm
6. 14 volt, two 60 amp alt, 35 amp-hour 12 volt battery Overvoltage +17volts = relay disables power supply from given alternator. Running off of battery
7. Annunciator light “0” on ammeter
8.
9. 2 engine driven vacuum pumps
a. AH or H.S.I. if not slaved
b. 4.8-5.2 in Hg @2000 rpm
c. 2
d. annunciator light, red inop on vacuum gauge
10. 2 Units left wing inboard 25 40, outboard 0 10
11. 2 electrical driven pumps, 2 engine driven, 1 heater fuel pump
12.1. electrical boost pump on X
2. cross feed X
3. check fuel pressure X
4. electrical boost pump off X
5. recheck fuel pressure X.
13.
a..Wheel switch, Electrically driven hydraulically reversible pump
b.Hydraulic pressure
c. Spring lock
d. Gear will drop, Green gear down lights
e.
1. less than 15 in MP with gear up
2. Flaps at 25 40 with gear up
3. Gear down on ground with switch up
f. Squat Switch
g. Gear switch down, pull red emergency gear down knob @ less than 100 kts
i. No
j. YES
k. red indicator light
14. hydraulically actuated disk brakes, rear top of NOSE compartment
15 manually operated, spring lock up
16. 0 10 25 40 degrees
17. 200lbs
18. Safety speed for intentional engine failure 82kts
19. flaps, gear, cowl flaps, flight control deflection, sideslip, props
20. aircraft manufacturing under FAR 23.149
21. minimum controllable airspeed with engine out to maintain heading
22. because it increases Vmc
23 1 CG, 2. Density altitude, 3. power, 4, feathered prop 5, gear/flaps 6, 5degree bank good engine
24. engine inop that most adversely affects handling/performance PAST
25. misalignment of fuselage with the relative wind through use of rudder to maintain heading
2-5 degree bank into operation engine “split the ball”
26. 80%
27. Vor every 30 days, transponder, altimeter, pitot-static 24 months ELT 12 months
28. 0 fpm 50 fpm climb
29. A.r.o.w.
30. vfr = land vfr nearest suitable squawk 7600 ifr= squawk 7600 avef for route mea for altitude
31. no because of centrifugal stop pins to prevent feathering upon engine shutdown
32
a. yes under left pilot dash close air intake and storm widow, heat and def on
b. AI, VSI, ALT
c. Under left wing
33.ground “fan” “open” 2 mins flight “open” for15 secs after heater is “off”
34. 110 gallons 2 unusable
35. 100 ll
36. 2 engine driven, 2 electrically 1 heater
37. start, landing, takeoff, maneuvers except steep turns (ATP) fuel tank X over
38 on, off, x feed
39. see above #12
40. adjust mixture, operating engine cowl flap open
41. open cowl flap, enrich mixture, lower nose
42. air pressure decrease as altitude increases
43. outside atmospheric pressure
44. because it measures outside air pressure, may give false operating indications
can anyone add to or improve my answers? would be apprecitated.
tos
1. Recite the V speeds. See Page 16
2. What is the maximum demonstrated crosswind component? 17 Knots
3. Describe the Seminole PA-44-180 engine. LHAND
a. 4
b. Lycoming
c. 180 hp @2700 rpm
d. Carburetor
e. Normally Aspirated
f. rotates to the left
g. horizontally opposed
h. engine driven magnetos
i. 4-6 Quart (79) 6-8 Quart (00)
4. Describe the propeller system.
a. Hartzell
b Lowers pitch
c. Blue, Black indirectly
d. Prop Governor
e. Feathers Prop
f. Feathers Prop
g. Rpm is set, prop pitch auto adjusts via governor to rpm set
h. Via engine oil @ various Pressures
i. prop blade aligned with the relative wind
j. Not if Rpm less than 950
k. Prevent feathering below 950
l.Prevent feathering below 950 on engine shutdown
5.Prop lever DRPM, lower airspeed/throttle to maintain < 2700 rpm
6. 14 volt, two 60 amp alt, 35 amp-hour 12 volt battery Overvoltage +17volts = relay disables power supply from given alternator. Running off of battery
7. Annunciator light “0” on ammeter
8.
9. 2 engine driven vacuum pumps
a. AH or H.S.I. if not slaved
b. 4.8-5.2 in Hg @2000 rpm
c. 2
d. annunciator light, red inop on vacuum gauge
10. 2 Units left wing inboard 25 40, outboard 0 10
11. 2 electrical driven pumps, 2 engine driven, 1 heater fuel pump
12.1. electrical boost pump on X
2. cross feed X
3. check fuel pressure X
4. electrical boost pump off X
5. recheck fuel pressure X.
13.
a..Wheel switch, Electrically driven hydraulically reversible pump
b.Hydraulic pressure
c. Spring lock
d. Gear will drop, Green gear down lights
e.
1. less than 15 in MP with gear up
2. Flaps at 25 40 with gear up
3. Gear down on ground with switch up
f. Squat Switch
g. Gear switch down, pull red emergency gear down knob @ less than 100 kts
i. No
j. YES
k. red indicator light
14. hydraulically actuated disk brakes, rear top of NOSE compartment
15 manually operated, spring lock up
16. 0 10 25 40 degrees
17. 200lbs
18. Safety speed for intentional engine failure 82kts
19. flaps, gear, cowl flaps, flight control deflection, sideslip, props
20. aircraft manufacturing under FAR 23.149
21. minimum controllable airspeed with engine out to maintain heading
22. because it increases Vmc
23 1 CG, 2. Density altitude, 3. power, 4, feathered prop 5, gear/flaps 6, 5degree bank good engine
24. engine inop that most adversely affects handling/performance PAST
25. misalignment of fuselage with the relative wind through use of rudder to maintain heading
2-5 degree bank into operation engine “split the ball”
26. 80%
27. Vor every 30 days, transponder, altimeter, pitot-static 24 months ELT 12 months
28. 0 fpm 50 fpm climb
29. A.r.o.w.
30. vfr = land vfr nearest suitable squawk 7600 ifr= squawk 7600 avef for route mea for altitude
31. no because of centrifugal stop pins to prevent feathering upon engine shutdown
32
a. yes under left pilot dash close air intake and storm widow, heat and def on
b. AI, VSI, ALT
c. Under left wing
33.ground “fan” “open” 2 mins flight “open” for15 secs after heater is “off”
34. 110 gallons 2 unusable
35. 100 ll
36. 2 engine driven, 2 electrically 1 heater
37. start, landing, takeoff, maneuvers except steep turns (ATP) fuel tank X over
38 on, off, x feed
39. see above #12
40. adjust mixture, operating engine cowl flap open
41. open cowl flap, enrich mixture, lower nose
42. air pressure decrease as altitude increases
43. outside atmospheric pressure
44. because it measures outside air pressure, may give false operating indications
