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tecnam P2006T > POH > Flashcards

POH Flashcards

1
Q

Fuel pressure

A

min 0,15 bar / 2,2 psi

max 0,40 bar / 5,8 psi

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2
Q

Guvernor

A

hydraulic controlled. Oil pressure to reduce pitch

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3
Q

maximum operating altitude

A 
14000 ft (4260 m)
above 12500 ft (3810 m) limited to 30 min. without oxygen
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4
Q

ambient temperature

A

-25 to +50 degree celcius

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5
Q

oil temp

A

min 50 degree celcius
normal 90 - 110 degree celcius
caution 50 - 90 and 110 - 130 degree celcius

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6
Q

propeller

A

normal 580 - 2265 rpm

caution 2265 - 2388 rpm

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7
Q

CHT

A

0 - 135 degree celcius

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8
Q

oil pressure

A

min 0,8 bar
normal 2 - 5 bar
caution 0,8 - 2 and 5,8 bar

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9
Q

weights

A

max takeoff weight 1230kg/2712lb
max landing weight 1230kg/2712lb
max zero fuel weight 1195/2635lb

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10
Q

Center of gravity

A

forward limit 0,221m (16,5 % MAC)

aft limit 0,415m (31 % MAC)

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11
Q

approved maneuvers

A 
normal categori CS23 
Any in normal flight
stalls except whip stalls¨
lazy eights
turns with bank less than 60 degrees
chandelle
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12
Q

maneuvers load factor limits

A

+3,8g and -1,78g

+2g and -zero g (with flaps)

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13
Q

Fuel

A

2 tank with 100 liter (26,42 US gal)
maximum 200 liter (52,8 US gal)
maximum usable 194,4 liter (51,35 US gal)

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14
Q

Approved fuels

A

MOGAS ASTM D4814
MOGAS EN 228
AVGAS 100LL

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15
Q

inflight engine restart

A

below 4000 ft
fuel pump on
normal engine starting

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16
Q

bagage load

A

80kg/178lb

max 0,9kg/dm2 or 19bls/sqft

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17
Q

landing gear

A

min 20 bar pressure

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18
Q

preflight inspection

A 
expiry of airworthy certificate
expiry of certificate of registration
expiry of certificate of insurrance
radio operators licens
maintenace release
component list acoording to KOL
walk around
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19
Q

breaking action reduce

A

medium to good 5 kts
medium 10 kts
medium to poor 15 kts

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20
Q

tail wind operation

A

max 5 kts

max 10 kts with 1200 m or more and hard surface runway

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21
Q

tire limits

A

104 kts/ 120 mph

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22
Q

wake turbulence

A

sink rate 400-500 kts

horizontal speed 5 kts

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23
Q

airwork checks

A 
fuel selectors 
fuelpumps
carb heat
props 2250 rpm
fuel level
eng. instruments
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24
Q

prop slipstream

A

both turning right (clockwise)

nose left

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25
Q

slow flight clean

A

19-20 MAP

5-10 kts before target speed increase power

26
Q

slow flight training speeds

A

clean 80 kts

full landing configuration 65 kts

27
Q

Stall

A 
natural horizon 
min 2000 ft after stall
props full forward after idle
no assymetric power
airwork checks and SLV
28
Q

stall clean configuration

A

12,5 degree pitch

84 kts

29
Q

stall approach configuration

A

7,5 degree pitch

84 kts

30
Q

stall landing configuration

A 
Takeoff flaps
initially 7,5 degree pitch 
84 kts
positive climb gear up 
hereafter
12,5 degree pitch 
84 kts
31
Q

spin recovery procedure

A 
throttle idle
neutral ailerons
rudder opposite direction of spin
yoke fully forward
neutralise rudder when rotation stops
recover from ensuing dive - airspeed below VA by pulling moderate G's
32
Q

G forces in turn (load factor)

A

load factor = 1 / cos (bank angle)

33
Q

new stall speed

A

new stall speed = Vs x sq( load factor)

34
Q

descent and approach checks

A

10 nm before entering CTR

35
Q

downwind checks

A 
fuel pumps on
power 22 MAP /carb 2250 rpm
carb heat on
flaps TO below 112 kts
taxi light on
trim for 90 kts
36
Q

before landing checks

A

flaps TO confrim
gear down 3 green
landing lights on when cleared to land
power 18-12 MAP

short final +100ft
gear down 3 green confirm
props fully forward
carb heat check off

speed on final
75 kts flap full
80 kts flap TO

37
Q

approach speed zero flap

A

abeam threshold 95 kts

short final 86 kts

38
Q

Go around

A 
props full
throttle full
7,5 pitch
flaps max TO
84 kts
positive climb gear up!
flap retract
climb 84 kts
climb checks
39
Q

turn during IMC

A

the lessor of

25 degree bank
rate 1 (3 degrees pr second)
rule of thumb = 10% IAS +7 = bank angle
40
Q

take off distance shall be determined with

A 
all engines at max thrust
cowl flaps in normal position for takeoff
VLOF equal/more VMC
V50 equal/more 1,1*VMC or
1,3*VS1 or
VX + 4
41
Q

landing distance

A

glide 1,3 VS1 until 50 ft

42
Q

minimum flight altitudes VFR

A

over congested areas
300m (1000ft) with a radius of 600 meter

other areas 150m (500ft) with a radius 500m

43
Q

aeroplane operating lights VFR

A

day
anti collision light system

night
naviagation and position and
two landing light or two fillaments
aircraft supplied instrument lighting
backup torch
44
Q

take off perfomance requirements found in

A

AFM and AIC B-24/08

45
Q

landing perfomance requirements found in

A

AFM and AIC-11/05

46
Q

mass and balance perfomance requirements found in

A

AFM and BL 5-5

47
Q

holding fuel same airport

A

VFR day 30 min

VFR night and above clouds 45 min

48
Q

holding fuel different airport

A 
taxi fuel
trip fuel
route reserve min 5% of trip
holding VFR day 30 min/VFR night and above clouds 45min
alternate fuel
extra up to the commander
49
Q

VNE

A

171 kts

50
Q

VNO max structual cruising speed

A

138 kts

51
Q

VA design manoeuvering speed

VO operating maneuvring speed

A

122 kts

52
Q

VLE

A

122 kts

53
Q

VLO

A

122 kts

54
Q

VFE

A

full 90 kts (POH 93 kts)

TO 112 kts (POH 122 kts)

55
Q

VMC

A

62 kts

56
Q

Blue line, best climb OEI

A

84 kts

57
Q

straight departure

A

track guidance VOR,NDB,RNAV within 10,8 NM of DER. It may not included turns more than 15 degrees

58
Q

turning departure

A

track guidance within 5,4 NM after completing required turn. Turns below 394 ft above DER are not alowed and minimum obstacle clearance of 295 ft must be availible before turn is initiated.

59
Q

omni directional departure

A

when track guidance is not availible.
may not include turns below 394 ft DER and these turns may not exeed 15 degrees unless obstacle clearance of 295 ft can be maintained.
If no particular omnidirectional departure is described a straight cimb to 394 ft DER is assumed. hereafter a turn in all directions is possible while maintaining a 295 ft obstacle clearance.

in these cases greybird uses circling altitude

60
Q

ROC/ROD

A

gradient (%) x GS = ft/min

61
Q

minimum obstacle clearance in holding

A

1000 ft

tecnam P2006T (1 decks)

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