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tecnam P2006T > POH > Flashcards

POH Flashcards

(61 cards)

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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
slow flight clean
19-20 MAP | 5-10 kts before target speed increase power
26
slow flight training speeds
clean 80 kts | full landing configuration 65 kts
27
Stall
``` natural horizon min 2000 ft after stall props full forward after idle no assymetric power airwork checks and SLV ```
28
stall clean configuration
12,5 degree pitch | 84 kts
29
stall approach configuration
7,5 degree pitch | 84 kts
30
stall landing configuration
``` Takeoff flaps initially 7,5 degree pitch 84 kts positive climb gear up hereafter 12,5 degree pitch 84 kts ```
31
spin recovery procedure
``` 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
G forces in turn (load factor)
load factor = 1 / cos (bank angle)
33
new stall speed
new stall speed = Vs x sq( load factor)
34
descent and approach checks
10 nm before entering CTR
35
downwind checks
``` 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
before landing checks
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
approach speed zero flap
abeam threshold 95 kts | short final 86 kts
38
Go around
``` props full throttle full 7,5 pitch flaps max TO 84 kts positive climb gear up! flap retract climb 84 kts climb checks ```
39
turn during IMC
the lessor of ``` 25 degree bank rate 1 (3 degrees pr second) rule of thumb = 10% IAS +7 = bank angle ```
40
take off distance shall be determined with
``` 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
landing distance
glide 1,3 VS1 until 50 ft
42
minimum flight altitudes VFR
over congested areas 300m (1000ft) with a radius of 600 meter other areas 150m (500ft) with a radius 500m
43
aeroplane operating lights VFR
day anti collision light system ``` night naviagation and position and two landing light or two fillaments aircraft supplied instrument lighting backup torch ```
44
take off perfomance requirements found in
AFM and AIC B-24/08
45
landing perfomance requirements found in
AFM and AIC-11/05
46
mass and balance perfomance requirements found in
AFM and BL 5-5
47
holding fuel same airport
VFR day 30 min | VFR night and above clouds 45 min
48
holding fuel different airport
``` 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
VNE
171 kts
50
VNO max structual cruising speed
138 kts
51
VA design manoeuvering speed | VO operating maneuvring speed
122 kts
52
VLE
122 kts
53
VLO
122 kts
54
VFE
full 90 kts (POH 93 kts) | TO 112 kts (POH 122 kts)
55
VMC
62 kts
56
Blue line, best climb OEI
84 kts
57
straight departure
track guidance VOR,NDB,RNAV within 10,8 NM of DER. It may not included turns more than 15 degrees
58
turning departure
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
omni directional departure
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
ROC/ROD
gradient (%) x GS = ft/min
61
minimum obstacle clearance in holding
1000 ft

tecnam P2006T (1 decks)

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