C310 Flashcards
1
Q
NEVER EXCEED SPEED (VNE)
A
223 KIAS
2
Q
Max structural cruise speed
A
181 KIAS
3
Q
Max manoeuvre speed
A
148 KIAS
4
Q
Best angle of climb
A
85 KIAS
5
Q
Best rate of climb also for SE
A
106 KIAS
6
Q
Flap extension
A
0-15 - 158 KIAS
15-35 - 139 KIAS
7
Q
Maximum Cross wind
A
19 KIAS
8
Q
Landing operation speed (Vlo)
A
138 KIAS
9
Q
Landing gear extended speed (VLE)
A
138 KIAS
10
Q
Landing gear operation down (VLO2)
A
138 KIAS
11
Q
Maximum landing light operation
A
130 KIAS
12
Q
Load facto flaps up
A
+ 3.8g and - 1.52g
13
Q
Load factor flaps down
A
+ 2.0
Bill negative
14
Q
Feather check rpm
A
1200 rpm
15
Q
Min rpm for feathering
A
1000 rpm
16
Q
Rpm to test ignition system
A
1700 rpm
17
Q
Rpm to test govoner system
A
1200 rpm
18
Q
During ignition test max drop and max diff
A
50 max drop
150 max diff
19
Q
Climb power settings
A
24.5” at 2700rpm
106 KIAS
20
Q
MTOW/Ramp
A
2500 kg (5500 lbs)
21
Q
MAX LANDING WIEGHT
A
2454 kg (5400 lbs)
Must burn 46 kg fuel before able to land. 100lbs
22
Q
Max ZFW
A
2223 kg (4900 lbs)
23
Q
Total Fuel
A
Total - 628 lts
Total Useabke - 617 lts
24
Q
Main tanks fuel
A
Total fuel - 386lts (193 per side)
Useable fuel - 378 lts (189 per side)
25
Fuel Aux tanks
Total fuel - 242lts (121lts per side)
| Useable fuel - 239 (119lts per side)
26
Planned fuel consumption
120lts/hr
27
Min oil capacity per engine
9 quarts
28
Max oil in sump
12 quarts
29
Max weight in nose locker
158kg
30
Max weight in wing locker
54kg
31
Max weight aft baggage area
72kg
32
Min control speed in air (Vmca)
80 KIAS
33
310R empty weight
1652kg
34
Glide speed
2494kg - 111 KIAS
2313kg - 107 KIAS
2131kg - 102 KIAS
35
Engine
2 X 285BHP at 2700rpm
| 6 Cylinder
36
Take off power/ Max continuous power
Full throttle at 2700rpm
37
Propeller Govoner
Oil pressure drives blades to High rpm ( low pitch )
Spring and counter weight drives blades to low rpm ( high pitch/feather)
38
Electrical system
28v negative ground alternator in each engine.
39
Battery
24v DC
| Located left wing aft of nacelle fairing
40
Taxi fuel
12 lts
41
Variable reserve
15% of flight fuel at 120lts/hr
42
Fixed reserves
45 min 90 lts
43
Holding fuel
75 lts
44
Climb power
24.5” at 2500 rpm
45
Cruise power
Below full throttle height
23” 2450rpm
About full throttle height
22” 2400rpm
21” 2450rpm
46
Fuel flow in cruise and leaning process
90lbs/hr
Lean to peak EGT the. Riches 3 divisions (75 c)
47
Descent procedure
Descent at 500f/min.
Reduce MAP to 20” and 1” per
Min.
Not below 17”-18”
Increase mix on descent to aid cooling.
48
Circuit configuration
Down wind - 18-20”, 2300rpm, 15 degree flap
Abeam threshold - time 20 sec then gear down.
Final - Max RPM, flaps 35 degree
Assymetric circuit
15 degree flaps base and 35 only when sure of making RWY.
49
Committed to land when
Below 400ft AGL or
More than 15 degree flaps selected
50
Aircraft configuration holding
21.5” 2100rpm, flap 15, gear up.
51
Aircraft configuration IAF
20”, 2300rpm, 15 flap, gear up
52
Descent after IAF
15-18”, 2300rpm, 15 flaps, gear down
53
Aircraft configuration FAF
15-18” max rpm, 15 flap, gear down
54
Aircraft configuration circling
18-22”, max rpm, 15 flap, gear down
55
Aircraft configuration missed approach
18-22”, max rpm, retract to 0 flap
56
On approaching fix include 5nm level segment to?
Allow slowing to first stage flap 15 - 158 KIAS
And gear extension speed 139 KIAS
57
Landing light
Used for all night landings
| Exemption speed 130 KIAS
58
Vortex Generators (Vg)
88 VG ON WINGS AND FIN with strakes mounted outboard of each engine nacelle.
Up to 4 missing No change
5 or more missing revert of non Vg limitations
59
Oil checks
Prior to first flight and not more than 3 hours flight time after
60
Cold Start procedure
```
Mixture. Rich
Pitch. Full fine
Throttles. Full
Mags. On
Alternators on
Battery On
Primer. Till positive fuel flow
Throttle Open 1 to 2”
Starter. Engage left engine and repeat for right.
```
61
Cranking starter care
Longer than 50 seconds allow 5 min cool down. As excessive heat can damage a mature windings
62
Hot start procedures
```
Mixture ICO
Throttle full open
Aux pump low for 20 seconds
Aux pump off
Throttle closed
Start normally
```
63
After start procedures
Manifold pressure. Stable
Rpm less than 1000
Oil pressure green working 30 seconds
Suction. Check after each start
64
TKOF safety Breif decision point?
Will be gear up selection when landing ahead option disappears or Vyse reached 106KIAS
65
TKOF safety breif with examining runway
If engine fails prior to decision point. I will close throttles, control aircraft and stop on remaining runway.
66
TKOF safety breif gear up or 106KIAS
```
If engine fails past gear up or 106KIAS I will
lower the nose,
maintain controls at 106KIAS (vyse),
check mixture up
Pitch up
Power up
Identify dead engine
Feather dead engine
Make a circuit and land informing TWR or ATC
```
67
TKOF procedure
```
Power full
Check P and Ts
Fuel flows 130-150 lbs/hr
Vmca 80KIAS
Climb to 50ft at 92KIAS
Gear up nil RWY remaining
Increase speed Vy - 106KIAS
```
68
Climb Procedure
Power 24” 2500rpm
Mixtures lean to 110/lbs per engine
Cowl flaps as required
69
Cruise procedures below full throttle height (65% power)
23” 2300 rpm
70
Cruise procedures about full throttle height
For 22”, 2400rpm
For 21”, 2450
If max MAP achievable is below 21” leave rpm at 2450.
71
Learning procedure in cruise
Lean to peak EGT
en riches 3 divisions (75 f)
Fuel flow should stabilise at 90lbs/hr
72
Short sector power setting ( less then 15min)
22”, 2300rpm
73
Descent Procedure
Calculated at 500fpm
Reduce power to 20” making sure to recursive at 1” per minute.
Set not below 17-18”
En rich mixtures in descent to dec EGT steadily.
74
Asymmetric circuit procedure
Down wind 18-20”, 2300rpm
Abeam threshold 20 sec, turn base, set 15 flap if needed
Final Max rpm
Gear down and flaps 35 once sure of making the landing environment
75
Committed to land when?
Below 400ft AGL OR
| more than 15 flap selected
76
Final approach to land
```
Fuel mains
Aux pumps on
Gear down three greens
Flaps 35
Pitch full fine
Approach speed 93 KIAS
VMCA 80KIAS
```
77
Baulked landing
```
Mixture up
Pitch up
Throttle up
Flaps 15
Gear up positive rate
Flaps 0
```
78
When does the stall warning sound?
4 to 9 kts about stall speed
| 76kts flap down, 70kt flaps up
79
Wing flap system
Split flap design
Actuated my electrical motor
when flap position equals selected position on switch a micro switch de energises flap motor.
80
Landing gear system
Retractable, tricycle type
Gear doors mechanically linked with gear.
Moving selector allows electrical power to energise gear motor.
Motor continues to run till up or down limits reached. Then gear box disconnects electrical power from motor.
81
Landing gear squat switch
Prevents gear retraction on ground
Safety switch on left shock strut.
When compressed switch is open, preventing power reaching gear motor.
82
Landing gear position lights
Three green when locked.
Red light illuminates when any or all gears are in locked.
No light illumination gear is up and locked.
83
Landing gear warning horn
Controlled by throttle and flap position
If throttles retard below 15” with gear up horn will sound
If 35 flaps selected horn will sound
When gear selected up on the ground
84
Landing gear hand crank
Below right front seat edge
About 52 cranks till gear locks.
Clock wise rotation.
85
Fuel low level warning light
When main tanks contain approx 60lbs of fuel each
Provided by two warning lights
Actuated by float switch.
86
Stall warning system
Left wing lead edge
Electrical Heater selected by turning on pitot heat
87
How do vortex generators improve MTOW?
```
By delaying flow separation of airflow.
Improves STOL performance
Reduces stall speed
Reduces Vmca
Improves aileron effectiveness
Improves SE climb performance
```
88
Low system voltage warning
Low system voltage warning lights illuminate when voltage decreases below approx 25v
89
Emergency alternate field switch
Used when alternators won’t self excited. Provides excitation from battery.
