Limitations

Question 1

Maximum Passengers

Answer 1

1. Full - 36/37
2. Combi Alpha 28/29
3. Combi Bravo 20/21
   * 2 children in 1 seat max combined weight 77kgs
   * 6 infants max in cabin
   * 0 pax in freighter config

Question 2

106 weights
Ramp weight
MTOW
MLW
MZFW
Min structural design weight

Answer 2

KG
16,556
16,466
15,377
14,515
  9,707

Question 3

103 weights
Ramp weight
MTOW
MLW
MZFW
Min structural design weight

Answer 3

KG
15,740
15,649
15,377
14,061
  9,707

Question 4

Manouvering Limits

Answer 4

Flaps retracted + 2.5g and - 1.0g

Flaps extended +2.0g and 0.0g

Question 5

Max Lateral Asymmetry

Answer 5

600lbs and 272kg of fuel

Question 6

a) Max Operating Altitude

b) For Take off and landing

Answer 6

25,000 ft

10,000 ft

Question 7

Max runway slope

Answer 7

+
- 2%

*supplement 35, +-3%

Question 8

Max tailwind for take off and landing

Answer 8

10kts

*supplement 3 allows for up to 20kts with restrictions

Question 9

Max crosswind component

Answer 9

36kts on dry hard runway

Question 10

Operating temperatures

Answer 10

+ 48.9 Celsius or +35 Celsius ISA

- 54 Celsius

Question 11

Airspeed Limitations

VMO
0-14,000
15,000
20,000
25,000

Answer 11

IAS
242
239
223
207

Question 12

Airspeed Limitations
Vfe

Flap 5
15
35

Answer 12

IAS
148
148
130

Question 13

Airspeed Limitations

Va
Vlo
Vle
Rough Air
Alternate Gear Ext

Answer 13

163
158
172
180
140

Question 14

Power plant - Torque
Max T/O
NML T/O
Max Cont
STRT
Transient
Max Rev

Answer 14

112.5
99.5
97.5
-
125
90

Question 15

Power plant - ITT 
Max T/O
NML T/O
Max Cont
STRT
Transient
Max Rev

Answer 15

816
785
800
950 - 850 to 950 for 5 secs, 816 to 850 for 20 secs
850
770

Question 16

Power plant - NH %RPM
Max T/O
NML T/O
Max Cont
STRT
Transient
Max Rev

Answer 16

100
100
100
  - 
102
100

Question 17

Power plant - Np RPM
Max T/O
NML T/O
Max Cont
STRT
Transient
Max Rev

Answer 17

1212
1212
1212
  -
1320
1212

Question 18

Power plant - Oil Pressure PSID
Max T/O
NML T/O
Max Cont
STRT
Transient
Max Rev

Answer 18

55 to 65
55 to 65
55 to 65
200 max
  -
55 to 65
* 40 to 55 allowed for engine speeds  below 75%
* 40 PSID for other than engine start req. shut down

Question 19

Power plant - Oil Temp (Mod 8/1050
Max T/O
NML T/O
Max Cont
STRT
Transient
Max Rev

Answer 19

40 to 115
40 to 115
40 to 115
- 40 min
125 max
40 to 115

Question 20

Useable Fuel

Answer 20

Per tank: 1287kg/2839lbs

Total: 2575kg/5678lbs

Question 21

Max speed for unfeathering propeller

Answer 21

165 IAS

Question 22

Start Cranking Limits

Answer 22

Start 1 1 min on/ 2 min off
Start 2 1 min on/ 2 min off
Start 3 1 min on/ 30 min off

Question 23

Max torque with propeller feathered
Min NH
Propeller operation between____ and _____ prohibited
Extended ops with propeller rpm in excess of ______ can only be done with the aeroplane __________

Answer 23

50%
60%
500 and 780 rpm
780 rpm, pointed into wind

Question 24

Max loadmeter readings - DC Generator
Ground
In Flight

Answer 24

0. 8 or 0.7 Mod 8/0481
   * may exceed value for 1 min during engine start

1.0

Question 25

Max loadmeter readings - TRU’s Ground In Flight

Answer 25

1. 0 or 0.5 at or above 10 degrees Celsius | 1. 0

Question 26

Max loadmeter readings - AC Generators Ground In Flight

Answer 26

1. 0 for up to 10 degrees celsius and 0.33 at of above 10 degrees Celsius 1. 0

Question 27

Max loadmeter readings - Inverters Ground In Flight

Answer 27

1. 0 | 1. 0

Question 28

Max altitude for extending landing gear and flaps

Answer 28

15,000ft * 30 min cooling period req. following any two flap cycles which begin and end on 0 degrees unless incorporating Mod 8/0583

Question 29

Max Tyre Speed

Answer 29

139 kts GS

Question 30

Normal cabin differential limit Max cabin differential limit Max cabin differential limit during taxiing, T/O and landing Max cabin altitude

Answer 30

5.5 +- 0.3 5.95 0.5 8000ft

Question 31

Icing conditions exist when SAT on ground and take off is ____ or SAT in flight is ___ and ____________ is present.

Answer 31

10 degrees 5 degrees Visible moisture * engine intake bypass open and ignition switch at MANUAL for engine operations in icing conditions

Question 32

Automatic Flight Control System (AFCS) | 11 limitations

Answer 32

1. AFCS approved for Category 1 ops only 2. Pilot must be seated at the controls with a harness 3. The AP must not be manually overpowered 4. AP and FD approaches GS angle 2.5 to 4.0 degrees. GS 3.0 or greater with flap 15 only 5. AP disengage at 200ft above RW elevation on approach 6. AP APP not allowed in SE APP 7. APP mode not allowed with flap 35 8. VOR without its DME not permitted in NAV and APP modes 9. AP backcourse not allowed 10. After T/O and GA, min 1000ft for AP engage. 11. APP must be disengaged in severe icing

Question 33

``` APU Max ambient temp Min ambient temp Must be attended while________ and with_______ Must not be operated while_________ Cranking limits ```

Answer 33

``` +48.9 or ISA+ 35 - 43 Pressure refuelling, passengers on board Gravity refuelling Same as engine starters (same brand of starter) ```

Question 34

``` Hydraulic System Fluids QTS System Normal Min No. 1 No. 2 Emerg ```

Answer 34

NML MIN 2. 68 1.5 5. 19 3.0 1. 25

Question 35

``` Operating Pressures PSI System Normal MIN EDP SPU PTU Low pressure warning Brake Pressure ```

Answer 35

``` NML MIN 3000 2900 2700 2000 3000 1500 ```

Question 36

``` Oxygen Sytem Volume (cu ft, Normal PSI and MIN dispatch PSI Crew fixed Crew Portable Pax First Aid ```

Answer 36

39.4, 1800, 1800 3 crew and 1300 2 crew 11.3, 1800, 1750 4.25, 1800, 1100 11, 1800, 1100