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AOM DHC-8-400 > Limitations > Flashcards

Limitations Flashcards

1
Q

What is the Maximum Ramp weight?

A

65,400 lb

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2
Q

What is the maximum takeoff weight? (MTOW)

A

65,200 lb

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3
Q

What is the maximum landing weight? (MLW)

A

62,000 lb

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4
Q

What is the maximum zero fuel weight?

A

58,000 lb

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5
Q

Centre of gravity limits, fwd and aft?

A

Fwd: 13.8% MAC

Aft: 36% MAC

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6
Q

What are the max cargo compartment weights?

A

Cargo compartment #1 (aft floor): 2,800 lbs

Cargo compartment #2 (aft step): 1,000 lbs or 30 bags

Forward cargo compartment #3: 910 lbs

Wardrobe: 160 lbs

Cargo compartments #1 and #2 combined: 2,800 lbs

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7
Q

Airplane must not be operated further than 1 hour flying time from a suitable airport for landing, unless…?

A

Both fwd and aft baggage compartments are empty. (Fire potential)

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8
Q

Maximum fuel imbalance between contents of main fuel tanks?

A

600 lbs

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9
Q

Maximum operating altitude?

A

25,000 ft

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10
Q

Maximum takeoff/landing altitude?

A

10,000 ft

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11
Q

Maximum altitude with landing gear and/or flap extended?

A

15,000 ft

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12
Q

Maximum altitude for airstart?

A

20,000 ft

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13
Q

Maximum runway slope for takeoff and landing?

A

+/- 2%

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14
Q

What is the normal maximum tailwind component?

A

10kt

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15
Q

What are the conditions that must be meet when conducting a takeoff with a tailwind between 10 and 20 KIAS (max)?

A
  • Nosewheel steering is operative
  • Antiskid is operative
  • Flight Spoilers are operative in ground and flight modes
  • Bleed air is selected OFF prior to takeoff
  • Runways are not contaminated
  • Takeoffs are conducted with flap 10 or 15
  • NTOP takeoff power rating is used
  • Takeoff is not conducted in icing conditions
  • Appropriate takeoff performance is provided in the Takeoff/ Landing Report (TLR)
  • not in Icing conditions or contaminated runway
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16
Q

What are the conditions that must be meet when conducting a landing with a tailwind between 10 and 20 KIAS (max)?

A
  • Nosewheel steering is operative
  • Antiskid is operative
  • Flight Spoilers are operative in ground and flight modes
  • Bleed air is selected OFF prior to landing
  • Runways are not contaminated
  • Landings are conducted with flap 35 with props 1020/max (850 rpm is not approved)
  • CAT II operations are not authorized
  • Appropriate landing performance is provided in the TLR.
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17
Q

What is the maximum operating ambient temperature limit?

A

50 C or ISA +35C

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18
Q

What is the minimum operating ambient temperature limit?

A

-54C

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19
Q

What are the maximum crosswind components for landing/takeoff:

On a Dry/wet runway?
Contaminated (up to 0.59 in)?
Compacted snow?

A

Dry/Wet: 32 kt (CAT II landing, 18 kt)
Contaminated: 14kt (CAT II, 14kt)
Compacted snow: 20 kt (CAT II, 18 kt)

Notes:

  • T/O with reduced power is prohibited
  • Max alt for T/O and landing is 6,000 ASL, max contaminate depth: 6cm (2.4 in)
  • Selection of power levers AFT of DISC is prohibited.
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20
Q

Maximum headwind component for a CAT II landing?

A

24 kt

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21
Q

Minimum turn radius required (180 deg turn)?

A

85 ft

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22
Q

Minimum runway width required?

A

98 ft

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23
Q

VFE speeds 5, 10, 15, 35?

A

Flap 5: 200 kt
Flap 10: 181 kt
Flap 15: 172 kt
Flap 35: 158 kt

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24
Q

VA (Maneuvering)?

A

204 kt

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25
Q

VLO (Landing gear operating)?

Extend or retract the gear

A

200 kt

26
Q

VLE (landing gear extended)?

A

215 kt

27
Q

Rough air speed (severe turbulence)?

A

210 kt

28
Q

Alternate Gear Extension Speed?

A

185 kt

29
Q

Maximum tire ground speed?

A

182 kt

30
Q

Maximum takeoff rating (MTOP) is limited to?

A

10 minutes

31
Q

Transient power (torques 135%) is limited to?

A

20 seconds

32
Q

Minimum oil temperature to unfeather propeller?

A

-18C

33
Q

Maximum oil temperature between discing and flight idle?

A

125C

34
Q

Maximum oil temperature permissible for completion of flight with a 20% reduction in power?

A

115C. maintenance action required prior to next flight.

35
Q

Maximum oil pressure at discing with OAT below 0C?

A

165 PSI

36
Q

Maximum allowable continuous NP over speed is?

A

1,071 RPM

37
Q

Starter cranking limits?

A

70 sec on: 2 min off
70 sec on: 2 min off
70 sec on: 30 min off

38
Q

Minimum SAT for engine relight is?

A

-40C

39
Q

Reduced takeoff power is prohibited if?

A
  • First flight of the day
  • Tailwind component exceeds 10kts
  • Windshear is present or suspected
  • Takeoff is conducted on a contaminated runway
40
Q

Reduced Np landings are prohibited when:

A
  • tailwinds exceed 10kts
  • anti skid is inoperative
  • CAT II approaches
  • flight spoilers are in GND mode
  • runways are contaminated
41
Q

With engine bypass doors open, maximum takeoff power (MTOP) and maximum continuous power (MCP) settings are limited to?

A

A maximum ambient temperature limitation of ISA +25C

42
Q

Takeoff with bleed ON is prohibited when:

A

Operations are conducted with maximum takeoff power and uptrim disabled.

43
Q

Landing with bleed ON is prohibited when:

A

Tailwind component exceeds 10kts

44
Q

APU stared limitations:

A

1st- 1 min on: 5 min off

2nd- 1 min on: 30 min off. Maintenance required

45
Q

APU limitations (6):

A
  • APU is approved for ground operation only
  • APU must be shut down prior to takeoff
  • must not be operated unattended with pax onboard
  • must not be operated during gravity refuelling
  • ambient temperature limitations (lower) -54C
    Note: when it has been shut down in -35C for more than 1 hour, is must be preheated.
  • ambient air temperature limitations (upper): +50C or ISA +35C, whichever is lower
46
Q

Usable fuel tank capacities are:

A

5,862 lb (2,659 kg) per tank (2 tanks)

47
Q

Auxiliary fuel pumps.

A

Must be on for takeoff and landing.

48
Q

Takeoff and continuous in-flight operation with fuel heater outlet temperature indication below _____ or above _____ is prohibited.

A

0C and 71C

49
Q

Torque, normal operating (green arc)

A

0-100%

50
Q

ITT normal operating (green arc)?

A

250C-880C for MTOP and MCP rating

51
Q

Propeller rpm (Np) normal operating?

A

660-1,020 rpm

Caution: (yellow arc) 1,020- 1,071

52
Q

Gas Generator (high pressure) rotor speed indicator (Nh), normal operating (green arc)?

A

64.2% to Nh Maximum limits shown in figure 2-4 for NTOP

53
Q

Oil Temp indicator normal operating (green arc)?

A

0-107C with prop selector OFF

55C (changing to 65C, 3 min after takeoff) to 107C with prop selector TEST or ON

54
Q

Oil Pressure indicator

Min (red radial)?
Caution (yellow arc)?
Low pressure warning light?
Normal operating (green arc)?

A
  • 44 psi
  • 44-61 psi and 72 -100 psi
  • 44-50 psi
  • 61-72 psi
55
Q

Fuel Temperature indicator.

Over-limit (digits)?
Caution (yellow digits)?
Normal operating (white digits)?

A
  • Above 71C
  • below 0C
  • 0 to 71C
56
Q

Ground operations in winds greater than ___kts must be recorded and the maximum wind speed provided to maintenance within 24hrs.

A

50kts

57
Q

What are the minimum dispatch parking brake pressure levels to start engine #1 and engine #2?

A

Engine #2 needs 500psi min

Engine #1 needs 1000psi min

Note: if required you can manually pump up the brake pressure in the #2 Nacelle

58
Q

What are the required oxygen psi levels for:
A) 2 crew?

B) 3 crew?

A

2 crew requires 1050 psi

3 crew requires 1450 psi

59
Q

What are the minimum dispatch limits for hydraulic fluid quantity levels in system 1,2 and 3?

A

40%

60
Q

STBY HYD PRESS and PTU CNTRL switches - Press. Verify the following lights are on: STBY HYD PRESS ON, PTU CNTRL ON and PTU pressure advisory lights.
• Verify MAIN HYD PRESS Indicators showing (2,900 – 3,100 psi)
• Verify STBY HYD PRESS Indicator showing (2,800 – 3,000 psi)
• Verify HYD QTY Indicators – check levels (No. 1, 2 and 3 systems – 40% minimum)

A

Yes

AOM DHC-8-400 (3 decks)

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