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Delta 7ER IQ > Volume 1 > Flashcards

Volume 1 Flashcards

1
Q

(757) Maximum Operating Altitude

A

42,000 feet pressure altitude

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2
Q

(767-300) Maximum Operating Altitude

A

43,000 feet pressure altitude

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3
Q

Maximum Takeoff and Landing Tailwind Component

A

10 knots, or as permitted by Delta Special Pages (Green Pages)

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4
Q

Runway Slope

A

+ / - 2%

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5
Q

Turbulent air penetration speed

A

290 KIAS / .78 Mach, whichever is lower

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6
Q

The Delta 757 / 767-300 crosswind limit for takeoff and landing

A

40 knots (including gusts)

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7
Q

After takeoff, the autopilot must not be engaged below:

A

200 feet AGL

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8
Q

Use of which secondary flight control is prohibited with the autopilot engaged?

A

Aileron trim

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9
Q

Maximum allowable Headwind when landing weather minima are predicated on autoland operations (e.g. CAT II autoland, CAT III)

A

25 knots

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10
Q

Maximum allowable Crosswind when landing weather minima are predicated on autoland operations (e.g. CAT II autoland, CAT III)

A

25 knots*

Note: The Boeing AFM low visibility autoland crosswind limitation is 25 knots. To both initiate and land, Delta Ops Specs further restricts CAT II and CAT III low visibility operations to a 15 knot crosswind limit. For CAT I or higher visibility, the autoland crosswind limit is 40 knots.

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11
Q

Maximum allowable Tailwind when landing weather minima are predicated on autoland operations (e.g. CAT II autoland, CAT III)

A

10 knots

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12
Q

Autoland ground speed limit

A

165 knots

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13
Q

Autoland flap configuration limitation

A

Autoland authorized for flaps 25 or 30 landing only

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14
Q

When must Continuous Ignition be selected on? (engine start selector in the CONT position)

A

While operating in severe turbulence

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15
Q

What two conditions provide Continuous Ignition automatically?

A
  1. ) Flap lever out of the “UP” position

2. ) In icing conditions when engine anti-ice is on

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16
Q

(757) EGT limit during engine start

A

485°C - 545°C (if start EGT surpasses 485°C, but does not exceed 545°C, engine shutdown is not required. Make a logbook entry and contact MCC)

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17
Q

(757) Continuous EGT limit

A

615°C

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18
Q

(757) Takeoff EGT limit - 5 minutes (some ship #s allow for 10 minutes)

A

645°C

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19
Q

Which thrust control mode is not permitted for takeoff on the 757?

A

N2 control mode (ENG LIM PROT light illuminated)

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20
Q

Engine Starter Duty Cycle

A

Continuous for 5 minutes. Cool for 30 seconds per minute of operation

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21
Q

APU Starter Duty Cycle

A

Maximum of 3 consecutive starts or attempts within a 60 minute period

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22
Q

APU bleed air limitation (in flight)

A

APU bleed air is available up to approximately 17,000 feet

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23
Q

Maximum altitude for flap extension

A

20,000 feet

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24
Q

Maximum allowable in-flight difference between Captain and First Officer altitude displays for RVSM operation

A

200 feet

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25
Q

Maximum allowable on-the-ground differences between Captain and First Officer altitude displays for RVSM operation (multiple)

A

25-50 feet. The limit varies depending upon pressure altitude and whether you’re in a 757 or 767. See chart on page L.10.9

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26
Q

Maximum allowable difference between Captain or First Officer altitude displays and field elevation

A

75 feet

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27
Q

Prohibited fuel types

A

Jet B and JP4

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28
Q

Maximum fuel temperature

A

49°C (120°F)

29
Q

Maximum fuel imbalance for dispatch

A

1,500 pounds

30
Q

Minimum inflight fuel tank temperature for Jet A

A

-37°C (3°C above the freeze point)

31
Q

Can the PF make aircraft configuration changes?

A

Yes. NP.10.4 states: If operational necessity requires an immediate configuration change and the PM is occupied with other duties, the PF may announce the change and move the appropriate control. This should be understood as the exception and not the rule.

32
Q

When must the Preflight Checklist be re-accomplished?

A

If all pilots vacate the flight deck after accomplishing the Preflight Checklist the first time

33
Q

How are runway/approach change items depicted on the checklist?

A

The symbol ■ precedes items that should be re-accomplished in the event of a runway, intersection, departure, performance data, approach change, or a go-around.

34
Q

Stabilized approach criteria that must be met by no lower than 1000 feet AFE:

A
  1. ) Fully configured for landing (gear and landing flaps extended)
  2. ) Maintain a stabilized descent rate not to exceed 1,000 fmp
  3. ) Aligned with the intended landing runway
35
Q

Stabilized approach criteria that must be me by no lower than 500 feet AFE:

A
  1. ) On target airspeed

2. ) Engines stabilized at the thrust setting required to maintain the desired airspeed and rate of descent.

36
Q

Low level limit for crew oxygen

A

1,000 psi. If crew oxygen pressure is below 1,000 psi, contact maintenance.

37
Q

Who normally loads the FMS, ACARS, etc. prior to each flight?

A

The pilot flying (PF), but either crewmember can complete it. In any case, both the PF and PM must confirm the FMS preflight entries.

38
Q

When does the First Officer select the Transponder to ON / ALT ON / or XPDR as appropriate for the local airport operating procedures?

A

When pushback clearance has been received.

39
Q

Re-engagement of the engine starter with N2 in excess of _____ will result in serious damage to starter and engine.

A

20%

40
Q

When is the FUEL CONTROL switch positioned to RUN during an engine start?

A

When N2 is at 25%.

Note: if 25% N2 is not possible at maximum motoring, attempt the start at a minimum of 18% N2 (757) / 15% N2 (767).

41
Q

During single-engine taxi, with engine anti-ice required, what specific pack / bleed configuration is required?

A

Operate only one pack.

42
Q

How can center tank UFI lockout be prevented during engine shutdown. (e.g. extended ground delay on taxi out)

A

Center fuel pumps must be turned off prior to engine shutdown.

43
Q

How many minutes should the engines be operating before applying takeoff thrust?

A

Minimum of 5 minutes (do not delay takeoff after 3 minute warm-up period)

44
Q

What is the recommended engine cool down time frame before shutdown?

A

3 minutes, but shutdown may be accomplished earlier for gate arrival.

45
Q

What weather minimums dictate that the Autopilot and Flight Director (if available) will be utilized for all ILS approaches?

A

When the reported weather is below 4,000 feet RVR or 3/4 mile visibility.

46
Q

When must the missed approach altitude be set by on a precision approach?

A

No later than 1,000 feet AFE.

47
Q

What weather conditions require Autopilot use for non-precision approaches?

A

IMC.

48
Q

When must the Autopilot be disengaged on a non-precision approach?

A

No later than 50 feet below DA.

49
Q

How early may V/S be selected prior to a descent point on a non-precision or circling approach? (no VNAV avail)

A

0.2 nm.

50
Q

Would an escape slide deploy if the gate agent were to open the entry door prior to it being disarmed?

A

No, escape slide and powered door opening is disarmed automatically when the door is opened from outside.

51
Q

How often must an Autoland be performed for an aircraft to remain certified?

A

Every 30 days.

52
Q

If differences exist between the Takeoff Data Uplink (TDU) and WDR (Weight Data Record), which is controlling?

A

WDR.

53
Q

Define icing conditions.

A

OAT (on the ground) or TAT (in flight) is 10°C or below and any of the following exist: visible moisture is present, or ice, snow, slush or standing water is present on the ramps, taxiways, or runways.

54
Q

Define visible moisture.

A

Clouds, fog with visibility of one statute mile (1600m) or less, rain, snow, sleet, ice crystals, etc.

55
Q

When is an engine run up recommended to minimize ice buildup during taxi?

A

When engine anti-ice is required and the OAT is 3°C or below.

56
Q

What is the engine run up procedure during taxi in icing conditions?

A

Run the engines up to a minimum of 50% N1 for approximately 1 second duration at intervals no greater than 15 minutes. (60% N1 for 30 seconds in 767-300s with GE engines)

57
Q

When engine anti-ice is required and the OAT is 3°C or below, which type of takeoff is required?

A

Standing takeoff - hold the brakes in position until engines are stabilized at or above 60% N1 before the start of the takeoff roll.

58
Q

When is engine anti-ice required in flight?

A

Engine anti-ice must be AUTO or ON during all flight operations when icing conditions exist or are anticipated, except during climb and cruise when the temp is below -40°C SAT. Engine anti-ice must be AUTO or ON before, and during descent in all icing conditions, including temps below -40°C SAT.

59
Q

What is the fan ice removal procedure during flight in moderate to severe icing conditions for prolonged periods with N1 settings at or below 70%, or if fan icing is suspected due to high engine vibration?

A

Increase thrust on one engine at a time to a minimum of 70% N1 for 10 to 30 seconds every 10 minutes.

60
Q

If ice accumulation is suspected to remain after landing, do not retract the flaps to less than ___ until the flap areas have been checked to be free of contaminants.

A

Flaps 20

61
Q

Maximum depth of runway contaminant (standing water, slush, or wet snow) for takeoff.

A

½ inch (1.2cm)

62
Q

Maximum depth of dry snow on runway for takeoff.

A

4 inches (10cm)

63
Q

Maximum depth of runway contaminant (standing water, slush, or wet snow) for landing.

A

1 inch (2.5cm)

64
Q

Maximum depth of dry snow on runway for landing.

A

4 inches (10cm)

65
Q

For performance purposes, when is a wet runway not wet?

A

If the runway is grooved or has a porous friction overlay in the last 2/3s of the stopping area.

Note: the 757-300 is the exception and cannot benefit from this logic, AWABS will automatically default to “wet” performance numbers when the runway is reported wet.

66
Q

True or False: During hot weather operations, use of RECIRC FAN(s) is recommended.

A

False. Turning on the RECIRC FAN(s) has a negative effect on passenger comfort. This introduces hot ambient air from around the cargo compartments to the mix manifold.

67
Q

What precipitation type(s) and intensities require the Engine Start selectors to be turned to CONT?

A

Moderate to heavy rain, hail, or sleet.

68
Q

How much additional airspeed should be added to the flaps up maneuvering speed on the 757-300 if wing anti-ice is selected on in flight?

A

Up to 5 knots may be added to flaps up maneuvering speed. This additive ensures full maneuver margin (40° bank capability).

Delta 7ER IQ (11 decks)

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