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DE AGA ÉLE provinhas > Study guide > Flashcards

Study guide Flashcards

1
Q

Company Approved CatIII
Where we can find it?

A

OMC 10.3.3.1

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2
Q

Area Briefs, where we can find it?

A

OMC section 8

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3
Q

Aerodrome Limitations and Briefings, Where we can find it?

A

OMC, Section 10.4

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4
Q

Middle East and Asia Climatology, where we can find it?

A

OMC, Section 11.2

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5
Q

Far East Climatology, where we can find it?

A

OMC, Section 11.7

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6
Q

Communication Failure Procedures, where we can find it?

A

-OMC, Section 5.2
-LIDO docs 1.7.2
-ICAO Doc 4444

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7
Q

Communication Failure IFR
Non Radar Area, describe procedure:

A

-7600
-Maintain Spd and Lvl for 20’
-Than Adjust to Flight Plan
-Try to land within 30’ of ETA

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8
Q

Communication Failure IFR
UNDER RADAR SURVEILLANCE, describe procedure:

A

-7600
-Maintain last assigned
Speed and Level for 7’
-Than adjust t o flight plan
-Descent from NAVAID
-IAP of designated NAVAID
-Try to land within 30’ of ETA

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9
Q

Communication Failure IFR
UNDER RADAR VECTORS, without limit given, describe procedure:

A

-7600
-Maintain last assigned
Speed and Altitude
-Proceed in the most direct manner possible to rejoin
the flight plan tracking before the next point.

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10
Q

Minimum FLA corrections
Where we can find it?

A

OMC, section 0.2.1

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11
Q

MFA Correction
Wind speed 0-30kt
Elevation 2000-8000ft

A

500ft

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12
Q

MFA Correction
Wind speed 31-50kt
Elevation 2000-8000ft

A

1000ft

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13
Q

MFA Correction
Wind speed 51-70kt
Elevation 2000-8000ft

A

1500ft

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14
Q

MFA Correction
Wind speed over 71kt
Elevation 2000-8000ft

A

2000ft

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15
Q

MFA Correction
Wind speed 0-30kt
Elevation above 8000ft

A

1000ft

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16
Q

MFA Correction
Wind speed 31-50kt
Elevation above 8000ft

A

1500ft

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17
Q

MFA Correction
Wind speed 51-70kt
Elevation above 8000ft

A

2000ft

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18
Q

MFA Correction
Wind speed over 71kt
Elevation above 8000ft

A

2500ft

Note: 2500ft will cover all situations

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19
Q

Minimum Grid Altitude
OFP LIDO MOCA adjustments

A

0 to 6000ft- 1000ft(round100)
Abv 6000ft- 2000ft(round100)

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20
Q

Airport Category Definitions
Where we can find it?

A

OMC - Section 10.3

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21
Q

Airport Category A,
Definition:

A

-Approved IAP
-No Performance Limitation
-22m wide taxiways
(767 9.3m - 30.6in)
-Circling Minima < 1000ft
-Night Operations
-No Terrain Restrictions

OMC 10.3.1.1

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22
Q

Airport Category B,
Definition:

A

-Doesn’t Satisfy A requiremt
-Non-Standard Approach
-Unusual Weather
-Performance Limitations
-Captain Should self-Brief.
-Tick the box Journey Log.

OMC 10.3.1.2

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23
Q

Airport Category C,
Definition:

A

For DHL:

-Doesn’t Satisfy A nor B
-Additional considerations
-Annual Risk assessment
-Simulator CAA approved.
-Captain Should be Briefed
-Tick the box Journey Log.

OMC 10.3.1.3

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24
Q

Category B Airports
That worths to remember
OMC 10.3.3

A

AMMAN OJAI. - Circling
DJIBOUTI HDAM. -Circling
DOHA. ODTB. -Circling
HNG KNG VHHH -Terrain
LARNACA LCLK. -Circling
NAIROBI. HKJK. -Terrain

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25
Q

Crosswind Limitations
Where we can find it?

A

OMB - Section 1.3.5
QRH - OI Section 0
FCTM - Tkoff Guideline 3.14
- Lndg Guideline 6.40
(TALPA)

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26
Q

Predictive Windshear System
PWS - Parameters are:

A

3NM 25°
12 seconds after start scan

Auto alerts below 1200ft

Auto enable
GROUND Takeoff Thrust
FLIGHT Below 2300ft

27
Q

Auto Throttle Failure,
How to get N1 values?

A

If A/T arm switch:
Select the desired regime at TMSP and adjust manually.

If TMSP check table on the reverse of laminates checklist
and/or

QRH PI - Performance Inflight
10.3 Climb
10.4 GoAround

FCOM - Performance Inflight
General
10.14 Max Takeoff Thrust.
10.19 Takeoff Thrust.
10.27 Max Climb
10.28 GoAround

28
Q

Rescue and Fire Fighting
RFF - DHL Airport Fire Cover
Minimum Categories

A

RFF 7 at destination
RFF 6 for alternates
RFF 5 for EDTO alternates

OMA 8.2.4.9

29
Q

OMA 8.3.9
Wake Turbulence
Distance Separation
on air (approach)

A

767 (H) follow a SUPER 6nm
767 (H) follow a HEAVY 4nm

Enhanced DXB HKG
H follow S = 5NM
H follow H = 3NM

Heavy definition > 136.000Kg

30
Q

OMA 8.3.9
Wake Turbulence
TIME Separation for DEPARTURE

A

Same Departure point
767 (H) follow SUPER or H 2’

Intermediate Point
767 (H) follow SUPER or H 3’

Heavy definition > 136.000Kg

31
Q

LMC
Last Minute Change Limits

A

ZFW 1.100 lb
FUEL 4.400 lb
If exceeded new Load Sheet

OMA 8.1.8.5

32
Q

OFP
Operational Flight Plan
Limit:

A

11.000 lb
If exceeded new OFP must be generated
OMB 5.2

33
Q

On Time Performance
Delays:

A

Up to 5’ no report nor codes
From 5’ to 15’ delay code EFB and logbook.
Beyond 15’ report and logbook

34
Q

ALTERNATE - OMA 8.1
Destination Alternate
When 2 alternates are a must

A

-Destination forecast +-1h
Below minima;

-No meteorological info;

35
Q

ALTERNATE - OMA 8.1
Isolated Alternate 3% contingency
Meteo Minima Requirements

A

-CAT II & III - RVR

-CAT I - above non-precision

-Non-Precsn. - +200ft/ 1000m

-Circling - Circling

OMA 8.1.3.1.4

36
Q

Tankering OMA 8.1.7.1.3
Shall never exceeded:

A

MLW minus 500Kg / 1100lbs

37
Q

Nominate the 3 reasons for tankering

A

P - Price

H - Handling

B - Business

38
Q

Which tankering reasons take precedence over payload? And which doesn’t?

A

Tankering price NEVER takes precedence ove payload
But…
Handling and Business, the DO TAKE precedence over payload

39
Q

DHL policy for fuel price differential exceeds_____ of flight before tankering is considered
OMA 8.1.7.1.3

A

4% per hour of flight

40
Q

Fuel Limitation:
Fuel Tanks max capacity
767-300

A

L 40.267
C 80.132
R 40.267

41
Q

Approved types of Fuel
And it’s respective fuel freezing points

A

JET - A = -40°C
JET -A1 = -40°C
JP - 5 = -40°C
JP - 8 = -46°C

42
Q

Limitations Fuel
Fuel Temperature

A

Max 49°C
Min -45°C or 3° above fuel frz

43
Q

Fuel Limitations
Maximum Imbalance

A

At 48.000lbs main tk - 1500lb
Linear to…
At 79.800lbs main tk - 2500lb

44
Q

Limitations

Maximum Main Deck Load

A

125.000lbs

45
Q

767 Engine CFM
Max EGT during Takeoff

A

960° C for 5 min

46
Q

767 Engine CFM
Max Continuous EGT

A

925°C

47
Q

767 Engine CFM
Max EGT during Start

A

870° C - 40 seconds

48
Q

767 Engine CFM
Max EGT start unlimited

A

750° C

49
Q

767 Engine CFM
Max N1

A

117.5%

50
Q

767 Engine CFM
Max N2

A

112.5 %

51
Q

B767 CFM
Start Duty Cycle

A

Normal: 5’on - 30”off per min

Extnd: two of 5’ -10’ cooling

52
Q

Aborted Engine Start Conditions are:

A

6 items;

1) no EGT within 25’ (wet)
2) impending hot
3) fails to accelerate (hung)
4) no oil press at idle
5) no N1 30’ after idle
6) tail pipe fire

OMB 2 - Normal Procedures
OMB 2.14

53
Q

What rate of imbalance should be considered as
Fuel Leak

A

2000 lb/h

54
Q

Excessive lateral imbalance of 4000 lb will require what trim adjustments?

A

4000lb requires 1 unit of aileron trim

55
Q

Stabilized Approach Criteria
OMA 8.0.1.2.

A

1) Correct Path
2) Minimal corrections speed and heading
3) Speed > VREF < REF+20Kt
4) Descent rate < 1000ft/m
5) Power appropriate
6) Completed Briefings and Checklists
7) ILS deviation < 1dot
8) Circling, level wings above 300ft.

56
Q

Windshear
anticipation, precaution and mitigation during takeoff
OMB2a
OMB 2a.16.6

A

-Full Rate Thrust
-Choose Longest runway
-Consider VR up to +20kt
-Be alert of fluctuations

57
Q

Windshear
anticipation, precaution and mitigation during LANDING
OMB2a
OMB 2a.16.6

A
  • Flaps 25 or 30
  • Stabilize above 1000ft
  • If A/T off adjust speed corrections
  • Avoid Idle
58
Q

Windshear indications and Characteristics
QRH Maneuvers 1.8

A

VARIATIONS MORE THAN:…
- 15 kt in speed
- 500 ft/m rate
- 5° attitude
- 1dot Glideslope
- Unusual thrust set

59
Q

Windshear escape maneuver
QRM Man 1.9

A
  • AP off
  • Push G/A
  • Agressv Max Thrust
  • A/T disconnect
  • Level wings
  • Spd Brake retract
  • Follow Guidance
  • Don’t Change configuration
60
Q

FLAP retraction
Last FCTM update,
June 30, 2023.

A

Page 3.32
In order to retract flaps to next position, the speed should be increasing and the target speed should be at or above the next Flp maneuver speed.
Maneuver Capability below next flap 15° + 15°
Above it 25° + 15°

61
Q

Speed Brake Operation
LHS and RHS

A

INFLIGHT: Both can operate

GROUND: Only the LHS can.

OMB Section 0
OMB 0.1.5
Normal Procedures.

62
Q

Predictive Windshear Fleet
Differences

A

NOTICE OF CHANGE
AB and AC don’t have it installed
NOC 23-16 A9C-DHAC
NOC 23-17 A9C-DHAB

63
Q

Glide Slope from Above
FCTM 5.15

A

Must be on Localizer to descent.

Arm GS
Landing Configuration
Target Altitude 1000ft AFE
V/S 1500ft/min
Green arc check
adjust 1000-1500ft/min
Not stable until 1000ft GA

64
Q

Standard Deviation Callouts

A

Speed VREF -5 + 20 SPEEED
Pitch inappr. or+7.5° PITCH
Bank Angle 30° BNK ANGLE
G/S 1/2 dot GLIDE SLOPE
Loc 1/2 dot LOCALISER
V/S >1300 ILS /
>1800 Non-Precision

DE AGA ÉLE provinhas (3 decks)

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