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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
Crosswind Limitations Where we can find it?
OMB - Section 1.3.5 QRH - OI Section 0 FCTM - Tkoff Guideline 3.14 - Lndg Guideline 6.40 (TALPA)
26
Predictive Windshear System PWS - Parameters are:
3NM 25° 12 seconds after start scan Auto alerts below 1200ft Auto enable GROUND Takeoff Thrust FLIGHT Below 2300ft
27
Auto Throttle Failure, How to get N1 values?
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
Rescue and Fire Fighting RFF - DHL Airport Fire Cover Minimum Categories
RFF 7 at destination RFF 6 for alternates RFF 5 for EDTO alternates OMA 8.2.4.9
29
OMA 8.3.9 Wake Turbulence Distance Separation on air (approach)
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
OMA 8.3.9 Wake Turbulence TIME Separation for DEPARTURE
Same Departure point 767 (H) follow SUPER or H 2’ Intermediate Point 767 (H) follow SUPER or H 3’ Heavy definition > 136.000Kg
31
LMC Last Minute Change Limits
ZFW 1.100 lb FUEL 4.400 lb If exceeded new Load Sheet OMA 8.1.8.5
32
OFP Operational Flight Plan Limit:
11.000 lb If exceeded new OFP must be generated OMB 5.2
33
On Time Performance Delays:
Up to 5’ no report nor codes From 5’ to 15’ delay code EFB and logbook. Beyond 15’ report and logbook
34
ALTERNATE - OMA 8.1 Destination Alternate When 2 alternates are a must
-Destination forecast +\-1h Below minima; -No meteorological info;
35
ALTERNATE - OMA 8.1 Isolated Alternate 3% contingency Meteo Minima Requirements
-CAT II & III - RVR -CAT I - above non-precision -Non-Precsn. - +200ft/ 1000m -Circling - Circling OMA 8.1.3.1.4
36
Tankering OMA 8.1.7.1.3 Shall never exceeded:
MLW minus 500Kg / 1100lbs
37
Nominate the 3 reasons for tankering
P - Price H - Handling B - Business
38
Which tankering reasons take precedence over payload? And which doesn’t?
Tankering price NEVER takes precedence ove payload But… Handling and Business, the DO TAKE precedence over payload
39
DHL policy for fuel price differential exceeds_____ of flight before tankering is considered OMA 8.1.7.1.3
4% per hour of flight
40
Fuel Limitation: Fuel Tanks max capacity 767-300
L 40.267 C 80.132 R 40.267
41
Approved types of Fuel And it’s respective fuel freezing points
JET - A = -40°C JET -A1 = -40°C JP - 5 = -40°C JP - 8 = -46°C
42
Limitations Fuel Fuel Temperature
Max 49°C Min -45°C or 3° above fuel frz
43
Fuel Limitations Maximum Imbalance
At 48.000lbs main tk - 1500lb Linear to… At 79.800lbs main tk - 2500lb
44
Limitations Maximum Main Deck Load
125.000lbs
45
767 Engine CFM Max EGT during Takeoff
960° C for 5 min
46
767 Engine CFM Max Continuous EGT
925°C
47
767 Engine CFM Max EGT during Start
870° C - 40 seconds
48
767 Engine CFM Max EGT start unlimited
750° C
49
767 Engine CFM Max N1
117.5%
50
767 Engine CFM Max N2
112.5 %
51
B767 CFM Start Duty Cycle
Normal: 5’on - 30”off per min Extnd: two of 5’ -10’ cooling
52
Aborted Engine Start Conditions are:
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
What rate of imbalance should be considered as Fuel Leak
2000 lb/h
54
Excessive lateral imbalance of 4000 lb will require what trim adjustments?
4000lb requires 1 unit of aileron trim
55
Stabilized Approach Criteria OMA 8.0.1.2.
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
Windshear anticipation, precaution and mitigation during takeoff OMB2a OMB 2a.16.6
-Full Rate Thrust -Choose Longest runway -Consider VR up to +20kt -Be alert of fluctuations
57
Windshear anticipation, precaution and mitigation during LANDING OMB2a OMB 2a.16.6
- Flaps 25 or 30 - Stabilize above 1000ft - If A/T off adjust speed corrections - Avoid Idle
58
Windshear indications and Characteristics QRH Maneuvers 1.8
VARIATIONS MORE THAN:… - 15 kt in speed - 500 ft/m rate - 5° attitude - 1dot Glideslope - Unusual thrust set
59
Windshear escape maneuver QRM Man 1.9
- AP off - Push G/A - Agressv Max Thrust - A/T disconnect - Level wings - Spd Brake retract - Follow Guidance - Don’t Change configuration
60
FLAP retraction Last FCTM update, June 30, 2023.
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
Speed Brake Operation LHS and RHS
INFLIGHT: Both can operate GROUND: Only the LHS can. OMB Section 0 OMB 0.1.5 Normal Procedures.
62
Predictive Windshear Fleet Differences
NOTICE OF CHANGE AB and AC don’t have it installed NOC 23-16 A9C-DHAC NOC 23-17 A9C-DHAB
63
Glide Slope from Above FCTM 5.15
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
Standard Deviation Callouts
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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