OMB/Limitations Flashcards
1
Q
Aeroplane dimensions
A
W 156’ (47.57m)
H 52’ (15.85m)
L nose to tail 159’ (48.51m)
2
Q
No SG for fuel
A
SG 0.78 should be used
3
Q
B767 type of operation
A
VFR
IFR
Icing conditions
Min crew Pilot and co-pilot
4
Q
767 Performance category
A
A
Assumed one engine inoperative cruise speed 400kts.
5
Q
Main deck cargo door operation
A
Operation 40kts
Open 60kts
Lower cargo door 40kts
6
Q
Cabin differential
A
Max 9.1psi
Max during climb 8.6 +/- 0.10psi
Max for T/O and LND 0.125psi
7
Q
A/P engaged
A
Not below 400’
8
Q
Disengage
APP V/S
APP ILS
A
300’ ARTE
180’ ARTE
9
Q
Auto land
A
All Engines
HW 25kts XW 25kts TWC 15kts
3.1-2.5 degree GS
F25/30
3 HYD SYS
2 GEN SYS (APU May be used)
IRS in NAV
2 AP and LAND 2 or LAND 3 at and below 600’
10
Q
Starter duty cycle
A
5 min on followed by 1/2 min off per min on
2x consecutive on req 10min cooling
11
Q
Engine warm up
A
3 mins prior to departure
70% N1 before full power.
12
Q
Lower EICAS display
A
Should not be blanked during T/O
13
Q
ENG RPM limits
A
N1 117.5
N2 110.5
14
Q
EGT limits
A
T/O 940
Max cont. 895
Start GND/FLT 870 transient 40sec
750 unlimited
15
Q
ENG oil
A
Min 10psi
Min 160
Max 15min 175
Dispatch 17 Quarts
16
Q
Max Fuel temp
A
49 deg C
17
Q
Min fuel Temp
A
-45 or 3 deg above freezing point
18
Q
Max Fuel
A
L/R main 43097
Centre 32376
19
Q
Max allowable Fuel imbalance L/R
A
2500lbs 48000lbs or less
1500lbs above 79800lbs
20
Q
Speed brakes
A
> F5 should be avoided and not below 1000’
Can be used to F20
21
Q
Flap speeds
A
1 240kts 5 220kts 15 210kts 20 195kts 25 190kts 30 162kts
22
Q
T/O flap
A
1,5,15,20
23
Q
Landing Gear Retract
A
270
24
Q
Landing Gear
A
Retract 270/0.82
Extend nml 270/0.82
Extended nml 270/0.82
Extend alt 250/0.75
25
Oxygen
Min psi for recharging by engineering 1200psi, provides 30 mins O2 for ALL seats 100%.
2 hrs at 25000’ smoke/fumes event
26
Start Valve open min duct psi
21psi
27
Start Aborts
ENG oil psi light not extinguished idle
No EGT 25secs.
No N1 rotation in 30secs. (N2 stabilised)
EGT rapid or limit
Tailpipe fire
Abnormal acceleration
28
Taxi technique speeds
Recommend 20kts
Max 30kts DHL
90 deg turn 10kts.
29
180 deg turn
39.3m
30
T/O procedure rotation and target SPD
At Vr 2-2 1/2 deg/sec toward 15 deg.
V2 + 20 to 1000’
31
Low level Alt CAP suggested call
CLB thrust
VREF 30+80
SPD mode.
32
Min speeds FL200 below and FL200 +
VREF 30+80
| VREF 30+100
33
Max rate CLB
F up manoeuvre SPD + 50kts until intc 0.78
34
Cruise speed
ECON
Less than 1 hr 290kts or 0.78 whichever is lower
35
Map integrity and Fuel checks
As soon as practical after TOC and hourly until TOD
36
Des speeds
0.78/290 FL100/10000’
Below 10000’ 250kts.
37
Auto brakes
1/2 normal
3/4 wet or slippery or auto land.
Max when stopping dist req.
38
AT manual THR landing speed bug
VREF 30 + 5 min. Max 15
Any TWC VREF 30 + 5 max
39
Rushed approaches.
ROD not exceed 3000fpm with 3000’ of MSA
Aircraft should be on a 3 deg slope by 15nm from TD
ROD for 3 deg slope is 1/2 GS x 10
40
AP use busy departures TMA or PRNAV
Must be engaged ASAP after passing 1000’
41
NML 2 ENG CLB SPD
V2 + 15-25
42
NPA limits
No part of the aircraft below MDA
LNAV maybe used if extracted from FMC otherwise HDG sel.
In marginal conditions CPT PF
Add 50’ to NPA minima
43
Circling APP
CAT C 4.2nm
Wings level by 300’
Lost VIS make an initial CLB turn towards the Aerodrome OH, followed by a turn as req to establish on the MAP procedure.
44
LVO CAT II/IIIA/IIIB and T/O min.
CAT II RVR 300 DH 100
CAT IIIA RVR 200 DH 50
CAT IIIB RVR 75 DH 0
Take off 150m
45
VIS < 1000m or rain min AUTO BRAKE
3
46
Autoland CAT I, II, IIIA equipment?
IIIB additional
RHS ASA
2 EADIs from separate symbol generators
3 HYD SYS
2 IDGs one maybe APU
CPT Stab trim
```
IIIB
2 EADIs from L/R SYMB GEN
Rudder pedal NWS
Atobrakes
RAD alt 0
```
47
Approach Ban
The approach shall be discontinued at 1000’ AAL. If TDZ RVR is not reported, mid point may be substituted at certain Aerodromes.
48
ENG Failure CAT II/III
If prior to selection of LND FLAP GA
>200’RA DH 50 200m
<200’RA DH 0
49
LVO VIS ref requirements
CAT PAR NPA any 1 of many vis clues
CAT II 3 consecutive lights + lateral element
CAT IIIA 3 consecutive lights
CAT IIIB zero
50
Auto throttle failure after AUTOLAND 3
Control manually idle at 45’
51
Autobrake NWS failure RVR min
200-125-75
52
Narrow RWY operations
Less than 45m
Min 28
XW 25 dry 18 wet
No autoland
CPT only
53
Run up to a min ____ for approx ____ duration are intervals of ____ mins
60% N1 30sec 30 min
54
ENG run up required when?
EAI is req OAT 3deg
55
Max motoring definition
N2 acc less than 1% in approx 5 secs
56
Weather radar monitoring technique
PM 160nm
| PF 80nm
57
WX/TS and T avoidance
20nm Above FL200 and 5-10nm below FL200
Avoid single magenta areas of T not associated with precipitation by at lease 5nm
58
EAI fuel consumption
EAI only 200lbs/hr
| EAI and WAI 310lbs/hr
59
Lido/mPilot yellow exclamation mark
May continue if cycle will be valid for the remainder of flight.
60
Lido/mPilot red X
EFB may not be used.
61
Circuit breaker policy
Maybe rest after a short cooling period of 2 mins at CPT discretion or by the direction of a checklist
Tripped fuel pump breakers are NOT to be reset.
62
STD engine failure procedure
Aircraft can CLB unrestricted straight ahead to 1500’
63
NON STD engine failure procedure
Unable to CLB unrestricted to 1500’
V2 CLB max bank angle 15deg
Lateral TRK must be flown accurately
64
ENG failure after V1 target pitch attitude
12.5 deg
65
ENG failure at altitude
Trim
Disconnect AT
Sel CON TMSP
Set CON manually
QRH
66
Damp runway
Moisture does not give shiny appearance
67
Wet runway
Covered less than 3mm. Reflective appearance.
68
Contaminated runway
More than 25% of the surface covered
69
Max tyre SPD
225mph
70
Max reduced thrust assumed temp
25%
71
Assumed temp thrust not allowed when?
Anti skid inop
Snow, slush or standing water
Potential windshear
72
Net takeoff flight path must?
Clear all obstacles by the req margin
Clean up to the en route configuration
Maintain prescribed min climb gradients
73
4 segment profile
1st gear up
2nd CLB to min flap retraction
3rd acc to flaps up
4 final CLB to 1500’
74
Single ENG CLB gradient
2.4%
75
Screen height wet___ dry___
15’ 35’
76
Flight planning dry runway landing
Full stop LND from 50’ above RWY threshold within 60% of LDA no reverse max manual braking.
77
Flight planning wet runway
LDA at least 115% of req landing dist cal for dry RWY
78
App CLB limit gradient
2.1% under all the following
Crit ENG inop
Live ENG at GA THR
Gear up
SPD not greater than 1.4 x Vsr
79
Guideline nml LND F30 below 280000lbs 3000’AMSL ISA +30 autobrake 2 any runway longer than______’ is adequate
9000’
80
Max total main deck load
94000lbs
81
One fitting main deck barrier fitting damaged max payload?
Two fittings damaged?
56400lbs
0
82
Departure without load sheet?
Not allowed and station copies must be retained for 3 months
Must be computer generated or not allowed.
83
Quick turn around limit specifies?
Max landing masses at F25/30 at least 58 mins must elapse from the time the aircraft comes to a complete stop before a T/O can commence.
84
Contaminated and slippery runway performance data is?
Advisory and should be avoided
85
Slippery runway landing
Both reversers and FULL braking must be available
86
TOW change more than _____ lbs a new OFP should be requested.
11000lbs
87
Rudder ratio XW limit
15kts
88
Main Cargo door warning. Alt limit _____ ‘
10000
89
C HYD SYS QTY and C HYD SYS PRESS EICAS.
Don’t? Otherwise expect?
Retract the gear or flaps on DEP. keep speed 220Kts
Gear disagree and flap disagree EICAS
