Limitations and op restrictions

Question 1

Cold temperature: Altimeter overeads by…

Answer 1

4% of ht per 10C below ISA

Question 2

Density Altiture = Airfield altitude +

Answer 2

1000ft/8 deg above ISA

Question 3

Strong winds and MOA - increase MOA by…

Answer 3

Increase MOA by 2000ft when W/V>50kts at MSA/SSA

Question 4

Suspect an inversion when…

Correction to CARD: Add…

Answer 4

clear/calm night and OAT>ISA + 15 add 3 degrees

Question 5

Severe windshear is considered to be uncontrollable changes from normal steady flight conditions below 1,000ft AGL, in excess of the following conditions:

Answer 5

15kts IAS
V/S change of 500 fpm
5 degrees pitch attitude
1 dot displacement from glideslope/glidepath
Unusual thrust levels for a significant period of time

Question 6

ETOPS TRANSIT CX

Restrictions on when it must take place:

Answer 6

Before every flight within 4hrs of STD.
No need for a Return to stand (only a night stop)

Question 7

MAX numbers of:
DEPA
DEPU
INAD

Answer 7

1 DEPA
2 DEPU
6 INAD

Question 8

sm to m conversion:
1/8 sm = … m
1/4 sm = … m
1 sm = … m

Answer 8

1/8 sm = 200 m
1/4 sm = 400 m
1 sm = 1600 m

Question 9

777 Aerodrome Category/ 777 Speed Category

Answer 9

Aerodrome Cat = E, Speed Cat = D

Question 10

RFF Category: 777 and ETOPS airfields

Answer 10

9/4

Question 11

RFF Temporary Downgrade:

Departure and destination airfields

Answer 11

-1 below a/c category (8)
-2 below a/c category if temporary downgrade (7)

(Not lower than Cat 4)

Question 12

RFF Downgrades:

T/O Alternate, Destination Alternate and en route Alternates

Answer 12

-2 below a/c category (7)
-3 if temporary downgrade or has been risk assessed (6)

(Not lower than Cat 4)

Question 13

RFF ETOPS minimum:

Answer 13

Cat 4 at 30 minutes notice

Question 14

R/T for CPDLC in NAT OCA:

Answer 14

BAW123,CPDLC REQ FREQ, GANDER NEXT
or
BAW 123 CPDLC, REQ SELCAL CX, EXIT ABCD

Question 15

GE ENGINE LIMITATIONS (warm up/cool down)

Answer 15

GE - 3 mins/3mins

Question 16

RR ENGINE LIMITATIONS (warm up/cool down)

Answer 16

RR - 5 mins or 3 mins (≤ 1hr30min)/1 min

Question 17

CORE ICE SHEDDING Rolls Royce MA->MU

Requirements:

Answer 17

FZFG, vis less than 300m, more than 45 mins taxi time

Question 18

TAXIING - ENGINE ICING REQUIREMENTS

Answer 18

TAXI -
When EAI is required and OAT ≤ 3°C:

50% N1 for 1 sec every 15 mins (-200 GEs)

50% N1 for 1 sec every 60 mins (-200RR/-300)

Question 19

T/O: ENGINE ICING REQUIREMENTS

Answer 19

When EAI is required and OAT ≤ 3°C:

RR: Run-up to a minimum of 50% N1 and confirm stable engine operation before the start of the takeoff roll.

ALL GEs
Run-up to as high a thrust setting as practical (minimum of 50% N1), confirm stable engine operation, ensure engine vibration indications are below 4 units before the start of the takeoff roll.

Question 20

ALTIMETER TOLERANCES:

Before T/O and before entering RVSM

Answer 20

Before T/O 75ft cf Airfield elevation

Prior to RVSM: P1 and P2 +/- 200ft

Question 21

200 DIMENSIONS (Span/Length/Tail)

Answer 21

200 DIMENSIONS (S/L/Tail):

61/64/19m

Question 22

300 DIMENSIONS (Span/Length/Tail)

Answer 22

300 DIMENSIONS (S/L/Tail):

65/74/19m

Question 23

MAX Rate Of Climb Speed:

Answer 23

Flaps up Manoeuvring Speed + 60kts until intersecting with M0.82 (FCTM)

Question 24

APU AND TAXI BURN in kg/hr

Answer 24

APU Burn: 300kg/hr, Taxi: 1800kg/hr (-200) and 2000kg/hr (-300)

Question 25

180 degree turn - minimum pavement widths:

Answer 25

-200 = 55m -300 = 60m

Question 26

CPDLC LOGON AND CLEARANCE TIMINGS:

Answer 26

CPDLC logon: 15 to 45mins before entry Oceanic clearance: 30 to 90 mins before entry

Question 27

PRECAUTIONARY RAPID DISEMBARKATION

Answer 27

ALERT call/NITS THEN: "Attention,attention,this is an important announcement. All passengers must leave the aircraft via the nearest boarding door in a quick and orderly manner. Leave all personal items behind"

Question 28

BEST CASE XWC T/O AND LDG (dry and wet): Max XXC sideslip ONLY:

Answer 28

XW T/O (D/W) 40/40 KTS XW LDG (D/W) 45/40 KTS see FCTM for weight/MACTOW combinations 28 kts sideslip ONLY

Question 29

BEST CASE XWC CONTAMINATED

Answer 29

XW (T/L-CON ) 35kts see FCTM for contamination type

Question 30

MAX TWC T/O and LDG

Answer 30

TW (T/L) 15 KTS

Question 31

MAX TWC LDG SLIPPERY

Answer 31

TW (L-SLIPP) 5 KTS

Question 32

LVP AUTO LAND WIND LIMITS

Answer 32

H=25, T=15, X=25 (15 USA)

Question 33

NON LVP AUTO LAND WIND LIMITS

Answer 33

H=32(33), T=15, X=28(29) NB: ( ) = 300ER

Question 34

Turbulence speeds

Answer 34

≤FL250 - 270 kts (250kts in desc if ≤MLW and ≤FL150) ≥FL250 - 280/0.82 (min 15kts above min manoeuvre speed when ≤M.82)

Question 35

max rwy slope

Answer 35

+/- 2%

Question 36

`max T/O and LDG TWC

Answer 36

15kt

Question 37

max operating altitude

Answer 37

43,100 ft

Question 38

max TO and ldg altitude

Answer 38

8,400ft

Question 39

restrictions on refueling and HF radios

Answer 39

don't operate HF and refuel

Question 40

avoid wxr ops in a hangar or within XXX ft (XXX m) of fuelling ops or a fuel spill

Answer 40

50 ft (15.25 m)

Question 41

flight deck security door - operational check

Answer 41

once per flight day

Question 42

without Land 2 or Land 3, the AP must be disengaged below

Answer 42

200 ft AGL

Question 43

do not use FLCH on final approach below...

Answer 43

1000 ft AFE

Question 44

the PVD system on TO has been demonstrated to perform satisfactorily in non LVO crosswind conditions up to:

Answer 44

25 knots

Question 45

max crosswind for LVOs where PVD is used is

Answer 45

15 knots

Question 46

autoland - max HWC

Answer 46

25 knots

Question 47

autoland - max TWC

Answer 47

15 knots

Question 48

autoland - max XWC + max XWC (USA)

Answer 48

25kts + 15 kts USA

Question 49

engine limit display markings: max and min limits are xxx caution limits are yyy

Answer 49

max and min - red caution - amber

Question 50

Oil system RR engines: oil temp must be greater than XXX for start and YYY degrees before advancing the Thrust Levers to T/O power

Answer 50

greater than -40 C for start greater than 50 C for TO

Question 51

max fuel temp

Answer 51

49 degrees C

Question 52

min fuel temp GEs - prior TO and airborne

Answer 52

prior T/O - tank fuel temp must not be less -40 or 3 degrees C above the fuel freeze point, whichever is the higher. Airborne: 3 degrees above the freeze point of the fuel being used

Question 53

min fuel temp RRs - prior T/O and airborne

Answer 53

prior TO - tank fuel temp must not be less -37 or 3 degrees C above the fuel FP, whichever is the higher. Airborne: 3 degrees above the FP of the fuel being used

Question 54

Restriction on RR engs, and RTOs:

Answer 54

if thrust reversers deployed, T/O is prohibited until maintenance action is complete

Question 55

300 GEs - grd ops (not T/O) - XWC and TWC limitation

Answer 55

TWC and XWC between 30 and 45 kts - limit N1 to 70%

Question 56

APU starter limits

Answer 56

3 attempts in 60 minutes wait a minute between each start

Question 57

Max altitude with flaps extended

Answer 57

20,000 ft

Question 58

main tanks must scheduled to be full if...

Answer 58

centre tank fuel is loaded

Question 59

the centre tank fuel may contain XXXX kg of fuel with less than full tanks provided centre tank fuel plus actual ZFW does not exceed max ZFW and C of G limitations are observed

Answer 59

1,360 kg

Question 60

use of look ahead terrain alerting is prohibited within XXX at an airport or rwy not contained in the GPWS terrain database

Answer 60

15nm of TO, approach or ldg

Question 61

ETOPS rule time and rule distance

Answer 61

180 mins and 1,200 nm

Question 62

In flight, APU bleed air is available at and below XXXX ft

Answer 62

22,000 ft

Question 63

SAC

Answer 63

An approach is considered stable when all of the following criteria are met: In the planned landing configuration (gear down land flap achieved). Stabilised on the correct vertical profile (see Note 1). Stabilised at the target approach speed (see Note 2).

Question 64

SAC definition of established on correct vertical profile...

Answer 64

A visual profile: In the complete absence of electronic or instrument approach guidance the method of defining the correct visual profile should be agreed at the briefing stage. The correct visual profile is that defined by either: A Visual Approach Slope Indicator System if available. Once established on the extended centreline, unless otherwise specified, an indication of “All Whites” or “All Reds” would not satisfy the requirements of this policy or; Where no VASIS guidance is provided the required profile will default to that commensurate with a 3° approach slope.

Question 65

Leeway on the ...... Stabilised at the target approach speed, part of the SAC:

Answer 65

Only in circumstances of rapid wind changes, turbulence or adherence to appropriate ATC speed requirements where the crew has failed to achieve speed stability by the 1000 ft auto-callout and the speed is close to the target approach speed and reducing, can the approach be continued. If the aircraft is not stable at the target approach speed before the 500 ft auto-callout then a go-around must be flown.

Question 66

Flap settings and windshear: For Optimum T/O performance, use flaps....

Answer 66

use flaps 20 for T/O Flap 15 may be used as a precautionary setting and will provide nearly equivalent performance to Flaps 20

Question 67

Nil/Minor change of load - up to +/- XX passengers

Answer 67

5 passengers