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ANA Study > Other Memory Items Not Official > Flashcards

Other Memory Items Not Official Flashcards

1
Q

Aircraft Upset Parameters

A

Pitch Attitude > 25deg nose up
Pitch attitude > 10deg nose down
Bank angle > 45deg

Within the above but at an airspeed inappropriate for the conditions

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2
Q

Nose High Recovery

A 
Recognize and Confirm
Disengage Autopilot and 
     disconnect Autothrottle 
Apply as much as full nose down elevator
Apply appropriate nose down Trim 
Reduce thrust 
Roll to obtain a nose down pitch rate
Complete the recovery 
  - approaching the horizon roll to wings 
     Level
   - check airspeed and adjust Thrust 
   - establish pitch attitude
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3
Q

Nose low Recovery

A 
Recognize and Confirm
Disengage Autopilot and 
   disconnect Autothrottle
Recover from Stall if required
Roll in the shortest direction to wings level
   ( unload and roll if bank angle is > 90deg )
Recover to level flight
   - apply nose up elevator
   - apply nose up Trim if required
   - adjust thrust and drag as required
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4
Q

Flight reference both engine

280000lbs

A

GEAR UP

Flaps Up/ level/ 210kias/ 3000ft
4.5deg ~ 59%N1

Flaps 1/ level/ 195Kias/ 3000ft
6deg ~ 61% N1

Flaps 5/ level/ 175Kias/ 1500ft
4.5deg ~ 62% N1

GEAR DOWN

Flaps 20/ level/ 155Kias/ 1500ft
4.5deg ~ 68%

Flaps 30/ level/ 140Kias/ 1500ft
5deg ~ 74%

Flaps 30/ 3deg ILS Final/ HW 7kt
2.5 to 3deg ~ 61-62%

Flaps 20 Abnormal landing/ 3deg ILS Final
VREF20+5/ 2.5deg ~ 50%N1

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5
Q

Flight Reference Single Engine

280000lb

A

GEAR UP

Flap Up/ level/ 3000ft/ 210kt
4deg ~ 76%N1

Flap 1/ level/ 195Kias/ 3000ft
6deg ~ 80%

Flap 5/ level/ 175KIAS/ 2000ft
5deg ~ 81%

Flap 5/ Des 1000fpm/ 174Kias/ 2000ft
2deg ~ 49%
Des 500fpm/3000-1500
3deg ~69%

GEAR DOWN

Flap 20/ 3deg ILS Final/ HW 7kts/ 149Kias
2.5 ~ 69%
Add 2-3%for each 10kt headwind and slight increase in pitch attitude to approx 3deg with 20kts HW

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6
Q

Flap placard speed

A 
Flap      767-300      767-300ER
  1            245kt             250kt
  5            225kt             230kt
  15          205kt             210kt
  20          205kt             210kt
  25          175kt              180kt
  30          165kt              170kt
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7
Q

Flap manouvre speeds

A 
0 - Vref 30+80
1 - Vref30+60
5 - Vref30+40
15/20 - Vref30+20
25 - Vref25
30 - Vref30
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8
Q

Weights 767-300

A

Max Taxi Wt 290700lb

MTOW. 288700lb

MLW. 280000lb

MZFW. 278000lb

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9
Q

What limits Mmo

A

High speed limit by shock wave

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10
Q

What limits Vmo

A

High speed limit by air load

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11
Q

What is VA

A

Maximum speed for maximum pitch control

You do not exceed the max load acceleration limits ( -1G to 2.5G flap up ) at design weight ( MTOW )

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12
Q

Landing gear placard speed

A

Normal system

Retraction 270kt
Extension 270kt/ .82M

Alternate system

Extension 250kt/ .75M

  • Extended VLE : 270kt/ .82M
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13
Q

Runway slope limit

A

+ or - 2%

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14
Q

Max operating pressure Altitude

A

43100ft

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15
Q

Max Takeoff and landing pressure Altitude

A

8400ft

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16
Q

Max X Winds

A

Dry ( including damp )….. 33kt
Wet ( grooved ) …………….25kt
Wet ( ungrooved)…………..20kt
Flooded ……………………….10kt

Ice or Snow
( Braking action)
Good ……………………………20kt (15 )*
Medium to good…………….20kt (15)*
Medium ………………………..20kt (10)*
Medium to poor……………..15kt
Poor …………………………….10kt

Slush (depth)
2mm or less ………………….15kt
3-12mm ………………………..10kt

  • Note these values are applied ONLY to landing on a runway less than 2500m
17
Q

Minimum inflight weight

A

Pax ….. 179000lb

300F ….177300lb

300BCF .. 180400lb

18
Q

Occupant limit Pax

A

Total number of Pax shall not exceed 290 because of the emergency evacuation and shall not exceed the number for which seating is provided.

19
Q

Flight manouvring load limits

A

Flaps UP - +2.5G to -1.0G

Flaps DOWN - +2.0G to 0.0G

With Flaps 25 and 30 positive limits vary linearly from +2.0G at max landing weight to +1.5G at max Takeoff weight

20
Q

280000lb speeds Pitch and N1 Settings

A

2 Eng GEAR UP
Flap Up 3000ft 4.5deg 59% Vref 30+80
Flap 1 3000ft 6.0deg 62% Vref 30+60
Flap 5 3000ft 4.5deg 63% Vref 30+40

2 Eng GEAR DOWN
Flap 30 3deg ILS 2.5deg 62% Vref 30+5
Flap 20 1500ft level 4.5deg 68% Vref30+20

1 ENG GEAR UP 
Flap Up 3000ft 4deg 76% Vref30+80
Flap 1    3000ft 6.0deg 80% Vref30+60
Flap 5    3000ft 4.5deg 82%
Vref30+40
1 ENG GEAR DOWN Flap 20
Level 1500ft 4deg 87% - Vref 30+20
Level 1500ft 5.5deg 87% - Vref 20+5
3deg ILS 2.5deg 67~70% Vref 20+5

All these are at 280000lbs straight from training manual 6G-5-9 and 10.

21
Q

Speeds for approach CAT D

A

Vat 141/165

Initial App - 185/250

Final App - 130-185

Max Circling speed - 205

Max MAP - intermediate 185
Final 265

ANA Study (4 decks)

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