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mandiel > memory subjects > Flashcards

memory subjects Flashcards

1
Q

Wind limitation

A

Auto land 25, 20, 15
Tail 15
Doors 65

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2
Q

Auto pilot limitation

A 
Min engage after take off 400 ft
Min alt single Chanel 50 ft
Auto land angel 2.5 - 3.25
Do not trim ailerons with autopilot engage
Flaps for auto land 30 or 40
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3
Q

Flaps & speed break limitations

A

Max alt for flaps 20000
Do not hold in icing condition with flaps
Do not op speed beaks below 1000 ft
Do not op speed breaks beyond the FLIGHT DETENT

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4
Q

Cat I CAT II CAT III Weather limitation

A

CAT I - vis 800 or 550 rvr and 200 ft. RVR below 750 m without TDZ lights and/or CL lights, a coupled or a flightdirector-flown approach are required
CAT II - 100 ft rvr 300 For CAT D aircraft an RVR of below 350 requires autoland.
CAT III - 50 ft rvr 200
Circling 1000 ft 5 km
Visual 1500 ft 5 km

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5
Q

Visual Approaches

A

Visual - required weather 1500 ceiling and 5km
Day - Airport seen from distance or visible after inst App
Night - The airport become visible
Should be to Left
Min Alt 1500 at night maintain MSA until within the area for the
traffic pattern

Circling - MDA 1000 5km

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6
Q

OPT landing limitations

A

Landing Enroute - In flight:

Normal configure - add 15%
Non normal no additional
AD - 1500 ft for CAT III or Autoland add another 513
Landing dispatch:
Gradient - landing climb 3.2%, APP Climb 2.1%
If runway is contaminated or wet or CAT III add 15% to landing
Far field = landing x 1.67

MEL 32-22-01B is selected, Assumed Temperature may not be printed
on the screen. Use of Assumed Temperature is not allowed even if it is displayed.

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7
Q

Holding limitation

A

Below 14000 feet 230 K and 1 min leg
14000 - 20000 ft 240 k 1.5 min leg
20000 - 34000 265
Above 34000 0.82

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8
Q

Stabilized approach

A

 The airplane is on correct flight path
 Only small changes in heading and pitch required
 At approach speed Vref < V < Bug+20
 Correct landing configuration
 Sink rate max 1000 f/m (or friefed otherwise before)
 Thrust setting appropriate for A/C configuration
 All briefing and checklist completed
 ILS- within 1 dot of GP and LOC or within Expanded LOC scale
 Circling approach- wings level at 300’

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9
Q

Mandatory missed approach

A

Full deflection
Failure of NAV aid need for the app
Significant deviation between instruments
RNAV limitations or massage unable RNP

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10
Q

Turbulence

A
  1. מהירות לחיתחות בטיפוס והנמכה: 0.76 / 280 )בהנמכה- 250 מתחת גובה 15 ומשקל
    המטוס פחות ממשקל נחיתה מירבי(. בשיוט – N1 על פי ה-FMC במסך CRZ
    AP – CWS A/T Disengage .PAX SIGNS ON , FLT -מצתים :חמור בחיתחות .2
  2. עם צפוי חתחות בגישה, דחייה מירבית של הורדת מדפים
  3. חגורות כתפיים
    .)CFSM 5.1 ,5.2( .שרות והפסקת ,ולצוות לנוסעים הודעה .5
  4. אסור לטוס ב RVSM ב- .SEVER TURBULANCE .
  5. מילוי דו”ח תקרית ותקלה.
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11
Q

Fasten seat belt

A
  • After fueling is completed or the preflight procedure has been completed, the later of the two;
  • At all times on the ground with the engines running;
  • During Take-Off and Landing;
  • In-Flight below 10,000 ft;
  • When moderate or severe turbulence is experienced or anticipated;
  • Whenever deemed necessary by the PIC.
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12
Q

No V speed rotation

A

5 - 10 before V2

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13
Q

Acceleration height for
2 engine no NADP
1 engine
Go around

A

1500 ft
According to OPT
1500
FCTM

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14
Q

Interception

A 
Follow interception
Transponder 7500
Try to contact on 121.5
Sings:
Wings &amp; navy lights blink
Slow turn = follow me
Landing + lights = land here
Steep turn = you are released
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15
Q

Lost communication

A
  1. maintain the last assigned speed and level, or minimum flight altitude if higher, for a period of 20 minutes
  2. thereafter adjust level and speed in accordance with the filed flight plan
    Control airspace radar
    in airspace where radar is used in the provision of air traffic control, maintain the last assigned speed and level, or minimum flight altitude if higher, for a period of 7 minutes following:
  3. the time the last assigned level or minimum flight altitude is reached; or
  4. the time the transponder is set to Code 7600; or
  5. the aircraft’s failure to report its position over a compulsory reporting point;
  6. proceed according to the current flight plan route to the appropriate designated navigation aid or fix serving the destination aerodrome
  7. hold over this aid or fix until commencement of descent
  8. commence descent at, or as close as possible to, the expected approach time last received and acknowledged
  9. complete a normal instrument approach procedure
  10. land, if possible, within thirty minutes after the estimated time of arrival
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16
Q

LMC

A
  1. 3% from MACZF & MACTOW fwd & aft
  2. PIC can do it on form
  3. LMC can be transmitted via VHF
  4. After upgrade need to write in upgrade form
  5. UPGRADE need 3% from FWD CG. FOR every 1% one more pax
  6. LMC 350 kg
17
Q 
OMA CHAPTERS
Fuel saving
Adverse weather (icing, turbulence, wind sheer, heavy rain more)
MEL
FLIGHT PROCEDURES
Incapacitation
Ground handling
A 
Fuel saving - 8.3.9
Adverse weather - 8.3.10
Flight procedures - 8.3.8
MEL 8.6
Ground handling 8.2
Incapacitation 8.3.16
18
Q

Action required confirmations

A 
Thrust Lever
Engine start lever
Engine, APU, CARGO Fire switch
Generator Drive switch
Flight control switch
IRS when only 1 available
19
Q 
MORA
MSA
MEA
CAVOK
NOSIG
VMC
A

MORA - 0 - 5000 ft 1000 ft clearance (lido 10nm)
LIDO clearance one ENG - 1500 above airport positive gradient, 1000 ft above terrain
MSA 25 mm
CAVOK vis above 10km cloud above 5000 ft no significant weather
VMC visibility 8 km above 10,000 ft AMSL and 5 km below
10,000 ft AMSL;
2. Distance from cloud 1,500 m horizontally and 1,000 ft vertically; and
3. Ceiling is not below 1,500 ft

20
Q

ENG ABORT START CONDITIONS

A

No light up after 10 sec
EGT rise over limit 725 c
Slow N1 or N2 acceleration
NO OIL press after eng stable in idle ( icing up 2 min)

21
Q

Wind-sheer briefing

A 
Avoid, precaution, recovery
Avoid:
Delay TO Approach
Change RW
PRECAUTION:
TO - use max thrust use OPT CALC
Flaps 5-15
Longest RW
VR + 20
Briefing: SPD changes and stick shaker, bulletin TOGA 61
APP:
Flaps 30
Stabilized at 1000 ft
Use ILS/GS VNAV VISUAL instrument
Add vref + 20
Recognition:
Below 1000 ft - 1, 5, 15, 500 unusual N1
22
Q

Windsheer warnings

A

Predictive. Below 1200 ft
Caution: “monitor radar display”
Warning: at TO “windsheer ahead” x 2, Pior to V1 reject, after escape
At app “go around, windsheer ahead” escape or normal GO AROUND
Disable: cautions - 80 kids until 400 ft, warnings - 100 Kai’s until 50 ft.

GPWS
WARNING: siren x 2 “windsheer” x 3 available below 1500 ft

Below 1000 ft:
1, 5, 15, 500 N1

23
Q

Fuel saving on ground

A

Use of contingency, Tankering extra & additional critical
Shut down one engine OMA 8.3.21 & OPS INFO

24
Q

Aborted engine start conditions

A

No N1 or N2 increase or slow increase
No light up after 10 sec
EGT rapid approaching or exceeding limit
No oil press after engine stable in idle

25
Q

Ground Equipment must for CAT III

A 
TDZ RVR
APP LIGHTS
RW LIGHTS
C/L LIGHTS DAY RVR BELOW 350, Night not allow. 
STBY PW
26
Q

Bulletins

A

PWS FAILS annunciation
GPWS Minimums Voice Callout Anomaly
Look-Ahead Terrain Alerting Display Anomalies
Predictive Windshear System Anomaly
Nuisance Stall Warning Stick Shaker Events
Inflight Elevator Tab Vibration
Impact of Arming VNAV on the Ground on the Windshear Escape
Nuisance Zone Temp Light Illuminations on 737-800 Airplanes
Reduced Engine Response Times

27
Q

Heavy Rain supplamentary procedure

A

ENGINE START switches …………………………………………..CONT

Autothrottle ………………………………………………………….Disengage

Thrust Levers ………………………………………………….Adjust Slowly

If thrust changes are necessary, move the thrust levers slowly. Avoid changing thrust lever direction until engines have stabilized at a selected setting. Maintain an increased minimum thrust setting.

IAS/MACH …………………………………………….. Use a slower speed Using a slower speed improves engine tolerance to heavy precipitation intake.

28
Q

Severe turbalance supplamentary

A

Yaw Damper…………………………………………………………………………… ON

Autothrottle ………………………………………………………………….. Disengage

AUTOPILOT ………………………………………………………………………. CWS A/P status annunciators display CWS for pitch and roll.

Note: If sustained trimming occurs, disengage the autopilot.

ENGINE START switches ………………………………………………………. FLT

Thrust ……………………………………………………………………………………..Set Set thrust as needed for the phase of flight. Change thrust setting only if needed to modify an unacceptable speed trend.

mandiel (7 decks)

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