KV Part 1

Question 1

Do you have to land at the nearest suitable airport if APU fire was extinguished?

Answer 1

No. Revision allows at CA discretion.

Question 2

Why would overhead GPS light illuminate?

Answer 2

Both sensors have failed, or one sensor failed and annununciator panel is pushed

Question 3

QRH guidance for MAINT light

Answer 3

Do not takeoff

Question 4

Stabilization Limits: Airspeed? Sink Rate? Crosstrack? Glideslope?

Answer 4

Airspeed: Target +10/-5

Sink Rate: 1,000 fpm

Crosstrack: 1 dot (5 degrees)

Glideslope: 1 dot

Question 5

Engine fuel leak? (not continuous stream)

Answer 5

Normal start procedure.

Question 6

PSEU light indicates? Dispatchable?

Answer 6

* Overwing exit flight lock fails to disengage

* or, general fault is detected

Yes

Question 7

Greater than 10 kt tailwind?

Answer 7

San Jose, Costa Rica

Question 8

When do you need two landing alternates?

Answer 8

1. 3585
2. Marginal (dest and alt less than 600-2)
3. NGRVR used for dispatch

Question 9

Standard Takeoff Minimums

Answer 9

1 SM / 5000 RVR

Question 10

FAA 45 min reserve NG? MAX?

Answer 10

NG - 3500

MAX - 3100

Question 11

Do you need a 2000 ft stoping margin to take off from a runway intersection?

Answer 11

No. Standard margins apply.

Question 12

MAINT light dispatchable on MAX?

Answer 12

No, but can be inhibited for certain MEL’s

Question 13

CDS MAINT

Answer 13

* Dispatchable

* Ground only

* Prior to 2nd engine start

(Not seen on MAX)

Question 14

CDS FAULT

Answer 14

* Non-dispatchable

* Ground only

* Prior to 2nd engine start

(Not seen on MAX)

Question 15

How to determine sufficient fuel in diversion?

Answer 15

AOM 18 In-Flight Performance Data Chart

Question 16

Three ways to reset PSEU light:

Answer 16

1. Press Master Caution
2. Set parking brake
3. Both engines shut down

* if none work, do not takeoff

Question 17

CSFF provisions on upper wing?

Answer 17

1. Within black lines (must have lines)
2. OAT at or above 4 C
3. Fuel at or above -16 C
4. No vis moisture (at or above 1 SM)

Question 18

How to manage risks

Answer 18

Dispatch, SOP’s, checklists, crew briefings

Question 19

NG holding burn? contingency burn?

MAX holding burn? contingency burn?

Answer 19

NG - 4500/4500

MAX - 3800/4100

Question 20

Where to find info on GPS service/operation?

Answer 20

Weather packet

Question 21

1.5 G buffet altitudes

Answer 21

NG - 3000 ft below FMC Max Alt

MAX - 3300 ft below FMC Max Alt

Question 22

PSEU light inhibited from:

Answer 22

Thrust lever advance to 30 sec after landing

Question 23

MAX pushback communication?

Answer 23

“Step stool is being used.”

Question 24

Takeoff below standard?

Answer 24

Ops Specs (Reference Card)

10-9A

Lighting/Notams

Question 25

Takeoff Alternate required when? How far?

Answer 25

Non-HGS, CAT 1 landing min One hour, still air, single engine (320 NM)

Question 26

Considerations if both IRS DC FAIL light illuminate:

Answer 26

\* Primary power source is AC (normal ops) \* Hot batt bus not powered or batt disch \* Fire ext poss unavail. APU poss not start.

Question 27

Where to find info on MEL process

Answer 27

FOM 19

Question 28

Irregularities between GE/ROW 44 and Panasonic?

Answer 28

AOMs

Question 29

MEL sticker name

Answer 29

SP #1B placarding

Question 30

Where to find meaning of FMC messages?

Answer 30

QRH - Ops info

Question 31

How long will IRS operate without AC power?

Answer 31

Right - 5 min Left - approx 30 / 60 (two batt) min or until DC power lost

Question 32

TERPS climb requirements

Answer 32

Standard 200 ft/NM Nonstandard - Reference 10-9A or SID (Use first gradient above 1000 ft AGL)

Question 33

“Look and see”

Answer 33

Not applicable to CAT III approaches

Question 34

TA mode only?

Answer 34

QRH or SIP

Question 35

Batt voltage range?

Answer 35

22-30V

Question 36

FMC position priority?

Answer 36

\* GPS \* DME \* LOC & DME \* 1 LOC

Question 37

Fuel limitations:

Answer 37

1. Main tanks full if center more than 1000 2. Center pumps on when more than 1000 3. Pumps off when first light illuminates 4. Deplane when less than 2000 lbs in tank 5. Personnel req’d in flight deck for pumps 6. Min -37 C; Max 49 C 7. Don’t reset fuel pump, fp control, or f quanity CB’s

Question 38

Where to find info on fuel transfer:

Answer 38

AOM 16

Question 39

Manual W&B load limitations:

Answer 39

Below ATOG and PTOW + 2,000

Question 40

TR UNIT light inflight implications?

Answer 40

\* TRU 1 or 2&3 have failed. \* Auto features of BUS TRANSFER switch inhibitted when AFDS is in APP mode w/ GS capture \* Other approaches are fine

Question 41

Two times when DC busses won’t have automatic backup:

Answer 41

1. BUS TRANSFER switch OFF 2. GS capture

Question 42

AUTO function of STANDBY POWER switch:

Answer 42

Allows automatic transfer of battery power to:

Question 43

What does the FAULT light on the Fire Control Panel indicate?

Answer 43

NORMAL - both loops are failed A or B - respective loop is failed

Question 44

What is the idication that the squib has fired and the extinguishing agent has been discharged?

Answer 44

L or R BOTTLE DISCHARGED

Question 45

What does this light mean? How can attitude be be restored inflight?

Answer 45

A system fault associated with the respective IRS has been detected. Select ATT while in level flight for approximately 30 seconds.

Question 46

Answer 46

Manually selected source is not powering the associated trasfer bus.

Question 47

Answer 47

Respective IDG is not powering to the transfer bus.

Question 48

What does DSPLY SOURCE 1 and DSPLY SOURCE 2 alerts mean in the MAX or an NG equipped with U13?

Answer 48

DSPLY SOURCE 1 or 2 (amber)—DPC 1 has failed or DPC 2 has failed. If a DPC fails **above FL220**— * The autopilot and flight directors are not affected. If a DPC fails during climb or descent **below FL220** with the failed side autopilot engaged— * The flight director pitch command bar is removed from both Pilots’ displays. * The flight director pitch command bar reappears at ALT ACQ. * The autopilot engages in CWS P. * LVL CHG, VNAV, and V/S are not available with the failed side autopilot. If a DPC fails during level flight **below FL220** with the failed side autopilot engaged— * Climb or descent to a new altitude is only possible in CWS P. If a DPC fails in the approach mode **above 400 ft** with both flight directors on— * The flight director pitch and roll command bars are removed from the display on the failed side.