Vmo=340 kias

Mmo=.82M

V_a is Maneuvering Speed and is the

speed above which maneuvers involving full rudder, aileron or elevator, or

manuevers near stall AOA should be

avoided.

V_a= 260 kias at sea level

and 306 kias at 31,000 feet

1, 2, 5 - 250 kias

10 - 210 kias

15 - 200 kias

25 - 190 kias

30 - 175 kias

40 -162 kias

Alternate Flap System - 230 kias

Landing Gear Placard Speed

(V_lo and V_le)

Retract...235 kias

Extend...270 kias/.82M

Extended...320 kias/.82M

Note: Verify Ldg Gear Limit (IAS) on the placard under Ldg Gear Lever during normal operations

With Engine Bleeds on, do NOT operate packs in High for ____, _____or _____.

(except for Cargo Fire and Smoke or Fumes Removal Checklists. Switches need to be in High to open the Overboard Exhaust Valve)

during all gnd and flt ops when icing conditions exist or are anticipated, except during climb and cruise when the temp is below -40C SAT (Prog pg 2)

Eng A/I must be on prior to and during descent in all icing conditions regardless of temp

Takeoff is not permitted if there is cold soaked fuel frost on the lower or upper wing tank surface, as follows:

-it exceeds 3mm on the lower surfaces

- on the upper surface and

         >it exceeds 1.5mm OR

         >not similar on both wings OR

         >beyond the black lines

-on the upper surface and

         >OAT is less than 0C  OR

         >there's visible moisture

True or False....

Use of the aileron trim with the autopilot engaged is prohibited.

Max allowable wind speeds when landing weather minima are predicated on autoland operations:

Headwind.........____

Tailwind.......____

Crosswind......____

Headwind........25 knots

Tailwind...........15 knots

Crosswind........20 knots

Max-3.25 deg

Min-2.5 deg

Engine Limit Display Markings

Maximum and minimum engine limits are  a _____.

Cautionary range is marked by_______.

Normal operating range is marked by _________.

Max/Min---------red line

Cautionary-------amber arc

Normal range----white arc

Engine RPM

Max limits are:

N1(low press compressor)

   N2 (high press compressor)

N1 

• 104.7% (20 seconds)
• 104.0% (continuous)

N2

• 105.0% (continuous)

Takeoff...................950C      5 min limit

Max Continuous......925C

Starting...................725C

Not a limitation...but nice to know:

Which of the following does the EEC monitor?

N₁

N₂

EGT

N₁ and N₂ all the time

EGT only during engine start

When EEC's are used in ALTN mode:

• derate thrust for T/O is ______
• ____ EEC's must be in alternate
• _____ the FMC T/O N₁ or V_speed value
• use of autothrottle for T/O is _____

• derate thrust for T/O is not allowed
• both EEC's must be in alternate
• do not use the FMC T/O N₁ or V_speed value
• use of autothrottle for T/O is prohibited

Engine Oil System

Min Oil Pressure-_____

Max Oil Temperature-_____

Max for continuous ops-___

Operational limit between 140C & 155C -______

Min Press- 13psi

Max Temp- 155C

continuous- 140C

Limit between 140/155C- 45 minutes

If oil press is in the amber band with T/O thrust set, do not takeoff.

Must be on for T/O, Landing, in Heavy Rain and during Anti-ice operation.

It's automatic for T/O, Landing and during Anti-ice ops.

APU (Max altitudes)

• Bleed & Electrical
• Bleed only
• Electrical only

• Bleed & Electrical......10,000 feet
• Bleed only.....................17,000 feet
• Electrical only..............41,000 feet

• ground air connected and isolation valve open
• Eng. No. 1 Bleed Air Valve open
• Isolation and Eng. No. 2 Bleed Air Valves open

Except: APU Bleed may be open during Eng. start, but avoid thrust above idle.

Flight Controls

Avoid ___________ control inputs, especially in combination with large changes in pitch, roll and yaw (e.g. ______) as they may result in structural failure at any speed, including below V_a.

rapid and large alternating

large side slip angles

Between Capt & FO ...... 50 feet

Between each altimeter and field elevation...... 75 feet

Air Data Inertial Reference Unit

ADIRU alignment must not be attempted at latitudes greater than ________.

Fuel System

Max allowable fuel weights

No. 1 or No. 2 tanks...........______

Center tank...........______

No. 1 or No. 2 tanks.......... 9,144 lbs each

Center tank.............  30,522 lbs

Fuel Loading

Load main tanks _______ to the desired quantity or until full.

Fuel Loading

If the center tank is going to have more than 1000 lbs, the main wing tanks _________.

True or False

The following fuels are allowed for use in the 737-800:

• Jet A
• Jet B
• JP-4

False

JP-4 and Jet B are prohibited

With no fuel in the center tank, use main tank to engine (main tank pumps-on, center tank pumps-off, crossfeed-closed)

With fuel in the center tank, use center tank fuel (all pumps-on, crossfeed-closed) until center tank fuel depleted (1000 lbs may be retained in center if balance has been considered)

• Minimum fuel operation
• to correct a fuel imbalance

• No personnel are available on the flight deck to monitor the low pressure lights
• Center tank quantity not greater than 1000 lbs. (unless defueling or transferring)
• when the low pressure lights illuminate (both off if quantity zero)

True or False...

For executing a short field landing, hold the brakes prior to touchdown.

False

Do not apply brakes until after touchdown.

Max Crosswind

Dry..................................................___

Wet (Grooved).............................___

Wet (Ungrooved)........................___

Flooded.........................................___

Dry..................................................29 knots

Wet (Grooved).............................25 knots

Wet (Ungrooved)........................20 knots

Flooded.........................................10 knots

Max Crosswind for Ice or Snow

Braking Action

Good.............................................____

Med to Good..............................____

Med.............................................____

Med to Poor...............................____

Poor..............................................____

Braking Action

Good............................20 knots

Med to Good..............20 (15*)knots

Med..............................20 (15*) knots

Med to Poor................15 (10*) knots

Poor..............................10 knots

* rwy less than 2500m & not for T/O

Max Crosswind

Slush

2mm or less..............................____

3-12 mm....................................____

2mm or less..............................15 knots

3-12 mm....................................10 knots

True or False...

Porous friction course runways should be treated as grooved runways.

True or False...

Operations when Braking Action is reported as Very Poor require a Max Crosswind of less than 10 knots.

Precipitation on Runway

T/O and Landing are prohibited when:

Slush.........................________

Wet Snow................________

Dry Snow..................________

Slush.........................at or above 13 mm

Wet Snow................at or above 51 mm

Dry Snow..................at or above 71 mm

Maximum demonstrated crosswind:

Non W.............____

With W...........____

Non W.............36 knots

With W...........33 knots