Shaded Box Limitations Flashcards by David Breton

Emergency Checklist Items

Engine Fire or Severe Engine Damage
(In Flight)
APU Fire
Engine Fire or Severe Engine Damage
(On Ground)
In Flight Engine Shutdown
Double Engine Failure
Smoke or Fumes Removal Procedure
SMOKE AFT (FWD) CARGO

** BACK **

MLG BAY OVHT
BRAKE OVHT
Passenger Evacuation
CABIN ALT or
Emergency Descent
Uncommanded Yaw Motion
Ditching or Forced Landing Imminent

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Length:
Wingspan:
Height

Length: 118 ft. 11 in.
Wingspan: 81 ft. 6 in.
Height: 24 ft. 1 in.

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Structural Weight Limitations:

MRW:
MTOW:
MLW:
MZFW:
MFW:

MRW: 85,000 (75,250)
MTOW: 84,500 (75,000)
MLW: 75,100 (67,000)
MZFW: 70,750 (62,300)
MFW: 45,000

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Cargo Limitations:

Aft: 3,650 lbs.
(Company)

Fwd: 1,700 lbs.

(700: 1,000 lbs.)

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Engine and Thrust

GE CF34-8C5

Normal: 13,600 lbs. thrust

APR: 14,510 lbs. thrust

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Max Mach RVSM:

82 in RVSM

700: 0.83

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Flap Speeds:
1:
8:
20:
30:
45:

1: 230 KIAS
8: 230 KIAS
20: 220 KIAS
30: 185 KIAS
45: 170 KIAS

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Landing Gear Speeds:

Extension:
Retraction:
Extended and locked:

Extension: 220 KIAS
Retraction: 200 KIAS
Extended and locked: 220 KIAS

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Max airspeed for:

windshield wiper operation

failed in a non-parked position

250 KIAS

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Max tire speed

195 Knots Groundspeed

700: 182 Knots

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Max speed for ADG operation

Vmo/Mmo

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Wind Components

Max tailwind:
Max x-wind t/o dry:
Max x-wind ldg dry:
Max x-wind wet:
Max x-wind b.a. FAIR:
Max x-wind b.a. POOR:
Max x-wind dry high mins CA/FO:

Max tailwind: 10 KIAS
Max x-wind t/o dry: 35 KIAS (28 KIAS)
Max x-wind ldg dry: 32 KIAS (30 KIAS)
Max x-wind wet: 27 KIAS
Max x-wind b.a. FAIR: 20 KIAS
Max x-wind b.a. POOR: 15 KIAS
Max x-wind dry high mins CA/FO: 25/15 KIAS

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Max pressure altitude

for t/o and ldg

8,000 feet

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Max and min temp. for t/o

Max: ISA + 35C

Min: -40C

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LAHSO min. distance

SL - 999 ‘ MSL:
7,000 ft. (700: 6,000 ft.)

1000-1999’ MSL:
7,100 ft. (700: 6,100 ft.)

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Flights must be within __ min.

of a suitable airport with cargo

60 minutes

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Max diff press:

Max neg. diff press:

During taxi, t/o and ldg
max diff press:

Max altitude single pack:

Max altitude EMER DEPRESS use:

Max diff press: 8.7 psi

Max neg. diff press: -0.5 psi

During taxi, t/o and ldg
max diff press: 0.1 psi

Max altitude single pack: 25,000 ft.

Max altitude EMER DEPRESS use: 15,000 ft.

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Minimum AP use height:

Visual and NPA:
ILS:
ILS Single Engine:

Max ILS glidepath angle:

Minimum AP use height:

Visual and NPA: 400’ AGL
ILS: 80’ AGL
ILS Single Engine: 110’ AGL

Max ILS glidepath angle: 3.5 deg

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kVA Load Limitation

Main generator (each):

APU generator:

kVA Load Limitation

Main generator (each):
40 kVA (0-41,000 ft)

APU generator:
40 kVa (0-41,000 ft)

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Max permissible continuous

load on each TRU

120 amps

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Cowl Anti-Ice ON

(GROUND and
TAKEOFF)

OAT 10C or below

AND

visible moisture

OAT 10C or below

AND

taxiing over SWISS
(standing water, ice, snow, slush)

Cowl Anti-Ice ON

FLIGHT

ICING CONDITIONS:

(TAT of 10C or below
AND
visible moisture,
unless SAT -40C or below)

ICE annunciated

Wing Anti-Ice ON

Takeoff

OAT 5C or below

AND

visible moisture

OAT 5C or below

AND

SWISS

NOTE: ON prior to thrust increase
if type 2-4 applied

Wing Anti-Ice ON

Flight

Icing conditions <230 KIAS

ICE annunciated

With APU as bleed source | in manual mode:

Wing and/or cowl anti-ice | PROHIBITED

Max fuel imbalance during: Takeoff: All other phases of flight:

Max fuel imbalance during: Takeoff: 300 lbs. All other phases of flight: 800 lbs.

When can you takeoff with more than 500 lbs. in center tank?

When each wing tank is above 4,400 lbs. OR When each wing tank is above 2,000 lbs. AND ZFW reduced by weight of fuel in excess of 500 lb.

Min. fuel for go-around

600 lbs. per wing Max 10 deg. nose up

Minimum fuel temperature Engine fuel for takeoff: Bulk fuel for takeoff:

Engine fuel for takeoff: 5C Bulk fuel for takeoff: -30C

Minimum temperature starting | cold soaked APU

-40C

APU starter motor duty cycle

3 starts/start attempts in 1 hr

How long must you wait between | APU start attempts

2 minutes

APU altitude limits Ground starting: Bleed extraction: Air starting: Generator loading:

APU altitude limits Ground starting: 15,000 ft. Bleed extraction: 25,000 ft. Air starting: 37,000 ft. Generator loading: 41,000 ft.

When can you exceed 75% N1 | after engine start?

2 minutes after start

Before FFOD when a/c cold soaked -30C for more than 8 hrs...

1. Motor engines 1 min. and verify N1 rotation 2. Thrust reverser actuated until deploy/stow cycles 2 seconds or less

Continuous Ignition Req'd

1. T/O and ldg contam. RWY 2. Flight in mod. or heavier rain 3. Flight in mod. or heavier turb. 4. Flight in vicinity of TS

Order if both cowl anti-ice and | continuous ignition req'd

1. Cowl anti-ice | 2. Continuous ignition

Cannot FLEX when CAWI

1. Contaminated runway 2. Anti-skid INOP 3. Windshear forecast 4. Wing and/or cowl a/ice in use

Max N2 with starter

45% N2

Engine Start Cycles | GROUND

Start 1 and 2: 1 min. 30 sec. ON, 10 sec. OFF Start 3,4,5: 1 min. 30 sec. ON, 5 min. OFF

Engine Start or Motoring Cycles (FLIGHT)

Start 1: 2 min. ON, 10 sec. OFF Start 2,3.4,5: 1 min. ON, 5 min. OFF

Motoring Cycles | GROUND

Motor 1: 1 min. 30 sec. ON, 5 min. OFF Motor 2,3.4,5: 30 sec. ON, 5 min. OFF

ITT temp for thrust lever | SHUT OFF to IDLE

Ground: < 120C Flight: < 90C

Thrust Reverser Usage Max reverse thrust PROHIBITED below: Idle reverse thrust achieved by:

Max reverse thrust PROHIBITED below: 75 KIAS Idle reverse thrust achieved by: 60 KIAS

Engine Operating Procedure Due To Wind: Less than 5 knots OR Within 30 deg. of nose:

Rolling, Normal, Standing T/O

Engine Operating Procedure Due To Wind: 5-30 knots MORE than 30 deg. off nose

Rolling or Normal Takeoff (Normal = Max 75% N1 before brake release)

Engine Operating Procedure Due To Wind: More than 30 knots MORE than 30 deg. off nose

Rolling Takeoff | Idle thrust before brake release

Flight Spoiler Usage Min. altitude: Min. speed:

Min. altitude: 1,000' AGL Min. speed: Vref + 10

What is min climb speed above | FL 330?

M 0.74

EICAS Messages At Various Altitudes 8,500 ft: 10,000 ft: 14,000 +/- 300 ft: 14,500 +/- 500 ft:

8,500 ft: CABIN ALT caution msg 10,000 ft: - CABIN ALT warning msg - NO SMKG and SEAT BELTS Signs Automatically On 14,000 +/- 300 ft: Oxygen masks drop 14,500 +/- 500 ft: Altitude limiter of outflow valve

What will not work when CPCP fails? (Cabin Pressure Control Panel)

1. NO SMKG and SEAT BELTS signs will not automatically turn on at 10,000 ft. 2. Oxygen masks will not drop at 14,000 +/- 300 ft.