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Horizon Air AQP 2017 part 2

Terms in this set (34)

Maneuvering Limit Load Factors
Flap retracted: +2.5g and -1.0g
Flap extended: +2.0g and -0.0g
At aircraft weights of _____________ lbs or less, V-Speeds and performance calculations are derived
directly from AeroData performance via EFB or Dispatch. (Do not use paper TLRs or charts.)
53,000
Minimum Runway Widths
CEME: E27P3
Normal operations...................................=_____ ft
Narrow runway operations .....................................................=_____ ft
100

60
Narrow runways are defined as runway widths less than 100 ft but not less than 60 ft. Takeoff and
landings on narrow runways:
• Should be accomplished by the Captain, using HGS (if available).
• Maximum crosswind: ____ kts
• Minimum Braking Action: ______
• Antiskid shall be operative.
• Maximum tailwind:
- Braking action Good: ____ kts
- Braking action Fair: ___ kts
15
Fair


10
5
FORWARD Cargo Compartment:
Max floor loading................................=_____ lb/ft2
Max permitted load.............................=_____ lb
NOTE:
The forward cargo compartment effective load is reduced to account for operational items included
in the BOW. The operational limits are defined in the iacbal app and Load Manifest form.
125
510
AFT ONE Compartment:
Max floor loading................................=_____ lb/ft2
Max permitted load............................=_____ lb
125
3,660
AFT TWO Compartment (aft step):
Max floor loading...............................=______ lb/ft2
Max permitted load...........................=______ lb
Maximum total load (AFT ONE plus AFT TWO)................................................=______ lb
75
1,000

3,660
Takeoff and/or landing with tailwinds of 11 to 20 knots maximum may be accomplished provided:
1. Nosewheel steering is operative.
2. Antiskid is operative.
3. Flight Spoilers are operative in ground and flight modes.
4. Bleed air is selected OFF prior to takeoff or landing.
5. Takeoffs are conducted with Flaps 10° or 15°.
6. NTOP or MTOP takeoff power rating is used.
7. Appropriate takeoff performance is provided in Takeoff Report or Performance Handbook.
8. Landings are conducted with Flaps 35°.
9. Appropriate landing performance is provided in Landing Report or General Landing Tables.
10. Approach and landing is accomplished at Props 1020 rpm. (RDC NP switch not selected on ECP.)
11. Landing approach angle is 4° or less.
12. Braking action Good.
Maximum tailwind for takeoff and landing is _____ knots.
20
Tank 1 and tank 2 _____________________ must be on for takeoff and landing.
auxiliary pumps
Setting takeoff power prior to brake release, with the nose of the airplane more than _____° out of wind, is
prohibited for wind speeds greater than _______ knots.
45

eight
. Minimum SAT for engine relight is -______°C.
40
Maximum cabin pressure differential limit ............................................................= _______ psi
5.95
Maximum cabin pressure differential limit during takeoff and landing .............................................. =_____ psi
0.5
Bleed air must be off for takeoff whenever:
• Tailwind component exceeds ten knots
• Takeoff is conducted with MTOP power selected
• Windshear is suspected QX
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