Term
| CG must remain forward of _____? |
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Term
| T/O Power + APR or go-around power (TRQ, ITT, ENG, PROP) |
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Definition
max 5 min: 107%, 940 C, 102%, 1396 RPM
max 2 min: 107%, 950 C, 102%, 1396 RPM |
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Term
| T/O Power (TRQ, ITT, ENG, PROP) |
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Definition
max 5 min: 100%, 917 C, 101%, 1396 RPM
max 2 min: 100%, 927 C, 101%, 1396 RPM |
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Term
| Max Continuous (TRQ, ITT, ENG, PROP) |
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Definition
| 100%, 940 C, 102%, 1396 RPM |
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Term
| Transient except T/O (max 12 secs) (TRQ, ITT, ENG, PROP) |
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Definition
| 112%, 965 C, 105%, 1572 RPM |
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Term
| Two start attempts with __ mins between, then __ mins cooling before subsequent starts |
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Definition
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| Motoring: 3 __ secs. ventilation with __ mins. cooling btwn each, then __ hour cooling period before subsequent starts or motoring |
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Term
| Time to light off (from initial Ng rotation to ITT rise) |
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Term
| Max time with engaged starter is __ secs. of which max __ secs. is plain motoring |
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Definition
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Term
| BAT start is not allowed if battery temp is below __ |
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Definition
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Term
| Min. voltage for battery start |
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Definition
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Term
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Definition
| 5690 lbs (850 gals); 2845 lbs per side (425 gals) |
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| Engine anti-icing must be __ when in incing conditions.....and maintained __ for at least __ mins. after exiting icing conditions. |
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Term
| Max Contaminant Levels (Water, Slush, Wet Snow, Dry Snow) |
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Definition
| Water, Slush, Wet Snow=1/2 inch; Dry Snow 3 inches |
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Term
| For propeller deicing, icing conditions exist when the OAT or SAT is __ degrees C or colder and any ice accretion is observed on any part of the a/c. |
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Definition
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Term
| (Prop deice) The __ selection should be selected when the SAT is between -5 C and -12 C. |
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Definition
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Term
| (Prop deice) The __ selection should only be selected when the SAT is -13 C or colder unless vibrations occur at the warmer temps. |
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Definition
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Term
| Definition of icing conditions for operation of wing/stabilizer boots |
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Definition
-OAT or SAT +5 C or colder and there is visible moisture present or
-Any amount of ice is observed on any part of the A/C, or
-If it is not certain there is no ice accumulation on the a/c. |
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Term
| The deicing boots should be use when... |
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Definition
-Operating in icing conditions as defined for operation of wing/stabilizer boots
-Until reaching 400 ft above t/o field elevation on t/o, use the boots only at the first sign of ice on a/c
-If the SAT is below -40 C, use boots only if ice is observed accumulating on a/c |
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Term
| The deicing boots can be turned of when |
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Definition
-OAT or SAT is warmer then 5 C and no ice is on the wipers or
-No visible moisture is present and 3 deicing boots cycles (9 min in continuous mode) have been completed after exiting visible moisture. |
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Term
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Definition
7 or 15: 175 KIAS
20: 165 KIAS
35: 140 KIAS |
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Definition
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Term
| Extension Speed Vloe, Emergency Extension Speed Vloee, Extended Speed Vle |
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Definition
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Term
| Maximum Operating Speed, Vmo |
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Definition
| 250 KIAS up to 16000 ft. Vmo decreases above this altitude as indicated by the pointer to approx 210 KIAS at 25000 ft. |
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| Max Rough Air Penetration Speed, Vra |
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Definition
| 190 KIAS up to 21000 ft. Above, reduce speed by the Vmo pointer minus 30 kts. |
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Term
| Min. speed in icing conditions |
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Definition
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Term
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Definition
| Weight dependent speed which is used as a minimum speed during the maneuvering portion of approach or departure |
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Term
| Minimum Maneuvering Speeds, Vmm (all flap settings) |
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Definition
0: Vref20+30;Vref35+35
7: Vref20+20;Vref35+25
15: Vref20+15;Vref35+20
20: Vref20+10
35: Vref35+10 |
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Term
| All engines operating climb above MSA, cruise, descent, holding and approach (all flap settings) |
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Definition
| Flaps 0: 160 KIAS; Flaps 7: 150 KIAS; Flaps 15: 145 KIAS; Flaps 20: 140 KIAS; Flaps 35: 130 KIAS |
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Term
| Minimum Airspeed for Icing Conditions during climb (no maneuvering) |
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Definition
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Term
| Minimum Airspeed for Icing Conditions during climb (maneuvering)below MSA |
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Definition
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Term
| Minimum Airspeed for Icing Conditions during climb above MSA, cruise, descent, holding and approach |
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Definition
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Term
| Minimum Airspeed for Icing Conditions corrected Vref |
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Definition
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Term
| Minimum Airspeed for Icing Conditions final approach (maneuvering) |
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Definition
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Term
| Minimum Airspeed for Icing Conditions during missed approach/go-around below MSA |
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Definition
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Term
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Definition
Flaps Retracted: +2.75 to -1.0
Flaps Extended: +2.0 to +-0 |
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Term
| Airport Pressure Alt. Limits |
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Term
| Min. main battery temp for takeoff |
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Definition
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Term
| Min emergency lighting batter temp for takeoff |
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Definition
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Term
| Maximum Differential Pressure; Auto Mode Schedule |
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Definition
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Term
| Abort (Normal Braking): Where normal braking has been used a __________ is adequate for brake cooling. |
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Definition
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Term
| If another takeoff after an abort is to be made, if abort was not mechanical of nature, the PIC will |
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Definition
1) Contact dispatch and notify of abort with no need for mx
2)Make sure that 15 minutes have elapsed prior |
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Term
| High Energy Abort is when |
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Definition
| abnormal braking has occurred or an abort is conducted above 80 KIAS at max braking. |
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Term
| In circumstances where abnormal braking has been necessary pilots must consult _____ to determine if additional cooling time will be required. |
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Definition
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Term
| In the case of high energy abort the PIC will: |
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Definition
1)Make an entry in the CA-1 discrepancy column
2)Contact dispatch and Mx to inform them
3)Mx will determine need for inspections and other steps to be taken |
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Term
| Use of the F/D during T/O is not authorized when below ___ AGL or ____ ____, whichever is higher |
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Definition
| 500', acceleration altitude |
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Term
| Autopilot operations not authorized |
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Definition
-during T/O below 500' ft AGL or acceleration altitude.
-during landing below 200' AGL on precision
-during landing below MDA on non-precision
-during landing below 500' AGL on visual
-during go-around below 200' AGL
-Speeds below 1.3xStall Speed- in HDG |
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Term
| Autopilot operations not authorized in ____ conditions as defined in icing conditions for adherence to ap/fd limitations. |
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Term
| In IMC final config must be accomplished prior to |
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Term
| In VMC, final config must be accomplished no later than |
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Term
| For single engine non-precision approaches final flaps will be delayed until... |
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Term
| For circling approaches, finals flaps will be selected when leaving the... |
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Term
| The cargo compartment is classified as a Class __ cargo compartment....it provides minimum fire protection for |
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Definition
| C; 60 min (forward lav. and Mod. No 1449 incorporated (2 bottles); 35 min for all other aircraft |
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Term
| Windshield Wipers: Low mode; high mode |
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Definition
| 130 KIAS Max; 160 KIAS Max |
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Term
| Crosswind T/O and Landing |
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Definition
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Term
| DC Gens: Maximum Load; Nominal Load per Gen. |
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Definition
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Term
Main Battery Temps
No Battery Start:
No Cross Gen Start:
Max for T/O:
Battery Hot Light: |
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Definition
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Term
External Power
Max Voltage:
Min. Current During Engine Start:
Max. Current During Engine Start: |
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Definition
29.5 VDC
1200 Amps
1600 Amps |
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Term
| O2 Min Dispatch Pressures |
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Definition
-800 PSI with 2-3 crewmembers below 10k
-1250 PSI with 2 crewmembers above 10K
-1650 PSI with 3 crewmembers above 10K |
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