• Min Control Speeds • o VMCA o Vmcl Vmcl-l2 o Vmcg
• Min Control Speeds
•
Minimum Control Speed in the Air-87.5 Kia’s
Minimum control speed landing-86.6kias
Minimum Control one engine inoperative- 84.6
Minimum Control Speed on the ground-88.9
Miscellaneous Speeds
Vwwo
Vw
Vt
Stall speed
o Misc Speed
o
o wiper operating speed-215kias–(windshield op)
o window open speed-215kias—-(sliding window open)
o ground speed- 195kias
o Stall speed- don’t fly below stall warning-duh?
• TO&LNDG Limitation o o Ruway slope o Airport pressure altitude o TO Tail wind component
• TO&LNDG Limitation
o Ruway slope – or + 2.5˚
o Airport pressure altitude- -1000ft /+14,000 SB2038
o TO Tail wind component- +5
• Weight Limitations (LBS) o Max Runway Weight o Max Take Off Weight o Max Landing Weight o Zeroe Fuel Weight o Minimum Flight Weight o o Baggage o Payload
• Weight o Limitations (LBS) o MRW----49,200 o MTOW--49,000 o MLW----44,500 o ZFW-----30,864 o MFW----20,700 o o Baggage- 2866 123lbs/sq ft. o Payload-5,960
Baggage compartment & Lavatory
Access to both prohibited Abv FL410
Lav door must be closed and latched
Cabin Pressurization
Max differential
Min neg differential
Dump
9.6 psi
-0.29psi
14,000+ or- 500ft
Auto-Pilot engagement
When is AP unavailable?
TO
LNDNG
GA
Min Use Height
Aft TO climb
On ILS Aprch
Auto Throttles
Auto-Pilot engagement
TO- Do not engage below V2+10kt
LNDNG-Do not engage below VREF+10
GA-NA
MUH
400ft
65kias
Same numbers for auto throttles (AT). 400ft up. 65kias downDC Voltage
max voltage
Eng Gen Limits
Max out put
Up to FL430
Abu FL430
On the groundDC voltage
32V
350A
300A
260A
225A
Battery Limitations
Warm Bat (CAS msg)
Hot Bat (CAS msg)
Battery Limitations
At or >120˚F (48.9˚C)
At or >160˚F(71.1˚C)
WARNING!!
OVHD BACKUP PWR LH OR RH FA
APU Generator LIMITATIONs
WARNING!!
No more bkup PWR supply for OH panel
350A (transient 1 minute)
300A stabilized
ARTHUR
Max spd w Arthur InOp
SLATS/FLATS
Max alt for slat flap opp
AIRBRAKES
Extension Limit
ARTHUR
260kias/.76m
SLATS/FLAPS
FL200
NO FLAPS or SLATS Abu FL200 Extension executed one notch at a time Low speed "cue" is lost when system can not identify airplanes configuration (makes sense) AIRBRAKES- NONE at or
Fuel ATA 28
Capacity (for 900LX)
LT
CT
RT
Total
Fuel ATA 28
1043gal. 6990lbs
1,027gal. 6885lbs
1,049gal. 7032lbs
Total. 2,804gal. 20,907lbs
Fuel ATA 28
Fuel Temp Fuel System Pressure Fuel Additives
Fuel ATA 28
3˚C Abv freezing point
50psi
What additives do we use
Hydraulics ATA29
Approved Fluids
Quantity
PressureHydraulics ATA29
5606
Green Range
3000 psi + or -200psiATA 30 Ice and Rain Protection
Icing conditions
ATA 30 Ice and Rain Protection
Icing conditions exist when OAT on grand or TAT in flight 10˚C or
ATA 30 Ice and Rain Protection (cont)-Engine Anti Ice
When not to use?
When to useATA 30 Ice and Rain Protection (cont)-Engine Anti Ice
When TAT is > 10˚C (50˚F)
During climb when them is -40˚C SAT
AI must be used when descending into known icing conditions & temp is ,-40˚C SATATA 30 Ice and Rain Protection (cont)-Wing Anti Ice
When to use
When not to useATA 30 Ice and Rain Protection (cont)-Wing Anti Ice
Not be used when TAT is >+10˚C
Not be used on ground except for checksWarning ATA 31
Speed Increase alert when?
Low speed alert when?
Warning ATA 31
Aprch w/o flaps VREF +30/30knts
When system cannot identify airplanes configurationATA 32-Tires and Bakes
Nose Wheel info?
Brake Limit?
Brake Cooling Time?ATA 32-Tires and Bakes
Must be equipped with chines to avoid water ingestion by engines
18,750 Joules
Use minimum turn around tables or check brake temp on PDU 153˚C if you have not done 10 full stops at taxi speed of
20knts or 40 full stops from taxi speed of 10knts
Brake cooling time not affected by park brake applicationATA33-Landing Lights
Ground Ops limit
ATA33-Landing Lights
Limited to 15min cycles w 45 min cooling period between cycles
ATA34-Navigation w M55595
IRS alignment
TCAS II System Op explanationATA34-Navigation w M55595
Functional btwn 78˚15' N 7815' S
Pilots are authorized to deviate from current ATC clearance in order to comply
Following clear of conflict” msg return to ATC clearance unless advised by ATC