FAN RPM (N¹)
100%
Maximum
102%
20 Sec. Transient
***************************
TURBINE RPM (N²)
101.8% Takeoff
101.8% Max Continuous
103% 20 Sec. Transient
Ground Idle (Min.) 47%
Flight Idle (Min.) 51.5%
XLS
102.8%
Takeoff
102.8%
Max Continuous
104%.
20 Sec. Transient
106.2.%.
5 Second
EXCEL
*******************************
INTER-TURBINE TEMP (ITT)
720°
Continuous
720°
Takeoff 5 min. / 10 min.
760°
20 Sec.
670°
7 secs. start
XLS
720° C
Continuous
XLS
720-740°C. Yellow
5 min. dual / 10 min. Single.
740° Max Starting 5 secs.
670° 7 secs. Starting
780° C. Transient 20 secs.
********************************
OIL PRESSURE
20 psi
Minimum (Red)
20-45.
45-140
(Yellow)
Normal
(Green)
Above 60% N²
250 psi
(◄ ► ) 120 secs.
EXCEL
XLS
20 psi
Minimum (Red)
20-45.
(Yellow)
45-160
Normal
(Green)
Above 60% N²
250 psi
400 secs. (◄ ►)
(6½ min.)
Gauge Tape will continue white to 250 psi until
time limit (400 secs.), then turns Red.
OIL TEMPERATURE
10° to 121° Continuous
121° to 135° 120 secs. ◄ ►
-40°
XLS
Minimum for Start
10 - 121° C Continuous
121 - 135° C 400 Secs. ◄ ►
(6½ min.)
-40° Starting
*********************************
AMMETER
200 Amps ▼ (ground)
(250/4 min. ground)
300 Amps
Red Line (flight)
*********************************
CABIN DIFFERENTIAL PRESSURE
9.5 psi
Pressure Relief
9.6 psi
Green
9.7 psi
Red Line
* Cabin Differential Pressure is
maintained at 9.3 psi
OXYGEN PRESSURE INDICATOR
0 to 400
Yellow
1,600 to 1,800 Green Arc
2000
Red
XLS
Crew Masks
40,000'
Passenger Masks 25,000'
Fuel Temp
-40°
Minimum
+57°
Maximum
********************************
Ground Idle Min: 47% N²
Flight Idle Min:
51.5% N²
Normal
Ground Idle: 48% - 51% N²
Flight Idle: 57% - 62% N²
L/R Ignition ON prior to reducing power to less than 70% N²
STARTER LIMITS
3 starts/30 minutes 90 sec. cooling period
Batt Limit: Engine 3 Starts/Hour
APU 9 Starts/Hour
BATTERY LIMITS
3 Engine Starts per Hour
BATT Start
1 Battery Debit
Air Start (with starter assist)
1 Battery Debit
Gen Assisted
1/3 Battery Debit
Engine Start w/APU
No Debit
Starting APU
1/3 Battery Debit
AutoPilot (Minimum Altitude)
180' AGL Precision
300' AGL Non Precision
1000' AGL Enroute
A/P Operation is Prohibited if any 9 Comparison Monitor lights are Illuminated
Cold Soak:
2 Hours or Longer in ambient temp of
-18°C (0°F) or colder, the cabin must be at a minimum of 10°C (50°F) prior to departure.
Takeoff Temp
Max ISA +39°C
Min
-54°C
-40°C Minimum Ambient Temp for Ground Starting
ISA
Sea Level
+15°C
29.92
WARNING
DO NOT retract flaps above 200 KIAS. Associated stabilizer movement can cause
significant nose down pitch upset
Altimeters: (RVSM)
±50' Departure Airfield
±75' of Each Other
In Flight: ±200' of Each Other
Tailwind / Crosswind
Max Tailwind 10 Kts
• Direct 90° Crosswind Dry/Wet - 24 Kts
• Contaminated Runway
Runway ≥ 150' in Width - 15 kts
< 150' in Width - 10 kts
FOM Fleet Specific FS.3
De-Ice Boots
A/S 150 ≥ KIAS -35° C
A/S < 150 KIAS -40° C
C.G. Ranges (approximate)
Zero Fuel 321.0" - 331.26"
Max Landing 330.74" - 331.0"
20,400
324.29" - 331.0"
Circle Approach
Category C Minimums
Vref + 20 min
30° Max. Bank Angle
1,000 fpm descent
Lined up on final by 300' AFE
ALTITUDE LIMITS
41,000'
1-3 Vortex Generators Missing
41,000' & 200 KIAS
Stab MisCompare
31,000' & 200 KIAS
Hyd Press Light Illuminated
Max. Operating Altitude 45,000'
Max. Takeoff/Landing 14,000'
AIRSPEED LIMITS
MMO (Above 26,515ft) ……...……………..
VMO (Below 8,000ft) ……………………….
VMO (8,000ft to 26,515ft) ………………….
Autopilot Operation ………..………………
VA ……………………………….…….…….
VSB ….………………………………………
VLE ………………………………………….
VLO …………………………………………
VFE (flaps 7º or 15º)……………………….
VFE (flaps 35º, fully extended) …………...
Turbulence Air Penetration ……………....
Max Tire Ground Speed ………………….
Min Speed in Icing…………………………
0.75 Mach (Indicated)
260 KIAS
305 KIAS
305 KIAS or 0.75 Mach Indicated
Varies with Weight & Altitude
No Limit
250 KIAS
200 KIAS
200 KIAS
175 KIAS
180 KIAS
165 KIAS
160 KIAS
(* except for approach & landing)
VMCG (AB, Rudder Bias) ………………….. 81 KIAS
VMCA ………………………………………… 90 KIAS
WEIGHT LIMITS
Max. Ramp Weight ……………………… 20,200lbs
Max. Takeoff Weight …………………… 20,000lbs
Max. Landing Weight ……………………18,700lbs
Max. Zero Fuel Weight (ZFW) ………….15,000lbs
Minimum Flight Weight (Gust Loading) .. 12,400lbs
Max. Fuel Imbalance (Normal) ………… 400lbs
Max Fuel Imbalance (Emergency) …….. 800lbs
Tailcone Baggage Compartment ………. 700lbs
* XLS
*20,400 lbs
* 20,200 lbs
* 15,100 lbs
** Takeoff Weight may be to be reduced to meet climb requirement or takeoff field length.
** Landing Weight may have to be reduced to make climb requirements, brake energy limits, or for
landing distance.
●Forward
Cabinet (Vacuum / First Aid Kit) - 20 lbs
Cabin Cargo Area (AED) - 80 lbs
● Maximum Floor Loading -100 lbs/ft²
● Aft Cabin Closet - 20 lbs
● Aft Exterior Cargo Area -700 lbs
● Maximum Floor Loading -100 lbs/ft² (74 cu. ft.)
● Rear
THRUST REVERSERS
Max. Reverse Thrust ……………………
Landing ……………………………………
Max. Allowable Deploy Time …………..
Touch and Go Landings ………………..
Preflight Check …………………………..
Use to Back Airplane ……………………
75% of Takeoff Thrust
Thrust to Idle @ 60 KIAS / Stow @ 40 KIAS
3 min/10 Min. Period
Prohibited
Conducted Prior to First Flight of the Day
Prohibited
LANDING GEAR & BRAKES
Antiskid Must Be Operational For Takeoff
GROUND HANDLING
Lektro Nose-Lift Tugs: All commercial models of the Lektro Tugs are approved for use.
Current Models 8699, 8650, 8700, 8750, 8850, 8950
Towing Restrictions:
95 Turning - Maximum
(60º When Towing if the Control Lock is Engaged)
Nose Wheel Steering: 20º
Engine Oil: Exxon/BP 2380
Max Oil Consumption: Excel 1 Quart/10 Hours XLS 1 Quart/8 Hours
Lav Service: 1.5 – 2.0 Gals Fluid
Maximum Runway Slope: ± 2%
Maximum Standing Water on Runway: ¾"
SPECIFICATIONS
Length …………………
Height …………………
Wingspan …………….
Wheelbase …………..
Turn Radius ………….
Door Width …………...
Height …………………
Cabin Aisle ……………
Height …………………
52' 10"
17' 2"
55' 8"
14' 11"
70' 7" (Wing) 38' (Wheel)
24"
57"
13"
5' 8"
Minimum Airspeed RVSM: 160 KIAS
Minimum Weight RVSM: 14,000 lbs