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69 Cards in this Set
- Front
- Back
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Max. Tailwind Component Crosswind Component |
10 kts (Tail) No Limit (Cross) - Demo at 24 kts Company Limit: 24 kts Crosswind including gusts |
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Max. Ramp Weight |
20,400 lbs |
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Max. Takeoff Weight |
20,200 lbs |
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Max. Landing Weight |
18,700 lbs |
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Max. Zero Fuel Weight |
15,100 lbs |
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Min. Flight Weight (Gust Loading) Min. Flight Weight (RVSM) xls+ only |
12,400 lbs 14,000 lbs |
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Max. Fuel Imbalance (normal / emergency) |
400 lbs / 800 lbs (emergency) |
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Tailbone Baggage Comp. |
700 lbs |
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Ambient Temperatures Max. Temp T/O + Landing Min. Temp T/O + Landing |
ISA +39 C / -54 C (XLS) ISA +35 C / - 54 C (XLS+) |
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Max. Operating Alt. |
45,000 ft |
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Max. T/O + Landing Alt. |
14,000 ft |
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Max. Alt. for Extension of Flaps and Gear |
18,000 ft |
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Airspeed Limits Mmo (above 26,515 ft) Vmo (8,000 - 26,515 ft) Vmo (below 8,000 ft) - Limit for? |
Mach 0,75 305 KIAS 260 KIAS (Bird Strike Limit) |
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Autopilot Operation Speed Limits |
305 KIAS or 0,75 Mach indicated |
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Airspeeds Flaps 7/15 |
200 KIAS |
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Airspeeds Flaps 35 |
175 KIAS |
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Airspeeds Landing Gear Extending |
V(LO) 250 KIAS |
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Airspeeds Landing Gear Retracting |
V(LO) 200 KIAS |
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Airspeeds Landing Gear Down |
V(LE) 250 KIAS |
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Airspeeds Speed Brake Extended |
V(SB) No Limit |
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Airspeeds Turbulent Air Penetration (severe turb) |
180 KIAS |
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Airspeeds Max. Tire Ground Speed |
165 KIAS |
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Airspeeds Min. Speed in Icing Conditions (except for app. & landing) |
160 KIAS |
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Airspeeds Minimum Speeds Clean / Flaps 7 / Flaps 15 / Flaps 35 Min. Control Ground Min. Control Air |
Clean: Vref + 30 ~ ca. 145 KIAS Flaps 7: Vref + 20 Flaps 15: Vref + 20 Flaps 35: Vref + 10 V(MCG) 81 KIAS V(MCA) 90 KIAS |
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Aircraft General Vortex Generators |
52 (26 per Wing) up to 3 may be missing (AC limited to 41,000 ft) |
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Aircraft General Boundary Layer Energizers |
22 (11 per Wing) non missing |
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Aircraft General Must be operational for T/O |
Rudder Bias + Heater Antiskid |
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Engine Type / Thrust / Bypass Ratio |
PW545B (xls) / 4.095 lbs = ca. 1900 kg = ca. 18,32 KN / 3,8:1 PW545C (xls+) / 4.095 lbs = ca. 1900 kg = ca. 18,32 KN / 3,8:1 |
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Engine - Max. ITT Starting - Starting Transient / Time |
XLS: 740 C Transient 780 C for 20 sec. XLS+: 670 C Transient 780 C for 20 sec. |
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Engine Min. Oil Temperature for starting engines |
- 40 C |
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Engine Take Off Power Time Limit |
5 Minutes / 10 Minutes for Single Engine |
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Engine Max. Oil Consumption |
1 quart per 10 hours |
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Thrust Reverser Max. Deploy Time Ground Operation Prohibited |
3 min. / 10 min. period Idle Thrust During Touch and Go Landings + to back the Airplane |
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Thrust Reverser Check |
1. prior first flight of the day 2. prior any flight TR is used for performance 3. first flight after maintenance |
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Fuel Min. / Max. Temperatur |
-40 C / + 57 C |
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Fuel Types / Prist |
Jet A; Jet A1; Jet B etc. AVGAS not approved Prist approved but not required |
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Fuel Boost Pumps Operation |
On for LO FUEL LEVEL annunciatior or 400 lbs or less indicated fuel |
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Electrics Starter Limits (Engine / APU) |
3 in 30 min. with 90 sec. rest between |
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Electrics Battery Limits |
3 engine starts in 1 hour Generator assisted start equals 1/3 battery start |
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Electrics GPU - Amperage - Volts |
800-1000 Amps 28 Volts |
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Electrics Loads Ground / Transient (time) / Flight |
200 amps ground 250 amps up to 4 min. transient 300 amps flight |
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Autopilot Operation Min. Use Heights |
1000 ft AGL - Cruise 300 ft AGL - NPA 180/200(xls+) ft AGL - PA (CAT I) 80 ft AGL - CAT II etc. |
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Autopilot Operation Overview |
- 1 Pilot must remain in his seat during AP operation - AP + YD off for T/O + Landing - AP engage height after T/O or missed approach (min.) 300 ft AGL |
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Avionics Operational Items for Dispatch |
PFD / MFD normal mode AOA System AHRS 1 & 2 ADC 1 & 2 Standby Flight Instruments (min. 1) ATT ALT ASI HSI |
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APU Operation prohibited when: |
- Test - Applying deice - TR deployment (more than 30 sec.) - if unattended - above FL 300 |
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APU Start attempts prohibited after: |
- APU fail light - after dual generator failure - after shutdown until 30 sec. after RPM reads 0% - above FL 200 |
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APU Cycles |
9 APU starts per hour (Battery limit) APU battery starts count as 1/3 of main engine start |
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Pitot Static Heat Limit |
2 Minutes on Ground |
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Tail Deice System Limits |
Min. Temp -40 C (Airspeed below 150 KIAS) Min. Temp -35 C (Airspeed at or above 150 KIAS) |
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T/O prohibited with frost on: |
- Wing leading edge - Wing upper surface - Windshield |
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T/O and Landing Operational Limits |
- engine sync must be off - paved runways only - when using TR min. width of RWY of 75 ft |
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Cabin Pressurization Limits |
Normal Cabin Pressure: 0,0 - 9,6 Pressure Relief Valve: 9,5 Pressure Gage Red Line: 9,7 |
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APU Operating Limits Max. EGT Max. N1 Start: Run: |
690 C 108 % 20,000 ft 30,000 ft |
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APU Temp Limits |
-54 bis +54 |
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Requirements RVSM |
- Pilot + Copilot primary Altimeters - Autopilot - Altitude alerter - ATC RBS transponder |
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Airspeed Min. RVSM |
160 KIAS |
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Load Factors Flaps Up |
-1,2g to +3,0g at 20,200 lbs |
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Load Factor Flaps T/O, T/O and Approach and Landing |
0,0g to +2,0g at 20,200 lbs |
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Load Factor Flaps + Landing Weigth |
0,0g to +2,0g at 18,700 lbs |
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Max. Landing Sink Rate |
600 ft / min. |
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Static Wicks |
20 pieces (6 Left Wing / 6 Right Wing / 8 empennage) Can be missing on the wing tips and/or on the stinger - all others must be present for flight |
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Max. Usable Fuel (lbs/USG/L) |
6.790 lbs 1006 USG 3810 Liter |
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Aircraft General Dimensions (ft/m) Wingspan / Length / Height / Main Wheel Spann |
Wingspan: 56,30 ft / ~ 17 m Length: 52,10 ft / ~ 16 m Height: 17,20 ft / ~ 5 m Main Wheel: 14,90 ft / ~ 4,5 m |
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Speed Brake Panels (how many) |
4 |
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DRY OPERATING MASS |
Ca. 13,100 lbs (XLS/XLS+) = ca. 2,000 lbs Payload for ZFM |
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Max. Landing Weight EDRY |
16,900 lbs (without approval from Flight OPS) |
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APU maximum Generator Loads |
200 ampere (on ground) 300 ampere (in flight) |
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Service Air (23psi) |
Supplied by the engines for:
1. horizontal stab deice boots Inflation pressure 2. pressurization outflow valve operation 3. cabin entrance primary door seal and acoustic door seals 4. throttle detents, eecs auto mode |
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Engine bleed air (P3) |
1. environmental / pressurization 2. wing anti-ice 3. service air |
