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Types of Aircraft Operations
This airplane is certificated in the Transport Category under FAR Parts 25, 36, JAR 25 and ICAO 16. When the appropriate equipment and instruments, as required by the airworthiness and operating regulations are approved, installed and in operable condition, flight in the following conditions are approved.
- * Day and Night
- * VFR and IFR
- * Flight in icing conditions
- * Reverse thrust taxi (single and two engine)
- Warning
- The airplane is prohibited from flight into severe icing conditions, which are outside of the certification envelope. In case of inadvertent encounter, refer to the Severe Icing Emergency Procedure, [ICE]
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Altitude
Maximum Operating Altitude
Minimum Takeoff and Landing Altitude
Maximum Takeoff and Landing Altitude
- Maximum Operating Altitude........................25,000 ft.
- Minimum Takeoff and Landing Altitude..........-1000 ft.
- Maximum Takeoff and Landing Altitude..........8,500 ft.
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Limiting tailwind component
Limiting tailwind component............................10 kts.
- Note
- Tailwind operations with up to 15 kts. are approved only when airport analysis supporting greater than 10 kts. of tailwind is provided.
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Maximum Demonstrated Crosswind component on a Dry Runway (kts.)
- Takeoff..............................................................35 kts.
- Landing..............................................................35 kts.
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Maximum Operating (Mach) Mmo
Mach .55
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Maximum Operating (KIAS) Vmo
250 KIAS
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Landing Gear Extension VLO(ext)
170 KIAS
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Landing Gear Retraction VLO(ret)
160 KIAS
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Landing Gear Extended VLE
185 KIAS
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Flap Placard Speeds VFE15 & VFE30
15
30o
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Maximum Rough Air Penetration VRA
VRA - 180 KIAS
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Maximum Maneuvering VA
VA - 175 KIAS
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Maximum Wiper Operating
160 KIAS
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Cabin Pressurization:
Max Diff
Min Diff
Max Diff w/ for overboard valve full open selection
- Max Diff..........................................................6.35 psi
- Min Diff............................................................-0.5 psi
- Max Diff for overboard valve full open selection..1 psi
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Autopilot/Flight Director Limitations
- A flight director mode must be selected prior to autopilot engagement.
- Minimum height for autopilot engagement after takeoff will be 500ft. AFL.VOR approaches uning NAV mode with either autopilort or flight director is authorized only if; - A collocated DME is available, and - DME HOLD is not slected.
- Minimum height for use of either autopilot or flight director. - Except during take off or executing an approach 1,000 ft. AGL. - APP, V/S or IAS mode during approach; 160 ft AFL
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During flight, severe icing conditions that exceed those for which the airplane is certificated shall be determined by the following:
PrimaryVisual Cues
Primary Performance Cues
PRIMARY VISUAL CUES are characterized by ice covering all, or a substantial part of the unheated portion of either forward side window, possibly associated with water splashing and streaming on the windshield.
AND/OR
PRIMARY PERFORMANCE CUES are characterized by unexpected decrease in airspeed an/or rate of climb.
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Max Fuel Imbalance (lb.)
1609 lb.
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