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DL B717 Limitations
| Question | Answer |
|---|---|
| Maximum operating altitude | 37000 |
| Maximum TO landing tailwind component | 10 knots |
| Maximum crosswind component for TO and landing | 38 knots 15 knots autoland Contaminated runway |
| Severe turbulence air penetration | 275 knots .75M |
| TO autopilot engage minimum altitude | 200 ft |
| Autoland maximum wind speeds | Headwind 25 knots Crosswind 15 knots Tailwind 10 knots |
| APU AIR | Switch must be off for take off and in-flight operations |
| RUNWAY SLOPE | +1.7% -2.0% |
| CENTER TANK FUEL IS PRESENT AND WILL BE NEEDED | Center tank fuel pumps must be individually checked to veryfy pump operation prior to engines start |
| LANDING GEAR SPEEDS | Max retraction 250 KIAS Max extension 300 KIAS Max tire 195 KIAS |
| FUEL TEMPERATURE | Maximum fuel temp is 54°C (JA1,JP5/8) 35°C (JB, JP4) Minimum fuel temp is the higher of Fuel freze point -42°C for TO, climb, and GA -48°C for flight above 150 |
| MAX TO AND LANDING PRESSURE ALTITUDE | 8500 feet |
| Manuver limit load factors | Flaps/slats retracted +2.5g to -1.0g Flaps or slats extended +2.0g to 0.0g |
| FUEL IMBALANCE | 1500 lb |
| FUEL MANAGEMENT | Use center tank fuel (excluding ballast fuel) prior to using main tanks fuel |
| WHEATHER RADAR | Do not operate in a hangar or within 50 ft of personell or fuel spill |
| ALTIMETER READING DIFFERENCES CA/FO | On the ground CA/FO 60 Ft CA/FO & field elevation 75 Ft On the air CA/FO 200 Ft |
| SPEED BRAKES | Don't use with flaps beyond 20° Don't move to ground spoiler position in flight |
| RUDDER | Rudder hydraulic power must be on for TO |
| APU | Max operatin altitude 370 Cycle 3 consecutive start attemts. Whait 30 minute prior to further starts. |
| ENGINE STARTER DUTY CYCLE | 3 start attempts with a minimum of 15 sec between attemps. Starter on max durtion 3 min. Allow 15 minutes cooling time before further start attemps are mad. |
| PRESSURIZATION | Max cabin differential 7.86 psi. Max emergency relief pressure is 8.27 psi. |
| CRACKED WINDSHILD | Do not operate W/S anti-ice and anti-fog. Below 10,000 ft speed Outer glass 315 KIAS Inner glass 235 KIAS |
| OXIGEN | 1000 psi |
| Engine oil | |
| Maintenance station 9 qt Non Maintenance 7 qt | |
| Hydraulic quantities left and right | |
| 7 quarts | |
| Take off thrust and engine shutdown time | 3 minutes |
| Documents before departure | Dispatch Release, Release Verification, Release Addendum, FSR/EFSR, PDC (30), NOTOC/NOTA (15), Pre-Pushback (8), Updated Weather Briefing, WDR (-5/+1). |
| 180° turn | 81 feet |
| Wing span and lenght dimensions | |
| Wing span 93 feet Fuselage lenght 124 feet Hight 29.1 feet |
Created by:
Gbaron
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