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RPA UPGRADE
LIMITATIONS
| Question | Answer |
|---|---|
| Max. Takeoff and landing TAILWIND component | 10 Knots |
| Max. Operating Altitude | 41,000' |
| Max. Flap Extension Altitude | 20,000' |
| Turbulent Air Penetration Speed: Below 10,000 MSL | 250 KIAS MAX |
| Turbulent Air Penetration Speed: Above 10,000 MSL | 270 KIAS / 0.76M MAX |
| Landing Gear Speeds (VLO and VLE) (E170 & E175): Max Landing gear EXTENSION speed (VLO) | 250 KIAS |
| Landing Gear Speeds (VLO and VLE) (E170 & E175): Max landing gear RETRACTION speed (VLO) | 250 KIAS |
| Landing Gear Speeds (VLO and VLE) (E170 & E175): Max landing gear EXTENDED speed (VLE) | 250 KIAS |
| Maximum Tire Ground Speed | 195 Knots |
| Maximum Flap Operating Speeds - VFE ; Flap Position 1 | 230 KIAS |
| Maximum Flap Operating Speeds - VFE ; Flap Position 2 | 215 KIAS |
| Maximum Flap Operating Speeds - VFE ; Flap Position 3 | 200 KIAS |
| Maximum Flap Operating Speeds - VFE ; Flap Position 4 | 180 KIAS |
| Maximum Flap Operating Speeds - VFE ; Flap Position 5 | 180 KIAS |
| Maximum Flap Operating Speeds - VFE ; Flap Position Full | 165 KIAS |
| Design Maneuvering Speed - Va | 240 KIAS (C) |
| Ice conditions exist when Static Air Temperature (SAT) on the ground / takeoff or Total Air Temperature (TAT) in flight is: | 10 Degrees Celsius or Below AND visible moisture in any form is present OR when operating on contaminated surfaces |
| During Taxi out and takeoff, the MCDU DATASET MENU must be set to | ALL when SAT is 10 degrees Celcius or below and icing conditions exist or are anticipated to be encountered below 1700 AFE (C) |
| Maximum Usable Fuel Quantity per tank | 10,393 pounds (1536.0 US Gal) |
| Unusable quantity per tank | 75 pounds (11 US Gal) |
| Aircraft Maximum fuel capacity (Usable + unusable fuel) | 20,936 pounds (3094 US Gal) |
| Maximum fuel imbalance between tanks | 790 lbs. (C) |
| The XFEED selector must be set to _____ during takeoff and landing | OFF |
| Air conditioning : The maximum altitude for single pack operation is: | 31,000' |
| Flaps: Maximum Altitude with flaps extended | 20,000' |
| Enroute use of flaps is: (Prohibited or not Prohibited?) | Prohibited |
| Are holds in icing conditions with flaps extended permitted? | No |
| Are Flaps 4 during approach and landing prohibited? | Yes |
| Thrust Reversers: Must be stowed below _____ knots | 60 KIAS |
| Maximum Crosswind Component (CAT II) | 12 Knots |
| Powerplant Warm up / Cool down: before applying takeoff thrust, allow the engines to warm up for a minimum of ____ minutes | 2 minutes |
| Powerplant Warm up / Cool down: Allow engines to cool down for _____ minutes prior to shutting down an engine | 2 minutes |
| EICAS Engine Limit Display Markings: Red | Maximum and Minimum Limitations |
| EICAS Engine Limit Display Markings: Yellow (amber) | Caution Range |
| EICAS Engine Limit Display Markings: Green | Normal Operating Range |
| Engine Thrust: Reduced Thrust takeoffs are prohibited when: (3 items) | 1. The runway is contaminated with standing water, slush snow or ice 2. Windshear is present or suspected 3. Performance mandates no FLEX |
| Single Engine Taxi is not authorized when: | Braking action is less than good OR RVR is less than 1,200' |
| Stabilized Approach Criteria | From 1000 feet above the TDZE, the aircraft will be: -Within the final landing configuration selected -On correct vertical path with a decent rate of 1000 FPM or less -Correct lateral tract (appropriate for type of approach being flown) From 500 feet above the TDZE, the aircraft will be: -At calculated approach speed (-5 to +10 kts) -With engines spooled* (The engines are stabilized at the thrust setting required to maintain the desired airspeed and rate of decent) |
| Maximum Airspeed for windshield wiper operation is: | 250 KIAS |
| APU Operational Limits: Max. Start Altitude | 30,000 ft |
| APU Operational Limits: Max. Altitude Operation: | 33,000 ft |
| APU Operational Limits: Max. Bleed Operation: | 15,000 ft |
| APU Operational Limits: Max. Altitude to assist engine start | 21,000 ft |
| Max Zero Fuel Weight E170 | 65,256 |
| Max Zero Fuel Weight E175 | 69,886 |
| Max Forward Cargo Compartment for the E170 | 3020# |
| Max Dry Ice E175 | 440# |
| Max Dry Ice E170 | 300# |
| Can Dry Ice go in both compartments? Why? | No, it is not allowed in the aft cargo compartment... It gives off gas as it melts, it must be in a ventilated area, if not it will build pressure |
| Max Takeoff and landing altitude | 8,000 feet |
| Minimum Temperature for takeoff and landing? | - 40 Degrees Celcius |
| Max Crosswind for RCC 6 | 38 kts |
| Max Crosswind for RCC 5 | 31 Kts |
| Max Crosswind for RCC 4 | 20 Kts |
| Max Crosswind for RCC 3 | 15 Kts |
| Max Crosswind for RCC 2 | 12 Kts |
| Max Crosswind for RCC 1 | 8 kts |
| Max direct Vision window speed operation speed | 160 Kts |
| Minimum Fuel Tank Temperature? | -37 degrees Celcius |
| Which tank is the fuel is the temperature measured from? | Left Tank |
| When does the Fuel Inbalance EICAS message turn on? When does it turn off? | 800# difference it turns ON ; it turns off at 100# difference |
| What is the Maximum cabin differential pressure? | 8.4 psi |
| What is the Maximum cabin differential Overpressure? | 8.8 psi |
| What is the Maximum cabin differential negative pressure? | -0.5 psi |
| What is the Maximum cabin differential pressure for takeoff and landing? | 0.2 psi |
| What is the RVSM altudes? | from FL 290 up to and including FL410 |
| What is the maximum ITT for engine start? | 815C |
| What is the minimum temperature to start the APU? | -54 degrees Celsius |
| Minimum Speed with RAT Deployed | 130 KIAS |
| Max Speed Below 8000 feet | 300KIAS |
| What is the coldest temperature we can operate in at altitude? | -65C |
| When is a hydraulic systems warm up required? | When the reservoir temps are below -18C Accomplish a hydraulic warmup proceedure. |
| What is the max AFT cargo compartment load on an E170 | 2271# |
| What is the max FWD cargo compartment load on an E175 | 3307# |
| What is the max AFT cargo compartment load on an E175 | 2535# |
| What is the max runway slope? | +/- 2.0% |
| What is the maximum ambient air for takeoff and landing? | 52C |
| What is the Maximum Flight Operation Latitude? | 78N to 78S |
| Thrust reversers are for ground use only? T/F | True |
| Can we perform a go around after the thrust reversers have been deployed? | Nope |
| Are power back operations authorized? | unfortunately no. although it would be really cool |
| When must the thrust reversers be stowed? | 60 KIAS |
| After selecting reverse thrust, do not move the thrust levers into the forward thrust range until thee REV icon on the EICAS is shown in amber or green. T/F | Truth |
| TAS, TAT and SAT are valid above what airspeed? | 60 KIAS |
| The standby magnetic compass is not valid when? | When transmitting on VHF 1 |
| LOC back course approaches are not authorized when using what? | The IESS |
| The maximum allowable altitude difference between PFD 1 and PFD 2 is what? | 200 feet |
| What is the maximum allowable difference between altimeters on the ground? | 75 feet |
| What is the minimum engagement height of the autopilot? | 400 feet |
| What is the minimum use height of the autopilot? | 50 feet |
| What flap setting is required for CAT 2 approach? | Flaps 5 |
| What is the engine starter duty cycle limitations for start attempts 1 and 2 on the ground? | 90 seconds followed by a 10 second cool down |
| What is the engine starter duty cycle limitation for start attempts 1 and 2 while airborne? | 120 seconds followed by a 10 second cool down |
| What is the engine starter duty cycle limitation for start attempts 3 through 5 on the ground? | 90 seconds on followed by a 5 minute cool down |
| What is the engine starter duty cycle limitation for start attempts 3 through 5 while airborne? | 120 seconds followed by a 5 minute cool down |
| What are the dry motoring duty cycle limits for start attempt 1? | 90 seconds followed by 5 minutes off |
| What are the dry motoring duty cycle limits for start attempts 2 through 5? | 30 seconds on followed by 5 minutes off |
| After 5 sequential dry motor starts, the cycle may be repeated after how long? | A 15 minute cool down period. |
| What are the APU Starter Duty cycle limits? | 1st and 2nd start attempts of 60 seconds followed by 60 second cool down period. 3rd start attempt of 60 seconds followed by a 5 minute cool down period. |
| What is the definition of visible moisture? | Visible moisture is defined as clouds, fog with visibility of one mile or less, mist, rain, snow, sleet and ice crystals |
| What is the definition of contaminated surfaces? | Contaminated surfaces are defined as ramps, taxiways or runways where the surface is cov-ered by snow, ice, standing water, or slush may be ingested by the engines; or freeze on engines, nacelles, or engine sensor probes. |
Created by:
lglippig