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123 Cards in this Set
- Front
- Back
What is the maximum allowable weight of the CR7/CR9 at the gate? Takeoff and Ramp |
CR7: 75,250 lbs. CR9: 85,000 lbs. |
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What is the maximum allowable takeoff weight of the CR7/CR9? |
CR7: 75,000 lbs. CR9: 84,500 lbs. |
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What is the maximum zero fuel weight of the CR7/CR9? |
CR7: 62,300 lbs. CR9: 70,750 lbs. |
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What is the maximum weight for landing for the CR7/CR9? |
CR7: 67,000 lbs. CR9: 75,100 lbs. |
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What is the maximum temperature for takeoff and landing? |
ISA + 35° C |
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What is the minimum temperature for takeoff and dispatch? |
-40°C. |
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What is the maximum takeoff and landing altitude? |
8,000 feet pressure altitude. |
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What is the maximum Runway slope? |
±2% Uphill ±2% Downhill |
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What is the maximum tailwind allowed for takeoff and landing? |
10 knots |
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Assuming aircraft weight and OAT allow, what is the maximum altitude the aircraft may be operated? |
CR2: FL360 CR7/CR9: FL410 |
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Your flight must be within 60 minutes for the CR7/CR9 of the nearest suitable airport under what conditions? |
If cargo is carried in the cargo compartment. |
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Assuming the BTMS system is operative, what is the minimum brake cooling time between a landing stop or a rejected takeoff and the subsequent takeoff? |
15 minutes. |
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What is the maximum crosswind? |
27 Knots |
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What is the maximum speed to raise the landing gear? |
200 knots. |
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What is the maximum speed with the landing gear extended? |
220 knots. |
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What is the maximum speed for flaps 1°? |
230 knots. |
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What is the maximum speed for flaps 8°? |
230 knots. |
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What is the maximum speed for flaps 20°? |
220 knots |
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What is the maximum speed for flaps 30? |
185 knots |
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What is the maximum speed for flaps 45°? |
170 knots |
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What is the maximum allowable tire speed for the CR7/CR9? |
182 knots ground speed |
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What is the maximum airspeed for turbulent air penetration? |
280 knots or mach .75 whichever is lower |
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What is the minimum altitude the autopilot may turned on after takeoff or go around? |
600 feet AGL. |
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What is the minimum altitude the autopilot may be used while flying a visual approach? |
400 feet AGL. |
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What is the minimum altitude the autopilot maybe used while flying a non-precision approach? |
400 feet AGL or 50 feet below the MDA (whichever is higher). |
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By what altitude must the aircraft be configured for landing and on a stable approach prior to commencing a Category II approach? |
By 1000 feet AGL |
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In order to takeoff with more than 500 lbs. of fuel in the center tank, how much fuel needs to be in the wing tanks? |
More than 4,400 lbs. in each wing tank. |
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What is the maximum permissible fuel imbalance between the contents of the main left tank and the main right tank? |
300 lbs - During takeoff. 800 lbs - All other phases of flight. |
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What is the minimum fuel quantity in each wing for a go around? |
600 lbs. |
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What is the maximum engine ITT allowed during all ground starts |
120°C. |
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How long must the engines stabilize at idle prior to shutdown? |
2 minutes. |
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Does taxi time count towards the stabilization time and if so under what conditions? |
Yes, taxi time at a stabilized 80% N2 or below may be counted towards the two-minute cool down period. |
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For how long must the engine starter cool after the third start attempt? |
5 minutes. |
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How long may the starter remain on during a start attempt CR2/CR7/CR9? |
CR2- 60 seconds CR7/CR9 - 90 seconds. |
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During Landing, Max Reverse Thrust is prohibited below what speed? |
75 knots. |
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Reverse idle must be achieved by what speed? |
60 knots. |
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Under what conditions do icing conditions exist on ground and for takeoff? |
OAT 10°C or lower with visible moisture present in any form with visibility 1 mile or less. |
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When must cowl anti-ice only be used? |
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When must Wing ice be used as well at Cowl Ice |
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What is the maximum 90 degree crosswind for takeoff and landing? |
27 knots |
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What is the maximum 90 degree crosswind for landing from a Category II Approach? |
15 knots |
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Maximum headwind for a landing from a Category II approach? |
16 knots |
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Maximum direct tailwind for takeoff and landing? |
10 knots |
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What is the minimum operating weight empty of the CR7/CR9? |
CR7: 42,000 lbs. CR9: 45,000 lbs. |
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Minimum flight crew? |
One Captain One First Officer |
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Maximum gear extended speed |
220 knots |
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Maximum airspeed for windshield wiper operation |
220 knots |
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Maximum airspeed for windshield wiper operation failed in the non-parked position |
CR2: 220 knots CR7/CR9: 250 knots |
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In the CR7/CR9 Vfe and Vfo are? |
Equal |
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Ground Contamination Definition |
Runways, ramps, or taxiways with surface snow, ice, slush or standing water. |
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Visible Moisture Definition |
Visible moisture or precipitation in any form (such as clouds, fog with visibility of one mile or less, mist, rain, snow, sleet or ice crystals) is present inflight, or below 400' AGL for takeoff. |
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Continuous engine ignition must be used during the following: (5 items) |
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EICAS Indicating Red mean? |
Maximum and minimum limitations |
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EICAS Indicating Yellow mean? |
Caution Range |
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EICAS Indicating Green mean? |
Normal Operating Range |
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ENGINE OPERATING LIMITS DUE TO WIND DIRECTION Within 30° on either direction of the airplane nose-no windspeed limit -OR- >30° in either direction of the airplane nose- <5 knots windspeed |
No limitations - TOGA thrust may be applied before brakes released. |
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ENGINE OPERATING LIMITS DUE TO WIND DIRECTION >30° in either direction of the airplane nose and between 5 and 30 knots windspeed |
Apply maximum of 75% N1 before brake release, then TOGA thrust. |
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ENGINE OPERATING LIMITS DUE TO WIND DIRECTION >30° in either direction of the airplane nose >30 knots windspeed |
Apply maximum of idle/taxi thrust before brake release, then TOGA thrust |
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ENGINE STARTER CRANKING LIMITS CR7/CR9 - Ground only |
Start 1 - 90 seconds on 10 seconds off Start 2 - 90 seconds on 10 seconds off Start 3 and subsequent - 90 seconds on 5 minutes off. |
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ENGINE STARTER CRANKING LIMITS CR7/CR9 - Flight only |
Start 1 - 2 minutes on 10 seconds off Start 2 and subsequent - 1 minute on 5 minutes off. |
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Associated Conditions. At initiation of thrust lever movement from SHUT OFF to IDLE: |
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Dry-Motoring Cycle. |
A dry-motoring cycle (with thrust levers at SHUT OFF) may be used for engine ground starts and engine air starts. Start 1 - 90 Seconds on 5 minutes off Start 2 and subsequent - 30 seconds on 5 minutes off. |
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Oil Pressure Steady-State Idle |
25 psi minimum |
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Oil Pressure Takeoff Power |
45 psi minimum |
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Oil Pressure Maximum Continuous |
95 psi maximum |
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Oil Pressure Maximum Transient |
156 psi when oil temp is <60°C |
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Oil Pressure Maximum transient after cold start(10 minutes maximum) |
182 psi or amber dashes |
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After cold start engine must? |
Remain at idle until oil pressure returns to normal range. |
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Fuel Quantity Pressure Refueling |
Left Tank - 7,492 lbs. Right Tank - 7,492 lbs. Center Tank - 4,610 lbs. Total - 19,594 lbs. |
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Fuel Crossflow Powered crossflow and gravity crossflow must be OFF for what phase of flight? |
Takeoff |
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APU Starter Limits The APU starter motor duty cycle is limited to not more than _______ (1) attempts in one _______(2) with a _______(3) delay between cranking attempts. |
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APU Bleed Air Air Conditioning Bleed air extraction from the APU is not permitted above what altitude? CR2/CR7/CR9 |
CR2 - 15,000ft. CR7/CR9 - 25,000ft. |
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APU Bleed Air Engine start during ground operations |
Each engine may be started using the APU as a bleed air source. |
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APU Door Open Limitation. With the APU door not closed or the door position is unknown. The airplane must be limited to? |
220 knots, or the APU must remain in operation |
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Taxi Light The taxi lights must be switched OFF whenever the airplane is stationary in excess of |
10 Minutes |
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Flight Spoilers. Minimum altitude for flight spoilers deployment: |
1000 ft. AGL |
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Flight spoilers To ensure adequate maneuver margins, flight spoilers must not be extended inflight at airspeeds below the |
Vr + 17 knots |
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Thrust Reversers During landing, maximum reverse thrust is not permitted at airspeeds below? |
75 knots, and reverse idle should be achieved by 60 knots. |
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Wheel Brake Cooling Limitations. Minimum brake cooling time is_____(1)? and All BTMS indicators must be _____(2)?and are not______(3)? |
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Automatic Flight Control System Use of SPEED MODE (DES or IAS), flight director or autopilot coupled, during approach is?
Permitted or Not Permitted |
Not Permitted. |
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Automatic Flight Control System CR9 Use of VNAV, flight director or autopilot coupled, during the climb and approach phases of flight is? Permitted or Not Permitted |
Not Permitted. |
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Automatic Flight Control System Operation with the autopilot engaged is prohibited at altitudes below 600 ft. AGL, except when performing thefollowing: 3 Things |
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Automatic Flight Control System Category II Approach must be flown with the autopilot. Engaged or Not Engaged |
Engaged. |
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RVSM Airspace. Maximum cruise speed in RVSM airspace is? |
0.82M. |
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RVSM Airspace. In flight, prior to entering RVSM airspace all required equipment for operation in RVSM airspace must be. |
Operational. |
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The ADC source coupled to the active FCC must be the same as that coupled to the ATC transponder during flight in? |
RVSM airspace. |
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RVSM Airspace. RVSM Required Equipment List Autopilot with Altitude Hold |
Must Be Operational |
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RVSM Airspace. RVSM Required Equipment List Altitude Alerting System |
Must Be Operational |
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RVSM Airspace. RVSM Required Equipment List Altitude Reporting Transponder (2) |
One Must Be Operational |
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RVSM Airspace. RVSM Required Equipment List Air Data Computers (2) |
Two Must Be Operational |
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Permissible DC Electrical System Loads. Ground Operations To protect the flight compartment CRT displays, the maximum permissible time for ground operations with DCpower only is? |
5 Minutes. |
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Slats/Flaps. Enroute use of slats/flaps is? Prohibited or Not Prohibited |
Prohibited. |
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Slats/Flaps. Maximum slats and/or flaps extended altitude: |
15,000 ft. |
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Taxi time at a stabilized _____% N____ or below may be credited towards the two-minute cool down period. |
80% N2 |
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During all starts, do not exceed _____%(1) N____ (2) for ____ (3) minutes after start, or until all operating indications are in the _____ (4) range, whichever is longer. |
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What is the maximum engine ITT allowed during all air starts. |
90°C. |
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Immediate Action Items Braking Loss/Asymmetry |
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Immediate Action Items CABIN ALT Msg or EMERGENCY DESCENT PROCEDURE |
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Immediate Action Items DOUBLE-ENGINE FAILURE |
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Immediate Action Items SMOKE/FUMES |
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Immediate Action Items CR7/CR9 STAB TRIM RUNAWAY |
1. Control wheel - Assume manual control and override runaway 2. STAB TRIM DISC - Push, hold and release |
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EMERGENCIES WITH IMMEDIATE ACTION ITEMS THAT ARE NOT MEMORY ITEMS 6 EMERGENCIES |
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Maneuvering Limit Load Factors Flaps Retracted/Extended |
Flaps Retracted -1.0 to +2.5G Flaps Extended 0.0 to + 2.0G |
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When does the Auto Fuel X-Flow turn on? |
200lbs low and shuts off when wing is 50lbs above. |
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When do the Transfer Injectors come on? |
94% and they shut off at 97% |
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What is the minimum fuel temp for takeoff? |
5C |
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What has to be confirmed in the plane? |
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What altitude and airspeed do you get the "Too Low Gear" warning on the EGPWS? |
500ft on the radio altimeter and less than 190kts. |
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Which Hydraulic System operates the manual gear release? |
Hydraulic System 2. |
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If we lose Hydraulic System 2, will we have the NLG? |
No |
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What are the maximum steering degrees for the Nose Wheel |
80 degrees with the tiller and 8 degrees with the rudder peddles. |
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What are the hydraulic systems of the 700? |
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Which Pumps are EDP and Which are ACMP |
EDP (Engine Driven Pump) 1a, 2a ACMP (AC Motor Pump) 3a, 3b, 1b, 2b. |
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When Does the Hydraulic Pressure Relief Valve open and close |
Opens at 3600psi and closes at 3200psi. |
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What is Normal operating range for Hydraulic Pressure |
3000psi +/- 200psi |
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What is Normal operating range for the Hydraulic reservoirs? |
45% - 85% If lower than 45% refer to the chart in the POH. |
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How do we close the Hydraulic SOV (L/R) |
or 2. Hydraulic SOV Shutoff Switch |
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What conditions must be met before the Auto Pilot can be engaged? (5 Items) |
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What conditions will cause Auto Pilot to be manually disconnected? (7 Items) |
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What conditions will cause Auto Pilot to be automatically disconnected? |
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Do not hold in icing conditions with _____________ extended? |
Slats or Flaps |
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Immediate Action Items CR2 STAB TRIM RUNAWAY |
1. Control wheel - Assume manual control and override runaway 2. Both STAB TRIM DISC - Push, hold and release 3. Captain Assumes PF Duties 4. STAB Trim CH1 cb (2F5) - Open 5. STAB Trim CH2 cb (4A1) - Open |
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Single Pack Operation is limited to? |
CR2 - 25,000ft CR7/CR9 - 31,000ft |