Pinnacle Cfm Ch3- Limitations

Front 1

Main Cabin Door

Back 1

4 passengers or 1,000 lbs

Front 2

Cargo

Back 2

-Fly within 45min of suitable airport if carried
-Max weight is 3,500lbs

Front 3

Altitude and temperature limitations
-Max pressure altitude for T/L?
-Max operating altitude?
-Max alt on one pack?
-Max temp for T/L?
-Min temp for takeoff?

Back 3

-10,000
-41,000 / 37,000 company
-25,000
-ISA +35C
- -40C

Front 4

Initial pitch target for rotation?

Back 4

10 degrees

Front 5

Structural Weight Limitations?
-Max taxi & ramp?
-Max T/O (MTOW)?
-Max landing weight (MLW)?
-Max zero fuel weight (MZFW)?
-Min flight weight?

Back 5

-53,250lbs
-53,000
-47,000
-44,000
-30,000

Hint 5

CFM 3-14 Double Box

Front 6

What are the Max runway slopes?

Back 6

+/- 2 %

Front 7

Wind Conditions:
-Max tailwind for T/L?
-Max X-wind for T/L on dry/wet runway?
-Max X-wind for T/L on contaminated runway?

Back 7

-10
-27
-15

Front 8

Operating in Icing Conditions (double boxed):
Visible moisture Definition?

Back 8

Visible moisture includes clouds, fog with visibility of one mile (grounds ops) or less, rain, snow, sleet or ice crystals.

Front 9

Engine Cowl Anti-Ice, Ground Operations: (double box)

Back 9

The COWL ANTI-ICE must be on when:
-The OAT is 10C or below and visible moisture in any form is present.
-The OAT is 10C or below when operating on runways, ramps, or taxiways where surface snow, ice, standing water, or slush is present.

Front 10

Wing Anti-Ice, Ground Operations: (double box)

Back 10

The WING ANTI-ICE system must be on for takeoff when icing conditions exist on the ground, the OAT is 5C or below and:
-Visible moisture in any form is present below 400AGL
-The runway is wet or contaminated
-In the presence of any precipitation
NOTE: If the wing anti-ice system is selected ON for takeoff, the cowl anti-ice system must also be selected ON.

(Continued with photo on flashcard titled "Wing/Engine Anti-Ice Ground Operations Limitations? (Con't)"

Hint 10

Clarification: For example if it is 5C out with no icing conditions, the wing anti-ice must only be on until sufficiently warm, then may be shut off prior to takeoff.

Front 11

Wing/Engine Anti-Ice Ground Operations Limitations? (Con't)

Back 11

Front 12

Engine Cowl Anti-Ice, Flight Operations: (double box)

Back 12

The COWL ANTI-ICE system must be on when:
-In icing conditions
-ICE is annunciated by the ice detection system

Front 13

Wing Anti-Ice, Flight Operations: (double box)

Back 13

The WING ANTI-ICE system must be on when:
-Ice is annunciated by the ice detection system
-In icing conditions and below 230 knots.

Front 14

Airspeed Limitations:(double box)
Vfe 8-company
Vfe 20-company
Vfe 30-company
Vfe 45-company
Vfo 8-
Vfo 20-
Vfo 30-
Vfo 45-

Back 14

-215kts
-215kts
-185kts
-170kts
-200kts
-200kts
-185kts
-170kts

Front 15

List of Immediate Action Items:

Back 15

-Aileron system jammed
-APU FIRE message
-Asymetric Braking/Loss of Braking
-BRAKE OVHT Message
-Cabin ALT message or Emergency Descent Procedure
-Configuration Warning
-Ditching or Forced Landing imminent
-Double Engine Failure
-Elevator System Jammed
-ENGINE OVERSPD message
-L(R) ENGINE FIRE Message or Severe Engine Damage (on ground)
-L(R) ENGINE FIRE message or Severe Engine Damage (in flight)
-L(R) JETPIPE OVHT message
-L(R) REV UNLOCKED Message
-Loss of all AC Power
-MLG BAY OVHT Message
-Passenger Evacuation
-Post-Shutdown Engine Tail Pipe Fire
-Rejected Takeoff
-Rudder System Jammed
-STAB TRIM Runaway
-Stall Recovery

Front 16

Max Landing gear Operating speeds:
VLE?
VLO up?
VLO down?

Back 16

-250kias
-200kias
-250kias

Front 17

Miscellaneous Speeds:
Max windshield wiper speed?
Max tire ground speed?
Max turbulent air penetration speed?
STAB or MACH TRIM INOP max speed?

Back 17

-220
-182
-280kias or .75mach (lowest)
-250kias or .70mach (unless auto pilot)
-NOTE: when below Vref + 10knots, angle of bank 15 degrees.

Front 18

Minimum Operating Limit Speed:(double boxed)

Back 18

Intentional speed reduction below the onset of stall warning, as defined by stick shaker operation, is prohibited, unless a lower speed is specifically authorized for flight test or training operation.

Front 19

Minimum Climb Speed (Company)(double box)

Back 19

Above 10000: climb at 250KIAS/.70Mach unless:
1.When mtn terrain in dept path, climb at Vx or Vref +10knots until clear or MEA.
2. Vy when requested except in icing cond above 15,000 feet.
3. If restricted by MEL, maintain highest speed allowed by the MEL, but not slower than Vx.

When unable to maintain 300FPM @ 250KIAS/.70Mach, stop climb and coordinate new altitude with ATC.

Front 20

Minimum Enroute Cruise Speed (Company):

Back 20

Above FL310 is Long Range Cruise LRC.
Below FL 310 is Two Engine Holding Vmd in calm air. Reference buffet margin chart during turb air.

Front 21

Engine Indications? (double box)

Back 21

Red-Max and Min Limitations
Amber- Caution Range
Green- Normal Operating Range

Front 22

What are the EICAS Engine Indications?

Back 22

Front 23

What are the Engine Operating Limits?

Back 23

Front 24

Airplane Cold-Soaked? (double box)

Back 24

Before first flight of the day -30C or below for more than 8 hours:
-motor engines for 60 seconds, fan rotation verified before start is initiated
-Reverse thrusters must be actuated until the deploy and stow cycles are less than 5 seconds.

Front 25

When must Continuous Ignition be used? (DB)

Back 25

-Takeoff and landings on contaminated runways
-Takeoffs with X-wind > 10knots
-Flight through moderate or heavier intensity rain
-Flight through moderate or heavier intensity turbulence
-Flight in the vicinity of thunderstorms
Engine op at or near the shaker and pusher settings is predicated on an operable auto-ignition system

Front 26

Describe Engine Stabilization? (DB)

Back 26

-Engines must be running for at least two minutes prior to takeoff
-prior to shutdown, IDLE for 2 minutes to dissipate heat and stabilize internal op temps.
-If ITT >350C and is increasing rapidly following shutdown, carry out an engine motoring cycle to cool ITT.
NOTE: Taxi time at 80% N2 or below may be considered in the 2 minute cool down period.

Front 27

When must the starter not be used (Ground and Air)? (DB)

Back 27

Not able to use if N2 exceeds 55%

Front 28

Associated Start Condition? (DB)

Back 28

Thrust Lever movement from SHUT OFF to IDLE:
-ITT < 120C or less for all ground starts
-ITT <90C or less for all air starts

Front 29

Dry motoring Cycle? (DB)

Back 29

The dry motoring cycle (with Thrust Levers @ SHUT OFF) may be used for engine ground starts and engine air starts.

#1, 90 seconds, 5 min off
#2+, 30 seconds, 5 min off

Front 30

Reduced Thrust Takeoff:
When can reduced thrust not be used? (DB)

Back 30

-Normal fan speed <85% N1
-Engine cannot achieve full rated thrust
-Wing/cowl anti-icing bleeds in use
-Contaminated runways with water, slush, snow or ice
-Windshear and downdrafts warnings
-Special Departure Procedure specifies full thrust for takeoff
-Anti-skid inop
NOTE: procedure may be used on wet runways provided that wet runway airport analysis data is used.
If reduced thrust can be used, fan speed cannot be < 85% N1

Front 31

Fuel System Limitations: (double box)

Back 31

Max fuel imbalance between L & R is 800 pounds.

Wing tanks must be above 4400 pounds to have greater than 500 pounds in center tank

The minimum fuel for a go around is 450# per wing when level. This assumes 10 degree nose up

Front 32

Fuel Temperature Limitations:

Back 32

Take off with engine fuel temperature indications below 5C is prohibited.

When using JET A, bulk temp must be > -30C. IF non-std fuel is used refer to table 3-19.

Front 33

What are the fuel cross flow procedures for Takeoff?

Back 33

Powered and gravity crossflow must be off for takeoff.

Front 34

Hydraulic System Limitations?

Back 34

The 3B pump must be ON for all phases of flight unless directed otherwise by an abnormal or emergency procedure.

Front 35

Oil System Limitations?

Back 35

Types- 1, 2, Castrol 4000
Max oil consumption: 6.4 ounces/hour or 189 cubic inches
Oil Level Checks: max w/o servicing is 16 hours, after 16 hours must be checked from ENGINE OIL LEVEL panel w/in 3min to 2 hours after every shutdown.

Front 36

Oil Replenishment System?

Back 36

-must be used from 15min to 2 hours after shutdown
-If more than 2 quarts used, must dry motor the engine
-procedure done my Mx personnel

Front 37

APU indications? (double box)

Back 37

Red- Max and Min limitations
Amber- Caution Range
Green- Normal Operating Range

Front 38

What are the APU starting limitations? (DB)

Back 38

Min ambient temp for starting a cold soaked APU on the ground is -40C.

Front 39

Limitations on starting the APU on Battery? (DB)

Back 39

first, 30s on, 2min off
second, 30s on, 20min off
third, 30s on, 2min off
fourth, 30s on, 40min off

Front 40

Limitations on starting the APU on DC Ground Power?

Back 40

first, 15s on, 2min off
second, 15s on, 20min off
third, 15s on, 2min off
fourth, 15s on, 40min off

Front 41

What is the APU Door Open Limitation? (DB)

Back 41

With the APU door open (APU message area in EICAS indicates DOOR_ _ _ _), comply with one of the following:
-speed < 300KIAS
-APU must remain in operation

Front 42

What are the Bleed-Air System Limitation?

Back 42

10th stage valves must be closed for takeoff and landing if the engine cowl and/or wing anti-ice systems have been selected ON.

Front 43

What are the Air Cond and Pressurization Max Differential Pressures?

Back 43

+8.7psi, -0.5psi, Taxi & Takeoff & Landing is 0.1psi

Must depressurize before opening any doors

N/A EMER DEPRESS switch above 15,000 feet

NOTE: When low-pressure air ground connection is used, cabin doors must be open.

Front 44

What is the Electrical System Limitations for Loads on the DC System?

Back 44

The max permissible continuous on each TRU is 100 amps.

Front 45

What is the max amount of time of DC ground power use to avoid damage to the CRT displays? (DB)

Back 45

5 minutes.

Front 46

What are the Wheel Brake Cooling Limitations? (DB)

Back 46

Brake cooling times must be observed after a landing or RTO and a subsequent takeoff, to ensure its ability to stop the aircraft if needed on the next takeoff.

Front 47

What are the Flap Control Limitations?

Back 47

-Takeoff flaps must be selected from the 0 detent
-N/A touch and go training with 14knots+ X-wind.
-Enroute use of flaps N/A, unless guidance from MOC during ferries. (DB)
-Ops above 15000 with flaps extended N>A. (DB)

Front 48

What is the Flap Extended Diversion AD? (DB)
AD 2009-06-12

Back 48

Upon arrival at dest, flaps will stay at 0 unless using precision approach and RVR is at or above mins and will remain there from the main body of the TAF until after landing. When using a non-precision approach ceiling AND visibility are controlling.

Hint 48

CFM 3-45

Front 49

What are the conditions with a Flap Failure and when a Takeoff Alternate is filed?

Back 49

-Min flight alt cannot exceed 15000 AND Fuel on board, at dept, shall be sufficient to divert to takeoff alternate or other suitable airport, with flaps extended to takeoff position, conduct approach, and land with 1000# fuel remaining.

Front 50

What are the Limitations on the Flight Spoilers? (DB)

Back 50

-N/A below 1000 feet
-N/A below recommended approach/maneuvering (Vref) speeds plus 17KIAS (NOTE: When maneuvering up to 40 bank, add 10KIAS to the recommended approach/maneuvering speeds. i.e. flaps 20 Vref is 150KIAS + 17 + 10 = 177KIAS)
-N/A with flaps more than 30degrees

Front 51

What are the Aileron Limitations? (DB)

Back 51

-Departed from contaminated runway, at 10,000 feet, or when SAT falls below 0C (which ever is later) manually operate ailerons every 5,000 feet until top of climb.

Front 52

What are the Stall Protection Limitations?

Back 52

-Test before First Flight of Day
-Both switches must remain ON for all phases of flight.
-Engine op at or near shaker/pusher predicated on operable auto-ignition system.

Front 53

Thrust Reverser Limitations are what? (DB)

Back 53

-Ground use only
-Full stop landings only
-N/A Takeoff with any of the following illuminated: THRUST REV UNLK, REV icon N1 gauge, L or R REV UNLOCKED caution message.
-Below 60KIAS at idle

Front 54

What are the Taxi/Recognition Lights Limitations? (DB)

Back 54

-Taxi lights must be switched OFF whenever the aircraft is stationary in excess of 10 minutes.

Front 55

What are the Automatic Flight Control Limitations? (DB)

Back 55

-Use of DES sub-mode (FD or autopilot coupled) is not permitted.
-N/A flight director per AD 2008-21-09 (dont use on takeoff)
-Operation of autopilot below 600 AGL N/A except: visual and non-precision approaches, min use is 400 AGL, For ILS min use is 80 AGL, ADC source coupled to autopilot must be the same as that coupled to the ATC transponder during RVSM ops.
Clarification: In DES submode, plane will pitch to maintain airspeed, it does not care about your altitude.

Front 56

Enhanced Ground Proximity Warning System Limitations? (EGPWS)

Back 56

-Pilots may deviate from ATC instruction to comply with EGPWS alert.
-May malfunction if there is no GPS input, temp below ISA, non-std temp lapse rates, wrong alt setting.
-The terrain database, terrain displays and alerting system do not account for man-made obstacles except for all known man-made obstacle in Canada, USA & Mexico.

Front 57

Flight Management System (FMS) Limitations?

Back 57

-N/A FMS use with ILS, LOC, LOC-BC, LDA, SDF and MLS, FMS does not provide transition to ILS.
-Approved for use in enroute, terminal, and non-precision approach phases of flight
-FMS thrust, range, fuel mgmt, and altitude/speed capability is advisory info only.

Front 58

What are the requirements for RVSM?

Back 58

Autopilot, Altitude Alerting System, (1) Altitude Reporting Transponder (1 of 2), Both Air Data Computers.

Front 59

What are the contaminated runway maximum depths?

Back 59

Standing water: Takeoff-.50", Landing-.75"

Slush: Takeoff .50", Landing .88"

Wet Snow: Takeoff 1.00", Landing 1.50"

Dry Snow: Takeoff 3.00", Landing 3.75"

Front 60

What is the Minimum Oil Temperature for starting?

Back 60

-40C

Front 61

What is the Maximum Oil Temperature continuously?

Back 61

+155C

Front 62

What is the Maximum permissible Oil Temperature?

Back 62

+163C

Front 63

What is the Minimum Steady State Idle Oil Pressure?

Back 63

25 PSI Minimum

Front 64

What is the Minimum Takeoff Power Oil Pressure?

Back 64

45 PSI Minimum

Front 65

What is the Maximum Continuous Oil Pressure?

Back 65

115 PSI Maximum

Front 66

What is the Transient after Cold Start Oil Pressure?

Back 66

156 PSI
(130 PSI AT IDLE, 10 MINUTES MAXIMUM)

Front 67

What are the Subsequent Engine Starter Limitations?

Back 67

(1) - 1min ON - 10sec OFF
(2) - 1min ON - 10sec OFF
(3) - 1min ON - 5min OFF

Front 68

Engine Cowl Anti-Ice Operation on the ground/air?

Back 68

GROUND: OAT <10C + visible moisture is present in any form, OAT <10C when operating on runways, taxiways, ramps where surface snow, ice, standing water, or slush is present.

AIR: Must be ON when in icing conditions, ICE is annunciated by the ice detection system.

Front 69

Wing Anti-Ice Operation on the ground/air?

Back 69

GROUND: OAT <5C + with icing conditions on the ground + Visible moisture is below 400AGL + the runway is wet or contaminated + in the presence of any precipitation

AIR: Ice is annunciated by the ice detection system + In icing conditions and the airspeed is < 230 KIAS.

NOTE: If the wing anti-ice system is selected ON for takeoff, the cowl anti-ice must also be selected ON.

Front 70

The FMS calculated thrust setting must not be used if the pressure altitude is greater than _ feet.

Back 70

36,000
CFM 3-52
(Limitations written)

Front 71

The cabin pressurization system must not be operated to _ feet when is system is in manual mode.

Back 71

-1,500
CFM 3-43
(Limitations Written)

Front 72

What is the core N2% at idle?

Back 72

56.5 to 68%
CFM 3-30
(Limitations written)

Front 73

If above _ feet, one air-conditioning unit or cowl anti-ice must be on for each engine.

Back 73

40,000
CFM 3-30
(Limitations written)

Front 74

T/F
During pre-flight check of the thrust reversers with the airplane stationary, reverse thrust must be limited to 40% N1.

Back 74

FALSE (30% N1)
CFM 3-48
(Limitations written)

Front 75

The APR (Automatic Power Reserve) system must be selected _ if an APR INOP caution message is displayed.

Back 75

OFF
CFM 3-32
(Limitations written)

Front 76

The TCAS resolution advisory programs are based on the pilot initiating the RA maneuver within _ seconds.

Back 76

5
(Limitations written)

Front 77

What are the APU Bleed Air Limitations for:
A/C in Flight?
Eng Start During Ground Ops?
Eng Start During Flight?

Back 77

Front 78

What is the procedure if only the Cowl Anti-Ice is needed either on the ground or in the air?

Back 78

Select wing anti-ice on, then cowl anti-ice on, then wing anti-ice off to prevent over pressurization of the cowl anti-ice.