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175 LIMITATIONS > 175 LIMITATIONS > Flashcards

175 LIMITATIONS Flashcards

1
Q

MAX RAMP WEIGHT?

A 
ERJ 175 (76) 85870
ERJ 175 (70) 85450
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2
Q

MAX TAKE OFF WEIGHT?

A 
ERJ 175 (76) 85517
ERJ 175 (70) 85098
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3
Q

MAX LANDING WEIGHT?

A 
ERJ 175 (76) 74957
ERJ 175 (70) 74957
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4
Q

MAX ZERO FUEL WIGHTS?

A 
ERJ 175 (76) 69886
ERJ 175 (70) 69467
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5
Q

FUEL LOAD FOR A LONG FLIGHT WITH STRONG HEAD WIND DECIDE ADD MORE FUEL. WAHT IS MAX FUEL WEIGHT?

A

20935

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6
Q

WING SPAN

A

93’ 11”

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7
Q

LENGTH

A

103’ 11”

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8
Q

DURING TAXIN IN DEN, WE ARE INSTRUCTED TO TAXI UNDER THE PAX BRIDGE. THE SIGN SAYS IT HAS 43 FEET OF CLEARANCE, CAN WE TAXI UNDER SAFELY?

A

YES

175 TAIL IS 32’ 4”

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9
Q

A TAXIWAY IS NOTAMD CLOSED TO AIRCRAFT WITH WINGSPAN OVER 100” CAN WE USE THIS TAXIWAY WITH THE ERJ 175

A

YES SINCE ERJ 175 WING SPAN

93’ 11”

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10
Q

MIN RUNWAY WITH

MAXIMUM RUNWAY SLOPE?

MAXIMUM TAILWIND SPEED FOR T/O AND LDG

A

100”

+/- 2%

15 KTS

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11
Q

MAX OPERATIONAL ALT

MAX T/O ALT

MAX LANDING ALT

A

41,000 FT

10000 FT

10000 ft

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12
Q

MAX TEMP FOR T/O

MAX TEMP LDG

A

ISA + 35C (52C)

ISA + 35C (52C)

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13
Q

MIN TEMP T/O

MIN TEMP LDG

A
  • 40C

- 40C

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14
Q

WHAT IS REQUIRED IF A LANDING OCCURS BELOW -40C?

A

THE AIRPLANE MAY NOT TAKEOFF WITHOUT FURTHER MX INSPECTION

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15
Q

MAX SINGLE PACK OPERATIONAL ALT?

A

31,000

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16
Q

ATC ASKS IF YOU CAN TAKE 42000 FOR TRAFFIC. CAN YOU?

A

NO, MAX ALT 41000.

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17
Q

MAX OPERATING SPEED LIMITS KIAS?
SL - 8000 FT.
10,000 MACH TRANSITION

A

VMO = 300 KIAS

VMO = 320 KIAS

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18
Q

MAX OPERATING SPEED LIMIT IN MACH

A

MMO = 0.82

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19
Q

HOW DO MAX OPERATING SPEED LIMITS CHANGE WITH ALT?

A

SL - 8000 STAYS CONS AT 300 KIAS
8000 - 10000 INCREASES TO 320 KIAS
10000 - 290000 STAYS 320 KIAS
29,000 - 41,000 DECREASES FROM 320 DOWN TO 243 KIAS / MMO .82M

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20
Q

VA

A

240 KIAS

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21
Q

MANEUVERING FLIGHT LOAD FACTOR LIMITS?
POSITIVE FLAPS UP FLAPS DOWN
NEGATIVE FLAPS UP FLAPS DOWN

A

POSITIVE FLAPS UP = 2.5 G FLAPS DOWN = 2.0 G

NEGATIVE FLAPS UP = 1.0 G FLAPS DOWN = 0 G

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22
Q

WHAT ARE THE MAX GUST INTENSITY / TURB PENETRATION SPEED?

A

LESS THAN 10,000 VB = 250 KIAS
EQUAL AND GREATER VB LOWEST OF 270 KIAS OR .
0.76 MACH

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23
Q

IS TURB PENETRATION SPEED A TARGET OR A MAXIMUM SPEED?

A

TARGET SPEED

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24
Q

MAXIMUM RAM AIR TURBINE DEPLOYMENT SPEED?

A

V RAT DEPLOY MAX = VMO/MMO

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25
Q

MAX WIPER OPERATION SPEED?

A

SKYWEST 250 KIAS

MANUFACTURER 253 KIAS

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26
Q

MAX SPEED TO OPEN DV WINDOW?

A

160 KIAS

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27
Q

MAX LANDING GEAR RETRACTION SPEED?

MAX LANDING GEAR EXTENSION SPEED?

A

VLO RETRACTION = 250

VLO EXTENSION = 250

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28
Q

MAX LANDING GEAR OPERATION SPEED?

A

VLE = 250 KIAS

VLE IS THE MAX SPEED AT WHICH THE AIRPLANE CAN BE SAFELY FLOWN WITH THE GEAR EXTENDED AND LOCKED.

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29
Q

MAXIMUM TIRE GROUND SPEED?

A

V TIRE = 195KT. OR 225 MPH

COULD BE AN ISSUE AT HOT AND HIGH ALT AIRPORTS WITH SLAP FAIL SCENARIO.

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30
Q 
FLAP LIMITATION SPEEDS
VFE 1
VFE 2
VFE 3
VFE 4
VFE 5
FULL
A 
VFE 1  230
VFE 2 215
VFE 3 200
VFE 4 180
VFE 5 180
FULL   165
RECOMMENDED TO NOT EXTEND OR FLY WITH THE FLAPS EXTENDED AT SPEED GREATER VFE -10 KTS
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31
Q

MAX TAIL WIND T/O AND LANDING

MAX DEM XWIND FOR DRY RUNWAY

A

15KT

38KT

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32
Q

MAX DEM XWIND FOR DRY RUNWAY

MAX DEM XWIND FOR WET RUNWAY

A

38KT

31KT

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33
Q

MAX DEM CROSS WIND FOR COMP SNOW?

MAX DEM CROS WIND FOR STAND WATER/ SLUSH/ WET SNOW/ DRY SNOW

A

20KT

18KT

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34
Q

MAX DEM XWIND FOR RWY ICE?

  1. T/O
  2. Landing

MAX RECOMMENDED X WIND FOR STATIC T/O

A
  1. 12KT
  2. 8kt

25kt

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35
Q

CAT II LIMITATIONS WINDS

175 CAT II ILS DEMONSTRATED WINDS?
HEADWIND
CROSSWIND
TAILWIND

A

X WIND 12
TAIL WIND 15

HEADWIND 25
CROSS WIND 12
TAILWIND 10

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36
Q

MINIMUM SPOILER SPEED?

A

180KTS

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37
Q

MAX TAXI SPEEDS ON CONTAMINATED SURFACE?
STRAIGHT
TURN

A

STRAIGHT 10

TURN 5

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38
Q 
WHAT INFO CAN THE GREEN DOT PROVIDE? 
1
2
3
4
5
6
A
  1. 1.3G ABOVE SHAKER WITH 40 DEGREES BANK PROTECTION
  2. SINGLE ENGINE DRIFTDOWN SPEED
  3. FLAP EXTENSION SPEED
  4. GREEN DOT MAY BE USED AS AN APPROACH SPEED DURING AN EMERGENCY RETURN TO FIELD
  5. GREEN DOT + 10KNOTS IS USED TO RETRACT THE FLAPS IF “F-BUG” DISAPPEARS.
  6. BEST ENDURANCE (TIME IN FLIGHT: MINIMUM FUEL, EMERGENCY FUEL)
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39
Q

WHEN CAN THE APU BE STARTED DURING THE AIRPLANE POWER UP PHASE?

A

WAIT 30 SEC AFTER THE EiCAS IS ENERGIZED TO START THE APU

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40
Q

AFTER THE EiCAS IS POWERED, HOW LONG MUST WE WAIT BEFORE STARTING THE APU?

A

30 SEC

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41
Q

FOR HOW LONG CAN THE APU BE LEFT OPERATING WITOUT BEING ATTENDED?

A

5 MIN (SKYWEST LIMIT)

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42
Q

WHAT ARE THE APU STARTER DUTY CYCLE OPERATION LIMITS?

A

START ATTEMPT 1: 60 SEC OFF
START ATTEMPT 2: 60 SEC OFF
START ATTEMPT 3: 5 MIN OFF

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43
Q

UP TO WHAT ALTITUDE MAY THE APU BE STARTED?

A

30,000 FT.

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44
Q

APU MIN START AMBIENT TEMPERATURE?

MAXIMUM APU START AMBIENT TEMP?

A

-54 C

ISA + 35

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45
Q

APU MINIMUM OPERATIONAL TEMP?

MAXIMUM OPERATIONAL TEMP?

A

-54 C

ISA +35

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46
Q

APU MAXIMUM OPERATIONAL ALT?

A

33,000FT.

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47
Q

WHAT ALT MAY THE APU GEN BE USED TO?

WHAT ALT APU ENG START ASSIST?

A

33000 FT.

21000 FT.

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48
Q

WHAT ALT APU BLEED AIR BE USED?

A

15,000 FT.

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49
Q

AN IDG FAILS INFLIGHT. THE QRH INSTRUCTS TO START THE APU. WHAT PARAMETERS SHOULD BE VERIFIED BEFORE STARTING THE APU?

A
  1. MAX START ALT 30,000 DESCEND IF ABOVE THAT ALT.
  2. MINIMUM TEMP = -54 C
    MAXIMUM = ISA +35 (CHECK FMS PROG PAGE 3 FOR CURRENT ISA) CHANGE ALT TO BE WITHIN APU TEMP RANG LIMITS
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50
Q

AFTER HAVING DESEND DOWN TO FL3000 TO START THE APU, TO SAVE FUEL, UP TO WHAT ALT CAN WE CLIMB THE ERJ 175 BACKUP TO?

A

FL 330

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51
Q

AUTO PILOT MIN ENGAGEMENT HEIGHT?

AFTER T/O, WHEN CAN THE AUTOPILOT BE ENGAGED?

A

400 FT.

400 FT. AGL

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52
Q

WHAT IS THE AUTOPILOT MINIMUM USE HEIGHT ON NON-PRECISION APPROACHES?

A

MDA

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53
Q

WHAT IS THE AUTOPILOT MINIMUM USE HEIGHT?

A

50FT.

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54
Q

WHAT IS THE BRAKE TEMP REQUIREMENT FOR T/O?

A

BRAKE TEMP INDICATION MUST BE IN THE GREEN RANGE FOR T/O

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55
Q

WHAT IS REQUIRED TO LAND ON A CONTAMINATED RUNWAY?

A
  1. AUTOBRAKES MEDIUM

2. MAX REVERSE

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56
Q

UP TO HOW MANY APPLICATIONS CAN THE EMERGENCY / PARKING ABLE TO PROVIDE?

A

6 FULL BRAKE APPLICATIONS.

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57
Q

MINIMUM BATTERY VOLTAGE REQUIREMENT?

A

22.5 V

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58
Q

MINIMUM VOLTAGE REQUIRED TO POWER UP AIRPLANE?

A

22.5 V

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59
Q

WHEN WOULD YOU NEED TO PERFORM THE SOPM CHARGING PROCEDURE?

A

WHEN BATTERY VOLTAGE FOR EITHER BATTERY IS BETWEEN 21.0 AND 22.4V < 21.0 V = CONTACT MAINTENANCE.

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60
Q

WHAT IS THE MINIMUM RAT START SPEED (QRH)?

A

150 KIAS

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61
Q

WHAT MAXIMUM SPEED CAN THE RAT BE DEPLOYED AT?

A

VMO / MMO

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62
Q

ONCE THE RAT HAS BEEN DEPLOYED, WHAT MINIMUM SPEED MUST BE MAINTAINED FOR IT TO OPERATE?

A

130 KIAS

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63
Q

EXPLAIN THE RAT AUTO DEPLOY OPERATION?

A

WHENEVER AC POWER SOURCE (IDG1/2,APU) ARE NOT POWERING AC BUSES 1 AND 2 INFLIGHT, THE RAT IS AUTOMATICALLY DEPLOYED.

AFTER 8 SECONDS, IT LATCHES AND SUPPLIES POWER TO THE: 1 AC ESS BUS
2. ACMP 3A

ONCE DEPLOYED IT WILL CREATE A VERY LOUD NOISE DUE TO THE HIGH ROTATION SPEED AND CANNOT BE STOWED BACK IN FLIGHT, EVEN IF NORMAL ELECTRICAL POWER IS REESTABLISHED

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64
Q

MAX ENGINE START ITT?

A

815 C

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65
Q

START ENGINE MINIMUM OAT REQUIREMENT?

A

NONE SPECIFIED BY THE MANUFACTURER.

66
Q

MINIMUM OIL PRESSURE FOR ENGINE STARTS?

A

25 PSI

67
Q

WHAT IS REQUIRED AFTER THE SECOND ENGINE START BEFORE TAKE OFF?

A

2 MIN WARM UP PERIOD

68
Q

STARTER LIMITATIONS FOR ENGINE STARTS ON THE GROUND?

A

START 1 90SEC ON 10 SEC OFF

START 2 90 SEC ON 10 SEC OFF

START 3 90 SEC ON 5 MIN OFF

START 4 90 SEC ON 5 MIN OFF

START 5 90 SEC ON 5 MIN OFF

69
Q

FOR GROUND STARTS WHAT IS THE MAXIMUM CUMULATIVE STARTER RUN TIME PER START ATTEMPT?

A

90 SECONDS (MOTORING + START TIMES)

70
Q

STARTER LIMITATIONS FOR ENGINE STARTS INFLIGHT?

A 
1  120 SEC ON    10 SEC OFF
2  120 SEC ON    10 SEC OFF
3  120 SEC ON    5 MIN OFF
4  120 SEC ON    5 MIN OFF 
5  120 SEC ON    5 MIN OFF
71
Q

FOR INFLIGHT STARTS, WHAT IS THE MAXIMUM CUMULATIVE STARTER RUN TIME PER START ATTEMPT?

A

120 SECONDS / 2 MINUTES ( MOTORING + START TIMES)

72
Q

FOR CROSS BLEED ENGINE STARTS, WHAT IS THE MINIMUM REQUIRED MINIMUM PRESSURE?

A

40-45 PSI (REFERENCE USING THE STATUS PAGE)

73
Q

WHEN DOES FADEC AUTOMATICALLY APORT ENGINE STARTS?

A

1 HOT START
2 HUNG START
3 NO LIGHT OFF

74
Q

PROCEDURES TO START AND ENGINE WITH A TAILWIND?

A
  1. MONITOR N1 INDICATION
  2. WHEN THERE IS NO POSITIVE INCREASE OF N1 INDICATION BEFORE STARTER CUTOUT (50% N2)
    THE ENGINE START MUST BE MANUALLY ABORTED.
75
Q

WHEN MUST THE ENGINE BE MANUALLY ABORTED BY THE PILOT?

A

OIL 1 NO POSITIVE OIL PRESSURE INDICATION WITHIN 10SECONDS AFTER N2 SPEED STARTS TO INCREASE
2. OIL PRESSURE STABILIZES BELOW ENGINE LIMITS
ITT 3. NO ITT INDICATION WITHIN 30 SEC AFTER INITIATION OF FUEL FLOW
4. ITT EXCEEDS START LIMT (>815 C HOT)
N1/N2 5. N1 AND / OR N2 FAILING TO ACCELERATE TO STABLE IDLE SPEED (HUMG START)
6. DURING ENGINE START WITH A TAILWIND WHEN POSITIVE INCREASE OF N1 IS NOT INDICATED BEFORE STARTER CUTOUT (50% N2) IN THIS CASE THE AIRPLANE IS REPOSITIONED PRIOR TO ENGINE START TO MINIMIZE TAILWIND EFFECTS.
ELECTRICAL 7. INTERMITTENT ELECTRICAL MALFUNCTION OCCURS BEFORE THE STARTER DISENGAGEMENT (50% N2) THAT IS FOR ELECTRICAL, PNEUMATIC AND STARTER.

76
Q

DURING AN ENGINE START, WE MUST SEE N1 ROTATION BY WHAT N2?

A

POSITIVE INCREASE OF N1 MUST BE INDICATED BEFORE STARTER CUTOUT (50% N2)

77
Q

HOW IS THE ENGINE START MANUALLY ABORTED?

A

AFFECTED ENGINE: START/STAOP SECTOR……STOP

THIS IS TO MANUALLY CLOSE OFF THE STARTER VALVE.

78
Q

WHEN FADEC AUTOMATICALLY ABORTS AN ENGINE START, WHY IS IT REQUIRED TO MANUALLY SELECT THE START / STOP SECTOR TO STOP?

A

BECAUSE THE PILOT HAS TO MANUALLY CLOSE OFF THE STARTER VALVE VIA THE ASSOCIATED ENGINE START/STOP SELECTOR

79
Q

HOW MANY START ATTEMPTS MAY BE PERFORMED AFTER AN ENGINE HOT START?

A

2 ADDITIONAL ENGINE START ARE ALLOWED WHEN
1 AN AUTO ABORT OCCURS DUE TO AN ENGINE HOT START…AND
2. NO ENGINE EXCEEDANCE EICAS MESSAGE.

80
Q

ENGINE DRY MOTORING LIMITATIONS?

A 
START 1  90 SEC ON     5 MIN OFF 
START 2  30 SEC ON    5 MIN OFF
START 3   30 SEC ON    5 MIN OFF
START 4   30 SEC ON    5 MIN OFF
START 5   30 SEC ON    5 MIN OFF
81
Q

AFTER 5 SEQUENTIAL DRY MOTORING CYCLES, CAN DRY MOTORING BE ACCOMPLISHED AGAIN?

A

AFTER 5 SEQUENTIAL MOTORING CYCLES, THE PROCESS MAY BE REPEATED FOLLOWING A 15 MIN COOL DOWN PERIOD

82
Q

CAN THE AUTOMATIC TAKE OFF THRUST CONTROL SYSTEM (ATTCS) BE TURNED OFF FOR TAKEOFF?

A

NO

83
Q

WHEN IS FLEX THRUST TAKEOFF USED?

A

USED FOR ALL TAKEOFFS UNLESS PERFORMANCE OR OTHER OPERATIONAL CONSTRAINTS DICTATE OTHERWISE.

84
Q

WHEN IS FLEX THRUST PROHIBITED?

A

CSW

  1. CONTAMINATED RUNWY
  2. SPECIAL DEPARTURE PRECEDURE SPECIFIES FULL THRUST FOR TAKEOFF
  3. WIND SHEAR IS REPRORTED OR FORECAST
85
Q

TRUE/FALSE
DUE TO ENGINE COMPRESSOR STALL POSSIBILITY, STATIC TAKEOFF IS NOT RECOMMENDED WITH A CROSSWIND COMPONENT GREATER THAN 25 KTS?

A

TRUE

86
Q

CAN A TAKEOFF CONTINUE OR A REJECTED LANDING BE ATTEMPTED ONCE THE THRUST REVERSERS HAVE BEEN DEPLOYED?

A

NO

87
Q

AFTER SELECTING THE THRUST REVERSERS, WHEN CAN THE THRUST LEVERS BE MOVED INTO THE FORWARD THRUST RANGE?

A

ONLY AFTER ONCE THE REV ICON ON THE EICAS IS SHOWN IN AMBER OR GREEN.

88
Q

THE USE OF THE THRUST REVERSERS FOR TAXI OPERATIONS ALLOWED?

A

NO ITS PROHIBITED

89
Q

CAN THRUST REVERSERS BE USED FOR POWER BACK OPERATIONS?

A

NO ITS PROHIBITED.

90
Q

WHAT IS THE EXHAUST NOZZLE OIL PUDDLE SIZE LIMIT?

A

WHE THE PUDDLE SIZE EXCEEDS 4 IN CONTACT MX

91
Q

WHEN CAN AN ENGINE BE SHUTDOWN AFTER LANDING?

A

RUN THE ENGINES AT IDLE THRUST FOR 2 MIN. THIS IS TO ALLOW FOR ENGINE THERMAL STABILIZATION BEFORE SHUTTING DOWN AN ENGINE.
NOTES: 1. MAKE SURE THRUST LEVERS ARE AT IDLE.
2. TIME SPENT TAXIING COUNTS TOWARD THIS REQUIREMENT.
3. SAME REQUIREMENT APPLIES WITH OR WITHOUT THE USE OF THRUST REVERSERS.

92
Q

WHAT IS THE MINIMUM SPEED BRAKE SPEED?

A

180 KTS.

93
Q

WHEN WILL THE SPEED BRAKES AUTOMATICALLY RETRACT?

A
  1. AIRSPEED DECREASES BELOW 180 KIAS
  2. DURING A GO-AROUND MANEUVER THE SPEED BRAKES WILL AUTOMATICALLY RTRACT ANYTIME LEVERS ARE ADVANCED BEYOND THRUST LEVER ANGE (TLA) 70 DEGREES. THIS IS TO PREVENT INADVERTENT OPERATION CONDITION
  3. FLAPS 2 OR GREATER
94
Q

MAXIMUM SLAT/FLAP LIMITATION SPEEDS?

A 
VFE 1     230
VFE 2    215
VFE 3    200
VFE 4    180
VFE 5    180
FULL     165
RECOMMENDED TO NOT EXTEND OR FLY WITH THE FLAPS EXTENDED AT SPEEDS > VFE - 10KTS.
95
Q

MAX ALTITUDE FOR SLAT / FLAP EXTENSION?

A

20,000

96
Q

CAN THE SLATS / SLAPS BE USE FOR ENROUTE OPERATIONS?

A

PROHIBITED

97
Q

WHAT FLAPS SETTING MUST BE USED FOR CAT II ILS APPROACHES?

A

MANDATORY FLAPS 5

98
Q

WHAT FLAPS SETTING MUST BE USED FOR SINGLE ENGINE OPERATIONS?

A

FLAPS 5

99
Q

WHEN PERFORMING A RNP APPROACH, WHAT FLAPS SETTING MUST BE USED ?

A

FLAPS 5

100
Q

WHAT FLAPS SETTING MAY BE USED TO PERFORM INSTRUMENT APPROACHES?

A

1 ILS CAT 1 VOR, RNAV, LOC, FLAPS 5 OR FULL

2. ILS CAT II, RNP AND SE FLAPS 5 ONLY

101
Q

IF LANDING FLAPS FULL, WHAT GO-AROUND FLAPS MUST BE SET?

A

GO-AROUND FLAPS 4

102
Q

IF LANDING FLAPS 5, WHAT GO-AROUND FLAPS MUST BE SET?

A

GO-AROUND FLAPS 2

103
Q

MAXIMUM FUEL CAPACITY?

A

20, 935 LBS

104
Q

MINIMUM FUEL TANK TEMP?

A

-37

105
Q

ARE FUEL CROSSFEED OPERATIONS ALLOWED FOR TAKEOFF AND LANDING?

A

NO

106
Q

WHAT IS THE MAXIMUM FUEL IMBALANCE?

A

794

107
Q

CAN TAKEOFF AND LANDING OCCUR WITH A FUEL IMBALANCE EICAS MSG?

A

YES, IT IS PERMISSIBLE TO TAKEOFF AND LAND WITH A FUEL IMBALANCE MSG AS LONG AS THE ACTUAL IMBALANCE DOES NOT EXCEED 794 LBS

108
Q

WHEN IS FUEL IMBALANCE INDICATED?

A

WHEN THE WING FUEL IMBALANCE REACHES ITS MAXIMUM OPERATIONAL LIMIT (800LB) THE EICAS CAUTION MSG. FUEL IMBALANCE IS DISPLAYED

109
Q

WHEN IS THE FUEL IMBALANCE CONSIDERED RESOLVED?

HOW IS THIS INDICATED TO THE PILOTS?

A
  1. WHEN THE WINGS FUEL IMBALANCE REDUCES TO 100 LBS
  2. THE EICAS ADVISORY MSG. FUEL EQUAL - X FEED OPEN IS DISPLAYED, INDICATING THAT THERE IS NO WING FUEL IMBALANCE CONDITION AND THE CROSS FEED VALVE IS OPEN
110
Q

WHAT HAPPENS IF THE CROSSFEED VALVE IS OPEN BEFORE REACHING THE FUEL IMBALANCE CONDITION OF 800 LBS.

A

IF THE CROSS FEED VALVE IS OPEN PRIOR TO REACHING THE WINGS FUEL IMBALANCE CONDITION (800LBS) THE MSG FUEL EQUAL = X FEED OPEN IS DISPLAYED EVEN IF WINGS FUEL IMBALANCE IS MORE THAN 100 LBS.

111
Q

WHEN SHOULD MINIMUM FUEL BE DECLARED?

A

2,250 LBS
WHEN AN AIRCRAFTS FUEL SUPPLY HAS REACHED A STATE WHERE, UPON REACHING THE DESTINATION, IT CAN ACCEPT LITTLE TO NO DELAY AT ALL.
THIS IS NOT AN EMERGENCY SITUATION BUT MERELY INDICATES AN EMERGENCY SITUATION IS POSSIBLE SHOULD ANY UNDUE DELAY OCCUR

112
Q

WHAT DOES MINIMUM FUEL PROVIDE

A

2,250 LBS

MINIMUM FUEL PROVIDES 45 MINUTE OF FUEL ENDURANCE BASED UPON 1,500 FT. AFE /GREEN DOT /CLEAN

113
Q

EMERGENCY FUEL BE DECLARED

A

WHEN THE ESTIMATED FUEL REMAINING AT TOUCHDOWN AT THE AIRPORT OF INTENDED LANDING WILL BE LESS THAN 30 MIN FUEL ENDURANCE / 1500LBS. IF FURTHER DEVIATION FROM THE PLANNED ROUTE OF FLIGHT COUD CAUSE AN EMERGENCY.

114
Q

EMERGENCY FUEL

A
  1. WHEN IT IS DETERMINED THAT THE AIRPLANE WILL HAVE LESS THAN 30 MIN WOR OF FULE AFTER LANDING ON THE GROUND.
  2. 1500 LBS.
    EMRG FUEL PROVIDES 30 MIN OF FUEL BASED ON 1,500 AFE/ GREEN DOT/ CLEAN
115
Q

EMERGENCY FUEL, WHAT DO YOU DO?

A
  1. REPORT FUEL REMAINING IN MINUTES TO ATC AND DISPATCH (TIME PERMITS)
  2. FUEL INDICATORS TURN AMBER WHEN FUEL IN THE RESPECTIVE TANK DROPS BELOW 1,320 LBS (2,640 LBS TOTAL)
116
Q

MINIMUM HYDRAULIC RESERVOIR TEMP FOR ENGINE STARTS?

A

= -18C

117
Q

WHEN ARE TAT AND SAT TEMP INFORMATION VALID?

A

> 60 KTS

118
Q

WHEN IS TAS INFO VALID?

A

> 60 KTS

119
Q

CAN THE MFD TAT RATING BE USED AT THE GATE OR DURING TAXI TO DETERMINE IF ICING CONDITIONS EXIST?

A

NO USE ATIS / ASOS OAT

TAT INFO IS ONLY VALID > 60 KTS.

120
Q

WHAT CAUTION MUST BE USED WHEN USING / READING THE MAGNETIC COMPASS INDICATOR?

A

WHILE TRANSMITTING ON VHF1 THE STANDY MAGNETIC COMPASS INDICATION IS NOT VALID

121
Q

WHAT MINIMUMBS ARE REQUIRED TO BE USED ON CAT 1 APPROACHES?

A

BAROMETRIC ALTIMETER MINIMUMS MUST BE USED FOR ALL CAT 1 APPROACHES

122
Q

CAN NAVIGATION BE PREDICATED ON THE USE OF EGPWS /TERRAIN AWARENESS SYSTEM

A

NO

123
Q

IF LANDING AT AN AIRPORT NOT IN THE EGPWS DATABASE WHAT SHOULD BE ACCOMPLISHED?

A

THE USE OF PREDICTIVE EGPWS FUNCTIONS SHOUD BE MANUALLY INHIBITED WHEN LANDING AT AN AIRPORT THAT IS NOT IN THE DATABASE TO AVOID UNWANTED ALERS
PRESS THE GRD PROX TERR INHIB BUTTON ON INHIBIT PREDICTIVE EGPWS FUNCTIONS

124
Q

WHAT IS THE REQUIREMENT FOR WHEN GPS DATA IS NOT AVAILABLE AT A DESTINATION

A

THE USE OF PREDICTIVE EGPWS FUNCTIONS MUST BE MANUALLY INHIBITED DURING QFE (LOCAL STATION BAROMETRIC PRESSURE) OPERATIONS, WHEN GPS DATA IS UNAVAILABLE OR INOPERATIVE. PRESS IN THE GRD PROX TERR INHIBIT BUTTON TO INHIBIT PREDICTIVE EGPWS FUNCTIONS.

125
Q

WHAT IAP MINIMUM IS NOT APPROVED TO BE USED:

A

RNAV (GPS) LP MINIMA ARE NOT AUTHORIZED.

126
Q

EXPLAIN ICING CONDITIONS ON THE GROUND?

A

GROUND
1. OAT LESS THAN OR EQUAL TO 10C ON THE GROUND OR FOR TAKE OFF
2. VIS MOISTURE IN ANY FORM
CLOUDS
FOG EQUAL TO OR LESS THAN 1SM
SNOW
SLEET
ICE CRYSTALS
3. OPERATING ON RAMPS, TAXIWAYS OR RUNWAYS WITH SURFACE MOISTURE CONDITIONS THAT MAY BE INGESTED BY THE ENGINES, OR FREEZE ON ENGINES, NACELLES, OR ENGINE SENSOR PROBES.
SURFACE SNOW—ICE–STANDING WATER —SLUSH

127
Q

EXPLAIN ICING CONDITIONS INFLIGHT?

A
  1. TAT EQUAL TO OR LESS THAN 10 DOWN TO SAT TEMP EQUAL TO OR GREAT THAN -39
  2. VISIBLE MOISTURE IN ANY FORM:
    CLOUDS
    FOG EQUAL TO OR LESS THAN 1 SM
    RAIN
    SNOW
    SLEET
    ICE CRYSTALS
128
Q

HOW CAN THE PRESENCE OF ICING ACCUMULATION ON THE AIRPLANE BE VERIFIED?

A 
CHECK THE: 
1.  WIND SHIELD
2.  WIND SHIELD WIPER
3.  WING SURFACE FOR ICE ACCUMULATION 
YOU MAY HAVE TO USE FLASH LIGHT
129
Q

IF THE PILOTS SUSPECT ICING ON THE AIRPLANE WITHOUT THE ANTI ICE SYSTEM AUTOMATICALLY TURNING ON, WHAT SHOULD BE DONE?

A

SELECT THE ANTI-ICE PROTECTION SYSTEM OVERIDE MODE KNOB TO ON

130
Q

WHAT SPEED SHOULD BE USED WHEN FLYING THROUGH DETECTED OR SUSPECTED ICING CONDITIONS?

A

USE ICE SPEEDS AS REFERENCE.

131
Q

WHAT IS THE TEMP LIMITATION FOR THE ANT-ICING SYSTEM AUTOMATIC OPERATION ?

A

THERE IS NO TEMP LIMITATION.

132
Q

FOR T/O IN ICING CONDITIONS, EXPLAIN THE PROCEDURE THAT IS REQUIRED TO BE COMPLIED WITH FOR THE ANT-ICING AUTOMATIC SYSTEM TO OPERATE.?

A

OAT FROM 5C TO 10C
THE T/O DATASET MENU ON THE MCDU MUST BE SET TO ENG IN THE FOLLOWING CASES WHEN OAT IS FROM 5 TO 10 AND:
—WHEN THERE IS ANY POSSIBILITY OF ENCOUNTERING VISIBLE MOISTURE UP TO 1,700FT AFE.
—-WHEN OPERATING ON RAMPS, TAXIWAYS OR RUNWAYS WHERE SURFACES NOW,ICE STANDING WATER, OR SLUSH MAY BE INGESTED BY THE ENGINES, OR FREEZE ON ENGINES, NACELLES, OR ENGIN SENSOR PROBES.

OAT LESS THAN 5C
THE TO DATASET MENU ON THE MCDU MUST BE SET TO ALL IN THE FOLLOWING CASES WHEN OAT IS LESS THAN 5C AND:
—–WHEN THERE IS ANY POSSIBILITY OF ENCOUNTERING VISIBLE MOISTURE UP TO 1,700AFE—-WHEN OPERATING ON RAMPS, TAXIWAYS OR RUNWAYS WHERE SURFACES NOW,ICE STANDING WATER, OR SLUSH MAY BE INGESTED BY THE ENGINES, OR FREEZE ON ENGINES, NACELLES, OR ENGIN SENSOR PROBES.

133
Q

WHEN THE PILOTS SELECT REF A/I OFF, WHEN WILL THE ANTI-ICE RESUME AUTOMATIC OPERATION INFLIGHT?

A

THE OFF SELECTION INHIBITS ANTI-ICE LOGIC AFTER T/O UNTIL 1,700 AGL OR
2 MIN WHICHEVER OCCURS FIRST

134
Q

HOW DOES THE ANTI-ICE SYSTEM NORMALLY OPERATE INFLIGHT?

A

THE ENGINE AND WING ATI-ICE SYSTEMS OPERATE AUTOMATICALLY, IN CASE OF ICE ENCOUNTER WHEN THE ICE PROTECTION MODE SELECTOR IS IN THE AUTO POSITION.

135
Q

WHAT MUST THE CREW DO IF BOTH ICE DETECTORS FAIL?

A

THE CREW MUST SET THE MODE SELECTOR TO ON WHEN ICING CONDITIONS EXIST OR ARE ANTICIPATED BELOW 10C TAT WITH VISIBLE MOISTURE.

136
Q

IF BOTH ICE DETECTORS FAIL, WHEN SHOULD THE PILOT SELECT THE ANTI-ICE MODE SELECTOR TO ON?

A

WHEN ICING CONDITIONS EXIST OR ARE ANTICIPATED BELOW 10C TAT WITH VISIBLE MOISTURE

137
Q

WHEN SHOULD THE ADS PROBE HEATER SWITH BE PRESSED IN BY THE FO? PRESSED OFF?

A
  1. FOD OAT < -18C OR WHEN THE SMART PROBES ARE FROZEN
    ANY TIME 1. OAT IS AT OR BELOW FREEZING 0C
    AND
  2. WATER, ICE, OR SNOW IS PRESENT OR SUSPECTED
    AND/OR
  3. PROBES ARE CONTAMINATED
    AND/OR
  4. PFD SHOWS DISCREPANCIES (AIRSPEED, ALT)
  5. PRESSED OUT DURING TH FO AFTER START FLOW
138
Q

WHEN DO THE ADS PROBE HEAT TURN ON AUTOMATICALLY?

A
  1. ONCE AN ENGINE IS STARTED
    OR
  2. AIRPLANE IS AIRBORNE
139
Q

WHAT ARE THE FROST LIMITS FOR THE FUSELAGE? UNDERWING?

A

FUSELAGE: ONLY A THIN LAYER OF FROST IS NOTICED, WHERE IT IS EASY TO DISTINGUISH THE FUSELAGE SURFCE FEATURES UNDERNEATH ( LINE OR MARKINGS) THAT IT IS OK TO T/O WITHOUT DEICING THE FUSELAGE’S UPPER SURFACE. MUST DEICE FUSELAGE FOR ICE OR SNOW

UNDERWING: CAN TAKE OFF IF FROST ADHERING TO THE WING’S UNDERSIDE CAUSED BY COLD SOAKED FUEL AS LONG AS FROST THICKNESS < 1/8 INCH

140
Q

WHAT IS MAX DIFFERENTIAL PRESSURE LIMIT?

A

LESS THAN OR EQUAL TO 37,000 = 7.8 PSI

> 37,000 8.4 PSI

141
Q

MAX DIFFERENTIAL PRESS FOR T/O

A

0.2 PSI

142
Q

WHAT IS THE MAX DIFF PRESSURE FOR LANDING?

A

0.2 PSI

143
Q

MAX DIFFERENTIAL OVERPRESSURE?

A

8.8 PSI

144
Q

MAX DIFFERENTIAL NEGATIVE PRESSURE?

A

-0.5 PSI

145
Q

WHEN WILL A “CABIN ALTITUDE HI” EICAS MSG APPEAR?

A

CABIN ALT EQUAL TO OR GREATER THAN 9,700 FT.

146
Q

HOW LONG WILL EMERG LIGHTS REMAIN LIT WITOUT NORMAL ELECTRIC POWER?

A

10 MIN

147
Q

THE CARGO LOW RATE FIREX BOTTLE CAN DISCHARGE HALON FOR HOW LONG?
WHAT DIVERSION TIME DOES THIS PROVIDE?

A
  1. 75MIN

2. 60 MIN DIVERSION TIME

148
Q

HOW MANY MIN OF OXYGEN WILL TH PAX MASKS PROVIDE?

A

12 MIN

149
Q

EXPLAIN THE CREW OXYGEN LEVEL COLOR MEANING?

A

GREEN: 3 CREW MEMBERS
CYAN: 2 CREW MEMBERS
AMBER: CALL MX

150
Q

REQUIREMENTS FOR A STABILIZED APP.

A

STABILIZED APP IS CHARACTERIZED BY

  1. CONSTANT ANGLE
  2. CONSTANT RATE OF DESCENT
  3. STABILIZED BY 1,000 FT. AGL/ RA
  4. LANDING NEAR THE TOUCHDOWN POINT
  5. AND ALL OF THE FOLLOWING CRITERIA, WHICH MUST BE ALLMET BY NO LATER THAN 500 FT AGL/RA

BY 1,500 FT AGL/RA OR TH FAF WHICHEVER OCCURS LATER

  1. LANDING GEAR DOWN
  2. AIRSPEED NO GREATER THAN 180 KIAS

AT 1,000 FT. AGL / RA
1. FINAL LANDING CONF
2. BEFORE LANDING CHECKLIST COMPLETE
3. AIRSPEED WITHIN +15 AND -5 OF TARGET AIRSPEED
4. ON LATERAL PROFILE
5. ON VERTICAL PROFILE WITH MINOR BRACKETING MANEUVERS
PM WILL ANNOUNCE DEVIATIONS FROM CONFIGURATION, SPEED OR DESCENT RATE FROM PLANNED.

At 500” FT. AGL

  1. AIRSPEED INDICATION ESTABLISHED IN THE CONFINES OF THE SPEED BUG.
  2. THRUST ABOVE IDLE
151
Q

MORE STABILIZED APPROACH

A

AT 1,000FT AGL/RA

  1. FINAL LANDING CONFIGURATION
  2. BEFORE LANDING CHECKLIST COMPLETE
  3. AIRSPEED WITHIN +15 AND -5 KTS OF TARGET SPEED
  4. ON LATERAL PROFILE
  5. ON VERTICAL PROFILE OR CORRECTING WITH MINOR BRACKETING MANEUVERS. PM WILL ANNOUNCE DEVIATIONS IN CONFIGURATION, SPEED OR DESCENT RATE FROM THE PLAN.

BY 500 FT AGL:

  1. AIRSPEED INDICATION ESTABLISHED WITHIN THE CONFINES OF THE SPEED BUG.
  2. THRUST SETTING ABOVE IDLE
152
Q 
1  MAX RAMP? 
2.  MAX T/O? 
3.  MAX LANDING? 
4  ZERO FUEL WEIGHT?  
5.  MAX FUEL WEIGHT?
A 
1  76 = 85870   70 = 85450
2  76 = 85517    70 = 85098
3.  74957 
4.  76 = 69886  70 =  69467
5.  20935
153
Q

DIMENSIONS?

  1. WING SPAN?
  2. LENGTH?
  3. HEIGHT/
A
  1. 93’ 11”
  2. 103’ 11”
  3. 32’ 4”
154
Q
  1. MAX TEMP T/O?
  2. MAX TEMP LAND?
  3. MIN FUEL TANK TEMP?
  4. MIN HYD RES TEMP ENG STARTS?
  5. MIN TEMP T/O AND LAND?
  6. MIN TEMP APU START AND OPERATION?
A
  1. ISA + 35 (52C)
  2. ISA +35 (52C)
  3. -37 C
  4. -18 C
    5 -40 C
  5. -54 C
155
Q
  1. MAX ALT?
  2. APU MAX OPERATION AND GEN USE ALT?
  3. APU MAX START ALT?
  4. SINGLE PACK OPERATION?
  5. APU ENG START ASST?
  6. MAX ALT SLAT / FLAP EXT?
  7. APU BLEED AIR USE?
  8. MAX ALT T/O AND LAND?
  9. AUTO PILOT MIN ENGAGE HEIGHT?
  10. MIN AUTO PILOT NON PREC APPROACH?
  11. MIN AUTO PILOT USE HEIGHT?
A
  1. 41,000
  2. 33,000
  3. 30,000
  4. 31,000
  5. 21,000
  6. 20,000
  7. 15,000
  8. 10,000
    9 400’
  9. MDA
  10. 50’
156
Q

WINDS

  1. MAX DEM X WIND DRY RUNWAY?
  2. MAX DEM X WIND WET, DRY/WET SNOW?
  3. MAX DEM X WIND STATIC T/O
  4. MAX HEADWIND CAT II?
  5. MAX DEM CROSS WIND FOR COMP SNOW?
  6. MAX DEM CROS WIND FOR STAND WATER/ SLUSH/ WET SNOW/ DRY SNOW
  7. MAX TAIL WIND T/O AND LANDING, MAX CAT II, MAX TAIL WIND CAT II
  8. MAX DEM XWIND FOR RWY ICE/WET ICE & DEMONSTRATED CAT II?
  9. MAX DEMONSTRATED TAIL WIND FOR CAT II?
  10. Braking action reported 1, 2 or POOR, CROSS WIND TAKE OFF OR LANDING?
A
  1. 38
  2. 31
  3. 25
  4. 25
  5. 20
  6. 18
  7. 15
  8. 12
  9. 10
  10. 10
157
Q

SPEEDS
1. MAX OPERATING SPEED LIMIT IN MACH?
2. 29,000 - 41,000 DECREASES FROM _____ DOWN TO ______ KIAS / MMO .82
3. 8,000 TO 10,000 TO 29,000
4. MAX SL - 8,000 KIAS?
5. WHAT ARE THE MAX GUST INTENSITY / TURB PENETRATION SPEED?
6 VA?

A
  1. .82
  2. 320 TO 243 /KIAS MMO .82
  3. 320
  4. 300
  5. LESS THAN 10,000 VB = 250 KIAS
    EQUAL AND GREATER VB LOWEST OF 270 KIAS OR .
    0.76 MACH
  6. 240
158
Q

GREEN DOT

A

1, 1,3G OR 40 DEGREE BANK

  1. L/D MAX
  2. SE DRIFT DOWN
  3. EMERGENCY RETURN
  4. FLAP EXTENSION / FLAP RETRACTION (+10)
159
Q

MAX TAXI SPEEDS

A

DRY STRAIGHT 30
WET CONTAMINATED STRAIGHT 10
DRY TURN 10
WET CONTAMINATED TURN 5

160
Q

IS IT OKAY TO USE THE APU BLEED AND THE HP CART PNEUMATIC AIR AT THE SAME TIME?

A

NO

161
Q

WHAT IS THE APU MIN START TEMP?

WHAT IS THE APU MINIMUM OPERATIONAL TEMP?

A
  • 54 C

- 54 C

162
Q

LANDING XWIND LIMITS RCC:

  1. RCC 6 DRY
  2. RCC 5 WET, DRY SNOW, WET SNOW (GOOD)
  3. RCC 4 COMPACT SNOW (GOOD TO MEDIUM)
  4. RCC 3 SLIPPERY WHEN WET, > 1/8 (MEDIUM)
  5. RCC 2 1/8 WATER OR SLUSH (MED TO POOR)
  6. RCC 1 ICE (POOR)
A
  1. 38
  2. 31
  3. 20
  4. 15
  5. 12
  6. 8

175 LIMITATIONS (21 decks)

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