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Dc-9/md-80 > Limitations > Flashcards

Limitations Flashcards

1
Q

What is the maximum operation alt of the MD-80

A

37,000 feet

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2
Q

What is the wing landing lite limitation

A

1 1/2 minute after initial
3 1/2 minutes after subsequent

Lamp duty cycle 10 min in still air. Extend speed max is Vmo/Mom

Max speed with wing landing lt not retracted in 250 KIAS

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3
Q

What is the maximum tailwind for the MD-80

A

10 knots

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4
Q

What is the maximum cross wind dry runway

A

30knots

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5
Q

What is the maximum cross wind limitations in manual or restricted rudder

A

12 knots

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6
Q

What is the maximum crosswind limitation with poor braking

A

10knots

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7
Q

What is the maximum cross wind limitations runway less the 150 feet wide

A

10 knots landing only

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8
Q

What are the contaminated runway limits to take off

A

Dry snow 4”
Wet snow half inch
Slush or standing water half inch

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9
Q

Does the company allow ops in NIL braking

A

No, idle thrust is more than braking capability

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10
Q

What is Vmo/Mmo

A

340 KIAs sL to 27,300

Than .84m above 27,300

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11
Q

What are the MD-83 weight limits

A

Max taxi 161,000
Max TO. 160,000
Max landing 150000
Max 0 fuel 122,000

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12
Q

What is the minimum altitude to engage the AP after TO

A

500’ AGL

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13
Q

What is the minimum altitude for AP use during app

A

IMC -50 feet below MDA/ DA

VMC 50 feet above TDZ

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14
Q

What situation required AT

Disconnect

A

If engine surge or stall detected during TO

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15
Q

What is AC power distribution volts/amps limit and normal

A

115 volts +- 8 VAC limit

115 volts +-3 VAC normal

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16
Q

What is the engine Generating max loads

A

Peak > 1.5 (5s)
Max 1.5 (5min)
Max continues 1.0

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17
Q

What is the APU gen limit

A

Maximum continuous (grd). 1.25

Maximum continuous (air) <25. 1.0

Maximum continuous at 25 -30 .7
30 to 37. .625

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18
Q

What is the D.C. Power distribution read from D.C. Busses in volts

A

26+-4 VDC limit

26+-2 VDC normal

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19
Q

What is the D.C. Power distribution on the Load meter

A

Maximum continuous 1.0

Maximum diff. Between 2 Gage’s same buss .3

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20
Q

What is the external power limits

A

Same S gen

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21
Q

Do not reset following CBS

A 
Batt charger
Aux. hydraulic pump
Fuel Quantity
Fuel gags 
LAvatory flush motor
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22
Q

What is the max limit for slats out mid/ flaps 0

A

280kias/.57mach

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23
Q

What is the speed limit;

Slats mid/. Flaps 11 degrees

A

280/.57mach

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24
Q

What is the speed limit for: slats full, flaps 15 degrees

A

240kias/.57mach

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25
Q

What is the speed limit for: slats full/ flaps /28 degrees

A

200 kias/.57m

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26
Q

What is the speed limit for: slats full, flaps 40degrees

A

195 KIAs/.57m

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27
Q

What flap settings are prohibited

A

Between 13-15 degrees

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28
Q

What are the speed brake limitations

A
  1. Only use with0 flaps
  2. do not use ground position in flt
  3. Do not extend fear with spoilers deployed
  4. Do not use below 220 knots
  5. Do not arm grounds spoilers prior to gear extension.
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29
Q

Can the gear be extended while speed brakes are deployed

A

No

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30
Q

What is min fuel for GA

A

500 Lbs

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31
Q

What is the max fuel imbalance wing tanker

A

1500 lbs

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32
Q

What is the max permissible aux fuel tank imbalance

A

400 lbs

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33
Q

What is the max fuel capacity combined

A

46,800 lbs

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34
Q

What is max ctr tank loading

A

21,000 lbs

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35
Q

When must engine anti-ice system be turned on

A

Taxi and takeoff in visible moisture at 5degress c or less

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36
Q

What temp/ dew point spread constitutes visible moisture

A

Spread of 3 degrees or less

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37
Q

If AF icing conditions are anticipated or encountered after dep. when can you turn on ice protection

A

Atengine failure cleanup alt.

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38
Q

Above what temp is it prohibited to use AF ice protection

A

10 degrees c

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39
Q

Engine and AF ice protection must be turned on during fight when RAT IS READING BETWEEN

A

?

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40
Q

When should tail deuce be activated

A
  1. 1minute prior to sel landing flaps
    2 at least every 20 minutes
    3 after leaving icing prior to turning AF anti ice off
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41
Q

Take off my borne accomplished unless visual check ofupper wingsurface and wing is clear of ice when:

A

A. If ice on lower wing or either wingon pre flight

B. Ambient temp below 15 degrees and high humidity or visible moisture

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42
Q

Define visible moisture

A

Rain, snow fog, drizzle, sleet, ice crystals or temp dewy spread of 3 degrees or less

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43
Q

When does the upper wing inspection apply

A

A. It sppplies regardless of whether or not the overwing ice protection detect system is installed operable or inoperable

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44
Q

What are the brake temp limits

A

A. Maximum for setting 300
B. Maximum for TO 205
Overheat lt on >305
Off <260

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45
Q

What are the gear speeds

A

VLE/extended 300/.70m

VRet 250 knots/.70m

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46
Q

What is maximum tire speed

A

195 knots ground speed

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47
Q

What is the limitation for use ofAPU air

A

APU air switch must be off for all inflight operations

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48
Q

What is the the maximum altitude for APU usage

A

35,000 feet

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49
Q

What are the APU EGT limits

A

Starting. 760 degrees c
30s
Trans load 732 degrees
Continuous. 710

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50
Q

What is the maximum APU

Rotor speed

A

110 percent

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51
Q

What general precautions

Observed for APU ops

A

1 APU air switch off for al inflt ops

  1. When starting engine w APU air AC supply switches must be off
  2. Maximum altitude for APU use is Fl35
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52
Q

What is the APU starter duty cycle

A 
1. 90s
R. 5m
2. 90s
R. 5m
3. 90s
R.60min
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53
Q

What will happen to the WAGS during sustaining banks greater than 15 degrees

A

Desensitized and alerts will be delayed

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54
Q

What mode does the charger have to be in prior to takeoff

A

Pulse mode

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55
Q

What are the approved fuels for the MD-80

A

Jet a and a1

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56
Q

If using TO flex mode what must be off

A

ART system

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57
Q

What is the maximum ground starting EGT for the engines

A

475 c

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58
Q

What is the starting EGT for the engines in flight

A

625 c

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59
Q

What is the ground idle maximums EGT of the engines if air bleed or power is being extracted

A

480 c

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60
Q

What are the ignition limitations

A

CONT. continuous
oVRD 2 m on the 3 off the 2 minutes then 23 off
If COnt is inoperable oVRD my be used
20m on 10 min off requires log book entry

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61
Q

What is min oil pressure for flight

A

40 psi

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62
Q

What is normal Oil Pressure

A

40-55 psi

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63
Q

What are the engine oil temp limitations

A

Cont less than 135

15 minutes 135-165

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64
Q

What is the n1 limits

A

Max Cont. 101.6
Max TO. 101.6

Normal. 219 98.8

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65
Q

N2 limits

A

Max cont 102.5
Max TO 102.5
Normal TO thrust. 100.9

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66
Q

What is the wing span of the MD-80?

A

107’10”

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67
Q

What is the length of the MD-80?

A

148feet

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68
Q

What is the tail height of the MD-80?

A

30 feet

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69
Q

What is the wheel base of the MD-80

A

17 feet

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70
Q

What is the turning radius of the MD-80?

A

95 feet

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71
Q

What precautions must be noted for the cargo door?

A

Shall not be operated or left open in winds of 45 or greater

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72
Q

What is the runway slope max gradient for TO

A

1.7 to -2.0 percent

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73
Q

What is the runway slope max gradient for landing

A

2.0 to -2.0 percent

74
Q

What is the max TO and landing altitude

A

8,500 feet

75
Q

What is the minimum takeoff and landing altitude

A

-1,000ft

76
Q

What is the maximum TO and landing temp below 2,525 feet

A

+50 degrees centigrade

77
Q

Maximum TO and landing altitude above 2525 to 8500 feet

A

STD ISA +40 degrees centigrade

78
Q

What is the minimum TO and landing temp

A

-54 degrees centigrade

79
Q

Max enroute temp

A

STD +35

80
Q

Minimum enroute temp

A

-76 degrees centigrade

81
Q

What is the main fuel tank capacity

A

9200 lbs

82
Q

What is the Aux fuel tank capacity

A

3700 lbs

83
Q

What is the wing landing light max extend speeds

A

340 below 27,300
Or.84 Mach
Company 250 KIAS

84
Q

What is the minimum battery voltage for start

A

25 volts

85
Q

What is the battery charging voltage

A

26 to 39 volts

86
Q

What is the maximum battery charging amp limits

A

0-65 amps to left

87
Q

With emergency power on

What is the maximum amp draw

A

10-50 to right

88
Q

What is the gen/APU/ external power freq. limits

A

400 cycles +-20

89
Q

What are the battery charging modes

A

Oscillating: must be stabile within 4seconds
Continuous:max 65 amp gradually decrease to 40 amps
Pulse: amps pulse between 0-40
Must be in pulse TO TO

90
Q

What are the engine EGT limits for TO and GA

A

625 for 5 minutes

630 for 2 minutes

91
Q

What is the the EGT limit for Maximum continuous thrust MCT

A

580

92
Q

What is the overall length of the MD-80

A

147 feet 10 inches

93
Q

What is the wing span of the MD-80

A

107’ 10”

94
Q

What is the turn radius of the MD-80

A

94’3”

95
Q

What three doors are non-plug type

A

Crew stairs, cargo and aft air stair

96
Q

What are the non-disable lights on the crew alerting panel

A

Doors and master Warnings

97
Q

What light is non Mel able

A

Anti collision light

98
Q

How many battery packs for the emergency lights

A

Many

99
Q

What kind of switch is the emergency light switch

A

A disagreement light

100
Q

What approach category does the md-82 fall under

A

C for approaches

D for circling

101
Q

What approach category does the MX-83 fall under

A

C for flaps 40

And D for flaps 28 and circling

102
Q

How much life does the EFB have to have to start a trip

A

Min 80/

103
Q

What is the green disk for located under the FO window

A

Green blow out disk for thermal relief of O2 bottle

104
Q

What bus are bugged for take off

A

V1,v2, flap ret, slat Rey

105
Q

How long is the airport analysis good for

A

48 hours

106
Q

Does TAws show man made obstacles

A

No

107
Q

What is proximate traffic

A

6 miles- blue

108
Q

What is a TA

A

20 to48s yellow

109
Q

What is an RA

A

15-35s- Red

110
Q

When does the stall shacker activate

A

10 percent of stall

111
Q

Are the forward strakes heated

A

Yes

112
Q

What should you varify with the lower cargo doors

A

Make sure compartment is empty

113
Q

What docs are in the aircraft manual

A

?

114
Q

What precautions should you take to disconnect ground power

A

Make sure it is off first

115
Q

How many battery are there

A

2 14volt DC

116
Q

What is unique about the emergency inverter

A

It is single phase AC

117
Q

Will the APU crosstie in flight

A

Yes but not on ground

118
Q

If you are on Emergency power, will the batteries still be charged

A

No

119
Q

Can you get Energency power with the battery switch off

A

Yes

120
Q

What is the amber arc. On the CSD

A

11.2

121
Q

What is the minimum speed for app with restricted rudder illuminated

A

135 knots

122
Q

What PSI does the inlet fuel pressure low light go on

A

5psi

123
Q

What PSID will the filter pressure drop illuminate (fuel)

A

5 PSID across the filter

124
Q

Is there a fuel tank temp gage

A

No

125
Q

What if you turn fuel heat on and get no fuel temp rise what happened

A

Low pressure pump failed

126
Q

What bleed source does fuel hear use

A

13th stage bleed

127
Q

How is the engine oil pump driven

A

N2 spool

128
Q

When will the oil dtrain clog light illuminate

A

35 PSID across the filter

129
Q

When will engine oil low presssure light illuminates

A

35 PSI

130
Q

What is maximum thrust for the JT 8D-219 engine

A

21700 lbs

131
Q

What is normal thrust of the -219 engine

A

21000

132
Q

What is max cont thrust of the -219 engine

A

18900

133
Q

When will the ART fire

A

W wind shear
A ART computer failure
F FGCP failure or switch
T thrust diff of 30 N1

134
Q

How much thrust will be diverted by the buckets

A

40 percent

135
Q

When will the RAmAPU door open

A

95 percent of APU

136
Q

What will cause the APU to auto shut down

A

?less than 2 psi oil
110 percent
APU fire light

137
Q

What is the allowable fuel density range

A

6.3 lbs to 7.1 lbs per gallon

138
Q

What fuel press is the D.C. Fuel pump

A

10 PSI

139
Q

What is minimum fuel for dispatch?

A

7500 lbs minimum

140
Q

What is the fire detection limitation (cargo)

A

Airplane must land with 60 minutes of discharge of bottle 1

141
Q

What does pulling fire handle do

A 
Silence the bell
H    Hydraulics reservoir
A.    Pneumatic  mech
L.     Elect GCR
F.      Fuel at wing root
Allows to rotate handle
142
Q

What is the tail ice icing cycle

A

150 seconds

143
Q

What is the starter standard duty cycles

A

90s on
5 m off
30s
5m offthen repeat

144
Q

What is the alternate starter duty cycles

A 
90s
10min off 
60s
10min off
Then continue
145
Q

How much reverse thrust is diverted?

A

40 percent

146
Q

When will the APU RAM door open

A

95 percent

147
Q

When does the APU low oil light illuminate

A

35 PSI

148
Q

What are the three things that will automatically shut the APU down

A

Oil p less the 2
APU fire light
110 percent overspeed

149
Q

What fuel pressure does the D.C. Fuel pump provide

A

10 psi

150
Q

What buss has fire detect and protect on it

A

D.C. Transfer bus

151
Q

How many lights will you get during the fire test

A

14

152
Q

What powers the pneumatic augment valves

And what happens it they depower

A

Normal D.C. Fail closed

153
Q

What temperature activates the tail compart

Temp hi warning light

A

180 f

154
Q

Where are the three places that temperature is sense in the PAC

A

Turbine inlet
Compressor outlet
Mixing chamber

155
Q

When will the PACS auto shutdown in auto mode

A

Engine failure

GA

156
Q

What activates the the cabin Alt warning light

A

9,500 -10000 foot cabin

9 sec aural then silent

157
Q

How are the brakes cooled inflight

A

A brake cooling inlet

158
Q

What does the ground shift mechanism do

A

1 centers steering
2 disconnects steering from rudder
3 retracts gear handle release rod
4 engage switch to allow ground control relay to switch to flight

159
Q

What will auto shut down the PAC

A

Switch in auto
70 psi difference in 13 th stage bleed air

Only operates at cabin diff of 1.3 psi

160
Q

When does the Pic have to submit a captains irregularity report to the DOM

A

Total vertical error if 300 ft

Altimetry system error of 245 or more

Assigned altitude deviation of 300 ft or more

161
Q

What arms the ART system

A

T with two good signals

O n the ground for more than 2m
A. Rts switch in AUTO
S. Lats not retracted
T est successful

162
Q

What turns light on ART

A

N1 past 64 percent

163
Q

When will ART fire

A

Wind shear
ART computers malf
Flight guidance malf
T 30 percent diff N 1

164
Q

What perameters does

The ATR system look at

A

AT engaged
B. Below ga epr
A. Above 350 RA
T o pitch TOTO

165
Q

When will ATR activate

A

.25 epr difference
7 percent N 1 difference
V speed less than 0 for 5 seconds

Exit by selecting new vertical mode

166
Q

What will shut down the

Hydraulic transfer pump

A

Less than 1.3 qts in

Reservoir

167
Q

Where are the hydraulic accumulators located

A

Rudder for gear up damping
Thrust reverser s 2
Brakes 2
Elevator August

168
Q

When will the hydraulic

Low pressure light illuminate

A

900 psi

169
Q

If hydraulic pumps fail what position do they fail electric failure

A

Aux pump fails off
Normal pump fail -hi
Transfer fail in position

170
Q

How does the gear work

A

Free fall
Duplicate micro switch
Normal lights
Gear door drags

171
Q

How are the brakes cooled in flight

A

Cooling inlet

172
Q

How many brake actuators or there

A
  1. 4 left

4 right

173
Q

How many fuse plugs

A

3

174
Q

Where are the transducer s located brakes

A

On wheel hubs

175
Q

Do you have auto skid in

Emergency power

A

No

176
Q

When will wheel not turning light illuminate

A

20 percent difference

177
Q

What must be done when using manual pressure

A

Takeoff and landing with cabin unpressurized

178
Q

What are the cabin press

Max diff and emergency pressure relief

A

Max diff 8.07

Max emergency relief 8.32

179
Q

What are the MD-82 weights

A

Max ramp. 150,500
Takeoff. 149,500
Max landing 130,000
Max zero fuel 122,000

179
Q

What is turbulence penetrate speed

A

275 to 285 or .75 to .79 m
Which ever lower.
Below 10k 250 or min man speed whichever higher

Dc-9/md-80 (13 decks)

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