Limitations Flashcards
1
Q
What is the maximum operation alt of the MD-80
A
37,000 feet
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
3
Q
What is the maximum tailwind for the MD-80
A
10 knots
4
Q
What is the maximum cross wind dry runway
A
30knots
5
Q
What is the maximum cross wind limitations in manual or restricted rudder
A
12 knots
6
Q
What is the maximum crosswind limitation with poor braking
A
10knots
7
Q
What is the maximum cross wind limitations runway less the 150 feet wide
A
10 knots landing only
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
9
Q
Does the company allow ops in NIL braking
A
No, idle thrust is more than braking capability
10
Q
What is Vmo/Mmo
A
340 KIAs sL to 27,300
Than .84m above 27,300
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
12
Q
What is the minimum altitude to engage the AP after TO
A
500’ AGL
13
Q
What is the minimum altitude for AP use during app
A
IMC -50 feet below MDA/ DA
VMC 50 feet above TDZ
14
Q
What situation required AT
Disconnect
A
If engine surge or stall detected during TO
15
Q
What is AC power distribution volts/amps limit and normal
A
115 volts +- 8 VAC limit
115 volts +-3 VAC normal
16
Q
What is the engine Generating max loads
A
Peak > 1.5 (5s)
Max 1.5 (5min)
Max continues 1.0
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
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
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
20
Q
What is the external power limits
A
Same S gen
21
Q
Do not reset following CBS
A
Batt charger Aux. hydraulic pump Fuel Quantity Fuel gags LAvatory flush motor
22
Q
What is the max limit for slats out mid/ flaps 0
A
280kias/.57mach
23
Q
What is the speed limit;
Slats mid/. Flaps 11 degrees
A
280/.57mach
24
Q
What is the speed limit for: slats full, flaps 15 degrees
A
240kias/.57mach
25
What is the speed limit for: slats full/ flaps /28 degrees
200 kias/.57m
26
What is the speed limit for: slats full, flaps 40degrees
195 KIAs/.57m
27
What flap settings are prohibited
Between 13-15 degrees
28
What are the speed brake limitations
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.
29
Can the gear be extended while speed brakes are deployed
No
30
What is min fuel for GA
500 Lbs
31
What is the max fuel imbalance wing tanker
1500 lbs
32
What is the max permissible aux fuel tank imbalance
400 lbs
33
What is the max fuel capacity combined
46,800 lbs
34
What is max ctr tank loading
21,000 lbs
35
When must engine anti-ice system be turned on
Taxi and takeoff in visible moisture at 5degress c or less
36
What temp/ dew point spread constitutes visible moisture
Spread of 3 degrees or less
37
If AF icing conditions are anticipated or encountered after dep. when can you turn on ice protection
Atengine failure cleanup alt.
38
Above what temp is it prohibited to use AF ice protection
10 degrees c
39
Engine and AF ice protection must be turned on during fight when RAT IS READING BETWEEN
?
40
When should tail deuce be activated
1. 1minute prior to sel landing flaps
2 at least every 20 minutes
3 after leaving icing prior to turning AF anti ice off
41
Take off my borne accomplished unless visual check ofupper wingsurface and wing is clear of ice when:
A. If ice on lower wing or either wingon pre flight
| B. Ambient temp below 15 degrees and high humidity or visible moisture
42
Define visible moisture
Rain, snow fog, drizzle, sleet, ice crystals or temp dewy spread of 3 degrees or less
43
When does the upper wing inspection apply
A. It sppplies regardless of whether or not the overwing ice protection detect system is installed operable or inoperable
44
What are the brake temp limits
A. Maximum for setting 300
B. Maximum for TO 205
Overheat lt on >305
Off <260
45
What are the gear speeds
VLE/extended 300/.70m
| VRet 250 knots/.70m
46
What is maximum tire speed
195 knots ground speed
47
What is the limitation for use ofAPU air
APU air switch must be off for all inflight operations
48
What is the the maximum altitude for APU usage
35,000 feet
49
What are the APU EGT limits
Starting. 760 degrees c
30s
Trans load 732 degrees
Continuous. 710
50
What is the maximum APU
| Rotor speed
110 percent
51
What general precautions
| Observed for APU ops
1 APU air switch off for al inflt ops
2. When starting engine w APU air AC supply switches must be off
3. Maximum altitude for APU use is Fl35
52
What is the APU starter duty cycle
```
1. 90s
R. 5m
2. 90s
R. 5m
3. 90s
R.60min
```
53
What will happen to the WAGS during sustaining banks greater than 15 degrees
Desensitized and alerts will be delayed
54
What mode does the charger have to be in prior to takeoff
Pulse mode
55
What are the approved fuels for the MD-80
Jet a and a1
56
If using TO flex mode what must be off
ART system
57
What is the maximum ground starting EGT for the engines
475 c
58
What is the starting EGT for the engines in flight
625 c
59
What is the ground idle maximums EGT of the engines if air bleed or power is being extracted
480 c
60
What are the ignition limitations
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
61
What is min oil pressure for flight
40 psi
62
What is normal Oil Pressure
40-55 psi
63
What are the engine oil temp limitations
Cont less than 135
| 15 minutes 135-165
64
What is the n1 limits
Max Cont. 101.6
Max TO. 101.6
Normal. 219 98.8
65
N2 limits
Max cont 102.5
Max TO 102.5
Normal TO thrust. 100.9
66
What is the wing span of the MD-80?
107'10"
67
What is the length of the MD-80?
148feet
68
What is the tail height of the MD-80?
30 feet
69
What is the wheel base of the MD-80
17 feet
70
What is the turning radius of the MD-80?
95 feet
71
What precautions must be noted for the cargo door?
Shall not be operated or left open in winds of 45 or greater
72
What is the runway slope max gradient for TO
1.7 to -2.0 percent
73
What is the runway slope max gradient for landing
2.0 to -2.0 percent
74
What is the max TO and landing altitude
8,500 feet
75
What is the minimum takeoff and landing altitude
-1,000ft
76
What is the maximum TO and landing temp below 2,525 feet
+50 degrees centigrade
77
Maximum TO and landing altitude above 2525 to 8500 feet
STD ISA +40 degrees centigrade
78
What is the minimum TO and landing temp
-54 degrees centigrade
79
Max enroute temp
STD +35
80
Minimum enroute temp
-76 degrees centigrade
81
What is the main fuel tank capacity
9200 lbs
82
What is the Aux fuel tank capacity
3700 lbs
83
What is the wing landing light max extend speeds
340 below 27,300
Or.84 Mach
Company 250 KIAS
84
What is the minimum battery voltage for start
25 volts
85
What is the battery charging voltage
26 to 39 volts
86
What is the maximum battery charging amp limits
0-65 amps to left
87
With emergency power on
| What is the maximum amp draw
10-50 to right
88
What is the gen/APU/ external power freq. limits
400 cycles +\-20
89
What are the battery charging modes
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
What are the engine EGT limits for TO and GA
625 for 5 minutes
| 630 for 2 minutes
91
What is the the EGT limit for Maximum continuous thrust MCT
580
92
What is the overall length of the MD-80
147 feet 10 inches
93
What is the wing span of the MD-80
107' 10"
94
What is the turn radius of the MD-80
94'3"
95
What three doors are non-plug type
Crew stairs, cargo and aft air stair
96
What are the non-disable lights on the crew alerting panel
Doors and master Warnings
97
What light is non Mel able
Anti collision light
98
How many battery packs for the emergency lights
Many
99
What kind of switch is the emergency light switch
A disagreement light
100
What approach category does the md-82 fall under
C for approaches
| D for circling
101
What approach category does the MX-83 fall under
C for flaps 40
| And D for flaps 28 and circling
102
How much life does the EFB have to have to start a trip
Min 80/
103
What is the green disk for located under the FO window
Green blow out disk for thermal relief of O2 bottle
104
What bus are bugged for take off
V1,v2, flap ret, slat Rey
105
How long is the airport analysis good for
48 hours
106
Does TAws show man made obstacles
No
107
What is proximate traffic
6 miles- blue
108
What is a TA
20 to48s yellow
109
What is an RA
15-35s- Red
110
When does the stall shacker activate
10 percent of stall
111
Are the forward strakes heated
Yes
112
What should you varify with the lower cargo doors
Make sure compartment is empty
113
What docs are in the aircraft manual
?
114
What precautions should you take to disconnect ground power
Make sure it is off first
115
How many battery are there
2 14volt DC
116
What is unique about the emergency inverter
It is single phase AC
117
Will the APU crosstie in flight
Yes but not on ground
118
If you are on Emergency power, will the batteries still be charged
No
119
Can you get Energency power with the battery switch off
Yes
120
What is the amber arc. On the CSD
11.2
121
What is the minimum speed for app with restricted rudder illuminated
135 knots
122
What PSI does the inlet fuel pressure low light go on
5psi
123
What PSID will the filter pressure drop illuminate (fuel)
5 PSID across the filter
124
Is there a fuel tank temp gage
No
125
What if you turn fuel heat on and get no fuel temp rise what happened
Low pressure pump failed
126
What bleed source does fuel hear use
13th stage bleed
127
How is the engine oil pump driven
N2 spool
128
When will the oil dtrain clog light illuminate
35 PSID across the filter
129
When will engine oil low presssure light illuminates
35 PSI
130
What is maximum thrust for the JT 8D-219 engine
21700 lbs
131
What is normal thrust of the -219 engine
21000
132
What is max cont thrust of the -219 engine
18900
133
When will the ART fire
W wind shear
A ART computer failure
F FGCP failure or switch
T thrust diff of 30 N1
134
How much thrust will be diverted by the buckets
40 percent
135
When will the RAmAPU door open
95 percent of APU
136
What will cause the APU to auto shut down
?less than 2 psi oil
110 percent
APU fire light
137
What is the allowable fuel density range
6.3 lbs to 7.1 lbs per gallon
138
What fuel press is the D.C. Fuel pump
10 PSI
139
What is minimum fuel for dispatch?
7500 lbs minimum
140
What is the fire detection limitation (cargo)
Airplane must land with 60 minutes of discharge of bottle 1
141
What does pulling fire handle do
```
Silence the bell
H Hydraulics reservoir
A. Pneumatic mech
L. Elect GCR
F. Fuel at wing root
Allows to rotate handle
```
142
What is the tail ice icing cycle
150 seconds
143
What is the starter standard duty cycles
90s on
5 m off
30s
5m offthen repeat
144
What is the alternate starter duty cycles
```
90s
10min off
60s
10min off
Then continue
```
145
How much reverse thrust is diverted?
40 percent
146
When will the APU RAM door open
95 percent
147
When does the APU low oil light illuminate
35 PSI
148
What are the three things that will automatically shut the APU down
Oil p less the 2
APU fire light
110 percent overspeed
149
What fuel pressure does the D.C. Fuel pump provide
10 psi
150
What buss has fire detect and protect on it
D.C. Transfer bus
151
How many lights will you get during the fire test
14
152
What powers the pneumatic augment valves
| And what happens it they depower
Normal D.C. Fail closed
153
What temperature activates the tail compart
| Temp hi warning light
180 f
154
Where are the three places that temperature is sense in the PAC
Turbine inlet
Compressor outlet
Mixing chamber
155
When will the PACS auto shutdown in auto mode
Engine failure
| GA
156
What activates the the cabin Alt warning light
9,500 -10000 foot cabin
| 9 sec aural then silent
157
How are the brakes cooled inflight
A brake cooling inlet
158
What does the ground shift mechanism do
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
What will auto shut down the PAC
Switch in auto
70 psi difference in 13 th stage bleed air
Only operates at cabin diff of 1.3 psi
160
When does the Pic have to submit a captains irregularity report to the DOM
Total vertical error if 300 ft
Altimetry system error of 245 or more
Assigned altitude deviation of 300 ft or more
161
What arms the ART system
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
What turns light on ART
N1 past 64 percent
163
When will ART fire
Wind shear
ART computers malf
Flight guidance malf
T 30 percent diff N 1
164
What perameters does
| The ATR system look at
AT engaged
B. Below ga epr
A. Above 350 RA
T o pitch TOTO
165
When will ATR activate
.25 epr difference
7 percent N 1 difference
V speed less than 0 for 5 seconds
Exit by selecting new vertical mode
166
What will shut down the
| Hydraulic transfer pump
Less than 1.3 qts in
| Reservoir
167
Where are the hydraulic accumulators located
Rudder for gear up damping
Thrust reverser s 2
Brakes 2
Elevator August
168
When will the hydraulic
| Low pressure light illuminate
900 psi
169
If hydraulic pumps fail what position do they fail electric failure
Aux pump fails off
Normal pump fail -hi
Transfer fail in position
170
How does the gear work
Free fall
Duplicate micro switch
Normal lights
Gear door drags
171
How are the brakes cooled in flight
Cooling inlet
172
How many brake actuators or there
8. 4 left
| 4 right
173
How many fuse plugs
3
174
Where are the transducer s located brakes
On wheel hubs
175
Do you have auto skid in
| Emergency power
No
176
When will wheel not turning light illuminate
20 percent difference
177
What must be done when using manual pressure
Takeoff and landing with cabin unpressurized
178
What are the cabin press
| Max diff and emergency pressure relief
Max diff 8.07
| Max emergency relief 8.32
179
What are the MD-82 weights
Max ramp. 150,500
Takeoff. 149,500
Max landing 130,000
Max zero fuel 122,000
179
What is turbulence penetrate speed
275 to 285 or .75 to .79 m
Which ever lower.
Below 10k 250 or min man speed whichever higher
