General + Limitations Flashcards
(146 cards)
1
Q
Length and width
A
22.670m x 24.572m (72 - 27m x 27m)
2
Q
Flaps position
A
0, 15, 25, 35 (72 - 0, 15, 30)
3
Q
FLAPS UNLK
A
untimely retraction 3 deg or more (72 - 4 deg)
4
Q
VMO clacker operates when VFE exceeds
A
15 deg - 180 kt
25 deg - 160 kt
35 deg - 150 kt
(72 - 15 deg - 185 kt
- 30 deg - 150 kt)
5
Q
Max fuel quantity
A
4500 kg (72 - 5000 kg)
6
Q
Max fuel quantity per wing
A
2250 kg (72 - 2500 kg)
7
Q
Electric pump off and on, when ?
A
over 8.5 PSI - off
under 5 PSI - on
(72 - the same)
8
Q
Fuel LO LVL
A
160 kg (72 - the same)
9
Q
Hyd normal level
A
9.35 L / max 9.6 L - min 8.5 L
72 - the same
10
Q
Hyd low level
A
under 2.5 L (72 - the same)
!!! In case of LO LEVEL alert the cross feed valve is inhibited or closes automatically if it was open !!!
11
Q
Hyd level for each system (blue/green)
A
4 L (72 - the same)
12
Q
Take off rating
A
2160 SHP (72 - 2475 SHP) !!! 0.9 x max take off rating !!!
13
Q
Reserve take off rating (RTO)
A
2400 SHP (72 - 2750)
14
Q
Blade angle operating range
A
- 14 deg (reverse) and + 78.5 deg (feather)
72 - the same
15
Q
Power corresponding to the mode selected (PWR MGT)
A
42 TO = 2160 SHP MCT = 2400 SHP RTO = 2400 SHP CLB = 2160 SHP CRZ = 2132 SHP
72 TO = 2475 SHP MCT = 2500 SHP RTO = 2750 SHP CLB = 2192 SHP CRZ = 2132 SHP
16
Q
PAX
A
48 (72 - 68 PAX)
17
Q
Weight
A
RAMP = 18770 KG (72 - 22970 KG) TAKE-OFF = 18600 KG (72 - 22800 KG) LANDING = 18300 KG (72 - 22350 KG) ZFW = 16700 KG (72 - 20800 KG)
18
Q
VMO/MMO
A
250 KT/ 0.55M (72 - same)
19
Q
VA
A
160 kt (72 - 175 kt)
20
Q
VFE
A
42 - 15 deg - 180 kt
25 deg - 160 kt
35 deg - 150 kt
72 - 15 deg - 185 kt
30 deg - 150 kt
21
Q
VLE
A
VLO - 180 kt 72 - VLO - 185 kt
VLO RET - 160 kt same
VLO LOW - 170 kt same
22
Q
VRA
A
180 kt (72 - same)
23
Q
VWO
A
160 kt (72 - same)
24
Q
Max tyre speed
A
165 kt (72 - same) GS
25
RTO TQ
100% (72 - same)
26
TO TQ
90% (72 - same)
27
MCT TQ
100% (72 - 90.9%)
28
Max fuel unbalance
550 kg (72 - 730 kg)
29
Max speed CRZ
304 kt (72 - 275 kt)
30
Compared with the 72, which items are not inhibited on the CAP
FLT CTRL and ENG
31
Trim green band
+4.5 to -1.5 (72 - +2.5 to 0)
32
Speed at which the extension of the flaps is inhibited
195 kt (72 - the same)
33
Refueling
Leading edge right wing (72 - LG bay, right side)
34
Brakes
Steel (72 - carbon)
35
Wind limitations
15 kt tail, 30 kt cross
36
Wind limitations (LVO)
10 kt tail/ 15 kt cross/ 15 kt head
| 72 - 10 kt tail/ 15 kt cross/ 30 kt head
37
ATPCS conditions
the same as 72 (PWR MGT TO, PL > 49 deg, TQ > 46%, ATPCS pb ON), except TQ > 53 %
38
Climb speed
160 kt (72 - 170 kt)
39
In GA, when is flaps 15 selected?
VGA + 15 or white bug, whichever is less
40
TQ =...
P/NP
41
ATPCS triggering condition
One TQ under 18% - 72
| One TQ under 21% - 42
42
Fuel temperature dial values
```
Red lines: -54, 57 deg
Yellow sectors:
-54 to 0 deg
50 to 57 deg
Green sector:
0 to 50 deg
```
43
Fuel tank temperature. Where is the probe located?
Left feeder tank
44
Lights and electricity
Beacon,NAV,logo /
Taxi and TO,Land,strobe/
Wing
- SVCE BUS
- ACW BUS
- DC BUS
45
DSPL knob, activation and light for....
All digit lighting
46
PNL rotary selector, lighting and intensity for...
Glareshield, pedestal and overhead panels instrument
47
TLU
180/185kt 72
| 190/195kt 42
48
High speed climb speed
190kt - both
49
GND HNDLG BUS is disconnected when...
Airborne
50
DC UNDV
STBY BUS under 19.5V
51
BAT OVRD toggle switch
Overrides all protection, ensuring the busses are supplied from their respective battery
52
OVRD P/B
Transfers DC STBY BUS and AC STBY BUS from HOT MAIN BAT BUS to HOT EMER BAT BUS
53
O2 PAX supply on. How many PAX
25% - both
54
If cockpit O2 bottle is under ...PSI use table
1400 PSI
55
PITCH TRIM ASYM
Pitch tabs desynchronization greater than 0.7 deg
56
RA between
-20 and 2500ft
57
"Five hundred" callout
During a non-precision approach or if the aircraft is outside the +/- 2 dots GS deviation
58
"Minimum" callout
If the aicraft has the LG extended when passing through the selected decision height
59
In what mode is the radar on ground?
STBY and can be activated by pressing STAB 4 times in 3 seconds
60
Vapp=...
Vref+wind factor
61
Taxi fuel, 14kg corresponds in average to...
2 min taxi
62
Hotel mode consumption is...
110 kg/hr
63
DOI..
0 - at 25% MAC
negative - in front of MAC
positive - after MAC
64
Cargo
Front right - 480kg
Front left - 448kg
Aft - 466kg aft + 300kg fwd
65
Which are the only doors monitored through the MFC?
FWD COMPT, CARGO and EMER
66
NAV lights....
Right - green
| Left - red
67
NAV lights coverage
Wings 110 deg, tail 140 deg
68
EMER EXIT LIGHTS...
- ON when DC STBY BUS under 18v or both generators lost
| - OFF when DC STBY BUS above 20v and at least one generator is running
69
The packs supply...
Lef pack - cabin and cockpit
Right pack - cabin only
! If one pack is inoperative, the other one supplies both compartments through the mixing chamber !
70
Landing elevation on AUTO PRESS is from...
-1500ft to 10000ft
71
AUTO PRESS DESCENT RATE...
Normal - 400ft/min
| Fast - 500ft/min
72
GUIDANCE (left side)...
Illuminates amber if CAT II conditions are lost or if an excessive deviation is detected
73
VHF communications is between 118.00 and 136.975 MHz and has a spacing of...
8.33KHz
74
Batteries
Main Ni-Cd 24V and 43Ah
| Emer Ni-Cd 24V and 15Ah
75
How many buses are there in the electrical network?
11
- DC BUS 1 and 2
- HOT MAIN BAT and HOT EMER BAT
- UTLY BUS 1 and 2
- DC SVCE BUS
- GND HDLG BUS
76
O2 cylinder capacity...
2180 l
77
ADC sw allows...
To feed both EEC, TAT/SAT/TAS indicator and GPS from ADC 1 or 2
78
ADC FAULT illuminates if...
The switch doesn't match the selection
79
RMI
CAPT - DC BUS 2
| FO - DC STBY BUS
80
Complete refueling in about...
16 min
81
The LP VALVE is controlled by the associated....
Fire handle
82
ICING AOA LT illuminates as soon as ...
One horn is activated
83
Wipers speed ...
- slow 80/min
| - fast 130/min
84
Exciters
- 2, A and B for each engine powered by the DC ESS BUS
| - each has two spark igniters (first 25s 5-6 sparks/s, then 1 spark/s)
85
Maximum runway slope and minimum width
- +/-2 deg
| - 30m
86
ONLY AT75:
- PL in RAMP, the TQ may go up to...
- PL in WALL, TQ may go up to...
- 100% and exceed, but not above 106.3%
| - 115%
87
In ICING conditions NP must not go below...
82%
88
Starter limitations
3 starts in 1min and 30 sec, total combined time, followed by 4 min off
89
Maximum value for TQ, time limit and when...
- AT 75: 120%, for 20s, in transient
| - AT 45: 137.5% for 20s, in transient
90
BRK TEMP
150 deg - 72
| 160 deg - 42
91
NAC OVHT
Over 170 deg
92
DUMP function is only available in ...
AUTO MODE
93
Maximum bank angle with AP on is....
- LO 15deg
| - HI 27deg
94
GND HDLG BUS is active and the battery discharges, even if it's not selected on, when...
- the passenger door is open or,
- cargo control door is open or,
- refueling control door is open
95
ITT
- 715 Hotel Mode ENG 2
- 765 Take Off (5 MIN)
- 800 MCT, RTO (10 MIN) - UPTRIM CONDITION
- 800 - 840 (MAX 20 SEC)
- 840 - 950 (START, MAX 5 SEC)
96
Aviation electricity
115V / 400Hz
97
Gust lock on when speed is....
40KT
98
When does the TOD distance appears on the GNSS?
When you are 200NM inbound of the airport
99
What happens with the flood light in the glareshield region when the storm light is on?
It stays off
100
When putting the battery sw ON, MFC 1A and 2A will flash if....
The cargo door is closed, otherwise, only MFC 1B and 2B will flash
101
Engine fire handle pulled, activates the following:
- propeller on feather
- fuel: LP valve closed
- air: BLEED and HP VALVE closed
- electric: DC and ACW GEN OFF
- deice: deice and shut off valve closed
- SQUIBS armed, light illuminates
+ HUD PROP BRAKE closed on ENG NO 2
102
PROP BREAK READY light conditions:
- A/C on ground
- fire handle not pulled
- gust lock engaged
- CL on FTR or FUEL S/O
- BLUE HYD pressure over 2100 PSI
103
Comparing AHRS FAIL and EFIS COMP, in which case will the AP disconnect:
EFIS COMP
104
How to recognize SGU FAIL
"X" appears on one screen, or both screens fail. We must move the SGU on the other side.
- "X" HDG and ATT
- FAIL flag on RMI
- AHRS 1 - EFIS 1, RMI 2
- AHRS 2 - EFIS 2, RMI 1
105
How to recognize CRT FAIL
Only ONE (!!!) screen fails
106
In case of EEC FAULT on ground, the PL's must be above GI position because ...
If the NP drops below 66% we will lose ACW
107
"DISCHARGE" will light up when ...
The fire extinguisher bottle is empty
108
The fire is considered extinguished when ...
The FIRE HANDLE turns off
109
"SQUIB" appears and are armed when ...
The FIRE HANDLE is pulled
110
DRIFT DOWN procedure, in case of SE OPS ...
- descend till the SE GROSS CEILING (normal or icing conditions)
- OBSTACLE: descend with white bug + flaps 15 deg
- NO OBSTACLE: descend with 200 kt until we reach a VS of 500 FT/MIN and stop the descent at approximately FL 80
111
Use of a weak GPU
If we have a voltage under 28 V we verify if it's above 26 V. If it's not above 26 V, we must SHED the consumers, if it's still under 26 V, we remove the GPU and start the engine on BATTERIES.
112
GREEN HYD FAULT "LO PR"
- LG
- normal braking
- after take off, T/O INHI won't cancel by itself, we must press RCL pushbutton
113
RAPID and EXPLOSIVE DECOMPRESSION descent speeds:
- RAPID: VMO - 10 kt
| - EXPLOSIVE: our current speed
114
TQ percentage in procedure (horizontal flight) and during approach:
```
In procedure
- 45% (2 ENG)
- 75% - 80% (1 ENG)
Approach
- 25% (2 ENG)
- 50% (1 ENG)
```
115
At MINIMUMS during a NON PRECISION approach the ADU must be put on ...
"STBY" (FD bars OFF), because it is considered that we have the runway in sight.
116
Emergency battery duration ...
30 min
117
AUX HYD PUMP activation
- one engine running
- PROP BRAKE OFF
- BLUE HYD SYSTEM pressure under 1500 PSI
- LDG down
118
VLO (185 kt/ 180 kt) is larger than V retraction (160 kt) and V lowering (170 kt) because ...
After the LDG is down, the doors will close, which means we can fly at a higher speed compared to V retraction and V lowering
119
The buttons on the overhead panel that have a yellow contour are used in case of ....
SMOKE
120
PROP DE-ICE, mode of operation ...
The blades are heated in sequence:
- 1-3-5
- 2-4-6
!!! "FAULT" sign will alternate ON and OFF only if one of the series doesn't work, if "FAULT" stays ON it means that the heating isn't working on any of the blades !!!
121
TCAS RA ...
- CLIMB: MCT, CL 100% OVRD
| - RADIO: "TCAS RA" and when it's the case, "CLEAR OF CONFLICT"
122
APM
- "CRUISE SPEED"
- "DEGRADED PERFORMANCE"
- "INCREASE SPEED"
- No action
- Checklist
- Severe icing
123
DADC ...
Digital Air Data Computer
124
- LO BANK
| - HI BANK
- 15 deg
| - 27 deg
125
Manual AP disengaged can be done by:
- force on the pedals
- force on the control wheel
- over 10 daN
| - over 30 daN
126
The altitude alert signals consist of a visual alert (amber light located on each of the two altimeters) which illuminates when the altitude is between ... and and aural "C" chord signal of ... duration which appears ...
- H + 250 FT and H + 1000 FT AND;
H - 250 FT and H - 1000 FT
- 0.75 s; every time the aircraft pases through one of those zone
127
RADIO MAGNETIC INDICATOR (RMI)
Is coupled to the opposite AHRS with a compass rose, showing magnetic heading, two pointers.
128
Minimum height for AP engagement after take off is ...
100 FT
129
Minimum height for use of either AP or FD:
- except during take off or executing an approach ...
- VS or IAS mode during approach ...
- CAT I approach ...
- CAT II approach ...
- 1000 FT
- 160 FT
- 160 FT
- 80 FT
130
NON PRECISION APPROACH - use of AP is recommended with:
- NAV mode ...
- HDG mode ...
- VS or IAS mode ...
- VOR
- NDB
- descent
131
Avoid PROP BRAKE immobilization when the temperature is below ... for a prolonged period of time.
- 20 deg
132
Avoid PARKING BRAKE engagement in wet conditions, when the temperature is below ...
- 5 deg
133
Maximum fuel unbalance during single engine operation is ...
200 kg
134
EXCESSIVE ITT DURING STARTALERTA hot start may be recognized by :
- - Rapid ITT increase,
- - NH slow increase,
- - Exhaust flames may be reported by ground crew.
135
An engine flame out may be recognized by:
- - sudden dissymmetry
- - TQ decrease
- - rapid ITT decrease
136
ENG OIL LO PR ALERT
Oil pressure drops below 40 PSI
137
FUEL ABNORMAL TEMP
- too high (>50_C)
- too low (<0_C)
- - Fuel is heated through a FUEL/OIL heat exchanger. Increasing fuel flow may reduce the fuel temperature.
- - Rapid throttle movement with high temperature fuel may cause surge or flame out.
- - In case of too low temperature, anti icing additive is needed to prevent ice formation in the fuel supply system. Record it in the maintenance book.
138
FUEL LO LVL
- - After fuel pump is selected ON, feeder tank is full within 10 minutes.
- - The LO LVL alert for each side will be triggered by: the fuel remaining indicated on FQI, when it is less than 160 kg / 352 lb.. the secondary low level detection system, when feeder tank is not completely full.
- - In case of feeder jet pump malfunction, fuel quantity unusable in each fueltank is raised from 20 kg / 44 lb to 130 kg / 287 lb.
139
EFIS COMP
When the two AHRS disagree (6 degrees or more) on:
- pitch information, amber PIT message is displayed on both EADI
- roll information, amber ROL message is displayed on both EADI
- both pitch and roll information, amber ATT message is displayed on both EADI
- heading information, amber HDG message is displayed on both EADI
!!! EFIS COMP can be triggered on ground by local magnetic perturbations. When the aircraft moves away from the magnetic perturbations source, the fault should disappear quickly !!!
140
ADC FAULT
- - When ADC 1 is lost, ADC 2 is automatically selected to supply the pressurization digital controller. The baro correction is no longer available (ref 1013 mb) and landing field elevation must be set in terms of pressure altitude.
- - If both ADC are lost, only standby instruments are available: air data instruments have a red flag and AHRS have lost their TAS inputs. Pressurization has to be performed manually.
- - If the selected ADC is lost, FDAU does not receive inputs; bugs are not available on TQ indicators. Each engine uses their own source (if ADC 1 is the faulty selected ADC).
- - Ten seconds are necessary to recover bugs on TQ indicator after selection of the valid ADC.
141
FINAL APPROACH SPEED
VAPP = VmHB + WIND FACTOR
Wind factor :The highest of
-1/3 of the reported head wind velocity -- or
-the gust in full
142
A few faults appear only on the CAP (not locally), these are ...
PRKG BRK, GPWS FAULT, MAINT PNL
143
Some alerts are not processed by the MFCs, they are processed locally. These systems are ...
- ENG FIRE
- EXCESS CABIN DIFFERENTIAL PRESSURE
- EXCESS CABIN ALTITUDE
- NACELLE OVERHEAT (2)
- SMOKE
144
TAT/SAT information are valid only when ...
the engine (propeller unfeathered) corresponding to the selected ADC is running.
145
A standing takeoff shall be performed under any of the following conditions:
- TOW is near limiting RTOW for RWY length or obstacle;
- Visibility / RVR at or close to takeoff minimum;
- Contaminated RWY.
The aircraft must be lined up and brought to a stop. Before releasing the brakes, the engines must be accelerated by setting the PL’s just above FI detent.
146
PROP BRAKE unlock/ lock time ...
- 5 sec. to unlock
| - 10 sec. to lock
