SF34 Saab 340 Memory Items + Extras Flashcards
Covers all Ch 2 & Ch 5 as well as other "good to knows".
1
Q
What is the span without extended wingtips?
A
21.44m
2
Q
What is the span with extended wingtips?
A
22.75m
3
Q
What counts as icing conditions?
A
If any form of visible moisture is present (such as clouds, fog with visibility of one mile or less, rain, snow, sleet, ice crystals) or standing water, slush, or snow is present on the ramps, taxiways or runways and the OAT or SAT is +5 degrees and below during ground and flight operation.
Min speed must be observed if in above conditions or if ICE SPD light is on.
4
Q
When in icing conditions or whenever the blue ICE SPD status light or EAI is on, what should you do?
A
Must observe the minimum speed for flight in icing conditions. IAS mode must be selected on the FD if climbing when these conditions exist.
5
Q
When may flaps be extended?
A
On ground as required for take-off, low altitude holding, approach and landing, up to a maximum altitude of 14,000ft.
6
Q
Vfe for flap 7 or 15?
A
175 KIAS
7
Q
Vfe for flap 20?
A
165 KIAS
8
Q
Vfe for flap 35?
A
140 KIAS
9
Q
Maximum gear retraction speed (Vlor)?
A
150 KIAS
10
Q
Maximum gear extension speed (Vloe)?
A
200 KIAS
11
Q
Maximum gear emergency extension speed (Vloee)?
A
200 KIAS
12
Q
Maximum gear extended speed (Vle)?
A
200 KIAS
13
Q
Vmcl (Flaps 20 and 35) (SF340A)?
A
103 KIAS
14
Q
Vmcl (Flaps 20 and 35 (SF340B)?
A
106 KIAS
15
Q
Vmcl (Flaps 20 and 35) (SF340B(WT))?
A
103 KIAS
16
Q
What is Vmo (max. operating speed)?
A
250 KIAS up to approx. 16,000ft.
Above 16,000 ft, Vmo decreases as indicated by the Vmo pointer to approx. 210 KIAS at 25,000ft.
17
Q
What is Va (max. manoeuvring speed)?
A
180 KIAS
18
Q
What is Vra (max. rough air penetration speed)?
A
190 KIAS up to 21,000 ft ISA.
Above 21,000ft, reduce the speed as indicated by the VMO pointer minus 30 kts.
19
Q
Maximum take-off tailwind component?
A
10 kts
20
Q
Maximum landing tailwind component?
A
10 kts (15 kts with AFMS-54/55)
21
Q
Maximum operating altitude?
A
25,000 ft
22
Q
Maximum crosswind component?
A
35 kts
23
Q
Deviations from the ATC assigned altitude, is authorised only to the extent necessary to comply with an _____?
A
ACAS Resolution Advisory (RA)
24
Q
In relation to ACAS:
Manoeuvres must not be based solely on information presented on what?
A
The Traffic Advisory display (TA).
25
Use of flight director information in go-around mode during _______ is not authorised.
take-off
26
When are autopilot operations not authorised?
Below 200 ft AGL - during take-off or go-around.
Below 500 ft AGL - during cruise.
Below 50 ft AGL - during approach.
Below 100 ft AGL - for a non-coupled approach.
27
During icing conditions, which mode is the only vertical mode to be used during climb when ice accumulation is observed or if it is not certain there is no ice accumulation on the aircraft?
FD/AP IAS mode.
28
When is it a requirement to disconnect the autopilot and re-trim the aircraft before re-engaging the autopilot?
Following an engine failure.
29
When is Yaw Damper not authorised?
For take-off, go-around or landing.
30
When must landing flap be set by?
300 ft AGL
(Must be called for by 500 ft AGL)
31
If holding in icing conditions, what flap setting must be used?
Flap 0
32
In terms of placards and instrument markings, what does the colour red mean?
Operating limits.
33
In terms of placards and instrument markings, what does the colour yellow mean?
Caution, temporary or idle range.
34
In terms of placards and instrument markings, what does the colour green mean?
Normal operating range.
35
In the case of a cargo fire on a Saab 340B (WT) aircraft, how long has the cargo compartment been demonstrated to provide fire protection for?
60 minutes.
36
In the case of a cargo fire on a Rex aircraft that isn't a Saab 340 B (WT), how long has the cargo compartment been demonstrated to provide fire protection for?
35 minutes.
37
When the Altitude/Heading Reference System (AHRS) is initialising, can the aircraft be moved?
No.
38
Regarding AHRS - Fill in the blanks:
Take-off is not permitted until __1__ minutes after initialisation is completed and the attitude difference between the attitude displayed on both EADI's and the standby attitude indicator is __2__ degrees or less (bank and pitch) and the heading on the compass card is not ______3______.
1 - 2 minutes
2 - 3 degrees
3 - slewing away from the aircraft heading
39
Maximum Taxi Weight of the Saab 340B(WT)?
13,290 kg
40
Maximum Take-Off Weight of the Saab 340B(WT)?
13,155 kg
41
Maximum Landing Weight of the Saab 340 B(WT)?
12,930 kg
42
Maximum Zero Fuel Weight of the Saab 340B(WT)?
12,020 kg
43
Maximum Taxi Weight of the Saab 340A?
12,840 kg
44
Maximum Take-Off Weight of the Saab 340A?
12,700kg
45
Maximum Landing Weight of the Saab 340A?
12,340 kg
46
Maximum Zero Fuel Weight of the Saab 340A?
11,660 kg
47
Max. in flight differential pressure?
7.5 psi
48
Max. landing cabin differential pressure?
0.3 psi
49
At what cabin pressure does the CABIN PRESS warning trigger?
7.5 psi
50
At what cabin altitude does the CABIN PRESS warning trigger?
10,000 ft
51
Max. DC voltage of the DC generators?
29 V DC
52
Normal nominal load per DC generator?
400 A
53
Maximum load for 5 minutes for the DC generator?
600 A
54
Main battery normal voltage?
24 V DC
55
External power - GPU max. voltage?
29.5 V DC
56
External power - battery cart max. voltage?
29.5 V DC
57
Max. external power amperage requirement for normal operation?
600 A
58
Max. external power amperage requirement for engine start?
1,600 A
59
Minimum fuel takeoff, each tank?
135 kg
60
Maximum imbalance of fuel between tanks?
90 kg
61
Normal kg for LOW LEVEL light to come on?
135 kg (+/- 30kg)
62
In regards to Fuel: System Limitations - Fill in the blanks:
XFEED and CONN VALVE switches shall be in the __1__ and ___2___ position during take-off and landing in normal operation.
1 - OFF
2 - CLOSED
63
Total quantity of useable fuel?
2,542 kg (@ 0.79kg/l)
64
Minimum time in NORM before switching to HIGH in regards to windshield heating?
7 min
65
Time from switching STBY PITOT ON until full ice-protection is obtained?
5 min
66
Maximum speed for LOW windshield wiper operation?
130 kts
67
Maximum speed for HIGH windshield wiper operation?
160 kts
68
In regards to Altimeters, Operational Tolerances - Fill in the blanks:
With an accurate QNH set, all the altimeters should read the nominated elevation to within __1__ ft.
If an altimeter has an error in excess of +/- __2__ ft, it is considered unserviceable.
The Saab 340 requires ___3___ altimeters for IFR operations; __4__ of the altimeters must read the nominated elevation to within __5__ ft. When the remaining altimeter has an error between __6__ ft and __7__ ft, flight under the IFR to the first point of landing, where the accuracy of the altimeter can be rechecked, is approved. In the event that the altimeter shows an error in excess of __8__ ft on the second check the altimeter must be considered unservicable.
1 - 60
2 - 75
3 - all three
4 - two
5 - 60
6 - 60
7 - 75
8 - 60
69
Maximum difference between the two airspeed indicators?
+/- 8 KIAS
70
Number of brake applications on fully charged brake accumulators?
11
71
Max. speed for use of brakes with the anti-skid system off or inoperative?
40 kts
72
In take-off power + APR or go-around power operating conditions, what is the operating limit on TRQ (5 minutes)? (Saab 340 B Model)
107 %
73
In take-off power + APR or go-around power operating conditions, what is the operating limit on TRQ (2 minutes)? (Saab 340 B Model)
107 %
74
In take-off power + APR or go-around power operating conditions, what is the operating limit on ITT (5 minutes)? (Saab 340 B Model)
940 degrees C
75
In take-off power + APR or go-around power operating conditions, what is the operating limit on ITT (2 minutes)? (Saab 340 B Model)
950 degrees C
76
In take-off power + APR or go-around power operating conditions, what is the operating limit on PROP rpm (5 minutes)? (Saab 340 B Model)
1,396 rpm
77
In take-off power operating conditions, what is the operating limit on TRQ (5 minutes)? (Saab 340 B Model)
100 %
78
In take-off power operating conditions, what is the operating limit on TRQ (2 minutes)? (Saab 340 B Model)
100 %
79
In take-off power operating conditions, what is the operating limit on ITT (5 minutes)? (Saab 340 B Model)
917 degrees C
80
In take-off power operating conditions, what is the operating limit on ITT (2 minutes)? (Saab 340 B Model)
927 degrees C
81
In take-off power operating conditions, what is the operating limit on PROP rpm (5 minutes)? (Saab 340 B Model)
1,396 rpm
82
In Max. Continuous (OEI) operating conditions, what is the operating limit on maximum TRQ? (Saab 340 B Model)
100 %
83
In Max. Continuous (OEI) operating conditions, what is the operating limit on maximum ITT? (Saab 340 B Model)
944 degrees C
84
In Max. Continuous (OEI) operating conditions, what is the operating limit on PROP rpm? (Saab 340 B Model)
1,396 rpm
85
In transient except take-off (max 12 sec) operating conditions, what is the operating limit on max. TRQ? (Saab 340 B Model)
112 %
86
In transient except take-off (max 12 sec) operating conditions, what is the operating limit on max. ITT? (Saab 340 B Model)
965 degrees C
87
In transient except take-off (max 12 sec) operating conditions, what is the operating limit on max. PROP rpm? (Saab 340 B Model)
1, 572 rpm
88
In engine start operating conditions, what is the operating limit on maximum ITT? (Saab 340 B Model)
965 degrees C
89
In take-off power operating conditions, what is the operating limit on TRQ (5 minutes)? (Saab 340 A Model)
108 %
90
In take-off power operating conditions, what is the operating limit on ITT (5 minutes)? (Saab 340 A Model)
930 degrees C
91
In take-off power operating conditions, what is the operating limit on PROP rpm (5 minutes)? (Saab 340 A Model)
1,396 rpm
92
In transient except take-off (max 12 sec) operating conditions, what is the operating limit on max. TRQ? (Saab 340 A Model)
118 %
93
In transient except take-off (max 12 sec) operating conditions, what is the operating limit on max. ITT? (Saab 340 A Model)
960 degrees C
94
In transient except take-off (max 12 sec) operating conditions, what is the operating limit on max. PROP rpm? (Saab 340 A Model)
1,572 rpm
95
In Max. Continuous (OEI) operating conditions, what is the operating limit on TRQ? (Saab 340 A Model)
100 %
96
In Max. Continuous (OEI) operating conditions, what is the operating limit on ITT? (Saab 340 A Model)
917 degrees C
97
In Max. Continuous (OEI) operating conditions, what is the operating limit on PROP rpm? (Saab 340 A Model)
1,396 rpm
98
In engine start operating conditions, what is the operating limit on maximum ITT? (Saab 340 A Model)
960 degrees C
99
In regards to Miscellaneous Limitations: Power Levers - Fill in the blanks:
It is prohibited to move the power lever(s) below _____1_____ when airborne. If the PL is moved below _____2_____ when airborne the propeller will go into __3__ pitch angle, the propeller speed will ___4___ uncontrolled with extremely ___5___ drag, possible uncontrolled flight, engine shutdown and loss of engine power.
1 - FLIGHT IDLE
2 - flight idle
3 - low
4 - increase
5 - high
100
In regards to Start Duty Cycle - Fill in the blanks:
__1__ start attempts with __2__ minutes cooling between , then __3__ minutes cooling before subsequent starts.
1 - Two
2 - 3
3 - 25
101
In regards to Starter/Generator Duty Cycle Limits: Motoring - Fill in the blanks:
__1__ __2__ - second ventilations with __3__ minutes cooling between each, then a __-hour cooling period before subsequent starts or motoring.
1 - Three
2 - 30
3 - 3
4 - one
102
Maximum time to light-off (from initial Ng rotation to ITT rise) for direct start only?
20 seconds
103
Maximum time with the starter engaged and how long within that time can be plain motoring?
70 seconds of which max 30 seconds plain motoring
104
Memory Items: Starting - No Light Up, Start Sequence Interrupted, Hung Start or Hot Start
Condition Lever - Fuel Off
Ignition Switch - Off
Motor Engine to ITT Below 175 degrees or for a minimum 10 seconds.
105
Memory Items: Engine Failure After V1
Power - Reduce to 20% - 30%
Condition Lever - Fuel Off
Caution - If propeller has not feathered, ensure AUTOCOARSEN switch is off and set PROPELLER PUMP switch to MAN FEATHER. Hold the switch until the propeller is in the full-feathered position.
106
Memory Items: Engine Fire
Power Lever - Reduce to 20% - 30%
Condition Lever - Fuel Off
Fire Handle - Pull
Fire Extg. Switch - On
(If fire indication still on after 30 seconds - discharge FIRE EXTG. opposite side)
Caution - If propeller has not feathered, ensure AUTOCOARSEN switch is off and set PROPERLLER PUMP switch to MAN FEATHER. Hold the switch until propeller is in the full-feathered position.
107
Memory Items: Uncommanded Engine Operation In Flight
Power Lever - Reduce to 20% - 30% (if TRQ indication is lost or unreliable set PL half an inch (12mm approx.) above flight idle.
Condition Lever - T/M Then Reset Prop RPM
Autocoarsen - Off
108
Memory Items: Uncommanded Engine Operation On The Ground
Shut down the engine.
109
Memory Items: Engine Shut Down
Power Lever - Reduce to 20% - 30%
Condition Lever - Fuel Off
Note - If TEMP rises above 540 degrees, or if there is evidence of combustion after shut down, MOTOR engine until TEMP decreases below 175 degrees.
Caution - If propeller has not feathered, ensure AUTOCOARSEN switch is off and set PROPERLLER PUMP switch to MAN FEATHER. Hold switch until propeller is in the full-feathered position.
110
Memory Items: Compressor Stall
CTOT - Off
Power Lever - Reduce to 20% - 30%
111
Memory Items: Air Conditioning Smoke
Oxygen Masks and Regulators - On and 100%
Smoke Goggles - On
Communications - Establish
112
Memory Items: Avionics or Electrical Smoke or Fire
Oxygen Masks and Regulators - On and 100%
Smoke Goggles - On
Communications - Establish
113
Memory Items: Rapid Depressurisation
Oxygen Masks and Regulators - On and 100%
Communication - Establish
Transponder - 7700
Seat belt Sign - On
Emergency Descent - Initiate
114
Memory Items: Tail Pipe Hot
Power Lever (affected side) - Reduce to 20% - 30%
115
Memory Items: Cargo Compartment Smoke
Cargo Fire Extg. Switch (single extg)- On
Cargo Fire Extg. Switch 1 (dual extg)- On
Caution - For dual cargo extinguisher installations, select only extg. 1 intially. Refer to QRH for direction on use of extg. 2)
116
Memory Items: Hydraulic Light On
Hydraulic Pump Switch - Off
Check hydr indicatiors - Emerg and main pressures are both low.
LEAVE FLAPS IN ACTUAL POSITION (Caution)
Speed below 200 KIAS
Landing Gear Handle - Down
Emerg LDG Handle - Pull
117
Memory Items: Hydraulic Fluid Loss
Hydr Pump Switch - Off
118
Memory Items: Elevator/Aileron System Jammed
Autopilot - Disengage (be prepared for trim transients - elevator only)
Interconnect Unit - Overpower (both pilots shall act on the controls. The pilot on the side not failed can, by overpower the interconnect unit, control the aircraft.
Pitch/Roll Disconnect Handle - Pull
119
Memory Items: Flap Fault
Flaps split
(The split may be reduced by reselecting previous flap setting)
120
Memory Items: Emergency Evacuation - Captains Duty
Park Brake - Set
Condition Levers - Fuel Off
Evacuation - Order (F/A will automatically initiate an evacuation on water)
Tower/Company - Advise
Battery Switches - Both Off
Caution - Do not order an evacuation until both Ng's are below 20%
121
Memory Items: Evacuation Drills - FO's Duty
At the direction “EVACUATION DRILLS” from the Captain:
Emergency Panel Switches (3) - On
Fire Handles (Both) - Pull
Fire Extg. Switches (Both) - On
122
Memory Items: Both Engines Flame Out
Power Levers (Both) - Flight Idle
Condition Levers (Both) - Fuel Off
Airspeed - 130 KIAS
Battery Switches (Both) - OVRD
Fuel STBY Pump Switches (Both) - OVRD
Autocoarsen - Off
Left Condition Lever - Start
Start Switch - Left
IF ENGINE RESTARTS:
Left Condition Lever - Max
Left Power Lever - Advance
Left Gen Switch - Reset then On (maximum two reset attempts)
IF ENGINE DOES NOT RESTART:
Left Condition Lever - Fuel Off
(Attempt to start right engine commencing at item 7)
123
Memory Items: Loss of both generators
Bus Tie Switch - Split
Both Gen Switches - Reset then On (maximum two reset attempts for each generator)
124
Pressurisation: Cabin VS in detent going up?
+ 500 FPM
125
Pressurisation: Cabin VS in detent going down?
- 300 FPM
126
Normal Hydraulic Pump Pressure?
2100 - 2900 PSI
127
Climb Power ITT Limit B Model Below FL150?
Max 840 degrees C
128
Climb Power ITT Limit B Model At and Above FL150?
Max 875 degrees C
129
Climb Power ITT Limit A Model Below FL150?
Max 825 degrees C
130
Climb Power ITT Limit A Model At and Above FL150?
Max 850 degrees C
131
Minimum climb speed, flap 0, max bank 15 degrees?
V enroute
132
Minimum climb speed, flap 0, max bank 30 degrees?
V enroute + 10 KIAS
133
Minimum climb speed, flap 15, max bank 15 degrees?
V2
134
Minimum climb speed, flap 15, max bank 30?
V2 + 10 KIAS
135
Cat C Initial Approach Speeds?
160 - 240 KIAS
136
Cat C Final Approach Speeds?
115 - 160 KIAS
137
Cat C Max Speed for Circling?
180 KIAS
138
Cat C Max Speed for Missed Approach?
240 KIAS
139
Company Speeds for Initial Approach?
160 - 200 KIAS
140
Company Speeds for Final Approach?
V fa + 10 - 160 KIAS
141
Company Speeds for Circling?
160 - 180 KIAS
142
Company Speed for Missed Approach?
146 KIAS (V enroute + 10)
143
Circle to Land Configuration?
IAF - 170 KIAS
FAF - 160 KIAS
Approaching IAF (IF for RNAV), Condition Levers Max
Below 175 KIAS, Flap 15 (Flap 7 OEI)
Approaching FAF or established inbound, reduce speed to 160 KIAS and maintain until visual circling is commenced.
Established inbound, maintain a constant descent profile.
Gear down and Flap 20 once visual and established within circling area. (OEI established on Final descent for landing)
144
Straight-In Landing Configuration?
IAF at 170 KIAS
FAF at 160 KIAS
Approaching IAF (IF for RNAV), below 200 KIAS, select gear down and condition levers to max. Below 175 KIAS, Flap 15 (OEI Flap 7)
Approaching FAF or established inbound, slow to 160 KIAS and select Flap 20.
Reduce speed to V fa20 + 10 by the MDA/DA.
Flap 35 shall not be selected until crew are visual and established for a straight in landing.
Established inbound, maintains constant descent profile.
145
Vmm Flap 0?
150 KIAS
146
Vmm Flap 7?
145 KIAS
147
Vmm Flap 15?
140 KIAS
148
Vmm Flap 20?
135 KIAS
149
Vmm Flap 35?
130 KIAS
150
Name the four Vmm increments.
Turns Above 30 degrees AOB - 10 KIAS
Ice Accretion/Icing Conditions - 10 KIAS
Moderate Turbulence - 10 KIAS
Severe Turbulence - 15 KIAS
(Accumulative)
151
ILS Glideslope Check - Temp Above ISA will cause what?
Low altitude reading check
152
ILS Glideslope Check - Temp Below ISA will cause what?
High altitude reading check
153
Timing from threshold before base turn?
What actions are taken?
25 seconds.
Speed 160 - 180 KIAS, Gear Down, 600 Fpm descent
Condition Levers max
Below 175 KIAS, Flap 15
Below 165 KIAS, Flap 20
"Final Checklist"
Min 135 KIAS turn onto base
154
Maximum Compartment Load C1?
510 kgs
155
Maximum Compartment Load C2?
270 kgs
156
Flight planning groundspeed B Model?
270 TAS + Wind Component
157
Flight planning ground speed A Model?
250 TAS + Wind Component
158
Fuel burn rate B Model?
500 kg/hr
159
Fuel burn rate A Model?
450 kg/hr
160
Fuel Takeoff and Initial Climb allowance?
30 kgs
161
Fuel Final Climb allowance?
3 min plus 10kgs
162
Circuit and Landing allowance?
15 kgs
163
Instrument Approach Fuel?
100 kgs
(If an alternate is required due to weather, 2 approaches must be planned for at the destination)
164
Fixed reserve fuel?
Half an hour at 400 kg/hr
165
Holding Fuel A Model?
460 kg/hr
166
Holding fuel B Model?
450 kg/hr
167
Holding fuel WT?
440 kg/hr
168
Taxi fuel for capital cities or single engine turnarounds?
40 kg
169
Taxi fuel for outports?
25kg
170
The right RECIRC fan may be turned off with less than how many passengers in a B Model?
27 passengers.
171
The right RECIRC fan may be turned off with less than how many passengers in an A Model?
25 passengers.
172
Maximum ITT with HP BLEED VALVE open on the ground?
800 degrees C.
173
Max speed in a holding pattern up to FL140?
230 kts
174
Max speed in a holding pattern above FL140 up to FL200?
240 kts
175
Max speed in a holding pattern above FL200?
265 kts
176
Memory Items: Unreliable Airspeed and/or Altitude Indications
Autopilot - Disconnect
Flight Path - Stabilze
Power Setting - Initially maintain power and attitude
177
Max Ng for motoring?
26%
178
Minimum stabilised Ng prior to Condition Lever to START?
17%
179
Minimum Ng prior to Tailwind start?
20%
180
Wind tip sweep - B Model
32m
181
Wing tip sweep - WT
33.3m
182
Minimum pavement width to turn?
18m
183
Minimum runway width
30m
184
What length must the runway be in order to change your aiming point to further down the runway? What conditions must be met?
2400m
Must be a controlled aerodrome and briefed prior.
185
If operationally feasible, at what speed should you be out of reverse by? When must you select ground idle to achieve this?
50kts, selecting ground idle by 60kts.
186
At what weight in C1 and C2 is the pogo stick required for a SET? Is there any exception and if so, what is it?
300kg.
If there are no pax in row 11, this can be increased to 550kg.
187
When can a SET be conducted?
No other aircraft operating on the apron.
No persons other than REX ground agents on the apron.
No extreme weather conditions - vis greater than 3000m, wind below 25kts, no heavy precipitation or dust storms.
No greater than 10kts wind from the right side of the aircraft.
FO/Ground staff must be at the bottom of the stairs during disembarkation.
Paperwork can only be conducted with someone at the guard position.
Passengers must not cross the extended centreline of the aircraft onto the right side.
No passengers requiring assistance, infants or children including UM’s, passengers in custody.
After a heavy landing or excessive braking, must shut down to inspect landing gear and brakes.
188
Minimum GPU amperage for start?
1400 amps
189
When may a landing with up to 15kts downwind be conducted?
LDA >1800m
Runway aligned approach
Profile guidance (electronic or visual)
WT only + CPT only
-1000 - 6300ft aerodrome elevation (flap 20)
190
Increased MTOW Saab 340B?
13,605kg
191
Increased MTW Saab 340B?
13,740kg
192
Standard Male weight?
91kg
193
Standard Female weight?
76kg
194
Standard Child weight?
49kg
195
Standard Infant weight?
16kg
196
Standard Guide Dog weight?
36kg
197
Standard Adolescence weights (male & female)?
70kg (m) and 64kg (f)
198
Max temperature for take-off?
47 degrees
199
Min and max load factors (flaps retracted)?
+2.75 - -1.0
200
Min and max load factors (flaps extended)?
+2.0 - 0
201
Max roll trim tolerance for dispatch?
1/2 unit from neutral
202
Max speed for A/P or FD coupled Localiser intercept?
200 KIAS
203
When can you select APPR or NAV mode when intercepting a Localiser?
Within 2 dots on the EHSI
204
What density are the fuel figures in the FCOM based on and what density does the company elect to use for more typical Australian conditions?
0.802 kg/l - FCOM/AFM
0.79kg/l - Rex
205
During AHRS initialisation, what should not be operated to avoid voltage transients and subsequent initialisation errors?
Hydraulic pump
206
When can an ENG OIL PRESS warning be ignored?
If the warning can be cleared by moving the condition lever into the unfeather position
207
Tq tolerance to selected CTOT value?
+/- 2%
208
Max Tq diff. between indications with CTOT selected on?
3%
209
Allowable oil pressure fluctuations?
25-45 psi - 5 psi
46 - 140 psi - 10 psi
210
Allowable ITT fluctuation?
+/- 5 degrees
211
Theoretically, what should Prop RPM be reduced to when operating at Maximum Continuous Power?
1384 down from 1396.
(in practice I have never seen a crew do this in both sim and aircraft)
