Limitations Atr600 Flashcards
WHAT MANUAL DO YOU REFER TO FOR ALL LIMITATIONS INCLUDING FMS, RVAV, PERFORMANCE
OM 12
MAX OPERATING FL
25000 Ft
VA LIMIT LOAD FACTOR
GEAR FLAP RETRACT
+2.5 g to -1g
VA LIMIT LOAD FACTOR
GEAR AND/OR FLAP EXTENDED
+2.5g to 0g
CARGO DOOR OPERATIONS
XWind no more than 45kt
Silver airways has “……….” PAX SEATS
70
Ramp weight
51080
TAKEOFF WEIGHT
50705
Landing weight
49273
ZFW weight
46296
Is a tail stand required for pax boarding/disembarking
Yes
Om 12 reference for No Tail Stand
VMO/MMO
250K / .55
VA
175 K
VFE … FLAP 15
185k
VFE……. FLAP 30
150 k
VLE
Landing gear extended
185K
Vlo
Retraction
160K
Vlo
Extension
170k
Vwo
Wipers
160k
Max tire speed
165k
Vmcl
Control landing flap 15
98k
Vmcl
Landing approach Flap 30
98k
TAILWIND LIMIT
15k
Max rwy slope
+/- 2%
Max XWIND
TO/LANDING FLAP 30
35k
Reserve Takeoff
Time limit
10 min
Reserve takeoff TQ
100%
Reserve TAKEOFF ITT
800c
Reserve takeoff NH
103.2%
Reserve takeoff NP
101%
Reserve takeoff oil press
55-65
NORMAL TAKEOFF TIME LIMIT
5 min
NORMAL TAKEOFF TQ
90%
NORMAL TAKEOFF ITT
Oat????
NORMAL TAKEOFF NH
101.9%
Normal takeoff NP
101%
Normal takeoff oil pressure
55-65
MAX CONTINUOUS TIME
None
MAX CONTINUOUS TQ
90.9%
MAX CONTINUOUS ITT
800
MAX CONTINUOUS NH
103.2%
MAX CONTINUOUS NP
101%
MAX CONTINUOUS OIL PRESSURE
55-65
GROUND IDLE NH
66% minimum
GROUND IDLE OIL PRESSURE
40 minimum
HOTEL MODE ITT
715
HOTEL MODE OIL PRESSURE
55-65
TRANSIENT TIME LIMIT
20sec
TRANSIENT TQ
120%
TRANSIENT ITT
840c
TRANSIENT NH
106.4%
TRANSIENT NP
106%
TRANSIENT OIL PRESSURE
40-100
STARTING TIME LIMIT
5sec
STARTING ITT
950c
PROPELLER
RUN UP
Engine run up must be performed into the wind
PROPELLER STATIC OPS
Avoid static operations between 41.6% - 62.5%
PROPELLER FEATHER
Avoid operations in feather above 66.6% TQ
INFLIGHT NP BELOW …… IN ICING NOT PERMITTED
82%
IDLE GATE DEVICE
Override in flight prohibited
STARTER LIMITS
3 within 1 min 30 sec with combined operations
Followed by 4 mins OFF
OIL TYPE
PWA 521 type 2
FUEL prohibited
JP4
Jet b
Refueling MAX PRESSURE
50psi
USEABLE FUEL
5510 per side
MAX FUEL UNBALANCE
1609
MAX FUEL IMBALANCE .. single engine
440
PRESSURIZATION MAX DIFFERENTIAL
6.35 psi
PRESSURIZATION MAX NEGATIVE
-.5 psi
PRESSURIZATION MAX LANDING
.35 psi
PRESSURIZATION MAX OVBD VALVE
1 psi
PRESSURIZATION MAX ALTITUDE FOR ONE BLEED OPS
20000 feet
DC GEN MAX LOAD
400
600
800
DC GEN MAX LOAD TIME
400-none
600 - 2 min
800 - 8 sec
INVERTER MAX LOAD
500 VA
575 VA
750 VA
INVERTER MAX TIME
500 - None
575 - 30 min
750 - 5 min
ACW GENERATOR MAX LOAD
20 Kva
30 Kva
40 Kva
ACW GENERATOR MAX TIME
20 - none
30 - 5 min
40 - 5 sec
TRU MAX LOAD
60 a
90a
TRU MAX TIME
60 - none
90 - 5 min
Single DC GENERATOR OPS
IN FLIGHT
ISA +25
Single DC GENERATOR OPS
Flight level
Limited to FL200
LANDING GEAR NO SHARP TURNS..
With fully braked wheels
Max tire speed
165 kts
Tire overspeed
TIRES MUST BE REPLACED
MFC
TAKEOFF WITH MORE THAN 1 failed
PROHIBITED
Minimum height for autopilot engagement
100ft
Minimum height for AP use in single source configuration
- Below ________ AGL below ________ kts OR
- With _________ inoperative
Do not use AP/YD in single source configuration
- Below 1000’ AGL below 160 kts OR
- With stall warning inoperative
MINIMUM height for use of either autopilot or flight director
Except during takeoff or approach
1000 ft
MINIMUM height for use of either autopilot or flight director
VS, or IAS mode during approach
160 ft
MINIMUM height for use of either autopilot or flight director
CAT 1 App mode
160 ft
______ Ark or Radial line: _______ and ________ limits
Yellow Ark - _______Area
Green Ark - _______ Area
RED Ark or Radial line: MINIMUM and MAXIMUM limits
Yellow Ark - CAUTION Area
Green Ark - NORMAL Area
Holding with flaps ________ is PROHIBITED in icing (except single engine)
Holding with flaps EXTENDED is PROHIBITED in icing (except single engine)
Icing conditions
Atmospheric TAT
7 c
Icing detection lights ______ be operative prior to flight into ______ conditions at __________
Ice detector _______ be operative for flight into ________ Conditions
Icing detection lights MUST be operative prior to flight into ICING conditions at NIGHT
Ice detector MUST be operative for flight into ICING Conditions
TCAS must be turned TA only in the following cases
1 engine out ops
2 stick pusher/shaker failure
3 flight with landing gear down
TCAS must be turned STBY if requested by ATC