Fichas
Embraer 145 Limitations
Fichas del conjunto (77)
- 1This is an operational envelope question. What is the MINIMUM takeoff/landing altitude?(neg / -) 1000 feet
- 2This is an operational envelope question. What is the MAXIMUM takeoff/landing altitude?+ 8000 feet
- 3This is an operational envelope question. What is the maximum operating altitude?37,000 feet
- 4Airspeed question. What is VFE FLAPS 9?250 KIAS
- 5Airspeed question. What is VFE FLAPS 18/22?200 KIAS
- 6Airspeed question. What is VFE FLAPS 45?145 KIAS
- 7Airspeed question. What is Mmo?Mach 0.78
- 8Airspeed question. What is Vmo?250 KIAS to 8000 feet
320 KIAS above 10,000 feet - 9Airspeed question. What is VLO (extension)?250 KIAS
- 10Airspeed question. What is VLO (retraction)?200 KIAS
- 11Airspeed question. What is VLE?250 KIAS
- 12Max tailwind component for takeoff/landing.10 KIAS
- 13Max crosswind dry/wet runway.30 KIAS
- 14Airspeed question. What is Va?200 KIAS
- 15Airspeed question. What is turbulent air penetration below 10,000 feet?200 KIAS
- 16Airspeed question. What is turbulent air penetration above 10,000 feet?250 KIAS
or
Mach 0.63
whicher is lower - 17Max altitude for flap extension20,000 feet
- 18Airspeed question. Max airspeed for windshield wiper operation.170 KIAS
- 19Airspeed question. Max recommended airspeed to remove DV windows140 KIAS
- 20Airspeed question. Max airspeed after takeoff/during climb without trimming.160 KIAS
- 21Electrical question. Max load on main generator400 A
- 22Electrical question. Max load on APU generator up to 30,000 feet400 A
- 23Electrical question. Max load on APU generator ABOVE 30,000 feet300 A
- 24Electrical question. Max battery temp70 C
- 25Autopilot question. Minimum engagement height after takeoff500 feet
- 26Autopilot question. Autopilot coupled approaches approved down to...200 feet
- 27Autopilot question. Is descent below MDA on a non-precision approach with autopilot engaged allowed?No, it's prohibited
- 28Autopilot question. Is single engine go-around with autopilot engaged allowed?No, it's prohibited
- 29Maximum altitude with yaw damper disengaged35,000 feet
- 30Fuel Limitation. Min fuel tank temp.(- / neg) 40 C
- 31Fuel Limitation. Min fuel temp @ FCOC without icing inhibitor+ 4 C
- 32Engine Limitation AE 3007A1/3 - AE 3007A1P Min oil temp for starting(- / neg) 40 C
- 33Max differential pressure7.8 PSI
- 34Max differential overpressure8.1 PSI
- 35Max negative differential pressure(- / neg) 0.3 PSI
- 36Max fuel imbalance between wing tanks800 LBS
- 37Usable wing fuel per tank5717 LBS
- 38Max fuel tank temperature52 C
- 39Unusuable quantity per fuel tank (elec pump inop)365 LBS
- 40Unusuable fuel per tank39 LBS
- 41Auxiliary Power Unit T-62-T-40C14 Max altitude for start30,000 feet
- 42Auxiliary Power Unit T-62-T-40C14 Max operating altitude37,000 feet
- 43Auxiliary Power Unit T-62-T-40C14 Max rotor speed108 %
- 44Auxiliary Power Unit T-62-T-40C14 Rotor speed for automatic shutdown104 %
- 45Auxiliary Power Unit T-62-T-40C14 Minimum battery temp for start( - / neg ) 20 C
- 46Auxiliary Power Unit T-62-T-40C14 Cooling period between first three start attempts1 MIN OFF
- 47Auxiliary Power Unit T-62-T-40C14 Cooling period between two series of three start attempts30 MINS OFF
- 48Engine Limitation AE 3007A1/3 - AE 3007A1P Max N1100 %
- 49Engine Limitation AE 3007A1/3 - AE 3007A1P Max N2 (steady state)102.4 %
- 50Engine Limitation AE 3007A1/3 - AE 3007A1P Max ITT for start800 C
- 51Engine Limitation AE 3007A1/3 - AE 3007A1P Max continuous ITT901 C
- 52Engine Limitation AE 3007A1/3 - AE 3007A1P Max ITT takeoff and corresponding max time948 C
5 mins max - 53Engine Limitation AE 3007A1/3 - AE 3007A1P Min/max fuel temp- (neg) 40 / 52 C
- 54Engine Limitation AE 3007A1/3 - AE 3007A1P Engine cool down (i.e. condition prior to shutdown)1 MIN
at idle / taxi speed
before shutdown - 55Engine Limitation AE 3007A1/3 - AE 3007A1P Engine warm-up2 MIN for WARM ENGINE
4 MIN for COLD ENGINE - 56Engine Limitation AE 3007A1/3 - AE 3007A1P Engine considered cold when...shut down for more than
90 MINS - 57Ice & Rain protection question State 3 conditions for HOLDING in icing conditionsLanding gear UP
Flaps UP
Airspeed ... MIN 200 KIAS - 58Ice & Rain protection question Define icing conditions10 C or less
and
VISIBLE MOISTURE - 59Ice & Rain protection question MAX temp for anti-icing operation10 C
- 60Ice & Rain protection question MIN temp for manual anti-icing operation( - / neg ) 40 C
- 61Ice & Rain protection question Single Engine or Single Bleed Max Alt in icing conditions15,000 feet
- 62Ice & Rain protection question Can we use APU bleed as pneumatic source for anti-icing system?No
DO NOT USE - 63Engine Limitation AE 3007A1/3 - AE 3007A1P ENG Start limits (1st - 4th cycles)1 MIN ON, 1 MIN OFF
- 64Engine Limitation AE 3007A1/3 - AE 3007A1P ENG Start limits (5th cycle)1 MIN ON, 5 MIN OFF
- 65Engine Limitation AE 3007A1/3 - AE 3007A1P ENG Dry motoring ops5 MIN ON, 5 MIN OFF
- 66Auxiliary Power Unit T-62-T-40C14 Max EGT for start884 C
- 67Auxiliary Power Unit T-62-T-40C14 Max continuous EGT680 C
- 68Auxiliary Power Unit T-62-T-40C14 Max continuous EGT for 5 MINS MAX717 C
- 69Engine Limitation AE 3007A1/3 - AE 3007A1P MIN oil pressure below 88% N234 PSI
- 70Engine Limitation AE 3007A1/3 - AE 3007A1P MIN oil pressure above 88% N250 PSI
- 71Engine Limitation AE 3007A1/3 - AE 3007A1P MAX OIL PRESS (Steady state, temp > 21 C)95 PSI
- 72Engine Limitation AE 3007A1/3 - AE 3007A1P MAX OIL PRESS (Transient 5 MIN)110 PSI
- 73Engine Limitation AE 3007A1/3 - AE 3007A1P MIN OIL TEMP CONT OPS21 C
- 74Engine Limitation AE 3007A1/3 - AE 3007A1P MAX OIL TEMP CONT OPS126 C
- 75Engine Limitation AE 3007A1/3 - AE 3007A1P MIN OIL TEMP FOR N2 ABOVE 83%40 C
- 76Engine Limitation AE 3007A1/3 - AE 3007A1P Cold weather ops restrictionIdle RPM max
until press < 95 PSI - 77Engine Limitation AE 3007A1/3 - AE 3007A1P Min oil temp to increase N2 above 83% State 3 options40 C or;
run eng for 8 mins or;
static runup to 88% N2 and ensure oil pressure is equal or less than 83 PSI