ERJ 145 Limitations AFM and AOM

Max. Ramp Weight (MRW) LR Post-Mod. SB 145-00-0032. 22700 kg. 21990 kg. 19300 kg. 22600 kg. 21090 kg.

Max. Takeoff Weight (MTOW) LR SB 145-00-0032. 22600 kg. 22700 kg. 19800 kg. 21990 kg. 22100 kg.

Max. Landing Weight (MLW) LR Post-Mod. SB 145-00-0032. 19800 kg. 18400 kg. 19300 kg. 20990 kg. 22090 kg.

Max. Zero Fuel Weight (MZFW) LR Post-Mod. SB 145-00-0032. 17900 kg. 19300 kg. 18400 kg. 19800 kg. 17100 kg.

LANDING GEAR OPERATION VLO for retraction. 200 KIAS. 250 KIAS. 160 KIAS. 190 KIAS. 210 KIAS.

LANDING GEAR OPERATION VLO for Extension. 250 KIAS. 200 KIAS. 190 KIAS. 320 KIAS. 145 KIAS.

LANDING GEAR EXTENDED VLE. 250 KIAS. 200 KIAS. 190 KIAS. 320 KIAS. 260 KIAS.

MANEUVERING SPEED (VA). 200 KIAS. 190 KIAS. 250 KIAS. 145 KIAS. 220 KIAS.

RAPID AND LARGE ALTERNATING CONTROL INPUTS, ESPECIALLY IN COMBINATION WITH LARGE CHANGES IN PITCH, ROLL, OR YAW (E.G. LARGE SIDE SLIP ANGLES) MAY RESULT IN STRUCTURAL FAILURES AT ANY SPEED, EVEN BELOW VA. TRUE. FALSE.

MAXIMUM FLAP EXTENDED SPEED (VFE) FLAPS 9°. 250 KIAS. 200 KIAS. 145 KIAS. 160 KIAS. 210 KIAS.

MAXIMUM FLAP EXTENDED SPEED (VFE) FLAPS 22°. 250 KIAS. 200 KIAS. 145 KIAS. 160 KIAS. 210 KIAS.

MAXIMUM FLAP EXTENDED SPEED (VFE) FLAPS 45°. 155 KIAS. 200 KIAS. 145 KIAS. 160 KIAS. 150 KIAS.

TAILWIND Maximum Takeoff and Landing Tailwind Component. 10 kt. 5 kt. 12 kt. 196 kt of ground speed (Vtyre speed H30 x 9.5 - 16 16PR). According BRAKE ENERGY LIMITED CHART (AFM 5-33).

KINDS OF OPERATION (Seleccionar todas las correctas). Visual (VFR). Instrument (IFR). Severe Icing conditions. Icing conditions. ETOPS. Volcanic Ash Conditions (Density Less than 1 g/m3 and particules smaller than 0.01 mm).

LOAD FACTOR LIMIT (Seleccionar todas las correctas). Positive FLAPS UP 2.50g. Positive FLAPS UP 2.00 g. Positive FLAPS UP 2.75 g. Positive FLAPS DOWN 2.00 g. Positive FLAPS DOWN 1.50 g. Negative FLAPS UP -1.00 g. Negative FLAPS UP -2.00 g. Negative FLAPS UP -2.71. Negative FLAPS DOWN 0 g. Negative FLAPS DOWN -1.00 g.

FUEL Maximum usable quantity per tank. 2594 Kg per tank. 2573 kg per tank. 5579 kg. 4250 kg. 2500 kg per tank. 6000 kg.

FUEL Maximum permitted imbalance between tanks. 363 kg. 262 KG. 45 KG. 121 KG. 22 Liters.

FUEL TANK TEMPERATURE (Seleccionar todas la correctas). Minimum -40°C. Minimum -52°C. Minimum -56°C. Maximum 52°C. Maximum 40°C. Maximum 45°C.

AUXILIARY POWER UNIT OPERATIONAL LIMITS OPERATION ALTITUDE. 37000 ft. 30000 ft. 25000 ft. 18000 ft. 37000 or 25000 ft (Only one engine or one bleed operative).

AUXILIARY POWER UNIT OPERATIONAL LIMITS START. 884°C. 800°C. 680°C. 921°C. 732°C.

AUXILIARY POWER UNIT OPERATIONAL LIMITS CONTINUOUS. 884°C. 800°C. 680°C. 921°C. 732°C.

APU STARTER LIMITS Cooling period between each starting attempt: (Seleccionar todas las correctas). Between Three Consecutive Attempts 1 MINUTE OFF. Between Five Consecutive Attempts 30 MINUTES OFF. Between Four Consecutive Attempts 1 MINUTE OFF. Between Two Series of Three Consecutive Attempts 30 MINUTES OFF. Between Three Series of Two Consecutive Attempts 30 MINUTES OFF. Between Two Series of Three Consecutive Attempts 1 MINUTE OFF.

OPERATIONAL LIMITS (ROLLS-ROYCE AE3007A OR AE3007A1/1) MAX N1. 100%. 102.4%. 108.4%. 108%. 102%.

OPERATIONAL LIMITS (ROLLS-ROYCE AE3007A OR AE3007A1/1) MAX N2. 100%. 102.4%. 108.4%. 108%. 102%.

OPERATIONAL LIMITS (ROLLS-ROYCE AE3007A OR AE3007A1/1) START. 800°C. 921°C. 868°C. 884°C. 680°C.

OPERATIONAL LIMITS (ROLLS-ROYCE AE3007A OR AE3007A1/1) TAKEOFF. 800°C. 921°C. 868°C. 884°C. 680°C.

OPERATIONAL LIMITS (ROLLS-ROYCE AE3007A OR AE3007A1/1) CONTINUOUS. 800°C. 921°C. 868°C. 884°C. 680°C.

Takeoff Thrust. is time limited to 5 minutes. is no time limited. is no time limited as soon as the ALT T/O - 1 mode is selected. is time limited to 10 minutes. is no time limited as soon as the T/O - 1 mode is selected and T.L. is on detent position or below.

ENGINE STARTER LIMITS On Ground: (Seleccionar todas las correctas). Starting or Dry Motoring UP TO 5 MINUTES ON, 5 MINUTES OFF. Starting or Dry Motoring UP TO 1 MINUTES ON, 5 MINUTES OFF. Starting or Dry Motoring UP TO 5 MINUTES ON, 1 MINUTES OFF. OR First to Fourth Cycles 1 MINUTE ON, 1 MINUTE OFF. OR First to Fourth Cycles 5 MINUTE ON, 1 MINUTE OFF. OR First to Fourth Cycles 5 MINUTE ON, 5 MINUTE OFF.

ENGINE STARTER LIMITS (Seleccione todas las correctas) In Flight: Maximum Continuous Operation Time..................5 MINUTES ON. Starting or Dry Motoring UP TO 1 MINUTES ON, 5 MINUTES OFF. Minimum Continuous Operation Time..................1 MINUTES ON. No cool down time is required should an in-flight start be reattempted. One minute down time is required should an in-flight start be reattempted. Five minute down time is required should an in-flight start be reattempted.

ENGINE WARM UP (Seleccionar todas las correctas) Prior to takeoff, the engines must be allowed to run at low thrust to stabilize the engine temperatures before takeoff thrust is adjusted. After start, the engines must run at idle or taxi thrust during at least: 4 minutes for cold engines. 2 minutes for cold engines. 5 minutes for cold engines. 2 minutes for warm engines. 4 minutes for warm engines. 1 minutes for warm engines.

The engine is considered cold if it has been shutdown for more than. 90 minutes. 45 minutes. 60 minutes. 6 hs. 3 hs. 4 hs.

ENGINE COOL-DOWN. The engines must run for at least 1 minute at idle or taxi thrust before shutdown. The engines must run for at least 2 minute at idle or taxi thrust before shutdown. No cool time period is requiered as the APU is supplying bleed air, and cross bleed is pushed in. No cool time period is requiered as the APU is supplying bleed air, and cross bleed is pushed out.

ICE AND RAIN PROTECTION OPERATION IN ICING CONDITIONS (Seleccionar todas las correctas). Maximum Temperature for Anti-Icing Operation ............... 10°C. Maximum Temperature for Anti-Icing Operation ............... 15°C. Maximum Temperature for Anti-Icing Operation ............... 5°C. Minimum Temperature for Manual Anti-Icing Operation ... -40°C. Minimum Temperature for Manual Anti-Icing Operation ... -54°C. Minimum Temperature for Manual Anti-Icing Operation ... -56°C.

ICE AND RAIN PROTECTION OPERATION IN ICING CONDITIONS. There is no temperature limitation for anti-icing system automatic operation. The temperature limitation for anti-icing system automatic operation is 10°C. There is no temperature limitation for anti-icing system automatic operation in flight, except with single bleed operation. For automatic anti-icing system operation, Total Air Temperature (TAT) in flight, must be 10°C or below and visible moisture in any form is present.

ICE AND RAIN PROTECTION OPERATION IN ICING CONDITIONS. Icing conditions may exist whenever the Static Air Temperature (SAT) on the ground or for takeoff, or Total Air Temperature (TAT) in flight, is 10°C or below and visible moisture in any form is present (such as clouds, fog with visibility of one mile or less, rain, snow, sleet, and ice crystals). Icing conditions may exist whenever the Static Air Temperature (SAT) on the ground or for takeoff, or Total Air Temperature (TAT) in flight, is 5°C or below and visible moisture in any form is present (such as clouds, fog with visibility of one mile or less, rain, snow, sleet, and ice crystals). Icing conditions may exist whenever the Static Air Temperature (SAT) on the ground or for takeoff, or Total Air Temperature (TAT) in flight, is 0°C or below and visible moisture in any form is present (such as clouds, fog with visibility of one mile or less, rain, snow, sleet, and ice crystals).

OPERATION IN ICING CONDITIONS Icing conditions may also exist when the SAT on the ground and for takeoff is 10°C or below when operating on ramps, taxi ways, or runways where surface snow, ice, standing water, or slush may be ingested by the engines, or freeze on engines, nacelles, or engine sensor probes. True. False.

WINDSHIELD WIPER OPERATION Maximum Airspeed for Windshield Wiper Operation. 200 KIAS. 170 KIAS. 160 KIAS. 150 KIAS. 175 KIAS.

ELECTRICAL Maximum Load on Main Generator. 400 A. 300 A. 400 A up to 30000 ft 300 A above 30000 ft.

ELECTRICAL Maximum Load on APU Generator: 400 A. 300 A. 400 A up to 30000 ft 300 A above 30000 ft.

Maximum Battery Temperature. 70°C. 71°C. 56°C. 40°C. 69°C.

PRESSURIZATION (Seleccione todas las correctas). Maximum differential pressure 7.8 psi. Maximum differential pressure 8.1 psi. Maximum differential pressure 6.8 psi. Maximum differential overpressure 8.1 psi. Maximum differential overpressure 8.5 psi. Maximum differential overpressure 7.8 psi. Maximum differential negative pressure -0.3 psi. Maximum differential negative pressure 0 psi. Maximum differential negative pressure -0.5 psi (400 ft below AFE).

Maximum Altitude for Flap Extension. 20000 ft. 25000 ft. 30000 ft. 37000 ft.

PITCH TRIM Maximum Airspeed after Takeoff/During Climb without Retrimming. 160 KIAS. 170 KIAS. 180 KIAS. Vfs. V2 + 10 kt.

AUTOPILOT Minimum Decision Altitude During ILS Approach. 200 ft AGL. 500 ft AGL. 160 ft AGL.

AUTOPILOT Minimum Engagement Height (Takeoff or Go-around). 200 ft. 500 ft. 160 ft. Aceleration Altitud.

AUTOPILOT Minimum Use Height. 200 ft. 500 ft. 160 ft. DH.

AUTOPILOT (Seleccione todas las correctas) The following limitations are applicable to the Autopilot: Descent below Minimum Decision Altitude on a non precision approach with autopilot engaged is prohibited. Single engine go-around with autopilot engaged is prohibited. Approach mode selection during Localizer capture is allowed only when airplane is inbound. Coupled go-around height loss may be 75 ft. Descent below Minimum Decision Altitude on a non precision approach with autopilot engaged is allowed only in VFR conditions in case of circling. Single engine go-around with autopilot engaged is allowed.

TURBULENT AIR PENETRATION SPEED. At or below 10000 ft --- 200 KIAS Above 10000 ft --- 250 KIAS/0.63 M Whichever is lower. 200 KIAS. 320 KIAS. At or below 23000 ft --- 250 KIAS Above 23000 ft --- 320 KIAS/0.70 M Whichever is lower. FLC mode in Flight Level changes. 0.63 M in Cruise. VA (220 KIAS).

MAXIMUM RECOMMENDED CROSSWIND (NON-AFM) Dry runway. 30 kt. 25 kt. 20 kt. 10 kt. 15 kt.

MAXIMUM RECOMMENDED CROSSWIND (NON-AFM) Wet runway. 30 kt. 25 kt. 20 kt. 10 kt. 15 kt.

MAXIMUM RECOMMENDED CROSSWIND (NON-AFM) Runway with Compacted Snow. 30 kt. 25 kt. 20 kt. 10 kt. 15 kt.

MAXIMUM RECOMMENDED CROSSWIND (NON-AFM) Runway with Ice (no melting). 30 kt. 25 kt. 20 kt. 10 kt. 15 kt.

THRUST REVERSER. For a Go-araund procedure after touch down, check the reverse (REV) indication is out before full thrust aplication. Do not attempt a go-around procedure after deployment of the thrust reversers following a landing. Reverse must keep deployed until a normal runway taxi out speed is reached.

Selection of thrust reversers in flight or their preselection before touchdown is prohibited. True. False. True, but preselection could be set 50 ft over the treshold if VREF is corrected by wind more than 10 kt.

ICE AND RAIN PROTECTION. Single engine or single bleed maximum altitude operation in icing conditions: 15000 ft. Single engine with APU ON and Cross bleed pushed IN, maximum altitude operation in icing conditions: 25000 ft. Single engine or single bleed maximum altitude operation in icing conditions: 25000 ft. Single engine with APU ON and Cross bleed pushed IN, maximum altitude operation in icing conditions: 20000 ft.