Embraer Legacy 500 Limitations

38096 lbs (17280 kg)

37920 lbs (17200 kg)

34128 lbs (15480 kgs)

26500 lbs (12020 kg)

• Max Altitude: 45000
• Min Altitude: -1000
• TO, LDG & Groundstart: 9600 ft to -1000 ft and -40 deg C to + 50 Deg C
• Mach min Operation Speed
• Mach 0.40: SAT From -57C down to -60C

• Mach 0.55: SAT from -60C down to -65 C

• Mach 0.67: SAT from -65C down to -70C

Flap 1......... 210 KIAS

Flap 2.......... 185 KIAS

Flap3.......... 185 KIAS

Flap FULL.. 170 KIAS

Maximum Altitude For Flap Extended........15000 ft

VLO........... 250 KIAS

VLE............ 250 KIAS

Maximum Tire Ground Speed....... 182 kt

• Max To and Ldg Tailwind Component....... 10 kt
• Rwy Contaminated..... 20kts
• Compacted Snow........ 20kts
• Wet Ice....................... 15kts

• – Visual Flight Rules (VFR);

• – Instrument Flight Rules (IFR);

• – Icing conditions;

• – Extended over water;

• – Category I.

Maximum loading:

Forward Cabinet............... 40 kg

Stowage Compartment...............150 kg

Cargo Compartment.................. 400 kg

NOTE: The maximum intensity of loading in each compartment is the following:

Stowage Compartment................. 370 kg/m2

Cargo Compartment..................... 370 kg/m2

Load Factor Limit: Positive G's

- Flap Up: ....................... 2.6g

- Flap Down( 1,2,3,F).......2.0g

Load Factor Limit: negative

- Flap up........................ -1.0 g

- Flap Down( 1,2,3,F).......0.0g

Runway Slope.........-2% TO +2%

Runway Surface Type....Paved

During taxi, takeoff and landing, cabin interior doors must be secured in the open position.
>FAA Certification

During taxi, takeoff and landing, the divan cannot be occupied by persons with the following characteristics:

– Under 15 years old;

– With shoulder height shorter than backrest height;

– Holding an infant, even with lap-held belt.

– Navigation must not be predicated upon the use of the TAWS.

– To avoid giving unwanted alerts, the TAWS must be inhibited when landing at an airport that is not included in the airport database.

– The use of TAWS functions should be manually inhibited during QFE operations if GPS data is unavailable or inoperative.

1. The following limitations are applicable to the Traffic Alert and Collision Avoidance System (TCAS) II:

The following limitations are applicable to the Traffic Alert and Collision Avoidance System (TCAS) II:

– Deviation from the ATC assigned altitude is authorized only to extent necessary to comply with a TCAS II Resolution Advisory (RA).

– Maneuvers must not be based solely on a Traffic Advisory (TA) or on information presented in the traffic display.

Fuel tank Capacity: 13,126 lbs,

Unusable fuel: 90 lbs

Max Temp for TO: 52dg C

The FUEL XFEED Knob must be set to OFF during takeoff, go-around, and landing flight phases.

1. Max in-flight Start: 31000ft
2. Max in-flight temp: -37dg C

Maximum: 31,000 ft

max: 23,000 ft

Max ECS usage: 20000

Start: Max 985dgC

Continous: Max 757 dg C

Up to three consecutive unsuccessful start attempts are allowed, with 30 second intervals between attempts.

Max ITT: 650 for 5 sec

Max continuous: 950 dgC

Static takeoff is limited to crosswind components up to 25 kt.

Max Motoring Time: 5 minutes, then 15 min cool down time

Prior to additional starts or motoring, a cooling period of 15 minutes is required

Start attempts 1 through 3:

80 seconds max. (After the third start attempt must have 15 minutes cool down.

Start Attempt 4 and Subsequent: 80 sec max time and then cool down of 15 min

-Backing the airplane with reverse thrust is prohibited.
-Upon landing, thrust reversers should be stowed at 40 KIAS.

- Max Diff Pressure................................ 9.7 psid

- Max Diff Overpressure...................... 10.4 psid

- Max Diff Negative Pressure............... -0.5 psid

- Max Diff Press for TO and LDG.......... 0.2 psid

Icing conditions may exist whenever the Outside Air Temperature (OAT) 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 presented (such as clouds, fog with visibility of one mile or less, rain, snow, sleet and ice crystals)

Maximum Operating Altitude (anti-ice single bleed operation)............. 20000 ft

Min Engage Height......... 400 ft Min Use Height................ 190 ft

– The following TOLD functions are not available in the Flight Management System:

– Derated Takeoff Mode (TO-2);

– CAT II operations;

– Ice Protection calculation for takeoff;

– Climb Gradients and obstacles.

– Do not select the TO-2 or CAT II when performing the flight planning in the FMS.

– The Flight Management System does not provide OEI speeds and driftdown altitude. If a driftdown is required, pilot must manually select the driftdown speed on the SPD knob and the altitude of level

– Set SPD knob to MAN before takeoff phase. After retracting Flaps, the SPD knob may be set to FMS as required.

– Set SPD knob to MAN before landing gear lever DN and flap setting for landing.

– When select SPD knob in FMS, the landing Flap must be defined on the FMS LANDING page for proper VAP speed target presentation, even when using manual VSPEED.

– Operations requiring RNP of less than 0.3 are not approved.

– RNP AR operations with missed approaches requiring RNP of less than 1.0 are not approved.

– TOLD function must not be used for abnormal landing performance calculations.

– Airworthiness approval of performance information obtained by TOLD does not constitute operational approval. Make sure that any required operational approval from the Regulatory Authority is granted prior to the intended use.

– FMS speed must not be used for takeoff phase.

– For dual FMS installation, the TOLD data displayed information is approved and does not need to be verified with AFM.

– Although OPERA software, AFM and TOLD are equally approved sources of performance data, the information used by the flight crew during a specific phase of flight must be obtained from only one of the approved sources of information (AFM, OPERA or TOLD). No intermixing of these data sources is permitted during a specific phase of flight.

– The following TOLD performance information is advisory only: AEO gradient, SID gradient, VAP and VFS on FMS LANDING page.

– For VNAV operations, the use of FD is required.

Runway slope must be manually entered on TAKEOFF and LANDING pages if departure or arrival is done on Brazil or China airports.

– Use of VNAV guidance below the published approach minimums without the appropriate visibility indications is prohibited.

– Barometric vertical navigation is prohibited in airports with remote altimeter setting.

– FMS speed must not be used during approach and landing phases.

– When a GPS-only approach is planned, prior to dispatch, the flight crew is required to make sure that the predictive RAIM at the destination ETA is within the approach criteria.

– For ILS approaches, APPR Button on AFCS Panel must be pressed only when airplane heading deviation from ILS course is less than 90°.

– When an ILS approach has been selected through the FMS format pages, the APPR Button on AFCS Panel must be pressed only when the airplane heading deviation from ILS course is less than 90° and airplane is within 30 NM of the destination airport.

– For LPV operations, dual GPS is required.

– For RNP AR operations, at least one GNSS sensor is required.

Min Alt for Use In-Flight ........................... 10000 ft

NOTE: Troubleshooting is not permitted in-flight.

The factory-installed cargo compartment fire extinguishing bottles agent duration can be either 78 or 110 minutes. Agent duration is identified by a placard installed in the cargo compartment.