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51 Cards in this Set
- Front
- Back
MAX Ramp Weight (MRW) |
38096 lbs (17280 kg) |
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MAX Takeoff Weight (MTOW) |
37920 lbs (17200 kg) |
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MAX Landing Weight (MLW) |
34128 lbs (15480 kgs) |
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MAX Zero Fuel Weight (MZFW) |
26500 lbs (12020 kg)
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Operational Envelope (Altitude and temp) |
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Maximum Flap Extended Speed (Vfe) |
Flap 1......... 210 KIAS Flap 2.......... 185 KIAS Flap3.......... 185 KIAS Flap FULL.. 170 KIAS |
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MAXIMUM ALTITUDE FOR FLAP EXTENDED |
Maximum Altitude For Flap Extended........15000 ft |
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LANDING GEAR OPERATION/EXTENDED SPEED (VLO AND VLE) |
VLO........... 250 KIAS VLE............ 250 KIAS |
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MAXIMUM TIRE GROUND SPEED |
Maximum Tire Ground Speed....... 182 kt |
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WIND LIMITATIONS |
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KINDS OF OPERATION: This airplane may be flown day and night in the following conditions, |
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BAGGAGE LOADING |
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 |
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MANEUVERING FLIGHT LOAD FACTORS (Positive) |
Load Factor Limit: Positive G's - Flap Up: ....................... 2.6g - Flap Down( 1,2,3,F).......2.0g |
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NEGATIVE MANEUVERING FLIGHT LOAD |
Load Factor Limit: negative - Flap up........................ -1.0 g - Flap Down( 1,2,3,F).......0.0g |
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RUNWAY SLOPE & TYPE |
Runway Slope.........-2% TO +2% Runway Surface Type....Paved |
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CABIN INTERIOR DOORS |
During taxi, takeoff and landing, cabin interior doors must be secured in the open position. |
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DIVAN SEATS |
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. |
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TERRAIN AWARENESS AND WARNING SYSTEM (TAWS) |
– 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. |
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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. |
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FUEL Capacity |
Fuel tank Capacity: 13,126 lbs, Unusable fuel: 90 lbs |
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Max Temp for TO: 52dg C |
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CROSSFEED OPERATION |
The FUEL XFEED Knob must be set to OFF during takeoff, go-around, and landing flight phases. |
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AUXILIARY POWER UNIT (APU)-Honeywell 36-150 |
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APU Operational Limit: Max altitude for Electrical Power usage |
Maximum: 31,000 ft
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APU Operational Limit: Max altitude for In-Flight Engine start |
max: 23,000 ft |
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APU Operational Limit: Max altitude for ECS usage |
Max ECS usage: 20000 |
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APU Max EGT during Start and Continous |
Start: Max 985dgC Continous: Max 757 dg C |
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APU UNSUCCESSFUL START ATTEMPTS |
Up to three consecutive unsuccessful start attempts are allowed, with 30 second intervals between attempts. |
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POWERPLANT: Operational Honeywell AS907-3-1E Max ITT C for ground start |
Max ITT: 650 for 5 sec Max continuous: 950 dgC
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CROSSWIND LIMITATION for Takeoff |
Static takeoff is limited to crosswind components up to 25 kt. |
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STARTER LIMITS -DRY MOTORING DUTY CYCLE LIMITS |
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
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STARTING DUTY CYCLE LIMITS |
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
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Thrust Reverser Limits |
-Backing the airplane with reverse thrust is prohibited. |
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PRESSURIZATION Limitations |
- 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
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OPERATION IN ICING CONDITIONS |
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) |
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MAXIMUM OPERATING ALTITUDE (Single bleed, Icing Conditions) |
Maximum Operating Altitude (anti-ice single bleed operation)............. 20000 ft |
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AUTOPILOT (MIN ENGAGE AND MIN USE HEIGHT) |
Min Engage Height......... 400 ft Min Use Height................ 190 ft |
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FLIGHT MANAGEMENT SYSTEM |
– 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. |
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RNP NAVIGATION |
– 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. |
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TAKEOFF AND LANDING (TOLD) FUNCTION |
– 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. |
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DUAL FMS INSTALLATION |
– 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. |
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VNAV OPERATION: FOR VNAV OPS, WHAT IS REQUIRED TO BE TURNED ON |
– For VNAV operations, the use of FD is required. |
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RUNWAY SLOPE |
Runway slope must be manually entered on TAKEOFF and LANDING pages if departure or arrival is done on Brazil or China airports. |
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APPROACH LIMITATIONS FOR BARO-VNAV |
– 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. |
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APPROACH LIMITATIONS FOR FMS SPEED |
– FMS speed must not be used during approach and landing phases. |
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APPROACH LIMITATIONS FOR GPS |
– 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. |
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APPROACH LIMITATIONS FOR ILS |
– 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. |
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APPROACH LIMITATIONS FOR LPV |
– For LPV operations, dual GPS is required. |
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APPROACH LIMITATIONS FOR RNP AR |
– For RNP AR operations, at least one GNSS sensor is required. |
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ON BOARD MAINTENANCE SYSTEM ALTITUDE LIMITATION |
Min Alt for Use In-Flight ........................... 10000 ft NOTE: Troubleshooting is not permitted in-flight. |
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FIRE PROTECTION CARGO COMT DURATION |
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. |