Especificações técnicas da aeronave

Boeing 737-800NG

Fabricante: Boeing

http://www.boeing.com.br/

http://www.boeing.com/

Generic Limitations:

● ALTITUDE: Maximum ZP 41 000 ft

                      Maximum ZP for T/O and Landing 8400 ft (Runway slopes : ± 2% )

● WIND: Max tailwind for T/O & Landing……………………….…10 kt

               Max demonstrated crosswind (runway dry or wet) ……36 kt

               Automatic landing (dual channel CAT2 or CAT3 approach):

                      - tailwind ………………………..…. 10 kt

                      - crosswind ………………………….20 kt

                      - headwind ………………………… 25 kt

● CABIN PRESS: Max cabin differential pressure (top of yellow band)………..….. 9.1 psi

                            Max cabin differential pressure for takeoff & landing………... 0.125 psi

  With engine bleed air switches ON, do not operate the air conditioning packs in HIGH for takeoff, approach or landing.

● AUTOPILOT: - Do not engage A/P for takeoff < 400 ft AGL

              - The A/P must be disengaged before the airplane descends more than 50 ft below the MDA (Minimum Descent Altitude) unless it is coupled to an ILS glide slope & localizer or in the go- around mode.

              - No ailerons trim with A/P engaged

              - The Minimum Use Height (MUH) for single channel autopilot operation is 158 ft AGL

● MAX AIRSPEED LIMITS & FLIGHT CONTROLS

       - Speedbrake may not be deployed in flight below 1000 ft radio altitude

       - Holding in icing conditions with flaps extended is prohibited.

       - Flaps 15 normal landings are prohibited. A Flap 15 landing may be performed when required by a non normal procedure.

               VMO / MMO ………………………..….....…340 kt / .82M

               Turbulence* ………………………….…. 280 KIAS /.76M

                Maximal Flap extension altitude……….……… 20 000 ft

                 Flaps 1…...…………………………………………. 250 kt

                 Flaps 2…...…………………………………………. 250 kt

                 Flaps 5.......………………...………………………. 250 kt

                 Flaps 10.....…………………………………………. 210 kt

                 Flaps 15…...…………………………………………200 kt

                 Flaps 25…...…………………………………………190 kt

                 Flaps 30…...…………………………………………175 kt

                 Flaps 40…...…………………………………………162 kt

 

        Alternate Flap duty cycle in flight:

                 - Flaps 0 -15 ……………………..…one cycle, 5 min. off

                 - Flaps greater than 15 ………..…one cycle, 25 min. off

 

        Window heat inoperative (< 10000 ft)** ………… 250 kt

        Max speed with Mach Trim inoperative.… 280 KIAS/.82

 

* Below 15000 ft, at less than Maximum Landing Weight, a speed of 250 kt provides adequate buffet margin

** Window heat should be ON 10 min. before takeoff Version 01 (Nov.06) Page 2 B737 BRIEFINGS

 

 ● FUEL: - Max Fuel temperature is +49°C

*Inflight, The fuel temperature must be maintained +3°C above freezing point

MAXIMUM USABLE FUEL:

     - Left + Right ...............................7830 Kg

     - Center .......................................13066 Kg

     - Total ..........................................20896 Kg

● LANDING GEAR: Max extension ……………………………….….………….270 kt / M.82

                                Max retraction …………………………………………..…………..235 kt

                                Max with gear extended………..……………..………….. 320 kt / M.82

                                Max Tyres Speed ………………….………………..225 MPH or 195 kt

 

● ELECTRICAL: AC Power system (115 V, 400 Hz, 3-phase)

   - Voltage :

      • Normal…………………………………………………………. 115V

      • Maximum…………………………………………...…………. 120V

      • Minimum ………………………………………………...……..110V

    - Frequency :

       • Normal………………………………………………...……... 400Hz

       • Maximum…………………………………………...…..……410 Hz

       • Minimum ………………………………………………..……390 Hz

    - Load limit :

       • IDGs + APU Generator + External Power………….……90 kVA - IDG :

       • Max oil temperature………………………..………...……... 182°C

       • mini oil pressure…….……………………………...……… 165 psi

    DC Power system - Voltage :

       • Normal………………………………..……………….…....…... 26V

       • Maximum…………………………………………….….….……30V

       • Minimum ……………………………………………….…..……22V

    Battery power

       • Capacity………………………………..……………….…..….40Ah

       • Voltage…………………………………………….….….………24V

    Miscellaneous

       AC service outlets (cabin, cockpit, equipt rack)…………....……115 V, 400 Hz, 1000 W

       DC service outlet (cockpit)…………………………………….….28 V

 

● HYDRAULICS:

     Minimum range………………………………….…..………... 2800 psi

     Normal range …………………………….………….……….. 3000 psi

     Maximum (relief valve setting)……………………...………..3500 psi

     Precharge pressure……………………….…….………...…. 1000 psi

     Minimum fuel for ground operation of electric pumps ……… 750 kg

     Hydraulics quantity :

        Refill level (Sys A)………………….………… 6.0 / 4.7 (RFL or 76%)

        Refill level (Sys B)………………….………… 8.5 / 6.9 (RFL or 76%)

        EIS ……………………………………...100% / 88% (on ground only)

 

● ENGINES:

     - Maximum & minimum limits are red while caution limits are amber

     - Engine ignition must be CONT for :

            • Takeoff & landing

            • Operation in moderate or heavy rain

            • Anti-ice operation

      Maxi N1 ….……………………...………………………………… 104%

      Maxi N2 …………………..……………………………………….. 105%

      Max startup EGT …………………..……………………………. 725°C

      Max T/O EGT …………...…………………………..…950°C (10 min.)

      Max continuous EGT ……..………………………….…..………895°C

      Mini oil press …………….………………………………..…..…..13 psi

      Mini oil press during takeoff…………..……………Above Yellow Arc

      Mini oil quantity prior to engine start ……………….. 3.2 USG / 60%

      Oil consumption……………………………….…maximum 0,5 l /hour

      Max oil temperature :

            - Maximum momentary ………………..………………………. 165° C

            - Maximum for 15 min. ………………..…………………..160 -165°C

            - Maximum continuous ………………..…………………….…. 160°C

● APU:

       - APU bleed valve may be open during engine start, but avoid engine power above idle.

         APU BLEED + ELECTRICAL load ……….…………………………………….until 10000 ft

         APU BLEED ………………………………………………………………………until 17000 ft

         APU ELECTRICAL ………………………..until 41000 ft (has always priority on Bleed air)

         Minimum RPM for power delivery……………………….………..……………………….95%

         Normal Operation……………………………………………….…………….……100 - 101 %

         Overspeed Limit……………………………………………….…….…………………… 107 %

         Electrical supply…………………………………..…………….………………………. 90 kVA

 

● PNEUMATICS:

         Minimum pressure for engine start ………………….. 30 psi at Sea Level (-0,5 psi/1000 ft)

         External Pneumatic Source :

            - Maximum Pressure ……………………………………………..………………………. 60 psi

            - Maximum temperature ………………………………………..…..……………………. 232°C

 

● ACCELERATION LIMITS:

        Flaps UP ……………………….…………..…..………….+2.5 g to - 1.0 g

        Flaps DOWN ….………………….………..……..……….+2.5 g to - 1.0 g

● FIRE PROTECTION:

    All Fire agents……………………………...…………..…...…………..…Halon

    Cargo Fire agent protection duration…………………..…….…..195 minutes

 

● PASSENGER EVACUATION: Main door emergency evacuation slide systems must be armed and engagement of each girt bar with the still fitting verified, prior to taxi, T/O and landing whenever passengers are carried.

 

● WATER & WASTE: Water tank capacity………………………………………. 235 lit. / 62.5 USG

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