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    G450 AFM Rev 44, 9 - 16 - 2022

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    The document provides information about flight load acceleration limits, weight limits, and center of gravity limits for the Gulfstream G450 aircraft. It includes tables and figures with numerical values for maximum weights at different stages of flight and the allowable center of gravity envelope as a function of gross weight.

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    G450 AFM Rev 44, 9 - 16 - 2022

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    432 views2 pages
    The document provides information about flight load acceleration limits, weight limits, and center of gravity limits for the Gulfstream G450 aircraft. It includes tables and figures with numerical values for maximum weights at different stages of flight and the allowable center of gravity envelope as a function of gross weight.

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    G450 AFM Rev 44, 9_16_2022

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    The document provides information about flight load acceleration limits, weight limits, and center of gravity limits for the Gulfstream G450 aircraft. It includes tables and figures with numerical values for maximum weights at different stages of flight and the allowable center of gravity envelope as a function of gross weight.

    Copyright:

    © All Rights Reserved
    Download as PDF, TXT or read online from Scribd
    Download as pdf or txt
    432 views2 pages

    G450 AFM Rev 44, 9 - 16 - 2022

    Uploaded by

    özgür barış anlar
    The document provides information about flight load acceleration limits, weight limits, and center of gravity limits for the Gulfstream G450 aircraft. It includes tables and figures with numerical values for maximum weights at different stages of flight and the allowable center of gravity envelope as a function of gross weight.

    Copyright:

    © All Rights Reserved
    Download as PDF, TXT or read online from Scribd
    Download as pdf or txt
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    G450™ AIRPLANE FLIGHT MANUAL

    G450™

    Airplane Flight

    Manual

    ™ ™
    FAA pA rp evo dA pri nal e ilF thg Manu la4G 05 Aipr nal e gilF ht Maun laFA MG ACA- C-4G 50 O- PS 0- 0R1ive ois 44n 4 S4 pe met be16r , 02 20 2 90- 61- G405

    Gulfstream Aerospace
    Gulfstream Model GIV-X™
    GAC-AC-G450-OPS-0001
    G450™ AIRPLANE FLIGHT MANUAL

    01-03-50: Flight Load Acceleration REVISION 442022-09-16

    1. Flaps UP (0°):
    -1 to 2.5 G for all weights up to maximum takeoff weight.
    2. Flaps 10° or 20° (T/O APP):
    0 to 2.0 G for all weights up to maximum takeoff weight.
    3. Flaps DOWN (39°):
    a. For All Weights Up To Maximum Landing Weight:
    0 to 2.0 G
    b. For All Weights Above Maximum Landing Weight:
    0 to 1.5 G

    01-03-60: Weight REVISION 442022-09-16

    Table 1. For G450 Airplanes

    Serial Number Maximum Zero Maximum Maximum Maximum


    Fuel Weight Ramp Weight Takeoff Weight Landing
    (1) Weight (2)
    4001 thru 4239 49,000 lb 74,300 lb 73,900 lb 66,000 lb
    (22,226 kg) (33,702 kg) (33,521 kg) (29,937 kg)
    4001 thru 4239 49,000 lb 75,000 lb 74,600 lb 66,000 lb
    with ASC 016 (22,226 kg) (34,020 kg) (33,838 kg) (29,937 kg)
    4240 and Sub 49,000 lb 75,000 lb 74,600 lb 66,000 lb
    (22,226 kg) (34,020 kg) (33,838 kg) (29,937 kg)

    (1) Maximum takeoff weight, unless restricted by climb performance, brake


    energy, or tire speed for approved altitudes and ambient temperature or
    by field length.
    (2) Maximum landing weight, unless restricted by climb requirements.

    01-03-70: Center of Gravity REVISION 442022-09-16

    1. The allowable Center Of Gravity (CG) range is a function of gross weight as


    shown in Figure 1. G450 Zero Fuel Gross Weight Center Of Gravity Envelope.
    2. Zero fuel gross weight CG must be within the allowable Zero Fuel Gross
    Weight CG Envelope. The fueled airplane CG will then be within limits for all
    fuel loads.

    Flight Load Acceleration


    FAA Approved Revision 44 2022-09-16 01-03-00: 12 of 16

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