euops gulfstream g650, gulfstream g650 br700-725a1-12

8/19/2019 Euops Gulfstream g650, Gulfstream g650 Br700-725a1-12

1/10

Aircraft Performance Group, IncApril 29, 2013

1

GULFSTREAM G650BR700-725A1-12

INTRODUCTION

Runway Analysis provides the means to determine maximum allowable takeoff and landingweights based upon:

Airport characteristics consisting of airport elevation, runway gradient and length,runway contaminants, and the obstructions within the takeoff flight path,

Environmental conditions consisting of temperature, wind, and pressure altitude.

Aircraft Configurations consisting of power settings, flap settings, bleed configurations,and Minimum Equipment List (MEL) inoperative components.

The performance and limitations are as outlined in the approved Airplane Flight Manual (AFM)for the specific aircraft considered. All takeoff and landing airport analysis data provided byAircraft Performance Group complies with EU-OPS regulations.

TAKEOFF

The maximum allowable takeoff weight is obtained by selecting the most limiting of thefollowing:

1. Maximum certified takeoff structural weight.

2. Climb limited weight – the maximum weight at which the appropriate airworthinessclimb gradients, for each takeoff segment, are attained for airport elevation andtemperature.

3. Runway field length limit weight – the maximum weight at which the aircraftcomplies with the appropriate airworthiness rules governing runway length, runwaygradient (slope), airport elevation, temperature, wind, pressure altitude, and runwaycontamination.

4. Obstruction limited weight – the maximum weight at which obstruction clearancerequired by the appropriate airworthiness rules can be attained. The obstruction limitweight is a function of aircraft configuration, obstacle height and distance, airportelevation, temperature, and wind. Unless otherwise stated, all takeoffs assume astraight out takeoff flight path along the extended runway centerline.

5. Brake energy – the maximum weight at which the aircraft brakes can absorb theamount of energy required to stop the aircraft.


2/10


2

6. Tire speed – the maximum weight so as not to exceed the maximum tire speedlimitations.

NOTE: Some runways/airports require a “Special Departure Procedure” in order tooptimize takeoff weight in terrain sensitive areas. The specific description of the Special

Departure Procedure is outlined on a separate page attached to the takeoff airportanalysis. These procedures describe the non-standard, one engine inoperative departureflight path. The maximum allowable takeoff weights, presented in the subsequentanalysis, are based upon following the specific procedure(s) outlined.

LANDING

The maximum allowable landing weight is obtained by selecting the most limiting of thefollowing:

1. Maximum certified landing structural weight.

2. Climb limited weight – the maximum weight at which the appropriate airworthinessclimb gradients, in the approach and landing configuration, are attained for airportelevation and temperature.

3. Runway field length limit weight – the maximum weight at which the aircraftcomplies with the appropriate airworthiness rules governing runway length, runwaygradient (slope), airport elevation, wind, pressure altitude, and runway contamination.


3/10


3

TAKEOFF PERFORMANCE CHARTDESCRIPTION / DEFINITIONS

GULFSTREAM G650 BR700-725A1-12

1. Chart Heading

The chart heading specifies the performance outlined (takeoff or landing), the airport byIdentifier, City/State, and Airport Name, the airport elevation, and the Aircraft type and Engine.

2. Aircraft Configuration

Aircraft configurations upon which the attached data is based on are presented in this block.Aircraft configurations consist of the following:

Takeoff flaps settings:10 Degrees and 20 Degrees10 Degrees WET and 20 Degrees WET

3. Special Departure Procedure

Some runways/airports require a “Special Departure Procedure” in order to optimize takeoffweight in terrain sensitive areas. The specific description of the Special Departure Procedure isoutlined on a separate page attached to the takeoff airport analysis. These procedures describethe non-standard, one engine inoperative, departure flight path. The maximum allowable takeoffweights, presented in the subsequent analysis, are based upon the specific procedure(s) outlined.If there is no “DP” attached to the runway identifier, the takeoff weights are predicated upon aSTRAIGHT OUT departure.

4. Runway Identifier

The runway identifier is specified as follows:• Full length runways indicated by basic identifier i.e. 34L• Intersection takeoffs include hyphen “-” i.e. 34L-A takeoff from intersection “A”• Temporary runway lengths / closures include “TMP”, i.e. 34LTMP• Special Departure Procedures include “DP” i.e. 34LDP

Declared distances used:• Takeoff Run Available (TORA)• Takeoff Distance Available (TODA)• Accelerate Stop Distance Available (ASDA)

Associated runway slope/gradient (percent)

5. OAT


4/10


4

This is the surface temperature, in degrees Celsius, upon which the performance data is based.The maximum temperature shown on the chart corresponds to the maximum operationaltemperature for airport elevation.

6. Takeoff Thrust Setting

Engine Power (EPR) settings for airport surface temperature and airport altitude are displayedfor Anti-Ice on and off.

7. Zero Wind Runway Limit Weight, V1

The zero wind runway limit weight displayed is the lowest of the following:

1. One Engine Inoperative Accelerate / Stop Limitations.2. One Engine Inoperative Accelerate / GO limitations.3. All Engine Operating Field limitations.

4.

Minimum Control limitations.5. Brake Energy limitations.6. Tire Speed limitations.7. Obstacle Clearance limitations.8. Flight Path / Level-off Altitude limitations.

In addition, the V1 speed corresponding to the zero wind limit weight is displayed.

8. Climb Limit Weight

The climb limit is a weight that meets the minimum climb gradients required for each takeoffflight path segment as defined in the certification regulations. The climb limit is determined fromthe applicable “TAKEOFF WEIGHT LIMITED BY CLIMB REQUIREMENTS” chart withinthe AFM. The climb limit is dependent upon reported surface temperature and airport altitudeonly.

THE LIMITING TAKEOFF WEIGHT IS THE LOWER OF THE RUNWAY LIMITWEIGHT, THE CLIMB LIMIT WEIGHT, OR THE MAXIMUM CERTIFIED

STRUCTURAL LIMIT WEIGHT.

CORRECTIONS

Corrections may be available to the zero wind runway limit weight and/or the Climb limitweight. A zero (0) may appear as a correction, which indicates that the adjustment item requiresno correction. An ‘NA’ may appear as a correction, which indicates that the adjustment item is

NOT AUTHORIZED for operations.

9. Wind Corrections


5/10


6/10


7/10


8/10


8

LANDING PERFORMANCE CHARTDESCRIPTION / DEFINITIONS

GULFSTREAM G650 BR700-725A1-12

1. Chart Heading

The chart heading specifies the performance outlined (takeoff or landing), the airport byIdentifier, City/State, and Airport Name, the airport elevation, and the Aircraft type andEngine.

2. Approach Climb Limits

The approach climb limit weights meet the minimum climb gradients required for theapproach climb (go-around) phase of landing as defined in the certification regulations.The approach climb limit weights are determined from the applicable Landing Weight

Permitted by Climb Requirements Charts within the AFM. The approach climb limit isdependent upon reported surface temperature and airport altitude only. Corrections aredisplayed for Anti-ice ON.

3. Aircraft/Runway Configuration for Landing

Landing data is provided for the following aircraft/runway configurations:Landing Flaps 39 degrees (Spoilers Automatic or Manual)

Landing distance factors of 60% or 80%Dry and Wet runways

Abnormal flaps landing (Unfactored)

Flaps 20, 10Dry and Wet runways

Flaps 0Dry runways

4. Runway Identifier

The runway identifier is specified as follows:• Full length runways indicated by basic identifier i.e. 34L• Temporary runway lengths / closures include “TMP”, i.e. 34LTMP

Declared Distances used:• Landing Distance Available (LDA)

Associated effective runway slope/gradient.

5. Landing Runway Limit Weight


9/10


9

The runway limit weight for landing distance available is displayed corresponding togiven wind component and aircraft/runway configuration.

THE LIMITING LANDING WEIGHT IS THE LOWER OF THE RUNWAYLIMIT WEIGHT, THE APPROACH CLIMB LIMIT WEIGHT, OR THE

MAXIMUM CERTIFIED STRUCTURAL LIMIT WEIGHT.

6. Temperature Correction

All landing field length limit weights are calculated at the standard day ( ISA )temperature for the airport elevation. For temperatures above standard, subtract the figureshown in LBS per Degree C from the landing runway limit weight.

7. Date

Indicates the date the performance chart was prepared.


10/10

-- THF -EDDI -- LANDING PERFORMANCE -- THF -EDDI -- GULFSTREAM G-650 BERLIN, DEU ELEVATION 167 BR700-725A1-12 ENG TEMPELHOF

*** APPROACH CLIMB LIMITS - APPROACH FLAPS 20 *** CLIMB PERFORMANCE NOT LIMITING BELOW 50 (C) TEMP(C) -20 50 CLMB WT 83500. 83500. CORRECTIONS: WING ANTIICE ON SUBTRACT 0 POUNDS ABOVE -20. DEGREES C

*** LANDING FIELD LENGTH LIMITS *** *** AUTOMATIC SPOILERS ***______________________________________________________________________________

RUNWAY | DESTINATION APT - FLPS 39 | ** ABNORMAL FLAPS LNDG-UNFACTORED ** | LENGTH WIND| FAR 60% FCTR| FAR 80% FCTR| FLAPS 20 | FLAPS 10 | FLAPS 0 | SLOPE KTS| DRY WET | DRY WET | DRY WET | DRY WET | DRY |______________________________________________________________________________

-10| 65096 53191| 83500 79854| 83500 83500| 83500 83500| 83500 | -5| 72149 59604| 83500 83500| 83500 83500| 83500 83500| 83500 | 09L | | | | | | 5466FT 0| 79153 66016| 83500 83500| 83500 83500| 83500 83500| 83500 | 0.25 | | | | | | 10| 83500 70573| 83500 83500| 83500 83500| 83500 83500| 83500 | 20| 83500 75537| 83500 83500| 83500 83500| 83500 83500| 83500 | TISA=14DEGC| | | | | |

14C-LB/DEGC| 306 264| 0 0| 0 0| 0 0| |______________________________________________________________________________

-10| 55862 45219| 83123 68892| 83500 82073| 83500 78406| 70429 | -5| 62348 51413| 83500 76350| 83500 83500| 83500 83500| 78929 | 27R | | | | | | 5180FT 0| 68833 57607| 83500 83144| 83500 83500| 83500 83500| 83500 | -0.34 | | | | | | 10| 73905 61830| 83500 83500| 83500 83500| 83500 83500| 83500 | 20| 78470 66053| 83500 83500| 83500 83500| 83500 83500| 83500 | TISA=14DEGC| | | | | |14C-LB/DEGC| 275 234| 0 328| 0 0| 0 0| |______________________________________________________________________________

30Apr13

euops gulfstream g650, gulfstream g650 br700-725a1-12

Documents