A319

OPERATIONS MANUAL VOL.3 M&S P 0.1

LIST OF EFFECTIVE PAGES REV 01

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Code PAGE IDENTIFICATION Page Number

Page Date

Include in Volume :

R List of Effective Introduction Pages 0.1 As Below All General 1.1-1.2 13 Jan 2011 All Emergency Turn Procedures 2.1-2.2 13 Jan 2011 All Explanation & Examples 3.1-3.9 13 Jan 2011 All Standard RTOW Chart Designations 4.1-4.3 13 Jan 2011 All Take Off, Approach and Landing Performance Tables 5.1-5.2 13 Jan 2011 All

R List of Effective RTOW charts - Destinations 6.1-6.3 10 Mar 2011 3M R List of Effective RTOW charts - Alternates 7.1-7.2 10 Mar 2011 3S List of Effective RTOW charts - MEL – Items 8.1-8.1 13 Jan 2011 3M

NOTE: Please do not remove existing Temporary charts (yellow Pages) unless advised. DELETED PAGES/RTOW CHARTS With this revision the following Pages/ RTOW Charts have been deleted: Page Ident Page Date RTOW Chart Ident Conf Chart Date

AUH 31R-A13 1+F,2 04 JAN 11

MOVE FROM “MAINS” TO “SUPPS”: NIL MOVE FROM “SUPPS” TO “MAINS”:. NIL Codes: R = Revised N = New NOTE: Ensure that VOL.3(M&S) is updated as per latest list of effective pages (LEP).


RTOW CHARTS - General REV 00

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1. RTOW CHARTS IN VOL.3 (M&S): RTOW charts (tables) in Vol.3 (M&S) have been produced with Airbus PEP TLO Module using approved aircraft database reference AD112E01. Using these tables, Flight Crew and Operations staff are able to obtain the following information for the given ambient conditions and airplane configuration: – Maximum takeoff weight and the performance limitation code, – Takeoff speeds. RTOW charts shall be provided in Vol.3 (M&S) as follows: VOL.3 MAINS :

1. RWYs without E/T Procedure:

Full length and Intersections - one (1) RTOW chart with CONF 1+F and CONF 2 on a

single page. 2. RWYs with E/T Procedure:

Full length and intersections - one (1) RTOW charts with optimum flaps CONF 1+F or

CONF 2 on a single page.

VOL.3 SUPPS :

1. RWYs without E/T Procedure: Full length and Intersections - one (1) RTOW chart with CONF 1+F/2 on a single page. 2. For RWYs with E/T Procedure:

Full length and Intersections - one (1) RTOW charts with optimum flaps CONF 1+F or CONF 2 on a single page.

Note 1: CONF 3 RTOW charts shall be provided only for short RWYs if payload benefit is expected or

in case specially requested by the Fleet Office.

2. COMPUTATION BASIS OF RTOW CHARTS: All RTOW charts have been computed on the following basis: i) Optimum V2/VS, optimum V1/VR and minimum V1. ii) Line-up allowances: TORA/TODA reduced by 16 meters and ASDA reduced by 27 meters. Note 2: Other assumptions/conditions like Air conditioning, Anti-icing, Reversers, QNH, Dry (Wet) Rwy

as well as correction values are given on the respective RTOW charts.


RTOW CHARTS - General REV 00

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3. RTOW CHARTS FOR INTERSECTION TAKEOFF:

RTOW chart provided for an intersection can also be used for Full Runway as well as for another intersection of the same runway with longer TORA.

4. QNH AND BLEED CORRECTIONS (Up to 9200 Feet) ( Ref.FCOM 2.02.24 P1)

To take into account QNH deviation and / or bleeds ON apply

CORRECTIONS ON TEMPERATURE IF FLEX TAKE-OFF PERFORMED

CORRECTIONS ON WEIGHT IF TAKE-OFF WITH FULL THRUST PERFORMED

Add 1 o C / 40 hpa until pressure altitude equals zero.

No correction for pressue altitude below 0 ft.

QNH above 1013 hpa Add 20 Kg / hpa until pressure altitude equals zero.

No correction for pressue altitude below 0 ft.Sub 1 o C / 6 hpa QNH below 1013 hpa Sub 90 Kg / hpa

Sub 5 o C *Engine A/ Ice ON Sub 250 Kg Sub 11 o C *Total A / Ice ON Sub 750 Kg Sub 5 o C **Air Cond….ON Sub 2200 Kg

NIL Air Cond….OFF NIL Note 3: a.* Correction valid only for OAT less than 10 o C. b. ** Correction valid only for RTOW charts produced with AIR COND..OFF. c. # For high altitude operation, refer FCOM 2.02.24 p 3 (if applicable).

COMPARE CORRECTED TEMP. (CT), FLAT RATING TEMP. (T REF) AND OAT

CT Higher than OAT and

CT Higher than T REF

} Take CT as flex. Temp. } limited to ISA + 60 o C }

Both conditions above not fulfilled

} No flexible take-off possible } Determine MAX TOW

5. SPECIFIC WET RWY, AC ON/OFF and QNH CORRECTIONS: Each RTOW chart in this volume is provided with its own specific WET RWY, AC ON/OFF (as applicable) and QNH corrections at the bottom. QNH corrections are given for +/-10 hpa and may be interpolated/extrapolated linearly.

Note 4: See complete instructions in FCOM 2.04.10 for the following: a) Wet runway RTOW/SPEEDS corrections with Reverse Thrust Inoperative. b) Contaminated runway RTOW/SPEEDS corrections with Reverse Thrust Operative. 6. SPEED CORRECTIONS FOR LOW WEIGHTS (Ref. FCOM 2.02.12 P5) In case Actual TOW is less than the RTOW at the top of appropriate Wind Column, apply a speed correction provided at the bottom of the RTOW chart to V1, VR and V2 limited to minimum speeds.

Note 5: This correction can also be applied if recommended procedure at FCOM 2.02.14 P2 (moving towards left) is followed and Actual TOW is less than the RTOW at the new column top.


RTOW CHARTS – Emergency Turn Procedures REV 00

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1. GENERAL. In a continued takeoff following an engine failure at or after V1 and before the first turning point, the aircraft must be flown as per the one-engine-inoperative procedure specified on the relevant RTOW chart to comply with obstacle clearance requirements. RTOW charts are calculated on this basis. 2. ONE ENGINE-INOPERATIVE PROCEDURE. 2.1 Straight Ahead Procedure If there is no emergency turn procedure on the RTOW chart, then the aircraft is to be flown on the extended runway centreline until all four segments of the takeoff are completed. 2.2 Emergency Turn Procedure (“E/T” procedure text as given on the RTOW chart) The aircraft is to be flown on the extended runway centerline to the first turning point, and then flown so as to complete the emergency turn procedure as specified.

Note 6: Based on available data, all obstacles upto 22 nm (approx.) in the takeoff path are considered. 2.3 Emergency Turn Procedure Operational Limitations. To satisfy the Aircraft Flight Manual one-engine-inoperative net takeoff flight path requirements, at all points on the one-engine-inoperative procedure path, the aircraft must be flown with the maximum available climb gradient. Therefore:

i) All turns must be flown at constant speed V2 and at a bank angle not exceeding 15 degrees when making the first turn below 400 ft or not exceeding 25 degrees above 400 ft. Thereafter, all turns must be at a bank angle not exceeding 25 degrees.

ii) The aircraft must not be accelerated above V2 until all the turns specified in the emergency turn

procedure have been completed and the aircraft has attained the minimum acceleration altitude/height specified on the relevant RTOW chart.

Note 7: For all runways with E/T procedure, Obstacle data (Ht/Dist) is different for CONF 1+F and

CONF 2/3. Obs data for CONF 1+F is based on gradient loss for bank angle 15 o during a procedure turn whereas Obs data for CONF 2/3 is based on gradient loss for 25 o bank angle. This has resulted from the fact that Autopilot/FD may bank the aircraft up to 25 o to meet the speed constraints during a turn with CONF 2/3 (V2 being greater than F speed), while CONF 1+F is limiting bank angle to 15 o.

Note 8: Where a turn procedure requires a bank angle greater than 15 degrees and/or acceleration

above V2 is required during a turn, this will be stated on the RTOW chart or in the “Fleet Instructions/NOTAM/Airfield Brief” for that airport.

Note 9: If the emergency turn procedure requires the aircraft to “track” (eg.”track 250 deg (M)”), then

the aircraft must be flown on a heading adjusted for drift so that the required track direction is maintained.


RTOW CHARTS - Emergency Turn Procedures REV 00

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2.4 ATC Communication As soon as operational circumstances allow:

• Advise intentions to ATC,

After completing the specific emergency turn procedure: • proceed as directed by ATC or, • manoeuvre for an instrument letdown or, • climb to MEA or above as required, • Refer to Instrument Approach Procedure (IAP) plates for indication of obstacles and terrain.


RTOW CHARTS – Explanation and Examples REV 00

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Please review the relevant sections of your FCOM’s, which have a full explanation on the chart layout and how to calculate performance using the Airbus OCTOPUS (Operational and Certified Take Off and landing Performance Universal Software) system. Below chart is an explanation to highlight the chart difference from FCOM format. The examples may be used for guidance only for entire A320 Family (A319-A321) ; for detailed explanation refer to FCOM2.

3

11 12 14

1 2 7 8 5 9 4

15

16

17

25

19

18

24

10

13

22

20

21 23

6

26




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1. Aircraft Type / Model and Regulation used to produce the chart. 2. Engine Type / Model. 3. OCTOPUS Version, production date of chart & database codes. 4. ICAO 4-letter code for airport. 5. IATA 3-letter code for airport. 6. Basic conditions on which the chart based:

Standard QNH, Air conditioning off, Anti-icing off, All Reversers operating for Wet Runway, No reversers credit for Dry Runway.

7. Apt Elevation, ISA temp, Rwy slope in %. 8. Runway declared distances (meters) used for calculation.

Take off run available (TORA). Take off distance available (TODA). Accelerate Stop distance available (ASDA).

9. Runway condition ( e.g.: Dry / Wet / Contaminated) Thrust setting (TOGA / NO Derate / Derated thrust etc,).

10. Runway Designation. 11. Flat rating temp (Maximum permissible temperature for takeoff). 12. Acceleration Altitudes (QNH) defined as:

a. Minimum: The maximum of all of the minimum acceleration altitudes calculated for each of the RTOW boxes on each RTOW page. This is the minimum altitude at or above which the aircraft may accelerate to achieve Flap Retraction Speed. Third Segment of the Takeoff Path is also called the acceleration segment. Regulation Min Acceleration is 400’ AGL. Min GF Acceleration is 800’ AGL or obstacle limited extended 2nd segment, whichever is lower.

b. Maximum Acceleration Altitudes: The minimum of all of the maximum Acceleration

Altitudes calculated for each of the RTOW boxes on each RTOW page. It is determined by the 10-minute Takeoff Thrust Limit with one-engine inoperative.

13. Shift value in meters (Distance from the beginning of TORA).

14. Takeoff configuration. 15. Wind components (from Tailwind 10 kts ….. to Headwind 10kts).




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16. GREY band indicates temperature above environmental limit (TMAX). Note 10: GREY band if in the limiting weight box, is a TVMC Band and indicates

Temp for which V1 / VR / V2 are close to limiting VMC. 17. MAX PERMISSIBLE 84.1 3/6 LIMITING CODES

TAKEOFF WEIGHT 156/68/69 SPEEDS (V1/ VR/V2) Note 11: FOR VR & V2 “1” to be prefixed, hence speeds 156 / 68 / 69.

18. Corrections for WET RWY, AC ON & QNH. Order of corrections: 1st. WET 2nd. AC ON INFL 3rd. QNH

19. Influence Box ∆TOW ∆Tflex ∆V1/∆ VR/∆V2 WET RWY -2.4 -2 Corrections to be applied INFL -13/ 0/ 0 Below TVMC (+60) 0.0 -1 Correcting to be applied TVMC -13/ 0/ 0 above TVMC. (see below) ∆V1 / ∆VR / ∆V2 ∆TOW ∆Tflex

Note 12: FCOM 2.02.10 P3 states TVMC is a temperature value given per column, and is fictitious value that indicates the temperature above which the speeds are close to a VMC limitation or are VMC limited. EG: If Outside Air Temperature or Flex Temperature is greater than the TVMC, use the shaded boxes (lower line) on the RTOW Charts.

20. No. of obstacles in T.O. Path; obs height / distance (Ref. Brake Release Point). 21. Min control speeds limitations. 22. Minimum values of V1/ VR/ V2 to which takeoff speeds must be limited when

decrements are applied. Check VMU limitation. Speeds correction for weights below the lowest weight of a column.

23. Limitation codes for takeoff performance. 24. Decoding the Influence box. 25. Outside Air Temperature (OAT).

26. Emergency Turn: Chart designation and procedure description if the RWY has an

Emergency Turn Procedure with one engine inoperative at or after V1.




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Considerations:

1. When using the RTOW Charts shown in Volume 3 Mains for your final takeoff calculations, your actual TOW must be lower than the RTOW figures you choose to use. For example, if your takeoff weight is 72,400 kgs, you must use the RTOW values in Volume 3 Mains of 72,400 kgs or greater, but not less than 72,400 kgs.

2. Keeping the above in consideration, locate your takeoff weight figures shown in the “Wind 0

kt” column (or Headwind 10 KT if applicable) that would be the closest to your actual takeoff weight. All of your final takeoff calculations (FLEX, etc) will be based on that row.

Note 13: You MUST use the RTOW figures shown in the row that is the closest match to

your takeoff weight in the “Wind 0 kt” column (or Headwind 10 KT if applicable). You are permitted to use the (generally) lower takeoff speeds and the corresponding figures in either tailwind column (“Tailwind -5 kt” or “Tailwind -10 kt”) as long as it is still at least your takeoff weight, and as long as you remain in the same row.

3. When MACTOW C of G is forward of 27%, apply FCOM corrections 2.02.10 P3 & 2.02.14

P3 (cross-referenced to FCOM 2.01.40 P2 & P3) as follows: a. Max TOW: Reduce RTOW by 1000 kgs & increase V1, VR & V2 by 1 kt. b. Flex Thrust: Reduce Flex Temp by 2˚C & increase V1, VR & V2 by 1 kt.

Note14: (MAC % Correction applicable to A320 ONLY)

4. OM(A) 8.1.2.4.1 (Page 8-11) states “For takeoff performance calculation, wind direction and

velocities expressed as ‘light and variable’ shall be considered as 5 knots tailwind.

5. TOGA is mandatory from a Contaminated Runway (reference FCOM 2.02.20 P2): “Flexible takeoff is not permitted on contaminated runways.”

6. Speed corrections for low weights (Ref FCOM 2.02.12 P5): In case Actual TOW is less than

the RTOW at the top of the appropriate Wind Column, apply a speed correction provided at the bottom of the RTOW chart to V1, VR and V2 limited to minimum speeds.

7. Use Config 1+F as per SOP; however if payload is restricted, you may use Config 2 or

Config 3 if and where needed.

8. Also as per company SOP, do not interpolate from the RTOW charts in Volume 3 for your final (actual) take-off calculations. If any values fall “between” what is on the charts, use the more conservative figures as shown. For example, if QNH is 998 hPa (1013 - 15), use, for example, 2 X -10, resulting in a correction of -4 to the Flex as shown in the “D QNH HPA” correction figures. This will be more conservative than using an interpolated value of “-3”. Note that Interpolation is allowed elsewhere. For example (from FCOM 2.02.25 P3): Pressure Altitude zero, Take-Off Weight 62,000 kgs: your min V2 could be 131 KIAS, or when checking what your MTOW will be.

9. Refer to FCOM’s if Anti-Ice (of any kind) is required.




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Example 1 – FLEX TEMP calculation: BAH RWY 12L FULL A/C A320-212 RWY Condition: Wet (FCOM 2.04.10 P1) Engine Anti-ice: Off OAT: +32 DEG C Packs: Off Actual weight: 69,000 Kgs Wind: Calm QNH: 1009 hPa MACTOW: 25% Step 1 – Check RTOW for the conditions given (ref FCOM 2.04.10 P2b – wet runway):

Given the above conditions, RTOW would be 82,700 kgs (obviously well above MTOW, however this will be needed when applying corrections). Step 2: Determining the amount of weight decrement due to water-covered runway

(Refer to FCOM 2.04.10 P3). Note 15: Use “All reversers” on wet runway and “No reversers” on dry runway:




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Take the Step 1 result (82,700 kgs) and subtract the above decrement figure for which configuration would result in the least decrement (Config 1+F = 300 kgs). Therefore, 82,700 kgs - 300 kgs = MTOW of 82,400 kgs. (Note BAH 12L – TORA 3956 m – has no clearway – ref RTOW Charts.) Regardless how high above the certified TOW your initial figure is, checking the decrement is critically important to determine exactly what your MTOW is for the given conditions. Also check that your actual take-off speeds do not exceed limiting speeds. Final calculations determine either Config 1+F or Config 2 could be used in this example. As per SOP, use Config 1+F. Step 3 – Locate your actual TOW in the zero column, and read the Flex Temp figure:

(Use zero wind for this example. 69,600 kgs is the closest to this example’s takeoff weight.) Step 4: Wet Runway Influence corrections:

Step 5: QNH corrections:




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“Final Figure” Calculations (from load-sheet weight):

Config 1+F (as per SOP) BAH 12L FULL 69,000 kg, Wet, +32 C, 0 kts, QNH 1009, Anti-Ice & Packs: Off

Flex Temp V1 VR V2

Initial Values 56ºC 161 161 161

FCOM Corrections N/A N/A N/A N/A

Ref 2.02.24 P1 (i.e. Anti Ice) Intermediate Values 56ºC 161 161 161

Wet Corrections 0 Line 1

-13 Line 2

0 Line 2

0 Line 2

T Flex ≤ TVMC apply lines 1&2 corrections T Flex > TVMC apply lines 3&4 corrections

Intermediate Values 56ºC 148 161 161

QNH Corrections - 2ºC Line 1

N/A N/A N/A T Flex ≤ TVMC apply line 1 corrections

T Flex > TVMC apply line 3 corrections

Intermediate Values 54ºC 148 161 161

*MACTOW Corrections (25% C.G corr.) - 2ºC +1 +1 +1

Final Values 52ºC 149 162 162 Note 16: * MAC % Correction not applicable to A321 & A319 Cross-check your results with the following:

• Min V1 / VR / V2 at Sea Level = (Reference applicable RTOW Chart, or use FCOM 2.02.25 P1 figures): 114 / 118 / 120

• Min V2 Limited by VMU/VMCA (69,000 kgs) = 144 (ref FCOM 2.02.25 P2) • T flex (52° C in this example) should be less than or equal to T Flex Max (60° C) and

greater than T Ref (30° C). Therefore, FLEX TAKEOFF permitted (Reference FCOM 2.02.20 P2).

Enter the “Final Value” figures onto the Takeoff Data Card and have the other crew-member independently cross-check your results.




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Example 2 – Contaminated Runway Calculation: BAH RWY 30R FULL A/C A320-212 RWY CONDITION: 6 mm Standing Water Engine Anti ice: On OAT: +29 DEG C Packs: Off Actual weight: 71,500 Kgs Wind: 360/15 QNH: 1012 hPa MACTOW: 31% Wind Component (in this example) is approximately 10 kts steady headwind which you can use. If in doubt, be conservative, and use zero wind. Be sure to check all configurations to determine which would be the best to use after considering the initial RTOW as well as the weight decrement (below). Although Config 1+F is SOP, in this case, step 2 shows that Config 1+F results in less decrement: Step 1: Check MTOW for the conditions given:

Interpolate 29° conservatively between 25° and 30° which will result in a “best” MTOW of 84,100 kgs at Config 1+F. Step 2: Determining the amount of weight decrement due to water-covered

runway (Refer to FCOM 2.04.10 P5):

The above shows the least weight decrement by using Config 1+F. Take Step 1 results and subtract from the above. (84,100 kgs – 10,100 kgs: Resulting MTOW of 74,000 kgs)

Note 17: BAH has no clearway. (Ref RTOW Charts.)

In this example, the RTOW check shows there is no restriction required to the ATOW of 71,500 kgs.




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Step 3: Takeoff Data Calculation – Refer to FCOM 2.04.10 P5: Use the appropriate table to determine takeoff speeds associated with the actual takeoff weight. In this example, Config 1+F or Config 2 could be used, however use Config 1+F for SOP purposes as there is no weight penalty associated. The actual TOW of 71,500 kgs falls within the “Equal To Corrected Weight” section of the “Config 1+F” table. Conservatively use the 72,000 kg speeds to obtain: 141 / 156 / 157. Cross-check your results with the following:

• Min V1 / VR / V2 at Sea Level = (Reference FCOM 2.02.25 P1): 114 / 118 / 120 • Min V2 Limited by VMU / VMCA (71,500 kgs) = 147 (ref FCOM 2.02.25 P2) • FLEX TAKEOFF is not permitted – TOGA is mandatory in this case.

Finally, enter the “Final Value” figures onto the Takeoff Data Card and have the other crew-member independently cross-check your results.


RTOW CHARTS – Standard Chart Designations REV 00


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1. FULL Runway with designated Taxiway entry.

When there is a designated taxiway entry at the beginning of the runway, the word FULL will NOT be used after the runway designation. Instead, “-“ (ie: dash) followed by taxiway designator will be used.

Examples:

BAH 12L-A DAC 14-N

2. FULL Runway with no Taxiway entry:

The word “FULL” will be used after the runway designation when:

• There is no turning pad at the beginning of the runway, • There is no taxiway entry at the beginning of the runway, • Minimum runway width is adequate for a 180o turn.

Note 18: Minimum runway width required for 180o turn, including edge safety distance 4.5m either side, is as follows:

A319: 45 m Examples:

BEY 35 FULL HBE 14 FULL




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3. FULL Runway with non-designated Taxiway entry. The word “FULL” will be used after the runway designation when:

• There is no turning pad at the beginning of the runway • The entry taxiway at the beginning of the runway is not designated appropriately.

Note 21: A dash (" – ") is added to the chart title to distinguish from back tracking. Examples: KWI 15L-FULL RKT 16-FULL SAH 18-FULL

4. FULL Runway with Turning Pad at the beginning.

The word “PAD” will be used after the runway designation when: • There is a turning pad at the beginning of the runway • There is no taxiway entry at the beginning of runway.

NOTE 22: Minimum Turning Pad dimensions required for 180o turn, including edge

safety distance 4.5m either side, is as follows: A319: 45m x 45m

Examples:

TRV 14 PAD ISB 30 PAD1




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5. Runway with Intersections or Turning Pad at intermediate position:

Takeoff data for departures from runway intersections (i.e. not full length) will be defined by the runway designator followed by either:

a) “-“ and taxiway designator; OR b) the word “PAD”. In case there are more than one (1) Turning Pads, those will be defined as PAD1, PAD2 …etc… ; Turning Pad with greatest TORA will be called PAD1.

Examples: ISB 30-A ISB 30 PAD1 ISB 12 PAD2


RTOW CHARTS – T/O, App. and Ldg. Perf. REV 00


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GO-AROUND CONFIGURATION: 2 or 3 Gradient : 2.1% ONE ENGINE OUT High Air Conditioning ONE ENGINE AT GO-AROUND THRUST Anti-Icing : OFF V = 1.23 Vs GO-AROUND LIMIT TEMPERATURES (OAT OC)

Pressure Altitude (Feet)

GO-AROUND WEIGHTS (1000 Kg) 75 74 72 70 68 66 64 62 60 58

Sea Level - - 46 49 52 55 55 55 55 55 1000 - - 42 46 49 52 53 53 53 53 2000 - - - 42 45 49 51 51 51 51 3000 - - - 25 42 45 48 48 48 48 4000 - - - - 38 42 45 47 47 47 5000 - - - - 35 38 41 45 45 45 6000 - - - - - 34 37 41 43 43 7000 - - - - - - 33 36 40 41 8000 - - - - - - 29 32 36 39

SPECIFIC AIRPORTS - GO-AROUND LIMIT TEMPERATURES (OAT OC) APT. Code

ALT. (Feet)

GO-AROUND WEIGHTS (1000 Kg) 75 74 72 70 68 66 64 62 60 58

ADJ 2555 - - - 40 43 47 49 49 49 49 AMM 2395 - - - 41 44 47 49 49 49 49 DAM 2020 - - - 42 45 49 50 50 50 50 ESB 3125 - - - 20 42 45 45 45 45 45 IFN 5072 - - - - 33 38 41 44 44 44 IKA 3305 - - - - 41 44 47 48 48 48 ISB 1668 - - 09 43 47 50 51 51 51 51 KRT 1260 - - - 26 48 51 52 52 52 52 KTM 4390 - - - - 35 40 43 45 45 45 MED 2151 - - - 42 45 48 50 50 50 50 PEW 1211 - - 28 45 48 51 51 51 51 51 RUH 2049 - - - 42 45 48 50 50 50 50 SAH 7237 - - - - - - 32 35 39 40 SYZ 4920 - - - - 35 35 42 45 45 45 T\iG 4848 - 35 35 42 45 45 45 NOTES:

1. With ENGINE AIR BLEED ‘OFF’, increase GA weight by 1300 Kg. 2. With ENGINE ON sub 300 Kg, TOTAL ANTI-ICE ‘ON’, sub 3400Kg 3. The Actual GA weight must not be greater than the RTOW for the selected

runway and temperature. 4. For data not covered in above tables, refer FCOM 3.05.35 Pages 2 & 3.


RTOW CHARTS – T/O, App. and Ldg. Perf. REV 00


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ONE ENGINE OUT ONE ENGINE AT GO AROUND THURST AIR CONDITIONING: ON ANTI-ICING: OFF V = 1.23 MAX LANDING WEIGHT: 62,500 KGS. CONF 3

APPROACH CLIMB GRADIENT %

Press Altitude (Feet)

OAT oC 0 10 20 30 40 45 50

Sea Level 4.1 4.1 4.0 4.0 4.0 3.9 3.3 1000 3.9 3.9 3.8 3.8 3.8 3.5 2.9 2000 3.7 3.7 3.6 3.6 3.6 3.1 2.6 3000 3.5 3.4 3.4 3.4 3.2 2.7 - 4000 3.3 3.3 3.2 3.2 2.9 2.3 - 5000 3.1 3.1 3.0 3.0 2.5 2.2 - 6000 2.9 2.9 2.9 2.8 2.1 - - 7000 2.7 2.7 2.6 2.6 - - - 8000 2.5 2.4 2.4 2.3 - - -


RTOW CHARTS – List of Effective RTOW Charts (Destinations) REV 01

Code IATA Chart Identifier Conf Chart

Date Code IATA Chart Identifier Conf Chart

Date

Codes: R = Revised N = New NOTE: All RTOW charts have been computed with ‘AC OFF’ unless mentioned.

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ADD 07L-A 1+F 11-DEC-10 ADD 07R-A 1+F 11-DEC-10 ADD 07R-B 1+F 11-DEC-10 ADD 25L-E 1+F 11-DEC-10 ADD 25L-D 1+F 11-DEC-10 ADD 25R-E 1+F 11-DEC-10 ADE 08-5 1+F,2 08-DEC-10 ADE 08-4 1+F,2 08-DEC-10 ADE 26-1 1+F,2 08-DEC-10 ADE 26-3 1+F,2 08-DEC-10 AMM 08L-H 1+F,2 08-DEC-10 AMM 08L-M 1+F,2 08-DEC-10 AMM 08R-A 1+F,2 08-DEC-10 AMM 08R-D 1+F,2 08-DEC-10 AMM 26L-A 1+F,2 08-DEC-10 AMM 26L-B 1+F,2 08-DEC-10 AMM 26R-H 1+F,2 08-DEC-10 AMM 26R-K 1+F,2 08-DEC-10 ATH 03L-A1 1+F 05 JAN 11 ATH 03L-A2 1+F 05 JAN 11 ATH 03L-A4 1+F 05 JAN 11 ATH 03R-D1 1+F 05 JAN 11 ATH 03R-D2 1+F 05 JAN 11 ATH 03R-D4 1+F 05 JAN 11 ATH 21L-D13 1+F,2 05 JAN 11 ATH 21L-D12 1+F,2 05 JAN 11 ATH 21L-D11 1+F,2 05 JAN 11 ATH 21R-A14 1+F,2 05 JAN 11 ATH 21R-A13 1+F,2 05 JAN 11 ATH 21R-A11 1+F,2 05 JAN 11 AUH 13L-A2 1+F,2 04 JAN 11 AUH 13L-A6 1+F,2 04 JAN 11 AUH 13R-E2 1+F,2 04 JAN 11 AUH 13R-E6 1+F,2 04 JAN 11 AUH 31L-E15 1+F,2 04 JAN 11 AUH 31L-E13 1+F,2 04 JAN 11 AUH 31R-A17 1+F,2 04 JAN 11

N AUH 31R-A14 1+F,2 09 MAR 11 BAH 12L-A1 1+F,2 11-DEC-10 BAH 12L-B 1+F,2 11-DEC-10 BAH 12L-C 1+F,2 11-DEC-10 BAH 12R-R 3 11-DEC-10 BAH 30L PAD 3 11-DEC-10 BAH 30L-H 3 11-DEC-10 BAH 30R-H 1+F,2 11-DEC-10 BAH 30R-G 1+F,2 11-DEC-10 BAH 30R-F 1+F,2 11-DEC-10

BEY 03 (Missed App)

- 11 JAN 11

BEY 16 (Missed App)

- 11 JAN 11

BEY 17-M 1+F 05 JAN 11 BEY 21-H 1+F,2 05 JAN 11 BEY 34 PAD 1+F,2 05 JAN 11 BEY 34-A 1+F,2 05 JAN 11 BEY 35 FULL 1+F,2 05 JAN 11 BEY 35-A 1+F,2 10 JAN 11

BGW 15L-S6 1+F,2 11-DEC-10 BGW 15L-S5 1+F,2 11-DEC-10 BGW 15R-P6 1+F,2 11-DEC-10 BGW 33L-P1 1+F,2 11-DEC-10 BGW 33R-S1 1+F,2 11-DEC-10 BGW 33R-S2 1+F,2 11-DEC-10

BOM 09 PAD 1+F 05 JAN 11 BOM 09-N9 1+F 05 JAN 11 BOM 14-E10 1+F 05 JAN 11 BOM 14-K1 1+F 05 JAN 11 BOM 27-N1 1+F 05 JAN 11 BOM 27-N3 1+F 05 JAN 11 BOM 32-E1 1+F 05 JAN 11

N BSR 14-FULL 1+F,2 02 MAR 11 N BSR 32-FULL 1+F,2 02 MAR 11

CAI 05L-A 1+F,2 29 DEC 10 CAI 05L-A2 1+F,2 29 DEC 10 CAI 05C-T 1+F,2 29 DEC 10 CAI 05C-Z 1+F,2 29 DEC 10 CAI 05R-F 1+F,2 29 DEC 10 CAI 23L-F 1+F,2 29 DEC 10 CAI 23C-T 1+F,2 29 DEC 10 CAI 23C-V 1+F,2 29 DEC 10 CAI 23R FULL 1+F,2 29 DEC 10 CAI 23R-A6 1+F,2 29 DEC 10

CMB 04-E 1+F,2 08 DEC 10 CMB 04-D 1+F,2 08 DEC 10 CMB 22-A 1+F,2 08 DEC 10 CMB 22-B 1+F,2 08 DEC 10

COK 09-C1 1+F 30 DEC 10 COK 27-C5 1+F,2 30 DEC 10

DAC 14-N 1+F,2 29 DEC 10 DAC 32-S 1+F,2 29 DEC 10

DAM 05L-U 1+F 30 DEC 10





Date



A-319-112

DAM 05L-S 1+F 30 DEC 10 DAM 05R-G 1+F 30 DEC 10 DAM 23L-A1 1+F 30 DEC 10 DAM 23R-P 1+F 30 DEC 10 DEL 09-K 1+F,2 06 JAN 11 DEL 10-N 1+F,2 06 JAN 11 DEL 10-M 1+F, 2 06 JAN 11 DEL 11-Z8 1+F, 2 06 JAN 11 DEL 11-Z6 1+F, 2 06 JAN 11 DEL 27-A 1+F,2 06 JAN 11 DEL 28-P 1+F,2 06 JAN 11 DEL 28-C 1+F,2 06 JAN 11 DEL 28-B 1+F,2 06 JAN 11 DEL 29-CE1 1+F, 2 06 JAN 11 DEL 29-Z3 1+F, 2 06 JAN 11 DMM 16L-J 1+F,2 22 DEC 10 DMM 16L-R 1+F,2 22 DEC 10 DMM 16R-B 1+F,2 22 DEC 10 DMM 16R-B4 1+F,2 22 DEC 10 DMM 34L-B 1+F,2 22 DEC 10 DMM 34L-B2 1+F,2 22 DEC 10 DMM 34R-J 1+F,2 22 DEC 10 DMM 34R-J1 1+F,2 22 DEC 10 DOH 16 PAD 1+F,2 29 DEC 10 DOH 16-A 1+F,2 29 DEC 10 DOH 16-B 1+F,2 29 DEC 10 DOH 34-G 1+F 29 DEC 10 DOH 34-E1 1+F 29 DEC 10 DXB 12L-M 1+F,2 04 JAN 11 DXB 12L-M3 1+F,2 04 JAN 11 DXB 12R-K1 1+F,2 04 JAN 11 DXB 12R-K2 1+F,2 09 JAN 11 DXB 12R-K6 1+F,2 04 JAN 11 DXB 30L-K17 1+F,2 04 JAN 11 DXB 30L-K13 1+F,2 09 JAN 11 DXB 30R-M14A 1+F,2 04 JAN 11 DXB 30R-M10A 1+F,2 04 JAN 11 EBL 18-A1 1+F,2 28 DEC 10 EBL 18-A2 1+F,2 28 DEC 10 EBL 36 PAD 1+F,2 28 DEC 10 EBL 36-A4 1+F,2 28 DEC 10 HBE 14 FULL 1+F,2 28 DEC 10 HBE 14-H 1+F,2 28 DEC 10 HBE 32 FULL 1+F,2 28 DEC 10 HBE 32-A 1+F,2 28 DEC 10

IFN 08L-J 1+F 03 JAN 11 IFN 08R-J 1+F 03 JAN 11 IFN 26L-G 1+F 03 JAN 11 IFN 26R-G 1+F 03 JAN 11

IKA 11L-C 1+F,2 06 DEC 10 IKA 11L-E 1+F,2 06 DEC 10 IKA 11R-C 1+F,2 06 DEC 10 IKA 11R-Z 1+F,2 09 JAN 11 IKA 29L-FULL 1+F,2 06 DEC 10 IKA 29L-H 1+F,2 06 DEC 10 IKA 29R-N 1+F,2 06 DEC 10 IKA 29R-J 1+F,2 06 DEC 10

IST 05-E1 1+F 07 DEC 11 IST 17L-B1 1+F,2 07 DEC 11 IST 17R-A1 1+F,2 07 DEC 11 IST 23 FULL 1+F,2 07 DEC 11 IST 35L-A6 1+F,2 07 DEC 11 IST 35R-B11 1+F,2 07 DEC 11

JED 16C-R 1+F,2 12 DEC 10 JED 16L-L1 1+F,2 12 DEC 10 JED 16R-B7 1+F,2 12 DEC 10 JED 34C-H1 1+F,2 12 DEC 10 JED 34L-B 1+F,2 12 DEC 10 JED 34R-V 1+F,2 12 DEC 10

KHI 07L-A 1+F 12-DEC-10 KHI 07L-D 1+F 12-DEC-10 KHI 07R-E 1+F 12-DEC-10 KHI 07R-C 1+F 12-DEC-10 KHI 25L-H 1+F 12-DEC-10 KHI 25L-F 1+F 12-DEC-10 KHI 25R-G 1+F 12-DEC-10 KHI 25R-F 1+F 12-DEC-10

KRT 18 PAD 1+F,2 08 DEC 10 KRT 18-A 1+F,2 08 DEC 10 KRT 36 PAD1 1+F,2 08 DEC 10 KRT 36-G 1+F,2 08 DEC 10

N KTM 02 PAD (AC

OFF) 1+F 10 MAR 11

N KTM 02 PAD (AC ON)

1+F 10 MAR 11

N KTM 20 PAD (AC OFF)

1+F 10 MAR 11

N KTM 20 PAD WET (AC OFF)

1+F 10 MAR 11

N KTM 20 PAD (AC ON)

1+F 10 MAR 11





Date



A-319-112

N KTM 20 PAD WET (AC ON)

1+F 10 MAR 11

KWI 15L-FULL 1+F,2 26 DEC 10 KWI 15L-E5 1+F,2 26 DEC 10 KWI 15R-W15 1+F,2 26 DEC 10 KWI 15R-W5 1+F,2 26 DEC 10 KWI 33L-W1 1+F,2 26 DEC 10 KWI 33L-W2 1+F,2 26 DEC 10 KWI 33R-E1 1+F,2 26 DEC 10 KWI 33R-E2 1+F,2 26 DEC 10 LCA 04-H 1+F,2 08 JAN 11 LCA 22-A 1+F,2 08 JAN 11 MAA 07-K 1+F,2 06 JAN 11 MAA 07-F 1+F,2 06 JAN 11 MAA 12 PAD 3 06 JAN 11 MAA 25-J 1+F,2 06 JAN 11 MAA 25-C 1+F,2 06 JAN 11 MAA 30 FULL 3 06 JAN 11 MCT 08-A1 1+F 06 JAN 11 MCT 08-E 1+F 06 JAN 11 MCT 26-A4 1+F 06 JAN 11 MCT 26-B 1+F 06 JAN 11 MED 17-D 1+F 28 DEC 10 MED 18-C 1+F,2 29 DEC 10 MED 35-A 1+F 29 DEC 10 MED 36-D 1+F 29 DEC 10 MHD 13L-H 1+F,2 28 DEC 10 MHD 13R-H 1+F,2 28 DEC 10 MHD 31L-E 1+F,2 28 DEC 10 MHD 31R-E 1+F,2 28 DEC 10 NJF 10-A 1+F,2 05 JAN 11 NJF 28-C 1+F,2 05 JAN 11 PEW 17-F 1+F 05 JAN 11 PEW 35-A1 1+F 05 JAN 11 RUH 15L-G 1+F,2 05 JAN 11 RUH 15L-G6 1+F,2 05 JAN 11 RUH 15R-A 1+F,2 05 JAN 11 RUH 15R-A6 1+F,2 05 JAN 11 RUH 33L-A 1+F,2 05 JAN 11 RUH 33L-A2 1+F,2 09 JAN 11 RUH 33R-G 1+F,2 05 JAN 11 RUH 33R-G2 1+F,2 05 JAN 11

SAH 18-FULL 1+F 24 DEC 10 SAH 36-FULL 1+F 24 DEC 10

SYZ 11L-A7 1+F 10 JAN 11 SYZ 11L-A5 1+F 10 JAN 11 SYZ 11R-B7 1+F 10 JAN 11 SYZ 11R-B5 1+F 10 JAN 11 SYZ 29L-B1 1+F 10 JAN 11 SYZ 29L-C2 1+F 10 JAN 11 SYZ 29R-A1 1+F 10 JAN 11 SYZ 29R-A2 1+F 10 JAN 11


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AAN 01-A 1+F,2 27 Feb 11 AAN 19-E 1+F,2 27 Feb 11 ADJ 06-A2 1+F,2 27 Feb 11 ADJ 24-FULL 1+F 27 Feb 11 ALP 09-A 1+F,2 08 Dec 10 ALP 27-A 1+F,2 08 Dec 10 ALY 04 PAD 1+F,2 06 Dec 10 ALY 22-E 1+F,2 06 Dec 10 AMD 05-A 1+F,2 16 Feb 11 AMD 23 PAD1 1+F,2 16 Feb 11 BJR 04 PAD 1+F,2 27 Feb 11 BJR 22 PAD 1+F,2 27 Feb 11 BKK 01L-E21 1+F,2 06 Dec 10 BKK 01R-B13 1+F,2 06 Dec 10 BKK 19L-B1 1+F,2 06 Dec 10 BKK 19R-E1 1+F,2 06 Dec 10 BLR 09-A6 1+F,2 08 Mar 11 BLR 27-A1 1+F,2 07 Mar 11 BND 03R-A 1+F 01 Mar 11 BND 21L-G 1+F,2 01 Mar 11 CCU 01L PAD 1+F,2 16 Feb 11 CCU 01R-D 1+F,2 16 Feb 11

CCU 19L PAD 1+F,2 16 Feb 11 CCU 19R PAD 1+F,2 16 Feb 11 CGK 07L-N6 1+F,2 17 Feb 11 CGK 07R-S7 1+F,2 17 Feb 11 CGK 25L-S1 1+F,2 17 Feb 11 CGK 25R-N1 1+F,2 17 Feb 11 CGP 05 PAD 1+F,2 14 Feb 11 CGP 23 PAD 1+F,2 14 Feb 11 CHQ 11-F 1+F,2 16 Feb 11 CHQ 29-A 1+F,2 16 Feb 11 CNX 18-A 1+F 01 Mar 11 CNX 36-H 1+F 01 Mar 11 ESB 03L-A2 1+F 01 Mar 11 ESB 03R-A 1+F 01 Mar 11 ESB 21L-A 1+F 01 Mar 11 ESB 21R-A1 1+F 01 Mar 11

GVA 05-G 1+F,2 20 Feb 11 GVA 23-A 1+F 01 Mar 11

HKT 09-A 1+F,2 16 Feb 11 HKT 27 PAD 1+F,2 16 Feb 11

HRG 16-J 1+F,2 16 Feb 11 HRG 34-B 1+F,2 16 Feb 11

HYD 09-A10 1+F,2 16 Feb 11 HYD 09-A8 1+F,2 16 Feb 11 HYD 27-A1 1+F,2 16 Feb 11 HYD 27-A3 1+F,2 16 Feb 11

ISB 12 PAD2 1+F,2 29 Nov 10 ISB 30 PAD1 1+F,2 29 Nov 10

JAI 09 PAD 1+F,2 01 Mar 11 JAI 27 PAD1 1+F,2 01 Mar 11

JHB 16 PAD 1+F,2 16 Feb 11 JHB 34 PAD 1+F,2 16 Feb 11

JIB 09 PAD 1+F,2 28 Feb 11 JIB 27 PAD1 1+F 28 Feb 11

KUL 14L-A1 1+F,2 13 Dec 10 KUL 14R-C1 1+F,2 13 Dec 10 KUL 32L FULL 1+F,2 13 Dec 10 KUL 32R-A11 1+F,2 13 Dec 10

LHE 18L-S 1+F,2 05 Jan 11 LHE 18R PAD 1+F,2 05 Jan 11 LHE 36L PAD 1+F,2 05 Jan 11 LHE 36R-Q 1+F,2 05 Jan 11

LKO 09 PAD 1+F,2 28 Feb 11 LKO 27 PAD 1+F,2 28 Feb 11

LXR 02-B 1+F,2 06 Feb 11 LXR 20-K 1+F,2 06 Feb 11

MLE 18 PAD 1+F,2 01 Feb 11 MLE 36 PAD 1+F,2 01 Feb 11

MUC 08L-A1 1+F,2 01 Mar 11 MUC 08R-B1 1+F,2 01 Mar 11 MUC 26L-B15 1+F,2 01 Mar 11 MUC 26R-A15 1+F,2 01 Mar 11

PEN 04-A 1+F 16 Feb 11 PEN 22-A 1+F,2 16 Feb 11





Date



A-319-112

PFO 11-A 1+F 01 Mar 11 PFO 29-E 1+F,2 01 Mar 11 PZU 17 PAD 1+F,2 16 Feb 11 PZU 35 PAD 1+F,2 16 Feb 11 RHO 07-F 1+F,2 28 Feb 11 RHO 25-A 1+F,2 28 Feb 11 RIY 06 PAD 1+F,2 01 Mar 11 RIY 24 PAD 1+F,2 01 Mar 11 RKT 16-A 1+F 16 Feb 11 RKT 34-B 1+F,2 16 Feb 11 SAW 06-J 1+F,2 28 Feb 11 SAW 24-E 1+F,2 28 Feb 11 SHJ 12-A 1+F,2 20 Feb 11 SHJ 30-G 1+F,2 20 Feb 11 SIN 02C-E11 1+F,2 06 Mar 11 SIN 02C-

E11SH (SHIP)

1+F,2 06 Mar 11

SIN 02L-W9 1+F,2 06 Mar 11 SIN 02L-

W9SH (SHIP)

1+F,2 06 Mar 11

SIN 20C-E1 1+F,2 06 Mar 11 SIN 20R-W1 1+F,2 06 Mar 11 SKG 10-F 1+F 01 Mar 11 SKG 16-A 1+F,2 01 Mar 11 SKG 28-F2 1+F,2 01 Mar 11 SKG 34-A 1+F 01 Mar 11 SLL 07-T 1+F 28 Feb 11 SLL 25-Z 1+F 28 Feb 11 SSH 04L-A 1+F,2 01 Mar 11 SSH 04R-M 1+F,2 01 Mar 11 SSH 22L-H 1+F 01 Mar 11 SSH 22R-G 1+F 01 Mar 11 TEQ 05-T1 1+F,2 16 Feb 11 TEQ 23-T3 1+F,2 16 Feb 11 TLS 14L-N8 1+F,2 28 Feb 11 TLS 14R-S11 1+F,2 28 Feb 11 TLS 32L-S2 1+F,2 28 Feb 11 TLS 32R-N1 1+F,2 28 Feb 11

TRV 14 PAD 1+F,2 16 Feb 11 TRV 32 PAD 1+F,2 16 Feb 11

UTP 18-A 1+F,2 16 Feb 11 UTP 36-D 1+F,2 16 Feb 11

VNS 09 PAD1 1+F,2 16 Feb 11 VNS 27 PAD 1+F,2 16 Feb 11

ZAH 17-J 1+F 16 Feb 11 ZAH 35-E 1+F 16 Feb 11

ZRH 10-B 1+F 16 Feb 11 ZRH 14 FULL 1+F 16 Feb 11 ZRH 16-E 1+F 16 Feb 11 ZRH 28-A 1+F 16 Feb 11 ZRH 32-H3 1+F 16 Feb 11 ZRH 34-E9 1+F 16 Feb 11





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Date

NOTE: 1. All RTOW charts have been computed with ‘AC OFF’ unless mentioned. 2. The above special charts have been provided to facilitate dispatch with optimum payload for

longhaul flights. For departure from other airports, MEL corrections may be applied directly to the Normal RTOW charts. However, if payload is affected, special RTOW/Takeoff Speeds data may be requested from ‘Dispatch(BAH)’.

Codes: R = Revised N = New A319-112 Fleet Effectivity: A9C-EU & EV 13 Jan 2011

A-319-112

INTENTIONALLY LEFT BLANK

A319

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