1 / 24

Aircraft Performance

Aircraft Performance. Osama Habahbeh. Takeoff Performance. Take Off Wt Performance Due to Engines. OAT. Take Off Wt Performance Due to Aerodynamics. OAT. Grad 1. Combined Take Off Wt Performance. Grad 2. OAT. T ref. Takeoff Performance. Thrust Rating.

avram-caldwell
Download Presentation

Aircraft Performance

An Image/Link below is provided (as is) to download presentation Download Policy: Content on the Website is provided to you AS IS for your information and personal use and may not be sold / licensed / shared on other websites without getting consent from its author. Content is provided to you AS IS for your information and personal use only. Download presentation by click this link. While downloading, if for some reason you are not able to download a presentation, the publisher may have deleted the file from their server. During download, if you can't get a presentation, the file might be deleted by the publisher.

E N D

Presentation Transcript

  1. Aircraft Performance Osama Habahbeh

  2. Takeoff Performance Take Off Wt Performance Due to Engines OAT Take Off Wt Performance Due to Aerodynamics OAT Grad 1 Combined Take Off Wt Performance Grad 2 OAT T ref

  3. Takeoff Performance

  4. Thrust Rating

  5. Example Minimum Control Speeds

  6. MAXIMUM FLAPS/SLATS SPEEDS ECAM: Electronic Centralized Aircraft Monitoring

  7. Example Speeds PERFORMANCE/ LPC

  8. PERFORMANCE/ LPC

  9. Example FIND MTOW WITH AND WITHOUT FAILURE AND COMPARE WITH MMEL FINDING. • TAIL NO.: JY-AIB • WIND= 0 DEG/KT • OAT= 35 C • QNH= 1013 HPA • FLAPS: OPT CONF • A/COND: OFF • A/ICE: OFF • DRY RWY • CG FORWARD • THRUST OPTION: TOGA • INOP ITEM: ENG A-ICE VALVE POSITION STUCK OPEN • A/P: OJAI • RWY: 08R PERFORMANCE/ LPC

  10. Using LPC WEIGHT DECREMENT= (MTOW WITHOUT FAILURE)- (MTOW WITH FAILURE) = 251711 KG - 243857 KG = 7854 KG PERFORMANCE/ LPC

  11. Using takeoff charts In Amman, ISA= 15 C - (2400 FT*(2 C/1000 FT)) = 15 C - 4.8 C = 10.2 C OAT= 35 C ISA + 5= 10.2 + 5 = 15.2 C OAT (35 C) > ISA + 5 (15.2 C) USING MMEL: WEIGHT DECREMENT = 13000 KG PERFORMANCE/ LPC

  12. MMEL PERFORMANCE/ LPC

  13. MMEL PERFORMANCE/ LPC

  14. Solution DIFFERENCE BETWEEN LPC AND MMEL: = 13000 – 7854 = 5146 KG Anti-Ice and Air-Conditioning are called “Bleeds” PERFORMANCE/ LPC

  15. Contaminated Runway

  16. Example Landing Performance

  17. Cruise - One Engine Inoperative

  18. Ground to Air Distance

  19. Aircraft Maximum Operating Speed (VMO, MMO)

  20. Update Airport Data Airport Raw Data Format Conversion & Obstacle reduction Data in Airport Manager format Import filtered data into PEP Import data into LPCA Prepare update files Running Update component in LPCU using update files PERFORMANCE/ LPC

  21. Update Aircraft Data Receive update files from Airbus Update PEP Prepare Update Files Update LPCA Running Update Component to Update LPCU PERFORMANCE/ LPC

  22. Update miscellaneous data Update LPCA Prepare Update Files Running Update component in LPCU using update files Note: In cases where update is not possible, a complete new installation is done PERFORMANCE/ LPC

More Related