This is for my aviation class i need help with the perofmace part this can help https://www.faa.gov/training_testing/testing/supplements/media/FAA-CT-8080-7C.pdf
AERO 4123 Commercial Flight Operations Calculations homework #1 Refer to flight log on the back and figures 104, 105, and 106 from the FAA Computer Testing Supplement. Complete the flight log in the numbered boxes on the second page. Show your steps in calculations below. Assume 13E for problem magnetic variation. There are 12 numbers you will complete in the flight log on the back. Attach additional pages to show your work. Fem Approved: (all No. \"me LLB, DEPARTMENT OF TMBPORTATION FEDERAL MAT ION AMI! ISTRA'IION FLIGHT PLAN 2. AIFICIIAFI' IAIRCRAFI' TYPE! 5. DEPARTURE PUNT DEPARTURE TIME 7. CH UISING IDENTIFIGITION SPEGML EQUIPMENT ALTITUDE PROPOSED (2) ACTUAL (2) emooom ms TUCSON m\" TUS TUSSEBN, llOATNP, TNPJIOWNE 3 LAX s, DESHNATIW (Nam. or upon 11. REMARKS U0 . Level Of! PM u Pound. Per Hom- '"" m nouns mum-ea TEC = Tower Enroute Comm] L08 ANGBLES INT'L This ight il opmtin' nude: FAR 135' Lot Annie- '2' FUEL m BOARD '31 ALTERMTE Almm, 15' \"was" Aeome nouns BUR Mink-Gilda\"- n. oesnmmou owner/135mm: (0mm Panda- 15 you bor- _ GIVII. amour-r PILO'TB, FAR Part It I' II. In I'-" I [plan no opum under IIIIMOM my: \"In in " miom mm mm. sum. 09 m: mu rm empamw mm mud :1 .m lot mu mum (mm m or m. Fuonl Adm M d 1 05'. u mended), lmy 6| aV Eln nlln is amended I. I need walling plaice. Bee alto Pannier ~'remmheonee vDVFFIlI- ' . FM Form7233-1ca-nz} CLOSE VFR FLIGHT PLAN WITH FSS ON ARRIVAL FLIGHT LOG 120/35 ISAV7 120/35 ISA-7 100/ 45 ISA 100/45 o'l'lfln DATA: ' Includes Taxi Fuel Nm= Use 676 PPH Tomi Fuel Flow From uo To Start Of Descent. Use 726 PPH Tolal Fuel Flow For Reserve And Alternate Requirements. A Missed Approach Requires 1204! of Fuel. AERO 4123 Commercial Flight Operations Calculations homework #2 Instructions: Use the gures book to answer the questions. Document any calculations in attached sheets of paper. If math is involved in your answer, you need to write out each step to get full credit for your answer. Problems requiring this will be labeled CALCULATIONSjust after the problem number. 1. Refer to figures 451 and 452. Flaps setting: 8 Reported temperature: 25C Anti-Ice: OFF Airport elevation: 3000' Runway slope: 0% Takeoff weight: 70,000 lbs Find: Vr and V2 2. CALCULATIONS Refer to figures 173A and 428. Reported temperature: 15C Engine Bleeds: CLOSED Find: takeoff thrust setting 3. CALCULATIONS Refer to figures 57 and 58. Brake release weight: 115,000 lbs Cruise pressure altitude: 34,000' Airport elevation: 6,000' ISA temperature: ISA +10 Find: aircraft weight at top of climb (TOC) 4. CALCULATIONS Refer to figures 74 and 75. Flap setting: 30 Aircraft weight: 95,000 lbs Reported temperature: 10F Airport elevation: 2,300' Wing anti-ice: 2 ON A/C bleed: ON Runway assigned: 31 Surface wind: 020/20 Find: go-around EPR, and VREF+10 5. Refer to figure 392. Reported temperature: +35C Pressure altitude: 4,000' Cabin heat: OFF Find: maximum engine torque for takeoff CALCULATIONS Refer to figure 67. Distance of trip: 750 nm Average wind component: 50 kt TW Find: trip time and trip fuel Refer to figure 72. Weight at engine failure: 110,000 lbs Engine anti-ice: OFF Wing anti-ice: OFF Engine A/C bleed: OFF ISA temperature: +10C Find: optimum driftdown speed and level off altitude CALCULATIONS Refer to figure 85. Weight: 175,000 lbs Engines operating: 3 Altitude assigned: 10,000' Holding time: 40 minutes Find: fuel burn for the hold
