Climb Calculations. Points to note: Climb time, fuel burn, and distance covered will be greater in the following conditions.

Similar documents
Flying The Boeing Advanced

PPL Exam 1 Working File. Where significant calculation/thinking is required.

Flying The Boeing

Flying The Embraer Brasilia (EMB-120)

1. You are flying near your favorite VOR. You experience 15 of bearing change in 11 minutes 36 seconds. How far are you from the station?

Takeoff Performance. A 1 C change in temperature from ISA will increase or decrease the takeoff ground roll by 10%.

2. At a ground speed of 184 knots, what will be the time required to cover 288 nautical miles? a. 86 minutes b. 90 minutes c. 94 minutes d.

Performance/Pilot Math

5. With winds aloft of 112 at 34 knots, TAS of 265 km/hr, and a TC of 057, what is the groundspeed and wind correction angle (WCA)?

PPL Exam 3 Working File. Where significant calculation/thinking is required.

Flight Planning & Aircraft Performance Part 2

Commercial Maneuvers for PA28RT-201

THE FLIGHT COMPUTER AND NAVIGATION PLOTTER

THE FLIGHT COMPUTER AND NAVIGATION PLOTTER

Lesson 5 Buffet Boundaries VMO/MMO Limits

CESSNA 172-SP PRIVATE & COMMERCIAL COURSE

Aircraft Performance Calculations: Descent Analysis. Dr. Antonio A. Trani Professor

Engine Performance reciprocating engine, turboprop engine, turbofan engine turbojet engine Manifold pressure (MAP) waste gate critical altitude

Airbus Series Vol.2 (c) Wilco Publishing feelthere.com

FLIGHT PERFORMANCE AND PLANNING (2) PERFORMANCE

Compiled by Matt Zagoren

GO AROUND PNF 3.THRUST REDUCTION/ACCELERATION ALTITUDE 1.GO AROUND INITIATION 5.DIVERSION. 4.HOLD (missed approach) 2.

Performance. Saturday, December 22, 2012

Mastering the Mechanical E6B in 20 minutes!

PILOT WIZZ - THE PILOTS COMPANION PilotWiz 1.0.5

I2103 WORKSHEET. Planned Route: Takeoff: KNSE, RWY 32 Altitude: 12,000 Route: RADAR DEPARTURE. Syllabus Notes None

SUPPLEMENT SEPTEMBER 2010 HIGH ALTITUDE TAKEOFF AND LANDING (ABOVE 14,000 FEET PRESSURE ALTITUDE) MODEL AND ON 68FM-S28-00 S28-1

Learning. Goals Speeds. Air speed. the air ASI. figure 1. Page 1 of 6. Document : V1.1

Takeoff and Landing Performance

TECHNIQUES FOR OFF AIRPORT OPERATIONS

SULAYMANIYAH INTERNATIONAL AIRPORT MATS

Civil Air Patrol Auxiliary of the United States Air Force

AIR NAVIGATION. Key Revision. Press F5 to start.

CALCULATING IN-FLIGHT WINDS

Normal T/O Procedure. Short Field T/O Procedure

LANDING TABLE OF CONTENTS

PROCEDURES GUIDE CESSNA 172N SKYHAWK

I2102 WORKSHEET. Planned Route: Takeoff: KNSE, RWY 32 Altitude: 12,000 Route: RADAR DEPARTURE. Syllabus Notes None. Special Syllabus Requirements None

PRIVATE PILOT MANEUVERS Practical Test Standards FAA-S A

See the diagrams at the end of this manual for judging position locations.

Visualized Flight Maneuvers Handbook

1. Sign in personnel, aircraft, and vehicles. Use mission flow chart

3rd Eurocontrol CDO Workshop

ENR 3. ATS ROUTES. For detailed descriptions of specific lower altitude ATS routes, refer to current editions of the following publications:

MOUNTAIN FLYING TEST

OBSTACLE DEPARTURE PROCEDURES Part 3

I2101 SIMULATOR ABBREVIATED CHECKLIST

Tecnam Eaglet Standard Operating Procedures and Maneuvers Supplement

Noise Abatement Takeoff 1 Close In Profile

Descent Planning with a Mechanical E6-B Flight Computer

Pressure and Density Altitude

VFR Circuit Tutorial. A Hong Kong-based Virtual Airline. VOHK Training Team Version 2.1 Flight Simulation Use Only 9 July 2017

Civil Air Patrol Auxiliary of the United States Air Force

CATS Workshop Target Windows modelling

Cessna 172R Profiles

FALCON SERVICE ADVISORY

DON T TO MATH IN THE COCKPIT

Answer Key. Page 1 of 5. 1) What is the maximum flaps-extended speed? A. 100 MPH. B. 65 MPH. C. 165 MPH. 2) Altimeter 1 indicates

FAA-S-ACS-6 June 2016 Private Pilot Airplane Airman Certification Standards. Task ACS Settings

Aviation Merit Badge Knowledge Check

NIFA CRM / LOFT CONTESTANT BRIEFING

SCT Trajectory & Separation Optimization

AIP MACAO GUANG ZHOU FIR HONG KONG FIR AD2-VMMC-60 SID MACAO RWY MAY 2016 (BIGRO 4 D, MIPAG 5 D, NLG 5 D, SHL 5 D) CAT A, B, C, D

CIVIL AIR PATROL United States Air Force Auxiliary Cadet Program Directorate. Cessna 172 Maneuvers and Procedures

Wake Vortices OPERATIONS. Where do Wake Vortices come from? What are the characteristics of wake vortices? CLAUDE LELAIE Former Head of Flight Test

Figure 1 BASIC AIRCRAFT PITOT-STATIC SYSTEM

VI.B. Traffic Patterns

Flight Profiles are designed as a guideline. Power settings are recommended and subject to change based

NORMAL TAKEOFF PILOT TRAINING MANUAL KING AIR 200 SERIES OF AIRCRAFT

Preliminary Study of Aircraft Dynamics and Performance: High Gust Condition Aspect

CSA 2018 ANNUAL QUIZ. 1. List the following speeds for each ship you fly. Assume single person. Solitaire Grob103 SGS 232 LS-4.

AEROCET MODEL 3500L/3500 FLOATS

NORMAL TAKEOFF AND CLIMB

NUCLEAR WEAPON DELIVERY WITH THE USE OF BOMBING TIMERS

Bonanza/Debonair Pilots

Get more out of life. AFTER ALL YOU VE ACHIEVED, WHY COMPROMISE NOW?

Lufthansa Flight Training (LFT) GmbH (Preliminary Text) Instrument Flight Procedures

LNAV & VNAV Integration Review Basics

AVIATION SAFETY BULLETIN

Vortex Generator Installation Addendum

Local Rules for F4C and H and F4K to be applied at the Championships

Tutorial A2A B377 Captain Of The Ship

Report on Phase 2 Causal Modeling for Schiphol Airport

GENERAL AVIATION - CLIMBING

South African Powered Paragliding Theoretical Knowledge Test

FLYING TO BANKSTOWN AND BACK TO BATHURST. Suggestions. Errol Chopping, December, Have Sydney VTC and Sydney VNC Charts

How to survive an engine failure in a single engine aircraft

C-182P MANEUVERS GUIDE TABLE OF CONTENTS

Glide Calculator SGS (e-version Jan 2007)

Aircraft Performance

Time-based Spaced Continuous Descent Approaches in busy Terminal Manoeuvring Areas

Lat. & Long. Review. Angular distance N or S of equator Equator = 0º Must indicate N or S North pole = 90º N

Gleim ATP FAA Knowledge Test 2011 Edition, 1st Printing Updates December 6, 2010

General. Procedure Checklists. Emergency Procedures. FSD Aerostar 700P Superstar

Enhanced Features and Functions Guide. English

Comparison of the Dispersant Mission Planner 2 (DMP2) and Estimated Dispersant System Potential (EDSP) Calculators

ABS/BPPP Performance Worksheet: Baron/Travel Air Pilots

OPERATION INSTRUCTIONS

Cessna 152 Standardization Manual

1. Determine his speed when he reaches the photo radar car.

Transcription:

B727 Flight Planning Climb page 1. Climb Calculations General In this assignment you will learn how to assess the climb time, fuel burn off (kilograms), and nautical miles covered in the enroute climb from your departure airport. Points to note: Climb time, fuel burn, and distance covered will be greater in the following conditions. Hot ambient temperatures. High aircraft brake release weights (takeoff weight). Higher cruise altitudes. Abbreviations used: BRW is the brakes release weight (Takeoff weight). TopC is the Top of Climb (ie: start of the cruise zone). ETI is the planned estimated elapsed time interval, and is expressed in minutes. Kg is the fuel burnt in kilograms. ANM is the air nautical miles. All B727 manual distances are expressed in air nautical miles. GNM is ground nautical miles. This is the air nautical miles quoted in the planning manual, corrected for average head or tail wind affecting the flight during the climb. In head wind conditions the ANM will be There are 3 climb tables presented in the B727 planning manual. One for ISA conditions (page 2-8), one for ISA+10 (page 2-9), and one for ISA+20 conditions (page 2-10). There are occasions where you will need to practice your interpolation skills, extracting from say the ISA and ISA+10 tables to get data for ISA+7 for example. At times you will need to set out a four-way interpolation because of a BRW that is also between book values. Interpolate very accurately, as rounding up or down on weights or temperatures can cause significant degradation in accuracy. Extraction of climb data No. 1: Data given: BRW 76, 000 kg. Average temperature in climb is ISA. Wind NIL Cruise level FL330. Extract from B727 manual page 2-8. ISA Enter BRW Enter cruise level FL330 Climb time 76, 000 kg 21 min/2, 800 kg 130 anm 3 engine fuel burn off (FBO) Air nm in climb. GNM same in nil wind

B727 Flight Planning Climb page 2. Extraction of climb data No. 2: Data given: BRW 80, 000 kg. Average temperature in climb is ISA +10. Headwind component 60 kt Cruise level. Extract from B727 manual page 2-9. ISA+10 Enter BRW Enter cruise level Climb time 80, 000 kg 26 min/3, 250 kg 165 anm 3 engine fuel burn off (FBO) Air nm in climb. GNM same in nil wind With a head wind we will cover more air nm than GNM. It is GNM that is of interest to us. A 60 kt headwind component means that if we were in the climb for 60 minutes, the GNM would be 60 nm less than the air distance shown in the manual. We are infact only subjected to this wind for 26 minutes in this case, so the nav computer set-up would be as shown below. Step 1. Set wind component of 60 kt Step 2. Opposite 26 minutes read 26 nm. The ground nautical miles (GNM) covered in the climb would be 139 gnm (ie: 165 ANM - 26 nm). Net climb data is... 26 min/3250 kg/139 GNM

B727 Flight Planning Climb page 3. Extraction of climb data No. 3: Data given: BRW 84, 000 kg. Average temperature in climb is ISA +20. TAIL wind component 30 kt Cruise level FL290. Extract from B727 manual page 2-10. ISA+20 Enter BRW Enter cruise level FL290 Climb time 84, 000 kg 39 min/4, 400 kg 254 anm 3 engine fuel burn off (FBO) Air nm in climb. GNM same in nil wind With a TAIL wind we will cover less air nm than GNM. It is GNM that is of interest to us. A 30 kt tailwind component means that if we were in the climb for 60 minutes, the GNM would be 30 nm more than the air distance shown in the manual. We are infact only subjected to this wind for 39 minutes in this case, so the nav computer set-up would be as shown below. Step 1. Set wind component of 30 kt Step 2. Opposite 39 minutes read 19.5 nm. (Say 20 nm) The ground nautical miles (GNM) covered in the climb would be 274 gnm (ie: 254 ANM + 20 nm). Net climb data is... 39 min/4400 kg/274 GNM

B727 Flight Planning Climb page 4. Extraction of climb data No. 4: This time we must interpolate between the ISA page and the ISA+10 page to get data relating to ISA+5. Data given: BRW 72, 000 kg. Average temperature in climb is ISA +5. TAIL wind component 50 kt Cruise level FL330. Extract from B727 manual pages 2-8 (ISA) and 2-9 (ISA+10). ISA data ISA+10 data 72, 000 kg ISA+5 72, 000 kg FL290 19 min/2, 500 kg 116 anm 21 min/2, 675 kg 132 anm 23 min/2, 850 kg 148 anm Step 1. Set wind component of 50 kt Step 2. Opposite 21 minutes read 17.5 nm. (Say 18 nm) The ground nautical miles (GNM) covered in the climb would be 150 gnm (ie: 132 ANM + 18 nm). Net climb data is... 21 min/2675 kg/150 GNM

B727 Flight Planning Climb page 5. Extraction of climb data No. 5: This time we must interpolate between the ISA+10 page and the ISA+20 page to get data relating to ISA+15. Data given: BRW 68, 000 kg. Average temperature in climb is ISA +15. HEAD wind component 45 kt Cruise level FL350. Extract from B727 manual pages 2-9 (ISA+10) and 2-10 (ISA+20). ISA+10 data ISA+20 data 68, 000 kg ISA+15 68, 000 kg FL350 23 min/2, 750 kg 149 anm 27 min/3, 050 kg 180 anm 31 min/3, 350 kg 211 anm Step 1. Set wind component of 45 kt Step 2. Opposite 27 minutes read 20 nm. The ground nautical miles (GNM) covered in the climb would be 160 gnm (ie: 180 ANM - 20 nm). Net climb data is... 27 min/3050 kg/160 GNM

B727 Flight Planning Climb page 6. Extraction of climb data No. 6: This time we must undertake a four way interpolation. To do this we need 4 sets of data, and we will calculate the data required in the centre of the data sheet. See below! Data given: BRW 78, 000 kg. Average temperature in climb is ISA +5. HEAD wind component 24 kt Cruise level. Extract from B727 manual pages 2-8 (ISA) and 2-9 (ISA+10). ISA +10 data ISA data 80, 000 kg 78, 000 kg 76, 000 kg 21 min/2, 850 kg 126 anm 20 min/2700 kg 120 anm 19 min/2, 550 kg 113 anm ISA+5 22.25 min/2900 kg 138 anm 26 min/3, 250 kg 165 anm 24.5 min/3100 kg 156 anm 23 min/2, 950 kg 146 anm Step 1. Set wind component of 24 kt Step 2. Opposite 22.25 minutes read 9 nm. The ground nautical miles (GNM) covered in the climb would be 129 gnm (ie: 138 ANM - 9 nm). Net climb data is... 22.25 min/2900 kg/129 GNM

B727 Flight Planning Climb page 7. Extraction of climb data No. 7: Data given: BRW 75, 000 kg. Average temperature in climb is ISA +8. HEAD wind component 36 kt Cruise level FL280. Extract from B727 manual pages 2-8 (ISA) and 2-9 (ISA+10). 76, 000 kg 75, 000 kg 72, 000 kg FL280 16 min/2, 350 kg 94 anm 15.75 min/2300 kg 15 min/2, 150 kg 86 anm Page 2-8 ISA FL280 ISA+8 18.75 min/2530 kg 112 anm FL280 20 min/2, 650 kg 120 anm 19.5 min/2588 kg 117 anm 18 min/2, 400 kg 108 anm Page 2-9 ISA+10 Step 1. Set wind component of 36 kt Step 2. Opposite 18.75 minutes read 11 nm. The ground nautical miles (GNM) covered in the climb would be 101 gnm (ie: 112 ANM - 11 nm). Net climb data is... 18.75 min/2530 kg/101 GNM Now attempt climb assignments 1 to 6.