General. Procedure Checklists. Emergency Procedures. FSD Aerostar 700P Superstar
|
|
- Felicia Barber
- 1 years ago
- Views:
Transcription
1 General The recommended procedures for coping with various types of emergencies and critical situations are provided in this section. These procedures are suggested as a course of action for coping with the particular condition described, but are not a substitute for sound judgment and common sense. Pilots should familiarize themselves with the procedures given in this section and be prepared to take appropriate action should an emergency arise. Most basic emergency procedures, such as power off landings, are a normal part of pilot training. Although these emergencies are discussed here, this information is not intended to replace such training, but only to provide a source of reference and review, and to provide information on procedures which are not the same for all aircraft. It is suggested that the pilot review standard emergency procedures periodically to remain proficient in them. Procedure Checklists AIRSPEEDS FOR SAFE OPERATION One Engine Inoperative Air Minimum Control...85 KIAS One Engine Inoperative Best Angle of Climb...10 I KIAS One Engine Inoperative Best Rate of Climb KIAS Maneuvering KIAS Never Exceed KIAS ENGINE SECURING PROCEDURE (FEATHERING PROCEDURE) Throttle CLOSE Prop control FEATHER (1000 RPM min.). Mixture idle cut-off Boost pump OFF Fuel selector......off Magneto switch OFF Alternator OFF Bleed air press to OFF Auxiliary hydraulic ARMED Prop sync (if installed) MANUAL Electrical load. REDUCE Trim AS REQUIRED Fuel crossfeed.. AS REQUIRED ENGINE FAILURE DURING TAKEOFF (BEFORE LIFTOFF) If sufficient runway remains for a safe stop: Throttles...CLOSE IMMEDIATELY Brakes... AS REQUIRED - 1
2 If insufficient runway remains for a safe stop: Throttles...CLOSE IMMEDIATELY Brakes...MAXIMUM (while runway remains) Mixtures...IDLE CUTOFF Fuel selectors... OFF Magneto switches.... OFF Battery... OFF Directional control MAINTAIN (maneuver to avoid obstacles) Crew and passengers...evacuate ENGINE FAILURE DURING TAKEOFF (AFTER LIFTOFF) If sufficient landing area remains for a safe stop: Throttles.. CLOSE Gear.. CHECK DOWN Flaps. FULL DOWN Airspeed. ESTABLISH 95 KIAS Brakes.. AS REQUIRED (after touchdown) If insufficient landing area remains for a safe stop and the decision is made to abort the takeoff: Throttles CLOSE IMMEDIATELY Gear......DOWN (terrain permitting) Flaps FULL DOWN Airspeed KIAS Mixtures IDLE CUTOFF Fuel selectors OFF Magneto switches..... OFF Battery... :... OFF Land avoiding obstacles. If insufficient landing area remains for a safe stop and the decision is made to continue the takeoff: Warning! Negative climb performance may result from an engine failure occurring after lift-off and before the landing gear and flaps have been retracted, the failed engine propeller feathered and a speed of 116 KIAS has been obtained. One engine inoperative climb performance is also affected by aircraft weight, density altitude and other ambient conditions. Lateral/ directional control maintain Airspeed ACCELLERATE to 101 KIAS Mixture controls.. FULL RICH Prop controls FULL FORWARD Throttles ADVANCE to 42.0 in. MAP Auxiliary hydraulic ON Gear UP Flaps UP Inoperative engine. DETERMINE Prop control (inoperative engine). FEATHER Airspeed KIAS after all obstacles have been cleared - 2
3 Trim AS REQUIRED Climb straight ahead (avoiding obstacles and attain sufficient altitude to execute One Engine Inoperative Landing procedure. Inoperative engine... SECURE (Refer to Engine Securing Procedure) ENGINE FAILURE DURING FLIGHT (BELOW 93 KIAS) Power...IMMEDIATELY REDUCE Lateral/ directional control... MAINTAIN Pitch attitude...lower nose to attain speed above 93 KIAS Continue with procedures given for "Engine Failure During Flight (Above 93 KIAS)." ENGINE FAILURE DURING FLIGHT (ABOVE 93 KIAS) Lateral/ directional control... MAINTAIN Airspeed...ATTAIN AND MAINTAIN at least 116 KIAS Mixtures... FULL RICH Power AS REQUIRED Boost pumps......on Fuel selectors ON If failed engine does not restart, continue as follows: Inoperative engine... DETERMINE Inoperative engine... SECURE (Refer to Engine Securing Procedure) Land as soon as practical at nearest suitable airport using the "One Engine Inoperative Landing" procedure. - 3
4 CROSSFEED (X-FEED) WITH INOPERATIVE ENGINE CAUTION Fuel system limitations outlined in Normal and Aircraft Systems checklists must be adhered to for crossfeed operation. When either X-FEED (crossfeed) selector is in the X-FEED position, the selected engine is obtaining its total fuel supply from the opposite wing fuel tank. Frequently monitor selected wing fuel tank quantity. Level coordinated flight...maintain Fuel selector (operative engine)...x-feed Fuel quantity (selected wing tank)... MONITOR FREQUENTLY After utilizing required fuel from inoperative engine wing fuel tank and prior to initiating descent, continue as follows: Fuel selector (operative engine)... ON AIR START (UNFEATHERING PROCEDURE) Fuel selector... ON Boost pump... ON Mixture IDLE CUT-OFF Throttle OPEN 1/2 inch Prop control SLIGHTLY FORWARD of feather detent Starter ENGAGE, released to BOTH Mixture.. FULL RICH Prop control.. ADJUST to 2000 RPM Throttle.. ADJUST to 15 in. MAP Oil pressure...check Boost pump... OFF, unless failure was engine driven fuel pump Alternator...ON Bleed air.. PRESS to ON Electrical equipment... ON as desired Engine temperature/ pressure...normal Prop controls... SET AS DESIRED Throttles... SET AS DESIRED Prop sync... ON AS DESIRED Mixtures SET Trim... AS REQUIRED - 4
5 ONE ENGINE INOPERATIVE LANDING Inoperative engine.. SECURED (Refer to Engine Securing Procedure) Altimeter SET Seat belts/ harnesses secure Boost pump (operative engine) ON Mixture (operative engine) FULL RICH Fuel selector (operative engine) ON X-FEED annunciator light... CHECK OUT Prop control (operative engine)... FULL FOR WARD Flaps 20 DOWN, do not extend more than 20 flaps Airspeed... MAINTAIN 116 KIAS minimum Throttle (operative engine)...as REQUIRED When landing is assured: Gear DOWN Gear down lights...,... 3 GREEN ON Airspeed (approach) Flaps UP KIAS Flaps 20 DOWN KIAS Throttle (operative engine)...retard slowly and flare for landing Directional control MAINTAIN as power is reduced Braking.. AS REQUIRED ONE ENGINE INOPERATIVE GO-AROUND WARNING Under certain combinations of aircraft weight, configuration, ambient conditions, and airspeeds a go around attempt may result in negative climb performance. Avoid if possible; but if necessary: Airspeed MAINTAIN climb speed Best angle K IAS Best rate KIAS Mixture (operating engine)......full RICH Prop control {operating engine) FULL FORWARD Throttle (operating engine) ADVANCE to 42.0 in. MAP Auxiliary hydraulic ARMED Gear UP Flaps.. (in steps) UP Trim... AS REQUIRED DECREASING MANIFOLD PRESSURE Prop control (cruise flight) SELECT HIGHER RPM Alternate air PULL OPEN - 5
6 ENGINE OVERHEAT Boost pump ON Mixture.. ENRICH Power REDUCE Airspeed. INCREASE (if altitude permits) LOSS OF OIL PRESSURE Engine.SECURE (Refer to Engine Securing Procedure) ALTERNATOR FAILURE Failed alternator. DETERMINE NOTE The appropriate alternator warning light should illuminate, however certain multiple failures may not annunciate. These failures may be determined by monitoring the voltammeter. Failed alternator OFF Electrical load.. REDUCE Circuit breaker (failed alternator) IN If circuit breaker resets satisfactorily: Failed alternator...on Volt-ammeter...CHECK Electrical load...increase AS REQUIRED If circuit breaker will not reset or if alternator will not re-excite: Failed alternator.. OFF Electrical load......maintain AT MINIMUM RADIO MASTER SWITCH/RELAY FAILURE Avionics ALL OFF Radio master ON Avionics ON only as required HYDRAULIC SYSTEM MALFUNCTIONS EMERGENCY GEAR EXTENSION (Loss of hydraulic system pressure) Airspeed...ESTABLISH below 130 KIAS Gear/Door release.. PULL OUT Gear handle...down Gear ind. lights... 3 YELLOW The hydraulic lines are opened allowing the hydraulic cylinders on the landing gear to drain. This process will take up to 20 seconds. The gears should free-fall extend through the doors under their own weight. Gear ind. lights... 3 green ON - 6
7 WARNING This process will destroy the hydraulic cylinders, transmission lines and seals for each landing gear. Therefore, it will not longer be possible to retract the landing gear. Replacement of the entire gear hydraulic system will be necessary. HYDRAULIC PRESSURE LOSS (ABOVE 500 PSI) A partial loss of hydraulic system pressure is probably caused by a failure of the right engine driven hydraulic pump or loss of accumulator charge. Flap handle...select NEUTRAL Aux. hydraulic. ARM Hydraulic pressure MONITOR If hydraulic pressure does not stabilize at or above 500 PSI, continue with procedures given for "Hydraulic Pressure Loss (Below 500 PSI)." If hydraulic pressure stabilizes at or above 500 PSI continue as follows: Land as soon as practical at nearest suitable airport following normal "Before Landing" procedures, except as follows: Flaps. AS DESIRED return handle to neutral WARNING Flaps will not operate at hydraulic pressures below 500 PSI! HYDRAULIC PRESSURE LOSS (BELOW 500 PSI) Continuously decreasing or totally depleted hydraulic system pressure indication is probably caused by a system failure rather than a failure of the right engine driven hydraulic pump. Flap handle.. Immediately select NEUTRAL Aux. hydraulic...arm, if pressure does not stabilize at 900 to 1050 PSI, turn aux. hydraulic OFF NOTE If the failure is the right engine driven hydraulic pump, the aux. hydraulic pump will increase and stabilize pressure at 900 to 1050 PSI. If hydraulic pressure stabilizes at 900 to 1050 PSI by means of the auxiliary hydraulic pump, continue with "Hydraulic Pressure Loss (Above 500 PSI)." - 7
8 FUEL SYSTEM MALFUNCTIONS FUEL PUMP FAILURE IN FLIGHT (Engine driven) Affected engine: Boost pump...on Mixture... FULL RICH After engine regains normal power: Mixture... AS REQUIRED NOTE If both engine driven fuel pump and boost pump fail, the engine will be inoperative. Perform "Engine Securing Procedure (Feathering Procedure)" and conduct "One Engine Inoperative Landing" procedure at nearest suitable airport. LOW FUEL WARNING LIGHT ILLUMINATED (12 gallons or less in fuselage tank) WARNING Do not use X-FEED for descent and landing. CAUTION When the low fuel warning light first illuminates continuously there is a maximum of 12 gallons usable fuel remaining in the fuselage tank. THERE MUST BE FUEL IN THE FUSELAGE TANK TO ENSURE AN UNINTERRUPTED ENGINE FUEL SUPPLY. If an immediate landing is feasible or fuel does not remain' in both wing tanks, proceed as follows: Boost pumps (both)...on Fuel selectors (both)...on Execute a landing at nearest suitable landing area with fuel remaining. If an immediate landing is not feasible and fuel remains in both wing tanks, proceed as follows: Level coordinated flight...maintain Boost pumps (both)...on Power...REDUCE to maximum range Wing fuel quantities (both)...determine Fuel selectors (both) X-FEED At first indication of fuel pressure drop or power interruption and/ or prior to initiating descent, continue as follows: Fuel selectors (both) ON - 8
9 PRESSURIZATION SYSTEM MALFUNCTION DIFFERENTIAL PRESSURE ABOVE 4.45 PSI OR STRUCTURAL FAILURE OCCURS OR APPEARS IMMINENT Dump valve.... PRESS to DUMP Descent... INITIATE NOTE If cabin does not completely depressurize, lift guard on cabin door seal switch and press to DEFLATE. Land as soon as possible if actual or imminent structural failure is suspected. LOSS OF ELEVATOR CONTROL IN FLIGHT Perform normal Before Landing procedures, except as follows: Pitch changes... use elevator trim (short inputs) and engine power Landing gear DOWN Establish a long straight- in landing approach with approx, 500 FPM rate of descent. Flaps DOWN maximum, at least 500 ft. above runway Approach speed... MAINTAIN 110 KIAS minimum Landing...touch down slightly longer than normal, maintaining rate of descent at or below 500 FPM.do not flare with trim Throttles...CLOSED at touchdown EMERGENCY DESCENT CAUTION If pressurized, the following procedures will result in an immediate loss of pressurization and the cabin altitude will rise at an uncontrolled rate until approximately equal to the airplane's altitude. Fuel selectors (both) ON Throttles......FULL CLOSED Prop controls......full FORWARD Airspeed KIAS ATC ADVISE After reaching desired safe altitude, continue as follows: Throttles... ADVANCE slowly to 15 in. MAP Prop controls...select 2000 RPM Cabin altitude control SELECT and obtain a cabin altitude equal to or higher than flight altitude Engine temperatures/ pressures...normal Prop controls... SET AS DESIRED - 9
10 Throttles... SET AS DESIRED Mixtures... SET AS DESIRED GEAR UP LANDING Radio... inform ground personnel Fuel...burn off (if time allows) Passengers...brief Cabin baggage... stow Normal landing checklist...complete Gear... UP Bleed air (both). PRESS to OFF Cabin door seal. DEFLATE Electrical load...reduce to minimum Alternators (both)...off Make a normal approach with FULL DOWN flaps. Boost pumps (on short final)...off When over landing area and landing assured: Prop controls. FEATHER Mixtures. IDLE CUT-OFF Touch down at minimum safe airspeed and level attitude. Fuel selectors OFF Hydraulic shutoff valve OFF Battery OFF Crew and passengers.. EVACUATE - 10
Beechcraft Duchess 76 Maneuver Notes
Beechcraft Duchess 76 Maneuver Notes I. Maneuver notes for Performance (AOA V), Slow Flight and Stalls (AOA VIII), Emergency Operations (AOA X), and Multiengine Operations (AOA XI) a. Maneuvers addressed:
Single Engine Complex Training Supplement PA28R-201 Piper Arrow III (Spring 2016 Revision)
Single Engine Complex Training Supplement PA28R-201 Piper Arrow III (Spring 2016 Revision) V-speed Quick Reference V-Speed KIAS Description Airspeed Indicator Marking VSO 55 Stall speed in landing configuration
Flight Profiles are designed as a guideline. Power settings are recommended and subject to change based
MANEUVERS AND PROCEDURES Flight Profiles are designed as a guideline. Power settings are recommended and subject to change based upon actual conditions (i.e. aircraft weight, pressure altitude, icing conditions,
CIVIL AIR PATROL United States Air Force Auxiliary Cadet Program Directorate. Cessna 172 Maneuvers and Procedures
CIVIL AIR PATROL United States Air Force Auxiliary Cadet Program Directorate Cessna 172 Maneuvers and Procedures This study guide is designed for the National Flight Academy Ground School. The information
www.guatemala-skies.com GUATEMALA GENERAL AVIATI INFORMATI TO GO Contents: Cessna 172 XP 1977 V Speeds & checklist Guatemala Radio Frequencies Emergency Transponder Codes & ATC Light Signals MGGT airport
NORMAL TAKEOFF PILOT TRAINING MANUAL KING AIR 200 SERIES OF AIRCRAFT
NORMAL TAKEOFF Climb-Out 1. Accelerate to 160 KIAS 2. Landing/Taxi lights: Out 3. Climb Checklist complete 1. 160 KIAS up to 10,000 ft 2. Decrease 2 KIAS per 1,000 ft above 10,000 ft to 130 KIAS at 25,000
Cessna 172S Skyhawk Standardization Manual
Cessna 172S Skyhawk Standardization Manual This manual is to be utilized in conjunction with the manufacturers approved POH/ AFM and the Airplane Flying Handbook (FAA-H-8083-3A). This manual should be
AEROCET 3400 AMPHIBIOUS FLOATS
FOUND SUPPLEMENT M400-S10 Transport Canada Approved Flight Manual Supplement For AEROCET MODEL 3400 AMPHIBIOUS FLOATS This supplemental manual is applicable to Aerocet Model 3400 amphibious float equipped
WIPLINE 3450 SEAPLANE FLOATS
FOUND SUPPLEMENT M400-S08 Transport Canada Approved Flight Manual Supplement For WIPLINE MODEL 3450 SEAPLANE FLOATS This supplemental manual is applicable to Wipline Model 3450 seaplane float equipped
Visualized Flight Maneuvers Handbook
Visualized Flight Maneuvers Handbook For High Wing Aircraft Third Edition For Instructors and Students Aviation Supplies & Academics, Inc. Newcastle, Washington Visualized Flight Maneuvers Handbook for
Compiled by Matt Zagoren
The information provided in this document is to be used during simulated flight only and is not intended to be used in real life. Attention VA's - you may post this file on your site for download. Please
POWER-OFF 180 ACCURACY APPROACH AND LANDING
POWER-OFF 180 ACCURACY APPROACH AND LANDING OBJECTIVE To teach the commercial student the knowledge of the elements related to a power-off 180 accuracy approach and landing. COMPLETION STANDARDS 1. Considers
Bonanza/Debonair Pilots
Bonanza/Debonair Pilots Completing this worksheet is a great way to reinforce the proper speeds for operating your Bonanza or Debonair under varying operating conditions, and to understand the changes
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
Name: Answer Key Score: 1) What is the maximum flaps-extended speed? A. 100 MPH. B. 65 MPH. C. 165 MPH. 2) Altimeter 1 indicates A. 10,500 feet. B. 1,500 feet. C. 500 feet. 3) In the Northern Hemisphere,
Diamond DA-40. Training Supplement ATPFlightSchool.com. Revised
Diamond DA-40 Training Supplement Revised 2017-01-12 904-595-7940 ATPFlightSchool.com a Copyright 2017 Airline Transport Professionals. The content of this manual is furnished for informational use only,
Flying The Boeing
Flying The Boeing 757-200 This section includes Pilot s Operating Handbook and Checklists. The POH section is first, followed by the Checklists. FOM: This section includes performance data on the Boeing
PIPER CHEYENNE IIXL PA-31
DEPARTAMENTO SEGURIDAD OPERACIONAL SUBDEPARTAMENTO LICENCIAS SECCIÓN EVALUACIONES PIPER CHEYENNE IIXL PA-31 A.- Operations Limitations 1.- Speed (Kias) Va 184 Vne 242 Vmo 242 Vfe 15 181 Vle/Vlo (Extension)
Flying The Boeing Advanced
Flying The Boeing 727-200 Advanced This section includes Pilot s Operating Handbook and Checklists. The POH section is first, followed by the Checklists. FOM: This section includes performance data on
CHAPTER 8 MANEUVERS TABLE OF CONTENTS
CHAPTER 8 MANEUVERS TABLE OF CONTENTS Transition Airspeeds... 3 Checklists and callouts during maneuvers... 3 Guidance to better maneuver execution... 3 Taxiing... 5 Pre-Maneuver Checklist... 6 Clearing
See the diagrams at the end of this manual for judging position locations.
Landing Events Penalties General Judges should use airport diagrams, satellite pictures or other means to determine, as accurately as possible, assessments of landing pattern penalties. Judges should be
CAP-USAF FLIGHT MANEUVERS GUIDE
CAP-USAF FLIGHT MANEUVERS GUIDE February 2012 Flight Maneuvers Guide This guide describes and standardizes the instruction and performance of the various flight maneuvers described in Chapter 3 of AFI11-2CAP-USAF,
Flying The Embraer Brasilia (EMB-120)
Flying The Embraer Brasilia (EMB-120) This section includes Pilot s Operating Handbook and Checklists. The POH section is first, followed by the Checklists. FOM: This section includes performance data
SECRETARY OF THE AIR FORCE 17 APRIL 2000 LOADMASTER MAFFS CHECKLIST. Summary of Revisions: Redundant pages removed.
BY ORDER OF THE AFI 11-2C-130V3 CL-10 SECRETARY OF THE AIR FORCE 17 APRIL 2000 LOADMASTER MAFFS CHECKLIST Flying Operations This checklist establishes procedures for the operation of C-130 aircraft employed
Uncontrolled Copy AEROCET 3400 AMPHIBIOUS FLOATS. Transport Canada Approved Flight Manual Supplement For SUPPLEMENT S01
FOUND SUPPLEMENT S01 Transport Canada Approved Flight Manual Supplement For AEROCET MODEL 3400 AMPHIBIOUS FLOATS This supplemental manual is applicable to Aerocet Model 3400 amphibious float equipped airplanes.
Guidance Notes PRIVATE AND COMMERCIAL PILOT TRAINING
PRIVATE AND COMMERCIAL PILOT TRAINING September 2005 1 st Edition ACKNOWLEDGEMENT Transport Canada thanks the Federal Aviation Administration of the United States for their permission to use the chapter
Engine Failure after Takeoff
Circuit Training Engine Failure after Takeoff Although engine failure in modern aeroplanes is quite rare, the takeoff phase incorporates all the worst aspects of this type of emergency. The aeroplane is
I2102 WORKSHEET. Planned Route: Takeoff: KNSE, RWY 32 Altitude: 12,000 Route: RADAR DEPARTURE. Syllabus Notes None. Special Syllabus Requirements None
Planned Route: Takeoff: KNSE, RWY 32 Altitude: 12,000 Route: RADAR DEPARTURE Syllabus Notes None Special Syllabus Requirements None I2102 WORKSHEET Discuss a. IMC Emergencies NATOPS statement on sound
I2103 WORKSHEET. Planned Route: Takeoff: KNSE, RWY 32 Altitude: 12,000 Route: RADAR DEPARTURE. Syllabus Notes None
Planned Route: Takeoff: KNSE, RWY 32 Altitude: 12,000 Route: RADAR DEPARTURE Syllabus Notes None I2103 WORKSHEET Special Syllabus Requirements Proceed direct to homefield using any available NAVAID. Discuss
1 In The Biginning. Nice Air Operation Procedure Cessna 172
1 In The Biginning Check how many hours remains for next 100h inspection and check squawk before take airplane. Perform pre-flight inspection using check list. Report to the front desk if you need fuel,
VII.E. Normal and Crosswind Approach and Landing
References: FAA-H-8083-3; POH/AFM Objectives Key Elements Elements Schedule Equipment IP s Actions SP s Actions Completion Standards The student should be able to perform a normal approach and landing
BOEING AIRCRAFT WEIGH WORKSHEET
WEIGHING FACILITIES AND EQUIPMENT ITEM MECH INSP The airplane should be weighed inside a closed facility that will: Exclude all wind and drafts. Permit shutdown of air conditioning during the weighing
C2201 Briefing Guide (Worksheet)
T-6B JPPT 1542.166A Simulator Event Briefing Guide C2201 Briefing Guide (Worksheet) Planned Route: Takeoff: KNSE, Rwy 05 Altitude: MOA Limits Route: North MOA Training Device: UTD / OFT SYLLABUS S: Introduce
Piper Seminole. Training Supplement ATPFlightSchool.com $
Piper Seminole Training Supplement 904-595-7940 ATPFlightSchool.com 2017-08-10 $29.95 Brings Pilots & Airline Recruiters Together by PilotPool places you in front of airline recruiters before you reach
Aviation Merit Badge Knowledge Check
Aviation Merit Badge Knowledge Check Name: Troop: Location: Test Score: Total: Each question is worth 2.5 points. 70% is passing Dan Beard Council Aviation Knowledge Check 1 Question 1: The upward acting
PERFORMANCE MANEUVERS
Ch 09.qxd 5/7/04 8:14 AM Page 9-1 PERFORMANCE MANEUVERS Performance maneuvers are used to develop a high degree of pilot skill. They aid the pilot in analyzing the forces acting on the airplane and in
RUTAN 61 Long-EZ USER MANUAL. Virtavia Rutan 61 Long E-Z DTG Steam Edition Manual Version 1.0
RUTAN 61 Long-EZ USER MANUAL 0 Introduction The Rutan 61 Long-EZ is an incredibly popular home-built aircraft flown by pilots all over the world. The prototype of the Long-EZ first flew in 1979. Approximately
Pilot Training Manual & Logbook
Canberra Model Aircraft Club Canberra A.C.T Pilot Training Manual & Logbook Issue Date: November 2009 www.cmac.org.au Contents Learning to Fly Radio Controlled Aircraft... 3 Introduction... 3 Student Pilot
VII.H. Go-Around/Rejected Landing
VII.H. Go-Around/Rejected Landing References: FAA-H-8083-3; POH/AFM Objectives Key Elements Elements Schedule Equipment IP s Actions SP s Actions Completion Standards The student should develop knowledge
Homework Exercise to prepare for Class #2.
Homework Exercise to prepare for Class #2. Answer these on notebook paper then correct or improve your answers (using another color) by referring to the answer sheet. 1. Identify the major components depicted
C-182P MANEUVERS GUIDE TABLE OF CONTENTS
INTRODUCTION The following maneuver guide is designed to provide a technique for completing each VFR maneuver required by the FAA s Practical Test Standards for the Private Practical Test. By performing
Section - III SYSTEMS DESCRIPTION
Section - III SYSTEMS DESCRIPTION Pro Line 21 Table of Contents Page GENERAL... 10-3 BLEED AIR SYSTEM... 10-3 ENGINE AIR BLEED... 10-3 MIXING VALVE... 10-3 MAIN AIR VALVE... 10-3 PRESSURE REGULATOR and
Circuit Considerations
Circuit Training Circuit Considerations This briefing deals with those aspects of a normal circuit that were deferred during Circuit Introduction, to avoid student overload. Objectives To continue circuit
S-Tec System 55X Autopilot w/ Altitude Selector/Alerter
Cirrus Design Section 9 Pilot s Operating Handbook and FAA Approved Airplane Flight Manual Supplement For S-Tec System 55X Autopilot w/ Altitude Selector/Alerter When the S-Tec System Fifty Five X (55X)
Attitude Instrument Flying and Aerodynamics
Attitude Instrument Flying and Aerodynamics 2.1 TURNS 1. An airplane requires a sideward force to make it turn. a. When the airplane is banked, lift (which acts perpendicular to the wingspan) acts not
B787-8 AIRCRAFT WEIGH WORKSHEET
WEIGHING FACILITIES AND EQUIPMENT ITEM MECH INSP The airplane should be weighed inside a closed facility that will: Exclude all wind and drafts. Permit shutdown of air conditioning during the weighing
Straight and Level. Basic Concepts. Figure 1
Basic Concepts Straight and Level This lesson should start with you asking the student what they did in the last lesson, what do they remember, and determining if they have remembered correctly. We must
Flying The. Traffic Pattern. Skill Level: Basic
Flying The Now that you ve mastered a number of basic and intermediate flying skills, it s time to put them all to the test in the exercise that combines them all Flying The Traffic Pattern. In this Flight
HANDLINGSENSE LEAFLET 1 TWIN PISTON AEROPLANES
HANDLINGSENSE LEAFLET 1 TWIN PISTON AEROPLANES 1 INTRODUCTION 2 PERFORMANCE 3 ENGINE FAILURE DURING TAKE-OFF 4 EFATO IDENTIFYING FAILED ENGINE 5 OTHER EFATO CONSIDERATIONS 6 PRE-TAKE-OFF BRIEF 7 HANDLING
MOONEY AIRPLANE COMPANY, INC. LOUIS SCHREINER FIELD KERRVILLE, TEXAS FAA APPROVED: AIRPLANE FLIGHT MANUAL SUPPLEMENT MOONEY M20M, M20R, M20TN
MOONEY AIRPLANE COMPANY, INC. LOUIS SCHREINER FIELD KERRVILLE, TEXAS 78028 FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT FOR MOONEY WITH S -TEC SYSTEM 55X, TWO AXIS, AUTOPILOT INSTALLED MODEL NO. REG.
Republic Seabee Initial Checkout Syllabus
Republic Seabee Initial Checkout Syllabus By Steve Mestler Note: Any questions or comments should be directed to Steve at smestler@bellsouth.net INTRODUCTION The purpose of this syllabus is to provide
Ice Protection System
Cirrus Design Section 9 Pilot s Operating Handbook and FAA Approved Airplane Flight Manual Supplement for Ice Protection System When the Ice Protection System is installed on the Cirrus Design, this POH
II.E. Airplane Flight Controls
References: FAA-H-8083-3; FAA-8083-3-25 Objectives Key Elements Elements Schedule Equipment IP s Actions SP s Actions Completion Standards The student should develop knowledge of the elements related to
VT-31 On-Wing Gouge Packet
VT-31 On-Wing Gouge Packet Updated Oct 2014 by LT Sean Anderson Updated Oct 14 FAM-0 BRIEF OVERVIEW 1. Introductions. 2. Flight Schedule: - How to read VT-31 flight schedule (www.vt31.net). - Schedule
How to survive an engine failure in a single engine aircraft
How to survive an engine failure in a single engine aircraft Don't Go In Pointed End First There you are 110 kts, 3,000 ft., enjoying being in the air and out of contact with all the folks on the ground;
PILOT S OPERATING HANDBOOK AND FAA APPROVED AIRPLANE FLIGHT MANUAL for the CIRRUS DESIGN SR22
PILOT S OPERATING HANDBOOK AND FAA APPROVED AIRPLANE FLIGHT MANUAL for the CIRRUS DESIGN FAA Approved in Normal Category based on FAR 23. This document must be carried in the airplane at all times and
CONTENTS. Section 1. Main points. Section 2. Flight Preparation. Section 3. Pattern Flight
CONTENTS Section 1. Main points 1. Yak-52. General Information. 2. Aircraft Main Technical Data. 3. Engine Main Technical Data. 4. Aircraft Perfomance. 5. Operation limitations. 6. Some Practical Aerodynamic
Front Cover Picture Mark Rasmussen - Fotolia.com
Flight Maneuvers And Stick and Rudder Skills A complete learn to fly handbook by one of aviation s most knowledgeable and experienced flight instructors Front Cover Picture Mark Rasmussen - Fotolia.com
SUPPLEMENT TO AIRCRAFT FLIGHT MANUAL FOR MOTOR-DRIVEN ROPE WINCH TYPE RPM 11/01
SUPPLEMENT TO AIRCRAFT FLIGHT MANUAL FOR MOTOR-DRIVEN ROPE WINCH TYPE RPM 11/01 (Langenthaler-Winch) Aircraft-Manufacturer: Avions Robin SA Type of Aircraft: Robin DR 300-180R DR400-180R DR 400-200R DR
TERMS AND DEFINITIONS
Ch 05.qxd 5/7/04 7:02 AM Page 5-1 GENERAL This chapter discusses takeoffs and departure climbs in tricycle landing gear (nosewheel-type) airplanes under normal conditions, and under conditions which require
Republic Seabee. Initial Checkout Guide. By Steve Mestler. Note: Any questions or comments should be directed to Steve at
Republic Seabee Initial Checkout Guide By Steve Mestler Note: Any questions or comments should be directed to Steve at smestler@pbtcomm.net 3/20/2016 International Republic Seabee Owners Club INTRODUCTION
TM CL TECHNICAL MANUAL OPERATOR AND CREWMEMBER CHECKLIST ARMY MODELS EH-1H/X HELICOPTERS
TECHNICAL MANUAL OPERATOR AND CREWMEMBER CHECKLIST ARMY MODELS EH-1H/X HELICOPTERS HEADQUARTERS DEPARTMENT OF THE ARMY 5 NOVEMBER 1983 URGENT TM 55-1520-247-CL C2 CHANGE HEADQUARTERS DEPARTMENT OF THE
Takeoffs & Landings Refresher. By Wally Moran
Takeoffs & Landings Refresher By Wally Moran About Wally Moran Wally Moran is a retired airline captain and spent much of his career as a training instructor and check airman on aircraft including the
BASIC AIRCRAFT STRUCTURES
Slide 1 BASIC AIRCRAFT STRUCTURES The basic aircraft structure serves multiple purposes. Such as aircraft aerodynamics; which indicates how smooth the aircraft flies thru the air (The Skelton of the aircraft
Discuss: 1. Instrument Flight Checklist
INST 1 Prerequisites: 1. OFT: Tac 1 2. CBT: Basic Instrument Flight, IFR Navigation I & II Lessons P2 501, P2 502, & P2 503. Discuss: 1. Instrument Flight Checklist NATOPS 13.1.3 Instrument Flight Checklist
FLIGHT MANUAL SUPPLEMENT
FLIGHT MANUAL SUPPLEMENT HUSKY / RF 8001 SKIS This supplement is valid for The Husky A-1. The following derivates of the Husky may use this Supplement after the approval of a minor change to operate the
Spins and how to keep the pointy end of the airplane going forward
Spins and how to keep the pointy end of the airplane going forward 8/14/07 Evan Reed, cfievan@yahoo.com Ed Williams Outline Spins and their general characteristics Accident statistics and scenarios Some
Columbia 300 (LC40-550FG) Information Manual Revison No. 2 (January 2003)
Columbia 300 (LC40-550FG) Information Manual Revison No. 2 (January 2003) THE INFORMATION IN THIS MANUAL WAS TAKEN DIRECTLY FROM THE FAA APPROVED AIRPLANE FLIGHT MANUAL. SINCE THE DATA IN THE LANCAIR COLUMBIA
Revision Number Revision Date Insertion Date/Initials 1 st Ed. Oct 26, 00 2nd Ed. Jan 15, 08
List of Effective Pages * Asterisk indicates pages changed, added, or deleted by current revision. Retain this record in front of handbook. Upon receipt of a Record of Revisions revision, insert changes
AIR FACTS The Magazine for Pilots March 1949
AIR FACTS The Magazine for Pilots March 1949 THE PIPER CLIPPER By Leighton Collins In pursuing further his long held thesis that rather than getting bigger and heavier all the time the strictly personal
SULAYMANIYAH INTERNATIONAL AIRPORT MATS
KURDISTAN REGIONAL GOVERNMENT SULAYMANIYAH INTERNATIONAL AIRPORT MATS APPENDIX " O " SPEED CONTROL GUIDANCE ( First Edition ) April 2012 Prepared By Fakhir.F. Mohammed Civil Aviation Consultant APPENDIX
Dash8-200/300 - Warning Systems WARNING SYSTEMS CONTROLS AND INDICATORS. Page 1. Fast / Slow indicator and Stall Warning Test Switch
WARNING SYSTEMS CONTROLS AND INDICATORS Fast / Slow indicator and Stall Warning Test Switch Page 1 Stick Pusher and Shaker Page 2 GPWS Controls and indicators Page 3 CENTER CONSOLE GPWS Controls and indicators
XII.A-D. Basic Attitude Instrument Flight
References: FAA-H-8083-3; FAA-8083-3-15 Objectives Key Elements Elements Schedule Equipment IP s Actions SP s Actions Completion Standards The student should develop knowledge of the elements related to
CIRRUS DESIGN. PILOT S OPERATING HANDBOOK AND FAA APPROVED AIRPLANE FLIGHT MANUAL for the. All-Electric SR20 Aircraft Serials 1268 and Subsequent
PILOT S OPERATING HANDBOOK AND FAA APPROVED AIRPLANE FLIGHT MANUAL for the CIRRUS DESIGN All-Electric Aircraft Serials 1268 and Subsequent FAA Approved in Normal Category based on FAR 23. This document
HOW TO FLY AIRPLANES
HOW TO FLY AIRPLANES Complimentary Ebook Available from bob@safe-flight.net HOW TO FLY AIRPLANES BASIC AIRCRAFT CONTROL Robert Reser, Publisher bob@safe-flight.net Tempe, Arizona Copyright 2012-2016 by
2. Page 2-13, Figure 2-19, top figure; change the green label Altitude Indicator to Attitude Indicator.
FAA-H-8083-25A Pilot s Handbook of Aeronautical Knowledge Dated 2009 Errata as of January 21, 2011 1. Page 1-18, right column, 1 st paragraph, last sentence; change the uniform resource locator (URL) to
16 - Flight Testing. Flight Testing. February GGG Page 16-1
Flight Testing February 2003 16-GGG Page 16-1 16 - Flight Testing This Page Intentionally Left Blank Page 16-2 16-GGG February 2003 Contents 16.0 - Chapter Preface...16-4 16.0.1 - Parts List...16-4 16.0.2
Go around manoeuvre How to make it safer? Capt. Bertrand de Courville
Go around manoeuvre How to make it safer? Capt. Bertrand de Courville LOC I Workshop 2012 Salzburg Year 2010 Year 2011 Jan to June 2012 + IATA Tool Kit + FSF Initiatives + ICAO Worldwide Programm Capt.
Basic Ice Protection System
Cirrus Design Section 9 Pilot s Operating Handbook and FAA Approved Airplane Flight Manual Supplement for the Basic Ice Protection System When the Basic Ice Protection System is installed on the aircraft,
Fuselage, Wings and Stabilising Surfaces
Fuselage, Wings and Stabilising Surfaces Chapter 1 DESIGN PHILOSOPHIES The aircraft manufacturer will attempt to design an aircraft to take into account all the loads that it may experience in flight.
PRIMARY FLIGHT CONTROLS. AILERONS Ailerons control roll about the longitudinal axis. The ailerons are attached to the outboard trailing edge of
Aircraft flight control systems are classified as primary and secondary. The primary control systems consist of those that are required to safely control an airplane during flight. These include the ailerons,
TAKEOFF & LANDING IN ICING CONDITIONS
Original idea from Captain A. Wagner T TAKEOFF & LANDING IN ICING CONDITIONS here have been a number of accidents related to take-off in conditions in which snow and/or other forms of freezing precipitation
REPLENISHING, OXYGEN SYSTEM - SERVICING
REPLENISHING, OXYGEN SYSTEM - SERVICING TASK 610 801 1. Quantity Check of the Oxygen System A. Reference Information REFERENCE TASK 12 00 07 861 801 TASK 12 00 07 861 802 TASK 614 801 DESIGNATION Connect
Get more out of life. AFTER ALL YOU VE ACHIEVED, WHY COMPROMISE NOW?
Get more out of life. Owning an airplane changes you. From my first hours in a Cessna 140, the freedom and flexibility, the efficient use of time, and just the sheer beauty of flight have become indispensable
DASSAULT FALCON 900EX EASY SYSTEMS SUMMARY
DASSAULT FALCON 900EX EASY SYSTEMS SUMMARY Air Conditioning & Pressurization The material contained on this site is to be used for training purposes only. Do not use it for flight! Please note that this
PPL Exam 3 Working File. Where significant calculation/thinking is required.
Copyright Avfacts 2014 - All rights reserved. PPL practice exam 3/page 1. PPL Exam 3 Working File. Where significant calculation/thinking is required. Q5. Refer to the P Chart figure 3 in the CASA Training
accidents which arise due to non-observance of these instructions and the safety information herein.
3 GALLON PANCAKE COMPRESSOR Model: 50959 CALIFORNIA PROPOSITION 65 WARNING: You can create dust when you cut, sand, drill or grind materials such as wood, paint, metal, concrete, cement, or other masonry.
AIRPLANE INFORMATION MANUAL for the CIRRUS DESIGN SR20
AIRPLANE INFORMATION MANUAL for the CIRRUS DESIGN Aircraft Serials 1268 and Subsequent with Analog or Avidyne Avionics System At the time of issuance, this Information Manual was harmonized with the Pilot's
Elevator Concepts ltd. by Wurtec Krause Riverview, MI Fax:
Hydraulic System Set-up Ver. 1 4/22/13 18720 Krause Riverview, MI 48193 734.246.4700 Fax: 734.246.2547 www.elevatorconcepts.com ADJUSTMENTS HYDRAULIC SYSTEM SETUP BLAIN EV10 & EV100 ¾ VALVE Refer to Blain
5 Function Indicator. Outside Air Temperature (C) Outside Air Temperature (F) Pressure Altitude Density Altitude Aircraft Voltage STD TEMP SL 15000
5 Function Indicator +20 +40-5000 STD TEMP SL 15000 Outside Air Temperature (C) Outside Air Temperature (F) Pressure Altitude Density Altitude Aircraft Voltage 427 HILLCREST WAY REDWOOD CITY, CA 94062
Columbia 400 (LC41-550FG) Information Manual
Columbia 400 (LC41-550FG) Information Manual Revision No. 3 (November 2004) THE INFORMATION IN THIS MANUAL WAS TAKEN DIRECTLY FROM THE FAA APPROVED AIRPLANE FLIGHT MANUAL. SINCE THE DATA IN THE LANCAIR
INSTRUCTOR GUIDE REFERENCES: PUMPING APPARATUS DRIVER/OPERATOR HANDBOOK, FIRST EDITION, IFSTA
TOPIC: RELAY PUMPING OPERATIONS LEVEL OF INSTRUCTION: TIME REQUIRED: ONE HOUR INSTRUCTOR GUIDE MATERIALS: APPROPRIATE AUDIO VISUAL SUPPORT REFERENCES: PUMPING APPARATUS DRIVER/OPERATOR HANDBOOK, FIRST
The Addition of Vortex Generators for STOL performance and or for Meeting the Light Sport Aircraft Rules
The Addition of Vortex Generators for STOL performance and or for Meeting the Light Sport Aircraft Rules This modification allows the Europa XS or Classic aircraft to operate with a greater stall margin
Cirrus Design Section 9. Pilot s Operating Handbook and FAA Approved Airplane Flight Manual Supplement for the. TKS Anti-Ice System
Cirrus Design Section 9 Pilot s Operating Handbook and FAA Approved Airplane Flight Manual Supplement for the TKS Anti-Ice System Approved for Flight Into Known Icing (FIKI) 8.0 gallon usable capacity.
Ops Manual 05 Page 40
Ops Manual 05 Page 40 Ops Manual 05 Pg 41 I. PRE -FLIGHT PREPARATION. (a) EXTERNAL CHECKS --Before entering the cockpit, a detailed inspection of the sailplane for proper condition should be carried out
Dash8 - Q400 - Oxygen
12.16 (ATA 35) OXYGEN 12.16.1 Introduction There is a fixed oxygen system for the flight deck crew and observer. Separate portable oxygen systems are supplied for the cabin attendants and passengers. Separate
Federal Aviation Administration, DOT Pt. 23 FLIGHT CHARACTERISTICS General Trim Stall warning Spinning.
Federal Aviation Administration, DOT Pt. 23 21.620 Changes in quality system. After the issuance of a TSO authorization (a) Each change to the quality system is subject to review by the FAA; and (b) The
A-License Information Packet
A-License Information Packet 1. Objective The objective of this packet is to review several parts of the United States Parachute Association (USPA) A License Proficiency Card and to learn additional aspects
A Different Approach to Teaching Engine-Out Glides
A ifferent Approach to Teaching Engine-Out Glides es Glatt, Ph., ATP/CFI-AI, AGI/IGI When student pilots begin to learn about emergency procedures, the concept of the engine-out glide is introduced. The
BRITISH MICROLIGHT AIRCRAFT ASSOCIATION HOMEBUILT AIRCRAFT DATA SHEET (HADS) NO: HM18 ISSUE: 5. EuroFOX
EuroFOX (1) MANUFACTURER Individual aircraft are amateur constructed from kits manufactured by Aeropro s.r.o. in Slovakia. BMAA is responsible for continued airworthiness (2) UK IMPORTER EuroFOX Aviation,
Jetstream PMDG s British Aerospace REVIEW BY DR JOHN LATTANZIO
REVIEW PMDG s British Aerospace Jetstream 4100 REVIEW BY DR JOHN LATTANZIO Cleared for take-off OK here we go. Advance power levers slowly. Watch the EGT though, because if you exceed the maximum (e.g.