Van's Aircraft RV-7 Especificaciones técnicas

VAN’S AIRCRAFT RV-7

I-MKLK

AIRCRAFT FLIGHT MANUAL

_____________________________________________________________________

Make: Van’s Aircraft

Model: RV-7 Serial

No: 74141

Registration: I-MKLK

THE AIRPLANE MUST BE OPERATED IN COMPLIANCE WITH INFORMATION AND LIMITATIONS

CONTAINED IN THIS DOCUMENT.

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I-MKLK AIRCRAFT FLIGHT MANUAL

Foreword

I-MKLK is a Van’s aircraft (www.vansaircraft.com) RV-7 all- metal, low

wing, two seat, high performance aircraft. It was built by Marco Grilli

from a Van’s quick-build kit during the years 2013 until 2014 under the

supervision of C.A.P Club Aviazione Popolare (www.federazionecap.it).

Disclaimer

This aircraft is classified as “experimental”. Hence certain design

features may deviate from the typical “spam can” certified production

aircraft. This aircraft has been built by the builder to the best of his

knowledge and quality of craftsmanship. Nonetheless, operating this

aircraft is at the sole risk of the pilot.

This Aircraft Flight Manual is not officially approved, while believed to

be complete and accurate at the time of publication, may not contain

ALL of the information needed. However, we suggest that any pilot

intending to operate I-MKLK should study its content and operate

accordingly. By virtue of its Experimental amateur-built status, all

persons entering this aircraft do so at their own risk.

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I-MKLK AIRCRAFT FLIGHT MANUAL

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0.3 TABLE OF CONTENTS

1.0G ENERAL

2.0O PERATING LIMITATIONS

3.0 ABNORMAL /EMERGENCY PROCEDURES

4.0N ORMAL PROCEDURES

5.0P ERFORMANCE

6.0M ASS AND BALANCE

7.0D ESCRIPTION OF THE AIRPLANE AND ITS SYSTEMS

8.0A IRCRAFT HANDLING AND CARE

9.0S UPPLEMENTS

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1.0 GENERAL

1.1 INTRODUCTION

1.2 CERTIFICATION BASIS

1.3 WARNINGS,CAUTIONS AND NOTES

1.4 DEFINITIONS AND ABBREVIATIONS

1.5 UNITS OF MEASUREMENT

1.5.1 CONVERSION FACTORS

1.5.2 CONVERSION TABLE [L]/[U.S. GAL]

1.5.3 CONVERSION TABLE [M]/[FT]

1.6 THREE VIEW DRAWING

1.7 SPECIFICATIONS

1.7.1 AIRFRAME

1..7.2 ENGINE /PROPELLER

1..7.3 INSTRUMENTATION /PANEL

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1.1 INTRODUCTION

THIS AIRPLANE FLIGHT MANUAL CONTAINS INFORMATION AND

LIMITATIONS FOR THE SAFE AND EFFICIENT OPERATION OF THIS

EXPERIMENTAL AIRPLANE.

1.2 CERTIFICATION BASIS

!EXPERIMENTAL

DAY VFR NOT IN VISUAL CONTACT WITH GROUND

NOT IN ICING CONDITION

NORMAL AND UTILITY CATEGORIES,ADDITIONAL AEROBATIC

MANEUVERS ON AFM

DOCUMENTS AVAILABLE:

THE FOLLOWING IS A CHECK LIST OF DATA,INFORMATION AND

LICENSES THAT ARE PART OF THE AIRCRAFT FILE AND REQUIRED BY

REGULATIONS.THEY SHOULD BE CARRIED ON BOARD AT ALL TIMES.

1. PERMIT TO FLY

2. AIRCRAFT STATION LICENSE

3. AIRCRAFT FLIGHT MANUAL

4. QUICK REFERENCE HANDBOOK

5. CHECK LIST

6. LIABILITY INSURANCE CERTIFICATE FOR AIRCRAFT

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1.3 WARNINGS,CAUTIONS AND NOTES

THE FOLLOWING DEFINITIONS APPLY TO WARNINGS,CAUTIONS AND

NOTES USED IN THIS AFM.

WARNING MEANS THAT THE NON-OBSERVATION OF THE CORRESPONDING

PROCEDURE LEADSTO AN IMMEDIATE OR IMPORTANT DEGRADATION

OF THE FLIGHT SAFETY

CAUTION MEANS THAT THE NON-OBSERVATION OF THE CORRESPONDING

PROCEDURE LEADSTO A MINOR OR TO A MORE OR LESS LONG TERM

DEGRADATION OF THE FLIGHT SAFETY.

NOTEDRAWS THE ATTENTION TO ANY SPECIAL ITEM NOT DIRECTLY

RELATED TO SAFETY BUT WHICH IS IMPORTANT OR UNUSUAL.

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1.4 DEFINITIONS AND ABBREVIATIONS

AIRSPEEDS

KIAS INDICATED AIRSPEED IN KNOTS;AIRSPEED AS DISPLAYED ON

THE INSTRUMENT.VALUES PUBLISHED IN THIS MANUAL

ASSUME ZERO INSTRUMENT ERROR.

KCAS CALIBRATED AIRSPEED IN KNOTS;INDICATED AIR SPEED

CORRECTED FOR INSTRUMENT AND POSITION ERROR

KTAS TRUE AIRSPEED IN KNOTS;AIRSPEED IN REFERENCE TO

UNDISTURBED SURROUNDING AIR,CALIBRATED AIR SPEED

CORRECTED FOR TEMPERATURE AND ALTITUDE.

GS GROUNDSPEED;SPEED IN REFERENCE TO GROUND

VAMANEUVERING SPEED;FULL OR ABRUPT CONTROL SURFACE

MOVEMENT ABOVE THIS SPEED NOT ALLOWED.

VFE MAX.FLAPS EXTENDED SPEED.DO NOT EXCEED FOR A

GIVEN FLAP SETTING.

VNO MAX.STRUCTURAL CRUISING SPEED.DO NOT EXCEED IN

CASE OF TURBULENCE.

VNE NEVER EXCEED SPEED IN SMOOTH AIR.NEVER OPERATE IN

EXCESS OF THIS SPEED.ATTENTION,KTAS FOR THE RV-7A!

VS0 STALLING SPEED WITH THE AIRPLANE IN LANDING

CONFIGURATION.

VS1 STALLING SPEED WITH THE AIRPLANE IN CLEAN

CONFIGURATION.

VXBEST ANGLE-OF-CLIMB SPEED;GREATEST GAIN OF

ALTITUDE OVER SHORTEST HORIZONTAL DISTANCE.

VYBEST RATE-OF-CLIMB SPEED;GREATEST GAIN OF ALTITUDE

OVER SHORTEST AMOUNT OF TIME

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METEOROLOGICAL TERMS

ISA INTERNATIONAL STANDARD ATMOSPHERE,IN WHICH:

-THE AIR IS DRY PERFECT GAS

-THE TEMPERATURE AT SEA LEVEL IS 15°C

-THE TEMPERATURE GRADIENT FROM SEA LEVEL TO THE

ALTITUDE AT WHICH THE OUTSIDE AIR TEMPERATURE IS

-56.5°C IS -0.00198°C PER FOOT AND ZERO ABOVE THAT

ALTITUDE.

MSL MEAN SEA LEVEL.

OAT OUTSIDE AIR TEMPERATURE;FREE AIR STATIC TEMPERATURE,

OB TAINED E ITHER FROM O NBOARD TEMPERATURE

INDICATORS OR GROUND METEOROLOGICAL SOURCES.

QNHTH EO R ETICAL AT M O S P HE RIC PRE SSURE AT M S L,

CALCULATED FROM THE ELEVATION OF THE MEASURING

POINT ABOVE MSL AND THE ACTUAL ATMOSPHERIC

PRESSURE AT THE MEASURING POINT.

PRESSURE ALTITUDE

ALTITUDE ABOVE MSL INDICATED BY A BAROMETRIC

ALTIMETER SET TO STANDARD PRESSURE (1013.25 HPA),

CORRECTED FOR INSTRUMENTERRORS.

DENSITY ALTITUDE

PRESSURE ALTITUDE CORRECTED FOR TEMPERATURE

STATION PRESSURE

ACTUAL ATMOSPHERIC PRESSURE AT FIELD ELEVATION.

WIND WIND VELOCITIES USED AS VARIABLES IN THIS MANUAL ARE

TO BE REGARDED AS HEAD OR TAILWIND COMPONENTS OF

THE REPORTED WINDS.

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