Aircraft Flight Manual Doc. No. 2008/100 Ed. 2 - Rev. 1 2018, March 12th .-····-··-····-······--··\ : l :. ...~ •············~ · / 1 TECNAM P2008 JC MANlJF ACTURER: C. A. TECNAM S.r.l. AIRCRAFTMOD EL: P2008JC EASA T YPE CERTTFICATENR. : A .583 (DATED2013, 27 SEPTEMBER) SERJAL NUMBER: ....J.043 ............. B UILDYEAR: ......~ oJ.5 .......... REGISTRATION MARKINGS: ..qb.-~.~.8 ..1. ... .. This Aircrafl Flight Manual is approved and applies on/y to EASA CS-VLA certifled airplanes. This Manual must be carried in the airplane at all times. This aeroplane has to be operated in compliance with procedures and limitations contained herein. Costruzioni Aeronautiche TECNAM srl Via Maiorise CAPUA (CE) - Italy Tel. +39-0823 997538 WEB: www.tecnam.com SECTION 0 INDEX 1. RECORD OF REVISIONS .......................................................................................... 3 2 . LIST OF EFFECTIVE PAGES .................................................................................... 7 3. FOREWORD .............................................................................................................. 9 4. SECTIONS LIST ...................................................................................................... 10 Ed. 2, Rev. 0 Aircraft Flight Manual INDEX 1. RECORD OF REVISIONS Any revision to the present Manual, except actual weighing data, is recordecl: a Record of Revisions is provided in this Section and the operator is advised to make sure that the record iskepl up-to-date. Thc Manual issue is identificd by Edition and Revision codcs rcported on each page, lower right siele. The revision code is numerical and consists of the number "O"; subsequentrevi­ sions are identified by the change of the code from "O"to "1" for the firstrevision to the basic publication, "2" for the second one, etc. Should be necessary tocompletely reissue a publication for contents and format changes, the Edition code will change to the next number ("2" for the second edi­ tion, "3" for the third edition etc). Additions, deletions and revisions to existing text will be identified by a revision bar (black line) in the left-hand margin of the page, adjacent to the change. When technical changes cause expansion or deletion of text which results in un­ changed text appearing on a different page, a revision bar will be placed in the right-hand margin adjacent to the page number of all affected pages providing no other revision bar appears on the page. These pages will be updated to the current regular revision date. NOTE: lt is the responsibility of the owner to maintain this handbook in a current status when it is being used for operational purposes. Ed. 2, Rev. 0 Aircraft Flight Manual RECORD OF REVISIONS .p· .. ···. ·,,.. Rev ..Rev:ised .Des~Hptiön of No · :.pl,lge Rev'isidn. '· \. '· .· ., ,,.. ,,c''·. : . "' Approved under the authority ofDOA, 0 all Editorial revision. A. Sabino C. Carnso M. Oliva ref. EASA.2IJ.335 (MOD2008/097.180126) 0-1,4,7 Cover, RoR and LOEP updated. Airspeed indicator markings amended; the indication is now 2-6 proper for both analogue and dig­ ital instruments. 3-20 Note amended. Note amended; informationh ave been added to airspeed for nor­ .Approvedunder the 4-3, 4-4 mal operations table; paragraph authority ofDOA, A. Sabino C. Caruso M. Oliva J shifted from page 3 to page 4. ref. EASA.211.335 (MOD2008/l03.180312) 4-9, Checklists amended; note to PFI revised; spced infonnation have 4-12 tbru 17 been moved to page 4-3. 6-9 W&B calculationsample. 6-11 tbrn 13 Equipment list. 7-1,5 tbru 16 Contents rearranged. 9-3 Supplements! ist updated. Ed. 2, Rev. 1 Aircraft Flight Manual RECORD OF REVISIONS INTENTTONALLY LEFT BLANK Ed 2, Rev. 0 Aircraft Flight Manual lNTENTlONALL Y LEFT BLANK Ed. 2, Rev. 0 Aircraft Flight Manual 2. LIST OF EFFECTIVE PAGES The List of Effective Pages (LOEP), applicable to manuals of every operator, Iists all the basic AFM pages: each manual could contain either basic pages or one variant of these pages when the pages of some Supplements are embodied. Pages affected by the ciment revision are indicated by an asterisk (*) following the re­ vision code. Edition 1, Rev 0 30 Jul y 2013 Edition 1, Rev 1 25 March 2015 Edition 1, Rev 2 7 April 2015 Edition 1, Rev 3 13 April 2015 Edition 1, Rev 4 14 July 2015 Edition 1, Rev 5 15 December 2015 Edition 1, Rev 6 20 December 2016 Edition 2, Rev 0 15 January 2018 Edition 2, Rev 1 12 March 2018 Section 0 2, 3, 5, 6, 8,9, 10 Rev0 1, 4, 7 Rev 1 Section 1 1 thru 14 Rev0 1 thru 5, 7thrn 30 Rev0 Section 2 6 Rev 1 Section 3 1 tluu 19, 21, 22 RevO 20 Rev 1 Section 4 1, 2, 5 thru 11, 13, 14, 18 Rev0 3, 4, 12, 15 thru 17 Rev 1 Section 5 1 thrn 16 Rev0 Section 6 1 tluu 8, 10, 14 Rev0 9, 11 thru 13 Rev 1 Section 7 2 thru 4 Rev0 1, 5 thru 16 Rev 1 Section 8 1 thrul0 Rev0 Section 9 1, 2 and4 Rev0 3 Rev 1 Ed. 2, Rev. 1 Aircraft Flight Ma nual LOEP INTENTIONALL Y LEFT BLANK Ed. 2, Rev. 0 Aircraft Flight Manual 3. FOREWORD Tecnam P2008 JC is a single-engine two-seat aircraft with a strut braced high wing and fixed landing gear. Section l provides general information and it contains definitions, symbols explana­ tions, acronyms and terminology used. Before using the airplane, you are recommended to read carefully this manual: a deep knowledge of airplane features and limitations will allow you for operating the airplane safely. For further information, please contact: COSTRUZIONI AERONAUT!CHE TECNAMs.r.l. Via MAIORISE CAPUA (CE) - ITALY a+39 (0)823 997538 ~ [email protected] Ed. 2, Rev. 0 Aircraft Flight Manual FOREWORD 4. SECTIONS LIST General (*) Section l Limitation s (**) Section 2 E merge ncy Procedures (**) Section 3 Normal Proceclures (**) Section 4 Performance(* **) Section 5 Wei ght ancl balance (*) Section 6 Airframe and Systems description (*) Section 7 Ground Handlin g and Serv ice (*) Section 8 AFM Suppl emen ts list (*) Sectio n 9 (*) non-approved Section (**) appr oved Section (** '') appro ved Section exccpt l'or pages 5-1 thru 5-4, 5-6, 5-11 thru 5-13 Ed. 2, Rev. 0 Aircraft Flight Manual SECTIONS LIST SECTION 1 • GENERAL INDEX 1. INTRODUCTION .................................................................................................. 3 2. CERTIFICATION BASIS .................................................... ............................... .... 3 3. WARNINGS - CAUTIONS - NOTES ...................................................................... 3 4. THREE-VIEW AND DIMENSIONS ......................................................................... 4 5. ENGINE ............................................................................................................... 6 6. PROPELLER ......................................................................................................... 6 7. FLIGHT CONTROL SURFACES TRAVEL .............................................................. 7 8. SPECIFIC LOADINGS ........................................................................................... 7 9, ACRONYMS AND TERMINOLOGY ....................................................................... 8 10, UNIT CONVERSION CHART .............................................................................. 13 11. LITRES / US GALLONS CONVERSION CHART .................................................. 14 Ed. 2. Rev 0 Section 1 - General INDEX lNTENTIONALLY LEFT BLANK Ed 2, Rev 0 Section 1 - General Page 1 - 3 1. INTRODUCTION The Flight Manual has been prepared to provide pilots and instructors with in­ formation for the safe and efficient operation of this very light airplane. This manual includes the material required to be furnished to the pilot of CS­ VLA. Ttalso contains supplernental data supplied by the airplane manufacturer. 2. CERTI FICATION BASIS This type of aircraft has been approved by the European Aviation Safety Agency in accordance with CS-YLA including Amendment I and the Type Certificate No.EASA.A.583 has been issued on (date) 27th September 2013. Category of Airworthiness: Normal Noise Certification Basis: EASA CS 36 Amendment 2. 3. WARNINGS - CAUT IONS - NOTES Following definitions apply to warnings, cautions and notes used in the Aircraft Flight Manual. meansthat the non-observationof the correspondingprocedure lead s to an immediate or importantdegradation of the flight safety. WARNlNG meansthat the non-observationofthe correspondingpr ocedure leads to CAUTTON a minoror to a more or less long term degradation ofthe flight safety. draws the attentionto any special iternnot directlyr elated to safety but which is importantor unusual. 1 :;m:i Ed. 2, Rev 0 Section 1 - General INTRODUCTION 4. THREE-VIEW AND DIMENSIONS Figure 1 - General views Ed. 2, Rev 0 Section 1 - General THREE-VIEW AND DIMENSIONS Page 1 - 5 Dimensions Wing Wing Span 9.00 m (29.5 ft) 2 2 Wing Area 12.16m (l30.9ft ) Aspect Ratio 6.7 Taper Ratio 0.8 Wing chord l.373 m (4.5 ft) Fuse/age Overall length 6.93 m (22.9 ft) Overall width l.20 m (3.9 ft) Overall height 2.67 m (8.8 ft) Empennage Stabilator span 2.90 m (9.5 1 ft) 2 Stabilator area 2.03 m2 (21.8 ft ) Vertical tail area 1.06 m2 (11.4 ft2) Landing Gear Wheel track 1.8 m (5.9 ft) Wheel base 1.94 m (6.4 ft) Main gear t ire 5.00-5 Nose Gear tire 5.00-5 Ed 2, Rev 0 Section 1 - General GENERAL FEATURES AFMS N °S7 for Hoffman propeller equipped airplanes with MTOW lncrement at 650 kg ~TECNÄ"'id[?~@@@ dJ@ • füO[?@[r@~ [?'~•@Du~[R-'Ä]@lli)(!!]@~ Page WHl-6 5 ENGINE Manufacturer Bombardier-Rotax GmbH Model 912 S2 Engine type 4 cylinders horizontally opposed with 1352 c.c. of overall displacement, liquid cooled