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Tecnam P2008 JC Flight Manual
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Tecnam P2008 JC Flight Manual

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i'
Aircraft Flight Manual
Doc. No.
20081100
Ed.1-Rev.6
Jan
uary
,
2a1 h
2016,
TECNAM P2008 JC
AIRCRAFf MODEL:P2008 JC
COSTRUZJONt AERONAUTtCHE
MANUFACTURER:
TECNAMs.r.l.
EASA TYPE CERTIFICATE No:A
.583
(DATED
2013, 27
.....
SERIAL NUMBER:
.
.
.
.H.B.
K,
M
L
GS:
REGISTRATION MARKI
.
.
.
.
This Aircraft Flight Manual is approved by
European Aviation Safety Agency
(EASA)
and applies only EASA CS-VLA certified airplanes.
This Manual must be carried in the air plane at all times.
The airplanehas to be operated in compliance with procedures and limitations
contained herein.
Costruzioni Aeronautiche TECNAM srl
Via Maiorise
CAPUA (CE)- Italy
.tecnam.com
Tel.
+39 (0) 823 997538
WEB:
www
SEPTEMBER)

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Summary of Contents for Tecnam P2008 JC

  • Page 1 Aircraft Flight Manual Doc. No. 20081100 Ed.1-Rev.6 uary 2a1 h 2016, TECNAM P2008 JC AIRCRAFf MODEL:P2008 JC COSTRUZJONt AERONAUTtCHE MANUFACTURER: TECNAMs.r.l. EASA TYPE CERTIFICATE No:A .583 (DATED 2013, 27 SEPTEMBER) ..SERIAL NUMBER: .H.B. REGISTRATION MARKI This Aircraft Flight Manual is approved by...
  • Page 2 Page RECORD OF REVISIONS SECTION 0 Record provid e d Any revision to the present Manual, except actual weighing data, is recorded: a make iskepl of Revisions is in this Section and the operator is advised to I NDEX up-to- d ate. sure that the record The Manual issue is identified by Edition and Revision codes reported on each page, lower right side.
  • Page 3 �rEc'N'A'M Page Pag e EASA Approval or Tecnam Approval EA SA App rov al or Description of Revised Tec nam App rov al Under DOA Und er DO A page Revision Des crip tion of Privileges Revised EAS A Priv ileg es...
  • Page 4 INTENTIONALLY LEFT BLANK INTENTIONALLY LEFT BLANK J, Rev. Ed.1, Rev. 0 Aircraft Flight Manual Aircraft Flight Manual...
  • Page 5 LIST OF EFFECTIVE PAGES The List of Effective Pages (LOEP), applicable to manuals of every operator, lists 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 current revision are indicated by an asterisk (*) following the re­...
  • Page 6 FOREWORD Tccnam P2008 JC is a single-engine two-seat aircraft with a strut braced high wing and fixed landing gear. S ection provides gen eral information and it contains d efinitions, symbols explana­ tions, acronyms and terminology used. Before using the airplone, you ar e re commended to read car efully this m anual: a deep knowledge of airplan.e femure and...
  • Page 7 P age I - I SECTION 1 G E N ERAL SECTIONS LIST INDEX Section General(*) Section 2 Limitations (**) INTRODUCTION ••••••••••••••••••••••••• ••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••• CERTIFICATION BASIS Emergency Procedures (**) Section 3 ••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••• WARNINGS - CAUTIONS - NOTES ••••••••••••••••••••••••••••••••••••• ••••••••••••••••••••••••••••••••• -..6 Section 4 Normal Procedures (**) THREE-VIEW AND DIMENSIONS...
  • Page 8 Page Pag e 1 INTRODUCTION The Flight Manual has been prepared to provide pilots and instructors with in­ formation for the safe and efficient openition of this very light airplane. This manual includes the material required to be furnished to the pilot of CS­ VLA.
  • Page 11 Page Page Meteorological terminology ACRONYMS AND TERMI NOLOGY lntenmtiona l t·andard Ahno phere: is the air atmospheric standard KCAS is the indicated airspeed expressed in knots, condition at sea level, 15°C (59°F) and at l 0 1 3. 25hPa corrected taking into account the errors related to the instmment (29.92i11Hg).
  • Page 12 Page Page Weight and balance terminology Aircraft performance and flight planning terminology an imaginary Datum "Reference datum" is vertical is the velocity of the crosswind component Crosswind Velocity plane from which all horizontal distances for the which adequate control of the air­ e measured for balance purposes.
  • Page 13 Page Page 1 0. U N IT CONVERSION CHART 9·(F-32) TEMPERATURE (oF) Celsius Fahrenheit (OCJ (�·c)+32 (oF) Celsius [OCJ Fahrenheit 2.205 FORCES Kilograms [kg] 0.4536 Pounds [lbs] Pounds (lbs] Kilograms [ k g] 196.86 SPEED Meters per second [mis] 0.00508 Feet per minute [ft/min] 1.853...
  • Page 14 [� AFMS for VFR NIGHT equipped airplanes [:!{) TECNA' M [p22@@@ dJ@ &rl!f@[f� lfDD@llilU �@Ui)()j]@O Page 2N SECTION 2 LIMITATIONS US GALL ONS CONV ERSIO N CHAR T 11. LITRE S Litres US Gallons I N D E X US Gallons Litres INTRODUCTION ..................
  • Page 16 650 kg MTOW AFMS N"S7 for Hoffman propeller equipped airplanes with Increment at [F O� @ lliJ Q [K'i]@ AFMS VFR NIGHT equipped airplanes E«J 'f'ECNAM �@® @ dJ @ &!! !I' @ [[ � Page WH2-5 [FOa@Uu U �@[Ji) QJJ @ O �...
  • Page 18 AFMS N°57 for Hoffman propeller equipped airplanes with MTOW Incremen t at 650 kg AFMS for VFR NIGHT equipped airplanes t«J TECNA. M [?�®@® &ll !? ©U'� l?Ua@GuQ [ty,i]@[ii) lYJ @U �TECNAM [f U� @[}uQ [tyA](ID[ii) lYJ @U Page WH2-9 [p�@@@ &ll lf @[f� Page 2N 9.
  • Page 19 AFMS for VFR NIGHT equipped airplanes AFMS for VFR NIGHT equipped airplanes (1() (1()fE'ciiA' iW TECN AM [?�@®@ dl@ &ilU'©U'@m rPOo@[}u� !iYAl@Uil(!!] @ O !?�®®® dl@ rPOo@[}u� !iYAl@Uil(!!] ® 0 &t!U'©U'@m Page 2N - 1 1 Page 2N - 10 POWERPLANT I NSTRUMENTS MARKINGS Powerplant instrument markings and their colour code significance are shown be­...
  • Page 22 AFMS N"S 7 Hoffman propeller equipped airplanes with MTOW Increment at 650 kg Page WH2-l 7 MANOEUVRES LOAD FACTOR LI MITS APPROVED MANOEUVRES Manoeuvre load factors limits are as follows: The aircraft is certified in Normal Category in accordance with EASA CS-VLA regu­ lation applying to aeroplanes intended for non-aerobatic operation only.
  • Page 26 AFMS for VFR NIGHT equipped airplanes AFMS for VFR NIGHT equipped airplanes E«J TECNAM [p�@®@ &/l!i'@[j'@OO lfU�@lfil� �@Ui)O!l@U Page 2N - 24 � 'T'EC'NiM dl© lP�®®® &l!!i'@li' ®O O lfUn@ltu� �IIDUilO!l@U Page 2N Usable fuel markings Th rottle marking R i g ht Ta n k...
  • Page 28 AFMS for VFR NIGHT equipped airplanes dl© l? U n@Uu� �&lITil(l!)@U E«) TECN AM [?�@®® &ll !i' ©!i' @O O Page 2N Ann unciator panel Upper panel labels [" [ . . lNTENTIONALL LEFT BLANK Switches labels FUEL A VIONIC PITOT STROSE LANDING...
  • Page 29 AFMS for VFR NIGHT equipped airplan e s � T ECNAM [?�@®�@ &ll [[ @!Y@OO [fO�@� �@Uill!!l @ O P ag e SECTION 3 EMERGENCY PROCEDURES 1 0. 1 . INDEX INTRODUC TION ........
  • Page 30 AFMS for VFR NIGHT equipped airplanes AFMS for VFR NIGHT equipped airplanes t«l lfOo@ltoU �@uuma &ll U' @d TECNAM [?�@@� @ lfO�@froU �@Ui)(!!] @ a P age 3 N - 3 &ll U' ©U'� Page 3N I NTRODUCTI ON Section 3 includes checklists and detailed procedures to be used in the event of emergencies.
  • Page 31 AFMS for VFR NIGHT equipped airplanes AFMS for VFR NIGHT equipped airplanes l?Dn@IIDQ �@ITilU!l @ D &ll !J'© d l?Dn@IIDQ �@ITilU!l@D �®® W© �@@W@ &ll !J' @d P age JN P age 3N ELECTRIC POWl!R SYSTEM MALFUNCTION 2. AIRPLANE ALERTS 2.1 .
  • Page 33 Increment at AFMS for VFR NIGHT equipped airplanes lfUH@� �@[ii) Q!l @U �@@@ dJ@ &l!U'@d Page W H3 �TECNAM lfUH@IJil� �@[ii) Q!l @U &l!U'@d Pa ge 3 N 5. ENGINE FAILURE 3. AIRPLANE EVACUATION With the engine secured and propeller stopped (if practical): 5.
  • Page 37 AFMS for VFR NIGHT equipped airplanes AFMS for VFR NIGHT equipped airplanes E«Jf£cNiAi (!{)r 'EcNi Ai lfOn@!fil U lMJ®Uil Ull ® O lfOn@lfil U �@Uil Ull @ O �� ®®� © CJ &ll rr @d ��®® �@ CJ &ll rr ©d Page 3N - Page 3 N - 1 6 7.3.
  • Page 39 AFMS for VFR NIGHT equipped airplanes AFMS for VFR NIGHT equipped airplanes &tJ[[@afilm �UH @ Gu� �@[fillliJ@U � TECNAM IP�®®� © &ll [f @afilm �Ua @ Gu� P ag e 3 N P age 3 N 1 0. 9. RECOVERY FROM U N I NTENTI ONAL SPIN...
  • Page 41 AFMS for VFR NIGHT equipped airplanes AFMS for VFR NIGHT equipped airplanes l?Un@OilQ li"il&i!Iiloo &ia �®®00 JJ@ &ll lf© d l?Un@OilQ li"il&iliil oo &iU &ll ir ©� �®®�© P age 3N P age SECTION NORMAL PROCEDU RES I N DEX Intro duction ..
  • Page 42 MTOW AFMS N"S7 for Hoffman propel ler equipped airplanes with Increment at 650 kg � TE CNAM [p�@@@ dJ@ &IJ[?@� [?O�@OiJ� �@ITi)(\(]@O Page W H4-3 AFM S for VFR NIGH T equip ped airpla nes �@ITi)(\(] @O &lj[J' @� [?O� @OiJ Q Page 4N - 2 �...
  • Page 44 AFMS for VFR NIGHT equipped airplanes [?�@®® Jl@ &t!U'@d lfO�@[}uG [AVlli} [Ji) O!J@O P age 4N J.2. AIRCRAFT WALK-AROUND -®-©- -© -© - - - (------- " -· nearby. ' � - - - - - - - Figure 4.1 Left fuel filler cap CHECK desired ji1el level (use graduated dipstick ).
  • Page 45 AFMS for VFR NIGHT equipped airplanes AFM S for VFR NIGH T equip ped airpla nes � 'fEc 'N'A'M [p�@@@ �@ &/l[[@ufilfil lfO�@lfil\k WAJ @ UilOO@O Page WAJ@ UilOO @O &!\U' @!f®O O lfOfi @Gu � P age 4N - 8 E«) TEC HA M (p�...
  • Page 47 AFMS for VFR NIGHT equipped airplanes AFM S for VFR NIGH T equip ped airpl anes [?�@@ ® dJ© &!llJ'©� lP O�@UilU li'1J@!Jil(![]@a Page 4 N �@[Ji)(![]@O &!llJ' @O'®O O lP O�@OuQ Page 4N [?�@ @ @ dJ@ ENGINE STARTING 4.2.
  • Page 50 Hoffman propeller equipped airplanes with I ncrement at 650 kg AFMS for VFR NIGHT equipped airplanes lfOH @� ltYAJ@!Jil!YJ@O �®@@ dJ@ &f!U'@O'filfil P a ge WH5- 1 E«)TECNAM !?�®®® dJ@ &!kr@d lfOH @ M ltYAJ@!Jil!Yl@O Pag e SECTION 5 PERFORMANCE • INDEX INTRODUCTION •...
  • Page 51 MTOW MTOW AFMS N"S7 for Hoffman propeller equipped airplanes with Increment at 650 kg AFM S N"S 7 for Hoffman propeller equipped airplanes with Increment at 650 kg �®®� dJ@ l?Dnoolfil� IAVilml!!l � D Ei(JrE'Cil TM &nLI'©d P age w H s- 3 1 .
  • Page 52 Hoffman propeller equi pped airplanes with Increment at 650 kg MTO W for Hoffman propeller equipped airplanes with AFMS N°57 Incre ment at 650 kg �TECNAM [p�@@@ JJ@ &JlLJ'@[j'� !fD�@Ilu� �@lli) l!!l @ O TE CNAM Pa ge WH5 - 5 [plJ®@@ JJ@...
  • Page 53 MTOW A F M S N°57 for Hoffman propeller equipped airplanes with Increment at 650 kg MTOW Increment at 650 kg ropeller equippe d airplane s with N°57 for Hoffma n p A F M S l?OO@� �@Oil(l!]@ a l?�®®® dJ@ &ll !i ©�...
  • Page 54 MTOW AFM S N " S 7 for Hoffman propeller equipped airplanes with Increment at 650 kg MTOW Increment at 650 kg an prope ller equip ped airpla nes with &tl!i'©!i'&lO O lfO�@� [jyA]&JIJilW AFMS N"S7 for Hoffm �TEC NAM �@ JJ@ P age w Hs-9 &tl!i'@ !i'�...
  • Page 55 MTOW AFMS N "S7 for Hoffman propeller equipped airplanes with Increment at 650 k MTO W Incr eme n t at 650 kg prop elle r equ ippe d airp lane s with [i\'.i;J@[Ji)l!!l @ U N"S 7 for Hoff man [?�®@@ dJ@ &n!J'©�...
  • Page 56 MTOW AF MS N ° 57 for Hoffman p ro p eller equipped air p lanes with Increment at 650 WH:-13 MTOW Incre ment at 650 airpla nes with an p rop eller equip p ed !?�@@@ c!J@ £tl[j@[j'� [?O� @ [}u� INJ@Oi)Q!l@O �TECNA M AFMS N °...
  • Page 57 AFMS N°S7 for Hoffm an prop eller equip ped airpl anes with MTO W Incre ment at 650 kg d)@ c &11 0' @� lfOH@� �@Uilllil@O E«J TECNAM �®@ @ P age wHs-14 r r] &/l[J'@IJ' � f:PO�@!fil� IA'-:iJ @ Uil@ @ fi Page WHS-1 5 1 1 .
  • Page 58 S EC TION6-WEI G HT AND BALANCE I N D EX INTRODUCTION ................WEIGHING PROCEDURES ........3 ..........�: � : ��=��=�� � : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : = : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : INTENTIONALLY LEFT BLANK Determination of C.G.
  • Page 59 I NTRODUCTION This section describes the procedure for establishing the basic empty weight and the moment of the aircraft. Loading procedure information is also provided. cerning the maximum takeo ff weight and CG excursion as re­ Aircraft must be operated in accordance with the limits con­ ported in Flight Manual Section 2 .
  • Page 60 N"S7 for Hoffma n propeller equipped airplanes with MTOW Increment at 650 kg AFM S �rE'CNA'M l?�®®@ �@ r?anoolfil� &Ila'©� Page w H6-5 W EIGHING RECORD 2 .5. DETERMINATION OF C.G. LOCATION 2.4 . Mode!P2 008 JCS/N: Weighing no. Date: Propeller Flange Drop a plumb bob tangent to the wing leading edge and trace a reference mark...
  • Page 61 MTOW N"S7 for Hoffman p ropeller equi pp ed air planes with AFMS Increment at 650 kg [?�@@@ dJ@ &IJ[J'@� [?UH@GiJU �@(]j)[!!] @ U W H6 - 6 Page " 2.6. W EIGHING RECORD ( I I ) WEIGHTS AND C.G. Mode!P2008 JCSIN: Weighing...
  • Page 62 t.a • S 7 fo Inc rem ent at 650 kg equ ippe d airp lane s wit h MTO W A f NI S r Hoff m an pro pell er l?O a@ M � &1Ui) 00&1 0 P age wH 6-9 &IJ U'©...
  • Page 63 �� � f M S AFM S N " m an prop eller equi pped airpl anes with MTO W MTOW N" S7 f or Hoffman propeller equipped airplanes with Increment at 650 Incr eme nt at 650 " �TE CNAM �@@ ffi JJ@ &Jj[j'@�...
  • Page 64 NIG HT equi ppe d airp lane AFM S �fi n@ [}j)Q � @r ri) ll!J @!I Pag e @ TEC NA M � ®@ @ dJ@ &!J IJ'@ IJ'&J@ ST EM S DE SC RI PT I AI RF RA ME AN D SY SE C TIO N INSTRUMENTS Altimeter MIKROTECHNA...
  • Page 65 In this context the fuselage and vertical fin are a un ique body. P2008 JC's airframe can be divided in the following main groups, as highlighted be­ low on: The horizontal tail is an all-moving type;...
  • Page 66 AFMS for VFR NIGHT equipped airplanes AFMS for VFR NIGHT equipped airplanes � TECNAM l?�®®® dJ© &ll U' ©U'®lm lfUD@llilU liYAl@UilOll @ U lP�®®® dJ© &ll U' ©U'®lm lfUo@llilU liYAl@UilOll @ U t«J 'fEcNAM Page Page 2.4. LANDING GEAR FLIGHT CONTROLS The main landing gear (see Figure consists of two special steel leaf-springs posi­...
  • Page 67 AFMS for VFR NIGHT equipped airplanes AFMS for VFR NIGHT equipped airplanes � TEcNAM �@®@ �@ f?O�@[Ju Q [iYAJ @[ii) U!J @O �@ &l!U'@[J'@OO E«JrE'CNiM l?�®®® &ilU'©U'lfilOO lfO�@DuU [iYA]@[ii) U!J @O Page N7 - 7 Page N7 - � I NSTRUMENT PANEL...
  • Page 69 AFMS for VFR NIGHT equipped airplanes AFMS for VFR NIGHT equipped airplanes � f'ECNIM l?�®®® dJ@ lfaooo!filtl �@ llil()!] @a lP�®®® dJ@ &ll U' ©U'IIDOO lfaooo!filtl �@ llil()!] @a &ll U' ©U'IIDOO � r'Ec'NAM Page Page N7 - 3 N7 - 2 1 .
  • Page 70 AFMS for VFR NIGHT equipped airplanes AFMS for VFR NIGHT equipped airplanes TEcNAM � �@@® c!J@ � TEcNAM �- c!J© 1¥0�� � IID!JUU!llID D &ll !Y @lralOO [¥0�@� �IIDIJilU!J@D �!Y©lralOO Page N7 - Page N7 2.4. LANDING GEAR FLIGHT CONTROLS...
  • Page 72 AFMS N'S7 for Hoffman propeller equipped airplanes with MTOW Incremen t at 650 AFMS for VFR NIGHT equipped airplanes P age wli7 :i E«JrlCNA'M �@®@ JJ© � ;EcN.iM &l!IT'©� Ui'Onoo� lt:'Al@UilQ!J®O �@XID@ JJ© Ui' Onoo llil Q lt:'Al @UilQ!l@O &l!IT'©d Page N7 7.
  • Page 73 AFMS for VFR NIGHT equipped airplanes AFMS for VFR NIGHT equipped airplanes - l t � TEcNAM [p�@@® Jl@ [? O �[}u� IMJ@[jj] (l l] @ D &Jl!J'@!J' @O O l1(]rEcNAM �- Jl@ l?D� @� !Ml @Uil(ll] @ D &D!i'@!J'®OO...
  • Page 75 AFM S for VFR NfGH T equip ped airpla nes � @@® JJ@ /j,\fj11© � f? AFMS for VFR NIGHT equipped airplanes � @ llu � Page N7 - 1 4 fA'fil @ UilMtID D i;s a n@l1iuQ ltYil ® UiJ()!]oo a �®®®...
  • Page 76 NIGH T AFM S for VFR equip ped airpla nes Page 8 lP� @@ ® dJ@ &UU' @U'@m r?Utl@ Oua �® UilOO® U Pag e SECTI ON 8 GROUND HANDLING & SERVICE 1 1 . BR AK ES for each P200 8 is prov ided with an i11d.,p end., n1 hydra ulica lly actua ted brak...
  • Page 77 Page 8 Page 8 I NT RO DU CT IO N AI RCRAFT INSPECTION I NTERVALS Tl�i s serv 1crn g. sec tion c�n rain s fact ory -rec �i:n ma inte nan ce req u irem ents rnen ded pro ced ure s fo r pro per dlu�...
  • Page 78 � TE C N A M -"""" "" "' Page 8 - Page 8 AI RC RA FT CH AN GE S OR RE PA IR S Airc raft chan ge-s Mn nun l nnd Job MAINTENANCE repa irs mus t be perf orm ed in acco rdan ce wit h Air craf t Ma in- tena nce card s pro vid ed by TE CN AM...
  • Page 79 ENGINE COWLI NG CHECK GRO U N D HAN DLING 5.1 . UPPER COWLING 6.1 . TOWING Parking brake: The aircraft is most easily and safely aneuvered by hand by pushing on wing Fuel selector valve: struts near attachments or by pulling it by its propeller near the axle. A tow bar III.
  • Page 81 Pag e S - 1 0 Page 9- 1 ICE REM OV AL Anti icin g pro duct s are not allo wed. To remo ve and oper ate with ice, to w the airc SEC TION AFM SUPPLEMENTS a soft brus h or a raft in the hang ar h umid clot h .
  • Page 82 � nee ded Registration marks: k.M L loc al nat ion al rule s. A ircraft SIN: Date: SUPPLEMENTS LIST FOR P2008 JC APPLICABLE: Sup. Title Date Rev. no. VFR Night equipment configura- Edlrev2 20/0 1 /2016...
  • Page 83 INTENTIONALLY LEFT BLANK J" Ed, Rev. O Section Supplements SUPPLEMl!NTS LIST...