Piper PA-31-350 Aircraft Flight Manual Supplement

Piper PA-31 Navajo Chieftain · Pilot's Operating Handbook

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Overview

This document is a Flight Manual Supplement for the Piper PA-31-350 Super Chieftain and T-1020 PA-31-350 series aircraft. It provides essential information regarding modifications made to the aircraft under STC SA00202SE, which includes enhancements to performance and safety features. The supplement is designed to be used in conjunction with the basic Aircraft Flight Manual (AFM) and outlines specific operating procedures, performance data, and emergency procedures relevant to the modified aircraft. Pilots and operators are encouraged to read this supplement thoroughly to ensure safe and effective operation of the aircraft.

The document is specifically for the Piper PA-31-350 and T-1020 PA-31-350 models.
Emergency procedures include specific airspeeds for engine failure scenarios: Vmc (minimum control speed) and Vx (best angle of climb speed).
Maximum Take-Off Power (MTOP) settings are crucial for safe operation during takeoff and climb.
Performance data includes critical metrics such as climb rates and takeoff distances, which are essential for flight planning.
Engine operation guidelines emphasize the importance of mixture settings and power management.

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Document details

Type: Pilot's Operating Handbook
Year: 1995
Pages: 403
File size: 7.7 MB
Publisher: flighttest.net

Documentation completeness

4/7

Most owners only have the POH. Here's the essential set for the Piper PA-31 Navajo Chieftain.

Pilot's Operating Handbook / AFM
Checklist
Maintenance Manual
Parts Catalog (IPC)
Systems & Wiring
Service Bulletins
Type Certificate (TCDS)

More Piper PA-31 Navajo Chieftainmanuals & documents

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In this document

General Introduction

This section welcomes pilots to the Super Chieftain modification and outlines the purpose of the manual. It emphasizes the importance of understanding the modifications for optimal performance and safety.

Emergency Procedures

This section details emergency procedures specific to the PA-31-350, including engine failure during takeoff and climb. It provides critical airspeed references and power settings necessary for safe operation in emergency situations.

Normal Procedures

This section outlines standard operating procedures for the PA-31-350, including engine operation, takeoff, and landing procedures. It specifies airspeeds for safe operation and emphasizes the importance of adhering to these guidelines.

Performance Data

This section provides performance data for the PA-31-350, including climb rates, takeoff distances, and other critical performance metrics. It includes graphs and tables to assist pilots in understanding the aircraft's capabilities.

Engine Operation

This section discusses engine operation parameters, including maximum takeoff power settings and mixture control. It highlights the importance of maintaining proper engine management to ensure safety and performance.

Safety notes

Always refer to the basic Flight Manual for limitations and procedures not covered in this supplement.
Ensure that the aircraft is operated within the specified performance parameters to maintain safety.

Full document text

Cirnl Avianon SafctyAuthoriry PIPE PA-31-i50 Aircraft S T C S A O O 2 O 2 S E InsreascdWeight BoundaryLayerResearch Inc. FLIGHTMANUALSUPPLEMENT No.AfMS-PCH-5 Drted19June1995 F O R P I P E RM O D E L P 4 . 3 1 - 3 5 0 A E R O P L A N E S S/Nos31-730500'1 and On & S / N o s3 1 - 8 2 5 3 0 0 1 a n dO n Modifiedin accordancewithSTC SA00202SE G r o s sW e i g h tl n c r c a s c Tbc abovementionedSupplementis rcqured to be inscncdinto the Aircraft Flight Manual whgn the aircraftbasbeenmodificd in accordanccwitb STC SA00202S8. The ln-formationcortaiDedthcrcin supplernentsrnformationrn the basic flrght manual For LLnritarrons,Proccdurcsand Performarccdatanot coatai-ocdin this supplemcnt. consultthe basicFlight Manual. Tbrspagc is to be attachcdto the front of the FAA ApprovedSupplcmcntdated I 9 Junc 1995or later,bcforc irsertion into thc aircraftFlight Manual , . V . n ^rr,*ftfty't/.p"t/Ior ttrrKuulonry / D a t e l 0 O c t o b e r1 9 9 5 l l r p l a n € F l i g h t M a n u a l S u P P l e m e n t 1 1 r p € rC h i e f t a i n l l M o d i f i c a l i o n f o r : P|P€RChlenaln PA'31-350S€rialNumMr31-7m:tr1ed On p|P€Rt.lO20 PA-31-350S€rialNum*t 31-8253@1sd On 7'-nour[ory toq* \ \ueaftfi, [nc. -- vq+(-dlF.@ S E C T I O N1 - G E N E R A L I N T R O D U C T I O N Welcome lo the ranks ol Aoundary Layer fusetrclt.fr. Super Chieltain Owners! Your Super Chieftain Modification has been desrgned and conslrucled lo give you lhe mosl in Performance, safety, and peace of mrnd ll rs our desire lhat you w,ll Iind flyrngil either lof busrnessor pleasure, a p r e a s a n ta n u p u l l d u r c e x p e l l e n c e FM-Approved Palols Operating Handbook and Airplane Flighl Manual Supplemenl was _--/gn€d lo help you salely ulilize your Piper Chietlain and T-1020 PA-31'350 Series Super Chietlain ll Modificalion ll contains inlormation aboul your Super Chiettain li N4odilicationoperating procedures and performance. We urge you to read il lhoroughly,and lo reler lo it frequenlly. Our inlerest in your salisfaclion with our products has nol ceased wilh your purchase of our Chiellain a n d T - 1 o 2 0 P A - 3 1 - 3 5 0S e r i e s S u p e r C h i e n a i nl l M o d i l i c a l i o n P l e a s ef e e l i r e e l o c o n l a c t u s a l a n y t i m e . EoundaryLayer\9sear6, Inc. Paine Field Airporl 3 1 2 5 1 0 0 1 hS l S W . H a n g a rC 7 5 ' 5 Everelt, Washlngton 98204 u.s. 206-353-6591 FAX 206-355-3046 The Eoundary -{,ayerfosearil, ,fru. Super Chiettain ll Modilicalion consists of lour engine nacelle strakes, 88 vodex generalors affixed lo the wings and verlical lail and main landing gear modification. The purpose ol lhe 'Bouniary Layer \uearot, ,fro. Syslem is lo improve slall characleristics and tc reduce slall and VMc^speeds through conlrol of boundary layer ajrllow FAA-Approved rnlormalron. lrmilalions, pertorrnance and dala are on pages marked at the botlom ' F M - A p p r o v e d D A T E ' . Oocumenl No. AFMS-PCH-s rfrp 19. 1995 & p l o n e F l i g h t M a n u a l S u P P l e m e n t t s e o r C h i e f t a i n l l M o d i f i c a t i o n l o r : - - ' " O E R C h , u t * , ^ P A 3 l - l 5 O S € t d N u m * t 3 1 7 3 0 5 @ 1 s d O n p P € R T - 1 0 2 0 P A ' 3 1 - 3 5 0 s e r 6 l N u m & r 3 1 ' 8 2 5 3 0 0 1 M d o n ,t-a^n[ory tor* "-,--re::,:*:J#.:* L O G O F E F F E C T I V EP A G E S R e v r s i o n N u m b e r I 2 3 ^c B 9 1 0 1 1 i J 1 4 1 5 t o 1 7 6/19/95 6/19/95 6/19/95 6/19/95 6/19/95 6/19/95 6/ 19i9s 6 , ' 1 9 i- 4 5 6 i 1 9 / 9 5 6 / 1 9 / 9 5 6 / 1 9 / 9 5 6/19/95 6/19/95 6/19/95 6/19/95 iri(:umenl No. AFMS'PCH'5 , AA.AppIoved .June 19. 1995 P a g e N o . I R e v i s i o n N o l F A A A o p r o v e d . P r o v i d e da s s u p p l e m e n t a lI n l c l ' m a t l o n A t r g l a n eF l i g h t M a n u a l S u P p l e m s n t t u p e r C h i s f t a i n l l M o d i f i c a t i o n l o r : --'",pER Cttt.h"tn PA-31-350.S6ridNumbr 3l'7305001andon i'rpin r-tozo PA-31'3s0ssrid Numbor31'82im1 sd on S E C T I O N3 . E M E R G E N C YP R O C E D U R E S z'-6if,[o,y to,t* \ \ u e a i e A , l m . -"- .trg.--dlpk N O T E A L L I T E M S R E M A I N A S I N B A S I C A F M E X C E P T T H E F O L L O W I N G A t l a i r s p e e d s q u o t e d i n t h l s s e c t i o n a r e i n d i c a l e d a i r s p e e d s ( | A S ) a n d a s s u m e z e r o l n s l r u m e n l e r r o r In lhis setaon, replace all relerences to maximum power with Maximum Take-Off Power irr,1iopl *ni.n is zszs Rptt't and Minure - Full Rich. MTOP may be mainlained wilhout r e s t r i c l l o no l m a x l m u m l i m e l i m t t S I I ' ' - E N G I N EO P E R A T I O N S E C T I O N4 - N O R M A LP B O C E D U R E S N O T E A L L I T E M S B E M A I N A S I N B A S I C A F M E X C E P T T H E F O L L O W I N G : A | | a i r s P e e d s q u o l e d i n t h i s s e c t i o n a r e | n d i c a t e d a i r s p e e d s ( l A S ) a n d a S S U m e z e | o i n s t r u m e n l e r r o l . A I R S P E E D S F O R S A F E O P E R A T I O N _ ,limum Single-Engine Control Speed (Vuc^) " " ' Best Single Engine Rate ol Climb Speed (V'*) " D e s i g nM a n e u v e r i n gS p e e d ' V p . . - . . . . . ." " " " " " " E N G I N EF A I L U B E D U B I N G T A K E O F F ( 9 2 K I A S o r a b o v e ) P o w e r . . . . . . . . . . . E N G I N E F A I L U R E D U R I N G C L I M B P o w e r . . . . . . . . . . . . . . . . . S I N G L E E N G I N E G O . A R O U N D P o w e r . . . . . . . . . . . . . . . . . M i n i m u m S i n g l e - E n g i n eC o n t r o l( V M c ^ ) . . D e s i g nM a n e u v e r i n gS p e e d , V p . . . . . . . . . . Final APProach Speed, VAEF NOI>-E/CHAF ACTEF ISTIC S . . . . . . 7 2K I A S ( 8 3 M P H - r A S ) . . . . . . . . . . . . . 1 0 7 K | A S ( 1 2 3 M P H - r A S ) _ . . .. . . . . . . . . . . . . . . . . 1 5 9 K I A S ( 1 8 3 M P H - l A S ) l,4TOPon oPeraltveeng. [,lTOP on operative eng. MTOP on operalive eng. . . . . . .. . 7 2 K t A S ( 8 3 M P H - l A S ) . . . . . . . . . 1 5 9 K I A S ( 1 8 3 t \ 4 P H - l A S )

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. . . . . . . . . 8 4K t A S ( s 7 M P H , T A S ) T h e f l y o v e r n o i s e | e v e | ' e s l a b | i s h e d i n c o m p l i a n c e w i t h F A R P a r l 3 6 ' A p P e n d | X G ' i s 8 4 ' 8 d B ( A ) ' N o d e t e r m i n a l i o n h a s b e e n m a d e b y t h e F e d e r a | A v i a t i o n A d m l n | S l r a l | o n l h a l t h e n o i s e level ol this airplane is. or should be acceptable or unacceplable lor operalton al inlo' or out of any alrpon. S E C T I O N 5 . P E R F O R M A N C E N O T EA L LI T E M SR E M A I NA S I N B A S I CA F M E X C E P TT H EF O L T O W I N G : T h e p e r f o r m a n c e o f a l l P i p e r c h i e t l a i n a n d T - 1 0 2 0 P A . 3 1 - 3 5 o a i r p l a n e s e q u i p p e d w i l h t h e B o u n d a r y LaverResearchSuperChietlainll Systemwillperlormto lhe graphsin lhisseclion oocumenl No. AFMS-PCH'5 FM-Approved June I 9. 1995 7-6il[or,t roq,, I R.e^,ra/clt,hc. - - - ' r * { t t v o . r \ F t r n u A i r p l a n € F l i g h t M a n u a l S u p p l e m e n t S u D e r C h i e f t a i nl l M o d i l i c a l i o n f o r : P | P E R C h i e l t a i n P A ' 3 ! - 3 5 0 S e r a l N u m b e r 3 t 7 3 O * P I P E R T - ! 0 2 0 P A - 3 1 3 5 0 S € r L d N u m b € r 3 1 . 8 2 5 3 U sv3'Hdr,\- c:f ds l-lvj-s 3 ? 3 R 9 8 Q s a - s v S v - c l S d s l l v - L s : F B B R 6 A R I - o W ; o < m P + U - o z a o @ E 6 o c o ; ; g s , i ' * i f l i+* i l I fLI . t i t l l a o ul U a a z o F O UJ I u IU o z a I z > - ) = u a > n F L 9 ( P < a i t r l - t 0 h O ^ z 5 < o z )U F i o v I U (r a )) F a U z o z U U (, z a o( L E U o O u (9 z E l o a a oJ U o F F ) o z U o l F F I o =TI z E o o u a o z l x u F xo t I L L E t1J o o u E ) F a (, z t l o o a o) U o l F F ) f a U F o z t l r l l l iltll l l : l fill {+ l+li l r r i i l , l T+ ilt I R : m ' {11: .il+ ll]: I r l _ +it t I i _ f ] i - LL: F . a l d. 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A i r p l a n e F l i g h t M a n u a l S u p P l e m e n t S u p e r C h i e t t a i n l l M o d i f i c a t i o n t o r : P I P E R C h l e l t a l n P A - 3 1 ' 3 5 0 S e r i a l N u m & r 3 1 ' 7 m f f i 1 P l P E f l T - 1 0 2 0 P A - 3 1 - 1 5 0 S e r r a l N u m b € r 3 1 - 8 2 5 m 1 r l - t 3 N V l S t OI J O - ! ) V ] D m u m e n l N o . A F M S - F J u n e 19 o ro C9 I F (f) I (L i- a ; 6 u (l t o o o a c o ^ z : ; R d R 3 i1 J R r * ( 9 R iii E ; R d o- t! F t a u o 4 , . F Y E ; l l l r ; i t i l i l l . lf l l l l l l t ] i i l ; s r H c r H S r l v l s a o I . . t g o t : t g v f t l d d v l 1lJ- ur t j 3 4 z: E P i [ l ; z - i l IatnlsF lE ttHE* l#g;[sg f d g g I E I IEi;ifrl iH ;Es$El l 6 = P E " - l z 7 i i < 3 = T = i U I E H E lO ,",,-,f.r.'.' , t z mtmlTl|ifrJ IllIIIIilIil||1l Iiilil > t a n e F l i g h t M a n u a l S u P P l s m e n t r e r C h i e f t a i n l l M o d i f i c a l i o n l o r : PTPERChlottaln PA-31-350SeriajNumb€r31'73o5m1MdOn PTPERT-1020 PA'31-350SoriojNumb€r31'8253m1trdOn U) m J R p - o UJ 3 E I F o =F z o Ez o u E 5 a U o o ;u o o o z o z > x = # ? => = E E d = W O J < o f H*i F z d H=o P t e t'F ; P 8 5@ L N T 1 J C F G o ^ t r 3 3 ^ u t l , 9 o ! l 5 = E d 2 o 5 3 S E - . : b [ 3 : ; o * i f * i - 3 ; 3 - e p : i o $ 6 8 * ; i q '1r - SCNVl.StO dO.I.S/fl.vd3"l3CCV H E q llllrrT'lffil $ r J . u l t J I f t i F l - t Y IflJ+I < ITT.ITF]d tlT+ltf @ lSffi o ftJJ]ll F '* lu ^o( t 1 9 E | J S U t16g [Iait HEgg Hh =5 trHrff tr#f #t+il K J i i l I l1-----ot ' I i O o H < 2 ILHIH O l H + f l - l Z lll+Ftr nr l-fffiF - t+t'Ft-i F I L T I F RO tlTl+tr o 'Bowdary Larytr \ueai&, lnc. A i r p l a n eF l i g h t M a n u a l S u p p l € m e n t S u p e r C h i e f t a i nl l M o d i l i c a t i o nf o r : PIPERChleltalnPA-31-350S€rd llumtur3t 7:{) P I P E R T - 1 0 2 0 P A - 3 1 - 3 5 0 S € r l a l f J u m f { . r l j 8 : l [:.i- ]f NVt!ilo .lo ts/t_LV8:.1Ef, lv E r F E 3 F . r H F i n D o c u m e n lN o A F M S ' J u [ e ' ! ! o l() coI F C9 I TL /'6-ourrdor,t Lo,t* I Ruui&, [nt. ----- -*.6r-^6*e r r o l a n eF l i g h t M a n u a tS u P P I € m € n t J p e r C h i e f t a i n l t M o d i f i c a t i o n l o r : "tJ,"r^ "n,u*'* PA'31-3s SetrdNumFt3l-7s5oo1andon ; l ; ; ; ; - 1 ; r ; P A ' 3 1 ' 3 $ s q r d N J n & r 3 r ' 8 2 s 3 o o 1 d d o n 9 e " R = ; s F a i d i i 6 ; r r f R E X b o @ E i l * r y ) ; t ; : J ; 9 0 a $ 5 . i g P a < I )l o- ' = o , U A u r l i l ! ! | u J u ) l 0 _ C o L g a E l ; I n J l - E o r - ! = u l c ) O I - g L 9 r l - o ? r s H t - E A * U i ^ t o i i (D . z O o D I ' , R Ez 0 l 6 = = f - - v E q 6 = T A - o z & 6 r € e 3 s 3 t ' 5 x e P ; x r ' = O Y , a Z 4 o L ; - i < 3 - o 2 u . l = a - - : t ! l u u J Y o c o f r 3 q f fI U J r ^ , P Y ; a * Z - = - ( * \ i l tu tr UJ F o z * x ' F v t L o i < J I L 3 o O z O < u o ro ({) I (9 I o- E E E gP R E S S U R EA L T I T U D E . F T , ) o c u m e n l N o . A F M S - P C H - 5 :AA-APProved June 19 1995 ----_ 7'-6f,lJon1roq* \----tii:{:."r,::;.. L E A N I N G- M A X I M U MC O N T I N U O U SP O W E R- 2 4 O OR P M t ! r s l r d r d i l r i l r r 0 u r I r u e r l o w o I J U U H H m u s l D e m a t n t a t n e d l h r o u o h 1 8 . i 3 : f e e l l h e n E G T l i m i l c a n b e u s e d a s a g u i d e f o r l e a n i n g w h r i h s t t r u l Cf e s ! l l I n I e s s l h a n 3 0 G P H f u e l f l o w A i r p l a n s F l i g h t M a n u a l S u p p l e m e n t S u p e r C h i e f t a i n l l M o d i f i c a t l o n f o r : PIPERChlettaln PA-31-350SeriajNumb€r31_73OSCO1 ed On PIPERT-tO20 PA-31-350SefldNuhb€r31,8253@tmd On I M I T S D O N O TE X C E E D Ari M P F F G T C H T S L 8 , 0 0 0 10 , 0 0 0 1 2 , 0 0 0 14 , 0 0 0 16 , 0 0 0 18 , 0 0 0 r 8 . 7 0 0 2 0 o c c 2 2 . 4 4 0 2 4 0 0 0 38 3 8 3 8 . 4 3 8 . 8 3 9 . 2 3 9 . 6 4 0 . 0 40 . 0 3 7 . 7 3 4 . 3 3 1 . 0 3 0 30 30 3 0 30 3 0 30 30 500 500 500 500 5 0 0 5 0 0 500 5 0 0 5 0 0 s 0 0 500 4 7 5 4 7 5 475 4 7 5 4 7 5 4 7 5 4 7 5 4 7 5 4 7 5 475 D m u m e n l N o . A F M S - P C H - 5 FAA-Approved June 19. 1995 A i r p l a n s F l i g h t M a n u a l S u P P l e m e n t S u p e r C h i e f t a i n l l M o d i f i c a t i o n f o r : P I P E R C h l e l t a l n P A - 3 1 - 3 5 0 S € f r d N u m F r 3 1 ' 7 3 0 U 1 M d O n P I P E R T - 1 0 2 0 P A - 3 1 - 3 5 0 S € l d N u m * r 3 1 - 8 2 5 n O O 1 s d O n y"tdJ- 8911t-t3 ro 3tvu D o c u m e n lN o . A F M S - P C H - 5 FAA -Approved Juncl-9-l_9_95 ,tfn*r[orr] tou* \--.-.-xz:i.*:_!#.:* @ co J iI o u 3 o ro coI (f) I o- :J L U F K a < o u 3 = a F o @ o u < l - : ! r - = ; F * S . s ' ; P d N E d U u.l o n J < oJ ( ! : 5 = t 5 3 r ( ) u l o ' z J H f r Hf , # r r r O I t = f i 5 H # F =qHq, : i n ) = " i l d o - A < ^ d E 7 > . o c O < | } . . F r y N = l < U 6 E U z z m 9 i l hu r > lrl F K T J t r X u l Y b f 2 lrl I l t i+ l l f rn E =() tu = (, z u l ' u J ' J o z o I t r i l t r t{r i l t : [ + +F fl_ fT r I +f A T 1+ f i :l l: l f ,tt , o o o I @ o o F r @ a I I a a o z l o o- o u uJ o. a 6 - O F I O u 3 7'6fror,tro,/r, \--=-(ff*J#.:* A i r p l a n e F l i g h t M a n u a l S u p p l e m e n t S u o e r C h i e f t a i n l l M o d i f i c a t i o n t o r : P I P E R C h i e f t a i n P A - 3 1 - 3 5 0 S e n a l N u m b € r 3 l - 7 3 O 5 O O 1 m d O n P I P E R T - r 0 2 0 P A - 3 1 - 3 5 0 S e r E l N u m b € r 3 1 - 8 2 5 3 m 1 m d O n Document No. AFMS-PCH'5 J u n € i1 9 1 9 9 5 F L U o l tr F <'zsooo t! t f a o r1l 20000 I PA-31-350 O P E R A T I V E E N G I N E :2 5 7 5R P M -M I X T U R E F U L LR I C H COWLFLAPOPEN INOPERATIVE ENGINE:PROPELLER FEATHERED - COWLFLAPCLOSED 15000 O U T S I O EA I R T E M P .- " C S I N G L EE N G I N ES E R V I C EC E I L G E A R A N D F L A P SR E T R A C T E D I r F f | | l - l t l I I 1 l - l + f r f i 1 1 t 1 i l 1 t l t I S E R V I C E C E I T I N GI S T H E P R E S S U R EA L T I T U O E AIRPLANE HAS CAPABILITY OF CLIMBING 50 FT/MIN W I T H O N E P R O P E L L E RF E A T H E R E D . Esmple: OAT: 1'15'C Welght: 6000 lbs. SeMcB ceillng: 14,200 n A i r p l a n e F l i g h t M a n u a l S u p p l e m e n t S u D 6 r C h i € f t a i n l l M o d i f i c a t i o n f o r : PTPERChietbln PA-31-350Serd Numbr 3r,7rc5m1ed on PTPERT-102O PA-31-35oSeld Numhr 3t-8253m1andOn a"6fror,t rou*'.---__*X,I:_tk* l 6 f - i l o f-3 tr . L o t ' T i " = o f 8 \ > t z J l - a 7a l @ F L-o u l o i F e e t ^ u Tr( 2t < l F a l 6 f. L; L" L 5 @ O F U o lo (o I (f) I IL _! E E P E , o * , i 9 < ; b @ H d I F o ) l - I 5 . ; c i - X - - - 3 = 6 ' 3 G I i o o o . ! 5 5 " ; . . F E ! ;O = ? o = : ' , , t = I ' v r ' r F F R c o + o r ; : . ^ i P - E ' i ' - 6 i E E b € 9 3 € n E o f o t ! . = E o " , 9 o I o . ! J E 9 l : : 6 ? i i o o c F i ' , i r i i - o o : 6 5 9 < 9 k € E 9 6 J L o t r o . F r i i - D o c u m e n tN o . A F M S - p C H - 5 J u n e ' 1 9 .1 9 9 5 7'-rrrur,forrr Loq, \---(ff*J::.:^- A i r p l a n e F l i g h t M a n u a l S u p p l e m e n t S u p e r C h i e t t a i nl l M o d i f i c a t i o nf o r : PTPERChleltaln PA-31-350 Send Numhr 31 73O5OO1edOn p l p E R T - 1 0 2 0 p A - 3 1 . 3 5 0 S e r a t N u m b e r 3 t _ B 2 A 3 O O 1 o d O n w d r - t h l l t c J o f l v u o to c.)I (r)I (L I U F ''- : o i t r I i , ; R ! ! ! N * P 5 3 q ! + 5 ! ; 9 ; 3 e i , f r 5 8 9 8 D m u m e n l N o A F M S ' P C H ' 5 F A A ' A p p r o v e d& ! q 1 9 . 1 9 9 5 A i r p l a n €F l i g h t M a n u a lS u P P l s m o n t S u p e r C h i e f t a i n l l M o d i t i c a l i o n f o r : P I P E F I C h i l l b i n P A - 3 1 - 3 S O S e n d N u m & r 3 l ' 7 9 5 m 1 i l d O n P I P E R T . I O 2 O P A ' 3 1 ' 3 5 0 S € r d N u m & r 3 l - 8 2 5 3 0 0 1 m d O n r.l - 33NV1StO9N|ON\.] a d) J I lrJ E = ! ! - r 3 € < i i _ t s u " " . " : ! 6 e e i ' E \ i E E ; 5 F X . . : o * - L 6 F r r 3 E3 E q d i 3 3 0 F U o ro (9 I F C9 I IL Documenl No. AFMS-PCH-5 FM-Approved June 19- 1€!5 7-'l^rrrdor,/ to,l, \--__x1:,:I:_*.:^" A i r p l a n e F l i g h t M a n u a l S u p p l e m e n t S u p e r C h i e l l a i n l l M o d i f i c a t i o n f o r : P t P € R C h i e f l a i n P A , 3 1 - 3 5 0 S e r i a ' N u m b € r 3 1 . 7 3 O 5 ( D 1 m d O n P T P E R T - 1 0 2 0 P A - 3 1 - 3 5 0 S e n a t N u m b € r 3 t - g 2 5 3 O O t m d O n rl - ScNVrstQ cNtoN\r'l f, E U t @ F o z = o ro (9 I F ceI IL a E J F I (, U B | J - o r E e < F . - 6 ^ u g r . E I u y = = N F P E E f= H * . . I c @ F c d v - e + ; : ' ! n $ 6 i ; ; , 5 F D @ u m e n t N o . A F M S - P C H - 5 F A A ' A p p r o v e d J u n e 1 9 . 1 9 9 5 l . : i t i l l l l r u i H l i l l i l t i t \ l l l N j I sticiix iTifiseo iiiiojiur., N, I lL Li_lI911lqv3l]1dll,or1\!110rtR . ' l E l a l F ] < l u J l J 1 ; i U I 3 1 o - J 1 ^ l o 1 < + = l t s t O I o + < t x ++ € l u l l u J t a J ' O T < 1 E 1 e + < ] - o o- J L 3 2 J UJ u UJ o ro E uJ o IU o z F. @ o CI z. o z o IIJ tr F tr o - E ;t iit f LI Fr IF IT FF FF FF FF FF + +E t

All Piper PA-31 Navajo Chieftain pilot's operating handbook