fy TABLE OF CONTENTS SECTION 6 WEIGHT AND BALANCE Paragraph Page No. : No. 6.1 General 6-1 63 Airplane Weighing Procedure . 6-2 6.5 Weight and Balance Data and Record . 65 6.7 General Loading Recommendations . 6-9 6.9 Weight and Balance Determination for Flight . . 6-10 6.11 Instructions for Using the Weight and Balance Plotter... 6-15 6.13 *Equipment List 6-19 (a) Propeller and Propeller Accessories . 6-20 (b) Engine and Engine Accessories 621 (c) Landing Gear and Brakes 62 (d) Electrical Equipment 6-23 (ec) Instruments. 6-26 wo Miscellaneou: 6-28 (g) Propeller and Propeller Accessories (Optional Equipment) . . 6-29 (hy Engine aud Engine Accessorics (Optional Equipment) . 6-30 () Landing Gear and Brakes (Optional Equipment)... | () Electrical Equipment (Optional Equipment)... 6-32 () Instruments (Optional Equipment) 634 () Autopilots (Optional Equipment) . 6-40 (m) Radio Equipment (Optional Equipment). 6-41 () Miscellaneous (Optional Equipment) 655 (0) | Maximum Zero Fuel Weight Increase . 6-65 ENCLOSED WITH ** Equipment List (Form 240 0017) . THIS HANDBOOK *For 1982 and preceding models only. **For 1983 and subsequent models only. REPORT: VB-1150 6-iPIPER AIRCRAFT CORPORATION SECTION 6 PA-34-220T, SENECA III WEIGHT AND BALANCE SECTION 6 WEIGHT AND BALANCE 6.1 GENERAL In order to achieve the performance and flying characteristics which are designed into the airplane, it must be flown with the weight and center of gravity (C.G.) position within the approved operating range (envelope). Although the airplane offers flexibility of loading it cannot be flown with the maximum number of adult passengers, full fuel tanks and maximum baggage. With the flexibility comes responsibility. The pilot must insure that the airplane is loaded within the loading envelope before a takeoff. Misloading carries consequences for any aircraft. An overloaded air- plane will not take off, climb or cruise as well as a properly loaded one. The heavier the airplane is loaded, the less climb performance it will have. ‘Cemer of gravity is a determining factor in Might characteristics. If the C.G. is too far forward in any airplane, it may be difficult to rotate for takeoff or landing. If the C.G. is too far aft, the airplane may rotate prematurely on takeolt or tend to pitch up during climb. Longitudinal stability will be reduced. This can lead to inadvertent stalls and even spins: and spin recovery becomes more difficult as the center of gravity moves aft of the approved limit. A properly loaded airplane, however, will perform as intended. Before the airplane is licensed, it is weighed, and a basic empty weight and C.G. location is computed (basic empty weight consists of the standard empty weight of the airplane plus the optional equipment). Using the basic empty weight and C.G. location, the pilot can easily determine the weight and C.G. position for the loaded airplane by computing the total weight and moment and then determining whether they are within the approved envelope. ISSUED: FEBRUARY 20, 1981 REPORT: VB-1150 REVISED: SEPTEMBER 13, 1982 6-1SECTION 6 PIPER AIRCRAFT CORPORATION WEIGHT AND BALANCE PA-34-220T, SENECA III The basic empty weight and C.G. location are recorded in the Weight and Balance Data Form (Figure 6-5) and the Weight and Balance Record (Figure 6-7), The current values should always be used. Whenever new equipment is added or any modification work is done, the mechanic responsible for the work is required to compute a new basic empty weight and © G_ pasition and to write these in the Aircraft Log Rook and the Weight and Balance Record. The owner should make sure that it is done, A weight and balance calculation is necessary in determining how much fuel or baggage can be boarded so as to keep the C.G. within allowable limits. Check calculations prior to adding fuel to insure against improper loading. The following pages are forms used in weighing an airplane in production and in computing basic empty weight, C.G. position, and useful load. Note that the useful load includes usable fuel, baggage. cargo and passengers. Following this is the method for computing takeoff weight and CG. 6.3 AIRPLANE WEIGHING PROCEDURES | Atthe time of licensing, Piper Aircraft Corporation provides each air- plane with the basic empty weight and center of gravity location. This data is supplied by Figure 6-5. The removal or addition of equipment or airplane modifications can affect the hasic empty weight and center of gravity. The following is a weighing procedure to determine this basic empty weight and center of gravity location: (a) Preparation (1) Be certain that all items checked in the airplane equipment list are installed in the proper location in the airplane. (2) Remove excessive dirt, grease, moisture, foreign items such as rags and tools from the airplane before weighing. (3) Defuel airplane. Then open all fuel drains until all remaining fuel is drained. Operate each engine until all undrainable fuel is used and engine stops. Then add the unusable fucl (5.0 gallons total, 2.5 gallons each wing). REPORT: VB-1150 ISSUED: FEBRUARY 20, 1981 “a PEVICEN. CEPTEMBED 12) 1007 NPIPER AIRCRAFT CORPORATION SECTION 6 PA-34-220T, SENECA III WEIGHT AND BALANCE (4) Fill with oil to full capacity. rs (5) Place pilot and copilot seats in fourth (4th) notch, aft of forward position. Put flaps in the fully retracted position and all control surfaces in the neutral position. Tow bar should be in the proper location and all entrance and baggage doors Closed (6) Weigh the airplane inside a closed building to prevent errors in scale readings due to wind. (b) Leveling (1) With airplane on scales, block main gear oleo pistons in the fully extended position (2) Level airplane (refer to Figure 6-3) deflating nose wheel tire. to center bubble on level. (c) Weighing - Airplane Basic Empty Weight es (1) With the airpalne level and the brakes released, record the weight shown on each scale. Deduct the tare, if any, from each reading, Scale Net Scale Position and Symbol Reading | Tare | Weight Nose Wheel (N) Right Main Wheel (R) Left Main Wheel (L) Basic Empty Weight, as Weighed | (T) WEIGHING FORM an Figure 6-1 ISSUED: FEBRUARY 20, 1981 REPORT: VB-1150 6-3SECTION 6 PIPER AIRCRAFT CORPORATION WEIGHT AND BALANCE PA-34-220T, SENECA III (d) Basic Empty Weight Center of Gravity (1) The following geometry applies to the PA-34-220T airplane when it is level. Refer to Leveling paragraph 6.3 (b). Level Points (Fuselage Left Side Below Window) *The datum is 78.4 inches ahead of the wing leading edge at the inboard edge of the inboard fuel tank. LEVELING DIAGRAM Figure 6-3 (2) The basic empty weight center of gravity (as weighed including optional equipment, full oil and unusable fuel) can be deter- mined by the following formula: C.G. Arm = N (A) +(R + L)(B) inches T Where: T=N+R+L UED: FEBRUARY 20, 1981PIPER AIRCRAFT CORPORATION SECTION 6 PA-34-220T, SENECA IIE WEIGHT AND BALANCE 6.5 WEIGHT AND BALANCE DATA AND RECORD The Basic Empty Weight, Center of Gravity Location and Usefu! Load listed in Figure 6-5 are for the airplane as delivered from the factory. These figures apply only to the specific airplane serial number and re number shown. The basic empty weight uf the airplane as delivered from the factory has been entered in the Weight and Balance Record (Figure 6-7). This form is provided to present the current status of the airplane basic empty weight and a complete history of previous modifications. Any change to the perima- nently installed equipment or modification which affects weight or moment must be entered in the Weight and Balance Record. ISSUED: FEBRUARY 20, 1981 REPORT: VB-1150 6-5SECTION 6 PIPER AIRCRAFT CORPORATION WEIGHT AND BALANCE ‘ PA-34-220T, SENECA III Ubertrag aus Flight-Manual Report Nr. VB-1110 MODEL PA-34-220T SENECA III 34-8133066 Airplane Serial Number Registration Number _N_8372B___OE-FeE Date 324-38 AIRPLANE BASIC EMPTY WEIGHT C.G. Arm » Weight x (Inches Aft = Moment item (Lbs.) of Dayém) (in Lbs.) Actual “ Standard Empty Weight* — QOWUKKEK 2855 , S 86.1 245776 Optional Equipment \ Ge. 5 100.0 35962 Basic Empty Weight haan 0 87.6 281738 ‘The standard empty weigh “iydes full oil capacity and 5.0 gallons of she ypely unusable fuel. 7 x AIRPLANE USEFUL T@AD - NORMAL CATEGORY OPERATION (Gross Weight) - (Basic Empty Weight) = Useful Load (4407 Ibs.) - (3215.0 1bs.) = 1192. 01bs. Z THIS BASIC EMPTY WEIGHT. C.G. AND USEFUL. LOAD ARE FOR THE AIRPLANE AS DELIVERED FROM THE FACTORY. REFER TO THE APPROPRIATE AIRCRAFT RECORD WHEN ALTERATIONS HAVE BEEN MADE. WEIGHT AND BALANCE DATA FORM Figure 6-5 REPORT: VB-1150 ISSUED: FEBRUARY 20, 1981 6-6SECTION 6 WEIGHS AND BALANCE 2 >< LE PIPER AIRCRAFT CORPORATION PA-34-220T, SENECA IIT 4 a A (peas . | en esbeuz erenee] | 7 | ~ | A lnpeeaomtoran woahion sye| A P29 2 AEAS| OV ES2E + 25H vIn Dae ‘Tre! 7K ISL ID ot O32 GSE) 4|4 [4 SNe 82) h'gerz] zore'z fee? [he | + BEvle re] haalk_e] oy [Sve @'o0l | syst + . 2 a c e o s t AMBUU NOD VWvellio “BELLS [O° SLE ot! cat) 001 cu) | cap |e > = WUaLOW. TAN quawow | wy am [2 & uoneoy.pow 40 5 aa a 3 | aq qsiom Mdwy, 4 3 2 2) ajonsy jo uondinsaq z oseg Sumuny sauey) BIA jo 2 ° Jaquinyy ade 4q4-9o PAN voHeNs! PUGQOEELS-VE AIQUINN [BU9S) LOZZ-PE-Wd 6-7 REPORT: VB-1150 WEIGHT AND BALANCE RECORD Figure 6-7 ISSUED: FEBRUARY 20, 1981SECTION 6 PIPER AIRCRAFT CORPORATION WEIGHT AND BALANCE PA-34-220T, SENECA III velo 3) aS /> Elen 5) 22 zie 3 | ad we & é = Bo €o 5 | &|? 3) 2 3/2/82 z £/) & < 3 & a a) me a a > a a 6-19 5 § @ 5PA-34-220T, SENECA II PIPER AIRCRAFT CORPORATION WEIGHT AND BALANCE SECTION 6 oir rse 6s (3uqy Yay) I I-spsue “BH yadig ‘r0us9,05 [see oul V'se fe — Guray 127) O1-srace Bq sadig ‘10uJ9,05 TezueH 0%5d OL - siseg “42D SIOUIZ.0D oIINeIPAH OME «o@ sf dui £07 oss (BuIA “UsTY) as-6StBOLa /ANWTO-AATI-OHA [POW 11911 itt £0 oss (Bul 27) U8-6SP89A /ANWOT-AATI-OHE [POW 119217H sisjjsdog om, og (uy-q7) wmreq yy (spunog)—-psuy wai] “ON weauoyw (uy) wy TBA EW wary souossacoy saljadorg pue ssy}adoig (2) ISSUED: FEBRUARY 20, 1981 REVISED: JUNE 11, 1982 REPORT:VB-1150 6-20SECTION 6 WEIGHT AND BALANCE PIPER AIRCRAFT CORPORATION PA-34-220T, SENECA IIT Ly6S1 LP6ST Cera) 1UaWOW WR BRE wine uv (uj) way op (sounod! 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OSL > ST90E-C “ON “C109 [Rays pu; P9ZIOSL AYL-OP “ON “Assy Stonposg 1raoqy pu ‘Jquassy jaayay ason ZIOSL-sisra uaz soqn] aeiniay 2 S9-0¢ “ON “Assy aqeag O6-0F ON “ASSV 1>94AN SINPOld RIBY Purara| “e So1QUOSSY [aaYAA UIE OM] wo] sayeg pur arog furpury rs ON wai] (2) ISSUED: FEBRUARY 20, 1981 REPORT: VB-1150SECTION 6 WEIGHT AND BALANCE PIPER AIRCRAFT CORPORATION PA-34-220T, SENECA III Ltt Lg wy cP (ul-a7) quawow € ume uv int Ole? 0687 oso! o°sol ) uy v0 (spunod) Tsuy qi JL RW C Si-6RL9¢ “Buq 19d) (pI-AG-SH-VZIPV UaPUA\) Kiddng 1amod St-68L9€ “8mq sadig ([fo€] sAi-a-oLpW UaeUAL) (EL) eqong uly Q0£) OSL - siseq “U9 St-68L9€ “3Mqq Jadid (p\-Wd-SL9W Y24UN) (eT) 14317 APN BUEN Q0£9 OSL - siseg 42D S7-68L9E “BM Addi (pi-Dd-SL9V UAPUA) (yBiy) 1dr] ABN BULA wait ywoudinby [eo.n091z (p) is es ON wary REPORT: VB-1150 ISSUED: FEBRUARY 20, 1981 6:PIPER AIRCRAFT CORPORATION SECTION 6 PA-34-220T, SENECA IIT WEIGHT AND BALANCE cs 9LI- te (uy-q7) waWOW ris “is To Ole wed uv (uy) way or v8e (spunog) ‘psuy BIA, Jew \ ‘uoisod papuarxs ul 1898 9sou YIM I-pe00ssd did (az00%-D04 N/d AI ODI AA, 211101591) (2) Keay 28e1]0A1040 £-F0889_"3Mq wdig )roreinfoy aajo, SEU Igy “HV SE ATI Aaenieg 0-0P796 “3mq Rdig (60S% N/d “4°D) Z) siya] Surpuey wat] (too) 1uawdinby yeo1991y “oN wai] (p) ISSUED: FEBRUARY 20, 1981 REPORT: VB-1150 6-24SECTION 6 WEIGHT AND BALANCE PIPER AIRCRAFT CORPORATION PA-34-220T, SENECA III ce ty te Cur-aT) 1uaWO 09 708 ftp TH wineg YW Cup) way ve (spunogi “ysuy Ws SOUR. “1yBiom Kup auiBua o1seq Ut Papnjduyy L-°9-8168L “BMC 42did (pizse 84 eS) io SuMeR 11S L- '9-8L68L “3M sacid (Z-981 U3 aes) soaiag Sue [INS (4211018914 699179 N/d WOL) (Z) sorewa[y 7-0:166 “3uq stadia I N/d tonuo> Way) {Z) Aejay s917g oBge9 “Bq sodig Aejay Kuaneg, mai] (v109) quswdinbg [eouy[y (p) SL el 69 L9 “ON wait REPORT: VB-1150 ISSUED: FEBRUARY 20, 1981 6-25PA-34-220T, SENECA III PIPER AIRCRAFT CORPORATION WEIGHT AND BALANCE SECTION 6 r 6L 799 Lyd OSL- siseg “U9 T-1PELE “Bm tadig (jeng) eBnvQ Moly long £6 6L 799 wl SPD OSL - siseg "aD PSsLe “Bmq sadig (1enq) ainssarg plowweW ov 16 £9 oe 60 24) OSL- siseg “way L-C9PLO “Bq Jodig - ssedwoy Vv 68 or #99 90 — 92) OSL - siseg “1129, S8S-6h)0SSd sadig - s01es1puy pardsiy gg tl 659 vi —_— 4019 OSL- siseg “14a g- 40 ¥3000SSd Jedig -sa1wNIY og Sg (ul-q1) umeq yy (spunog) “ysuy wail “ON UsWOW (uy) wiy 1 sian, Jew wail squaunasuy (2) ISSUED: FEBRUARY 20, 1981 REPORT: VB-1150 6-96SECTION 6 WEIGHT AND BALANCE PIPER AIRCRAFT CORPORATION PA-34-220T, SENECA IIT 61 821 89 6 um (ara) qusWoW, 67 elo 89g 659 ca) wned Vv Cup) wy 0 61 zl vi v0 (spunog) UBIO O-leLte “Bmq Jedid Fo, Moy susug 7-86896 “Bmq Jodie (2) Kiquiassy sa3sn[) €-90LL8 19 Z-90LL8 “BMC Jodid (2) Assy zvex2UaH YOR Z-6956E 19 €-8796E “Sma sodtd (eng) serowoyor | Z-1EL8 “Sm Jodta (jenq) a8ney, aunyeioduiay sep isnvyxy “psuy ural OUR, squauInasuy “oN wip @) 6-27 REPORT: VB-1150 ISSUED: FEBRUARY 20, 1981 REVISED: SEPTEMBER 17, 1984PIPER AIRCRAFT CORPORATION SECTION 6 WEIGHT AND BALANCE PA-34-220T, SENECA III L61 9s (ura) wawoW 1071 Oro 698, wmeq uy ¢ ) way 1 91 81 (spunog) 118M ‘psuy Jew ve-P-6L00SSd 194 (z) (uo4g) paxtg - sauseH Japinoys JI OSL ~ SIG “U2 SSd Jadid 1g 19g YY Je OS. Coot i dy 189g Jad, = siseg “U9 JD _OSL - s18%E “U2D Tr-OL00SSd dtd (2) sujag yeag qw04 may] snoauRy|2o1y) ) oll aut sil tl “ON wat} ISSUED: FEBRUARY 20, 1981 REPORT: VB-1150 6-28SECTION 6 WEIGHT AND BALANCE PIPER AIRCRAFT CORPORATION PA-34-220T, SENECA III lel os Ul 79E stk (uraT) qUaWO A ~/ eto ous ae £0e wneg yy (uy) wry juauidinbe jeucndo pue puepueis usamieq souasayip luswOU FUE UBIO ole —_ S186¢ ‘BMq sodig surasés Suyayreasuyy saqjadorg ezt os (cporreisiy aze sdoud pareoy Way AA) T-61LL8 ‘BMq sedtd 9 ss (-patteasut 1cu aue sdoud pareay UDYA\) Z6ILL8 ‘BMC 1adid 8s 7-0689¢ ‘Smq sodig & twaseydosyouss wz uses TOLid - siseq “HD (Bur 14314) 9-WANZET [60SOZEAVE [920 AaINeDOW (BULAN ET) S-WANTS [80SDZEAWE 1920 A21NBDOW sifjadorg OML =D STI (spunog) —“Lsuy uni ON wa CW wary (ueudinbg jeuondg) soliosssooy wifedosg pur sojjedo.g (8) REPORT: VR-1150 ISSUED; FEBRUARY 20, 1981 REVISED: JUNE 11, 1982 6-29SECTION 6 WEIGHT AND BALANCE é Weight (Pounds) E 3 a Z B 8 Bos 2-2 8 2 2s Ex ge a we 2s as ied 2 Ae ae as 3 gs go mw B 22 E; £8 oo of Es 32 REPORT: VB-1150 PIPER AIRCRAFT CORPORATION PA-34-220T, SENECA HII ISSUED: FEBRUARY 20, 1981SECTION 6 WEIGHT AND BALANCE PIPER AIRCRAFT CORPORATION PA-34-220T, SENECA IIT juzwdinbs jeuondo pur prepuris uscmi9g ouasajsip 1uowoU pur uss. (uuswdinbs prepueis se owes) —_= 299 OSL - siseq “URD aqny yy oily Suney Aid 8 U1 adil Pagare 9 € 00°9 YoLEPOCH °q gle 8601 Cl 79D OSL - siseq “9D (2) agny yum any Buney Aid 8 IT adh pacary 9 ¥ 00°9 ¥97D OSL - sIsea 12D, (2) “Assy aed E80E (2 “Ass [994M DOZI-OP sionforg weary puejancD “e TON dnosp fing Aka DET (ul-qq) ume yy — (spunod) “psu way ON usw W (up) wy 1ysiomM, 1 Ye wary (vowdinbg yeuondg) soywig pue 1295 Suipuey — (1) € € c 631 REPORT: VB-1150 ISSUED: FEBRUARY 20, 1981 REVISED: JUNE 11, 1982PIPER AIRCRAFT CORPORATION SECTION 6 PA-34-220T, SENECA III WEIGHT AND BALANCE £s es ts es 8s SL (Cur-q7) qUSMOW, O'sol o'sol o'sol O'sol OSIT f6rl wmeg yy (up) way s0 s0 so s0 29 3s (spunog) ‘psuy wae RW YI-¥-W-G-Ad-009 Ua!UM GT) 14817 eqons pay Pur ABN [EL /SUIA v1-¥-W-C-9d-009V YePUM (ay8ry) 1417] aqons pay pue ABN TEL /2U PI-W-C-ad-009 YaPUM (yD) WIT aqong axy AL Paw ARN TEL /ZULM vI-W-C-Dd-009V wPUM (try) W817 aqons a1yA DUE ABN Te] /BuIM I-bS10-01# SeMNID (2) “4 T-¥S10-014 sawn (7) “e siygr] Suipeoy wai] (Quamdinbg jeuordo) qwuamdmbg peony (0 IST 6r1 raat Srl al “ON wal] REPORT: VB-1150 6-32 ISSUED: FEBRUARY 20, 1981 REVISED: OCTOBER 16, 1981SECTION 6 WEIGHT AND BALANCE PIPER AIRCRAFT CORPORATION PA-34-220T, SENECA III vl tsi €8 oly Cura) wawowW O1Ez wmed yv Cup) ay juauidinha: 70 ov 97 ot Sle (spunog) 1USI2 A, “psuy FORA resuaatun, MOA ZI “Z9POOeE 39148TT Z-SSEZ9 “Bu sadid [qed amo [euUsa1xy 1389 “8a Jedd apeidaooy Mog AzBIIKNY polls ‘Bmq tadid ‘s1y3'T GOODY ALL SULA (siuay] aqons wy pl-AC-VGH-V-ELPY WIPUAN Kidding samod wy (1uo2) (uaudinby [zuondg) quswidinbg yeo12199)q, PU PIEDURIS UDdWIag ADUALT|FIP 1UNWOW DUR TYAN « 6S1 ust Sst Sl est onl wait 6-33 REPORT: VR-1150 ISSUED: FEBRUARY 20, 1981 REVISED: OCTOBER 16, 1981PIPER AIRCRAFT CORPORATION SECTION 6 PA-34-220T, SENECA III WEIGH] AND BALANCE trl 6f7 Ost Srl (ur-q7) qwaw9 W] v9 f'rs rn (spunog) IN %D OSL - sistq 142 8 AC b- “E-"Z-70006 “BM aodig ‘ork apy (v8ZINI Nid 221v-2pa) TSEs9e “BMC sadig sdung wnnoe, omy -q TF 0-66E6L ‘Bmq wadid sdung wnnsea om] “e uoney|esuy waisks wnnse,, wary (uauidinbg jeuondo) siuaumnsu| ‘ op fLI “oN wary ISSUED: FEBRUARY 20, 1981 REPORT: VB-1150SECTION 6 WEIGHT AND BALANCE (uowdinta prepueis se aues) ae 42D OSL - SIseE “149 L8S-6900SSd J9did soyeorpuy paads-nuy, D 6LT 868 99 Le —_— PZSD 26D “95D OSL - sISeI "UA (paaeis-V09E-CSN N/d 149) (ISH) s0v01puy UoReNItS [eLUOZIIO H BL ele 6e9 or — B7SD 6D °99D OSL - sISea “HED (VO9E-ASN N/d [uo (ISH) so1e01pu] UoHENIES [eIvOZIIOH rm 891 Ly 9% an 25D OSL - sis “1499 L- 40 p- *€- '7-£0066 “BHC dacig ‘orkD feuonoaN1 sul (uray) meg yy (spuncd) sul w91} ON luawow = (UI) WY wsiay URW wart (qoo) (1z9urdinbg jeuondo) squawniisut — (4) € € C PIPER AIRCRAFT CORPORATION e 5 ey + st =< = 6-35 REPORT: VB-1150 ISSUED: FEBRUARY 20, 1981 REVISED: JUNE 11, 1982PA-34-220T, SENECA IIE PIPER AIRCRAFT CORPORATION WEIGHT AND BALANCE SECTION 6 y y Y ‘uauidinbs jeuondo pur s1epueis usow19g souD29)y1p 1UWOW pur 1YIOM. 989 OSL- s1se@ 1499, ve v9 s aa £-01066 “3Mq Jadig “q 99 6°59 ol — S- 10 % °Z-01066 “Bmq sadiy -e paads jwonsa, 281 aS sus o1 — 88D OSL - siseq 425 49pooug apniryV OOS-YV OseN ssl 9s w9s o1 — 889 OSL - siseg “uaD, (€d-SZ1§ Nid Stuswinaisuy feuuy) saznifig apninty €g1 6s 6°59 60x = —— 889 A019 OSL - siseq “uaa L- 10 9-80005Sd s2dig aaawiyy Surpeoug Dg (u-q1) weg yy (spunog) nsuy wai] “ON luawO0 WW, (uy) way 1YysIaQy yee wai] (1uos) Quaudinbg jeuondg) swuaumnasuy — (3) ISSUED: FEBRUARY 20, 1981 REPORT: VB-1150 6-36PIPER AIRCRAFT CORPORATION PA-34-220T, SENECA III SECTION 6 WEIGHT AND BALANCE ol &@ ka 698 6L6 91 Cul-aT) qUsWOW Sue soe Flo 707 est ro unig yy (up uy v0 cP vs 9% (spunod) 1USI9 MA “isu Je, 9162 “Bm sadig s8neo ainieiodway ny pHsele “mq sadig OO] [eu YD o1pey OI-VU Fury Z-€69LE “Buq sadig Jo sWUTY APPEY OLA QED OSL > sISeg “UID €- 10 Z-0€00SSd Jadid soyeatpuy dyg pue win, ual (Qquos) (uaudinby jeuondo) sqaunssuy 661 L6l S6l £61 681 “oN way] oD REPORT: VB-1150 ISSUED: FEBRUARY 20, 1981 REVISED: JUNE I1, 1982 6-37PA 34 220T, SENECA III PIPER AIRCRAFT CORPORATION WEICHT AND BALANCE SECTION 6 Or x99 90 4ZD OSL - Siseg “12D L8S-6r00SSd 42dig soreoipu] paods-np 9 soz x9. Ly 9 — 2S OSL - siseg “1199 £10 b “E-7-£0056 "BN dadig "0445 [RuoNoaIIg £07 wr ry wz — 2D OSL - SIS8@ “1aD 8 10 b- “E= "7-70086 “Ba Jadid ‘0145 opmmy 10z yeiuauinnsuy poourapy siojido> wnieq yy (spunog) way ‘ON (up) uy aya 1 UP wai ‘uos) (uawdinby jrsondo) stusunaisu| ISSUED: FEBRUARY 20, 1981 REPORT: VB-1150 aweSECTION 6 WEIGHT AND BALANCE PIPER AIRCRAFT CORPORATION PA-34-220T, SENECA III RY 9 ve 99 (up-q1) WIWOW € plo Lv 699 umed yWv Cup) way (spunoe) 1ysI9A\ [sul EW pod gD OSL - siseq 49D {> 40 Z-0¢00SSd 2did soveorpuy dig pue wn 401 OSL > SIS=4_ 42D S- 40 p-8000SSd Jodig ‘4919UNIV 48.9 OSL. - sised 49D £-01966 “3uq sadg “4 S- 40 F °7-01066 “Bad Jadid “® paads [Roiu9,, wait (juo9) (Quewdinbg jeuoidg) squawinsisuy u 1% Mz 607 L0z “oN warp @ REPORT: VB-1150 ISSUED: FEBRUARY 20, 1981 6-39PIPER AIRCRAFT CORPORATION SECTION 6 PA-34-220T, SENECA IIE WEIGHT AND BALANCE €1z Oe Tz O81 9ese L16 e9Id e9ld 1-a7) waWOW, ve seo cr 19¢1 vol O'sPl Ost wrieg yy (uy) way qeane Sinead a tl voy vor (spunog) = “asuy MBM EN A-MSILEEVS OLS = 182g 32D S6L6E “3M sedig vS7dzs 0-AD yeuoNoang “Pp LIDS woz H Bu1s99:g °9 LLIAZS woz} Bujs20xg “q LOTUS “PUI UOZIOH "e Tp famiuag roj1deiny C-MSPBEEVS DLS - SISeE 1499) 96L6¢ Bmq sdig 17 Gamiuag roj!dony AOLPIIVS OLS - siseq 1229, sorky ,€ pue 101ecIpUT UOZIJOH 2pnINiy Bsz-Dy ‘weIshs, Jouu>D 14314 00Z-D4y Fy AOLPIIWS OLS - siseq 12D soiky ,¢ pue 401991¢] UBT] 9SZ-1N “Wasks Jorg 18Tq 00t-OAN UY wary £0 1% 617 L1z “ON waty ISSUED: FEBRUARY 20, 1981 REPORT: VB-1150 6-40 REVISED: JUNE 11, 1982SECTION 6 WEIGHT AND BALANCE PIPER AIRCRAFT CORPORATION PA-34-220T, SENECA IIT RLI pz 0zI 7 (cu-a7) qWwaWoW, 99 reo veo 899 wre UV (uy) way RT x91 (spunog) 1ysI9M “psuy JORW “a|qno pur eauaiue sapnjou! 1y319A\~e pL OSL - sIseg “HAD sopucdsuery 0907-YL X1PU9E 2999 "20h “9969 "PED OSL > SISP@ “39D tend “4 aiaurs °e Joves1pul ap 10Z MI XIFUSE 20D “ALE “9ED “PSED "PED OSL - SISeA HAD ABN/mUWOD [ENC 1107 xIpus wai] (1uaudinbg jeuondo) quawidinby 0. pey (w) LU St “oN way] REPORT: VB-1150 ISSUED: FEBRUARY 20, 1981 REVISED: JUNE 11, 1982 6-41PIPER AIRCRAFT CORPORATION SECTION 6 PA-34-220T, SENECA III WEIGHT AND BALANCE ry eel (Cuq-q7) UIE W wmeg yy (uy) way (spunog) LBD, “psuy Jue “4 pur euuaue jenp sopnyour 1ydoA\ew 1Qtd pur RuUaIUe Sapnfoul UTE STA PI 4molg xX1pudg 6t7 “LOG SL - siseg “ua UT VOLOZ M1 XIpurg LT sowurafoig Ary OP02-dN *1PUDg set 7999 OSL - SIs*g “1499 O¢07 AWA X1pucg eee 2 “Ib OSL - sista 1429 eng “q aug -e Ruuaiuy ¢207 § OL0 ACV - X!puag 1k7 ws “ON wai} Quos) (\usudinby jevondg) quauidinbg o1pey ISSUED: FEBRUARY 20, 1981 REPORT: VB-1150SECTION 6 WEIGHT AND BALANCE PIPER AIRCRAFT CORPORATION PA-34-220T. SENECA HII tor tee los RPT (ura) waWoW € zo z's9 v7 v7 wed UV (up) way ol ot (spunog) 1st9M | “psu EW 20pD OSL - sise@ "HD reng "4 aauig “e soveopul JOT/YOA ( ) OSE-GNI SUIIOD 29¢) “80P) OSL ~ 49aaaay ABN, ISE-UIA 40 OSE-UIA SUELOD aged “alt OSL sisea U2 wend “a aisug “e Joatoosues | Wwo> ISZ-AHA 10 OSZ-4HA SUILOD wait (too) (quawdindy jeucndg) quowdinby o1pey c She tz Ive ON wai} REPORT: VB-1150 ISSUED: FEBRUARY 20, 1981 6-43t 3 Zz og w e Ss a g 4 ° < a e < e 3 = a S e 5 < Pa & < a a = WEIGHT AND BALANCE SECTION 6 17 vel Ove ae $8 (u1-q7) qUaWOW, £9 oro veo 3°98 aso wmeg yy “Uy) way uy JEW "91929 pur Ruuar 99.9 OSL -siseq U2) PUT WIM 1Sp-3W SUIIOD POPS OSL - siseg ‘aD quaudinby Sunnduo > DUEISIC OOP AD SUTIOD S9fD OSL - SIs 9D PED OSL - sIseq aD adojg @PND OSE-S19 sUIIOD 296.9 "20%. OSL - siseq U9 -01891PY] SO/IOT/ AOA ) ISE-GNI suo> (woo) (uaudinbg yeu qwauidinby o1pey Sst eSt Ist. 6r7 Lv “oN waly ISSUED: FEBRUARY 20, 1981 REVISED: JUNE 11, 1982 REPORT: VB-1150 6-44SECTION 6 WEIGHT AND BALANCE ENECA HT PIPER AIRCRAFT CORPORATION PA-34-220T, SLi 60P 668 SSR Cura) quawoW sey eet voll aa wned uv (uy) way BU ete an oL (spunod) BISA ‘o|qes pue rauaiue sapnios! IAI pL OSL ~ SSPE "WD sapuodsuesl 0S6-UCL SUID 0s 'PSED OSL sIsea “9D joued 19422 Jorpny OSe-HWV SUtLIOD 21pD OSL ~ sIseq “U2D Joo1puy VOS9-CNI pue seuuaruy pur 19A10204 SCV VOS9UIA SUTOD P1pD OSL - Sse “UD 40189 1PU Os9-CINI pue euuauy pue J9n1900y AAV 0S9-UDY S| wait (Qquoz) (uaudinbg jeuondo) wawdinby o1pey (w) , £9 197 687 REPORT: VB-1150 ISSUED: FEBRUARY 20, 1981 6-45PIPER AIRCRAFT CORPORATION SECTION 6 PA-34.220T, SENECA III WFICHT AND BALANCE 78t v6 OF Te 6S £0€ ee ole Cur-aT) qUaTO £871 umed yy (uy) wy “21qeo pur euusise seprjou! 1BIOA\e tu ——— uoowag saxIeW I7-YY Bury, ost — Teng ‘saroosuezy -q SL — ayiurg ‘saatsosuery -e (ARN /wul0g AHA) ( ) 041 Xx Bury P9€D ‘kOrO. “Q8ED “ALED OSL - siIseq “2D ‘s — Joaaoey adorg apilg inoywm “4 us — Jaaiaoay edolg 9pID YAM "e ABN /MWOD JHA $91 XX Bury B9ED ‘OPD “Q8€O “ALED OSL - siseg “2D sb Joataozy adojg aptly inoyn~y ‘2 es ey adois ePID “q o's 1dwy oIpny YUM “e J9/1909y AeN/UWOD AHA SSI X¥ Bury (spunog) “sur wary wa RW (atoo) (auewidinbg yeuendo) quowdinby o1pey tf) u (a) 197 997 $9 $97 “ON wary ISSUED: FEBRUARY 20, 1981 REPORT:VB-1150 6-46 TINE 11 1009 PEvicen.SECTION 6 WEIGHT AND BALANCE PIPER AIRCRAFT CORPORATION PA-34-220T, SENECA II 607 0g 98 oss ly 9fb (uy-a1) qwawWoW € e9 ee 919 el 6°59 el 6s vol ves 60 €%7 OL umeq yy (spunog) (uy) way WSI9\ “ysuy, ery FING V29-NX 3Uy Slt 060 ‘9969 ‘OPED OSL - SISPE 2D JOSIPU] AEN-Y 90Z-TH BUPA ele 29£9 ‘BOD OSL - sIsed “42D, sOItoIpU DOT AOA 702 1 FUT ue OPO ‘29€D ‘VED OSL - SSPE 49D O1s6E “Bmq Jadig ‘3192 pue euunuy 09-WH pue J01201pUT ZLS-1GM “ANC €9-NW SAPHIOUT AUN BLY 18-SN¥ BUY, te JOM OGA bl OZ-W BU "B AEN-Y O8-SNY SUI 69% wary “ON wary (quo) (quurdinbg yeucrndo) quawdinby oipey (wi) C REPORT: VB-1150 ISSUED: FEBRUARY 20, 1981 REVISED: JUNE 11, 1982 6-47PIPER AIRCRAFT CORPORATION SECTION 6 PA-34-220T, SENECA IIL WEIGHT AND BALANCE £64 9Lt £0r cz 1 961 (uq-q7) qwewOW, f'P0l oreo oso oro £'s9 reo wued yy (uy) way OL 8 fs (spunod) TyBIOM Y “ago pue euuciue sopnfour UsIOA\e euuaiuy asusg pur dooq ECH-VY MIM 98-9 Sur 99£9 ‘PED “FOP OSL - sISeE 139-0 4DAIQOOY ABN €S-NW SUry 2969 “OPED “FOPD OSL - ISG 112 rend “4 aiauig -e 32A1209% SD UMM 49A1999¥ ABN ES-NY SUry, Ieueg ry Tonw0D OIpry 7-VINX 9bLD OSL - sIse@ “429 Jopuodsuray ( ) ou Ly fury “psuy wary Jew (uo) (1uewdinbg jeuondo) quoudinby oipey (uw) 87 £87 ISSUED: FEBRUARY 20, 1981 REPORT: VB-1150 6-48 REVISED: JUNE 11, 1982SECTION 6 WEIGHT AND BALANCE PIPER AIRCRAFT CORPORATION PA-34-220T, SENECA III est Ov 91 OP ty dort So Lp 9st Cur-aT) qUaMOW ss9 Lz oz 919 Tes SPr6l Vedi “eg Cr wnied YW Cup wy (spunod) qs u “a[qeo pue euvaiue sepnpour ysioMe 20D ‘a8tD “QL€D “9€9 OSL - SPE “WO soveo1puy STI/YOA vOe-TX SULy 'P s9at299¥Y adols apHo SL NX Bury 9 9119AU0D DOT YOA ZL NX Bury “a TeAtoosuUBLE "e AHA ( ) Set X¥ 3uy 21yD OSL ~ SSPE “2D @ VIN Moye ‘dury oipny ’P tend (2) arduis (1) euUsUy app WH "2 tend “q aiauis “e “pur pue JOABOTY ACV LEU BU wei (quo9) (ueudinby [euonco) quoudinbg o1pey, L87 S87 ‘oN wei] (a) REPORT: VB-1150 ISSUED; FEBRUARY 20, 1981 6-49PIPER AIRCRAFT CORPORATION SECTION 6 PA-34-220T, SENECA III WEICHT AND BALANCE ses 390 06 $01 91 tor (ul-a71) q2swOW sso OT O19 ume yy Cup) wiy v3 tb a1 c su (spunog) “psu Wa Few rN QED “QUES OSL - sIS*A "UID feng -q asug -e JOABOSUeL] 61-7¥ Bury Q8ED “LED OSL - sistg "1399 jeng ‘q agurg “2 de1soog Jamod S71 a u/M JOALSCSURLL F96I-AM BUY POP ‘as¢D “QED "96D OSL - sistg "1599 40181pUT DOTYOA £02-14 Bury “9 qeueruod, DOT/YOA ZL NX Fury “q (puz) searsosaezy “e JHA ( ) SLI X¥ Bury way (vos) (wewdinbg jevondo) quswdinbg oipey (wu) EE eee £67 167 687 “oN wary ISSUED: FEBRUARY 20, 1981 REPORT: VB-1150 65aSECTION 6 WEIGHT AND BALANCE PIPER AIRCRAFT CORPORATION PA-34-220T, SENECA III 96 80¢ bbe tLe 4 £67 82 $9 (ul-aT) qwsWOW 0'09T S76 Lt Ist Err 607 699 699 wmeg yv (ap) way 1t4 zr oT (spunod) 1WsI9%, aswag 4dV aiau's 0 wu0d HHA 2H A wwod AHA |# *® 91qeD pure etuauy ones nUy 81-OP00SSd HWOD AHA tH > 81-y00SSd MUWIOD AHA | “9 UddZI-AV JO L€ AWA BUIAIDDY ABN 'B 2qeD pue euuIuy 2ObD “99ED ‘PED OSL - SISA “19D, 1018{puy SO/DOT/AOA 602-14 BUH BObD '99€9 ‘9PED OSL - Siseq UID. JoveOIPU] DOT/AOA 80c-1H BUA “psuy wary J yew (use) (uawidinbg peuondo) yuawidinby cipey (a) C 10€ 667 L627 $67 “ON wait 6-51 REPORT: VB-1150 ISSUED: FEBRUARY 20, 1981 REVISED: JUNE 11, 1982PIPER AIRCRAFT CORPORATION SECTION 6 PA-34-220T, SENECA III WEIGHT AND BALANCE +8 cy wy 17 tel St6 67 (ura) qWAWOW 6°69 669 8'0L 8'0L v'99T Sse CLIT 0°661 wnreq YVv (Cu) way Y Y “VOA1909Y WORE 1942 01 DUM xPOD BUUDTUE sopnIout IUBIOAL» ee 32 £0 asd Tle (spunog) qWsIOM “psuy 1 ew 9-9€06L “Bmq sadig - jen “P ~ ajBurg “9 00. [9POW oo1eN P-9€06L “3uq sadig - eng “q £-9€06: ‘mq jadig - aj8urs “e POY sorsnooy xao], suoydoniy 16D OSL - siseq “Uap POH ssx00y pue sous “a xe) pue euusiuy “e (01-114 aPOW o22eN) Jonpusver] 1012007] doussucwy 9-LELOE “Bmq_ sedig 701 1D 1ueWOD tuusiUy Uooveg Joye wei] (1uos) (1uawdinbg jeuonég) aouidinby o1pey (w) Ot £0€ te “oN wary ee ISSUED: FEBRUARY 20, 1981 REPORT: VB-1150 6-52 REVISED: JUNE 11, 1982SECTION 6 WEIGHT AND BALANCE PIPER AIRCRAFT CORPORATION PA-34-220T, SENECA IIT Te et col Is 92 ) yuau0 vz osy Slo S'sk Ssk wimeg yv Cup) way s6l 0 0 £0 (spunog) —“118uy waa, JERI 49, > OSL > siseg “UE T-916LE “Buq Jedd depey xipug G1-9S889 “mq Jadid “laspesH 02866 “8MC sadig “s9yvad 6-40 uae lend “q ajuig “e (00-62929 N'd) THEW SxS XORL E-126LE “Baq Jodid laspeay{ - suoqdorsiy, woog (1uo9) (iuaudinby jeu wary nd) qwoudinbg orpey ( ) ie 60E LOE “on wai] REPORT: VR-1150 ISSUED; FEBRUARY 20, 1981