Inspection Report

tlghtmu and damage.. ........................12. Inspect aileron hinge pins and blocks for e x m a m e r and c o r n i o n (Red- Dins and - 8 --- O O C 0 O O C 0 O O E 0 0 0 0 o o c 0 0 O O C 0 0 D O C 0 o o c 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 D O 0 D O 0 0 3 0 0 0 - . . 11 bladu urequired.) ...............1.. .........13. I n w e n 1l.o mtachmnnta and b n e ~ . for E c c c C c C C c c C a 0 0 0 0 0 0 ~~~~ ~ t b h u w u and &mega. ........................ 14. lnmpmcl f l g Lullcnrk, mmrol rod. pins and Mock8 for e x a n m e r md wrmaion (Replax pi^ and blocks as n g u i d . 1 ................... 16. Lubriate per lubrication clun ................. 18. R I * I W I irupoction p h e s and falr(ngs ......... 11 F. LANDING GEAR QROUP ............................. II 1. Remom fair~ngs.. 2. Inspect fabric and finish tor cracks and .................................. deterioration 3. Inapect gear. enbane and shock strut bolts and nuts for safety ............................ 4. Hoist airplane, inspect gear, ubane and shock erut bolts and bushinm fw excess wear and II ..................................... corrosion (replace bolti and/or bushlngs as reguired) 5. lnsnen shock cords for broken threads and ~~ ~ wiikness. and if eppliuble. s o c k str& for wwknaas (replace cords and/or shak nruts as necessary) ................................. 6. Impem pear wheel alignment (0' Toe in/outl ... 7. Impen firas f w cuts, uneven or excessive wear and slippage. ............................8. Remove whwls. clean, h e c k and replck burinps.. .................................... 9. Inspect wheals for crack%Corrosion and broken b o b .................................. 10. Check main w h w l tire premun 1800 r 4-24 .......................... PSI, 8 0 0 x 6-28PSI.l 11. Impem brake lining end drumE or disks for excessive w a r .............................12. ~namctbrake 11nes for chmim and ..curw ..... 13. l m b t bnke cylindan and &king valve= for operation and leaks (check fluid kwl as ..................................... requirodl 14. INP.CI tail wheel acuehmerns for tightness and n f w .................................... 15. Inspect tail wheal fork for looseness on ....................................... bracket 16. l w t tail A w l t i n for cuts and u n m w excwwivo w..r ............................... 17. Ramow toil wheel, dean, check end repack b r i n g s . . .................................... 18. Inrpect tail wheel for cracks. mrmbion and .................................. broken bdtr 19. Irtlp.sttail w h d tire pressure, if appliuble (30 PSI1 ...................................... 20. Lubricate per lubrication chan ............................................. 21. Rdnnall fairings.. 11 0; FLOAT QROUP ................ I .................... 1. Inspm float attachment fittings 2. Inspm llmw Iff &Inage.. ..................... 3. Inspm p u l k n and cabla Circle Type of hpcctioa (See Note 1. PIpt 3) 100 soo roo0 A ~ W I H. AQRICULTURAL OROUP Chwk oil low1 - dustergear box ................................ Inspect univeml drive joints.. Inspect brakes and controls.. ..................Inspect grease cups, sprayer fan ...............C l a n hopper tank =roan .....................Inspect top hopper tank w a l .................................. Inspect bottom hopper tank 1011 R~movometal belly plate a d c h r n fusolag.. .............. 1nrp.aduster fan mount ac~umbly;. I m c t sprayer pump m o m asumbly .........Check op.mtion of dump valw.. ............... Check agitator tweration.. .....................Inrp.ct for hoppor tank Ieaki ................................. Inspect spray boom attachmanm ........................... C h n spray nozzks .................. lwpect all plumbing for lab I. OPERATIONAL INSPECTION 1. Check f m t tank rslector .................................................. 2. Check fuel quantity ............ 3. Check oil pressure and temperature ...................... 4. Check generator output.. ........................ 5. Check carburetor heat. ......................... 6. Check parking brake.. ........................ 7. Check vacuum gauge.. 8. Check gyros for noise and roughness.. ......... 9. Check cabin heater operation .................. 10. Check magneto switch operation ............... Pcrfonn nll inspections or optrations at each of the impaction intervalsas m d i w t d by a circle (0). DESCRIPTION 8 11. Check magneto RPM variation ................. 12. Check throttle and mixture operation ........... 13. Check propeller smoothness ................... .......... 14. Check electronic equipment operation ................... 15. Check engine idle (550 rprn) s 8 L J. GENERAL E f 1. Aircraft conforms to F A A Spatcifiations ........2. All FAA Aimvorthirrcru Oiroctiws c o m p i i i with .........................................3. All Manufacturers SeNias Letten and ....................... Bulletins romplid with 4. Check for proper flight Manual ................6, Aircraft papers in proper order.. ............... NOt.8: 1. Refer to the last card of the Piper Pans Price Lisi Aerofiche. for a check list of current revision dates to Piper InspectionReports and Manuals. 2. All inopectionsoroperations are requiredat each of the inspectionintewals ss marked by a 101. Both the annual and 100 hour ins~ectionsare com~leteins-ions of the airdane, identical in mope, while both the 500.and 1000 hour h p e c t i o k are extensions of the annual or 100 hour inmection, which rwuire a moredetailedexamination of the Jrdane, and overhaut or r e p l 8 ~ e ~ n t of some maGr components. Inspectionsmust be accomdfished bv w r w n s authorized by the FAA. 3. ~ i p i rService Bulletins ah of special importance and must be complied with promptly. 4. Piper Service Letters are ~roductim~rovernentsandservice hints wrtainina tosewicinothe ahlane and should be given careful attention. - - 5. Replace or overhaul as required a at engine overhaul. (For engine werhwl. nfer to the latest revision of Lmming Service Instructions No. 1009.) 6. Tearon Lycoming Service Bulletin No. 480 recommends 25-hour interval oil change and screen cleaning for all engines employing a pressure screen system; 60-hour interval oil change and filter replacement for all engines using full-flow filtration: not more than four months maximum between changes for both systems. 7. When using alternate fuels. refer to Lycoming Service Letter No. L185A for additional information and ssrvice procedures. 8. Check cable tension. Elevator cable tension 62 Ibs. + 2 l b s Aileran tabla tonsion 40 Ibs + 2 Ibs. Set flaps at 50" + 2 O . Adjust left flap and set right flap to it. To sat up the rudder cables place the rudder pedals and rudder in their neutral position and plaw the cable end on the rudder horn using one of the holes in the cable end that aligns with the hole in the ruddsr horn. 9. Refer to latest revisionsofPiper Service Bullatin No. 364 and !hrvicli LeuarNo. 944and me Special Instruction on Lubrication Chart. 10. The recommended flight time beween recondiiioningfor Sansenich fixed-pitch metal pro- pellers is 1000 hours, provided the propeller has not received prior damage requiring im- mediate attention. Reconditioninnaccomolishes the remwal of fatiaued surfaOs metal and accumulatsdsmatl nicks and cutbtoo numerous to repair individualb. Contact a Senrenich factory approved repair station. 11. Replace flexible oil lines at Engine T.B.O. per latest Lycomina Semce Bulletin No. 240. 12. Refer to Piper Service Bulletin 1670. 1 13. Check all items under WING GROUP tor evidence of corrosion. I 14. Whan InspecSng this Item, pay spselal attention for evldenca of wear and corrosion. Inspect all sMes ot attachmentsand flttlngs including inside of clevis botts and back side of flttlngs. Disassembly of compomnts may ba rsqulrsd to facllltats Inspection. I IC m i i No. I Total Time on Atmiam (3) REVISED: AUGUST 22,1999 SPECUC INSTRUCTIONS LUMICATE wa SELECTOR VUM PN n 4 1 a . o ~ .IF F U E ~ SELSCTW V 4 L X W A S SOOWOURS ORMORETOTALTIHEIN SEWICE.WIIYIN1HE N E n I~HOURSOFOPEIAl10NANO EVEIV WO H W R S THEIIEAFlER. USE DOW CORNIN0 MOLVCOAl NO. FS.31111 O1 FS.34S2. P W f l P L m NO. II. FUEL S€lEClOn VALVE A SEE S=CUL INSlRUCT0YS LEOEND 3. '?RIM CAOLES - U I # R WO C ~ T A ~ Sl(LM l H E RIM C-LEI THE COCKPIT m THE REAR o~ me ME- MOLIcOAl IC MIUTED.ilo TOCIEVEm SUPPAGE) 4. c o m a crsrcr - w r c WAN AT nwun r n E n A L s WT *IMGlCIY UL6.nm. SAE 20 BELOW WF AIR TEMP. ] CONIIWEM.L ~ N Q ~ T SAE W ABOVE IS r AM TEMP.