EFTA01702231.pdf

,e Cor S;,:- .: I; ,c1 k, • n2 7 n ‘" • r . ,,c. • ' • .c. . :, -:ST , . NOINTG -4 c eil 't"ig :..Ehs. n. cir • ;--e. ,. 30 ' 0 Ai:, •~ v 1.9 .. • C' • rtIO -- ~s Yew e 4 % .Y • ... .11A niriZ NI Vt W $ . , • 14' 6 • -9 / I N2 • tit.\ tiv‘ --*-. -kJ • 0 • OAT .• TOTAL FOR THE DAY: PA. 9 —S.- / If /4 AIRCRAFT & ENGINE AIRCRAFT ENG. HOURS ENG. CYCLES TORQUE LANDINGS I CERTIFY THAT THE DAILY FLIGHT HRS / CYCLES i RIN HOURS ENG. 1 ENG. 2 ENG. 1 ENG. 2 EVENTS INSPECTION WAS COMPLETED ACCORDING TO THE TOTALS BROUGHT FORWARD: --.)// . c"• 04 .s . MAINTENANCE MANUAL. c.)/ • il RS ),S-1/3 TOTALS FOR TODAY: .0 / 9 /1 • /9 7 4/ ACCUMULATIVE TOTAL: • " 6 V CA( Q_ • Pre ) .109 NEXT SCHEDULED NAME & CERTIFICATE NO. INSPECTION DUE: TYPE INSPECTION (60,100, ETC.) 5© ' IR 6(2)-e -C:0 Cr 0 C 1 • .C: 1O SO • Cr) DATE: ANNUAL INSPECTION DUE DATE: 9 ei PILOTS AND MAINTENANCE RECORD PILOTS ENTER DISCREPANCIES - MECHANICS ENTER ALL MAINTENANCE PERFORMED FLIGHT DISCREPANCIES REMARKS CORRECTIVE ACTION SoMV3firif cstoolhotArr were- bac - oxeiz AMEN Viii ,5-01-1/ 34r#StasiMAre Iva ZAAI 8#7; 4427-42,4 AT Aar 516, 4,1 Alen' bug" 4-1 gar 624,V ae. 406- ob , ;20eliegar,r7A< CORRECTIVE ACTION .360//defrnit/ TA PC uffie bye - CORRECTIVE ACTION JeOhlOolril IA Pe tat 347ta en -'/o7 -MM Ar 407 6-76,V 06;heob / Alen DA" 41Aar 876,1DL Au& 06 07.61 ‘4 RRECT I VE f ACTION CAI 62tht Dist P.9a6 AloeicrioAl 4:- Ala (596,1,/ 0.5"Mi :1 2.6- tht kt_coubirmoper.zAlivarioAl .bile" - / 101 Av. d7A/Mi CORRECTIVE ACTION c/a &vie 4C.lizl'etrA90 4"-V4/ 41 ACC 1C4 s 47"/4aT 3- 7474 ecV/13/O HELICOPTER LOG Bell Helicopter lulajj 7861 55349 REV 195 rol.. on AI nr • tpa woo. ..... EFTA01702231  .., . .. •• • t•••• i:. ' ,.: fr ii.g.... • .i f t • V , a48•“:4 / 17:: 1,4•" 4t• : •'44.841 4 t 31 1 . . . 1- iZr • 4,4;1 ; . .•411 • ?-kl; ":1•7 I 24,9Z,n rt : ; • Kgg ft M ; . BR 464. .: ''-• ' ,••ev.• fitsm ,lea -'7,, . - -•? it PILOT DATE TYPE OF ACFT. HRS. ENG. STARTS TORQUE LANDINGS POWER •14 ENG. 1 ENG. 2 . FLIGHT ENG. 1 ENG. 2 EVENTS ASSURANCE ,=.1:)C: 1 6vE -D... ►. ,517,1 2- O • E I 1 3 3 TORQUE \ t c).N \\ .Vr-CA•k •-4.-4 i n • / 3 TOT/ITT .%, 644 L :.-Uteredtk o • Li / 3 ? NI 2-A g tk\ \/ I C'4\<\ - 4 4 i., o •I / ....3 -....E N2 JaN N..*,- * La i, 6 1 ais Lc) 6 • a a OAT TOTAL FOR THE DAY: / •7 r Li If PA. AIRCRAFT a ENGINE AIRCRAFT ENG. HOURS ENG. CYCLES TORQUE LANDINGS I CERTIFY THAT THE DAILY FLIGHT HRS / CYCLES / RIN HOURS ENG. 1 ENG. 2 ENG. 1 ENG. 2 EVENTS INSPECTION WAS COMPLETED ACCORDING TO THE TOTALS BROUGHT FORWARD: MAINTENANCE MANUAL. 5 ?0 . LI 5% . g i Ilio 65 -9- 155 I TOTALS FOR TODAY: /•7 /n 1 ' S" If 1. ACCUMULATIVE TOTAL: P8? .S78'R ' //75- /C74 dif )\-_------ 15t NEXT SCHEDULED A060(0 ": NAME 8 CERTIFICATE NO. INSPECTION DUE: oh 4 (9244 (9t540 TYPE INSPECTION - 47. 69- - a c -- (50, 100. ETC.) 25 SO /per DATE: ANNUAL INSPECTION DUE DATE: SSP (4, PILOTS AND MAINTENANCE RECORD PILOTS ENTER DISCREPANCIES - MECHANICS ENTER ALL MAINTENANCE PERFORMED FLIGHT DISCREPANCIES REMARKS 1 CORRECTIVE ACTION 2 CORRECTIVE ACTION 3 CORRECTIVE ACTION 4 CORRECTIVE ACTION 6 CORRECTIVE ACTION HELICOPTER LOG Bell Helleoptertatial • 1..•••• t • h., *4 )861 55349 REV 195 llllllllll 4.04. MI. POI MI • PCOI EFTA01702232 L, a l , i 4 , , N N.X. la R7 e O. i A Ssi --.-11.1::4. .‘It; .;:. th iW k6 '‘; t. ' Ill'} .. , EX ' ....a:e........ ,:. •k TI. eirSaz 'Tce • '..-v ‘ • • :, e •,,_ .-..7 , 4A..: 1., .t • "- .• • •" . 8 E.24- y 67 ) A GI:i.).11-6nir 4 4354 . 8 . PILOT DATE TYPE OF ACFT. HRS. ENG. STARTS TORQUE LANDINGS POWER ENG. 1 ENG. 2 FLIGHT ENG. 1 ENG. 2 EVENTS ASSURANCE Ro CbR I 6 Li F.Q., ICA I Lc) 0 • ii r -3 ? TORQUE V trcv 1pEt110-€- 6)di t/.-. 0 • I .3 TOT/ITT J^ \A 1\hE CA. cA-C (31° I 6 • 2 A ...5- ....r NI <‘1o‘ earaiftr 1 • _&__ C 7 7 N2 V A'N ‘A%uPd-in 6log L si a • 2 / 3 .....? OAT TOTAL FOR THE DAY: 4 . 2 /6 di kJ ,. PA. AIRCRAFT 8 ENGINE AIRCRAFT . ENG. HOURS ENG. CYCLES TORQUE LANDINGS I CERTIFY THAT THE DAILY FLIGHT HRS / CYCLES/ RIN HOURS ENG. 1 ENG. 2 ENG. 1 ENG. 2 EVENTS INSPECTION WAS COMPLETED ACCORDING TO THE TOTALS BROUGHT FORWARD: p8 . 3 S)& 3 • IR C /5-4 Isdic MAINTENANCE MANUAL. TOTALS FOR TODAY: 41 .3 4 ._.? lo oil ACCUMULATIVE TOTAL: P I > .‘ F .‘ . MOE - 6 23 I NL IS N NEXT SCHEDULED US 10 NAME & CER FICATE NO. INSPECTION DUE: CC " rani 6c ---‘ TYPE INSPECTION C 't) ( (60,100, ETC.) ANNUAL INSPECTION r-,T 5 so Jo s° DATE: DUE DATE: SR2p 0( PILOTS AND MAINTENANCE RECORD PILOTS ENTER DISCREPANCIES - MECHANICS ENTER ALL MAINTENANCE PERFORMED FLIGHT REMARKS DISCREPANCIES 1 CORRECTIVE ACTION 2 CORRECTIVE ACTION 3 CORRECTIVE ACTION 4 CORRECTIVE ACTION 5 CORRECTIVE ACTION HELICOPTER LOG Bell Helicopter '*.tali 7861 55349 REV 195 Pet ,,,,, ••••• • EFTA01702233  ' • • 5: om .5 t 4 • . . 1 i . C.343.rr.V '. L .fi: ' I f:4 ow ' 4- 4;..Thr, •'-••- " •••• e• '" \E' */ VI I a:1 -, - • llti1& • kk 4: • a ' . . PILOT DATE TYPE OF ACFT. HRS. • ENG. STARTS TORQUE LANDINGS POWER ENG. i EN-G, 2. FLIGHT ENG. 1 ENG. 2 EVENTS ASSURANCE \ eriN \ TS.UCLA If" e LO e, • 4 / 3 3 TORQUE V ci,(\i \'\Nlit ‘, ht in c •9 / ...? 3 TOT/ITT (.. .6 Lc) a • 40 et ..? -...? N1 MilIVIC n/ Cas Ls-3 / • 0 (9 8 CP N2 . OAT TOTAL FOR THE DAY: AIRCRAFT & ENGINE I a' • a 6 i /7 /7 I PA. AIRCRAFT ENG. HOURS ENG. CYCLES TORQUE LANDINGS I CERTIFY THAT THE DAILY FLIGHT HRS! CYCLES! RIN HOURS ENG. 1 ENG. 2 EVENTS ENG. 1 ENG. 2 INSPECTION WAS COMPLETED TOTALS BROUGHT FORWARD: aa .6, sr),. 6- ACCORDING TO THE ' AS LiTIS LIS7 MAINTENANCE MANUAL. k •a g .3A TOTALS FOR TODAY: 6" 1 /7 /7 ACCUMULATIVE TOTAL: NEXT SCHEDULED O il • P ,S-0' Y • • 00 /eh j6 4 NAME & CERTIFICATE NO. INSPECTION DUE: TYPE INSPECTION 6 °C) / - I I 60/ I(/5-.( (60, 100, ETC.) a ° -S- CO / no DATE: ANNUAL INSPECTION . DUE DATE: ! i 1S -C436‘ PILOTS AND MAINTENANCE RECORD PILOTS ENTER DISCREPANCIES - MECHANICS ENTER ALL MAINTENANCE PERFORMED FLIGHT DISCREPANCIES REMARKS 1 CORRECTIVE ACTION 2 CORRECTIVE ACTION 3 CORRECTIVE ACTION 4 CORRECTIVE ACTION 5 CORRECTIVE ACTION HELICOPTER LOG Bell HelicopterWALLS 7861 55349 REV 195 • no.... EFTA01702234  eY , G iS , ,.1 :i tl ' ; a I i 1 ' '1^ — . TZ,› .-, ,. . a, 1 t:. 2 Sit M t/P 1"..C .4 1 nevatafFie" - en • 1 1 r BP-14/ ) OY. ... PILOT DATE TYPE OF ACFT. HRS. g c J 4. a .' ENG. STARTS TORQUE LANDINGS POWER ENG. I ENO. 2 FLIGHT ENG. 1 ENG. 2 EVENTS ASSURANCE \I ON \\.V4-Ckt.. W 7t> tr. L Qi • • / ...._.? 2 TORQUE PitNi \\A.Clik. N 74 :4 1,< cs • xJ, / S ...? TOT/ITT .....5, j (T.iNngWaCO\ IQ .2-4, °16 G • Y j . / _; in • ,IPkiNi\\LAGik n) 71q W‘1.LN n • 9 / _2 2 N2 per Cutkretr q_aR-0 I at+ • S SAD -lc OAT TOTAL FOR THE DAY: >0' i i PA. AIRCRAFT F. ENGINE AIRCRAFT ENG. HOURS ENG. CYCLES TORQUE LANDINGS FLIGHT HRS / CYCLES/ RIN I CERTIFY THAT THE DAILY HOURS ENG. 1 ENG. 2 ENG. 1 ENG. 2 EVENTS INSPECTION WAS COMPLETED R • Al ACCORDING TO THE kic )(o& TOTALS BROUGHT FORWARD: .ai i i so. MAINTENANCE MANUAL. TOTALS FOR TODAY: VP • ‘ S.,• 3o Se ACCUMULATIVE TOTAL tow s (zVr=Ser WO "31 • I axil !t9,440 N•VA-N1 )tI • .C,I.A. NEXT SCHEDULED NAME & CERTIFICATE NO. INSPECTION DUE: TYPE INSPECTION (50,100, ETC.) ,k)QA \ 41, a&36 ATE: i ANNUAL INSPECTION . DUE DATE: PILOTS AND MAINTENANCE RECORD ' PILOTS ENTER DISCREPANCIES - MECHANICS ENTER ALL MAINTENANCE PERFORMED FLIGHT DISCREPANCIES 'REMARKS CORRECTIVE ACTION 2 CORRECTIVE ACTION 3 CORRECTIVE ACTION 4 CORRECTIVE ACTION 5 CORRE8TIVE ACTION HELICOPTER LOG c,4 Bell Helicopterri*SitWI 7861 55349 REV 195 .M1 4.1....1•••••••••••• ..... EFTA01702235  558801 AIRCRAFT MODEL SERIAL NO. REGISTRATION NO. OWNER 1-4(11 A-if Gk 1S 1 Lint PILOT DATE TYPE OF ACFT. HRS. ENG. STARTS TORQUE LANDINGS POWER ENG. 1 ENG,'. FLIGHT ENG. 1 ENG. 2 EVENTS 12.34A _Lm ASSURANCE Pm_ (k./14/3.‘ -tSt.n. Ci•-•D`t-O6. µ.."-L-r O'3 I I 475 TORQUE 1---/AoleY //-zz-on, /47P /9 /z1 /0 0 TOT/ITT Hi g<e•‘/ H•72-0/- clini O •/ / / 4 N1 N2 OAT , TOTAL FOR THE DAY: • PA. AIRCRAFT 8, ENGINE AIRCRAFT ENG. HOURS ENG. CYCLES TORQUE LANDINGS I CERTIFY THAT THE DAILY FLIGHT HRS I CYCLES! RIN HOURS ENG. 1 . s ENG. 1 ENG. 2 EVENTS INSPECTION WAS COMPLETE Iron ACCORDING TO THE 610 .9. lotts.9 i LK D4 i TOTALS BROUGHT FORWARD: 610 .ct MAINTENANCE MANUAL. I 10 4-0 TOTALS FOR TODAY; • • • ACCUMULATIVE TOTAL: . NEXT SCHEDULED . NAME & CERTIFICATE NO. INSPECTION DUE: L,101:2--- -• 3-o-1 TYPE INSPECTION SoBr/ 3Msr, FiCe i (50,100, ETC.) i LAI.L.s DATE: ANNUAL INSPECTION DUE DATE: LI-OOO1 PILOTS AND MAINTENANCE RECORD PILOTS ENTER DISCREPANCIES - MECHANICS ENTER ALL MAINTENANCE PERFORMED FLIGHT DISCREPANCIES REMARKS 1 DATE II-1-O b ACTT 10iI.a vi4 533/S" THIS AIRCRAFT WAS INSPECTED ARO FOUND TO BE In AIRWORTHY CONDITION FOR THE CORRECTIVE MUNTENANCELALTEPATIONS PERFORMED. PERTINENT DETAILS OF THE WORK PERFORMED ARE ON FILE AT THIS AGENCY UNDER WORK ORDER(S) ACTION CO'73OIER . THE AIRCRAFT IS APPROVEDFOR RETURN TO SERVICE FOR TE T FUGHTS TO CONDUCT REQUIRED OPERATIONAL CHECKS OF THE 2 .MINI ANC 'PERFORMED PER FAR 91 407(8). INSPECTOR FOR CORRECTIVE EDWARDS S ASSOCATIES. ACTION FM REPAIR STATION FICFRO0D 3 • DATE //-72.O( ACTT 4/3./ S/N 53375 ' CORRECTIVE PERFORMED MAINTENANCE TEST FLIGHTS TO CONDUCT REQUIRED ACTION OPERATIONAL CHECKS OF MAINTENANCE/ALTERATIONS PERFORMED AND FOUND NO APPRECIABLE CHANGES TO THE FLIGHT CHARACTERISTICS AND NO SUBST IAL EFFECTS TO THE SAFE OPERATION OF THE AIRCRAFT I CORDANCE WITH FAR O1.4O7(B). CORRECTIVE ACTION FAA CERTIFIED PILOT 5 CORRECTIVE ACTION HELICOPTER LOG Ben lieticopterbi*-11LN TN: 55349 REV 195 .... EFTA01702236  P. S/N W/O C07301EA 11.22-06 " 611.2 ENG 611.2 /HOBBS 611.2 /CYCLES RUN-ON LANDINGS 44 1242 TQ EVENTS 1641 Downloaded FADEC Fault History. No tefults in systd m. Removed & reinstalled M/R blades to facilitate maint enance. Performed 300 Hour/12 Month/Annual/24 Month Airfra me Periodic Inspections, and all 6 Events of the Airframe Progressive Inspection per Bell's 407 Maintenance Manual. Performed 150 Hour/300 Hour Engine Inspections per Rolls Royce C47B Maintenance Manual. Performed annual P/N and S/N check of components with records. Drained and reserviced transmission & T/R gearb ox oils with Royco 555. Drained and reserviced engine oil with Mobil 254. Greased swashplate, pitch link trunnions, & T/R pitch change assembly with Mobil 28. Greased T/R hanger bearing & oil cooler bearings with Mobil 28. Serviced Concorde lead acid battery P/N RG407A1 S/N 40104 102. Washed engine compressor. Engine oil flow checked 226cc. Cleaned hydraulic filters. Drained and reserviced hydra ulic fluid. Installed new airframe fuel filter P/N 1743645-02. Installed new transmission oil filter P/N 204.040-760-109 . Installed new CEFA oil filter P/N 23066697. Lubed hydraulic pump adapter with Plastilube. Lubed litter door seal. Performed 100 Hour Inspection of M/R yoke. Performed 300 Hour recurring torque checks and swash plate tilt friction check. Adjusted swashplate tilt friction. Performed 300 Hour Inspection of BHT Optional Equip ment. Performed Inspections 'of all optional equipment items per the appropriate ICA Inspection Guidelines: 180 Day/500 Hour Inspection of BHT Emer gency Float Kit, 300 Hour/Annual Inspection of BHT Aux Fuel Tank Klt, Annual Inspe ction of AAI High Visibility Crew Doors, 300 Hour/Annual Inspection of AAI Floats teps, 300 Hour/Annual Inspection of AAI Aft Crosstube, Annual Inspection of AAI T/R Pedal Lockout Kit, 50 Hour/100 Hour/Annual Inspection of ACC Air Conditioner Kit, Annu inspe al ction of ACC Heater Kit, Annual Inspection of ACC Engine Bleed Air System, Annu al inspection of Bristol Aerospace WSPS, Annual Inspection of AAI Pre-Flight Step Hand les, 100 Hour/6 Month Inspection of AAI Skid Tubes, and Annual inspection of Edwards installed avionics per FAA 337/ICA's. Installed new ACC air conditioner compressor P/N S300S EC-6 & line P/N S-5050EC-H5. Performed 12 Month Inspection of M/R mast. Performed 24 Month Inspection of fuel syste m, cyclic controls, and M/R flight control bolts Performed 1200 Hour/24 Month Inspection of T/R pitch change control tube. Removed M/R Hub Assembly P/N 407-010-100-115 S/N A-393 TSN 611.2 TO 1641. Installed 4 each new Bearings P/N 407.310-101-105 SIN LK1102, SIN LK11586, S/N LK11491, and S/N LK11887, 2 each new Pitch Horns P/N 407-010-10 3-113 S/N AZ-146 and S/N AZ-298, and new Lower Plate P/N 406.010-117-125 SIN AZ-16 5. Reinstalled serviceable M/R Hub Assembly S/N A-393 TSN 611.2 TQ 1641. Removed T/R Blades P/N 406-016-100-119 S/N A-237 9 & S/N A-2403, both TSN 611.2 and sent to RBI for repair & refinishing. Reinstalled serviceable T/R Blades S/N A-2379 and S/N A-2403, both TSN 611.2. Installed 4 each new Transmission Corner Mounts P/N 407.310-203-101 S/N LP3931, S/N LK4307, S/N LP3881, & S/N LK4449. Removed engine Fuel Nozzle P/N 23077067 S/N 1PP02599 TSN 611.2 and installed overhauled Fuel Nozzle P/N 23077067 S/N AG59 355 TSO 0.0. Installed new starter generator brushes P/N 30300-1383. Installed new Fire Extinguisher Model RT-A6 00 SIN W-755929, Mfg 2005. Installed new R/H Auxiliary Fin P/N 407-023-00 3-106. LA-linua..t_ on A tzi- EFTA01702237  558802 AIRCRAF. !LW S/N ACTT 611.2 11-22-06 Entry Continued seats and sent to UAA for recovering and reinstalled. Removed seat belts/harnesses and sent to AmSafe Aviation for rewebbing and reinstalled. Installed new Flight Manual Pocket and Map Pockets from UAA. Removed AN UM 8, R/H Windshields P/N 407-546-1211-122 and installed new AAI U/H and PILOT R/H Windshields P/N 407-546.1211.122. :NG. 2 Installed new ELT Batteries, next due 9-2008. Performed ELT annual inspection. Performed transponder biennial inspection & pitot static system leak check. Removed Stormscope Processor P/N 78-8060-5790-3 S/N JWP03703338 and sent to L3 Communications for repair. Reinstalled repaired Processor S/N JWP03703338. Removed KSG105 DG Remote S/N 8288 and installed overhauled KS0105 DG Remote S/N 6628. Installed new 1K1 Start Relay PIN SM2OACD300A21. Installed new engine igniter plug P/N CH34187AJ0B. Ground run and leak checked good. Torque checked M/R mast nut, M/R hub through bolts, & MIR hub lower cone after 15` 1 ground run. AIRCRAF Balanced T/R & oil cooler assemblies and tracked & balanced M/R assy using RADS. OLT FLIGHT HI Power assurance check performed +22. PLETEC Swung compass. L. TOTALS B TOTALS F Complied with the following: TB 407-98-10 100 hour inspection & lube of T/R drive splines, no defects noted. ACCUMUL ASB 407-01.48(B) Part V & AD 2003-05.03(e) 150 hour inspection of tailboom, no defects noted. 10. NEXT SCE INSPECTIt ASB 407-04-63(B) & AD 2004.10-07 300 hour inspection & lube of T/R driveshaft bearings, no defects noted. TYPE INSI ASB 407-05-70(A) Inspected hydraulic servo clevis/shafts, no defects noted. (50, 100, E ASB 407-06-72 Inspected and found N/A to P/N 407-023401-109 S/N BP417 Horizontal ANNUAL I Stabilizer installed. DUE DATE ASB 407-06.73 Inspected and found N/A to turbine S/N CAT-44587; no turbine maintenance performed since 10.04 por CEB-A-72-6060. All work was performed per Bell's 407 and Rolls Royce C478 Maintenance Manuals. This FLIGHT aircraft complies with all applicable ASB's and AD's through ASB 407-06-73 and DISC REP. AD 2006-23-17 at the date of this inspection. See complete ASB/AD lists. This aircraft is approved for return to service. END 1 NOTE:, ..M/R mast nut, M/R hub through bolts, M/R hub lower cone, T/R mast nut due torque checks in 1 to 5 flight hours. CORREC ACTIC