EFTA02685105.pdf

Edwards Rotorcraft Solutions, Inc. 2011 South Perimeter Road, Suite L Lauderdale, Florida 33309 Phone: Fax: Email: • Edwards Rotorcralt Solutions, Inc. Friday, May 16, 2014 HYPERION AIR Make / Model: BELL 430 Serial Number: Registration: Total Time: It em Descript ion Part s Labor COMRS WITH 12 MONTH TEST REOUIRBA ENTS ON ELT SYSTEM Complied with 12 month tat requirements in accordanat with 14 CFR Part 91 §91.207(d) on ELT system. Battery due replacement: 1 September 2016. $0.00 $53.00 COMFLY WITH 24 MONTH TEST REOUIRBIA ENTS ON RIOT / STATIC AND TRANSPONDER SYSTEMS Complied with 24 month test requirements in accordance with 14 CFR Pet 91 §91.411 ad §91.413 on pitot / static aid transponder 2 'items Tees performed by Tropic Radio. Certification expiration May 31e. 2016. $742.50 PERFORM 150 HOURAND 600 HOUR LIMITATION INSPECTION ON MAIN ROTOR YOKE ASS/3ABLY 3 Reformed 150 hour aid 600 hour limitation inadections in accordance with BHT-430•M M-2 Table 4.2 on man rotor yoke ariernbly. $0.00 Ind #6 PERFORM 50 HOUR/ 12 MONTH INSPECTION 4 Performed 50 hour / 12 month inspection in accordasce with BHT-430-MM-2 Section 5-13 $0.00 Ind #6 FEWORA 150 HOUR/ 12 MONTH INSPECTION IN ACCORDANCE WITH BHT-430-MM-2 SECTION 5-14 Reformed 150 hour 12 month inspection in accorda-ice with BHT-430-MM-2 Section 5-14. Performed operational checksas applicable to disturbed components Note: Contents of the following performed during compliance of this action • 150 hour limitation invection in 5 accordance with 017-430-MM-2 Table 4-2 on man rotor yokes FAA A099.23-03 paa D (Vertical fin attachment). FAA AD2006.19-02 $0.00 Ind #6 and BHT AS3430-00-17 (Hydraulic actuator support) PERFORM 600 HOUR/ ANNUAL INSPECTION IN ACCORDANCE WITH BHT-43041M-2 SECTION 5-15 Rearmed 600 hour! annual inspection in accordance with BHT-430-MM-2 Section 5-15. Performed operations/ checks as applicsbie to 6 disurbed components $0.00 $19.610.00 EFTA_R1_02008390 EFTA02685105  Edwards Rotorcraft Solutions, Inc. 2011 South Perimeter Road, Suite L Fort Lauderdale, Florida 33309 s aw 116 1 0 Phorii Fax: Email: Edwards Rotorcraft Solutions. Inc. Friday, May 16, 2014 HYPERION AIR Make / Model: BELL 430 Serial Number: • Registration: Total Time: It em Descript Ion Parts Labor FERFORM EVERY 100 HOURSOFCOMFONENT OFERATION INSIECTION ON WAS-IRATECONTROLS 7 Performed every 100 hoursof component operation Inasection in axordace with BHT-430-MM-2 &Ction 5.28 on seastiplate controls $0.00 Ind 46 PERFORM EVERY 300 HOURSOF COMPONENT OFERATION INSPECTION ON 9NASHFLATE CONTROLS Reformed every 300 hours of component operation Mae:ellen in a:cadence with BHT-430-MM-2 Section 5-29 on avaMplate controls 8 S0.00 Ind 116 Reformed operational checks as appliasble to digurbed components Sometiplate friction measured al 31 lbs PEF:FORM EVERY 600 HOURSOR6 MONTHSOFCOMFONENT OPERATION IN9) ON FIRE ECINGUI94ER AND CARTRIDGE Performed every 600 hours or 6 months of component operation inspection in accordance with DIT-430-MM-2 Section 5-30 on engne fire 9 S0.00 Ind 46 eginguither and cartridge. Performed opergional checks as applicable to disturbed components FERFORM EVERY 600 HOURS OR 12 MONTH OF COMPONENT OPERATION INWECTION AND 600 MR/ 12 MONTH LUBRICATION Performed easy 600 hours or 12 monthsof component operation inspection and 600 hour t 12 month lubrication requirements in 10 accordence with BEIT-430-MM-2 Section 5-31 aid Figure 12-5 on man drive:tett (Engine to trawnigion driveehaft) gel tel rotor drive:haft. $288.60 Ind #6 Performed operational and leek checks as applicable to disturbed components and dynanic baaice of man drivgliatt's FERFORM EVEN 800 HOURS OF COMFONENT OPERATION INSFECTION ON ENGINE STARTER GENERATOR AND Mt R YOKES Reformed every 600 hours of component operation inaction in exordave with BHT-430-MM-2 Section 5-32 on engne staler generator 11 and man rotor yokes Performed operational and leak checksasapplied:4e to disturbed components $3.34 Ind #6 PERFORM EVERY 6 MONTHS INS:ECTION ON STANDBY ATTITUDE INDICATOR Reformed every 6 monthsinto:ton in accordance with BHT-430-MM-2 Section 5.35 on standby attitude indication. Reformed operational 12 checks as applicable to disturbed components $0.00 Ind #6 EFTA_R1_02008391 EFTA02685106  Edwards Rotorcraft Solutions, Inc. 2011 South Perimeter Road, Suite L Lauderdale Florida 33309 s aw 116 10 Phone: Fax: Email: Edwards Rotorcraft Solutions. Inc. Friday, May 16, 2014 HYPERION AIR Make / Model: Serial Number: Registration: Total Time: It em Descript ion Parts Labor FERFORPA 6 MONTH INSPECTION ON CLOCK BATTERY FOWEFt 9JFFLY Rrformed 6 month inspection in accordance with BHT-430-MM-10 Paragraph 95-200 on dock battery power apply. FWformed operational 13 $0.00 Ind #6 checks as applicable to disturbed components PERFORM EVERY 2 CALENDARYEAFtSINSFECTION IN ACCORDANCE WITH BHT-430-MM-2 Performed every 2 Benda years inspection in accordance with BHT-430-MM -2 &salon 5-36 on egashplate controls man rotor mast, instruments and vertical fin. Nrformed operational checks asapplicable to disturbed components Note: Leda inspection required between 1- 14 $993.80 Si 696 00 5 flight hours in accordance with BHT-430-MM-2 Section 5-41 on man rotor yoke& aid between 5.10 flight hours in accords-ice with BHT- 430-MM-2 Section 5-42 on vertical fin. replaced vertical fin nuts (8) each. FERFORM AFTER EVERY MAIN ROTOR BADE RIEMOVAL SPECIAL INSPECTIN ON MAIN ROTOR YOKES 15 Reformed after every man rotor blale removal special inaction in accordance with BIT-430-MM-2 Bongo 5.40 on man rotor yokes $0 .00 hid #6 PEFFORM 150 HOUR! 6 MONTH, 300 HOUR 600 HOUR! 12 MONTH AND MIXBJANEOUS931VICING REQUIREMENTS Reformed 150 hour / 6 month. 300 hour. 600 hour! 12 month aid miscellaneous servicing requirements in accordance with BHT-430-MM- 2. Figure 12-1 on tail rotor gearbox. nom taxiing gee centering actuator. environmental control unit cooling turbine, trawnigion. hydraulic 16 reservoir, battery end electrical power receptacle. Serviced tail rotor gearbox aid Irmsnigion oil sygems with Royco 555 oil. Replaced $454.23 Ind #6 traismisgon oil filter with new item. Serviced hydraulic oil wen with MIL-H-5606 oil. Performed opergione aid leek cheers as applicable to Achirluel rnmnanante FERFORM 25 HOUR 50 HOUR 100 HOURS, 300 HOUFtSAND 300 HOUR! 12 MONTH LUBRICATION REQUIREMENTS Formed 25 hour. 50 hour. 100 hours 300 hour and 300 hour 12 month lubrication requirements in accordance with BHT-430-MM-2 Figure 12-5 on pitch link universal. rotating ring agernbly, cyclic lever, tel rotor input lever bearing, idler link. collective lever, tail rotor 17 $0.00 Ind #6 driveshalt haver. ore-gland bearing housing. counterweight Sentra* housng. flapping beating housing aid men aid noes laiding gear wheels Reformed operational checks as applicable to disturbed components FEFFORM CORFtOSON CONTROL INSPECTION IN ACCORDANCE WITH CSTD-PSE-87-001 SECTION 30.7 18 Reformed corrosion control inspection in accordance with C.S33 FEE 87-001 Section 30-7 $0.00 $848.00 EFTA_R1_02008392 EFTA02685107  Edwards Rotorcraft Solutions, Inc. 2011 South Perimeter Road, Suite L Lauderdale Florida 33309 ai ir ma 11 6 1 0 Phone: ifFax Email. Edwards Rotorcraft Solutions. Inc. Friday, May 16, 2014 HYPERION AIR Make / Model: BELL 430 Serial Number: Registration: Total Time: ■ Item Descript ion Parts Labor COMPLY WITH FAA A D2008-19-02 AND BHT AS3430-00-17 Complied with FAA AD2008.19-02 RECO (a) effective October 16th. 2008 (Hydraulic actuator support) aid BHT AS3430-00-17 dated May 19 $0.00 553.00 19th. 2000 (Hydraulic actuator report pin 222-040-125-001. Inspection of) in accordance with AD awl A93 Instructions PERFORM 150 HOUR AND 300 HOUR/ 12 MONTH ENGINE INSFECTIONSAND SERVICING REQUIREMENTSON #1 ENGINE Performed 150 hour and 300 hour 12 month engne inspections and syncing requirements in accordance with Rolls Royce 250-C40B Operation aid Mantenalce Manuel Section 72-00-00 Table 606 on No 1 engine. Drained and serviced engne oil system with Royco 560 oil. 20 $412.74 Ind 116 Replaced CEFA oil filter with new iten. Reformed operationat old leek checks as epplicable to disturbed components and compressor wash and rinse. FERFORM 150 HOUR AND 300 HOUR? 12 MONTH &WINE INSFECTIONSAND SIRVICING REQUIREMENTSON #2 ENGINE Reformed 150 hour and 300 hour / 12 month engne directions and 93fwing requirements in accordance with Rolls Royce 250-O409 Operation and Mainteinance Manua Section 72-00-00 Table 606 on NO. 2 engine. Drained and serviced engine oil system with Royce 560 21 50.00 Ind #6 oil. Replaced CWA al filter with new den. Rarformed operational ad leek checks as applicable to disturbed COmpOnerds, ad compreeenr wash and tin= PERFORM 300 HOUR/ 6 MONTH 600 HOUR/ 12 MONTH SERVICING REQUIREMENTS Reformed 300 hour 1 6 month 600 hour I 12 month sevicing requirements in accordance with Rolls Royce 250-C40B Operation and 22 Maintenalce Manual, Section 72-00-00 Para 8.0 - Engine =noting on engine oil and filter systems on both engines Serviced engine oil systems $1,917.90 Ind #6 with %yea 560 oil. Replaced CWA oil filterswith new items PERFORM 100 HOUR ANNUAL AND 300 HOUR/ 1 YEAR INS'ECTIONS ON INLET BARRIER ALTER SYSTETA Reformed 100 hour. annual and 300 hour / 1 yea- inspections in accordance with Aerospace RItraion *gems Instructions for continued 23 arworthinees Report No. A FS-E*1430-IBFICA on inlet barrier filter system. Rydormed operational cheicks as applicable to disturbed $0.00 Ind #6 components OFERATORREFORTSNO. 1 HYDRAULIC PUMP LEAKING FROM SIAFT WAL ( STATIC LEAK) Trouble Mot PI Hydraulic system / pump. trouble Mot #2 Hydraulic system; during gear eying found =costive hydraulic fluid leaking from internal panels and dry= Song with gear leak down during timed up tern. Removed all panels renoved baggage floor aid found leek to be 24 originating from hydraulic rider aseembly, troubleshot aid further found loom connection a valve body. °tined axes tightened linesend $0.00 $3.392.00 performed gear lest. no leek noted and gar passed unlock leg. EFTA_R1_02008393 EFTA02685108  Edwards Rotorcraft Solutions, Inc. 2011 South Perimeter Road, Suite L Fort Lauderdale. Florida 33309 rf 0 Phone: Fax: Email Edwards Betatron Solutions. Inc. Friday, May 16, 2014 HYPERION AIR Make / Model: BELL 430 Serial Number: Registration: Total Time: It em Descript ion Part s Labor OFERATORREFORTSCO-RLOT AIR WINDOW HAS BROKEN CUP 25 Replaced broken latch assembly. S82.00 553.00 OFERATOR REPORTS LEFT HAND MICROSWITCH FOR DOOR LOCK FOSTION REQUIRES RERACIEM ENT Removed interior ade pavesand adjusted both man cabin door wenches after course of a few daysIIDScoition limit cane back old further 26 $0 .00 51 4 84 00 trouNeehooting reveled that door watch and terminal on item 55 below were caging caution light. OPERATOR REFORTSOVERTORQUE OF MAIN ROTOR TO 105.6% FOR 2 SECONDS 27 Reformed al visa invections in acoordaice with Chapter 5 over torque checklists $0 .00 $1,484 00 OPERATOR REPORISOIL LEAK EVIDENT FROM NO. 1 ENGINE 28 Clewed engine. engne deck wee aid performed leak check with black light. $161.80 $0.00 OPERATOR REPORTSOIL LEAK EVIDENT FROM NO. 2 ENGINE 29 Cleaned engne, engne deck am and performed leak diedc with black light. $0.00 $0.00 COMBS WITH FAA AD2008.14-01 AND MT TB430-03-33 Complied with FAA AD2008-14-01 effective August 14, 2008 (Biel valve watch) and BHT TB430-03-33 Dated .brie 11, 2003 (Fuel wave 30 $0.00 $0.00 witch, rewiring of) in accordance with AD and TB instructions Note: Verified previouly complied with. No action taken. EFTA_R1_02008394 EFTA02685109  Edwards Rotorcraft Solutions, Inc. 2011 South Perimeter Road, Suite L rt Lau I Florida33309 Email■ Phone: . Fax: Edwards Rotorcraft Solutions. Inc. Friday, May 16, 2014 HYPERION AIR Make / Model: BELL 430 Serial Number: Registration: Total Time: It em Description Parts Labor COMPLY WITH FAA AD2013-18-06 AND BHT AS3430-09-42 Complied with FAA AD2013.18-06 effective October 17, 2013 (Baring ingaltation) aid BHT AS3430-09-42 Dried April 7, 2009 (Sakai 31 $0.00 $0 .00 bearings one time inspecting of) in accordmce with AD and A93 instructions COMPLY WITH FAA AD2013-20-03 AND BHT A93430-0544 Complied with FAA AD2013-20-03 Effective December 5. 2013 (Third gage turbine vibration). BHT A334 30-O5-34 Dated June 10. 2005 (New trzneent limit aid power turbine FFM (NP) Seedy Sate operation /madam Introduction of). and Rolls Royce 250-CA0B CEB A-72- 32 5048 Dated June 13. 2005 (Engine Turbine asearnbly - New threshold event recording and new aeady-stale operation atoidance range limit) S0.00 S0.00 in accordance with AD, A . and CEBIndruchons snip, Varificrl nrcntinaldu enninliad with Nn 2rtinn Item RIGHT HAND MAIN LANDING GEAR WHEIEL THROUGH BOLT. NUT AND WAS-IERS DAMAGED. REQUIRE REPLACEMENT Man aiding gear wheel trough bolt. nut. aid washer had mechanical damage a corroeon beyond allowable limits removed aid replaced with 33 new PAW 8HTI MM-5. $941.30 $53.00 RIGHT AND RIGHT HAND MAIN LANDING GEARWHEEL ASSEMBLY DAMAGED BEYOND LIMITATIONS 34 Removed and replaced both man lading wheel arremblies $20,184.00 $1,272.00 RIGHT AND LEFT HAND MAIN LANDING GEAR YVHSEL AXLE PACERSCORRODED. REQUIRE FaEFLACEMENT 35 Removed aid replaced right had landing gear asel aceastswith new due to corroeon beyond allowable limits $2,046.00 $318.00 NO. 1 DRIVESHAFT FORWARD CAPDAMAGED. REQUIRESREPLACEMENT 36 Replaced No. I man drive:hit forward retana cap with new item pin 222-044.682-103 in aocordace with BHT-430-CR& 0 chaater 63. WARR $0.00 EFTA_R1_02008395 EFTA02685110  Edwards Rotorcraft Solutions, Inc. 2011 South Perimeter Road, Suite L rt Lauderdale, Florida 33309 ai itmw 116 1 0 Phone: , Fax Email: Edwards Rotorcrsit Solutions. Inc. Friday, May 16, 2014 HYPERION AIR Make / Model: BELL 430 Serial Number: Registration: Total Time: ■ Item Description Parts Labor NO. 1 ENGINE BCHAUST SECTOR CRACKS 37 Removed 111 exhaust gad( and 93nt to Miami for certified repar. reinstated exhaua stack. $562.50 $212.00 LOWER ANTI COLLISON LIGHT INOPERATIVE 38 Trouble 910t lower anti colliaon light found strobe assembly to be awned out most likely due to hydraulic fluid leek. 5475.00 S106.00 NO. 2 HYDRAULIC SYSTEM LEAKING ON FIGHT HAND SDE OF LOWER RJS2LAGE Invertigated discrepency and noted loose fitting on right held wing for larding gear satem. Secured fitting. Work performed in accordance with 39 BHT-430-MM chepter 7 and 32. FErformel operational aid leek diedisas applicable to disturbed components No further discrepancies $0 .00 Item #24 noted. ALL 1ELE-TEMFS FOR MAIN ROTOR DRIVESHAFTSTO BE RERACED Replaced tele-temps for man rotor driveshaft with new itemspin 6000.1 (qty 8) aid 6000-2 (qty 8) in accordance with 0 40 chin 32 $263.25 $212.00 TAIL ROTOR GEARBOX CHIPDETECTOR LEAKING AND CHECK VALVE DOES N0T RJLLY CL0SE Investigated diszrepancy. Removed. darned. inspected. and instated tal rotor chip detector and housing. No mechanical defects noted. 41 Replaced pad/Vsfor detector aid lousing with new 'terns p/n; AS3209-011 aid M8324811-907. Work performed in ern/dance with $2.12 $159.00 BHT430-MM Chapter 65. Performed leek checks as applicable to disturbed components No further discrepaicies noted. DRVE LINK BOLT RN 50-04706-86 DAMAGED. FEOUIRES REPLACEMENT 42 Resta:led drive link bolt rain 50-04706-99 with new item ems pln in accordance with BHT-430-MM chapter 67. $1,362.00 $0.00 EFTA_R1_02008396 EFTA02685111  Edwards Rotorcraft Solutions, Inc. 2011 South Perimeter Road, Suite L Fort Lauderdale, Florida 33309 S in rf 0 Phone Fax: Email: • Edwards Rotorcraft Solutions. Inc. Friday, May 16, 2014 Make / Model: HIS • BELL 430 Serial Number: Registration: Total Time: Item Description Parts Labor TAIL ROTOR SERVO LEAKING AT SERVO Inveedigated dis:repaxy in accordance with BHT-430-MM chapter 29. Leakage rate determined to be within permisible limitations No further 43 $0.00 S106 00 action to be taken. TAIL ROTOR CONTROL TUBE HAS CONTACT AGAINST LIGHTNING HOLE IN BULKHEAD Inverted tail rotor control tube. Mechanical damage limited to siperficial damage to pant only. Applied protective finith to freesasapplicable 44 Work performed din axordexe with SIT-430-MM Chapter 67 and BHT-ALL-SPM Chapter 3. Complied with BHT AS3430.13.51 Dated $260.00 S212.00 September 3. 2013 (pin 430-001-007-101. tail rotor control tube assembly modification) In accordance with AS Instructions WAS.IER NOT INSTALLED ON RGHT HAND MAIN LANDING GEAR AXEL RN 140-009A815112 45 II-dated new washer RN 140-009A81S1 12 in exordaxe with 8HTI M M-5. S9.95 $0 .00 NUTRATE DAMAGE FOR RIGHT HAND UFFEFt STABILIZER Acces PANEL (3RD FROM TOP, FORWARD &ID) 46 Replaced nut plate with new item p/n MS71059L3 for right hand stabilizer upper emspaned in accordance with SIT-A LL-SRM Chapter 3 $0.00 $106.00 CENTER BUFFER PADS FOR MAIN ROTOR YOKES DAMAGED BEYOND 10% REPAIR LIMITATIONS Performed 24 month man rotor yoke inspection and found buffer pads to be deteriorated beyond allowable limits removed (misting pads and 47 installed new pads 24 month insection. $3,290.00 $1,272.00 MAIN ROTOR HUB THROUGH BOLTS (X8) AND DRVE BUSHINGS (X7) DAMAGED Main rotor hub through bolts (8) ern and drive bushings (7 ) each have mechanical da-nage and wear beyond allowable limits 24 month 48 inspection. S21.205.00 Ind #47 EFTA_R1_02008397 EFTA02685112  Edwards Rotorcraft Solutions, Inc. 2011 South Perimeter Road, Suite L Fort Lauderdale. Florida 33309 ai ra 0 Phone: Fax: Edwards Rotorcraft Solutions. Inc. Friday, May 16, 2014 Make / Model: BELL 430 Seal ration:: R Registration: Total Time: It em Descript ion Parts Labor MAIN ROTOR RICH CHANGE LINK LOWER BOLTS DAMAGED 49 (4) each man rotor pitd) links have wear aid mechanical damage beyond allowable limits 24 month inmedion. S1,056 00 $0 .00 TAIL ROTOR RICH CHANGE LINKS WORN BEYOND UMITATIONS 50 Notated tail rotor pitch control linkswith new itemspin 230.312.001.101 in accordance with BHT-430-MM chapter 67. $9.990.00 S106.00 COLLECTIVE UNK BOLT DAMAGED 51 Collective link bolt found to have mechanical damage beyond allowable limits 24 month invention. S1.519 00 $53.00 93W0 MOUNT BOLT DAMAGED 52 Savo mount bolt found to hate mechanical damage beyond allowable limits 24 month inwection. $339.00 $106 00 NO. 2 ENGINE COMFRESEOR SCROLL DISCHARGE DUCT DAMAGED 53 Engne compressor distharge duct found to be damaged beyond allowable limits removed aid replaced with new. $1,461.00 $212.00 EECTOR BLADE CRACKED ON LEFT HAND INLET COWLING. BLADE LOCATED 3RD FROM BOTTOM 54 Removed aid replaced defective cowling ejector blade. fawner aM grommet. $36.55 $79.50 EFTA_R1_02008398 EFTA02685113  Edwards Rotorcraft Solutions, Inc. 2011 South Perimeter Road, Suite L Lauderdale Florida 33309 11 0 Phone: Fax Email■ Edwards Rotorcratt Solutions. Inc. Friday, May 16, 2014 HYPERION AIR Make / Model: BELL 430 Serial Number: Registration: Total Time: It em Description Parts Labor BAGGAGE DOORMICROSINITCH FOUND TO BE DEf£CTIVEAND CAUSING IIDS CAUTION During trouble tooting of item 26 above the coition light cane on over the course of the weekend, further troubleshooting determined that 55 the baggage door micro snitch and terminal were found to be defective. S1,060 00 S1.272.00 FERFORM TAIL ROTOR DRVE SHAFT AND MAIN ROTOR TRACK AND BALANCE 56 Performed bane of both crone drive Sons tal rotor and man rotor track aid balance. $0 .00 $848.00 57 Consimables $4.000.00 S0.00 58 Freight Charges $620.00 $0.00 a/B-TOTAL $75,739.58 $35.377.50 5% DISCOUNT ON HELL ScECIAL °ROMEO I44RTSFEr? USA GRB31.4BV T 2') 2 ' $0.00 TOTAL $107,914.98 EFTA_R1_02008399 EFTA02685114