DS9 Document EFTA01155090

Phone Item Edwards Rotorcraft Solutions, Inc. 2011 South Perimeter Road. Suite L Fort Lauderdale. Florida 33309 Fax: Email: • HYPERION AIR O37301FL Description Edwards Rotorcraft Solutions, Inc. Friday, May 16, 2014 Make / Model: BELL 430 Serial Number: 49078 Registration: N331JE Total Time: Parts Labor 1 2 3 4 5 6 COMFLY WITH 12 MONTH TEST FEOUIFEMENTSON ELT SYSTEM Complied with 12 month lest requirements in accordance with 14 CFR Part 91 §91.207(d) on ELT sigem. Battery due replacement.. September 2016. $0.00 $53.00 COMFLY WITH 24 MONTH TEST REOUIFEMENTSON RIOT! STATIC AND TFtA NSFONDER SYSTBA S Complied with 24 month leg requirements in accordance with 14 CFA Pan 91 §91.411 and §91.413 on pitot / static and transponder systems Tests performed by Tropic Radio. Certification expiration May 31g. 2016. $742.50 FEFFORM 150 HOUR AND 600 HOUR UMITATION INSFECTION ON MAIN ROTOR YOKEAS93ABLY Reformed 150 hour and 600 how limitation inspections in accordance with BHT-430-MM-2 Table 4-2 on man rotor yoke assembly. $0.00 Ind #6 FEFFORM 50 HOUR! 12 MONTH INSFECTION Ftsformed 50 hour / 12 month inspection in accordance with BHT-430-MM-2 Section 5.13 $0.00 Ind #6 PEFFORM 150 HOUR! 12 MONTH INSFECTION IN ACCORDANCE WITH BHT-430-MM-2 SECTION 5.14 FWformed 150 hour / 12 month inspection in accordancewith BHT-430-MM-2 Section 5.14. Performed operational checksas applicable to disturbed components Note: Contentsal the following performed during compliance of thisaction 150 hour limitation inspection in accordance with 947-430-MM-2 Table 4-2 on man rotor yokes FAA A099.23.03 para D (Vertical lin attachment). FAA A02008-19.02 and BHT AS430-00-17 (Hyckaulic actuator sipport) $0.00 Ind #6 PERFORM 600 HOUR/ ANNUAL INMECTION IN ACCORDANCE WITH BHT-430-MM-2 MOTION 5.15 FWformed 600 hour / annual inspection in accordance with BHT 430-MM-2 Section 5-15. Reformed operational checks as applicable to disturbed components $0.00 $19,610.00 EFTA01155090 Phone: Edwards Rotorcraft Solutions, Inc. 2011 South Perimeter Road. Suite L Fort Lauderdale. Florida 33309 Fax: Email: • Edwards Rotorcraft Solutions, Inc. Friday, May 16, 2014 HYPERION AIR Make / Model: BELL 430 037301FL Serial Number: 49078 Registration: N331JE Total Time: It em Description Part S Labor 7 8 FEFFORM 9 FERFOFM 10 FERFO 11 12 PERFORA EVER( 100 HOURS OF COMPONENT OPERATION INSPECTION ON SINA9IPLATE CONTROLS Pctformed every 100 hoursof component operation inspection in accordance with BHT-430-M M-2 action 5.28 on snashplate controls $0.00 Ind #6 FERFOFM EVERY 300 HOU FtSOF COM FONENT 0 FEFtATION INSPECTION ON SWARMATE CONTROLS arlormed every 300 hoursof component operation inspection in acoordance with BHT-430-M M-2 action 5.29 on avashplate controls Fir formed operational checks as applicable to disturbed components Svashplate friction measured at 31 lbs $0.00 Ind #6 EVERY 600 HOURSOR 6 MONTHSOF COMPONENT OFERATION INSP ON RFE EXTINGUISHER AND CARTRIDGE Performed every 600 hoursor 6 months ol component operation inspection in accordance with BHT-430-MM-2 action 5-30 on engine fire extingiidter and cartridge. Pet formed operational checks as applicable to disturbed components $0.00 Ind #6 EVERY 600 HOURSOR 12 MONTH OF COMFONENT OPERATION INSPECTION AND 600 HR/ 12 MONTH LUBRICATION Fbrformed every 600 hoursor 12 months of component operation inqtection and 600 hour / 12 month lubrication requirements in accordance with BHT-430-MM-2 action 5-31 and Rgure 12.5 on man driveMalt (Engine to trananission driveshaft) and tail rotor driveshall. Ftt formed operational and leak checks asapplicable to disturbed components and dynamic balance of man driveshafFs $288.60 Ind #6 RM EVERY 600 HOURSOF COMPONENT OPERATION INSPECTION ON ENGINE STARTER GENERATOR AND M/ R YOKES Ftirformed every 600 hoursof component operation inspection in acoordance with BHT-430-M M-2 action 5.32 on engine garter generator and main rotor yokes Performed operational and leak chedtsas applicable to disturbed components $3.34 Ind #6 FEFFORM EVERY 6 MONTHS INSPECTION ON STANDBY ATTITUDE INDICATOR Ferformed every 6 months inspection in accordance with BHT-430-MM-2 Section 5.35 on Sandby attitude indication. Rorlormed operational checks as applicable to disturbed components $0.00 Ind #6 EFTA01155091 Phone: It em Edwards Rotorcraft Solutions, Inc. 2011 South Perimeter Road. Suite L Fort Lauderdale, Florida 33309 Fax: Email: • HYPERION AIR O37301FL Description Edwards Rotorcraft Solutions, Inc. Friday, May 16, 2014 Make / Model: BELL 430 Serial Number: 49078 Registration: N331JE Total Time: Part S Labor 13 14 15 16 17 18 FERFOFIA 6 MONTH INSECTION ON CLOCK BATTERY POWER SURLY Performed 6 month inadection in accordance with BH7.430-MM-10 Paragraph 95.200 on clock battery power apply. Performed operational checks as applicable to disturbed components $0.00 Ind #6 PERFORM EVERY 2 CALENDAR YEARS INSFECTION IN ACCORDANCE WITH BHT-430-MM-2 Performed every 2 calendar years invection in accordance with BHT-430-MM-2 Saction 536 on weashplate controls main rotor mat instruments and vertical lin. Performed operational checks as applicable to disturbed components. Note: *card invection required between 1- 5 flight hoursin accordance with BHT-430-MM-2 aCtion 5.41 on main rotor yokes and between 5.10 flight hours in accordance with BHT- 430-MM-2 &lotion 5.42 on vertical lin. replaced vertical fin nuts (8) each. $993.80 $1.696.00 PEPPORM AFTER EVERY MAIN ROTOR BLADE FtEMOVAL SPECIAL INSFECTIN ON MAIN ROTOR YOKES Performed after every man rotor blade removal coda inspection in accordance with 847-430-MM-2 action 5.40 on main rotor yokes $0.00 Ind #6 PERFORM 150 HOUR! 6 MONTH, 300 HOUR, 600 HOUR/ 12 MONTH AND MISCELLANEOUSSERV ICING FtEOUIREMENTS Performed 150 hour / 6 month. 300 hour. 600 hour / 12 month and mixellanocus wrWcing requirements in accordance with BHT-430-MM- 2. Rgure 12.1 on tel rotor gearbox. now landing gear centering actuator. environmental control unit cooling turbine. transnission. hydraulic restivoir. battery and electrical power receptacle. avviced tail rotor gearbox and transnission oil systems with Royco 555 oil. Replaced transnission oil tiller with new flan. Serviced hydraulic oil side!) with MIL-H-5606 oil. Performed operational and leek checks as applicable lo rnmnnnantc FIFFORM 25 HOUR, 50 HOUR, 100 HOURS 300 HOURSAND 300 HOUR/ 12 MONTH LUEFdCATION FtEOUIFEMENTS $454.23 Ind #6 Redeemed 25 hour. 50 hour. 100 hours 300 hour and 300 hour f 12 month lubrication requirernentsin accordance with BHT-430-MM-2 Rgure 12.5 on pitch link univocal. rotating ring assembly. cyclic lever. tall rotor input lever bearing. idler link. collective lever. tail rotor driverhalt hanger. crosshead bearing housing, counterweight Belli:rank houdng. flapping bearing houang and main and nos? landing gear wheels Reformed operational checks as applicable lo disturbed components $0.00 Ind #6 PEFFORIA COFFOSON CONTROL INSPECTION IN ACCORDANCE WITH CMFEE-87-001 SECTION 30.7 Ft/formed corrodon control invection in accordance with CSSD-Pg-87.001 action 30-7 $0.00 $848.00 EFTA01155092 Phone It em Edwards Rotorcraft Solutions, Inc. 2011 South Perimeter Road. Suite L Fort Lauderdale, Florida 33309 Fax: Email: • HYPERI0N AIR O37301FL Description al n Edwards Rotorcraft Solutions, Inc. Friday, May 16, 2014 Make / Model: BELL 430 Serial Number: 49078 Registration: Total Time: Part s N331JE Labor 19 20 21 22 23 24 COM FLY WITH FAA AD2008.19-02 AND EHT AS8430-00.17 Complied wilh FAA A D2008-19-02 Para (a) effectiveOda/far 16th, 2008 (Hydraulic actualor sipport) and BHT A93430-00-17 dated May 19th. 2000 (Hydraulic aclualor swport prn 222-040-125-001. inwedion of) in accordance with AD and A93 intudions FEFLORA 150 HOUR AND 300 HOUR/ 12 MONTH ENGINE INSPECTIONSAND SERVICING REQUIRal ENTSON N1 ENGINE %formed 150 hour and 300 hour / 12 monlh engine inqaeclions and sarvicing requirements in accordance with Rolls Royce 250-C40B Operation and Maintenance Manual action 72-00-00 Table 606 on No 1 engine. Drained and serviced engine oil system with Royco 560 oil. Replaced CEFA oil filler with new item. Nrformed operalional and Walt *wits asapplicable to diaurbed components and compressor wash and rinm. R3:tRDR)4 150 HOUR AND 300 HOUR! 12 MONTH ENGINE INSPECTIONSAND SERVICING REQUIFEMENTSON 82 ENGINE unformed 150 hour and 300 hour / 12 monlh engine inqaeclions and sarvicing requirements in accordance with Polls Royce 250-C40B Operation and Mainlenance Manual. Section 72.00.00 Table 606 on NO. 2 engine. Drained and sarviced engine oil system with Royoa 560 oil. Replaced CEFA oil filter with new ilem. Rarformed operalional and le* checks as applicable to disturbed components and compressor wash and rinse. PEfFORIA 300 HOUR/ 6 MONTH 600 HOUR/ 12 MONTH SERVICING REQUIREMENTS Ftdormed 300 hour / 6 month 600 hour / 12 monlh wevicing requirements in accordance with Flails Royce 250-C408 Operation and Mainlenance Manual. Section 72.00.00 Paa 8.D Engine servicing on engine oil and filter systemson both engines Serviced engine oil systems with Royce 560 oil. Replaced CEFA oil fillerswith new hems R3:FORIA 100 HOUR ANNUAL AND 300 HOUR/ 1 YEAR INSFECTIONSON INLET BARRIER FILTER SYSTEM %formed 100 hour. annual and 300 hour / 1 year inwectionsin accordance with Aerospace nitration Systems indrudionslor continued airworthiness Report No. A FSBH430-IBF-ICA on inlet barrier filler sygem. Perlormed operational chedts as applicable to disturbed components OPERATOR REFORTS NO. 1 HYDRAULIC RUMP LEAKING FROM 9IAFT SEAL ( STATIC LEA Trouble Mot N1 Hydraulic system / pump, !rouble Mol 42 Hydrailic system: during gear wing found excessive hydraulic fluid leaking from internal panels and drain along with gear leek down during timed up led. Removed all panels removed baggage floor and found leak to be originating from hydraulic wider assembly. trouble Mot and further found Wow connection at valve body, gained access lightened linesand performed gear led, no 'Minified and gear passed uplock test. $0.00 $53.00 $412.74 Ind #6 $0.00 Ind #6 $1,917.90 Ind #6 $0.00 Ind #6 $0.00 $3.392.00 EFTA01155093 Phone: It em Edwards Rotorcraft Solutions, Inc. 2011 South Perimeter Road. Suite L Fort Lauderdale, Florida 33309 Fax: Email: • HYPERION AIR 037301FL Description Edwards Rotorcraft Solutions, Inc. Friday, May 16, 2014 Make / Model: BELL 430 Serial Number: 49078 Registration: N331JE Total Time: Part S Labor 25 26 27 28 29 30 OPERATOR FEFOFITSCO-FILOT AIR WINDOW HAS BROKEN CUP Replaced broken latch amen*. $82.00 $53.00 OFERATOR REPORTS LBT HAND MICFOSWITCH FOR DOOR LOCK POSITION FEOU IRBB RERACEM ENT Removed inlerior sde panelsand adjusted bolh man cabin door witches after come of a lee days II DScantion Inghl came bah and further troubleshooting reveled than door witch and terminal on item 55 below were cauSng caution $0.00 $1.484.00 OPERATOR FEPORTSOVERTOROUE OF MAIN ROTOR TO 105.6% FOR 2 SECONDS Ryformed all visual inveclions in accordance with Chapter 5 over torque checklists. $0.00 $1.484.00 OPERATOR REFOFITSOIL LEAK EVIDENT FROM NO. 1 ENGINE Clewed engine. engine deck area and performed leek check with black light. $161.80 $0.00 OFERATOR FEFORTSO IL LEAK EVIDENT FROM NO. 2 ENGINE Cleaned engine. engine deck area and performed leek check with black light. $0.00 $0.00 COM FLY WITH FAA AD2008.14-01 AND BHT TB430-03.33 Complied wilh FAA A D2008-14-01 effective August 14, 2008 (Fuel valve stitch) and BHT TB430.03.33 Dated June 11. 2003 (Rues valve switch. rewiring ol) in accordance with AD and TB instructions Note: Verified previoudy complied wilh. No action taken. $0.00 $0.00 EFTA01155094 Phone It em Edwards Rotorcraft Solutions, Inc. 2011 South Perimeter Road. Suite L Fort Lauderdale Florida 33309 Fax Email: • HYPERION AIR 037301FL Description Edwards Rotorcraft Solutions, Inc. Friday, May 16, 2014 Make / Model: BELL 430 Serial Number: 49078 Registration: N331JE Total Time: Part S Labor 31 32 33 34 35 36 COMPLY WITH FAA AD2013.18-06 AND BHT AS3430-09-42 Complied wilh FAA AD2013-18-06 effectiveOctober 17. 2013 (Bearing installation) and 9 -IT A93430.09.42 Dated April 7. 2009 (staked beaings one lime invading ol) in accordance with AD and A 93 Instructions $0.00 $0.00 COM FLY WITH FAA AD2013.20-03 AND BHT AS6430-05-34 Complied wilh FAA A D2013.20.03 Elleclive December 5. 2013 (Third gage lurbine vibration). BHT AS430.05-34 Dated June 10. 2005 (New trangent limil and power turbine RIM (NP) Seedy state operalion avoidance. Introduction of). and Polls Fbyce 250-C408 CEB A-72. 5048 Dated -tine 13. 2005 (Engine. Turbine aseembIy New threshold event recording and new steady-gale operation avoidance range limit) in accordance with AD. A . aid CEBIrntructions AIM, 11 stair-lel exrrmini Leh. rnmnline4 ittil Fs bi n Winn Yiu.n $0.00 $0.00 RIGHT HAND MAIN LANDING GEAR WHEEL THROUGH SDLT, NUT AND WASHEFtSDAMAGED. PEOUIRE REPLACEMENT Main landing gear wheel trough boll. nut. and washer had mechanical damage a corrogon beyond allowable limits removed aid replaced with new IAW BHTI M M.5. $941.30 $53.00 RIGHT AND FIGHT HAND MAIN LANDING GEAR WHEEL AS93vIBLY DAMAGED BEYOND LIMITATIONS Removed and replaced both man landing wheel assemblies $20.184.00 $1.272.00 FIGHT AND LEFT HAND MAIN LANDING GEAR WHEEL AXLE SPACERSCORRODED. FtRIUIFE REPLACEMENT Removed and replaced right hand landing gear are spars with new due to oorroaon beyond stowable limits $2,046.00 $318.00 NO. 1 DRIV MIA FT FORWARD CAP DAMAGED. REOUIFtESFERACEMENT Repladed No. 1 man driverhalt lorwad retainer cap with new item pin 222-044-682-103 in accordaw.e with BHT-430-CRS 0 chapter 63. WARR $0.00 EFTA01155095 Phone: Item Edwards Rotorcraft Solutions, Inc. 2011 South Perimeter Road. Suite L Fort Lauderdale Florida 33309 Fax: Email: • HYPERION AIR 037301FL Description Edwards Rotorcraft Solutions, Inc. Friday, May 16, 2014 Make / Model: BELL 430 Serial Number: 49078 Registration: N331JE Total Time: Part S Labor 37 38 39 40 41 42 NO. 1 ENGINE EXHAUST SECTOR CRACKED Removed #1 Waist stack and sent to Miami for certified rimer. reinggled exhaug Sack. $562.50 $212.00 LOWER A NTI COWSON UGHT INOPERATIVE Trouble Mot lower anti colliaon light found strobe assembly to be gloried out mog likely due to hydraulic flied leak. $475.00 $106.00 NO. 2 HYDRAULIC SYSTEM LEAKING ON FIGHT HAND SDE OF LOWER RJSELAGE Investigated discrepancy and noted loom Idling on right hand wing for landing gear Osten. Smered lilting. Work performed in accordance with BHT-030-MM chapter 7 and 32. Performed operational and leak chedeas applicable to digurbed components No further discrepancies noted. $0.00 Item #24 ALL TEI_E-TEMFS FOR MAIN ROTOR DRIVESHAFTSTO BE REPLACED Replaced teletempslor main rotor drive-Malt with new items pr n 6000.1 (qty 8) and 6000-2 (qty 8) in accordance with BHT-430-CR8 0 chgater 32 $263.25 $212.00 TAIL ROTOR GEARBOX CHIP DETECTOR LEAKING AND CHECK VALVE DOES NOT FULLY CLOSE Investigated discrepancy. Removed. cleaned. inadected. and installed tail rotor chip detector and houang No mechanical detects noted. Replaced padkinil s tor detector and houang with new itemspin: AS3209.011 and M83248/1.907. Work performed in accordance with BHT-030-MM Chapter 65. Reformed leak checks as gdplicable to digurbed components No further discrepancies noted. $2.12 $159.00 DRIVE UNK SOLT RN 50-047C6-66 DAMAGED. REQUIRES FEFLACEM ENT Replaced drive link bolt pen 50.047C6-99 with new item we pin in accordance with BHT-430-MM chapter 67. $1,362.00 $0.00 EFTA01155096 Phone It em Edwards Rotorcraft Solutions, Inc. 2011 South Perimeter Road. Suite L Fort Lauderdale, Florida 33309 Fax: Email: • HYPERION AIR 037301FL Description Edwards Rotorcraft Solutions, Inc. Friday, May 16, 2014 Make / Model: BELL 430 Serial Number: 49078 Registration: N331JE Total Time: Part S Labor 43 44 45 46 47 48 TAIL ROTOR SERVO LEAKING AT SERVO Investigated discrepancy in accordance with BHT.430-MM chapter 29. Leasage rale determined to be within permissible limitations. No further action to be taken. $0.00 $106.00 TAIL ROTOR CONTROL TUBE HASCONTACT AGAINST LIGHTNING HOLE IN BULKHEAD Invected tail rotor control tube. Mechanica damage limited to ape/tidal damage to pant only. Applied protective linith to areas as applicable. Work performed din accordance with BHT-430-MM Chapter 67 and BHT-A LL-SPM Chapter 3. Complied with BHT AS3430.13.51 Dated September 3. 2013 (pin 430-001407-101, tail rotor control tube assembly modification) in accordance with AS3 Instructions $260.00 $212.00 WASHER NOT INSTALLED ON RIGHT HAND MAIN LANDING GEAR AXEL FYN 140-009A81S1 12 Installed new washer FYN 140-009A813112 in accordance with BHTI M M $9.95 $0.00 NUTRATE DAMAGE FOR RIGHT HAND UFFER STA BIUZER ACCESS PANEL (3RD FROM TOP, FORWARD BM) Replaced nut plate with new item pin M 1059L3 for right hand stabilizer upper axespanel in accordance with EtLIT-ALL-ScIM Chapter 3 $0.00 $106.00 CENTER BUFFER PA DSFOR MAIN ROTOR YOKES DA MAGED EEYOND 10% FEPA IR LIMITATIONS Rs/formed 24 month man rotor yoke inspection and found buffer pads to be deteriorated beyond allowable limits. removed existing pads aid installed nevi pads 24 month inspection. $3,290.00 $1,272.00 MAIN ROTOR HUB THROUGH BOLTS (X8) AND DRIVE BUSHINGS (X7) DAMAGED Man rotor hub through bolts (8) each aid drive buSings (7) each have mechanical damage and wear beyond alowable limits 24 month inspection. $21,205.00 Ind #47 EFTA01155097 It em Edwards Rotorcraft Solutions, Inc. 2011 South Perimeter Road. Suite L Lauderdale Florida 33309 Phone: Fax: Email: HYPERION AIR 037301FL Description Edwards Rotorcraft Solutions, Inc. Friday, May 16, 2014 Make / Model: BELL 430 Serial Number: 49078 Registration: N331JE Total Time: Part S Labor 49 50 51 52 53 54 MAIN ROTOR PITCH CHANGE UNK LOWEF1BOLTS DAMAGED (4) each man rotor pitch links have wear and mechanical damage beyond allowable limits 24 month inspection. $1,056.00 $0.00 TAIL ROTOR PITCH CHANGE UNKS WO RN BEYOND UMITATIONS Replaced tat rotor pitch control links wish new items prn 230-312-001-101 in aocordance with BHT-430-MM chapter 67. $9,990.00 $106.00 COLLECTIVE UNK BOLT DAMAGED Collective link bolt found to have mechanical damage beyond allowable limils 24 month inspection. $1,519.00 $53.00 SERVO MOUNT BOLT DAMAGED Savo mount bolt lourd to have mechanical damage beyond allowable limits 24 month ingoeclion. $339.00 $106.00 NO. 2 ENGINE COM PRESSOR SCROLL DISDHARGE DUCT DAMAGED Engne compressor dir-harge dud found to be damaged beyond allowable limils removed and replaced with new. $1,461.00 $212.00 EJECTOR BLADE CRACKED ON LEFT HAND INLET COWLING. BLADE LOCATED 3RD FROM BOTTOM Removed and replaced defective cowling ejector blade. fastener and gommd. $36.55 $79.50 EFTA01155098 Phone: It em Edwards Rotorcraft Solutions, Inc. 2011 South Perimeter Road. Suite L Fort Lauderdale Florida 33309 Fax: Email: • HYPERION AIR 037301FL Description Edwards Rotorcraft Solutions, Inc. Friday, May 16, 2014 Make / Model: BELL 430 Serial Number: 49078 Registration: N331JE Total Time: Part S Labor 55 56 57 58 BAGGAGE DOOR MICROSNITCH FOUND TO BE DEFECTIVEAND CAUSNG IIDS CAUTION During trouble Tooling of item 26 above the caution light cane on over the course of the weekend. further troubleshooting determined that the baggage door micro snitch and terminal were found to be ddective. $1,060.00 $1.272.00 FEFFORM TAIL ROTOR DRIVESHAFT AND MAIN ROTOR TRAGIC AND BALANCE Rdformed balance of both engine drive shahs tail rotor and man rotor track and bane. $0.00 $848.00 Constmables $4,000.00 $0.00 Freght Charges $620.00 $0.00 SUBTOTAL $75.739.58 $35,377.50 5% DISCOUNT ON BELL ScECIAL ORDERED PA nrs FB4 °SAGAMI/15NT -$3,202.10 $0.00 TOTAL $107,914.98 EFTA01155099