EFTA Document EFTA01919378

Phone: Edwards Rotorcraft Solutions, Inc. 2011 South Perimeter Road, Suite L Fort Lauderdale Florida 33309 Fax: Email: HYPERION AIR C07301FL It em Descript ion Edwards Rotorcrelt Solutions. Inc. Friday, May 16, 2014 Make / Model: BELL 430 Serial Number: 49078 Registration: N331JE Total Time: Part s Labor 1 2 3 4 5 6 COMPLY 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: September 2016. $0.00 $53.00 COMR.Y 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 and §91.413 on pitot / static and transponder 'items Teas performed by Tropic Radio. Certification expiration May 31= 2016. $742.50 PERFORA 150 HOURAND 600 HOUR LIMITATION INSPECTION ON MAIN ROTOR YOKE ASS/3ABLY Reformed 150 hour aid 600 hour limitation inanections 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 Performed 50 hour / 12 month inspection in accordance with BHT-430-MM-2 Section 5-13 $0.00 Ind #6 FEWORA 150 HOUR/ 12 MONTH INSPECTION IN ACOORDANCE WITH BHT-430-SAM-2 SECTION 5-14 Reformed 150 hour 12 month inspection in =cordate 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 infection in accordance with 811T-430-MM-2 Table 4-2 on man rotor yokes FAA A099.23-03 pare D (Vertical fin attachment). FAA AD2006.19-02 and BHT AS3430-00-17 (Hydraulic actuator support) $0.00 Ind #6 FERFORM 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/ checksasapplicable to disturbed components $0.00 $19,610.00 EFTA_R1_00361521 EFTA01919378 Edwards Rotorcraft Solutions, Inc. r rib al 2011 South Perimeter Road, Suite L Fort Lauderdale Florida 33309 Phone: Fax: Email: s aw 116 1 0 Edwards Rotorcralt Solutions. Inc. Friday, May 16, 2014 HYPERION AIR Make / Model: BELL 430 C07301FL Serial Number: 49078 Registration: N331JE Total Time: It em Descript Ion Parts Labor 7 8 9 FERFORM 10 FERFORM 11 12 PERFORM EVERY 100 HOURSOFCOMFONENT OFERATION INS1ECTION ON SWAS-IRATE CONTROLS Performed every 100 hours of component operation Intsection in axordanoe with BHT-430-MM-2 Section 5.28 on arastiplate controls S0.00 Ind #6 FERFORM EVERY 300 HOURSOF COMPONENT OFERATION INS:ECTION ON 9NASHFLATE CONTROLS Reformed every 300 hours of component operation intsection in a:cadence with BHT-430-MM-2 Section 5-29 on avaMplate controls Reformed operational checks as applicable to digurbed components Soreetiplate friction measured al 31 lbs S0.00 Ind #6 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 edinguither and cartridge. Performed operational checks as applicable to disturbed components S0.00 Ind #6 EVERY 600 HOURS OR 12 MONTH OF COMPONENT OPERATION INWECTION AND 600 FIR/ 12 MONTH LUBRICATION Performed army 600 hours or 12 monthsol component operation inspection and 600 hour / 12 month lubrication requirements in accordence with BHT-430-MM-2 Section 5-31 end Figure 12-5 on man driveetutt (Engine to trawnision drive:haft) wet tel rotor drive haft. Performed operational aid leek checks as applicable to disturbed components and dynanic baffiCe of man drivretiatt's $288.60 Ind #6 EVEN 800 HOURS OF COM FON ENT OPERATION INSFECTION ON ENGINE STARTER GENERATOR AND M/R YOKES Reformed every 600 hours of component operation inwection in accordance with BHT-430-MM-2 Section 5-32 on engine staler generator and man rotor yokes Performed operational and leak checks as applicalre to disturbed components $3.34 Ind #6 PERFORM EVERY 6 MONTHS INS:ECTION ON STANDBY ATTITUDE INDICATOR Atrtormed every 6 months insedion in accordance with BHT-430-MM-2 Section 5.35 on standby attitude indication. Reformed operational cheeks as applicable to disturbed components $0.00 Ind #6 EFTA_R1_00361522 EFTA01919379 Phone: Edwards Rotorcraft Solutions, Inc. 2011 South Perimeter Road, Suite L Fort Lauderdale Florida 33309 Fax: Email: HYPERION AIR C07301FL It em Descript ion 0 Edwards Rotorcraft Solutions. Inc. Friday, May 16, 2014 Make / Model: BELL 430 Serial Number: 49078 Registration: N331JE Total Time: Parts Labor 13 14 15 16 17 18 PERFORM 6 MONTH INSPECTION ON CLOCK BATTERY FOWEFt SURLY %formed 6 month inspection in accordance with BHT-430-MM-10 Paragraph 95-200 on dock battery power gayly. FWformed operational checks as applicable to disturbed components $0.00 Ind #6 TEFFORM EVER Y2 CALENDARYEARSINSÆCTION IN ACCORDANCEWITH BHT-430-MM-2 Performed every 2 lenda yews inspection in accordance with BHT-430-MM -2 stadion 5-36 on washplate controls mån rotor mast, instruments and vertical fin. Nrformed operationg checks asapplicable to digurbei components Note: 41ECiai inspection required between 1- 5 flight hours in accordance with BHT-430-MM-2 Section 5-41 on main rotor yokes and between 5.lo flight hours in accordance with BHT- 430-MM-2 Section 5-42 on vertical fin. replaced vertical fin nuts (8) each. $993.80 51.696 00 PERFORM AFTER EVERY MAIN ROTOR BLADE REMOVAL WECTAL INWECTIN ON MAIN ROTORYOKES Performed after every mån rotor blale removal wecial inspection in accordance with BHT-430-MM-2 Section 5.40 on man rotor yokes $0 .00 Ind #6 PEFFORM 150 HOUR! 6 MONTH, 300 HOUR 600 HOUR! 12 MONTH AND MIW.ELLANEOUSS3WICING 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 tat rotor gearbox. now taxiing gear centering actuator. environmental control unit cooling turbine, trangnision. hydraulic reservoir, battery and electrical power receptacle. Serviced WI rotor gearbox and Irengnision oil sygeis with Royco 555 oil. Replaced tram's:ion oil filter with new item. Serviced hydraulic oil wgern with MIL-H-5606 oil. Performed operational aid leak checks as applicable to Ajtt heel rewnrinnante FERFORM 25 HOUR 50 HOUR 100 HOURS 300 HOUFtSAND 300 HOUR! 12 MONTH LUBRICATION REQUIREMENTS $454.23 Ind #6 FR -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 assembly, cyclic lever, tal rotor input lever bearing, idler link. collective lever, tel rotor driveshall hanger. crognead bearing hougng. counterweight Bekaa* hougng, flapping teeing housing and mån and noes landing gear wheels Rrformed operational checks as applicable to disturbed components $0.00 Ind #6 FEFFORM CORROSION CONTROL INSPECTION IN ACCORDANCE WITH CSTD-FEE-87-001 SECTION 30.7 l%formed corrosion control inspection in accordance with CM RE 87-001 Section 30-7 $0.00 $848.00 EFTA_R1_00381523 EFTA01919380 Phone: Edwards Rotorcraft Solutions, Inc. 2011 South Perimeter Road, Suite L Fort Lauderdale. Florida 33309 Fax: Email: HYPERION AIR C07301FL Item Descript ion aselmw 11 6 1 0 Edwards Rotorcraft solutions. Inc. Friday, May 16, 2014 Make / Model: BELL 430 Serial Number: 49078 Registration: N331JE Total Time: Parts Labor 19 20 21 C0MRY WITH FAA A D2008-19-02 AND BHT AS3430-00-17 Complied with FAA AD2008.19-02 Fora (a) effective October 16th. 2008 (Hydraulic actuator support) aid BHT AS3430-00-17 dated May 19th. 2000 (Hydraulic actuator stupor( p/n 222-040-125-001. Invention of) in accordance with AD aid A93 Instructions $0.00 S53.00 PERFORM 150 HOUR AND 300 HOUR/ 12 MONTH ENGINE INSFECTIONSAND SERVICING REQUIREMENTSON #1 ENGINE Performed 150 hour aid 300 hour 12 month engne inspections and syncing requirements in accordance with Roils Royce 250-C40B Operation aid Mantenasse Manua Section 72-00-00 Table 606 on No 1 engine. Drained and serviced engne oil system with Royco 560 oil. Replaced CEFA oil filter with new iten. Rarforrned operational aid lea checks as epplicable to disturbed components and compressor wash and rinse. $412.74 Ind 116 FERFORM 150 HOUR AND 300 HOUR? 12 MONTH &WINE INSFECTIONSAND SIRVICING REQUIREMENTSON #2 ENGINE Reformed 150 hour and 300 hour / 12 month engne inventions and Sewing requirements in accordance with Rolls Royce 250-C409 Operation and Maintenance Manua Section 72-00-00 Table 606 on NO. 2 engine. Drained and serviced engine oil system with Royco 560 oil. Replaced CEFA al filter with new den. Rarformed operational ad leek checks as applicable to disturbed components, ad compreeeor wash and rinse $0.00 Ind #6 PERFORM 300 HOUR/ 6 MONTH 600 HOUR/ 12 MONTH SERVICING REQUIREMENTS Pit/formed 300 hour / 6 month 600 hour I 12 month sarvicing requirements in accordance with Rolls Royce 250-C40B Operation ad 22 Maintenalce Mauna Section 72-00-00 Paa 8.0 - Engneaarvicing on ai9ne oil aid filter systems on both engines Serviced engine oil systems with Royca 560 oil. Replaced CEFA oil filterswith new items $1,917.90 Ind #6 23 24 PERFORM 100 HOUR ANNUAL AND 300 HOUR/ 1 YEAR INS'ECTIONS ON INLET BARRIER RLTEFt SYSTEM Performed 100 hour. annual and 300 hour / 1 yew inspections in accordance with Aerospace RItraion *gems Instructions for continued arworthiness Report No. A FS-E*1430-IBFICA on inlet barrier filter system. Rydormed operational cheas as applicable to disturbed components $0.00 Ind #6 OFERATORREFORTSNO. 1 HYDRAUUC PUMPLEAKING FROM SIAFT WAL ( STATIC LEAK) Trouble Mot PI Hydraulic system / pump. trouble Snot #2 Hydraulic system; during gear siring found =carve hydraulic fluid leaking from internal panels aid drain Song with gear leas down during timed up tern. Removed all panels renoved baggage floor aid found leek to be originating from hydraulic rider aseembly, troubleshot aid further found loose connection a valve body. gained axes tightened linestrid performed gear lest. no le* noted and gar pared unlock leg. $0.00 $3.392.00 EFTA_R1_00361524 EFTA01919381 Phone: Edwards Rotorcraft Solutions, Inc. 2011 South Perimeter Road, Suite L Fort Lauderdale Florida 33309 Fax: Email: HYPERION AIR C07301FL It em Descript ion Edwards Rotorcraft Solutions. Inc. Friday, May 16, 2014 Make / Model: BELL 430 Serial Number: 49078 Registration: N331JE Total Time: Parts Labor 25 26 27 28 29 30 OFERATORRS:ORTSCOPILOT AIR WINDOW HAS BROKEN CUP Replaced broken latch ataimbly. S82.00 $53.00 OPERATOR REPORTS LEFT HAND MICROSWITCH FOR DOOR LOCK FOSTION REQUIRES RERACEM ENT Removed interior ade pales ad adjusted both man cabin door stitches after course of a few days II DS caaion IOU cane back ad further trouNechooting reveled that door watch and terminal on item 55 below were caiang caution light. S0.00 $1.4 84 00 OPERATOR REFORTSOVERTORQUE OF MAIN ROTOR TO 105.6% FOR 2 SECONDS Performed al vista inspections in accordance with Chapter 5 over torque checklists S0.00 $1,484 00 OPERATOR REPORISOIL LEAK EVIDENT FROM NO. 1 ENGINE Clewed engne. engne deck wee ad performed leak check with black light. $161.80 $0.00 OPERATOR REPORTSOIL LEAK EVIDENT FROM NO. 2 ENGINE Cleaned engine. alone deck aea and performed IS check with black light. $0.00 $0.00 COMELY WITH FAA AD2008.14-01 AND BHT TB430-03-33 Complied with FAA AD2008-14-01 effective August 14, 2008 (Rid valve stitch) and BHT TB430-03-33 Datei .one 11, 2003 (Fuel wave aritch, rewiring ol) in axordance with AD and TB instructions Note: Verified previouly complied with. No action taken. $0.00 $0.00 EFTA_R1_00361525 EFTA01919382 Phone: Edwards Rotorcraft Solutions, Inc. 2011 South Perimeter Road, Suite L Fort Lauderdale. Florida 33309 Fax: Email: HYPERION AIR C07301FL It em Descript ion ai itmw 11 6 10 Edwards Rotorcraft solutions, Inc. Friday, May 16, 2014 Make / Model: BELL 430 Serial Number: 49078 Registration: N331JE Total Time: Parts Labor 31 32 33 34 35 36 COMPLY WITH FAA AD2013-18-06 AND BHT AS430-09-42 Complied with FAA AD2013.18-06 effective October 17, 2013 (Baring ingalation) aid BHT AS3430-09-42 Dated April 7, 2009 (Sakai bearings one time inspecting of) in accordance with AD and AS3Instruchons S0.00 $0.00 COMPLY WITH FAA AD2013-20-03 AND BHT A93430-0544 Complied with FAA AD2013-20-03 Effective December 5. 2013 (Third stage turbine vibration). BHT ASB430-05-34 Dated June 10. 2005 (New traaent limit and power turbine FFM (NP) Seedy Sate operation avoidance, Introduction of). and Rolls Royce 250-CA0B CEB A-72- 5048 Dated June 13. 2005 (Encino Turbine assembly - Nev threshold event recording and new Seedy-stale operaion avoidance range limit) in a:cordaice with AD, AS1 and C133 Indruchons Sap Varificrl nrcntinaldu enninliad with Nn 2rtinn Item RIGHT HAND MAIN LANDING GEAR WHEIEL THROUGH BOLT, NUT AND WAS-IERS DAMAGED. REQUIRE REPLACEMENT S0.00 $0 .00 Man aiding gear wheel trough bolt. nut. aid washer had mechanical damage a corrosion beyond Stowable limits removed aid replaced with new PAW 8HTI MM-5. S941.30 $53 00 RIGHT AND RIGHT HAND MAIN LANDING GEARWHEEL ASSEMBLY DAMAGED BEYOND LIMITATIONS Removed aid replaced both man lading wheel asiemblies $20,184.00 $1,272.00 RIGHT AND LET HAND MAIN LANDING GEAR WHS AXLE PACERSCORRODED. RIMUIRE FaEFLACEMENT Removed and replaced right had landing gear awl wet:erswith new due to corrosion beyond allowable limits $2.046.00 $318.00 NO. 1 DRIVESHAFT FORWARD CAPDAMAGED. RBSUIRESREPLACINENT Replaced No. 1 man drive:hit forward retaner cap with new item pin 222-044.682-103 in accordance with BHT-430-CR& 0 chacter 63. WA FR $0.00 EFTA_R1_00361526 EFTA01919383 Phone: Edwards Rotorcraft Solutions, Inc. 2011 South Perimeter Road. Suite L Fort Lauderdale Florida 33309 Fax: Email: HYPERION AIR C07301FL Item Descript ion aiitmw 116 10 Edwards Rotorcraft Solutions. Inc. Friday, May 16, 2014 Make / Model: BELL 430 Serial Number: 49078 Registration: N331JE Total Time: Parts Labor 37 38 39 40 41 42 NO. 1 ENGINE EXHAUST SECTOR CRACKS Removed #1 exhaust gad( and 93nt to Miami for certified repair. reinstated exhaua stack. S562.50 $212.00 LOWER ANTI COLLISON LIGHT INOPERATIVE Trouble 910t lower anti colliaon light found strobe assembly to be awned out most likely due to hydraulic fluid leek. 5475.00 $106.00 NO. 2 HYDRAULIC SYSTEM LEAKING ON FIGHT HAND SDE OF LOWER RJSELAGE Investigated discrepancy and noted loess fitting on right had wing for lading gear system. Secured fitting. Work performed in accordance with BHT-430-MM chaster 7 and 32. FErformel operational aid leek diedesas applicable to disturbed components No further discrepancies noted. 50 00 Item #24 ALL 1ELE-TEMFS FOR MAIN ROTOR DRIVESHAFTSTO BE RERACED Replaced teietemps for man rotor drive:elan with new itemspin 6000.1 (qty 8) aid 6000-2 (qty 8) in accordance with INIT-430-CRS 0 chi*" 32 $263.25 $212.00 TAIL ROTOR GEARBOX CHIPDETECTOR LEAKING AND CHECK VALVE DOES NOT RJLLY CLOSE Investigated discrepancy. Removed. darned. inspected. and instated tal rotor chip detector aid homing No mechanical defects noted. Replaced packings for detector aid houang with new 'terns p/n; AS3209-011 aid M8324811-907. Work performed in accordance with BHT430-MM Chapter 65. Performed leek checks as applicable to disturbed components No further discrepancies noted. $2.12 $159.00 DRVE LINK BOLT RN 50-04706-86 DAMAGED. FEOUIRES REPLACEMENT Replaced drive link bolt rain 50-04706-99 with new item ems p/n in accordance with BHT-430-MM chapter 67. $1.362.00 $0.00 EFTA_R1_00361527 EFTA01919384 Phone: Edwards Rotorcraft Solutions, Inc. 2011 South Perimeter Road, Suite L Fort Lauderdale Florida 33309 Fax: Email: HYPERION AIR C07301FL It em Descript ion Edwards Rotorcraft Solutions. Inc. Friday, May 16, 2014 Make / Model: BELL 430 Serial Number: 49078 Registration: N331JE Total Time: Parts Labor 43 44 45 46 47 48 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 action to be taken. $0.00 $106.00 TAIL ROTOR CONTROL TUBE HAS CONTACT AGAINST LIGHTNING HOLE IN BULKHEAD Inspected tail rotor control tube. Mechanical damage limited to siperficial damage to pant only. Applied protective finish to frees as applicable Work performed din exordaxe with SIT-430-MM Chapter 67 and BHT-ALL-SPM Chapter 3. Complied with BHT AS3430.13.51 Dated September 3. 2013 (p/n 430-001-007-101. tail rotor control tube assembly modification) In accordance with AS Instructions $260.00 $212.00 WAS.IER NOT INSTALLS ON RGHT HAND MAIN LANDING GEAR AXEL RN 140-009A81 5112 Installed new washer RN 140-009A813112 in axordaxe with BI-ITI M M-5. S9.95 $0 .00 NUTRATE DAMAGE FOR RIGHT HAND UFFEFt STABILIZER ACCESS PANEL (3RD FROM TOP, FORWARD am) Raplaced nut plate with new item p/n MS71059L3 for right hand stabilizer upper aces paned 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 peas to be deteriorated beyond allowable limits removed (misting pads and installed new pads 24 month inspection. $3,290.00 $1,272.00 MAIN ROTOR HUB THROUGH BOLTS (X8) AND DRVE BUSHINGS (X7) DAMAGED Main rotor hub through bons (8) each and drive bushings (7 ) each have mechanical da-nage and wear beyond allowable limits 24 month inspection. S21.205.00 Ind #47 EFTA_R1_00361528 EFTA01919385 Phone: Edwards Rotorcraft Solutions, Inc. 2011 South Perimeter Road, Suite L Fort Lauderdale Florida 33309 Fax: Email: HYPERION AIR C07301FL It em Descript ion ai,tmw 116 10 Edwards Rotorcret Solutions. Inc. Friday, May 16, 2014 Make / Model: BELL 430 Serial Number: 49078 Registration: N331JE Total Time: Parts Labor 49 50 51 52 53 54 MAIN ROTOR RICH CHANGE LINK LOWER BOLTS DAMAGED (4) each man rotor pitch links have wear aid mechanical damage beyond allowable limits 24 month Invection. S1,056 00 $0.00 TAIL ROTOR FiTCH CHANGE LINKS WORN BEYOND UMITATIONS Replaced tail rotor pitch control links with new itemspin 230.312-001.101 in accordance with BHT-430-MM chapter 67. $9.990.00 $106.00 COLLECTIVE UNK BOLT DAMAGED Collective link bolt found to have mechanical damage beyond alowable limits 24 month invection. $1,519 00 $53.00 SERVO MOUNT BOLT DAMAGED Savo mount bolt found to hate mechanical damage beyond +Movable limits 24 month inwelion. $339.00 $106.00 NO. 2 ENGINE COMPRESSOR SCROLL DISCHARGE DUCT DAMAGED Engne compress>, discharge duct round to be damaged beyond allowable limits removed and replaced with nee. $1,461.00 $212.00 EECTOR BLADE CRACKED ON LEFT HAND INLET COWLING. BLADE LOCATED 3RD FROM BOTTOM Removed aid replaced defective cowling ejector blade. fagener aid grommet. $36.55 $79.50 EFTA_R1_00361529 EFTA01919386 Phone: Edwards Rotorcraft Solutions, Inc. 2011 South Perimeter Road, Suite L Fort Lauderdale Florida 33309 Fax: Email: HYPERION AIR C07301FL It em Descript ion Edwards Rotorcratt Solutions, Inc. Friday, May 16, 2014 Make / Model: BELL 430 Serial Number: 49078 Registration: N331JE Total Time: Parts Labor 55 56 57 58 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 troublefhooting determined that the baggage door micro *etch and terminal were found to be defective. S1,060.00 $1.272.00 FERFORM TAIL ROTOR DRVE SHAFT AND MAIN ROTOR TRACK AND BALANCE Performed bane of both crone drive than% tal rotor and man rotor track aid balance. 50.00 5848.00 Conaimables S4.000 00 S0.00 Freight Chases $620.00 $0.00 SUB-TOTAL $75,739.58 $35.377.50 10% DISCOUNT ON LABOR FOR LONG TGRiV1 CUSTOMER R54 DB A GRESIBV T $0.00 -53 537 75 5% DISCOUNT ON BBL SaECIAL ORDERED PARTS FIST DB A GREI3,18V TOTAL -53 232 13 $0.00 $102,377.23 EFTA_R1_00361530 EFTA01919387