EFTA01120072.pdf

Edwards Rotorcraft Solutions Inc. CUSTOMER ORDER 2011 S. Perimeter Road, Suite L Fort Lauderdale Fl. 33309 Order Number: C03486FL Phone Or Date: 4/9/2012 Fax Page: 1 Sold To Sh To FREEDOM AIR INTERNATIONAL, INC FREEDOM AIR INTERNATIONAL, INC 1131 PINE POINT ROAD 1131 PINE POINT ROAD SINGER ISLAND, FL 33404 SINGER ISLAND, FL 33404 UNITED STATES UNITED STATES CUSTOMER ID CUSTOMER P.O. PAYMENT TERMS FREIGHT TERMS 04911 PREPAID/CREDIT CARD Freight billed SALES REP ID SHPPING METHOD F.O.B. SHIP DATE SHARIEFA AU 2/15/2012 QUANTITY IT UNIT EXTENDED Otto PART ID I DESCRIPTION X PRICE PRICE 1.00 FLA-MAINTENANCE 300 HOUR / 12 MTH INSPECTION 77,406.10 $77,406.10 Work Order ID: C03486FL 1 SEE DETAIL REPORT SUB TOTAL $77,406.10 SALES TAX $4,644.37 FREIGHT CHARGES $905.00 TOTAL ORDER AMOUNT $82,955.47 EFTA01120072  EFTA01120073 Date Printed : April 05, 2012 Edwards Rotorcraft Solutions Inc. Order Charge Detail Report C03486FL Customer ID 04911 Aircraft I Item Aircraft Time 823.2 FREEDOM AIR INTERNATIONAL. INC Type iQZ Enloe Time 823.4 1131 PINE POINT ROAD a 53375 823.2 SINGER ISLAND. FL 33404 Reldstration No. tgLuga Part No Deactl on Isa.ue City MM Unit Price Ext. Price 1743645-03 FUEL FILTER KR 1.00 EA $99.00 $99.00 2-009 PACKING 1.00 EA $10.67 $10.67 206-040-279-101 PACKING 1.00 EA $34.95 $34.95 206-050-247-131 COVER ASSEMBLY RH 1.00 EA $516.00 $516.00 23066697 ELEMENT - LUBE,FILTER 5/0 1.00 EA $692.25 $692.25 555-1OT ROYCO 555 OT 10.00 EA $19.86 $198.60 67588 SPRING 1.00 EA $15.95 $15.95 756-10T ROYCO 756 MILPRF5606H 1.00 EA $9.62 $9.62 AS3208-03 PACKING 2.00 EA $1.00 $2.00 AS3209-014 PACKING 1.00 EA $1.90 $1.90 AS3209-016 PACKING 1.00 EA $14.20 $14.20 AS3209-024 PACKING 2.00 EA $3.30 $6.60 AS3209-113 PACKING 1.00 EA $15.30 $15.30 AS3209-126 PACKING 1.00 EA $3.70 $3.70 M25988/1-138 PACKING 1.00 EA $12.75 $12.75 M83248/1-021 PACKING -PREFORMED 1.00 EA $1.30 $1.30 M83248/1-029 PACKING 1.00 EA $1.13 $1.13 MOBIL254OT MOBIL JET OIL 254 5.00 EA $24.78 $123.90 MS21042L4 NUT 7.00 EA $1.30 $9.10 MS21042L5 NUT 12.00 EA $1.50 $18.00 MS28773-12 RETAINER TEFLON 2.00 EA $2.47 $4.94 MS28774-211 RETAINER TEFLON 2.00 EA $1.45 $2.90 MS28775.211 ORING: NITRILE, 70. HYDRAULIC 2.00 EA $0.67 $1.34 MS28778-16 PACKING 2.00 EA $1.00 $2.00 MS28778-4 PACKING 5.00 EA $0.70 $a 50 MS29513-270 PACKING 1.00 EA $11.40 $11.40 MS9372-029 GASKET. METAL 0 -RING 3.00 EA $18.20 $54.60 $1,867.60 Part No Ihttalise ?zap_ Sellinu PrIce SrL Se 1271762 PRESSURE VESSEL 2.00 EA P005071FU1 $6,110.00 $12,220.00 204040.760.109 FILTER ELEMENT 3U 1.00 EA P005081FL11 $452.00 $452.00 206-073-761.101 DECAL 2.00 EA P005320FU2 $27.30 $54.60 206-076-034-003 HYDRAULIC FILTER ELEMENT 2.00 EA P005082FU1 $287.00 $574.00 209-340-265-103 SEAL 1.00 EA P005320FU6 $413.00 $413.00 31-023-8B DECAL 2.00 EA P005320FU3 $2.50 $5.00 31-023-9B DECAL 2.00 EA P005320FU4 $3.80 $7.60 406-012-108-107 PITCH HORN ASSEMBLY 2.00 EA PO05232FU3 54,175.00 $8.350.00 406-376-001-101 GASKET 1.00 EA P005081F1J5 $23.05 $23.05 407-001-116-101 SHOCK CORD ASSEMBLY 2.00 EA PO05232FL/2 $113.00 $226.00  EFTA01120074 407-023-003-105 AUX FIN ASSEMBLY 1.00 EA PO05313FU2 $alsoao $8,150.00 407-073-762-101 DECAL 2.00 EA PO05313FU1 $128.00 $256.00 407-362-013-103 FUEL PRESSURE SWITCH 1.00 EA PO05313FU3 51.384.00 $1,364.00 7270 BELT 1.00 EA PO05233FU1 $89.34 $89.34 AS3208-03 PACKING 1.00 EA PO05320FU1 $1.00 $1.00 AS3209-140 PACKING 1.00 EA PO05320FU5 $6.60 $6.60 AS3209-162 ORING: FLUOROCARBON,75 1.00 EA P005231FL/3 $6.15 $6.15 AS3209-236 PACKING 1.00 EA PO05081FU2 $4.60 $4.60 AS3209-240 PACKING 1.00 EA PO05320FL/7 $5.75 $5.75 AS3209-258 PACKING 1.00 EA P005231FIJ4 $8.80 $8.80 D0164-1 BOLT (LONG) 4.00 EA PO05308FU1 $96.00 $384.00 D0314-1 FRICTION PAD ASSEMBLY 4.00 EA PO05292FU1 $973.00 $3,892.00 M2002-1 STARTER BRUSH 4.00 EA PO05231FU2 $96.77 $387.08 MS21920-66 CLAMP 1.00 EA PO05232FU5 $82.00 $82.00 MS28775-015 PACKING 2.00 EA PO05093FU1 $0.53 $1.07 MS28778-12 ORING 3.00 EA PO05328FU1 $3.20 $9.60 MS28778-6 PACKING 2.00 EA PO0S177FU2 $0.85 $1.70 RG407 BATTERY:SEALED LEAD ACID 1.00 EA PO05231FU1 $4,165.00 $4,165.00 SL211-3-1 CLIP NUT 2.00 EA PO05320FU8 $3.15 $6.30 $41,146.24 MISC 40 PERFORM AIR SPEED PEDAL STOP FUNCTIONAL TEST IN $142.50 ACCORDANCE WITH BHT-407-MM CHAPTER 96 PARAGRAPH 96- 358 PG. # 493. PRESSURIZED PITOT TUBE AIRSPEED READS 55 KTS RUDDER PEDAL STOP ENGAGES 51 KTS DISENGAGES. MISC 50 P/N 407440-011-103 M/R MAST ASSEMBLY S/N: BP19,T TT: 823.2 $3,112.61 INSPECT AND REPAIR AS NECESSARY. MISC 60 P/N 407-023-003-105 FINLETT ASSEMBLY S/N: BP258 $660.00 REQUESTING PAINTING OF FINLETT IN ACCORDANCE WITH BHT- 407-SPM Regular hour 190.48 Regular Total $20,190.88 Overtime hour 77.13 Ohime Total $12,263.67 Consumables $250.00 Freight Charge: $905.00 Discount -$2,227.40 Price Grand total $78.311.10  EFTA01120075 Edwards Rotorcraft Solutions, Inc. Art a 2011 South Perimeter Road, Suite L .K Fort Lauderdale, Florida 33309 Phone Fax: Email:- Edwards Rotorcraft Solutions, Inc. Thursday, April 05, 2012 CO3486FL FREEDOM AIR, INC Make / Model: BELL 407 Serial Number: 53375 Registration: N491GM Total Time: 823.2 Item Description PARTS LABOR HRS LABOR $$ COMPLY WITH FAA AD2005-03-07 EFFECTIVE MARCH 17TH, 2005 Complied with FAA AD2005-03-07 Effective March 17th, 2005 (Landing gear crosstubes) and BHT ASB407-03.59 Dated October 15th, 2003 (All forward and aft 1 crosstube assemblies, part numbers as described below, assignment of RIN (retirement index number) to) in accordance with AD and ASB Instructions. RIN count assigned as 79 for each crosstube as of date of installation. (PERFORM POWER ASSURANCE CHECK IN ACCORDANCE WITH BHT-4O7-FMS-3, SECTION 4 2 Performed power assurance check in accordance with BHT-407-FMS-3 Section 4. Engine calculated at; (+ 12). (COMPLY WITH FAA AD2O11-25-O1 EFFICTIVE JANUARY 17TH, 2012 Complied with FAA AD2011.25.01 Effective January 17th, 2012 (Apical Industries 3 Emergency Floatation Kit) in accordance with AD Instructions. Not applicable due to configuration of aircraft. Apical kit not installed. (PERFORM 12 MONTH TEST IN ACCORDANCE WITH 14CFR PART 91§91.2O7(D) ON ELT SYSTEM Performed 12 month test in accordance with 14CFR Part 91 §91.207(d) on ELT 4 system. Battery due replacement; March 2015 PERFORM 100 HOUR LIMITATION INSPECTION IN ACCORDANCE WITH BHT-407-MM-1, TABLE 4-2 ON YOKE ASSEMBLY Performed 100 hour limitation inspection in accordance with BHT-407-MM-1 Table 4- 5 2 on Yoke assembly (PERFORM 300 HOUR / 12 MONTH INSPECTION IN ACCORDANCE WITH BHT-407-MM-1 SECTION 5-12 THRU 5-18 Performed 300 hour / 12 month inspection in accordance with BHT-407-MM-1 6 Sections 5-12 through 5-18. Operational check, leak check, and dynamic balance of tail rotor system performed satisfactorily.  EFTA01120076 !PERFORM 150 HOUR INSPECTION IN ACCORDANCE WITH BHT-407-MM-1 SECTION 5 18A ON ENGINE CONTROLS Performed 150 hour inspection in accordance with BHT-407-MM-1 Section 5.18A on 7 Engine controls. Work performed under Item No 6 'PERFORM 300 HOUR INSPECTION FOR OPTIONAL EQUIPMENT ON PARTICLE SEPARATOR, ROTOR BRAKE, DUAL CONTROL Performed 300 hour inspection for optional equipment in accordance with BHT- 8 407-MM-1 Section 5-19 on Particle separator, Rotor brake, and Dual control. !PERFORM 300 HOUR, 300 HOUR OR 12 MONTH AND 25 MONTH INSPECTION ON AUXILIARY FUEL SYSTEM Performed 300 hour, 300 hour or 12 month, and 24 month inspections in 9 accordance with BHT-407-MM-1 Section 5-19 and BHT-407-MMS-6 Sections 5-3 and 5-4 on Auxiliary fuel system. Operational and leak checks performed satisfactorily. !PERFORM 600 HOUR INSPECTION ON ROTOR BRAKE AND MAIN ROTOR FRAHM Performed 600 hour inspection in accordance with BHT-407-MM-1 Section 5-20 on 10 Rotor brake and Main rotor Frahm. Operational and leak checks performed satisfactorily. 'PERFORM 600 HOUR OR 6 MONTH INSPECTION ON MAIN ROTOR HUB AND BLADE Performed 600 hour or 6 month inspection in accordance with BHT-407-MM-1 11 Section 5-21 on Main rotor hub and blade 'PERFORM 12 MONTH INSPECTION IN ACCORDANCE WITH BHT-407-MM-1, SECTION 5-22 Performed 12 month inspection in accordance with BHT-407-MM-1 Section 5-22. Operational checks, leak checks, post ground run special Inspection on lower cone, 12 and dynamic balance of main rotor system performed satisfactorily. Special inspection required In 1 - 5 flight hours on lower cone. !PERFORM 300 HOUR SPECIAL INSPECTIONS IN ACCORDANCE WITH BHT-407-MM-1, TABLE 5-3 Performed 300 hour special inspections in accordance with BHT-407-MM-1 Table 5-3 13 on Tail rotor gearbox, Tail rotor driveshaft disc pack couplings, Tail rotor hub mast nut, Tailboom attachment hardware, Swashplate tilt friction. Swashplate friction 'PERFORM 12 MONTH COMPONENT INTERIM INSPECTION ON MAST POLE Performed 12 month component interim inspection in accordance with BHT-407- MM-1 Table 5.4 on Mast pole. Post ground run special inspection performed 14 satisfactorily. Special inspection required between 1 - 5 flight hours in accordance with BHT-407-MM-1 Table 5-3 on Main rotor mast nut. !PERFORM 12 MONTH OR 500 FLIGHT HOUR INSPECTION ON EMERGENCY FLOATATION SYSTEM Performed 12 month or 500 flight hour inspection in accordance with BHT-407-MMS 15 1 on Emergency floatation system.  EFTA01120077 I PERFORM DAILY AND 100 HOUR LIMITATION INSPECTIONS IN ACCORDANCE WITH BHT-407-MM-1, TABLE 4-2 Performed Daily and 100 hour limitation inspections in accordance with BHT-407- MM-1 Table 4-2 and BHT ASB407-07-80 Parts Ill and IV Dated August 27th, 2007 16 (Tai!boom assembly 407-030-801-107, and 407-530-014-101/-103, New inspection renuirements) on Tailboom assembly. I PERFORM 206 SERIES 100 HOUR OR 90 DAY CORROSION INSPECTION IN ACCORDANCE WITH CSSD-PSE-87-001 Performed 206 Series 100 hour or 90 day corrosion inspection in accordance with 17 CSSD-PSE-87.001 Section 30-5 I PERFORM 300 HOUR SERVICING REQUIREMENTS ON AIRFRAME FUEL FILER Performed 300 hour servicing requirements in accordance with BHT-407-MM-2 18 Table 12-1 on Airframe fuel filter. Replaced fuel filter kit with new item p/n; 1743645-03. Operational and leak checks performed satisfactorily. I PERFORM 300 HOUR INSPECTION AND LUBRICATION REQUIREMENTS IN ACCORDANCE WITH BHT-407-MM-2 Performed 300 hour inspection and lubrication requirements in accordance with BHT-407-MM-2 Table 12.2 and BHT A5B407-04.63 Revision B Parts IV and V Dated 19 September 5th, 2006 (Tail rotor driveshaft bearing 407-340-339-101/-103, Replacement of) on Tail rotor driveshaft and oil cooler blower hangar bearings. acre is Ananr fnr cee ernrine_inm7 ore EMI I PERFORM 25 HOUR, 50 HOUR/3 MONTH, 150 HOUR, 300 HOUR AND 300 HOUR/3 MONTH LUBRICATION REQUIREMENTS Performed 25 hour, 50 hour / 3 month, 150 hour, 300 hour, and 300 hour / 3 month lubrication requirements in accordance with BHT-407-MM-2 Table 12-2 on Litter 20 door seal, Swashplate bearings, Pitch change link bearings, Tail rotor driveshaft splines, Hydraulic pump drive, and Tail rotor pitch change mechanism. Special inspection required between 10 - 25 flight hours on Tail rotor driveshaft disc pack !PERFORM 300 HOUR/12 MONTH SERVICING REQUIREMENTS IN ACCORDANCE WITH BHT-407-MM-2, TABLE 12-3 Performed 300 hour/ 12 month servicing requirements as detailed. Serviced transmission and tail rotor gearbox oil systems with oil; Royco 555. Serviced 21 hydraulic oil system with oil; MIL-H-5606. Replaced transmission filter with new item p/n; 204.040.760.109. Replaced hydraulic filters with new items p/n; 206-076- 340-003. Operational and leak checks performed satisfactorily. 'PERFORM MISCELLANEOUS SERVICING REQUIREMENTS IN ACCORDANCE WITH BHT-407-MM-2 Performed miscellaneous servicing requirements in accordance with BHT-407-MM-2 22 Paragraphs 12-45, 12-47, 12-54, and 12-55 on Battery, Fire extinguisher, Windshield and windows, and Oil cooler blower impeller. Operational check performed !PERFORM 50 HOUR, 100 HOUR AND ANNUAL INSPECTION ON AIR CONDITIONING SYSTEM Performed 50 hour, 100 hour, and Annual Inspections in accordance with Air 23 Comm. Instructions for Continued Airworthiness Report 407EC-200M-2 on Air 'PERFORM ANNUAL INSPECTION IN ACCORDANCE WITH AIR COMM INSTRUCTIONS FOR CONTINUED AIRWORTHINESS Performed Annual inspections in accordance with Air Comm. Instructions for 24 Continued Airworthiness Reports 407H-200M-2 and 407H-500M-1 on Cabin heater system and Engine compartment bleed air system. Operational checks performed  EFTA01120078 'PERFORM 300 HOUR / ANNNUAL INSPECTION ON FLITESTEP / FLOATSTEP KIT Performed 300 hour / Annual inspection in accordance with Aeronautical 25 Accessories, Inc. Instructions for Continued Airworthiness Report AA-01162 on Flitestep / Floatstep kit 'PERFORM ANNUAL INSPECTION ON HIGH VISIBILITY CREW DOOR KIT Performed Annual inspection in accordance with Aeronautical Accessories, Inc. 26 instructions for Continued Airworthiness Report AA-01072 on High visibility crew rtnnr Int 'PERFORM ANNUAL INSPECTION PRE-FLIGHT STEP / HANDLE Performed Annual inspection in accordance with Aeronautical Accessories, Inc. 27 Instructions for Continued Airworthiness Report AA-00123 on Pre-flight step / handle 'PERFORM ANNUAL INSPECTION ON FLODING MAINTENANCE STEP Performed Annual inspection in accordance with Aeronautical Accessories, Inc. 28 Instructions for Continued Airworthiness Report AA-0126 on Folding maintenance IPERFORMM 300 HOUR / ANNNUAL INSPECTION ON CROSSTUBES Performed 300 hour / Annual inspection in accordance with Aeronautical 29 Accessories, Inc. instructions for Continued Airworthiness Report AA-00061 on IPERF kiM4OUR / 6 MONTH INSPECTION ON SKID TUBES Performed 100 hour / 6 month inspection in accordance with Aeronautical 30 Accessories, Inc. Instructions for Continued Airworthiness Report AA-01141 on Skid tubes 'PERFORM ANNUAL INSPECTION ON TAIL ROTOR PEDAL LOCKOUT KIT Performed Annual inspection in accordance with Aeronautical Accessories, Inc. 31 instructions for Continued Airworthiness Report AA-99032 on Tail rotor pedal Inrkniit kit 'PERFORM ROUTINE INSPECTION IN ACCORDANCE WITH BRISTOL AEROSPACE LIMITED INSTRUCTIONS 32 Instructions Performed routine inspection in accordance with Bristol Aerospace Limited for Continued Airworthiness Report ER 95008 'PERFORM 150 HOUR AND 300 HOUR / 12 MONTH ENGINE INSPECTIONS 7830 [ o oRromllesdRo1y5Oceh2o5uor and 00hro autiro/n12month engine inspections in accordance 33 With c4 pe and Maintenance Manual Section 72-00-00 Table 606. Operational and leak checks performed satisfactorily. IPERF RM 600 H0UR/12 MONTH SERVICING REQUIREMENTS Performed 600 hour / 12 month servicing requirements on Engine oil and CEFA filter systems. Serviced engine oil system with oil; Mobil 254. Replaced CEFA oil 34 filter with new item p/n; 23066697. Servicing, filter replacement, operational checks, and leak checks performed under Item No. 33  EFTA01120079 'COMPLY WITH FAA AD2011-15-51 EFFECTIVE NOVEMBER 14TH, 2011 Complied with FAA AD2011.15-51 Effective November 14th, 2011 (Hydraulic servo assemblies) and BHT ASB407-11-96 Revision B Dated August 29th, 2011 (Clevis 35 Assembly - hydraulic servo assemblies, Part number 206.076.062-105 and 206-076- 062-107) in accordance with AD and ASB Instructions. COMPLY WITH BHT ASB407-11-94 DATED FEBRUARY 8TH, 2011 Complied with BHT ASB407-11.94 Dated February 8th, 2011 (Main rotor mast 407-040- 038.101, -105, -109, -111, -111R, -111T, or -11111, Inspection of) in accordance with 36 ASP Instructions. Operational and leak check performed satisfactorily. Next due compliance in 12 months. (EME GENCY FLOATATION SYSTEM RESERVOIRS DUE RETIREMENT Replaced emergency float system reservoirs with new items p/n; 1271762 s/n; 4353 and 4348 DOM; September 2011. Replaced fwd clamp for left hand reservoir with 37 new Item. Serviced reservoirs to; 3025 psi at 30 °C. Leak checks performed satisfactorily. Work performed in accordance with BHT-407-MMS-1 'FORWARD RIGHT HAND FLOAT BAG COVER TORN Replaced Forward Right hand float bag cover with new item p/n; 206-050-247-131 in 38 accordance with BHT-407-MMS-1 'CORROSION NOTED IN AREA OF OIL COOLER DRAIN Performed repair of oil cooler deck drain in accordance with BHT-ALL-SPM and BHT- 39 ALL-SRM. Protective finish re-applied. 'AIRCRAFT MAIN BATTERY FAILS CAPACITY CHECK THREE 13) TIMES. REQUEST REPLACEMENT Replaced aircraft main battery with new item p/n; RG-407 s/n; 40484086 in 40 accordance with BHT-407-MM Chapter 96 and Concorde Installation instructions. Operational check performed satisfactorily. 'STARTER GENERATOR BRUSHES WORN Replaced starter generator brushes with new items p/n; M2002-1 (x4) in accordance 41 with BHT-407-CR&0-V Chapter 96. Operational check performed satisfactorily. 'PITCH SHOCK CORDS EXCESSIVELY STRETCHED Replaced pitch control spring shock cords with new items p/n; 407-001-116-101 (x2) 42 in accordance with BHT-407-MM Chapter 67 (TAIL ROTOR PITCH HORNS CORRODED BEYOND PERMISSIBLE LIMITATIONS Replaced tail rotor pitch horns with new items p/n; 406-012-108-107 (x2) in 43 accordance with BI-IT-407-MM Chapters 64 and 67. MAIN ROTOR BRAKE LININGS AND BOLTS WORN / DAMAGED. TO BE REPLACED Replaced rotor brake linings and guide bolts with new items p/n; D0314-1 (x4) and 44 p/n; D0164-1 (x4) respectively in accordance with BHT-407-CR&O-V Chapter 63. Leak and operational checks performed satisfactorily.  EFTA01120080 'AIR CONDITIONING DRIVE BELT WORN EXCESSIVELY Replaced air conditioning system drive belt with new item p/n; 7270 in accordance 45 with Air Comm Corporation Service Manual 407EC-200M-2. Operational check performed satisfactorily. Belt tension check required after 2 hours of operation. 'CORROSION ON LEFT HAND AUXILIARY FINLET ABOVE POSITION LIGHT J.,Replaced left hand auxiliary fin due to excessive corrosion with new item p/n; 407- 46 023.003.105 s/n; BP258 in accordance with BHT-407-MM Chapter 53. Operational checks performed satisfactorily. 'PAR CLE SEPARATOR CORRODED ON UPPER LEFT HAND SIDE Mechanically removed corrosion to particle separator in accordance with BEIT-ALL- 47 SPM. Protective finish re-applied. 'ENGINE COWLING CORRODED ON UPPER SURFACE Mechanically removed surface corrosion from affected area of engine cowling 48 exhaust cover panel in accordance with BHT-ALL-SPM. Protective finish re-applied. 'UPPER AND LOWER WIRE STRIKE KITS CORRODED Mechanically removed corrosion on upper and lower wire strike blades in 49 accordance with BHT-ALL-SPM. Protective finish re-applied. 'ENGINE ACCESSORY GEARBOX CASING CORRODED AT 12 ° CLOCK POSITION Performed repair to engine accessory gearbox at 12 o'clock position in accordance 50 with Rolls-Royce 250-C47 Series Overhaul Manual Section 72-60-00 'LEFT HAND BOOST PUMP SWITCH INOPERATIVE Replaced left hand fuel boot pump switch with new item p/n; 407-362-013-103 in 51 accordance with BHT-407-MM Chapters 28 and 96. Operational and leak checks performed satisfactorily. 'COMPLY WITH BHT-ASB407-07-79 REV A DATED JUNE 7TH, 2011 Complied with BHT ASB407.07.79 Rev A Dated June 7th, 2011 (Freewheel aft seal 209- 340-265-103, Installation procedures improvement of and oil dam ring 406-040-547- 52 103, one time verification) in accordance with ASB Instructions. Operational and leak checks performed satisfactorily. "OPERATOR REQUESTS REPLACEMENT OF NUTPLATES (X2) ON PARTICLE SEPARATOR COWLING FOR EJECTOR COVER PLATES Replaced nutpiates for particle separator exhaust cover plates with new items p/n; 53 SL211-3.1 (x2) in accordance with BHT-407-MM Chapter 71. 'PERFORM 1-5 FLIGHT HOUR SPECIAL INSPECTION ON M/R HUB MAST NUT AND M/R HUB LOWER CONE Performed 1 - 5 flight hour special inspection in accordance with BI-IT-407-MM 54 Table 5-3 on Main rotor hub mast nut and Main rotor hub lower cone. No movement noted.  EFTA01120081 'PERFORM 2 HOUR OF OPERATION TENSION CHECK ON AIR CONDITIONING SYSTEM DRIVE BELT Performed 2 hours of operation tension check in accordance with Air Comm 55 Corporation Service Manual 407EC-200M-2 on Air conditioning system drive belt. Total Parts and Outside Services $46,928.95 I Consumables S250.00 Freight Charges 5905.00 Discount -$2,227.40 Sub-Total S45,856.55 0 S32,454.55 TOTAL $78,311.1O