EFTA01119963.pdf

s Work Order Detail M• QO•••MMv Repair Station: FAA CRS GR4R216M am Rd. - Savannah, Georgia 31407 Department: SC Maintenance Order: SC35I348 Title: HYPERION AIR, INC. Status: Completed Resolution: No Weight and Balance revisions required during this visit. Signed Off 12/4/2013 6:38:19AM By. IGGLEHART, DAVID-312188 Completed: 12/4/2013 6:38:19AM BY: IGGLEHART, DAVID-312188 Squawk: 1.20 Discrepancy: Exterior Paint and Weight & Balance Requirements. skin replacements resulting in Review scope of aircraft exterior paint touch-up/repairs, and paint reapplication, and determine affect on weight and balance. of existing paint on an For surfaces where paint is stripped and reapplied or added on top before and after area greater than 36 square feet the thickness values will be documented and balance revision is not painting . If average thickness values remain the same, weight required. after paint For surfaces painted with an area greater than 36 square feet and before and weight and balance revision will be required. thickness average varies, QC review for possible 6 or other • Thickness will be plotted on an aircraft drawing derived from AMM chapter order and measuremen ts taken on a two square foot suitable sketch, attached to the work grid. • Reference CAMPS 4000, paragraph 3.5.1 for paint restrictions to flight control surfaces and RVSM certified aircraft. "I N • Reference CAMPS 4000, total average thickness shall not exceed 6 mils. • Per CAC Mass Properties Engineering, paint thickness of 5 mils equals .055 pounds per square foot. • If after QC review, weight change is greater than 2 pounds or .05% of MAC, the weight and balance report will require recomputation. Status: Completed Resolution: No Exterior Paint Weight and Balance revisions required during this visit. Signed Of 12/4/2013 6:37:51AM IGGLEHART, DAVID-312188 Completed: 12/4/2013 6:37:51AM By: IGGLEHART, DAVID-312188 Squawk: 1.21 Discrepancy: Aircraft Ready for Return to Service. All required inspections, to include preflight inspections, maintenance tasks, operational & leak checks, related documentation, and cleaning activities complete. Status: Wafting approval (L) Resolution: Aircraft returned to service for the maintenance workscope. ------------------------------ Squawk: 1.22 Discrepancy: Advise customer of preservation requirements per ATA Chapter 10 of the relevant maintenance manuals for Airframe, Engines, and APU; review requirements in relation to scheduled Date Promised and later potential Date Completed; and perform maintenance or preservation actions as directed by the customer and documented as a Work Order Squawk. Status: Completed Resolution: Advised customer Signed Off 12/4/2013 6:38:05AM By IGGLEHART, DAVID-312188 Inspected: 12/4/2013 10:37:36AM By: LINDEMAN, STANLEY H-300563 Completed: 12/4/2013 10:37:36AM Br LINDEMAN, STANLEY H-300563 ,uawk: 1.23 Discrepancy: Pre-Compliance Induction inspection Status: Waiting approval (L) Resolution: Item: 2 ENGINE TAY Mark 611-8 Part II: Tay Mark 6114 Serial H: 16291 GACWorkOrderDetailspt TEST Printed: 12/5/2013 4:12:37AM Page 5 of 15 Rd XIS EFTA01119963  R.,(,)( 1 -501 Rev. 22 Work Order: Fuselage and Wings Measuri ng Guide riallIAMLJULDIMITI welt ec et A A • /SS • • *AM% oa *C8OLEVA- 01 n Mnt, CO`r•h SURFACES lan.88. 1IIPERATILY PER awn NSTRuCTCfraS 18 IR )0 )1 • • • • 27 26 25 24 —7r- 23 22 RH * Note GV1 aircraft shouts. acceptable to measure points 5 & 12 adjace nt to 4 & 13 for CIV-X aircraft. )1399.111 totes APPROX•IATIN V €01.11LLLY Ill'ACED AT u00.0.0 GA3968 09/11 Page 67 of 68 EFTA01119964  1085 Mil Readings Aircraft Is SC. 351348 j Date 12-2-13 Squawk Fusela e used PosiTector 6000 #556353- Cal due 2/2014 Lt at -toe L 1 68 1 1 103 1 1 1 2 94 2 2 79 2 2 2 3 11 1 3 3 11 7 3 3 3 4 109 4 4 196 4 4 4 5 123 5 5 105 5 5 5 6 11 5 6 6 15 6 6 6 7 11.6 7 7 128 7 7 7 8 11.7 8 8 11 7 8 8 8 9 102 9 114 9 9 9 10 14.2 1 10 85 10 10 10 11 12 1 11 14 7 11 11 11 12 15.9 12 15 5 12 12 12 13 14.7 13 12 4 13 13 13 14 17 9 14 13.5 14 14 14 15 10.3 16 14 3 16 15 15 16 16 16 Total 180.6 0 Total 0 0 Total 189.8 0 Total 0 0 Total 0 0 Total 0 0 Lt upper Md Rear Lt lower Mid Near Rt upper id Hear Rt lower Md Hoar Lt rudder Rt rudder Total ISO Total Total 155 a total Total Total Dade i Divide Divide 15 Divide Divide la Total Total Total Total Total Total Add Add Add Add Add Add Divide Divide Divide Divide Divide Divide I Tota! Average I 12 04 Total Average 1 _Total Average 1 12 65 Total Average I Total Average r Total Average EFTA01119965  1085 Mil Readings Aircraft # SC, 351348 I Date 12-2-13 Squawk # Aileron-used Pos Tector 6000 #556353- Cal due 212014 For rudder Positector 200 #559877 Cal due 9/20 4 it .upp.. Mid Rear avower Mid Rear Itt -upper Mid Rear Rt -lower Mid Rear - Lt rudder Mid Rear Rt rudder Mid Rear 1 8 67 1 4.7 46 1 8.4 83 1 4.3 42 1 49 54 1 38 48 2 8.9 83 2 5.1 4 2 9.9 68 2 3.9 56 2 59 5 2 51 54 3 8.7 7.1 3 5.5 27 3 12.5 83 3 4.5 46 3 42 51 3 42 48 4 10 74 4 5.8 4 4 11.8 91 4 3.4 43 4 66 36 4 41 47 5 6.4 5 32 5 91 5 6 5 66 47 5 35 51 6 59 6 28 6 84 6 89 6 49 54 6 52 69 7 10.8 7 35 7 12.5 7 34 7 54 7 5 8 75 8 32 8 12.1 8 36 8 54 8 48 9 67 9 41 10 55 10 59 11 68 11 4 12 18 12 66 Total 35.6 60.1 Total 21.1 28 Total 42.6 74.6 Total 16.1 40.6 Total 33.1 60.8 Total 25.9 62.1 Lt upper Mid Rear Lt lower Mid Rear Rt upper Mid Rear Rt lower Mod Rear Lt rudder Mid Rear Rt rudder Mid Rear Total 35 6 60.1 Total 21 1 28 Total 42 6 74 6 Total 16 1 40 6 Total 33 1 60.8 Total 25 9 62 1 Divide 4 8 Divide 4 8 Divide 4 8 Divide 4 8 Divide 6 12 Divide 6 12 Total 8 9 7 51 Total 5.27 35 Total 10 65 9.5 Total 4 02 5.0/ Total 5 51 5 (.#:. Total 4 31 S 1/ Add 16 41 Add 8 77 Add 19 95_, Add 909 Add 10 57 Add 9 48 Divide 2 Divide / Divide 2 Divide I Divide 2 Divide 2 Total Average 8.2 Total Ave ale ) 4.38 Total Average I 9.97 Total Average 4.54 Total Average 5 28 Total Average 4 74 EFTA01119966  1085 Mil Readings Aircraft a SC 351348 Date 12.2.13 Squaws a Elevators and to sot wi s used Post Tector 6000 4556353- Cal due 22014 Lt .upper Mho Rear u teat Mid Rear Rt upper Mod Rear Rt -low Mid Rear Lt top wing Rt top wing 1 6.8 6.9 1 5.2 5.1 1 7.1 8.1 1 6.5 7.4 1 1 29.9 i' 1 20.2 2 6.5 5.7 2 5.4 6.6 2 7 9 8.1 8.2 2 _I 26.7 2 24.1 3 6.6 5.3 3 6.6 5.6 3 7.7 8.1 3 7.7 81 3 I 27.7 3 14.5 4 6.1 4.3 4 4.9 5.9 4 8.1 8.8 4 7.2 71 4 t 24.8 i 4 24.8 5 6.3 6 5 5.1 5 5 7.8 9.3 5 7.8 8.8 5 I 4.2 5 22 6 6.6 6.7 6 6.6 6 6 6.3 11.7 6 6.4 6.1 6 \ 6 7 7.4 7.7 7 6.4 5.2 7 5.7 7.9 7 6.8 7.2 7 7 \ 8 7.8 6.9 8 7.1 5.1 8 5.9 7.4 8 6 6.6 8 8 9 117 53 9 117 9 6.8 9 9 10 76 55 10 7 10 73 10 10 11 8 56 11 54 11 56 11 11 12 86 ` 56 12 59 12 53 12 12 13 79 54 13 54 13 53 13 13 14 74 59 14 52 14 57 14 14 15 78 59 16 54 16 5 15 16 16 82 57 16 6 16 55 16 16 Total 54.1 116.7 Total 47.3 88.3 Total 56.6 122.3 Total 56.5 106 Total 113.3 0 Total 106.6 0 Lt upper Mod Rear Lt lower Mod Rear Rt upper Mod Rear Rt lower Mod Rear Lt rudder 113 3 Rt rudder 105 6 Total 54.1 115.7 Total 47 3 883 Total 556 122 3 Total 56.5 106 Total Total Divide 8 16 Divide 8 16 Divide 8 16 Divide 8 16 Divide 5 Divide 5 Total 6 76 7 23 Total 5 91 5 51 Total 695 7.64 Total 706 6.62 Total 22 66 Total 21.12 Add 13 99 Add 11.42 Add 14.59 Add 13 68 Add Add Divide 2 Divide 2 Divide 2 Divide 2 Divide Divide 'Total Average 6.99 Total Average 5 71 Total Average I 7.29 Total Average L 6.84 Total Average 122.66 Total Average 21 12 EFTA01119967