EFTA01735291.pdf

z ananv Work Order Detail Repair Station: FAA CRS GR4R216M am Rd. - Savannah, Georgia 31407 Department: SC Maintenance ri Order: SC351348 Title: HYPERION AIR, INC. shun. Completed Resolution- No Weight and Balance revisions required during this visit. Signe& O1T 1,214I2013 6:38:19AM By: IGGLEHART, DAVID-312188 Completed: t2/4/2013'' 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. existing paint on an For surfaces where paint is stripped and reapplied or added on top of before and after area greater than 36 square feet the thickness values will be documented balance revision is not painting. If average thickness values remain the same, weight and 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 work order and measuremen ts taken on a two square foot suitable sketch, attached to the grid. * Reference CAMPS 4000, paragraph 3.5.1 for paint restrictions to flight control surfaces and RVSM certified aircraft. • Reit e G • Per GAC Mass Pro Mies En ineerin aint thickness 55 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 CO 12/4/2013 6:37:51AM By: IGGLEHART, DAVID-312188 Completed: 12/4/2013 6:37:5IAM 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: Waiting 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 By: LINDEMAN, STANLEY 11-300563 . . . ..................... ........................ ............ .................. ,uawk: 1.23 Discrepancy: Pre-Compliance Induction inspection Status: Waiting approval (la Resolution: Item: 2 ENGINE TAY Mark 611-8 Part H: Tay Mark 611-8 Serial 1: 16291 0AC_Work0rdatetail.rpt TEST Printed: 12/5/2013 4:12:37AM Page 5 of 15 Ida EFTA R1 00017375 EFTA01735291  RSOCT -501 Rev. 22 A/C SIN: Work Order: I. Fuselage and Wings Mea suring Guide LiaaajC • II C • A`C in.CA At 'CCM M1 4 S • • • • • ... • • • IS 1 • =AO • EniW" -* •• Lp•. Cyr.:. 5.•••• :E: VIAS.0 i2St•toCi• • =" GAUPS .N.S. R.-C - D..S 13 19 /0 at • • • • • • • • •. • P. s S 30 • 28 27 11 26 24 23 25 * Note C VI aircraft shown. acceptable to measure points 5 & 12 adjacent to 4 & 13 fur GINCX aircraft. POWs APPROltiOrivt ECUALLYSPACtor YO.00RO GA3968 09/II Page 67 of 68 EFTA_R1_00017T76 EFTA01735292  1085 Mil Readings Aircraft # SC 351348 Date 12-2-13 Squawk # Fuselage used PosiTector 6000 #556353- Cal due 212014 .n-tt et 11 I—i 1 94 1 1 179 1 2 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 7 116 7 7 128 7 7 7 8 117 8 8 117 8 8 8 9 102 9 114 9 9 9 10 142 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 14 179 14 135 14 14 14 15 10 3 15 14 3 15 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 Mid ear Lt lower Mid Rear Rt upper Mid Hear Rt lower Mid Hear Lt rudder Rt rudder Total 180 6 Total Total 189 Total Total Total Divide Divide Divide 13 Divide Divide avide Total Total Total Total Total Total Add Add Add Add Add Add Divide Divide Div.de _ Divide Divide Divide otal Average j 12 04 Total Average I atotal Average 12.65 Total Average J Total Average Total Average EFTA_R1_00017377 EFTA01735293  1085 MD Readings Aircraft # SC 351348 Date 12.2.13 1 .1 S%iaviiii # Aileron-used PosiTector 6000 #556353- Ca due 2/2014 For rudder Positector 200 #55987 7 Cal die 9/20 4 li*VOIS Mid Rear Lt -lower Mid Rear Rt -uppef Mid Rear at Gower Mid Rear Lt rudder Mid. Retit - 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 5 4 _ 3 8.7 71 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 4 36 4 41 47 ,..- 3.4 43 66 5 64 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 7 108 7 35 7 125 7 34 7 54 7 5 8 75 8 32 8 121 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 Mid 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 93 Total 4 02 5 Or Total 5 51 5-06 Total 4 31 S 17 Add 16 41 Add 8 77 Add 19 95 Add 909 Add 10 57 Add 9 48 Divide 2 Divide 2 Divide 2 Divide A Divide 2 Divide I Total Average 8.2 Total Average 1 4.38 Total Average J 9.97 Total Average 4.54 Total Average 5 28 Total Average 4;74 EFTA_R1_00017378 EFTA01735294  1085 Mil Readings Aircraft 0 SC 351348 Date 12-2-13 Squaw', 0 Elevators and tops of ',viols used PosiTector 6000 a556353 Cal due 1 2014 Ita ceps, Mid Rear - anew - Mid iRear Ititrgow Mid ' FR 4bioc:. Mid/ Rear LA top win Rt top win 1 6.8 5.9 1 6.2 5.1 1 7.1 8.1 1 6.5 7.4 1 1 29.9 1 1 20.2 2 6.6 5.7 2 5.4 6.5 2 7 9 2 8.1 8.2 2 26.7 I 2 24.1 3 6.6 5.3 3 6.6 5.6 3 7.7 8.1 3 7.7 8.1 3 t 27.7 l' 3 14.5 4 6.1 4.3 4 4.9 5.9 4 8.1 8.8 4 7.2 7.1 4 24.8 4 24.8 5 6.3 6 5 6.1 5 5 7.8 9.3 5 7.8 8.8 5 4.2 5 i 22 / 6 6.6 6.7 6 6.6 5 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 11 7 53 9 11 7, 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 15 54 15 5 15 15 16 82 57 16 6 16 55 16 16 Total 54.1 115.7 Total 47.3 88.3 Total 55.6 122.3 Total 56.5 106 Total 113.3 0 Total 105.6 0 Lt upper Mid Rear Lt lower Mid Rear Rt upper Mid Rear Rt lower Mid Rear Lt rudder 113 3 Rt rudder 105.6 Total 54 1 115 7 Total 47 3 88 3 Total 55 6 122 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 6 95 764 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 Iriatangeopfint4 Total'Avriigsai ,2246 Total Average •• 21:1i EFTA_R1_00017379 EFTA01735295