Appendix_K_-_Aircraft_Phase_Inspection_Workload_estimates.xlsx

XLSX spreadsheet 389 KB Posted Dec 30, 2015

Attached to: T-38 Aircraft Maintenance Program Solicitation Federal contract opportunity
Solicitation number: FA4890-15-R-0007
Issued by: Department of the Air Force Air Combat Command

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Appendix K - Aircraft Phase Inspection Workload estimates

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Other files attached to T-38 Aircraft Maintenance Program Solicitation, newest first.
File	Type	Posted
RFP_FA4890-15-R-0007_U0004_T-38_AMP.pdf	PDF	Feb 11, 2016
Attach_7_-_Schedule_T38_CLIN_Spreadsheet-_Final--10Feb16_REV_2.xlsx	XLSX spreadsheet	Feb 11, 2016
PWS_App_F_T-38_Performance_Incentive__Award_Fee_(PI-AF)_Plan_1_Feb_16.pdf	PDF	Feb 5, 2016
Attachment_5_-_Section_L_Revision_3-_1_Feb_16.pdf	PDF	Feb 5, 2016
Attach_7_-_Schedule_T38_CLIN_Spreadsheet-_Final--1Feb16.xlsx	XLSX spreadsheet	Feb 5, 2016
Industry_Questions_3_Feb_16.pdf	PDF	Feb 3, 2016
Appendix_C_-_Publications_and_Forms_21_Jan_16.pdf	PDF	Jan 28, 2016
Appendix_K_-_T-38_AMP_Off_Station_Recovery-MRT_Workload_Data_Corrected_8_Jan_16.xlsx	XLSX spreadsheet	Jan 28, 2016
Attach_7_-_Schedule_T38_CLIN_Spreadsheet-_Final.xlsx	XLSX spreadsheet	Jan 28, 2016
T-38_AMP_Industry_Questions_22_Jan_16.pdf	PDF	Jan 22, 2016
Appendix_K_-_T-38_FLEET_NMC_FY14.xlsx	XLSX spreadsheet	Dec 30, 2015
Attachment_1_-_T-38_PWS__Effective__30_Dec_2015.docx	DOCX document	Dec 30, 2015
Appendix_K_-_T38C_Mx_Data.xlsx	XLSX spreadsheet	Dec 30, 2015
Appendix_K_-_Site_Specific_Workload_Data.xlsx	XLSX spreadsheet	Dec 30, 2015
Attachment_5_-_Section_L_-_30_Dec_15.pdf	PDF	Dec 30, 2015
Appendix_K_-_Workload_Data_30_Dec_2015.pdf	PDF	Dec 30, 2015
RFP_FA4890-15-R-0007_T-38_AMP_as_of_16_Dec_15_FINAL.pdf	PDF	Dec 16, 2015
Appendix_L_-_KTR_Min_Workforce_Qual_10Dec2015.pdf	PDF	Dec 16, 2015
Attachment_4_-_T-38_CTP_CBA_2013.pdf	PDF	Dec 16, 2015
Appendix_K_-_Workload_Data.pdf	PDF	Dec 16, 2015
Appendix_E_-_GFF.pdf	PDF	Dec 16, 2015
Appendix_F_-_T-38_PI-AF_Plan_10_Dec_15.pdf	PDF	Dec 16, 2015
Attachment_2_-_DD_FORM_254_T-38_AMP_16_Oct_15.pdf	PDF	Dec 16, 2015
Attachment_5_-_Section_L_-_14_Dec_15.pdf	PDF	Dec 16, 2015
Appendix_C_-_Publications_and_Forms.pdf	PDF	Dec 16, 2015
Appendix_A_-_8_Dec_15.pdf	PDF	Dec 16, 2015
Attachment_6_-_Section_M_-_14_Dec_15.pdf	PDF	Dec 16, 2015
Attachment_1_-_T-38_PWS__Effective__8_Dec_2015.pdf	PDF	Dec 16, 2015
Appendix_D_-_Host_Base_Vehicles.pdf	PDF	Dec 16, 2015
Gov_Furnished_Property.pdf	PDF	Dec 16, 2015
T-38_AMP_Pre-Proposal_Conf_Attendees.pdf	PDF	Dec 14, 2015
T-38_AMP_Pre-Proposal_Conference_Official_Questions.pdf	PDF	Dec 14, 2015
T-38AMP_Pre-Proposal_Brief_9_Dec_2015--updated.pdf	PDF	Dec 14, 2015
Appendix_E_-_GFF.pdf	PDF	Nov 25, 2015
T-38_PI-AF_Plan_29_Apr_15.pdf	PDF	Nov 25, 2015
Attachment_2_-_DD_FORM_254_T-38_AMP_16_Oct_15.pdf	PDF	Nov 25, 2015
Appendix_B_-_CDRLs.pdf	PDF	Nov 25, 2015
Attachment_3_-_Wage_Determinations_T-38.pdf	PDF	Nov 25, 2015
Host_base_Vehicle_Support.pdf	PDF	Nov 25, 2015
RFP_FA4890-15-R-0007_T-38_AMP_as_of_25_Nov_15.pdf	PDF	Nov 25, 2015
KTR_Min_Workforce_Qual.pdf	PDF	Nov 25, 2015
https //www.fbo.gov/index mode form id 5bae3bae259506bde7bc9af9ba770465 tab ntype	—	Nov 25, 2015
Attachment_5_-_Section_L_-_3_Nov_15.pdf	PDF	Nov 25, 2015
Host_base_Vehicles.pdf	PDF	Nov 25, 2015
Appendix_A_-_24_Mar_15.pdf	PDF	Nov 25, 2015
Draft_T-38_AMP_App_G_QMS_Nov_2015.pdf	PDF	Nov 25, 2015
Attachment_1_-_T-38_PWS__Effective__2_Sep_2015.pdf	PDF	Nov 25, 2015
Appendix_C_-_Publications_and_Forms.pdf	PDF	Nov 25, 2015
Attachment_6_-_Section_M_-_3_Nov_15.pdf	PDF	Nov 25, 2015
Gov_Furnished_Property.pdf	PDF	Nov 25, 2015

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PE work load estimates

INSP	ADDITIONAL REQUIREMENTS		TIME REQ	ACTUAL SCHED TIME
225 HPO			7.5 Hrs per 6WC	1 Day
								Total	7.5 MH
450 Hr PE			79.9 Hrs per 6WC	14 Days + 1 NDI day+ 1 Canopy Rig + 1 Wash day+ Post Dock
				8 Hrs	8 Hrs	8 Hrs	4 Hrs	4 Hrs
				X 1 Ind
				X 4 Dir	X 3 Dir	X 2 Dir	X4 Dir	X 3 Dir
				560 MH	24 MH	16 MH	16 MH	12 MH
								Total	628 MH
900 Hr PE			169.5 Hrs per 6WC	17 Days + 6 NDI days+ 1 Canopy Rig + 1 Wash day+ Post Dock
	Canopy Insp/Polish		6 hrs per canopy/12 total	8 Hrs	8 Hrs	8 Hrs	4 Hrs	8 Hrs
	Backshop Generator CK's		3 hrs per generator/6 total	X 1 Ind
	Backshop Stab Actuator Insp/CK		6 hrs per actuator/12 total	X 4 Dir	X 3 Dir	X 2 Dir	X 4 Dir	X 3 Dir
	Backshop Brake Master Cyl CK		4 hrs per cylinder/16 total
	Backshop SAS Actuator Insp/CK		2 hrs	680 MH	144 MH	16 MH	16 MH	24 MH	880 MH
	Backshop Rudder Actuator Insp/CK		6 hrs per actuator/12 total
	Backshop Aileron Actuator Insp/CK		6 hrs per actuator/12 total
				Back Shop					72 MH
				Roto Scan (New)					75 MH
								TOTAL	1027 MH
1800 Hr PE			230.15 Hrs per 6WC	20 Days + 8 NDI days+ 1 Canopy Rig + 1 Wash day+ Post Dock
	Canopy Insp/Polish		6 hrs per canopy/12 total	8 Hrs	8 Hrs	8 Hrs	4 Hrs	8 Hrs
	Backshop Generator CK's		3 hrs per generator/6 total	X 1 Ind
	Backshop Stab Actuator Insp/CK		6 hrs per actuator/12 total	X 4 Dir	X 2 Dir	X 2 Dir	X 4 Dir	X 3 Dir
	Backshop Brake Master Cyl CK		4 hrs per cylinder/16 total
	Backshop SAS Actuator Insp/CK		2 hrs	800 MH	192 MH	16 MH	16 MH	24 MH	1048 MH
	Backshop Rudder Actuator Insp/CK		6 hrs per actuator/12 total
	Backshop Aileron Actuator Insp/CK		6 hrs per actuator/12 total
				Back Shop					72 MH
				Roto Scan (New)					75 MH
								TOTAL	1195 MH
		NOTES:
		Wing drop recurring inspection required every 2700 hours: Add 4 additional phase days / 160 Man hours
		4 T-38C assigned to test group at CAT 3 for inspections - see CAT 3/CAT 5 tab for differences

Dash 6 inspections

T.O.	Required Inspection	Hrs Reqd
-6WC-1/-3	225 Hourly Post Flight Inspection (HPO)	7.5
	450 Hour Periodic (Minor PE)	79.9
	900 Hour Periodic (1st Major)	169.5
	1800 Hour Periodic (2nd Major)	230.15
-6 insp
23	Wing lower skin fastener holes 140-161, 206….. (Ultrasonic)	7.5
24	Wing lower skin fastener holes 116-139, 196-….. (Ultrasonic)	4
25	Wing lower skin fastener holes 1-29, 162-…(Ultrasonic)	4
26	Wing lower skin fastener holes 723-727, 735-….. (Ultrasonic)	4
27	Wing lower skin fastener holes 290-295, 470-….. (Ultrasonic)	4
28	Wing lower skin fastener holes 451-455, 496-….. (Ultrasonic)	4
29	Wing lower skin aft edge, land and radius W.S. 26.6-60 and 60-64.8 (visual and eddy)	2
30	Wing root radius at W.S. 25.1 (eddy current)	16
31	Wing lower wing skin land W.S. 77, 44 and 66% spar (Eddy Current)	4
32	Wing fwd land between WS 72.25 and 76.7 (eddy current	1
33	Wing lower milled pockets at WS 78 between 39 and 44% spar (ultrasonic)	3
34	Wing lower skin screw holes and aileron access doors between 76 an 101 on 44% (eddy current)	2
35	Wing lower skin critical fastener holes 728 to 734 (Ultrasonic Roto-scan)	2
36	Wing spars and ribs (radiograph)	2
37	Wing 66% between 101 and 76 (eddy current)	1
38	Thin skin wing only, Fasteners at 44 and 39% spar (ultrasonic)	0.5
39	Thin skin wing only, Wing root radius WS 25.88 (eddy current)	0.5
40	Thin skin wing only, Wing lower skin WS 26.6 - 64-8 (eddy current)	0.5
41	Wing attach trunnions (ultrasonic and Eddy current)	6
42	Wing attach bushings flanges 15 and 44% (dimensional check)	120
43	Not required (required when bushings are removed)	2
44	Wing attach bolts (mag particle)	3
45	Cockpit longeron FS 146 (prior to TCTO 717) (eddy and penetrant)	0.5
46	Cockpit longeron FS 146 (after TCTO 717) (eddy and penetrant)	0.5
47	Cockpit longeron hook slots (except cat 5) (eddy current)	0.5
48	Cockpit longeron hook slots FS 267 (cat 5 only) (Eddy current)	0.5
49	Cockpit longeron hook slots FS 267 (eddy current)	4
50	Outboard engine mounts (mag particle)	4
51	Inboard engine mounts (Mag particle)	4
52	V-tip antenna (eddy current)	2
53	Vertical stab radius (ultrsonic/borescope)	0.5
54	H-stab torque tube fillet (visual)	4
55	Upper longeron canted FS 264 (eddy Current)	0.5
56	Upper longeron splice FS 284 bolt installed (ultrasonic)	0.5
57	Upper longeron splice FS 284 bolt uninstalled (ultrasonic)	0.5
58	Upper longeron splice bolt	0.5
59	Steel dorsal longeron (eddy current)	7
60	Steel dorsal longeron hi-Loc holes at 400.02 (eddy current)	0.5
61	Steel dorsal longeron rivets FS 351.25, 367, and 380 (fluorescent Pen)	8
62	Steel dorsal longeron rivets FS 405.05 (eddy current)	1
63	Steel dorsal longeron upper edge (eddy current)	6
64	Steel dorsal longeron vertical fastener holes (eddy current)	1
65	Aluminum dorsal longeron nut plates FS 317-393 and 400-424 (eddy current)	0.5
66	Aluminum dorsal longeron holes FS 329 (eddy current)	0.5
67	Aluminum dorsal longeron holes FS 337. 351, 364. 378, 389 (eddy current)	0.5
68	Aluminum dorsal longeron nutplate holes (eddy current)	0.5
	hours required for -6 and -6WC inspections

CAT 3

CAT 5

Sheet3 image1.emf image2.emf

File details come from the government source that posted it. Updated Nov 14, 2017.