DASH_6_PHASE_WORK_LOAD_ESTIMATES.xlsx

XLSX spreadsheet 30 KB Posted May 7, 2015

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

About this file

From the source

DASH 6 PHASE WORK LOAD ESTIMATES

View the file

Other files for this federal contract opportunity

Other files attached to T-38 Aircraft Maintenance Program (AMP), newest first.
File	Type	Posted
T-38_AMP_Pre-Proposal_Conf_letter_(2)-signed.pdf	PDF	Nov 13, 2015
T-38_AMP_Required_Security_Clearances.xlsx	XLSX spreadsheet	Jun 22, 2015
Industry_Day_Attendees_7_May_15.pdf	PDF	Jun 16, 2015
T-38AMP_Site_Pictures_-_5_May_15.pdf	PDF	May 8, 2015
Appendix_K_-_Aircraft_Inspection_Info.xlsx	XLSX spreadsheet	May 7, 2015
ACC_T-38_FLEET_NMC_FY14.xlsx	XLSX spreadsheet	May 7, 2015
Appendix_K_-_Combined_T-38A_AT-38B_Summary_Mx_Data.xlsx	XLSX spreadsheet	May 7, 2015
AETC_FY14_T-38C_Stats.xlsx	XLSX spreadsheet	May 7, 2015
Rm_100_(Storage).jpg	JPG image	May 1, 2015
Bldg_52_(Hangar_Exterior_2).jpg	JPG image	May 1, 2015
Rm_103_(CTK_1).jpg	JPG image	May 1, 2015
Rm_121_(Break_Room).jpg	JPG image	May 1, 2015
Hangar_3_Interior.JPG	JPG image	May 1, 2015
Building_205_Support_Area_Walk-in.JPG	JPG image	May 1, 2015
Building_205_Support_Area_Overflow_bulk.JPG	JPG image	May 1, 2015
Building_205_Support_Area_Tool_checkout.JPG	JPG image	May 1, 2015
QC_and_Team_Leads_Office_-_Room_135.jpg	JPG image	May 1, 2015
Langley_Bldg_753_-_Hangar_200_Unused_Space_(Second_Floor).pdf	PDF	May 1, 2015
Hangar_Bay_Rear.jpg	JPG image	May 1, 2015
Langley_Bldg_753_-_Hangar_200_First_Floor_Plan.pdf	PDF	May 1, 2015
Bldg_300_compressor_room.jpg	JPG image	May 1, 2015
Bldg_580_Storage.jpg	JPG image	May 1, 2015
Bldg_300_int_reverse_view.jpg	JPG image	May 1, 2015
Holloman_Building_Pictures.pptx	PPTX presentation	May 1, 2015
Bldg_300_gearbox_room.jpg	JPG image	May 1, 2015
Bldg_578_int.jpg	JPG image	May 1, 2015
Bldg_315_Fuel_Shop.jpg	JPG image	May 1, 2015
Bldg_280_NDI_office.jpg	JPG image	May 1, 2015
Bldg_280_NDI_Tool_and_Equip_rm.jpg	JPG image	May 1, 2015
Bldg_282_Corrosion_-_Wheel_-_Tire_Back.jpg	JPG image	May 1, 2015
Bldg_282_front.jpg	JPG image	May 1, 2015
Bldg_282_Corrision_int.jpg	JPG image	May 1, 2015
Bldg_218_SM_int.jpg	JPG image	May 1, 2015
Bldg_282_int.jpg	JPG image	May 1, 2015
Bldg_280_Machine.jpg	JPG image	May 1, 2015
638_-_639_Test_Cell.jpg	JPG image	May 1, 2015
Beale_Bldg_1243_(Dock_7).JPG	JPG image	May 1, 2015
Flight_Shack_(Support_Section).JPG	JPG image	May 1, 2015
AFI_21-101_CAF_Sup_1__Compliance_Matrix.xlsx	XLSX spreadsheet	May 1, 2015
AFI_10-220_IP.pdf	PDF	May 1, 2015
1T-38C-6-WA-1.pdf	PDF	May 1, 2015
Host_Base_Pubs_14_Apr_15.xlsx	XLSX spreadsheet	May 1, 2015
CDRL_A002_Finance_Management_and_Contract_Cost_Report.pdf	PDF	May 1, 2015
CDRL_A006_Environmental_Protection_Plan.pdf	PDF	May 1, 2015
CDRL_A008_Incident_Report.pdf	PDF	May 1, 2015
CDRL_A007_ESOH_Program.pdf	PDF	May 1, 2015
FA4890-15-R-0007_DRAFT_L_ _M.pdf	PDF	May 1, 2015
Attachment_2_-_Industry_Day_Announcement.docx	DOCX document	Apr 21, 2015
Attachment_4_-_Market_Research_Questionnaire.docx	DOCX document	Apr 21, 2015
Attachment_1_-_Draft_Performance_Work_Statement.docx	DOCX document	Apr 21, 2015

Show all 50

T-38 Aircraft Maintenance Program (AMP) has more files on GovTribe.

On GovTribe

Work with this file on GovTribe

Download the original file
Contacts named in this file
Similar government files
Ask GovTribe AI about this file

Try for free Login

Text version

The file's text, extracted by GovTribe without its formatting.

PE WORKLOAD

		PRIOR TO ASIP
		Dash 6 WC	ASIP	NEW DASH 6
Phase	Fequency	MAN HOURS	MAN HOURS	MAN HOURS
Minor	450	320.9	27	347.9
1st Major	900	410.5	77	487.5
2nd Major	1800	471.15	350	821.15
					TCTO	FIX HOURS	FIX PERCENTAGE AVG
			TOTAL	1656.55	246.1	137.35	8.2913283632

Dash 6 inspections

T.O.	Required Inspection	Hrs Reqd	62-3615	62-3691	62-3702	62-3706	62-3722	63-8131	63-8133	63-8154	63-8163	63-8218	63-8229	64-13176	66-8404	67-14828	67-14923
-6WC-1/-3	225 Hourly Post Flight Inspection (HPO)	"7.5"
	450 Hour Periodic (Minor PE)	"79.9"																7/10/09
	900 Hour Periodic (1st Major)	"169.5"																2/15/08
	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														N/A
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														N/A
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														N/A
66	Aluminum dorsal longeron holes FS 329 (eddy current)	0.5														N/A
67	Aluminum dorsal longeron holes FS 337. 351, 364. 378, 389 (eddy current)	0.5														N/A
68	Aluminum dorsal longeron nutplate holes (eddy current)	0.5														N/A
	hours required for -6 and -6WC inspections		471.15	471.15	471.15	471.15	471.15	471.15	471.15	471.15	471.15	471.15	471.15	471.15	471.15	464.65	471.15

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