DASH_6_PHASE_WORK_LOAD_ESTIMATES.xlsx

XLSX spreadsheet 30 KB Posted May 7, 2015

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

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DASH 6 PHASE WORK LOAD ESTIMATES

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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.