Appendix T - P-3 A S Template 25 October 2009.xls

XLS spreadsheet 823 KB Posted Aug 25, 2010

Attached to: Sustainment, Modification, and Installation Program in support of P-3 Aircraft (all T/M/S)
Solicitation number: N00019-09-R-0216
Issued by: Department of the Navy Naval Air Systems Command Naval Air Warfare Center

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Appendix T P-3 A S Template dtd 25Oct09

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09R0216-Amend0011-3of9.PDF	PDF	Apr 6, 2011
09R0216-Amend0011-4of9.PDF	PDF	Apr 6, 2011
09R0216-Amend0011-8of9.PDF	PDF	Apr 6, 2011
09R0216-Amend0011-6of9.PDF	PDF	Apr 6, 2011
09R0216-Amend0011-9of9.PDF	PDF	Apr 6, 2011
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09R0216-Amend0011-7of9.PDF	PDF	Apr 6, 2011
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N00019-09-R-0216-0010.PDF	PDF	Mar 3, 2011
N0001909R0216 Amend 0009.PDF	PDF	Dec 15, 2010
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Appendix B - SSI-K	—	Sep 16, 2010
Appendix D - SSI-K	—	Sep 16, 2010
Attch_(1)_SOW_for_P-3_Aircraft_Sustainment_dtd_09_Sept_2010.doc	DOC document	Sep 16, 2010
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Appendix U -ALD-9 Reqs 25 October 2009.xls	XLS spreadsheet	Aug 25, 2010
Appendix B - SSI-K Drawings 09 June 2010.xls	XLS spreadsheet	Aug 25, 2010
Appendix A - Acronyms 25 October 2009.doc	DOC document	Aug 25, 2010
Appendix V - P-3 IDP 25 October 2009.pdf	PDF	Aug 25, 2010
Appendix G - SSI-K Zone 5 BOM 09 June 2010.xls	XLS spreadsheet	Aug 25, 2010
Appendix E - SSI-K BOM 09 June 2010.xls	XLS spreadsheet	Aug 25, 2010
Attch	—	Aug 25, 2010
Appendix C - Zone 5 Drawings 09 June 2010.xls	XLS spreadsheet	Aug 25, 2010
Appendix R - Misc BOM 16 Mar 2010.xls	XLS spreadsheet	Aug 25, 2010
Appendix Q - Misc Drawings 09 June 2010.xls	XLS spreadsheet	Aug 25, 2010
Appendix L - CWA BOM 16 Mar 2010.xls	XLS spreadsheet	Aug 25, 2010
Appendix H - DIMPLE Ch 2 19 July 2010.pdf	PDF	Aug 25, 2010
Appendix D - SSI-K Zone 5 Drawings 09 June 2010.xls	XLS spreadsheet	Aug 25, 2010
Amendment 0005.PDF	PDF	Aug 25, 2010
Appendix F - Zone 5 BOM 09 June 2010.xls	XLS spreadsheet	Aug 25, 2010
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Appendix M - OW Drawings 09 June 2010.xls	XLS spreadsheet	Aug 25, 2010
Appendix J - FCP 25 October 2009.xls	XLS spreadsheet	Aug 25, 2010
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Appendix S - P-3 Shoring Guide 25 October 2009.xls	XLS spreadsheet	Aug 25, 2010
Attch	—	Aug 25, 2010
Attch	—	Mar 23, 2010
N00019-09-R-0216-0004.pdf	PDF	Mar 23, 2010
Q As posted 19 Mar 2010.pdf	PDF	Mar 19, 2010
Changes to SOW Appendicies 19 Mar 10.doc	DOC document	Mar 19, 2010
Exhibit	—	Mar 19, 2010

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Instructions

	P-3 electronic data alignment sheet
This spreadsheet is intended for use with a laser tracker system.
General instructions:
1. Aircraft should be fully assembled with all structural components installed (small internal items, parachutes and CAD devices may be removed).
2. Position aircraft inside hangar, levelled (with a plumb bob) sitting on 4 jacks as shown in 3-2 Section I Figures.
	Close hangar doors if wind speed exceeds 10 knots or if aircraft movement exceedes 0.002" or if the sun shines on or near the aircraft.
3. Allow aircraft to temperature stabilize for approximately 24 hours (depending on temp difference).
4. Adjust propellors to 0 degrees pitch
5. Rope off aircraft and not not allow personnel on aircraft.
6. Establish aircraft coordinates using points 7, 1L, 1R and check squareness using point 8 or 14.
	Aircraft coordinate system reference plane intersects point 7 and is 15.08" below points 1L and 1R.
7. Establish references on the hangar floor to facilliatate moves of the tracker head.
8. Shoot points on the aircraft.
9. Copy data from the tracker software to the appropiate blocks in this spreadsheet.
	Blocks 1-7 on "Fig 1-2 SH 5" sheet.	yellow blocks
	Incidence and Dihedral Data Table on "Fig 1-2 SH 5" sheet.		Cells C39-C52
	Engine/prop data onto "Engine Data" sheet.
10. Do not overwrite numbers (baselines) or zeros (formulas)
11. Results will be auto calculated and will display
12. Submit in accordance with contractural requirements, preferrably using this xls file, not as a pdf.
13. "oops" on the right of the figures stands for "out of published specs".
POC	Dan Marlowe
	P-3 FST-1 FRCSE Jacksonville
	904-542-5901
	daniel.marlowe@navy.mil

&F Page &P of &N daniel.marlowe@navy.mil

Manual Figures

Double Click page to show in full resolution

&F Page &P of &N

FIG 1-2 SH 5

Notes

"oops"

out of published specifications from NA 01-75PAA-3-2

"OK"

within the published specifications

Enter data only into yellow fields. Do not enter data into gray areas

Do not overwrite values or zeros

P3 Aircraft Alignment and Symmetry Checks

SEQ #

BUNO

DATE

WO#

INSTRUMENT #

Name

COMMENTS

AIR TEMP

DURING ENGINES MEASURMENTS

START

°F

ENDING

°F

DURING AIRFRAME MEASURMENTS

START

°F

ENDING

°F

Dimension

Nominal Distance

Measured Distance

Allowable Difference

Dimension

Measured Distance

Allowable Difference

Dimension

Measured Distance

Allowable Difference

A3Lp

818.75

C3Lp

C3Rp

A3Rp

818.75

A3Lp

A3Rp

Difference

+/- 1.00

Difference

90.32+/- 1.00

oops

Difference

90.32 +/- 1.0

oops

Dimension

Nominal Distance

Measured Distance

Allowable Difference

Point

Distance

to C.L.

Allowable Difference

C3Lp

909.07

Nominal

Measured

C3Rp

909.07

6Lp

251.14

Difference

+/- 1.00

6Rp

251.14

Difference

+ 0.50

Dimension

Nominal Distance

Measured Distance

Allowable Difference

Point

Distance

to C.L.

B6Lp

696.53

Measured

allowable (left or right)

B6Rp

696.53

0.15

Difference

+/- 0.5

15p

1.00

Incidence Checks

Dihedral Checks

Incidence and dihedral

(Do not enter data into these fields)

data table

Point

Height above level sight line. A/C 8

Point

Height Measurement

Allowable difference

Point

Height Measurement

Allowable difference

15.08

Difference (1l-2L)

15.08

1.78 +/- 0.10

oops

Difference (3L-1L)

-15.08

49.68 +/- 2.00

oops

15.08

Difference (1R-2R)

15.08

1.78 +/- 0.10

oops

Difference (3R-1R)

-15.08

49.68 +/- 2.00

oops

Difference (4L-3L)

0.34 +/- 0.10

oops

Difference (3R-3L)

+/- 1.00

13L

Difference (4R-3R)

0.34 +/- 0.10

oops

Difference (6L-13L)

34.20 +/- 0.65

oops

12L

12R

13R

13L

Difference (6l-5L)

0.07 +/- 0.10

Difference (6R-13R)

34.20 +/- 0.65

oops

13R

13L

13R

Difference (6R-5R)

0.07 +/- 0.10

Difference (13L-13R)

+/- 0.16

12L

13L

Vertical Stabilizer Perpendicularity Check

Difference (12L-13L)

0.13 +/- 0.12

oops

Dimesion

Measured Distance

12R

10L to 11L

13R

10R to 11R

Difference (12R-13R)

0.13 +/- 0.12

oops

Difference

13L

Allowable Difference

+/- 0.36

15.08

Difference (13L-1L)

-15.08

91.93 +/- 0.50

oops

13R

15.08

Difference (13R-1R)

-15.08

91.93 +/- 0.50

oops

&F Page &P of &N

FIG 1-2 SH 7

	1. Set blade angle at flat pitch at tips and mark propeller blades 1, 2, 3 and 4 (see detail).
	2. Positon propeller as shown with point 1 directly above point 3.
	3. Measure and record in table the difference of horizontal distances X and Y from
	Upper and lower blade tips to transit vertical plane.
	4. Rotate propeller 90 degrees and repeat through all points.
		Power Plant Incidence Check
	NO. 1			NO. 2			NO. 3			NO. 4
Points	(x-y) Horizontal Difference	Angle d	Points	(x-y) Horizontal Difference	Angle d	Points	(x-y) Horizontal Difference	Angle d	Points	(x-y) Horizontal Difference	Angle d
1 vs 3	0	0	1 vs 3	0	0	1 vs 3	0	0	1 vs 3	0	0
2 vs 4	0	0	2 vs 4	0	0	2 vs 4	0	0	2 vs 4	0	0
3 vs 1	0	0	3 vs 1	0	0	3 vs 1	0	0	3 vs 1	0	0
4 vs 2	0	0	4 vs 2	0	0	4 vs 2	0	0	4 vs 2	0	0
Measured Average	0	0	Measured Average	0	0	Measured Average	0	0	Measured Average	0	0
Nominal Average	4.99*	1.77°	Nominal Average	3.67*	1.3°	Nominal Average	3.67*	1.3°	Nominal Average	4.99*	1.77°
Allowable Variation	+ 0.71 - 0.56	+ 0.25° - 0.20°	Allowable Variation	+ 1.00 - 0.56	+ 0.36° - 0.20°	Allowable Variation	+ 1.00 - 0.56	+ 0.36° - 0.20°	Allowable Variation	+ 0.71 - 0.56	+ 0.25° - 0.20°
	oops	oops		oops	oops		oops	oops		oops	oops
	* Includes Static Deflection

&F Page &P of &N

FIG 1-2 SH 8

	1. Set blade angle at flat pitch tips
	2. Position blades 1 and 3 on vertical C.L.
	3. Measure and record distances from each pair of blade tips.
	4. Rotate propeller 90 degrees and repeat through all points.
	5. Propeller diameter tip to tip is 162.00 +/- 0.258
NO. 1			NO. 2			NO. 3			NO. 4
Points	Measured X14	Measured X15	Points	Measured X16	Measured X17	Points	Measured X18	Measured X19	Points	Measured X20	Measured X21
1 vs 3	0	0	1 vs 3	0	0	1 vs 3	0	0	1 vs 3	0	0
2 vs 4	0	0	2 vs 4	0	0	2 vs 4	0	0	2 vs 4	0	0
3 vs 1	0	0	3 vs 1	0	0	3 vs 1	0	0	3 vs 1	0	0
4 vs 2	0	0	4 vs 2	0	0	4 vs 2	0	0	4 vs 2	0	0
Average X14	0		Average X16	0		Average X18	0		Average X20	0
Average X15		0	Average X17		0	Average X19		0	Average X21		0
Difference		0	Difference		0	Difference		0	Difference		0
Allowable Difference		+/- 0.51	Allowable Difference		+/- 0.51	Allowable Difference		+/- 0.51	Allowable Difference		+/- 0.51
		OK			OK			OK			OK

&F Page &P of &N

ENGINE DATA

ENGINE 1	POINT ID	X	Y	Z
E1_1VS3_1
E1_1VS3_2
E1_1VS3_3
E1_1VS3_4
E1_2VS4_1
E1_2VS4_2
E1_2VS4_3
E1_2VS4_4
E1_3VS1_1
E1_3VS1_2
E1_3VS1_3
E1_3VS1_4
E1_4VS2_1
E1_4VS2_2
E1_4VS2_3
E1_4VS2_4
ENGINE 2	POINT ID	X	Y	Z
E2_1VS3_1
E2_1VS3_2
E2_1VS3_3
E2_1VS3_4
E2_2VS4_1
E2_2VS4_2
E2_2VS4_3
E2_2VS4_4
E2_3VS1_1
E2_3VS1_2
E2_3VS1_3
E2_3VS1_4
E2_4VS2_1
E2_4VS2_2
E2_4VS2_3
E2_4VS2_4
ENGINE 3	POINT ID	X	Y	Z
E3_1VS3_1
E3_1VS3_2
E3_1VS3_3
E3_1VS3_4
E3_2VS4_1
E3_2VS4_2
E3_2VS4_3
E3_2VS4_4
E3_3VS1_1
E3_3VS1_2
E3_3VS1_3
E3_3VS1_4
E3_4VS2_1
E3_4VS2_2
E3_4VS2_3
E3_4VS2_4
ENGINE 4	POINT ID	X	Y	Z
E4_1VS3_1
E4_1VS3_2
E4_1VS3_3
E4_1VS3_4
E4_2VS4_1
E4_2VS4_2
E4_2VS4_3
E4_2VS4_4
E4_3VS1_1
E4_3VS1_2
E4_3VS1_3
E4_3VS1_4
E4_4VS2_1
E4_4VS2_2
E4_4VS2_3
E4_4VS2_4

&F Page &P of &N

NOTES

&F Page &P of &N

MBD005A6B1D.pdf

NAVAIR 01-75PAA-3-2

1-7 Change 1

Figure 1-2. Alignment and Symmetry (Sheet 5)

MBD005A711E.pdf

1-9 Figure 1-2. Alignment and Symmetry (Sheet 7)

MBD005A7464.pdf

1-10 Figure 1-2. Alignment and Symmetry (Sheet 8)

MBD005A6DFE.pdf

1-8 Figure 1-2. Alignment and Symmetry (Sheet 6)

MBD005A650C.pdf

1-5 Figure 1-2. Alignment and Symmetry (Sheet 3)

MBD005A67ED.pdf

1-6 Figure 1-2. Alignment and Symmetry (Sheet 4)

MBD005A5E29.pdf

1-3 Figure 1-2. Alignment and Symmetry (Sheet 1)

MBD005A615E.pdf

Change 1 1-4 Figure 1-2. Alignment and Symmetry (Sheet 2)

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