APPENDIX A

SECTION A1 (WRECKAGE RECOVERY ANDWRECKAGE DISTRIBUTION)

Al

-m

4 .:

I

H x 8

I I

I I

I 1

0’0 ot

u- I

-

:..:: :........ i:“: . . . . ..I.....

:.......... :.. :....: ..;::; ‘.....

,.;:,. I . . ...‘.. ;::; . . . . . . . . ;:.: . ..-.. . : ..: :I:

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w-

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.: -, .:. .I

2 .: .I

0 .:. ..: ;

m

.- .:.: ;

Q

.I LL-I

;; (-y

r- ,: a

.:. 0 m 0 N

:: : . . .‘-

.:

. .

.1 ..: .: .. ,

: . . . :,r..

;:.. :..

.,.. .;:

,. :..

.,.. -;:

,’ :.’

‘,. ,‘I

. . ::

. ..‘ .

.

:. 0

.: .:

z .: .: .: . .

z .: : ‘. . . .:

.: .:

l-02 8E

ZL-

;- . . : _:

. .

co \ 2

-x z

0

? -I 5

0

. ---.

-.

-

0‘0 9E

ZL-

0’05 SC a-

0’0 LC

ZL-

l

cm703 A490 8/19/96-11 403824.48 -7238 27.12 spanwise beam #2 RH web door RBL 8-30

FBMIOA A2039 A662 403840.20 -72 38 42.30 floor beam lower chord; FS 880; RBL 35-86

FBMlOB A741 8l24&6-8 403832.40 -72 38 53.00 floor beam lower chord FS 880 LBL 5-25

FBMllC Al67 8/06l96-1 403842.21 -72 38 50.28 seat track RBL 33-99 FS 800-840; 1 bra I

FBM28 A611 wW96-4 403833.90 -7239 09.90 seat track RBL 33.99; STA 950 to 995 WI seat leg attached

FBMJE A676 w19l96-11 403831.60 -723847.50 floor beam upper chord FS 940, RBL 12-33 I

FBM4A A2044 ------y---- A532 0 38 08.67 -72 38 05.68 fioor

FBM6B A229 40 3832.71 -72 38 29.30 floor beam lower chord (3’ long); FS 920; LBL 28-71

FBMGC A054 floor beam 8 frame FS 920 RBL 100 to SOB, S 25-27.5

FBM8A A261 8mw96-14 403831.73 rt is part of LF36 & FBM- i

LFIZB A181 .-

8106196-I 403848.07 -72 38 35.95 FS 820-900; stringers 14L-25L ,

LFl2C Al36 ---.- -_-__

8/05/96-2 403840.86 -72 38 45.07 L2 door 65804425-411; escape door hatch “65Bl5630” 403# on the Inner door by latch

LF22-25 A2063 wo3b6-85 --

FS 700-720 stringer 38L-39L; changed to white, mixed FBI lot #

- Al.4

) 1, i ‘..’ ..-

GRP # Log # Tag % FBI # Source Tag # Latitude Longitude Deecfiption (Actual)

LF22-29 A2064 wo3196-85 FS 760-780 stringer 45L-46L; changed to white due to mixed FBI lot #

I I I LF22-9

I A2061

I I I FS 540-560 stringer 39L-43L; changed to white due to mixed FBI lot #

I

LF37A A614 I

Wt2B6-4 03828;29. -

I

- ------_

t-

-._.- -72 38 49.71 forward lower cargo bay structure FS 800 left hand side

-.-.- _-.-------

I I I LF37B

I Al82

I WO6/96-1

I I 0 38 31.07 -72 38 56.26 forward lower cargo bay structure, FS 800 Riiht hand side

I LF43 A453

I W17i96-4 40 38 26.08 -72 38 48.49 forward lower cargo bay structure FS 920 left hand side

LF50 AI31 wo5l96-2 40 38 31.09 -72 38 58.69 forward lower cargo bay structure FS 860-880 left hand floor cargo

LF55A , A744 8/24/96-8 40 38 29.20 -72 38 54.30 forward lower cargo bay structure FS 1000 left hand CW outer skin (canted

LF55B

press bulkhead w/some body skin)

A449 W22/96-7 40 38 27.7I -72 38 48.87 forward lower cargo bay structure FS 1000 left hand side

I

1 I

1 LF57 I A709 I I I

0 39 44.95 I-72 36 31.34 FS 920 frame; stringer 33L-35L; (rib assy #65001736401)

LF58A A734

LF58B A2047

8/24@6-8

WI 71964

40 38 25.50 -72 38 55.40 Forward lower bay cargo structure FS 960 lefi hand side

A462 40 38 17.80 -72 38 32.84 FS 960 lower body frame stringer 43L47L

LFGA Al41 8105/96-2 40 38 34.48 -72 39 00.37 FS 800-1000; stringer 40L40R with forward lower cargo bay structure w/rollers attached

LF74 x2201 Ql23l96-5 40 38 05.24 -72 38 37.29 large section of metal (8’ x 6’) changed from 23453 to X2201 to match actual

LF94

debris field (Kurt and Deb)

x4005 11/20~31 fuselage skin segment FS 880-900 stringer 34L-36L

RF118 x4001 11114/96-211 T7005 fuselage skin, FS 880, sblnger 5R - 6R

RFIZIA x4006 11/20/96-161 FS 1000 RHS underwing bulkhead

RF1 22D X4028 1 l/23/96-128 77852 FS 840 frame segment stringer 1 L-8R

RF1 22G x4029 1 l/20196-68 77665 FS 860 frame sement tension tie

RF1221 l x4030 I l/29/96-238 l7858 FS 880 frame segment stringer 4R-6R

RF1 22J x4031 1113l9742 FS 880 frame stringer segment ,

RFl22L X4023 1 l/16/96-158 T7603 --_

frame FS 900, stringer .5L-5R

I; I I I I I --.- l-J------ Al.5

GRP # Log#’ Tag # FBI # Source Tag # Latitude Longitude Description (Actual)

RFl22M X4032 1 lLw96-4 l7144 FS 900 frame segment stringer 5R-12R

RF1220 x3005 I O/02/96-1 403822.77 -72 39 06.67 FS 920 frame segment string 2R-5R; approx 1’ long curved piece of fiberglass

RF122P x4050 11 l20/96-% T7106 --..--- . .-.. . ..-_--._

FS 920 frame iegment stringer 2R-5R _-I_-___~_

RF1 22Q A2003 8/19/96-23 A525 40 38 26.42 -72 38 39.48 FS 920 frame segment stringer 17R-20R

RF122R x4033 1 l/20/96-8 l-7696 FS 940 frame segment stringer 13R-18R

RF1 22T x4034 1 l/20/96-123 77087 FS 960 frame segment stringer 11 R-16R

RFl22V A713 8/24/96-0 403822.81 -72 38 24.99 FS 960 frame segment stringer 9R-11 R; interior metal sheet with rivets 8 strut 65801741

RF1 23A x4035 11/23/96-l 31 l-7843 FS 860.948stringer

RF1238 X4036 1 l/20/96-186 T7133 FS 840-970 stringer segment 3AR

RF123C x4037 11/20&6-67 T7685 ______-

FS 868-875 stringer segment 3R

RFl23D X4038 1 l/20/96-173 l-7117 FS 840-868 stringer segment 3R

RFl23E A424 8/i 4196-i 1 403822.55 -_.

-72 38 34.25 FS 883-948 stringer segment 2AR

RF1 23F x4039 1 l/14/96-150 T7507 FS 900-948 stringer segment 1 R

RF1 23H x4041 11/23/96-l 59 l-7835 FS 925-938 stringer segment 2L

RF1231 x4040 12107/96-28 T7283 FS 820-836 stringer segment 2L

RFl23L X4042 1 i/29/96-260 l-7190 FS 635-905 stringer segment 3AL

RFl23M x4043 lll23/9&175 -I7841 FS 905-938 stringer segment 3AL

RF124A A2004 WlW96-23 A520 40 38 20.94 -72 38 28.49 FS 760-810 stringer segment 37A i

RF1 248 s A2056 81171964 A649 4 ~ ~~--.-

0 38 54.80 -72 38 53.30 FS 81 O-830 stringer segment 37R -

RF1 24C X3002 9/28/96-t 40 38 24.57 -72 38 43.94 FS 890-990 stringer segment 40R

RFl24D A485 W16/96-10 40 38 26.85 -72 38 53.82 FS 900-980 stringer segment 41 R

_-- --..-- ---_ Al.6

) j I ) .._ LJ

Tag # FBI # Some Tag # Latitude Longitude DescfiMion (Actual) GRP # Log #

-I- -- LW16

,

t-- LF88A

I

C2170 1 1 C240 FO 39 50.14 --

#2-LH web door perimeter --------I

+z2+.-+.-~.~ -. liFi z7yiz.. +7 -...-...--.. I.-.--- .-- . --_-._.- .- - -.- ._._.._^ ._._..__ --{ leff wing flap track support LWBL 353 5-7

C2168

Cl667 8i29196-4

Cl85 40 39 49.80 -72 37 28.10 lower CW skin;‘RBL 98127.5; R.S. to STR 1

---- - . -.... -.-.-_. . 40 39 47.80 -72 37 29.60 .--- __ .-..--. --. . ..-.... . - -.- g2220-2330 _ ----.- (lower L5 door) string&j513T”v’ .--.-- -‘- -----.-

22537

Cl682

9/I 11964

8Q9l96-4

23081 40 39 43.25 -72 37 23.45 FS 1350; stringer 23L-30L; fuselage skin w/ red paint

40 39 47.80 -72 37 29.60 FS 2360-2506; stringer 8L-2OL; piece of outer skin of aircraft

1 I I 22851 I I

23518 0 39 49.00 -72 37 29.00 FS 1480-1490 stringer 43L-44L

C2414 c434 40 39 42.93 -72 36 24.91 FS 1560-1580 stringer 45L46L

C2420

22856 9/21/96-l

Cl301 40 39 48.70 -72 37 28.20 FS 1500-l 520 stringer 40L

23417 40 39 41.24 -72 36 36.62 FS 1670-l 680 stringer 49L-5OL

22721

22850

9102/96-l 1 .Z3276 40 39 45.03 -72 37 27.01 FS 910-940; stringer 13L-14L

23417 40 39 41.24 -72 36 36.62 FS 1430-1460 stringer 22L-26L

22857

22855

9/04/96-l 23417 40 39 41.24 -72 36 36.62 FS 1438 stringer 27L-29L

23389 40 39 50.60 -72 37 26.20 FS 1380-l 410 stringer 31 L-33L

c2441 Wl l/96-2 c300 40 39 42.00 -72 37 22.00 FS 1241 stringer 23L-28L

22858 9/21/96-l 23417 40 39 41.24 -72 36 36.62 FS 1241 stringer 23L-28L

I I 22550

I 911 l/964

I I 23072 0 39 43.20 -72 37 23.30 fuselage skin wl red paint

z2759 g/25/96-2 z3517 40 39 49.10 -72 37;29.10 FS 940-960; stringer 38L4OL; fuselage skin under body faking; lot # 9-25-96- 2

b C2434 cl301 40 39 48.70 -72 37 28.20 FS 1520-1540 stringer 25L-26L

22860 9/22/96-l --- 23389 40 39 50.60 -72 37 26.20 FS -I-..

1560-1580 stringer 39L --

C2443 8/30/96-l Cl301 40 39 48.70 -72 37 28.20 FS 1620-1640 stringer 33L-34~

I I I -I - Al.21

GRP # Log # Tag # FBI # Source Tag # Latitude Longitude

FS 960-990 stringer segment 42L

,

RF1241 A739

RFl24J x4051

8l24/96-8 40 38 30.84 -72 38 49.80 FS 807-820 stringer segment 41 L

1 l/23/96-129 T7839 FS 820-885 stringer segment 41 L

RF1 24L X4046 11120/96-164 l-7119’ FS 885-908 stringer segment 38L

, !

RFl24M 3

A2055 B/17/964 A649 40 38 54.80 -72 38 53.30 FS 908-935 stringer segment 38L

RF1240 x4047 1 l/29/96-267 l-7203 FS 790-800 stringer segment 39L

I

I I I RFl24Q

I I x4948

I ll/lW96-213

I l-7596 FS 780-882 stringer segment 37L

I RFl24S x4049 1 l/23/96-130 77834 FS 840-950 stringer segment 36L

8110196-9

W/96-46

WI 1196-l

403811.33 -72 37 31.77 FS 880-900 stringer skin/6”x2”x2” alum StNt;

lR3R RHS l’xl’ fuselage crown

40 38 21.82 -72 38 25.96 FS 940-1000; stringer 9R-15R

40 38 21.75 -72 38 27.64 body crown fuselage; changed from B561 to A2031 to match actual debris field

40 38 40.92 -72 38 25.24 FS

RF3 !

A052 0 39 03.78 -72 38 27.88 FS 560670

RF35 I I

A421 I

8/14/96-l 1 0 37 54.37 -72 38 53.54 15’xlO’ siding “TR” on side: FS 640-960; stringer 6R-25R with window frame

I

RF46 A476 8119/96-l 1 40 38 23.46 -72 38 31.94 FS 840-880. Stringer RI-R6

RF5 A071 8103196-85 40 38 43.10 -72 39 19.80 FS 740-780 stringers 15R-26R with R2 door attached 7 on inner door frame)

(#5804951 bottom

RF57 - A710 0 38 22.30 -72 38 30.00 FS 900 frame stringer 25R-21 R

// A033 I 8/03/96-85 40 38 39.55 -72 30 07.45 FS 800-840; stringer 13R-16R with R2 door frame

I I I RF91

I A2021

I I W04J96-66

I Al01 0 38 51.72 -72 38 48.02 FS 300340 stringer 27R41 R;

/ s :

, I : GRP# Log # Tag # FBI # Source Tag # Latitude Longitude Descriptton (Actual)

I RFl22C A204 806&646 40 38 33.74 -72 38 42.75 FS 840 frame segment 2L-6L & 5’ Piece of 5/8” 02 Tubing -

RF1 9A Al66 8/06/96-l 40 38 33.55 -72 38 42.25 - FS 900-940; stringer 0-6R, 5x3 munded alum siding: inside p/n 41114#158; 7380-2DBLR; RH fuselage crown skin;

2 LF31 A601 8t12B64 ---._

40 38 35.80 ---- -72 39 09.00 forward lower cargo bay structure FS 800-840 centerline (FS 980 floor _----

beam - LBL 20 to RBL 11.

LF55B A2049 8l22/96-7 A696 40 39 45.10 -72 36 28.75 bulkhead instl segment under wing, front spar FS 1000, LBL 26 - 42

RF1 23K A2053 8/22i96-7 A696 40 39 45.10 -72 36 28.75 FS 855-938 stringer segment 3L

RF32 A605 8112l96-4 40 38 35.80 -72 39 09.00 Right belly and cargo track between FS 800-940; stringer 37R44R

3 LFl4A, A2048 A004 4 LF55D

0 38 41.29 -72 39 15.25 keel beam section box; also refer to LF 55D; LF55D = bulkhead instl segment under wing, front dbor spar FSlOOO, RBL 9 - LBL 18; attached to forward portion of keel beam (LFl4A) ; FS 1000 bulkhead undenving

RF01 attached to LF14A

A004 40 38 41.29 -72 39 15.25 FS 760-960; stringer 22R-37R; p/n 6580173

4 RF84 A2030 8104196-66 Al26 40 38 35.38 -72 38 08.94 FS 400420; stringer 24A-32A right hand fuselage:

RF87 A2032 8104196-66 A126 40 38 35.38 -72 38 08.94 FS 270-290; stringer 39R:

5 RF1 07 A2022 8lO496-66 A126 40 38 35.38 -72 38 06.94 FS 300-340; stringers 34R-39R; this part is probably yellow, per Boeing engineer

L RF88 A2025 8tO4196-66 Al26 40 38 35.38 -72 38 08.94 fuselage skin FS 260; stringer 39R41 R;

RF89 A2020 8IO4196-68 Al 26 40 38 35.38 -72 38 08.94 fuselage skin FS 360-400 stringer 34R41R;

6 LFl2A Al26 8104196-66 40 38 35.38 -72 38 08.94 fuselage FS 940-820; stringer 6L-17L

RF121 B A2050 8103l96-85 A022 40 38 41.57 -72 39 07.30 FS 1000 underwing bulkead stiffner at BL R33.89

7 FBMGD A518 8119196-23 40 38 24.30 -72 38 31.08 floor beam and frame segment FS 920 LBL 100-SOB S25L-27.5 I

LF05 A022 8103196-85 40 38 41.57 -72 39 b7.30 FS 780-920; stringer 23L-37L

4’xl’ framing and wire harness

7

-840 RBW to LBL 94

IzA Al.8

GRP # Log # Tag # FBI # Source Tag # Latitude Longitude Description (Actual) . ..(_ .A423 . . ~38.2j.7d

seai track RBL 11.33 FS 940-960

I LF88D A2026

m.--- ___ 810619646 A202 40 38 39.27 _. ‘---~~~.ji~~

10 FBMllD A2043 - -- _. ̂_ Al45 40 -----72 -.. 38 40.51 38 55.05

FMBZOD A639 8116196-l 0 40 38 40.70 -72 38 55.00

.-..... _ ..- --.-- _ ..- --.. .--..- fuselage belly skin ; FS 1580-1600 stringer 3=-- .‘- - .‘. ..- -. --- “‘. --.-’

., .-_.- . _ -. ..I_____ seat track LBL 33.99 FS 840-880-““-‘- ---v-e.-* .-

_.. . .._._- .- ^...._ ._

12” floor beam upper chord STA 800, RBL 55 to RBL 70

11 FBM6A A2040 I I

Al09 I

0 38 37.29 72 39 12.46 floor beam upper chord FS 920, RBL 16-37 I I

LF32 Al45 8/05/96-2 I

40 38 40.51 -72 38 55.05 FS 940 tension tie; 665809631-57 753

12 FBMlOF

FBMllA

I

A2046 A231 I

40 38 35.99 -72 38 38.36 STA 880 floor beam lower chord LBL 25-70

Al09 8/04/96-65 40 38 37.29 -72 39 12.46 floor beam with seat track; FS 840-880; RBL 33.99 I I I

13 FBMlOC I

A673 I

8/l 9196-l 3 I I

0 38 37.54 -72 38 36.75 floor beam lower chord FS 880 LBL 70-121 (SOB)

I I I FBMM Al44 8/05/96-Z 40 38 35.99 -72 38 37.89 floor beam and frame connection FS 960, LBL 110 to SOB S25-29

1 1 14 CW608 I A533

I 8/20/96-l 5

I I 0 38 30.66 -72 38 59.76 3 pieces: 1) metal 1 O”xl8”;

6’X6”X2” 2) spring/hinge, small; 3) plastic cowling

WV911

FBMPl

LF24A

A2054

Al39

A2017

8/08/96-l 4

WO5/96-2

A252

40 38 27.14

40 38 37.20

40 38 26.39

-72 38 34.54

-72 30 36.84

-72 38 34.66

cw spanwise beam #l section

floor STA 780-800 RBL assy. 33 to RBL 72.3x3 alum area

framing possible cargo

FS 800-860; stringer 39L-44L

I

LF24B A252 I

8/08/96-l 4 I

40 38 26.39 -72 38 34.66 FS 800880; stringer 36L4OL

LF44 I ,

A536 !

8/20/98-l 5 I I

0 38 30.66 -72 38 59.76 Forward lower cargo bay structure FS 940 left hand side

15 CW603 A227 8lO6I96-46 40 38 39.15 -72 38 52.96 SWB #3 RBL 23 to LBL 20; p/n 65601110 19 I

LWO5, LW06 A2018 8tO6t96-46 A227 40 38 39.15 -72 38 52.96 LW05 lower wing skin outboard; LW06 upper wing skin outboard; both are --.- --.._ I_- --- .--. attached to A201 8

16 cw513 - ..- ___-__ A500 -.- ..-. _--I_ 8/19/96-l 1 _ ..-. . --.- - .-. ..--. - . . . . . . . . _ 40 38 32.60 -72 38 38.37 _-- ,-.. .--.-.. -I--. front web RBL 76 spar

-.---.------- -.-... ----_^._ __________ -__

1 FBMGE A225 8iO6t96-46 40 38 32.48 -72 38 37.73 floor beam chord 8 upper web FS 920, LBL 102-72

I 17 CW602 A210 8fO6l96-46 40 38 32.43 -72 38 37.87 spanwise beam #3 -mid right side; p/n 65810683 2

‘GRP # Log# Tag # FBI #I Source Tag # Latitude Longitude Description (Actual) ---...-- --... I.-.-- ._ -- ------ .

17 FBM3C ..-_-..--. - -. _ --.I- .-.. . . ..- r--.- _” - --..

Al 74 -. . ..- .-.-_.- ._. .__ .._-. .._..

8/06/96-l 40 38 32.33 -72 38 38.95 framing 3x1 rollers on bottom; floor cargo framing

----- -- --- -.-.- -_- --_.. . .._ ._..... .-..-____. _ ..-___ cw512

.__.-. .-. -... ._ . . 18

.__.....__._. _.._, ..,_ . _. _______. -.-_ . A230 8/08/9614 40 38 31.08 -72 39 05.10 SWB FS #3; Web RBL 66-RBL 4$

LF36 A260 8/08/96-14 40 38 31.20 -72 39 04.68 FS 980 lower frame 40L-42R Stringer

.

Also

? j :.

GRP R LogI Tag I FBI t Source lag # Latitude Longitude Description (Actual)

CW304 82023 8097 right SOB CW rib; web between R.S. and SWS 1.

cw305 82022 .-.-___-_._

8097 right SOB CW rib; web. between SWB 1 and mid spar. Lablong is in Red field

CW706 82002 8m4l96-64 spanwise beam #2 web and chord LBL 26-RBL 3 I

CW805 82024

FBM22A 8571 8/l 7&6-1 floor beam STA 780; BL 0 to RBL 34

LP8A 82085 8AKv96-145 upper portion of FS 140 bulkhead

LF3OD 82076 8m8/96-3 1 BO81 40 39 09.49 -72 38 31.92 FS 160-i 80 stringer 24R-26R

RF31 82014 8io4m-64 FS 1480-1550,148O bulkhead WL 220 to stringer 36R; changed to white due to mixed FBI lot #

RF68 82060 FS 480-520, stringer 37R40R;

RF69 82063 FS 300340, stringer 21R-26R;

RF72 82064 FS 400-433, stringer 43-BLO;

RFl22B 8343 WI o/96-9 40 39 00.00 -72 38 24.00 FS 820 frame srlnger 3AR-6L segment

1 LF7D 8257 8107196-l 5 40 39 04.90 -72 38 24.80 FS 140-380; stringer 045L; top of skin below cockpit window structure

LF8C 82051 8265 40 39 04.90 -72 38 24.80 FWD pressure bulkhead portion FS 180

LFBD 82052 8/07/96-l 5 B265 40 39 04.90 -72 38 24.80 FWD Press Bulkhead Portion FS 180

LFBF B264 8/07&6-l 5 40 39 04.90 -72 38 24.80 Front end passenger floor 8 radome bulkhead FS 140-180

LF19A 8265 8107196-l 5 40 39 04.90 -72 38 24.80 left side upper fuselage, FS 380-520, stringer 18L-19R;

LFl9B ’ s 82068 8/07/96-l 5 8265 40 39 04.90 -72 38; 24.80 part of LFISA; saw cut separated part into two pieces

LF22-01 8290 wow96-31 40 39 04.70 -72 38 26.80 skin panel section 42; FS 660-680; stringer 41L47L

LF22-02 8298 wo8/96-31 40 39 04.70 -72 38 26.80 FS 680-700; stringer 41 L-47R

Al.11

‘\ i ) j ’ .-

GRP # Log # Tag # FBI t Source Tag t Latitude Longitude Deqcrfption (Actual)

1 Lf=22-24 8332 8lW96-4 40 39 04.70 -72 38 26.80 skin/frame; FS 760-780 Stringer 40L42L

LF23 B325 8fl2f964 40 39 04.70 -72 38 26.80 - ---- -----

FS 675-725; stringer 34L-38L I

LF25 B307 8/08196-31 40 39 04.70 -72 38 26.80 FS 340-380; stringer 9L - 19L

RFGC 8318 S/08/96-3 1 40 39 04.70 -72 38 26.80 FS 570-600 stringers 22R-23R

RFSC 8263 8/07/96-15 40 39 04.90 -72 38 24.80 FS 140-220; stringer O-31A with window belt

RF24 8333 8/l U964 40 39 04.70 -72 38 26.80 FS 740-760 stringer 32R-36R

RF25 8289 S/08/96-31

--.-.-.---w-e--.- -...---- ------ 40 39 04.70 -72 38 26.80

-. - -.... . ._ _- ..-- ---..-- .-.-. --I.-_----.- . -. -._-. . _........- . -_._. ._ ._ FS 520-560 stringer 27R-35R, bin cargo #7430;

RF78 8286 S/08/96-31 40 39 04.70 -72 38 26.80 FS 340-400 stringer 15R-19R(passenger cabin skin, section 410)

RF80 8299 8108196-31 40 39 04.70 -72 38 26.80 FS 400-420; stringer 18R-23R with window

RF81 8285 8iOSl96-31 40 39 04.70 -72 38 26.80 FS 380-400; stringer 19R-23R with window (skin panel: wl window)

RF92 8294 S/08/96-31 40 39 04.70 -72 38 26.80 FS 540-560; stringer 34R (cargo door skin; RF FWD)

RFl22A 8292 S/08/96-31 40 39 04.70 -72 38 26.80 FS 800 frame frame stringer 3L-7L segment

2 cw704 82003 7/27/96 BOO3 40 39 03.00 -72 38 32.00 spanwise beam #2 RBL 11 stiffener, cut from BOO3 (CW704)

FBM23 82071 S/03/96-145 8122 40 39 04.30 38 -72 27.20 floor FS 740-800: RBL II .33 to RBL assy 11.33

FBM25 82072 8/03/96-l 45 8122 40 39 04.30 -72 38 27.20 floor FS 720-740; LBL 2 to assy; LBL72

LFI 82006 NoFBI# 8163 40 39 04.30 -72 38 27.20 FS 580-800; stringer 23L-39L (upper deck floor beam length))

segment (approx 20”

LFO4, RF04 8103 8/03/96-145 I 40 39 04.30 -72 38 27.20 FS 520-800; stringer 4L-24L (Note: saw cut above from RF04)

LFO6B 82016 Bl41 40 39 04.30 -72 38 27.20 FS 740-800; stringer 44L43R

LF7A ’ 8134 8fO4f96-65 40 39 04.30 -72 38 27.20 FS 380488; stringer 17L-30L includes door Ll

LF7B 8170 S/05/96-34 40 39 04.30 -72 38 27.20 FS LF7C 8176

8m5196-34 40 39 04.30 -72 38

27.20 380-58O;dI

FS 260-400; stringer 23L42L from window belt to nose wheel’well

A1.12

GRP # Log # Tag # FBI # Source Tag # Latitude Longitude Deecrlptlon (Actual)

2 LF8B 82066 8tO4I96-66 B254 403904.30 -72 38 27.20 lower%lO bulkhead structure -. ---

LF8E --.----.-.. --.-. _ ..-.. -- -...___ . ____.

8254 -“. 8/07/96-15 403904.30 __ _.

-723827.20 forward.preSs;;eiJuii;hea;i _

LFllA 8073 403903.00 -72 38 32.00 canted bulkhead FS 260; 2X4 Bulkhead w/L323 Equip Center Light - FWB

.--. . ..- ..-. . . ._. _ LFllC 8216

,. 403904.30 -72 3827.20 nose wheel well structure upper pressure panel

LFilD 8115 8rn3/96-145 403904.30 -72 38 27.20 nose wheel well skin surrounding nose seal FS 320-260

LFllG 8239 8107t96-15 403904.30 -72 38 27.20 side panel, nose wheel well, FS 245340, p/n65807942 pressure panel

LFllH 8231 8/07/96-15 403994.30 ---.

-723827.20 .-._--__-_

-nose gear wheel well RND bulkhead w/actuator .-_.

LFlli 8067 8/03/96-l 45 40 39 03.00 - -72 38 32.00 -.’ canted bulkhead FS 400 ~--.

LFllJ B156 ww96-65 403904.30 -72 38 27.20 canted bulkhead FS 400

LFllK SO66 403903.00 -72 38 32.00 canted bulkhead FS 400

1 LFIIL 8080 403903.00 -72 38 32.00 forward bulkhead FS 400

LFllO 82074 8223 403904.30 -72 3827.20 portion of nose wheel well structure FS 400 bulkhead

LFllQ SO10 8m3n6-85 403903.00 -72 38 32.00 FS 340 bulkhead

LF19 8131 403904.30 -72 3827.20 L-I door

LF20 8180 8/06/96-2 403904.30 -72 38 27.20 FS 440-580; stringer 42L-37R

I LF21 8215 8/07/98-l 5 403904.30 -72 3827.20 cockpit windows to FS 400; stringer 9L-15R includes 8211 and 8238; skin

with wash nozzles and crew service door LF21 8211 8107196-15 403904.30 -72 3827.20

LF22-3 82036 wo5/96-34 Bl69 403904.30 -72 38 27.20 FS 700-720 stringer 44L-43R 1

LF22-8 * 82081 8223 403904.30 -72 38'27.20 FS 520-540 stringer 39L-43L

LF22-04 B160 8/05/96-5 --- 403904.30 -72 38 27.20 --- FS 741; stringer 45L-43R (l’x2’x5’ twisted AL w/U stiffeners: cargo bin white

w/primer)

LF22-06 8233 8/07/96-15 -I_- -’ -72 3827.20 belly piece; FS 780-800 Stringer 4OL-45~

Al.13

,

GRP # Log % Tag C FBI # Source Tag # Latitude Longitude Description (Actual) 2 LF22-11 8232 --.. -.- wo7/96-15 _--- -----...-- -L-..- ..--... ..-.. --.- -.--......-. . . ._.. _ ---..... -- . * . _- ._._.. -__~-. -

40 39 04.30 -72 38 27.20 right fuselage FS 580-560 stringer 4044

LF22-13 .--.--.---------._.---- -.--.------ _ ..--..-.. _ 1.. 8234 --_. .-. 8/07/96-l 5 .._.-....-_ - _..... ._.._ -.-.__ ..-..... . . .._ 40 39 04.30 -72 38 27.20 FS 660-680; stringer 41 L-45L

LF22-14 SO18 -.-__-_.--_--

wo3m6-85 40 39 03.00 -72 38 32.00 -..--.-- -...---._-

FS 600-620; stringer 42L-39L

LF22-18 82043 8/03/96-l 45 BIOI 40 39 04.30 -72 38 27.20 FS 640-660 stringer 45L47R

LF22-19 SO13 WO3/96-85 40 39 03.00 -72 38 32.00 FS 580-600; stringer L38-L39

LF22-20 8249 8/07/96-l 5 40 39 04.30 -72 38 27.20 FS 600620; stringer 44R47R

* LF22-21 82044 8/03196-l 45 8101 40 39 04.30 -72 38 27.20 FS 620-640 stringer 46R42R

LF22-22 82073 8101 40 04.30 -72 39 38 27.20 FS 620-640 stringer 47L-48R

LF22-23 8251 WO7/96-15 40 39 04.30 -72 38 27.20 FS 640-660; stringer 44R46R

LF22-27 8201 8tO6t962 50 39 04.30 -72 38 27.20 FS 560; stringer 44R

LF22-28 82079 BlOl 40 39 04.30 -72 38 27.20 FS 720-741 stringer 43L45L

LF22-30 82080 8101 40 39 04.30 -72 38 27.20 FS 580-600 stringer 42R46R

LF22-34 B209 WO7/96-15 39 40 04.30 -72 38 27.20 FS 500-540; stringer 40R45R

LF3OB 82078 8tW96-65 8133 40 39 04.30 -72 38 27.20 FS 200-240 stringer 24R45R

LFJOC 8078 8/03/96 145 40 39 03.00 -72 38 32.00 stringer 26R - 38R Canted bulkhead FS 260-280

LF3OF 8204 8106196-2 40 39 04.30 -72 38 27.20 FS 240, skin splice, fuselage; FS 260-280 i

LF30G 8235 8/07/96-l 5 40 39 04.30 -72 38 27.20 skin section FS 200-260; stringer 3443

LF30E(2) 82077 WO498-65 6133 40 39 04.30 -72 38 27.20 FS 180-120 two stringer 26R-36R, pieces

LF72 - 82065 8125 40 39 04.30 -72 38 27.20 circular stairway cutout in deck upper

LF82M 82083 -_ 8132 40 39 04.30 -72 38 27.20

LF84 82084 8223 40 39 04.30 -72 38 27.20

GRP # Log # Tag # FBI # Source Tag # Latitude Longitude Description (Actual)

i 2 RF3A 0250 a/o7f96.t --..-- __ 5

0 39 04.30 1 -72

---

38 27.20 -T- FS 600-780 stringer 23R44R with attached cargo door ~-

-.

I , I I ’ RF% 1 8223 1 a/o?f%-15 1 ---- k 03g-04.30 I --____-..- I .- ------.-.._ --.--_ .._.-.. - ._-. _-.-.-

-72 38 27.20 FS -----..

600-720, stringers 24R-26R with rear top portion of forward cargo door -

1

_ _. - _. _ 24R-3dR with top right corner of forward cargo door

RFJE 8221

RFJF 8011

RFJH 82017

a/07/96-1 5

a/04/96-65

8250

40 39 04.30 -72 38 27.20 small section of forward door upper cargo

40 39 03.00 -72 38 32.00 FS 680-720 Stringer 26R36R

40 39 04.30 -72 38 27.20 fwd lower portion right cargo door; FS 560-670; target # 2931.28

RFGA 62004 afo3i96-85 BOO8 40 39 03.00 -72 38 32.00 right hand fuselage window bays; FS 620-740 stringer 19R-26R with windows

RFGB

RF86

8240

B256

a/07/96-1 5

8/07/96-l 5

40 39 04.30 -72 38 27.20 FS 560-640; stringer 19R-23R with window belt

40 39 04.30 -72 38 27.20 FS 240-287; stringer 8A-14R

I I I I I RFBD

I 6068 8/03/96-145 0 39 03.00 -72 38 32.00 FS 240-287; stringer 22R-26R (Right fuselage: WI pitot tube)

RF8E 8268 8/08/96-31 40 39 04.70 -72 38 26.80 FS 160-220; stringer 22R-24A with window belt

RF8F 8248 atO?/9a-15

RFIM Bl18 alo3/96-145

RF18C 8141 8/04/96-65

RFl8D 82021 a/05/96-3

RF1 8E 8202 aEw96-2

RFl8F 82013 alO?l96-15

8123

8141

0224

40 39 04.30 -72 38 27.20

40 39 04.30 -72 38 27.20

40 39 04.30 -72 38 27.20

40 39 04.30 -72 38 27.20

40 39 04.30 -72 38 27.20

40 39 04.30 -72 38 27.20

FS 220-287; stringer 14A-22R with window belt

FS 420440; stringer 20R-27R

FS 488-560 stringer 13R-3lR, aft and beneath R-l door (Aircraft door frame and 3 window frames)

FS 460-520; stringer 31 R-38R

FS 420480 stringers 11 R-l 9R, door 1 upper door cutout;

FS 440-520; stringer 9R-14R

I , RFl8G 821 a 8/07/96-l 5 40 39 04.30 -72 38 27.20 FS 520-560; aff; 40” long stringer 12R-19R

I

RF39B . l 82087 8132 40 39 04.30 -72 38;2?.20 FS 1720-l 740 stringer 23R-26R

RF50 8255 8/07&6-l 5

RF70 8167 8/05/96-17

, 40 39 04.30 -72 38 27.20 section 41 FS 300-340. NWV Right fuselage side panel

40 39 04.30 -72 38 27.20 avionics bay; seat 9-l 0

/! j I GRP # Log # Tag # FBI # Source Tag # Latitude Longitude Description (Actual)

2 RF79 82059 8/0?/96-15 8212 40 39 04.30 -72 38 27.20 FS 340-360; stringer 19R-22R with window

RF82 8222 8/07/96-l 5 40 39 04.30 -72 38 27.20 FS 380400 22R-23R (piece of window frame) 1 stringer , .---.--

RF83 82058 8/07/96-l 5 8212 40 39 04.30 -72 38 27.20 FS 360-380; 19R-23R with window stringer

RF85 8203 8/06/96-2 40 39 04.30 -72 38 27.20 FS 340-380, stringer 23R-37R

RF90 Bl91 8/06/96-2 40 39 04.30 -72 38 27.20 fuselage skin; FS 340-360; stringer 37R41 R

RF1128 82086 8163 40 39 04.30 -72 38 27.20 FS 450440 stringer 34R43R

RF113 8070 8/03/96-l 45 40 39 03.00 -72 38 32.00 2’x3’ red 6 white skin peeled

3 cw704 Boo3 40 39 03.00 -72 38 32.00 SWB #2 RBL 33-3. was cut by NTSB, its associated piece is 82003 or (CW 704)

LFl8 8001 40 39 03.00 -72 38 32.00 nose wheel well sidewall and FS 340 Bulkhead

LF22-05 8005 40 39 03.00 -72 38 32.00 FS 740; stringer 39L44L

RF38 BOO8 8/03196-85 40 39 03.00 -72 38 32.00 FS 600-640 stringers 26R-25R with portion of floor beam

RF3G BOO? 8103196-85 40 39 03.00 -72 38 32.00 RF 3 Cargo door hinge; 2 rollers

RF188 BOO6 8lo3l96-85 40 39 03.00 -72 38 32.00 RI Door Top

I I I I I I RWO? 8004 0 39 03.00 -72 38 32.00 RH wing upper skin plank; Right Hand Wing Upper Skin Plank

Al.16

CW1008 8/24/96-7 03942.44 -72 38 19.01 rear spar, left corner section

t-l CWI 023 22814 10103l964 21771 rear spar stiffener at RBL 46, complete

--- cw1101 C2402 --- --...- --.. --.- .- .-.-- -.._._ 403950.46

_ __ ..-. -72378.96

._._ ._. --;--. --...--.- . . ..-----._--- - --.-- -_- .._._ _ CW BBL 0 rib, from mrd spar aft 20”, from upper rib chord down 36”

_ ___ ._

cw114

CWI 21

23028

C413

9108196-2

8/14l96-9

403957.98 -72 3723.73 upper CW skin FS to stringer 27; LBL 17-l I? (4’ x 5’ section of interior structure)

403949.49 -72 3709.00 fuselage (yellow) 2.5’x18”

cm137 24013 1 l/06/96-98 T6528 CW upper skin LBL 108-l 19, between stringer 7 and 9 I

CWI38 24004 11106/96-12 ---_ T6519 -____. --_--

CW upper skin, -.-.

stringer LBL 34 21, j

I

CW142 22868 23258 403943.60 -72 37 II.10 part of CW fuel tank

I I I cw147

I 22786

_I_-.- 1 --.---- .---.-_-. -..--- .-... . .-_.

I I ._ .._ -..- -.___-.____ -...- _.__ - .._..._. .- ___. - ..__ r .._ _ ..-.

I

cw150 24005 1 Ill l/96-2? CW upper skin, RBL 57, stringer 22

CWIBI 24009 1 l/l 1196.79 CW upper skin, at mid LBL spar, 34

I , CW152

I 24010

I 11/14/96-78

I T6242

I CW upper skin stringer 16 LBL 27-57

CW208 c2234 a/1 8196-6 lower CW skin: STR 12-l 5; LBL 1 I- RBL 37

CW211, cw1009

cw237

Cl031

Z2831

8723/96-l 5

9/l 2/96-l

403950.46 -72 3721.45 lower CW skin; R.S. to STR 1; LBL 15 to RBL 15

CW lower skin RBL 13.RBL 25 midspar lower fwd chord 8 4” of skin.

1 CW238 24006

I Ill1 l/96-25 T6025

I CW lower skin RBL 4047, stringer 12 - SWB #2

I

cw239 24007 1 l/l 1196-70 T6024 CW lower skin RBL 80-98, mid spar aft chord with 5” of skin

I 1 ill 1196-78 T6139 0 CW lower skin, RBL 90, SWB #I, 4’x3”

RH SOB rib 5”x8” web at 40” forward of rear spar

GRP # Log # Tag # FBI # Source Tag # Latitude Longitude Description (Actual)

cW332 24003 1 m6lQ6-29 T6522 RH SOB rib lO”x25” web forward of SWB #2

I I I I CW334 24012 1 l/14/96-102 T6239 / --1--‘-06 ribwebatSWBR3 --

cW335 24011 ilill/Q6-58 T6195

--- --_ --I.-- .___- RH SOB rib web forward of SW6 #3

CW518, LF38

cw519

C851

23029

8116196-5

9/08l96-2

40 39 52.48 -72 37 14.03 FS 900-1350 strtnger 4R-29L; portion cut per NTSB and secured to CW mockup

I 40 39 46.70 -72 37 36.51 front spar web; RBL 65-l 12;

H1 22575 9/l l/96-5 40 39 53.90 -72 30.08 37 fuselage fragment or flight control surface or wing \

H6 23002 9lOW96-2 40 39 45.13 -72 37 21.52 6’ x 4’ edge of wing target #GRS992

H6 c2394 CO71 40 39 45.83 -72 37 08.61 horizontal stabilizer right side inboard nose section

H8 23125 9/l 01964 40 39 46.00 -72 21.20 37 horizontal stabitiier skin between aux. and rear stabilizer upper spar spar. STA 143.60-180.50

LFlOE CO44 8/l 1196-l 40 39 39.49 -72 36 32.23 portion of aft bulkhead; 9x6’ tapering mass w/ins1 attached p/n pressure 6580263456 on clip

LFl4B. co61 60 4l969 LFl4A

keel beam box, FS i 000-I 140

LF59 C708 8f26iQ6-4 FS 91 O-960; stringer 14L -1 QL

LF67A 23304 Q/l 2196-2 40 44.20 39 -72 37 23.10 ME0 3L cutout skin, LWR part FS 1265-l 350, stringer 23L-31 L

LF68 23100 9llm6-2 40 39 44.30 -72 37 27.90 FS 1060 stub beam

LF69 22586 9116/98-2 40 39 44.42 -72 36 55.17 crown skin FS 1241-1438 stringer 5L-8R

LF71 B 23268 9119/96-l 40 39 54.46 -72 37 33.57 FS 1350-I 394 stringer 23L - 33L

LF73B C2183 8129196-2 I I

Cl652 A I

0 39 45.40 -72 37 35.20 FS 2412-2436 (3x2.5’); stringer 18L-23L

LF82W I I

- 22849 23459 40 39 43.24 -72 36 30.45 FS 1540-l 550 stringer 33L-34L

LF86L . Z2842 23417 I-

FS 1260 segment stringer 28L-30L

-.--.. 7. LF87A 1-~l~---/.--z34ij.-~------- _.-_ _. -- 1 FS 960-980 stringer 32L-34L ------l

. . - . . . - - LF870-‘. -.-z2ii~~ ._I . .__ --_---_ - - - _ . - - - - . . . . - . . - - - . . _ . .

23518 _ . - . - . - .

FS 990 segment stringer 35L

Al.18

GRP # Log w Tag t FBI# Source Tag t Latitude Longitude Description (Actual) LF88H 21787 - lOrn7/96-1 --.--. 4 o 3Q 53.38 -72 3734.22 ----.. ~si~~~;~2~s~~~~~~~8~~~“- -- .---- _--_ --_--.. - .I._

LF88J z3731 10117/96-1 40 39 58.97

- -72 37

26.18- FS 1660-l 720 stringer 31 L-35L; aircraft skin with red paint

LF88M 23786 10/18/96-3 40 39 59.83 -72 37 skin yellow/green. with electrical wiring and

44.60- ribs attached

4

I

LF89 25058

LW30 co10

LW31 C2262

LW32 C428

RF1 14A 23568

RF1 148 22854

RF115 23496

RFl22H 24024

RF1 22N 25051

RF1 23G 24025

RF123J 24026

RF1240 23571

RFl24T 23573

1 O/l 7196-2 40 39 37.86 -72 36 34.77 3’ X 4’ metal piece

WO9/96-37 40 39 43.28 -72 37 19.15 left wing skin, WS 505584 from STR 16-22 upper

8/09/96-37 CO1 0 40 39 43.86 -72 37 18.00 left wing skin; LWS 554-580 from STR 7-10 upper

8/24/98-7 40 39 05.64 -72 36 03.45 left wing outboard aileron section and wing bulkhead

9/28/96-l 40 39 49.80 -72 37 38.30 window; fuselage .

23589 40 39 50.40 -72 37 17.50 FS 1060-1080 stringer 24R-26R

g/25196-2 40 39 48.10 -72 37 31.20 7x9 section of metal debris

1 l/29/96-39 T7180 FS 880 frame stringer segment

10117/96-2 40 39 34.02 -72 37 08.58 FS 920 frame stringer segmentl3L.18L

11/11/96-51 T6177 FS 912-940 stringer segment 0

11108196-18 T6582 FS 820-885 stringer segment 2AL

9/28/96-l 40 38 22.91 -72 38 46.91 I

FS 865-880 stringer segment 43L

Q/28/96-1 40 38 23.77 -72 38 40.56 FS 880-930 stringer segment 35L

RF23

RF34

c299 8/10/96-16

CO67 8714196-9

FS 1020-1240; stringer 11 R-l 9

body crown area FS 980-i 160, STGR 11 R-3L

RF41

RF76

RW13

. C848 8/E/96-5 40 39 50.72 -72 37 13.33 fuselage Fragment; FS 1135-1280; stringer 1 I R-6L

22526 23031 40 39 45.61 -72 37 10.01 RT stub Frame FS - 1060, RBL 98.58 RBL 127.50

co14 -..----...--~-,.-.---_-__-

8109196-37 40 39 52.08 -72 37 18.66 #5 flap track “TWA 17729” mfg 5881129-6; flap track with jack screw

--._--_~ -- Al.19

/’ ‘1 ; GRP # Log iy Wl?

--I

FB1 # Source lag # Latitude Longitude Descrlptton (Actual)

RW15C C813 8MY98-8 right hand outboard aileron WS 1358-1488

RWI8 23318 Q/l 8l96-2 40 39 55.63 -72 37 28.84 right hand inboard flap assembly trailing edge with carriages (2O’xlo’)

RW23 23596 10/10198-1 40 39 56.10 -72 37 24.39 ‘--‘---.-.-.----~ -#6 flap track - --.--

-- V4 co20 8/09196-37

I---.....-.- ---- . ..I .._.. _- . . . ---~-.. _“.__. ___ 40 39 31.08

.- ._ - .-_ ._ . _-.... _ ,. . ._ _. -72 36 57.32 LHS vertical stabilizer upper fin station 370-520

_

v7 C2393

I CWI 108 22773 23552 40 39 47.11 -72 37 13.88 portion of span wise beam CW tank

cw117 23038 918196-2 40 39 45.30 .-----. -.

-72 37 23.70 -- 15’ long structural member -

cw139 22736 z3440 40 39 42.31 -72 38 10.57 CW upper skin (9-22-96-I)

cW201 C2147 Cl08 40 39 48.90 -72 37 27.90 lower cw skin-right fwd side STR 1-21

CW232 23376 Q/22/96-1 40 39 48.01 -72 37 27.06 CW lower skin. RBL 960, STGR 10-13

CwIOl C874 8/l 6/96-5 40 39 50.80 -72 37 23.47 spanwise beam #2 - RH web; SOB rib to RBL 90

cw914 22808 23451 40 39 46.40 -72 37 26.80 SWB #l web right hand closure panel

LF45A C976 8/20/96-12 40 39 47.24 -72 37 27.28 FS 1480 bulkhead & skin

LF82N C2413 c%! 40 39 47.36 -72 37 27.71 FS 1580-l 600 stringer 44L-45L

RF103 c2200 8i29l96-4 Cl700 40 39 47.80 -72 37 29.60 piece of fuselage, left side

RFiOA Cl06 0

8104196-l 11 40 39 46.90 -72 37 27.90 - FS 1480-1860; stringers 2R-23R with window belt and R4 door frame j

RF44A c2054 8li8/96-6 CI 14 40 39 46.90 -72 37 27.90 lower Portion bulk cargo door surround FS 1960 - 2080 ; stringer 36R - 45R

RF45B C2276 8/05/96-70 Cl 14 40 39 46.90 -72 37 27.90 FS 1840; stringer 45R46R

2 I I

CWI105 N 22826 I O/09/96-1 a249 40 39 49.35 =

_._ _ _.. _ ---__ CW402 C2026

_I-.--- 8/l 8196-6 C891 40 39 46.15

--- --

cw404 C2269 (2896 40 39 46.15

-. Al.20

GRP # Log i Tag # FBI # Source Tag # Latitude Longitude Description (Actual)

1 3 LWOl COO6 8/02l96-23 40 39 45.00 -72 37 27.00 lower left wing skin; WBL 448-1098: mid to rear spar

--. -- ._--~--- LWO2 coo5 40 39 45.00 -72 37 27.00 lower left wing skin; WBL 584-910; lower panel skin splice to aft spar

I I I I ---.--- -L- -__---- LW2I COO8 0 39 45.00 -72 37 27.00 #4 flap track assembly

LW3I C2263 811 I/96-2 C300 40 39 42.00 -72 37 22.00 left wing fragment mates in LWS up 554-580 behind mid-spar small fragment

LW34 Cl685 --.

8l29l96-4 --- --._.. .-._-_.- -._. . _ - ..-._ .__- -_. --- -.-. ._._ -. _..-. .- ._..._-. . . ..---. .-.. _ _- .._ _ - -.. - .-.- -_

40 39 47.80 -72 37 29.60 left wing outboard aileron - outer I/3 of the aileron

I I I I I I

LW43 23083 9/I 1 I964 0 39 44.75 -72 37 26.20 left wing flap track actuator #2

RF106 Cl664

RFIllC Z2852

81291964

23417

--. 40 39 47.80 -72 37 29.60 FS 2440-2500, aft fuselage, upper crown skin

40 39 41.24 -72 36 36.62 FS 1540-l 560 stringer 48R-51 R

RFIIIG C2433 c434 40 39 42.93 -72 36 24.91 FS 1520-l 540 stringer 26R-28R

RFl22W 22865 9/30/96-l

RF2 coo4 8/02/96-23

RF38 C811 8/15/96-8

RF43 C810 8/15lS6-8

RF65 Cl661 8l29l96-4

RF74 Cl668 8l29196-4

RF95 23072 9/l 11964

RW19 22807 Q/25/96-2

v9 Cl658 8/29/964

23201 40 39 49.55 -72 37 26.39 . FS 980 frame segment stringer 6R-14R

40 39 45.80 -72 37 26.70 FS 2100-2280 stringer 23R-2R

40 39 49.50 -72 37 22.80 fuselage right side; FS 1350-1480, stringer 23R-32R with FS1350 bulkhead frame and RHS landing gear beam

40 39 49.50 -72 37 22.80 body landing drag strut 8 gear

40 39 47.80 -72 37.29.60 FS 1500-1600; stringer 12R-21 R; with window belt

40 39 47.80 -72 37 29.60 FS 42R-51 L 2280-2345, stringer

- 40 39 43.20 -72 37 23.30 FS 920-I 35R40R 000; stringer i

23517 40 39 49.10 -72 37 29.10 right surface near WS wing upper rear spar 1250

40 39 47.80 -72 37 29.60 misc. section) of aircraft part (tail 4

; 4 CW324 - 22804 23450 40 39 38.99 -72 36 22.67 right SOB web at first stiff forward of M.S., FS 1120, below CW303

--- --. - CW326 22797 23629 40 39 47.30 -72 37 07.90 web-lower segment right SOB

CW606 23045 Q/09/9649 40 39 47.37 -72 05.80 SWB #l web; 1’ x 2’ sheet metal with rivets 37 green

--..------- I._._. _..-. _ _..... -... -.___- ..---. _ .-..---_._- -- J Al.22

GRP # Log # Tag # FBI # Source Tag # Latitude Longitude Descrlptlon (Actual)

rzp__

4 Cv609 22671 23275 40 39 45.80 --- -72 37 17.40 --.SWB#3-~pper~~~~~-~~---------- ____ ---...

CW610 22764 10/03/96-4 --.--. -__--- -_-. I_- -.--...- - --. ..-._...-- -.-.... . . ..--- --.- --_--

23208 40 39 45.90 -72 37 18.40 ..- -----. -.- ._-.- ---.- . . . . ---.

CW tank spanwise beam #3 LBL 82-98.6

CW611 22765 1wowg64- -I_--.-- -.--.- ----__. .-.-- ._... .- -.L -.- . . --

23218 40 39 48.40 -_-__-_---.--- ___...-- -_ _ ._.. _

-72 37 17.00 CW tank spanwise beam 3 LBL 98.6 side of body

CW810 22762 23224 40 39 52.85 -72 37 26.54 CW tank midspar web LBL 52-78

CW815 Z2774 23120 40 39 47.40 -72 37 23.50 portion of spanwise beam CW tank

CW818 22513 23045 40 39 47.37 -72 37 05.80 mid spar CW stitener

cw907 22662 9/l 9196-l 23274 40 39 45.80 -72 37 17.40 center wing fuel tank spanwise beam

cw913 23394 9/24/96-l 6 40 39 51 .oo -72 37 28.00 CW SWB #l stiffener + web, RBL 83.2

cW915 22809 Z3450 40 39 38.99 -72 36 22.67 SWB #1 web right hand closure panel

CW918 22812 23450 40 39 38.99 -72 36 22.67 SWB #I web right hand closure panel

cw919 22813 23450 40 39 38.99 -72 36 22.67 SWB #l web right hand closure panel

H4, LElA C674 8/23/96-l 5 40 39 47.04 -72 37 26.90 inboard portion LHS inboard elevatir ES 106-156

LFlOD C2260 WO5/96-70 Cl20 40 39 46.90 -72 37 27.90 portion of aft press bulkhead FS 2360 1

LFl OF, c409 w14/96-9 40 39 47.00 -72 37 29.00 portion aft section bulkhead

LFlOG C2383 8/20/96-12 C946 40 39 47.41 -72 37 27.64 portion of aft pressure bulkhead

LF27F Cl53 8lO6l96-46 40 39 47.00 -72 37 27.90 LF FS 1940-l 960

LF28A Cl54 W06196-46 40 39 47.00 -72 37 27.90 LF FS 1960-2020

LF28C Cl75 8lO6l96-46 40 39 47.00 -72 37; 27.90 fuselage sect w/parts of 3 window apertures, FS 2020-2100

LF3 * coo3 ---.-. --------

40 39 46.60 -72 37 26.70 FS 1720-2018, stringer 27L-3R ---

LF33A c410 --.

w14/96-9 40 39 47.00 -72 37 29.00 -.. fuselage fragment 12’xlO’ w/windows and door, FS 2140-2280

LF34 C412 8/l 4l96-9 40 39 47.00 -72 37 29.00 fuselage fragment lO’x8’ greenEwhite; STA 2320-2489, stringer 3L-1 IL

Al.23

GRP# Log # Tag # FBI # Source Tag # Latitude Longitude Dwcrlptfon (Actualj

4 LF35A c401 “------- -----_. -..- ._-.. . . ..__.___ -I_

w14/96-9 40 39 47.00 ‘-72 37 29.00 lefl fuselage FS 2200 - 2240~‘<?~-;‘46~ f&&&g~bulkhe&$&ndow, red ---.__

and white 3x4’

LF41 Cl01 8lO4i96-64 40 39 46.90 -72 37 27.90 LH keel chord FS 1480-1620

LF42A C2006 C923 - 40 39 47.38 -..-- .-72 37 2r7-- Fsisoo-1soo;~~r~g~~~~R-50i-.- -- -.-.--.-.-- .-----,. - ..I. -.. --------

LF42D C2404 CO62 40 39 45.72 -72 37 02.67 FS 1875-I 920 stringer 46L49L

LF42F c952 8/20/96-l 2 40 39 47.41 -72 37 27.64 FS 1740-l 780; stringers 46L49L. fuselage skin

LF45B C2387 8120/96-l 2 C946 40 39 47.41 -72 37 27.64 FS 1480-1500 stringer 23L-27L wl frame support

LF48 C961 8/20/96-12 40 39 47.41 -72 37 27.64 FS 2600.2640; station 4L-46L

LF47 C926 8/l 9196-22 40 39 47.36 -72 37 27.71 FS 1920-2020; stringer 44L49R

LF49 C2406 CO62 40 39 45.72 -72 37 02.67 FS 2484-2552 stringer 25L44L

LF53 c700 8/23/96-l 5 40 39 46.89 .-- -72 37 26.59 FS 1680-i 800; stringer 461.50R

LF54A C2388 WO4196-111 Cl08 40 39 46.90 -72 37 27.90 FS 1416-l 480 stringers 28L-33L with chord beam

LF546 C2389 8t23/96-15 - ---c700 -.------ .^ - ---- ----.

40 39 46.89 -72 37 26.59 FsG3ili 4~~~~~~er~~L~i I---.- --_---. .--.__ -.--- ___.

LF56A c2390 8/20/96-l 2 C946 40 39 47.41 -72 37 27.64 FS 1660-l 700 stringer 39L42L

LF64 22520 9JO9196-49 z3119 40 39 47.40 -72 37 23.00 skin segment: FS 990-l 000; stringer 32L-34L

LF70B 23119 9/09/9649 40 39 47.40 -72 37 23.80 FS 940-960 (2’ long); stringer 31 L-32L I

LF75 23110 9lO9196-49 40 39 47.60 -72 37 23.70 FS 2517-2598 (6’x2’); stringer 8L-11 L

LF82A 22738 z3394 40 39 51.00 - -72 37 28.00 FS 1480-1520 stringer 4OL44L; body landing gear bunion support backup fitting aft 1450 inner and outer

LF82C c2409 C605 403947.24 - -723727.28 FS 1580-l 820 stringer 42L43L

LF82F . C2410 -- ----P.---w-

CO62 40 39 45.72 -... -72 37 02.67 FS 1520-l 540 stringer 35L-4Oc---‘-----’ -B--w-

LF821 C2405 C306 40 39 47.60 --- -72 37 27.10 FS 1660-1700 stringer 36L-39L

. . . _... _, LF83

. . ..---.-I.+.... - . . . . _.. -_ _.___ __,.,_ 23225 1 O/02/96- 1

..- ._---_-__ __ 403952.85

..- -723726.54 4.5-5' X 2-3’ piece of skin (red/white & green metal)

--- Al.24

.GRP # Log# Tag #

4 LF92 Cl04

L I I LW39 22661 ..-----.-.-- _ I I ._.._______ LW46 23123

RF1 1 C2246

RF1 14C 23215

RF12 C2247

RF1 22s co77

RF14 Cl57

RF30A C2252

RFJOB C2253

RF33E C2245

RF33K C692

RF44A c2254

RF530 C686

RF53C Cl025

_I__-.- - .-._ -____. -. .

FBI # Source Tag # Latitude Longitude Description (Actual)

8/04/96-56 40 39 46.90 -72 37 27.90 left body FS 1480 bulkhead gear ; assy LBL 8-75 part of LHS body gear LG3

23274 -_.-.-_. 4 0 39 45.80 -72 37 17.40 left upper wing skin; WS 13361423; stringer 5-14

.-----

9109l96-49 __..- _ .--.. 40 39 47.80 -72 37 23.50 WS left lower wing skin (101x2’); 557-670; mid-spar to stringer 8

8lO8196-46 40 39 47.00 -72 37 FS 27.90- 1580-1620, stringer 30R-39R fuselage bulkhead w/frame section

8/05/96-70 cl 12 40 39 46.90 -72 37 27.90 FS 1660-1680 stringer 31 R-35R

7l19198 C316 40 39 47.62 -72 37 27.15 FS 1620 frame section from stringer STR 5R-9R

9/30/96-l 40 39 48.40 -72 37 17.00 3.5’ to 4’ plane skin square

7119196 C316 40 39 47.62 -72 37 27.15 FS 1220 frame from stringer 5R-II R

8/14/96-IO 40 39 47.95 -72 37 07.80 FS 940 frame segment stringer 9R-13R

8iO6196-46 40 39 47.00 -72 37 27.90 FS 1060-I 120; stinger 19R-24R, fuselage skin sect w/2 windows,

wo5/96-70 cl 12 40 39 46.90 -72 37 27.90 FS 1820-l 840 stringer 23R-27R with aft cargo door hinge

8/05/96-70 Cl21 40 39 48.90 -72 37 27.90 FS 1840-1960; stringer 23R-26R ,

WO5/98-70 cl 10 40 39 46.90 -72 37 27.90 FS 1620-1680; stringer 36R42R

8/23/96-I 5 40 39 47.04 -72 37 26.90 fuselage skin FS 1680-1700; stringer 42R44R

WO5/96-70 Cl 14 40 39 46.90 -72 37 27.90 FS 1960-2080 stringer 36R-45R bulk door surround cargo

8/23/98-l 5 40 39 47.04 -72 37 26.90 FS 1540-1600; stringer 35R43R

8l23/96-15 40 39 46.89 -72 37 26.59 FS 1540-I 620; stringer 24R-31 R

8/23/98-15 40 39 48.89 -72 37; 28.59 FS 1725-l 820, stringer 44RbOR

w23Kl6-15 40 39 46.89 -72 37 26.59 FS 1760-1780, stringer 43R45R

‘-ti2zim.2’ -- -.-. . . . . . . 4 o I...._. -..-- -... 3g 47.4,

_-.- -.._...___._,._ -.,...-- -72 37 27.64 FS 1760-l 850: stringen 44R48R

8l24l96-7 40 39 46.89 -72 37 28.59 FS 2140-2160; stringer 23R - 35R

i Al.25

GRP # Log # Tag # FBI # Source Tag # Latitude Longitude Deecription (Actual)

4 RF60 Cl049 8ml96-7 403946.89 -7237 26.59 right main wheel welt; FS 1460; (body steering harness included)

RF67 Cl696 8l30/96-23 403946.70 -72 3726.50 FS 920-1000, stringer 29R-34R I

I I I

RF94B c404 8/14/96-9 403947.00 -72 37 29.00 cabin entry door RS, partial structure (window damage distinctive); FS 2240- 2285; stringer 18R-22R

RFSD C2248 813019623 Cl697 403948.70 -723726.50 FS 20182040, with partial window

RW14 Cl94

RW20 23274

6lO8/96-30

9119196-l

403947.00 -723727.90 #7 flap track

403945.80 -723717.40 right upper wing skin 96”x33” adjoins mid spar FS1250

I I I I RW21

I

22806 I

23450 0 39 38.99 -723622.67 right wing upper surface, stringer g-mid spar, WS 1250

V6 Cl656 8I29196-4 40 39 47.80 -723i29.60 mist piece of metal from.aircraft

I , I I I I CW316

I

22798

I

23450 0 39 38.99 -72 36 22.67 right SOB stiffener, 4th aft of SWB #3; 65Bi 1554-16

’ 1

8

CW323 22796 23450 403938.99 -72 3622.67 right SOB web at SWB #l

cw601 (2868 8l17/96-7 403950.94 -72 3723.39 spanwise beam #3 RBL 76-127.5

CW612 Z2794 23467 403951.70 -72 37 25.50 mid spar web RBL 112-l 16, 7’x6

RWl 0 C869 8117196-7 4039 so.94 -72 37 23.39 right LW outboard

cw307 C2370 C668 403950.94 -72 37 23.39 SWB #3 chord with small segment right SOB web attached ,

cw411 22547 23096 403948.50 -72 37 27.00 upper web at rear spar LH SOB

cw710 Z2540 9llll96-4 23061 403948.50 -72

-- 37 27.00 CW spar

CW811 22782 23370 403948.01 -72 37 27.06 portion of spanwise beam CW tank

ON901 - c970 8l2Ol9612 403947.41 -7237i7.64 spanwise beam #lBL 0 - 60 I chord segment

cw904 C2177 C897 40 39 51.19 -72 3722.50 span wise beam #l upper LBL SOB connection -

LFlOB C2255 Cl67 403947.60 -72 3727.90 portion aft press bulkhead FS 2360

fl Al.26

GRP #

6

Log #

LF39A

Tag #

a60

FBI C

8/l 7l96-7

j ,

Source Tag # Latitude Longitude Description (Actual)

0 39 50.94 -72 37 23.39 IFS 1319-1434; stringer 5L-23-L -j

I I I I I

LF7OA Z2518 23096 039 48.50 -72 37 27.00 FS 923-960; stringer 29L-35L with FS 940 frame segment

LW08 C862 8l17/96-7

I

----_.. .., --.-- - ------.- 403950.94 -72 3723.39 left lower.wing & skin WS 1214-1420

---- -...--.. .._. -. ._-._ . ____.___ __, . . . _ _

LWl 0 C859 8/l 7/96-7 403950.94 -72 3i23.39 LWS 1309-1423; left upper wing skin

RF42 C845 8ll6l965 403951.19 -72 37 22.50 FS 1170-l 500; stringer 7R-24R with window belt and door frame

-.--.- RW17 .-- -----

23096 9/12/96-2 40 39 48.50 -72 37.27.00 right hand inboard aileron actuator and support assembly

7 GW218 C2161 C269 403947.00 -72 37 31.00 cw lower skin-left S-l to S-l 5 4

, cW221 23492 g/24/96-16 40 39 50.10 -72 37 30.30 external aircraft skin #i85815697-5 1 approx. O’x8

CW225 22756 23426 403948.47 lower center wing skin panel; RBL 98; stringer 9; Lot # 9-22-96-l

CW227 22753 23426 403946.47 13-14, Lot # 9-22-96-l

I I I I I 02.59

I cw230 22752 23426 0 3948.47 -72 37 lower center wing skin panel mid spar at BLO; Lot # 9-22-96-l

ml234 22757

cw235 22754

23426 403946.47 -72 3702.59 lower center wing skin panel; front spar at BLllO; Lot # 9-22-96-l

23468 403949.70 -72 37 30.50 lower center wing skin panel; RBL 85; stringer M-15; Lot# 9-24-96-16

CW36 22755

1 1 I

23466 0 3949.70 -72 37 30.50 tower center wing skin panel; RBL 57-75; stringer 13-14; Lot # 9-24-96-16

cw712 I

22815 9l211961 23425 403939.69 -72 3620.69 SWB #2, LBL 93.48 web, 9’xl4’H incl fuel hole

LFlOA Cl67 I 1 I I

8KW96-46 0 39 47.80 -72 3727.90 aft pressure bulkhead (approx 50%);

LF82U

LF88G

22646 23494 403949.40 -72 3730.00 FS 1580 segment stringer 34L

22847 23494 403949.40 -72 3730.00 FS 1640 segment stringer 321

RFlOD - % C2235 8/10/96-16 C274 403947.00 --‘--723731.00 FS 1640 frame section

RF26A C274 8/l 0196-I 6 403947.00 ---7237 31.00 FS 22752360 stringer 11 R-23R, aft lower body skin;

lRF27~--.t-------.~~----- -. /-7237310-y---.- FS 2340-2360; stringer 8R-4L aft portion of RHS crown skin

Al.27 I I I I 1 ---.-.--.. l--______L__--- I

GRP # Log # Tag # FBI # Source Tag # Latitude Longitude Description (Actual)

7 RF44B C266 6/1OtM-16 40 39 47.00 -72 37 31 .OO bulk cargo door structure PS I9602060; stringer 23R-46R

RF45C C277 8.‘10/96-16 40 39 47.00 -72 37 31 .OO fuselage skin cargo door surround FS 1920-1960; stringer 27R-34R

-I---..--- RF97 C273

8,10,g6-16 -- ---..---._.....___... .._ _.- ____ 40 39 47.00

. . . . . . -.-.-- - ._. _ _._..... ,__ -72 37 31 .OO FS 18701930; stringer 22R-23R with window frame (fuselage’strip with 3

._ -- _

window frame portions)

8 cw144 22784 23425 40 39 39.69 -72 36 20.69 CW upper skin 5 pieces

cW322 22735 23440 40 39 42.31 -72 36 10.57 CW

9 CW308 22728 23440 40 39 42.31 -72 36 10.57 right SOS web (9-22-96-l)

cw309 22727 23440 40 39 42.31 -72 36 IO.57 right SOB web

cW314 22730 23440 40 39 42.31 -72 36 10.57 SW6 web (9-22-96-l)

CW316 22734 Z+440 40 39 42.31 -72 36 10.57 CW stiffener (9-22-96-l)

CWQIO 22724 9/22/96-I 23440 4 - .

0 39 42.31 -72 36 10.57 SWB #l (9-22-96-I) _-_-

IO CWI 25 22723 Q/21/96-1 22604 40 39 44.36 -72 37 04.63 CW upper skin (9-21-96-I) I

CW807 22720 z%40 40 39 42.31 -72 36 IO.57 CW mid spar

CW808 22719 23440 40 39 42.31 -72 36 IO.57 CW mid spar RBL 87.26-98.59 (9-22-96-I)

cWQ12 22725 Q/21/96-1 22604 40 39 44.36 -72 37 04.63 SWB #I (9-21-96-I t

11 CWI 103 22749 g/28/96-2 23592 40 39 47.20 -72 37 15.16 center wing rear spar to SWB #I ; BLO rib; Lot # 9-28-96-2

CWI 104 22702 9/22/96-l 23362 40 39 48.04 -72 37 22.06 spanwise beam web

CWll8 z3035 9/08/96-2 40 39 45.30 -72 37 23.70 15’ long structural member

cw122 23347 _-_- -.-..___ ----__

9/l 9196-l . ---. .-.-----_-.--I__

40 39 44.50 -72 37 13.30 CW upper skin M.S. to SWB #x?%xzBL 96 -._----_ --..

CWI 23 . 22674 23347 40 39 44.50 -72 37 13.30- --’ i&??:i’i;&$ii$i- -- -- .___l_._l- ~ ---_- .---_....-. -_

CWI 24 22675 9121196-l upper center section stringer, LBL 11.3 - RBL 76

CW126 22722

11 c i ‘) ,I

Lstltude GRP # Log # Tag # FBI # Source Tag # Longitude Description (Actuel)

CWI 29 22747 ZXG! 40 39 47.20 -72 37 15.16 center wing left SOB-LBWO; upper hand STR22-27 -3

cW220 22673 23352 40 39 49.02 -72 37 stringer 25.09 CW 22 RH end ---.

---~--3~-- -.- “.&.-+ -. ..- --.......---_.. . . . 23360 4Oj948.50 -72 37 22.70 possible CW lower skin

cW313 22732 BkV 40 39 46.40 -72 37 26.80 CW SOB rib

cW315 22685 23352 40 39 49.02 -72 37 25.09 right hand SOB stiffener

CW325 22805 23451 40 39 46.40 -72 37 26.80 --right SOB rib lower chord at SWB #I segment

CW328 22827 9/22/96-l 23358 40 39 49.00 -72 37 25.05 RH SOB rib 13” of - portion iwr chord FS 1039 1052

CW329 22828 9/22/96-l 23358 40 39 49.00 -72 37 25.05 RH SOB rib 24” portion of iwr - chord FS 1058 1082

cW333 22829 9/22/96-l 23358 40 39 49.00 -72 37 25.05 RH SOB rib 26” of inbd 8, outbd mipspar stiffener

CW607 22506 9/09/96-49 23105 40 39 47.25 -72 37 21.90 CW tank piece

cW711 23259 9/l 9/Q6-1 40 39 46.90 -72 37 16.00 misc. metal pieces t

CW816 22780 23010 40 39 47.25 -72 37 21 .QO portion of spanwise beam CW tank

CW908 22679 9/19/96-l 23347 40 39 44.50 -72 37 13.30 SWB #I stiffener free flange

H5 23338 Q/l 9/96-l 40 39 44.50 -72 37 13.30 large wing section with window

LF42E c391 8/l 4196-g 40 39 46.50 -72 37 28.00 FS I QOO-1960; stringer 49L-51 R

LF63 22519 23037 40 39 45.30 -72 37 23.70 skin segment FS 960-1000 stringer 27.5L -31.5L I

LF65 22659 9/09/96-49 23037 40 39 45.30 -72 37 23.70 FS 1080 stub beam at side of body LHS

LF80 Z3256 9119/96-l 40 39 46.90 -72 37 16.00 main entry door L3

LF82G \ C2437 6l26/96-36 C714 40 39 46.40 -72 37 27.80 FS 1620-1680 stringer 48L-5OL

LF86G C2427 C714 40 39 46.40 -72 37 27.80 FS 1416-1438 stringer29L-31L

LF86J C2438 a/26/96-36 -72 37 27.80 FS 1470-1480 stringer 28L-30L

----..--.. - .-_ -----.- _-__- .____ -- -d Al.29

> ! i GRP# Logiy Tag# FBlt SourceTag# Latitude Longitude Deecrlptlon(Actuel)

II LF87H -- 22859 --I__-- ---.--

Qto9tQ6-49 23037 403945.30 -723723.70 FS 920-940 stringer 28L-29L

I LF87l Z2845 23037 403945.30 -72 3723.70 FS 990 segment stringer 31 L-32L

LFQI 25112 1 O/30/96-2 403948.40 -72 3724.50 FS 1000 lower ring chord stringer 34L-35L; mist items, details on hard many COPY

LW40 22538 9/l 1196-4 23084 403945.20 -723722.70 left lower wing skin; WS 1120-I 180; stringer 5-7

LW41 22517 9tOQt96-49 23037 403945.30 -72 37 23.70 left lower WS rear wing skin; 1140-1210; spar stringer S5

I I I I I LW44 1 23364 1 g/22/96-1 )

I 1403948.70 j-72 37 25.50 left lower wing skin (6x8’); WS 1335-1450; stringer s4 to mid spar

LW47 23025 9/08/96-2 403947.25 -72 37 21.90 left wing aileron (o/b) 3x4 segment

LW50 22544 9/I 11964 23084 403945.20 -72 3722.70 left wing spoiler #5 with actuator

R5 23034 9/08/96-2 40 39 47.25 -72 37 21 .QO cargo portion rudder net full of debris; of

RFIIIB C2429 C714 40 39 46.40 -72 37 27.80 FS 1540-1580 stringer 42R-44R

RF77 22505 23046 403947.25 -723721.90 FS 1120-l 140, 23R-27R stringer

RW22 23007 --- Q/08/96-2 40 39 47.25 -72 37 21 .QO right hand HF antenna assembly approximately 8’ long

12 cw203, CWI 005

CW204, CWI 007

Cl93

Cl59

8tO8tQ6-30 40 39 47.00 -72 37 27.90 lower CW skin; STR 1-3; LBL 60-I 3

40 39 47.00 -72 37 27.90 lower CW skin - STR R.S. LBL 104-62 -3;

) CW306 1 Cl96 1 /-72- 8tO8t9630 1 k 0 39 47.00 /right cw body rib in-between rear spar and SWB #1

LF86D C2425 C714 40 39 46.40 -72 37 27.80 FS 1438-1460 stringer 26L-27L

13 cw1022 C2372 8tllt96-1 CO37 4039 49.51 -72 37 14.83 rear stiffener at RBL 21, complete spar

WV709 C2265 8/11196-l CO39 403949.51 -72 37 14.83 intercostal between beam #2 to #3

I I I I ,

CW802 . c2164 CO38 0 39 49.51 -72 37 14.83 mid spar-lower web piece LBL 66-87

FS 1394.1880fuselage; strlnger26L.12R

6. L.0 keelbeamweb(wheelwell)FS1460-1480

Al.30

GRP #

13

Log #

RF33J

Tag #

Cl207

Cl080

FBI # Source Tag # Latitude Longitude Description (Actual) ----- --.----_---_-- -.___..__ -.--.--_ .___ .__.__.___.__

6/26/96-36 40 39 46.40 -72 37 27.80 stage skin FS 1780-1800; stringer 34R40R

8/26/96-36 40 39 46.40 -72 37 27.80 FS 1900-1940 aft door cargo surround; stringer 41 R-44R

_I--

t- LW42

RW25 23129

RW9

! 15 CWlOl8

cw1019

co40

22766

I I I I I Z2767 1 O/03/964 23270 0 39 46.76 -72 37 14.05 LBL 66; rear spar web skin segment with 2’ of stiffener

LF87C ’

22769 1 o/03/964

22758 9/20/96-33

I.. 1480-1570;

.__ . FS stringer 36R45R with’body landing gear trunion

.... ... .. .-. -.-I-...--- .. _ “, - ... ... . ....... .. ..- .- LBL 66; rear spar web segment with sbffener flange

. ......

I I I I I 22772 1 9/30/96-l 1 23130 /40 39 46.60 I-72 37 18.60 CW tank rear spar LBL 85 stiffener

23211 9/30/96-l 40 39 45.90 -72 37 18.40 8’ to 9’ piece of metal w/yellow exterior paint

I I I ) 1 PO

-- ---_. -t -72 37 18.40

. .___._______I_I___.___ - ..__..__ ._ .__-_._-.-.- ._.._ -...-._ _. ..-- __ .._ -- 22771 1 O/03/964 23208 39 45.90 t- CW tank upper skin segment

.-. . -.---I.- - --...-.-....--..---.-..... ..-- - ----..-.. skin -- segment@ LBL 106, stnnger T 2

-.- CW tank upper

23126 9/l 01964 _.- . --_-- __.---- ..-_-.- ._ .._..._.. -..-..-

40 39 46.90 left upper wing skin (3x10’); WS 1200-1330; stringer 5-12

9/l 01964 40 39 46.60 -72 37 18.60 11’ long, narrow angular piece with rivets - green color

8ll1196-1

1 o/03/96-4

40 39 49.51 -72 37 14.83 15’x4.5’xl.S green metal: right wing with skin

23270 40 39 46.76 -72 37 14.05 LBL 70; rear spar segment upper web at chord with 8” piece of stiffener

23270 40 39 46.76 -72 37 14.05 CW tank upper skin segment with piece of spanwise beam and chord

23277 40 39 46.76 -72 33 14.05 fuselage skin under body fairing; Lot # 9-20-96-33

I I I I I

22751 z3550 0 39 47.11 -72 37 13.88 lower center wing skin panel; LBL 100; stringer 2; Lot # 9-27-96-l

I I I I

) 23397 ]40 39 49.70 j-72 37 27.30 /CW lower skin

b 22729

---__ -- 23397 4 0 39 49.70 -72 37 27.30

_--- t- right SZB web (9-23-96-5)

22717 23397 40 39 49.70 -72 37 27.30 terminal fitting rear spar wing

--.-.-----..--.-.--__. ..- ..___ ______ Z2714

___~ -.- . ..__-__-_--__ .-.-._ 23397

-- 4 0 39 49.70 -72 37 27.30 CW stringer

Al.31

GRP # Log I# lag t FBI # Source lag # Latitude Longltude Description (A&al)

16 cw413 22677 23277 4 -_--__-

0 39 46.76 -72 37 14.05 -_-_.___~_~._--

LH SOB rib RS

--- .-__ _.- WI---_---_-. ., --.--_ _..._.- - .-._ -... .-. . . -. .* ._. ._. cw414 22676 Z3277 40 39 46.76 -72 37 14.05 LH SOB web forward of rear spar - ‘- .-.‘.

CW613 Z2712 -.-.-

23397 4 ----.-.-- -..-._-._-_

0 39 49.70 --- ----_-. -- _-.. -.- .-.. ---- -_

-72 37 27.30 spanwise.beam section

17 CW226 --_ -

22709 -__-.. .-. .___._ .-.,- ._..... .- _

23397 4 __,.. . .____. --. __... . .-. ._-. . . . . .- _.

0 39 49.70 -72 37 27.30 CW lower skin‘

CW228 22710 23397 40 39 49.70 -72 37 27.30 CW tower skin

CW814 22711 23397 40 39 49.70 -72 37 27.30 spanwise beam section

18 cw1014 22656 9J20/96-33 23090 40 39 45.20 -72 37 25.50 LeR butt line 98 rear spar stiffener

cw1015 22652 23090 40 39 45.20 -72 37 25.50 Aft leff rear spar pickle fork, upper rear spar kik fitting

cw115 23089 9/l l/96-4 40 39 44.75 -72 37 26.20 CW upper skin M.S. to SWB #l, LBL 45 - LBL 98

cw149 22788 23090 40 39 45.20 -72 37 25.50 upperCWtank=skin Q side of body 4” X 6”

LF67B 22548 9/l 2J96-2 23092 40 39 45.40 -72 37 24.80 MED 3L cutout skin, lower part FS 1250-1241 stringer 24.5L-28.5L

LF87E 22760 9/l 2l96-2 23090 40 39 45.20 -72 37 25.50 stringer 34; Lot # 9-12-96-2

LWl2 C886 ww96-6 40 39 46.15 -72 37 26.49 tower left wing skin; WS 525-690 I

LWl3 C894 8l18J98-6 40 39 46.15 -72 37 26.49 left lower wing skin WS 520-660

I LW22

. .

C887 8J1m6-6 40 39 46.15 -72 37 26.49 #3 left flap track and carriage assembly

LW23 C906 8119J96-22 40 3946.15 -72 37 26.49 --

left wing #l flap track

LW33 C888 8/l 6196-4 40 39 46.15 -72 37 26.49 left wing outboard aileron section and wing bulkhead WS 1325-1390

19 LWl 1 C884 8l18J96-6 403946.15 -72 37 26.49 left wing lower skin; (WS 650-1035; midspar to front spar)

-_. ----__ -- LW27 ’ C881

-- .-.. -I..- .._.....-._ - -_-.- -..-.-_- .._. -.- _____.__._.__.____ __ 8/l 8196-6 40 39 46.15 -72 37 26.49 left wing up skin: LWS 586-688; from STR 10 to midspar

upper CW skin: LBL 72-93; stringer 12-13; this part is part of CWl13 8

LH BL127.5 (SOB) rib stiff at mid spar (lower half) o/b wing side 65811557-3

. Al.32

, ! ,j

GRP # Log # Tag # FBI # Source Tag # Latitude Longitude Description (Actual) ’ - 20 CW4076 C2266 , I--_-. . ..-. _..- .-.I. ---_.. -..- . .._-_ . - c88 403946.15 26.4g ,.‘-.-. .-:7j137 ..-._..-.-.. -..- _- . ..._” ” ..-. .._..-._ . . - .-..-.-.__..___-..._ _ .___.__.._._._._.___ _

LH BL127.5 (SOB) rib, stiff at MS (upper half) o/b wing side 65Bl1557-3

LWO9 C876 ----- -- ------_ -... -.--.- - . . . . ..--. -.---- - _ - .-..... -. 8117196-7 .~~.-~~--_--.----__-._-._ 403946.15 -72 37 26.49 left wing lower skin LWS 1030-1230; front aft to Sl spar

LW20 C2230 8/l 9196-22 C863 40.3946.15 -72 3726.49 left lower wing skin panel segment; WS 860-902

IN26 c2264 6/l g/96-22 C863 403948.15 -72 37 26.49 left wing skin: WBL 470 to WS 791 from midspar to STR 17 upper up

LW28 C2261 8/19/96-22 C863 403946.15 -72 37 26.49 left wing skin; LWS 499-528 from STR 4-7 upper

21 cw107 C2023 8118196-6 C891 40 39 46.15 -72 3726.49 stringer 7-13; left hand splice body to center wing LBL 127.5(C891) upper

CWIII C22;6 8118196-6 C879 403946.15 -72 3726.49 upper CW skin; LBL 107.5-I 18.5; upper STR 3; center fuel tank

cw112 -- ----’ c2229 40 39 46.15 -72 m--- -.---

C921 upper CW skin piece; LBL 6-29 stringer 20-21

cw509 C2016 C912 403946.15 -72 3726.49 front spar LH terminal fitting piece

LWl4 C2017 8/19/96-22 C863 403946.15 -72 37 26.49 left lower wing skin; WS 660-734; stringer S5S8

22 cw106 C2007 C880 403946.15 -72 3726.49 center wing tank skin stringers 3-6 upper

cw109 C2014 C873 403946.15 -72 3726.49 CW left hand splice stringer 17-28 upper

LWl9 c2010 B/i g/96-22 C863 403946.15 -72 37 26.49 left upper wing skin LWS 870-725 with front spar to S23

RF51 c2002 8/l 8196-6 C891 39 40 46.15 -72 37 26.49 FS 920-1000; stringer S 24-28 (C891)

23 Cw215, C251 8/08/96-30 403950.14 -72 37 27.24 Cw503,

front spar RH terminal fitting/jack point #2; right hand lower panel; contains

- RWOZ : jack point #2; this part is part of CW215, RWOZ, 8 CW503

CW223 22168 C256 403950.14 -72 37'27.24 rear spar CW tank Q RBL 127, was cut from lower right wing I

Cm303 c239 8/09/96-37 403950.14 -72 37 27.24 Rl4 #5 CW Body Rib. SWB #2 to mid spar

H3 Cl028 8muQ6-15 403946.89 -72 37 26.59 piece of horizontal stabilizer .

LFISA, c259 8/09/98-37 403950.14 -72 3727.24 RFOSC

FS 2100-2160; stringers 22L-30L

LF26 C255 8109196-37 403950.14 -72 37 27.24 FS 2285-2360; stringer 8L-24L

RF47A C885 8/06/96-30 4039 50.14 -72 37 27.24 FS 2530 -2618 stringer 23R - 49L

Al.33

‘t .

,

,I !

/ GRP #

-.

Log # Tag # FBI # Source Tag # Latitude Longitude Description (Actual)

23 RW30 C260 we-

8/oQ/98-37 ,.---II-----. . - ._.- -. ..-.

403950.14 -72 .-....-.--.. 3727.24 _ , - -_ _. ._ _ -. _

flap section

24

RW6 C258

CWIOI C808

cw1010 C2138

8109/96-37

8/l 5196-8

8/09/96-?

403950.14 -72 37 27.24 ---;‘-~---r-~~~-- --- -.-----*. ~:‘-"-‘- .-..--. - -.-..-.. - - . ._... -_ ._ ._ ._.. ._. ._.___. right lower wrng skn, SOB nb, brear

__ stnnger spar

403947.40 -723724.60 top fwd, right and center; stringer 22 to front LBL 33 to RBL spar; 127.5

C233 403950.14 -72 3727.24 rear spar RBL 1 I-80 web Q lower chord -

,

CWI 16 C2166 918196-30 C224 403950.14 -72 37 27.24 cw stringer

CWIlQ C2167 818196.30 C224 403950.14 -72 37 27.24 cw lower skin stringer

CAN206 C2160 I

C223 403950.14 -723727.24 cw lower skin-left side mid spar to S13: left SOB to LBL 104

cw209 C2169 C224 403950.14 -72 37 27.24 lower CW skin; STR 14-15; RBL 30-80

cw219 c2159 C240 403950.14 -72 37 27.24 lower cw skin&d left corner

cw903 C2131 C224 403950.14 37 -spanwise -72 27.24 beam #l-lower RBL 53 to 66

RF28 C217 8/08/96-30 403950.14 -72 37 27.24 R3 main entry door

RWI 1 C804 8115196-8 403947.40 -72 3724.60 right hand upper wing Segment, front to mid WS spar spar 1186-1280

( 25 LF40 C802 1 8115196-8 403947.40 -72 3724.60 BLO web body gear wheel well

RF55B C603 atI 5196-a 403947.40 -72 37 24.60 FS 2638-2709, stringer 7R4L

26 cw1003 C2143 8108196-30 ci a3 40 39 49.60 -72 37 28.10 rear spar RBL33 to RBL67

cw1004 C2139 Cl83 40 39 49.60

-h -723728.10 rear spar web RBL-21 -LBLll

cw1011 C2145 Cl83 403949.60 -723726.10 rear spar right side RBL 70 to RBL 33 at lower chord

cw1012 c2144 #09/96-31 Cl83 403949.60 -723728.10 rear spar RBL85

cw105 , Cl88 8/08M-15 403949.60 -72 3728.10 upper CW skin; RH side R.S. to STR 19

cw202 Cl86 8/08/96-15 403949.60 -72 37 28.10 lower aft CW skin Sl to S5; LBL 76 to RBL 98

- RF37, C601 8/15/96-8 -.. .-- cw517 40 39 47.40 -72 37 24.60 FS 930-I 065; stringer 1 OR-27R; CW front spar - RH web and stiffener with window frame (upper RH comer) see CW517; this part is part of CW517 &

%RF37 Al.34

I

GRP # Log # Tag # FBI W Source Tag # Latitude Longitude Deacrfpffon (Actual)

27 RW3 1 C185 181(38/96-15----- --.. ..-. --- .-- ..--.-.. 7 T3T49.6. 1-723728.10 - -- ., r riQht .‘. .” -‘--‘-..._- winQ,part of ruserageFs --.-..-.-- .i’jiK;3.i ---- .- .__.._ - -__... -.-. ._.__.

I ,

RW8, I

cl83 a/08/96-1 5 CW803 40 39 49.60 -72 37 28.10 right wing/part of fuselage FS 1140-1319; mid spar upper SOB paddlelfittinghnreb; right wing upper skin cut into 3 pieces - see C2281 and

28 LF45C C2256 al29lQ6-4 RF1 7; part of CW803 & RWO8

Cl672 0 39 47.80 -72 37 29.60 FS 1480 bulkhead outer cord

I LF82S C2417 Cl 656 40 39 47.80 -72 37 29.60 FS 1690 segment stringer 43L44L

29 LF73C

RF104

RF71

c2220 8l29l96-4

C2218 8/29/964

C2215 8l29196-4

I

Cl682 40 39 47.80 -72 37 29.60 FS 2436-2484; stringer 17L-23L

Cl700 40 39 47.80 -72 37 29.60 portion of fuselage

Cl700 40 39 47.80 -72 37 29.60 FS 1480-1500: stringer lOR13R

RF94A c2222 8l29lQ6-4 Cl684 40 39 47.80 -72 37 29.60 cabin entry door R5 upper flap seal (upper gate #5R door FS 2261); stringer 17R

RF94C C2207 8129/96-d Cl684 40 39 47.80 -72 37 29.60 cabin entry door R5 lower section; FS 2240-2285, stringer 24R-25R

30 RF56 c996 8&!/96-5 40 39 47.24 -72 37 27.28 FS 2180-2240; stringers 36R-44R

RF93 C2206 al29l96-4 Cl684 40 39 47.80 -72 37 29.60 FS 2320-2340; stringer 20R-21 R

31 RF45F 8lW96-5 40 39 46.89 -72 37 26.59 aft door lower aft section cargo

RF52A C646 8lW965 40 39 46.89 -72 37 26.59 lower belly skin

32 LF51 c642 8/22&6-5 40 39 46.89 -72 37 26.59 FS 940-l 000; stringer 35L-39L with piece of bulkhead under wing front spar

k- LF78 LF52 * c370 C611 8/14/96-9 8/22/96-5 40 39 47.35 -72 37i27.06 FS FS 2020-2160 1680 frame stringer 41L - 45R

segment; stringers 4L-12L

LF79 C388 8/l 4196-Q 40 39 47.35 -72 37 27.06 FS 1860 frame segment; stringer 6L-15L

33

RF96 c364 ---- 8/14/96-9

- 40

- J 39 47.35 -72 37 27.06 FS 1800-1848 stringer 22R with two windows (fuselage bulkhead, w/window

LF82E -

fragment)

C315 8l14/96-9 40 39 47.35 -72 37 27.06 FS 1540-1560 stringer 34L40L; interior bulkhead fragment l’x2

I RF526 C365 8/14/96-Q 40 39 47.35 -72 37 27.06 fuselage bulkhead fragment

) 34 CWIOIG 23297 9iNQ6-1 40 39 49.03 -72 37 27.01 inboard leg CW tank left hand pickle fork rear

I’ I I I I I I ’ Al.35

) 1 !

GRP # Log # lag # FBI # Source Tag # Latitude Longitude Description (Actual)

34 WV1017 22726 Q/20/96-33 f3280 403946.40 -72 37 26.10 CW rear spar stiffener and web -LBL 98 (Q-20-96-33)

CW104, C2151 cw301,

C729 403946.40 -72 3727.80 upper right fwd CW skin, double plus chord , STR 19-30; also a portlon of right SOB CW rib (CW301); also upper CW skin right hand side SIR 19-30

Cw707 $XV104); spatiwise beam #2 RBL127.5 upper paddle fitting/web (CW707); this part is part of CW3Cll &CWlO4

cw131 c2391 8/19/96-22 ca63 403946.15 -72 3726.49 -- CW upper skin LBL 98 Q S-16

CWl32 22823 Q/20/96-33 23277 403946.76 -72 37 14.05 CW upper skin LBL127; S-2 to R.S.

cwl33 22822 Q/20/96-33 23277 403946.76 -72 37 14.05 CW upper skin LBLl27; S-2 to R.S.

cw145 is785 23277 403946.76 -72 37 14.05 CW upper skin, 10 pieces

CW146 f2787 23295 403946.40 -72 37 26.10 CW upper skin tension fittings Q SWB #i, 3” X 6” LBL 98

cw147 c2382 C863 403946.15 -72 37 26.49 right side CW upper skin

cwl48 22737 23440 4 -v-e--

0 3942.31. -72 36 10.57 ~-~

CW upper skin ~I_I

cw210 c2149 c729 403946.40 -72 37 27.80 lower CW skin; left SOB to LBL 100; R.S. to STR 3; (wing center section, lower skin segment, 20” x 16” fits at intersection of rear spar and Left side of

CM216 c2i48 -body)

Cl08 40 39 46.90 -72 37 27.90 lower cw skin- right fwd side S21 to 523

cw224 22750 z3298 403946.08 -72 37 26.07 lower center wing skin panel; LBLl27; stringer 2-5; Lot # Q-21-96-1 1

cw317 22795 23295 403946.40 -72 37 26.10 right SOB web- just below CW310

cw405 C2373 c863 403946.15 -72 37 26.49 left SOB rib stiffener free FLG + web - 14” long

cwao9 23550 9/27/96-l 403947.11 -72 37 j3.88 large metal piece

cwa20 22793 z3295 403946.40 -72 37 26.10 mid spar web, LBL 97-105,9x12

cw902 ca97 8/16/96-5 ca45 403951.19 -72 37 22.50 spanwise beam #l- LBL 60-100 web segment

cwQo6 ~ 23272 -

9/N&6-1 .--._ -.__^

40 39 46.50 ---- -72 37 14.50 ----

CW SWB #lBL 0 - RBL53,5 stiffeners8 access door

cw909 22741 Q/22/96-1 23440 403942.31 ----7236 lo.57 portion of spanwise beam #l upper chord

--I-.- .------. -- .- ._.. -.- _...._.__._.. CW916 22810 23451 4

..--..-- -. _.I_. - . ..- -I_ -_...- I- -.-. ..-_.__ __. 0 3946.40 -72 37 26.80 SWB #I web right hand closure panel

--.-.. ------

Al.36

GRP # Log # Tag # FBI # Source lag # Latitude Longitude Description (Actual) . .- -.. _-_-_- 34

,

w/917

37 26.80-

--. ---- -------_-----I- r __._. --__.._. 22811 23451 4 o 39

46,40

-72 SWB #I web right hand closure panel

!

LE2B _-.----.-.- -.--.-.-_ --...... .._. -._. -. - ___.. __. ..,__ .

Cl078 8i26/98-36 40 39 46.89 -72 3726.59 LE2B is of LHS outboard elevator from ES FS .. portion 335-385

LFlM _._.-...--.-. --.- -I.-- -- --.-.--- ..- - . -.___. -... . .I.-.--..- ._-- -.---. .- ____,..... - ._ _ ._.

Cl20 B/05/96-70 403946.90 -72 37 27.90 FS 2000-2120; stringer 8L-22L with window belt

LF13B Cl39 ___.- -... --.-.-- -- ..--.. -.. . ._.^ __ -. .._. .. _-_-_.. ..-.. . ._. . -

403947.00 -7237 27.90 FS 2120-2180; stringer 13L-22L with window belt

LF14D

LF16A. cw1002

LFlGB, CWI 006

LF17

LF27B

LF27D

LF27E

LF28B

LF35D

c2440 8iO5/96-70 Cl14 403946.90 -72 3727.90 FS 1466-1480 keel beam segment

C2146 Cl08 403946.90-- -7237~--- ------- -z--

part of CW1002; Note: saw cut separates part into two preces; fear spar RBL- 0-RBL76

C2136 Cl08 403946.90 -723727.90 part of CW1006; Note: saw cut separate part into two pieces; rear spar web LBL21-LBL57 ._

Cl09 8/04/96-111 403946.90 -72 3727.90 BL 0 keel beam center web from FS 1330-1241

Cl46 8iO6i96-46 403947.00 -72 3727.90 Left FS 1760-1800. S25L -31 L

Cl49 8i06i96-46 403947.00 -72 37 27.90 LF FS 1840-l 940; Stringer 22L - 30L

C2354 8iO6i96-48 Cl46 403947.00 -7237 27.90 FS 1820-I 840 stringer 31 L-34L I

Cl47 8iO6i96-46 403947.00 -72 3727.90 LF FS 1980-2020

C2385 8i26i98-36 C739 403946.40 -72 3727.80 FS 2160-2200 stdnger 35L42L

LF39B

LF42G

Cl12 8io5/98-70

C2174 8i26i96-36

403946.90 -72 3727.90 FS 1350 frame stringer 22L-29L

Cl098 403946.40 -72 37 27.80 FS 1916-1960; stringer48R-51R

LF42H C2386 I I I ,

8i26/96-36 c739 0 39 46.40 -72 37 27.80 FS 1720-l 750 stringer 45L48L

LF48

LF66

LF76

LF77

LF82B

Cl48

C2322

l C2346

C2347

C2408

a/06/9646

8i26/96-36

a/14/96-9

8i22i96-5

--- 403947.00 -72 37 27.90 mist fuselage skin sect wi red paint; FS 1960-2020; stringers 30L - 37L

t

Cl080 403946.40 -72 37 27.80 LHS fuselage FS 1416 segment

c370 403947.35 -72 37i7.08 FS 2484-2598; stringer 23L-42L

C651 0 3946.89 -72 3726.59 FS 1800 frame segment: stringer 6L-14L

C863 10 39 46.15 ~~~~trfnger - 38L-41 L Al.37

/

GRP # bzI# Tag # FBI C Source Tag # Latitude Longitude Dwcriptlon (Actual)

34 LF82H C2403 C863 4 -w--e--

0 39 46.15 -72 37 26.49 Fs 1630~1660 stringer 39L4, L -.-.-.- --.I--- - -..-.--.-..-- --.--.--

LF82J C2407 c714 4 --- .-.--.- ~

0 39 46.40 -72 37 27.80 FS 1660-i 680 stringer 41 L-44L

LF82K C2411 c714 40 39 46.40 ---

-72 37 27.80 FS 1800-1820 stringer 45L48L ‘I-.- -‘------- --.._----.---

LF82L C2412 C714 40 39 46.40 -72 37 27.80 FS 1630-1660 stringer 4lL43L

LF82P C2415 c714 40 39 46.40 -72 37 27.80 FS 1550-I 560 stringer 45L48L #

LF82R C2418 Cl674 40 39 46.70 -72 37 26.50 FS 1625-I 635 stringer 40L

LF82T C2418 C863 40 39 46.15 -72 37 26.49 FS 1500-l 540 stringer 26L-28L

--------.---.-.--. ---- -.------._.- - ..^ _--- ̂ -.-.. --- .- .-..... - ..---..._ _ __.-. _ ._.-. --__. LFSBA- C2422 c714 40 39 46.40 -72 37 27.80 FS 1394-1420 stringer 23L-26L

LF86B C2423 c863 40 39 46.15 -72 37 26.49 FS 1394-1420 stringer 26L-28R

LF86F C2426 Cl674 40 3946.70 - -72 37 28.50 . FS 1438 segment stringer 29L-31 L

LFBBH c2428 C306 4 0 39 47.60 -72 37 27.10 FS 1420 segment stringer 24L-25L

LF87D C2333 Bi22f96-5 C605 40 39 47.24 -72 37 27.28 --.--

FS 960-980 stringer 34L

LF87F 22779 9/21/96-1 23298 40 39 46.08 -72 37126.07 fuselage skin under body faking; stringer 37L; Lot # 9-21-96-1,

LFBBB 22846 23391 40 39 49.35 -72 37 27.93 FS 1560-l 580 stringer 35L-37L

LFBBC c2442 8/l 9/96-22 C863 40 39 46.15 -72 37 26.49 FS 1560-I 580 stringer 37L-39L i

LF88E C2436 Cl674 40 39 46.70 -72 37 26.50 FS 1660-1680 stringer 34L-37L

LFBBK 22861 9/20/98-33 23277 40 39 48.76 -72 37 14.05 FS 1840-1660 stringer 34L-35L

LFSO 22825 g/20/96-33 Z3277 - 403946.76 -72 37 14.05 FSIOOO ring chord segment with stringer 37L end fitting

LF93 6 22833

j -‘ GRP # Log t lag 1 FBI # Source Tag # Latitude Longitude

---_ - 34

I 1

-----..-... - _-_. LWO7,

c ;---..- . .

cw106, I

.------- Description (Actual)

. .._. _ ._.. ._,___ wow96-70

I

- . I. . . . -72 37 27.90; ieft upper wing’skin;

--.. -.. SOB to V&L 260; part of CWlo6, LW67, ‘8 CW4dl

I - cw401 !---- ' I I - ..-_ -. _..._ I -- . .- . . - _. _ - I .-.-...-.-..-- -.-..... -.. .-.-...-. .._I _.___.__.__ _.__ -.--1 -- . . .._.... -- .- -_... _ .______.I_ - -. _

1

LW29C C2380

6/19t96-22 c910

0 39 - 46.15 -72 3726.49 left upper wing skin WS 766780; stringer 24-25 ------i I I

LW35 I

c222 I

8tO8t96-30 I I

0 3947.00 -72 3727.00 leff wing -outboard section of the inboard aileron

LW49 C23i6 WO4196- 111

Cl08 403946.90 - -723727.90 left wing outboard tip HF antenna portion - ---- -__.-.---

RF100 c2341 6tO4/96-111 Cl08 403946.90 -72 3727.90 FS 1982-2020 36R-39R; section of aft bulk cargo door

RF101 C2342 8tO4t96-111 Cl 08 40 39 46.90 -723727.90 FS 1980-2010, stringer 38R; handle from aft bulk cargo door

RF102 C2124 I I

8t23t96-15

I Cl006

P" 3g 46.8g I -72 3726.59 Iright hand side aft bulk cargo door lower section

I I

I I RF1 09A c2379

I I 8tOSt9670

I Cl12

I 0 39 46.90 -72 3727.90 FS 1610-1640 stringer 37R40R

RF1090 Cl069 8t24/96-7 403946.89 FS1620-1660 stringer 30R-33R

RFlOA(1) c2419 6t26/96-36 C714 403946.40 -723727.80 FS 1520 frame stringer 5R-8R

I RF1 OA(2) C2421

8t26t96-36 c714 4 0 3946.40 -723727.80 I

FS 1620 frame stringer 14R-20R

RF106 Cl15 8tO5t96-70 403946.90 -72 3727.90 door (R4)

RFlOC C2236 8lOW96-70 Cl10 403946.90 - -72 3727.90 FS 1630-1680; stringer 22R-30R, with R4 door structure

RF110 23298 9mt96-1 403946.08 -72 37 26.07 FS 1700-I 760; stringer 26R-28R

RF1 1 IA C2424 Cl674 40 39 46.70 - -72 37 26.50 FS 1560-1590 stringer 49R-5lR

RFlllD C2430 Cl674 403946.70 37i6.50 -72 FS 1620-1640 stringer 42R-45R

RFlllE C2431 Cl674 403946.70 -72 3726.50 FS 1560-l 590 stringer 32R-34R

RFlllF --%52 -------.----_.-- .______.._

C863 4 o 39-%.ij-- --.- -72 3726.49 30R-32R~ . ..---- --.-.-- - FS1nger --

RFlllH 22853 23391 403949.35 -72 3727.93 FS 1540-1580, stinger 23R-24R

RF15 Cl17 403946.90 -723727.90 FS 2280-2340 includes saw cut RF9NB

L “_- --____.-- -- Al.39

\ \ - /- .I 1 GRP# Log # Tag # FBI # source Tag t Latitude Longltude Description (Actual) I 34 RF22 C2334 cl 12 40 39 46.90 -72 37 27.90 FS 1480-1580, stringer 19R-26R with window frame

L--.-. RF26B Cl10

--_- --- 8/05/96-70 40 39 46.90 -72 37 27.90 FS 2200-2310 stringer 21 R-38R, cargo door right bulk side lower

-.-~

4zr-L 1.3 ;;:C3; FS 1660-l 700; stringers 40R-f13R

I

4’; ;3.223;

FS 1640-I 740; stringers 43R-51 R and 51 L49L

RF33i-i ’ I C2244 a/14/96-9 cl 10 40 39 46.90 -72 37 27.90 FS 1720-l 820; stringers 49L-51 L, 51 R

j RF331 C2243 8/l Z96-3 ‘3 10 40 39 46.90 -72 37 27.90 FS 1620-1680; stringers 45L-51 L,51 R

RF36 Cl42 -..----A_

8lO6f96-46 09 f

47.00 -72 37 27.90 mist fuselage skin sect wl red paint; FS 1080-l 120 24R-27R stringer

: RF39A Cl23 atoww-70 40 39 46.90 -72 37 27.90 bulk door structure FS 1960-2080; cargo

10 39 46.90 -72 37 24.90

FS 1960) stringer 23R45R (Fuselage skin;

RF40 C2330 8105/96-70 Cl14 FS 1480-i 520 stringer 26R-30R, from lot # 8-5-96-70 ,---I *

RF44C C2277 .-_---

a/05/96-70 Cl12 k ~ 0 39 46.90 -72 37 27.90 FS 2040 stringer 32R-33R

RF44D C2348 ‘8/05/96-70 -._-_.-._-_ .- I-.-----.-. Cl23 i” 0 39 46.90 -72 37 27.90 FS 1960-I 980; stringer 28R-31 R

RF44E c2349 Cl23 40 39 46.90 -72 37 27.90 FS 2060-3000; stringer 29R-36R

RF45A Cl22 8105196-70 !:: 812396-l 8/05/96-70 5 43 locks

RF45D

RF45G

C2335

-_ &2133

---___

Cl 14 40746.89 40 39 39 46.90 46.90 -72 -72 -72 37 37 37 26.59 27.90 27.90

_ -._._ --.-_-

aft FS aft cargo cargo 1760 stringer door door fragment - lower 42R43R sill latches &

J \ / 1 ; w__,--

GRP # Log # Tag # FBI # Source Tag # Latitude Longitude Description (Actual) 34 RF52E c2094 8/22/955- - . ..-- ---.. ---.-.-

C607 -I.._ _... - ---_._...- 40 39 47.24 -72 37 27.28 - _________.__..._..__ _ ____ __.. .-.. - .--....-. -- ..--._... .-.. - _--- -.-.-- ._..... - .._. rFs beam”. ---- ski” rear be,,y kee, i

_- RF52F c2439

-__ c932 -..-.- --- .I-- -- 4 0 39 47.36 -72 37 27.71 __-.-_I_-___- -_____ - ---I-- FS 1640-1660 stringer 51 R49R

-. RF52G c307 8112l96-3 40 39 47.60 -72 37 27.10 bulkhead fragment, approx 3x4

RF53D C2087 8/20/96-l 2 C936 4

o;j-i7.3r’. -. - --.- .-----.. -72 37 27.71

. - --.. ..__ --. ._..- _- __.- .-_._-_ .-_, ___-_--__-__ ___-__---__ FS 1680-1720, stringer27R-31R

RF54D c2106 8/22/96-5 C647 40 39 46.89 -72 37 26.59 FS 1840-l 920, stringer 47R-50R

RF54E C2336 C946 40 39 47.41 -72 37 27.64 FS 38R46R forward lower 1780-l&QOT-s?nger out. Lot # a-20-96-12

comer of aft cargo door cut-

RF55A Cl067 a/24196-7 40 39 46.89 -72 37 26.59 tail cone I APU exhaust; FS 2742-2775

RF55C C2338 a/22/96-5 C65l 40 3946.89 -72 26.59 3; . FS 2725-2742. of RH part APU access door hinge

RF550 Cl27 816l96-46 40 39 47.00 -72 37 27.90 FS 2664-2742, LH APU access door hinge

RF62 C2337 8/26/96-36 ci’39 40 39 46.40 -72 37 27.80 . FS 1920-l 940, stringer 34R-40R. Lot # 8-26-96-36

RF64 C2153 40 39 46.40 -72 37 27.80 RHS keel chord aft of FS 1480

RF66 c2156 8726/96-36 cl093 40 39 46.40 -72 37 27.80 FS 1536-1620, stringer 42R-49R

RF73 I

c2339 I

*

I I RF75

I C2082

I 8/20/96-12

I cQ40 0 39 47.36 -72 37 27.71 FS 1847-I 877, stringer 20R-23R

I I I I RF98 1 C2155 1 8/26/96-36 ( c730 ko 39 46.40

I I l-72 37 27.80 IFS 1810; outer frame aft cargo door panel stringer STR 24R-28R (aft upper

RF99 c2340 8lO5l9570

main cargo door sill)

cl 12 40 39 46.90 -72 37 27.90 FS 1810-l 836; stringer 27R-30R; forward right upper comer of aft cargo door

RFSA C2331 Cl 17 40 39 46.90 -72 37 27.90 FS 1900-2320 stringers lOL-6R Note: saw cut from RHS for RFSB and RF15

RFSB C2332 cl 17 40 39 46.90 -72 37 27.90 FS 1900-2140; stringer 6R-22R with window Note: saw cut from RF 9A and RF15

RWI 8 l 23384 9l22l951 40 39 49.60 -72 37 27.30 #8 flap track assembly and carriage transmission

RW32 c210 8/08/96-30 -._-...-__ 40 39 47.00 -72 37 27.00 right wing trailing edge flap; upper airfoil section

-..-.--- .-._.- VlO 22824 -.-_--- 23277 40 39 46.76 -72 37 14.05 vertical stabilizer station, fin stalon 230.412410,045

--.-_-- Al.41

1 GRP# Log # Tag # FBI # Source Tag # Latitude Longitude Description (Actual)

35 cw120 C2327 811 g/96-22 C9O4 h0 39 46.15 --. -. .l-.23ix45 ------- --.- .:.. . ..--_.__.-.- --.5---.-. ..- .-.._. -.-_---- . ..__. ._

center wrng tank spanwtse beam -_- _ -._ __-___ ___, _

CW806 C2344 8/i g/96-22 C896 40 39 46.15 -- -72 37 26.49 cw mid spar stiffener BL 1 IL -- -

LF67C c2345 8mt96-6 C894 40 39 46.15 _ -72 37 26.49 FS 1260-1280 stringer 28L-31 L

I LW29A c2329 8118t96-6 C891 40 39 46.15 -72 37 26.49 lefl upper wing skin WS 780-804 from stringer 22 to forward edge of panel

LW45 C2357 C880 40 39 46.15 -72 37 26.49 left wing front spar ILES 280440

36 CWlOl3 c2284 C2268 40 39 46.15 -72 37 26.49 upper rear spar web

CW412 C2283 C2268 40 39 46.15 -72 37 26.49 middle web area at first stiffener forward of rear spar LH SOB _’

LW37 c2291 8/l 9196-22 C863 40 39 46.15 -72 37 26.49 IefI wing #3 trailing edge flap drive gear box

37 CWllO C2227 8/l 6196-6 C879 40 39 46.15 -72 37 26.49 upper center wing skin piece; LH side at stringer 5-l; LBL 104-l 15 at upper STR 5-1

cW217 c2093 C662 40 39 46.89 - -72 37 26.59 Wing Skinx 2

cw229 C2165 c904 40 39 46.15 -72 37 26.49 cw lower skin-matches w/C21 60. LBL 104 STR 11.5-I 3.5

CW408 C2282 C2268 40 39 46.15 -72 37 26.49 center fuel tank stiffener, SOB, LH S3 upper S2 lower

cw410 C2270 C896 40 39 46.15 -72 37 26.49 SOB rib at upper FS LH side

CW504A C2108 8/22/96-5 C657 40 3946.89 -72 37 26.59 front spar LH web above access hole approx 8” x 8” section

cw505 C2140 C880 40 39 46.15 -72 37 26.49 front spar- LH web SOB above access hole

CW506 C2135 C906 40 39 46.15 -72 37 26.49 front spar LHS comer fitting

cw507 C2186 8118196-6 C2140 40 39 46.15 -72 37 F6.49 Front spar center section web

CW508 C2137 C880 40 39 46.15 -72 37 26.49 front spar lower dry bay access hole

C906 4 -.-.-.I--.----- --.. - I- .-..- l-l__-

0 39 46.15 --_-- _-__.__ --__

-72 37 26.49 front spar, lower dry bay access hole ---

cw511 C2187 C2175 40 39 46.15 -72 37 26.49 lower front spar Side of Body outboard wing left -

CW516 --- - C2226 -----_-_- ._,..-._..__

8/l Q/96-22 I_--.--.---_v_

C863 40 39 46.15 -72 37 26.49 front spar web piece; center fuel tank ---_ ,

-------_ ._ Al.42

/ GRP # Log # Tag R FBI # Source Tag # Latitude ------- Longitude ---- ..-- -..- ._

37 ._-.__ -

CW605 ______ .-

C2172 . . -

Description (Actual)

8119/96-22 ..__. .-. C902 -72 37 40 39 46.15 26.49 spanwise beam paddle #3LBL 127.5 fitting and web

--... .-. -. .-- -.. .-. . cWQo5

,.__, ._,, C2107 C657 40 39 46.69 -72 37 26.59 spanwise beam #I - lower web at LBL 98 intercostal (wing center section

LW15, cw C2175 8/l 8x6-6

intercostal) , ._-_ 403 C902 ---.--~ ..- ---- --.- _-.-. -----------.-- ------‘----- -- 4 0 39 46.15 -72 37 26.49 jeR upper wing skin at soB s25-s33

RF476 C219 8/18lQ6-6 __-- --- .-... _..-- 40 3946.15 -72 37 .-.--. - . .-... -.------ -_.-- ._ ._ -. _._ .

26.49 FS 2484-2638, stringer 1 R-17R

c891 40 39 46.15 - -72 37 26.49 CW outboard leg of left RS terminal fitting

C912 40 39 46.15 low/ -72 37 26.49 left

LW296 C2040 C891 40 39 46.15 . -(left - -72 37 26.49 wing up skin; LWS 771-808 with front span cap (skin segment (C891))

39 CWI 08, C2027 8/l

-_-__ 8196-6

CW804 C879 4

o 3s 46.,5------7237-z--49 ..-- --..-‘----7- upper CW LH s~kce S14 (M.S.) (CW108); mid spar - 3’ portion of~~~~

cW207 C238

fitting; this part is part of CW108 & CW804

8/09/96-37 40 39 50.14 -72 37 27.24 lower center and left CW skin 5-10 5-15; to LBL 97 to RBL 104

LF27G C2355 8/09/Q6-37 C237 40 39 50.14 -72 37 27.24 FS 1920-1940 stringer 32L-36L

LF33B C2384 8/09/96-37 C232 40 39 50.14 -72 37 27.24 FS 2270-2300 stringer 1 OL-13L

LW38 C2029 8/l 8196-6 C891 40 39 46.15 -72 37 26.49 left wing #I flap carriage (C891) (See C229)

RF59 C236 8iO9/96-37 40 39 50.14 -72 37 27.24 fwd upper inboard section wheel well wall; FS 1360-1380

RW31 C2374 8/09196-37 C232 40 39 50.14 -72 37 27.24 right wing outboard fore flap

40 LF27A C2352 8108f9630 C227 40 39 50.14 -72 37 27.24 FS 1740-l 800 stringer 30L-34L

LF27C C2353 8/09196-37 C232 40 39 50.14 -72 37 27.24 FS 1760-l 810 stringer 25L-30L

41 LFlSB C2351 8/09/96-37 c259 40 39 50.14 -72 37 27.24 FS 2160-2220; stringer 23L-30L

LF60 C2321 8/09/96-37 C259 -40

-- --_..._ 39 50.14 -72 37 - 27.24 skin panel FS 2020-2040; stringer 36L-41 L

RW26 l c234 8/09/96-37 40 39 50.14 -72 37 27.24 trailing edge flap

RW28 C235 8/09/96-37 40 39 50.14 -72 37 27.24 trailing edge flap / RW5 C232 1

8109196-37 40 39 50.14 -72 37 27.24 right wing lower skin; RWS 1196-1424

Al.43

,j > )

GRP # Log # Tag # FBI # Source Tag # Latitude Longitude Description (Actual)

42 CW801, C224 8/08l96-30 40 39 50.14 cW102,

mid spar web RBL 85 to LBL 49 (CW801); SWB #2 RH web RBL 30-80

- cW702 ---m- -.--. ----..I -...-.. --.- (CW702); Top right porhon of CW tank (CW 102)

---- -- -._..- ._ _____ -.--- .--.-.. --.- -.. -..-.---.-

H9 -.--, -.-. ..-.--.---- - .-.-.-. - .._-._ -.

C226 8/08/96-30 -.-- _... _ ..-._---.,I- -.... ._. __._ .__..l_____l.

40 39 50.14 -72 37 27.24 horizontal stabilizer skin section

43

44

45

LF29 C227 I 8lO819530 40 39 -72 50.14 37 27.24 FS 1540-l 820 left side fuselage I

LW38 c229 8/08/96-30 40 39 50.14 -72 37 #1 27.24 left wing flap carriage ((See C2029)

RWI 2 C2232 8109196-37 C232 40 39 50.14 -72 37 27.24 lower wing skin; right hand wing; WS 1214-1243; FS 6 to rear spar

RW29 C223 8/08/96-30 40 39 50.14 -72 37 27.24 right trailing edge flap section

cw103 c221 8/08/96-30 40 39 50.14 -72 37 27.24 CW - upper skun LBL 5 RBL 100, r.s. to SWB #I

CW205 C218 8/08196-30 40 39 50.14 -72 37 27.24 lower CW S-4 to skin: S-IO; left SOB to RBL 80

cw1001 C2280 Cl83 40 39 49.60 -72 37 28.10 #3 of piece side rear (seexC22’18 3 tags on same right CW (RF1 7), spar c2279 (CW302))

cW302 c2279 Cl 83 40 39 49.60 -72 37 28. IO #2 of 3 on same piece right side CW upper segment SOB rib (see also C2278 (RFI’I), C2280 (CWlOOl))

CW708 C2275 8lO8M-68 Cl83 40 39 49.60 -72 37; 28.10 spanwise beam #2; RBL 83-l 10 at lower chord

RF17 C2278 Cl83 40 39 49.60 -72 37 28.10 right hand body attached to right hand wing with 3R door opening: (#I upper of 3 tags (see also C2279 (CW302), C2280 (CWlOOi)))

, -----_* ----_-I -_.

i Al.44