N902FD

ATA 5754

Part: SKIN — DAMAGED (NR 9 SLAT) · airframe 53,534 hrs · 22,034 cycles

EXISTING DOUBLER REPAIR ON NR 9 SLAT INBD AND OTBD END UPPER SURFACE. COMPLY WITH ATTACHMENT "B" OF EO F-5100-7-5001 PT 1 EVALUATED REPAIR IAW EO F-5100-7-5001 ATTCHEMENT "B". REPAIR FOUND TO BE IAW SRM 51-70-10, REPAIR 2, FIG 201. REPAIR IS CLASSIFIED AS A MAJOR IAW GMM 6-2-100. EA F-5750-142290 ATTACHED FOR TRACKING PURPOSES IAW EO F-5100-7-5001 PT1 INSTRUCTIONS, STEP 3.

ATA 5347

Part: SEAT TRACK — MISALIGNED (ZONE 200) · airframe 53,534 hrs · 22,034 cycles

SEAT TRACK STA 377-440, LBL 25 REQUIRES CHANGE IAW CUSTOMER REQUEST. R & R SEAT TRACK STA 377-440, LBL 25 IAW SRM 51-40-02. CLASSIFIED CATEGORY "A" MAJOR REPAIR.

ATA 5310

Part: STRUCTURE — DAMAGED (BS 1620-1661) · airframe 53,534 hrs · 22,034 cycles

SMOKE DETECTOR CUT OUTS INCORRECTLY LOCATED AT STA'S 1620, STA 1640 AND STA 1661, LBL 28.25. A REPAIR WAS ACCOMPLISHED ON STAM EA-757-5365-16-F2884, FOR THE SMOKE DETECTOR CUT OUTS INCORRECTLY LOCATED AT STA 1620, 1640, AND 1661, LBL 28.25. AN 8110-3, DATED 10/05/2010 WAS ISSUED FOR DTA EVALUATION. EA F-5310-141226, ISSUED TO ESTABLISH THE DTA TRACKING IN THE SYS. MAJOR ALTERATION.

ATA 5340

Part: FITTING — MISINSTALLED (ZONE 200) · airframe 53,534 hrs · 22,034 cycles

POTENTIAL SHORT EDGE MARGIN CONDITIONS IN THE 675N3161-11 FITTING DUE TO INCOMING FASTENER HOLE LOCATIONS AT STA 1640, S-17L- 18L. A REPAIR WAS ACCOMPLISHED ON STAM EA 757-5362-16-F2804 FOR POTENTIAL SHORT EDGE MARGIN CONDITIONS IN THE 657N3161-11 FITTING AT STA 1640 STRINGERS 17 AND 18L. 8110-3, DATED 10/11/2010, ISSUED FOR DTA EVALUATION. EA F-5310-142275 ISSUED TO ESTABLISH THE DTA TRACKING IN THE SYS. MAJOR ALTERATION.

ATA 5340

Part: FITTING — MISINSTALLED (ZONE 200) · airframe 53,534 hrs · 22,034 cycles

POTENTIAL SHORT EDGE MARGIN CONDITIONS IN 657N3161-12 FITTING DUE TO INCOMING FASTENER HOLE LOCATIONS AT STA 1640, S-17R- 18R. A REPAIR WAS ACCOMPLISHED ON STAM EA 757-5362-16-F2803, FOR POTENTIAL SHORT EDGE MARGIN CONDITIONS IN THE 657N3161-12 FITTING AT STA 1640, STRINGERS 17 AND 18R. 8110-3 , DATED 10/11/2010 ISSUED FOR DTA EVALUATION. EA F-5310-141218 ISSUED TO ESTABLISH DTA TRACKING IN THE SYS. MAJOR ALTERATION.

ATA 5311

Part: FRAME — DAMAGED (ZONE 200) · airframe 53,534 hrs · 22,034 cycles

MISDRILLED HOLES COMMON TO 143N1002-18 FRAME WEB, 143N1002-9 FRAME DOUBLER AND 143N1114-3 INBD CHORD AT STA 460, BETWEEN S-13L AND S-14L. A REPAIR WAS ACCOMPLISHED ON STAM EA 757-5332-16-F2898 FOR MISDRILLED HOLES COMMON TO THE 143N1002-18 FRAME WEB, 143N1002-9 FRAME DOUBLER AND THE 143N114-3 INBD CHORD AT STA 460 BETWEEN S-13L AND S-14L. 8110-3 DATED 10/11/2010 ISSUED FOR DTA EVALUATION. EA F-5310-142278 ISSUED TO ESTABLISH THE DTA TRACKING IN THE SYS. MAJOR ALTERATION.

ATA 5330

Part: SKIN — MISREPAIRED (ZONE 200) · airframe 53,534 hrs · 22,034 cycles

EXISTING EXTERNAL DOUBLER ON L-2 DOOR LOWER FWD HINGE CUTOFF DOES NOT MEET SRM REQUIEMENTS. ACCOMPLISHED EA F 5210-141214,DOORS L-2 DOOR OUTER SKIN EXISTING REPAIR REPLACEMENT, PN 143N6100-3, SN 000474. MAJOR REPAIR.

ATA 5754

Part: WEDGE — DENTED (NR 1 SLAT) · airframe 53,534 hrs · 22,034 cycles

NR 1 SLAT T/E WEDGE UPPER SURFACE HAS SEVERAL DENTS REPAIRED NR 1 SLAT WS 711.5 TO 743.5 T/E WEDGE UPPER SURFACE IAW SRM 51-70-10, PN 114N4002-153A, SN A1-0616. CLASSIFED CATEGORY "A" MAJOR REPAIR.

ATA 5330

Part: SKIN — DENTED (BS 980-1000) · airframe 53,534 hrs · 22,034 cycles

EXTERNAL FUSELAGE SKIN LT SIDE, STA. 980-1000 BETWEEN S-9L TO S-10L IS DENTED. DENT OUT OF LIMITS IAW SRM 53-00-01 FIG 101, DET.III, ACCOMPLISHED EA F-5330-141197 DTD 03SEP10, FUSELAGE STA. 993 SKIN DENT NEAR S-10L LAP SPLICE. PN: 144N3140.

ATA 5330

Part: SKIN — DAMAGED (ZONE 200) · airframe 53,534 hrs · 22,034 cycles

CUT FOUND AT S14R FROM BS 781 THROUGH BS 781,156 RUNNING VERTICAL UNDER LAP SEAM AT THE EDGE OF THE BUTT JOINT, DURING LAP SEAM INSP FOR SCRIBE LINES. ACCOMPLISHED EA F-53330-139219 FUSELAGE- PLATE/ SKIN (AD2007-19-07) EO F-5330-7-5000 SECTION 43 SKIN SCRATCH BS 781.0; S-14R, TREATED & PRIMED AREA IAW SRM 51-20-01. MAJOR REPAIR.

ATA 5320

Part: WEB — DAMAGED (ZONE 200) · airframe 53,534 hrs · 22,034 cycles

THIS NON ROUTINE FOR TIME AND REPAIR TRACKING. W/C MAE MOD (43607420001 / 118350499EZ2R01). REWORK REQUIRED AT LBL 29. FLOORBEAM WEBS AT FS 1620, 1640, AND 1661. STRUCTURES MECH MIS-READ DWG 657N3374, SHT 1, AND DRILLED / CUT A2" HOLE AT LBL 29 IN FLOORBEAM WEBS AT STA 1620, 1640, AND 1661, AN EA IS REQ LBL 29, STA 1620, 1640, & 1661, REPAIRED IAW / MAE EA 757-5365-16-F2884, REV -, DATED 09/03/10. REPAIR DETAILS ON WORK CARD 118350499EZ2R01, THIS NON ROUTINE IS FOR TRACKING PURPOSES ONLY. MAJOR REPAIR.

ATA 5330

Part: SKIN — PUNCTURED (ZONE 100) · airframe 53,534 hrs · 22,034 cycles

OUTER PUNCTURE ON FUSELAGE SKIN AT STA 710 BETWEEN S-26R TO S-27R EVALUATED DENT, FOUND PUNCTURE OUT OF LIMITS IAW SRM 53-00-01, FIG 101, DETAIL III. REPAIRED SKIN AT STA 710, BETWEEN S-26R TO S-27R IAW SRM 53-00-01, FIG 201, REPAIR 7 CLASSIFED CATEGORY "B" REPAIR WITH INSP THRESHOLD OF 24,000 FC AND INTERVAL OF 12,000 FC.

ATA 5330

Part: SKIN — DAMAGED (ZONE 100) · airframe 53,534 hrs · 22,034 cycles

SCRIBE LINE FOUND AT STA 586.375 TO 602.250 S-26L DURING LAP SEAM INSP FOR SCRIBE LINES ACCOMPLISHED EA 5330-141725. CLASSIFIED CATEGORY "A" MAJOR REPAIR.

ATA 5320

Part: ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 53,534 hrs · 22,034 cycles

INTERCOSTAL PLATE BET 29R AND S28R ON ATA 740 HAS CORROSION. (FWD CARGO). REMOVED CORROSION IAW SRM 51-10-02, BLENDED AREA STA 740, STR28R AND 29R, L=2" W=3" D=0.008 MAT ORIG .071 MAT REMAIN .063 OUT OF LIMITS IAW SRM 53-00-04, FIG 101, DET II. REMOVED ANGLE CHANNEL IAW SRM 51-40-02, FABRICATED NEW ANGLE CHANNEL ON MAT T10848067 LOCATED DRILLED IAW SRM 51-40-05, INSTALLED NEW ANGLE IAW SRM 51-40-02. MAJOR REPAIR.

ATA 5330

Part: SKIN — DAMAGED (ZONE 100) · airframe 53,534 hrs · 22,034 cycles

SCRIBE LINE FOUND AT S-26L FROM STA 529-530.438 DURING LAP SEAM INSP FOR SCRIBE LINES ACCOMPLISHED EA F-5330-141725. CLASSIFED CATEGORY "A" MAJOR REPAIR.

ATA 5330

Part: SKIN — DAMAGED (ZONE 100) · airframe 53,534 hrs · 22,034 cycles

SCRIBE LINE FOUND AT STA 538.5 TO 539.563 S-26L DURING LAP SEAM INSP FOR SCRIBE LINES ACCOMPLISHED EA F-5330-141725. CLASSIFIED CATEGORY "A" MAJOR REPAIR.

ATA 5240

Part: DOUBLER — DAMAGED (L2 DOOR) · airframe 53,534 hrs · 22,034 cycles

L-2 DOOR INTERNAL SKIN A DOUBLER HAS A DOUBLE DRILL HOLE AT APPRO 8" AFT OF FWD EDGE AND 27" FROM THE BOTTOM EDGE. ALL REPAIRED ACCOMPLISHED ON EA F-5210-141186, MAJOR REPAIR

ATA 5347

Part: SEAT TRACK — CORRODED (BS 640-780) · corrosion level 2 · airframe 53,534 hrs · 22,034 cycles

SEAT TRACK RBL 45 STA 640-780 CORRODED AND GOUGED. REMOVED CORROSION AND GOUGES AT SEAT TRACK RBL 45 STA. 640-780 IAW SRM 51-10- 02. BLENDED AREA ORIGINAL MATERIAL=.070 IN. L=4.0 IN W=1.0 IN. D=.022 FOUND OUT OF LIMITS IAW SRM 53-00-52, FIG 101, DETAIL VII. R & R SEAT TRACK IAW SRM 51-40-02. THIS IS A MAJOR REPAIR.

ATA 5532

Part: SKIN — DENTED (VERTICAL STAB) · airframe 53,534 hrs · 22,034 cycles

DENT IN LT SIDE OF VERT STAB FSS-153 EVALUATED 2EA DENTS ON STAB STAB STA FSS 153. DENTS WITHIN 1SQ FT OF EACH OTHER. FOUND OUT OF LIMITS IAW SRM 55-30-01, FIG 101, DETAIL III AND NOTE "H". REPAIRED DENTS IAW SRM51-70-10, REPAIR 2 CLASSIFIED CATEGORY "A" MAJOR REPAIR.

ATA 5313

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 53,534 hrs · 22,034 cycles

AFT CARGO PIT COMPT STA 1600-1620 S-29L STRINGER SPLICE CORRODED REMOVED CORROSION & FOUND OUT OF LIMITS IAW SRM 53-00-03 FIG 101. FURTHER INVESTIGATION 29L STRINGER IS ALSO CORRODED AND FOUND TO BE OUT OF LIMIT 100% MATERIAL LOSS. FABRICATED REPAIR STRINGER WITH TRAVLER T10/849692. FABRICATED REPAIR SPLICE WIGH TRAVLER T10/849798. INSTALLED NEW REPAIR STRINGER AND SPLICE IAW SRM 53-00-03 FIG 201. MAJOR REPAIR.

ATA 5311

Part: FRAME — CRACKED (ZONE 200) · airframe 53,534 hrs · 22,034 cycles

AFTER REMOVAL OF TV MONITOR BRACKETS FOUND FRAME CRACKED STA 377-7, BETWEEN S-1 TO S-2L. CRACKED FRAME STA 377.7 S-5L TO S4R FOUND OUT OF LIMITS IAW SRM 53-00-07 FIG 101 DETAIL I. REMOVED AND REPLACED FRAME IAW SRM 51-40-02. CLASSIFIED CATEGORY "A" MAJOR REPAIR

ATA 5532

Part: SKIN — DENTED (VERTICAL STAB) · airframe 53,534 hrs · 22,034 cycles

DENT ON LT SIDE VERT STAB FSS-146 EVALUATED 2EA DENTS ON VERT STAB STA FSS-146. DENTS WITHIN 1SQ FT OF EACH OTHER. FOUND OUT OF LIMITS IAW SRM 55-30-01, FIG 101, DETAIL III NOTE "H". REPAIRED DENTS IAW SRM 51-70-10, REPAIR 2. CLASSIFIED CATEGORY "A" MAJOR REPAIR.

ATA 5310

Part: SEAT TRACK — CORRODED (BS 1540-1640) · corrosion level 2 · airframe 53,534 hrs · 22,034 cycles

MAIN CABIN SEAT TRACK , STA. 1540 - 1640 RBL 25 IS GOUGED AND HAS CORROSION. BLENDED OUT CORROSION AND GOUGES THE MAX DEPTH IS .030 IN. AND IS OUT OF LIMITS IAW SRM 53-00-52 FIG.101 DETAIL 1. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-40-02. REPAIR IS CLASSIFIED AS MAJOR.

ATA 5347

Part: SEAT TRACK — CORRODED (BS 1540-1640) · corrosion level 2 · airframe 53,534 hrs · 22,034 cycles

MAIN CABIN BETWEEN BS 1540 - 1640 LBL 25 SEAT TRACK WITH CORROSION AND GOUGES. BLENDED OUT GOUGES AND CORROSION AND MATERIAL REMAINING IS .085 AND IS OUT OF LIMITS IAW SRM 53-00-52 FIG 101, DETAIL 1 OF CROWN AREA. R & R SEAT TRACK IAW SRM 5I-40-02. REPAIR IS CLASSIFIED AS MAJOR.

ATA 5320

Part: NUT PLATE — CORRODED (FLOOR SUPPORT) · corrosion level 2 · airframe 53,534 hrs · 22,034 cycles

AFT CARGO COMPARTMENT FLOOR STRUCTURE BS 1340 - 1320 HAS NUMEROUS RUSTY NUT PLATES, LBL 7.55.

ATA 5744

Part: RIB — CHAFED (ZONE 500) · airframe 53,534 hrs · 22,034 cycles

LT WING INBD T/E FLAP INBD SUPPORT FITTING HAS WORN/CHAFED SPOT. CHECKED AREA L = 1.5 W = .060 D =.042, ORIGINAL MATERIAL THICKNESS = .090, MATERIAL REMAINING = .048 AND OUT OF LIMITS IAW SRM 57-53-02 FIG. 101 DETAIL VIII. R & R SUPPORT FITTING AND RIB ASSY IAW SRM 51-40-02. REPAIR CLASSIFIED AS MAJOR.

ATA 5321

Part: FLOOR PANEL — CORRODED (ZONE 200) · airframe 53,534 hrs · 22,034 cycles

MAIN CABIN AREA AT BS. 1720 LBL 35 FLOOR PANEL WITH CORROSION. REMOVED CORROSION AT BS 1720, LBL 35 FLOOR PANEL, BLENDED OUT DAMAGE L= 4.00 X W=3.00 X D.016, ORIGINAL MATERIAL =.071, MATERIAL REMAINING = .055 IS OUT OF LIMITS IAW SRM 53-00-51 FIG. 101 DETAIL III. FABRICATED REPAIR DOUBLER AND INSTALLED IAW SRM 53-60-51, FIG 201.

ATA 5330

Part: SKIN — DENTED (ZONE 100) · airframe 53,534 hrs · 22,034 cycles

EXTERNAL FUSELAGE SKIN STA 1620- 1640 S-22R TO S-23R HAS 2EA OUTWARD DENTS. EVALUATED (2EA) DENTS, NR1 A/Y=26.47, NR2 A/Y=20.37, BOTH DENTS FOUND OUT OF LIMITS IAW SRM 53-00-01, FIG 101, DET III. REPAIRED SKIN AT STA 1620-1640, BET S22R TO S23R IAW SRM 53-00-01, FIG 201, R3. THIS IS A CLASS 'B' REPAIR WITH FURTHER INSPECTIONS REQ'D AT 25,000 F.C., WITH INTERVALS AT 6,000 FC IAW SRM 53-00-01, FIG 201, R3, DET II, TABLE V. SKIN PN 146N3780-2. MAJOR REPAIR.

ATA 5347

Part: SEAT TRACK — GOUGED (BS 700-780) · airframe 53,534 hrs · 22,034 cycles

CABIN FLOOR SEAT TRACK AT LBL 45.50 AT STA 700-780 SEVERAL NICKS. BLENDED OUT SEVERAL NICKS ON CABIN FLOOR SEAT TRACK AND FOUND TO BE OUT OF LIMIT. REMOVED SEAT TRACK FROM STA 700-780 IAW SRM 51-49-02 REPLACED WITH THE NEW SEAT TRACK WITH BATCH NR 1869949 AND INSTALLED ON STA 700-780 IAW RM 51-40-02. BLENDED AREA L= 18.0" W= .50" D=.025 OUT OF LIMITS IAW SRM 53-00-52 FIG 101 DET I. SEAT TRACK PN 143N5470-1. MAJOR REPAIR

ATA 5310

Part: CREASE BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 53,534 hrs · 22,034 cycles

MAIN DECK STA 665-755, WL 208, LBL 65 CREASE BEAM INBD CHORD IS CORRODED. REMOVED CORROSION ON INBD CREASE BEAM CHORD STA 665-755 LBL65 IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-30-15, FIG 101, DETAIL IV ORIG MATERIAL .080 AFTER REWORK .055 L=60" W=1.0. R & R CHORD IAW SRM 51-40-02. CLASSIFIED CATEGORY "A" MAJOR REPAIR.

ATA 5347

Part: SEAT TRACK — CORRODED (BS 900-1040) · corrosion level 2 · airframe 53,534 hrs · 22,034 cycles

MAIN CABIN SEAT TRACK STA 900-1040 RBL 25 IS GOUGED AND HAS CORROSION . REMOVED CORROSION ON SEAT TRACK STA 900-1040, RBL 25 IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, FIG 101, DETAIL I. DEPTH EXCEEDS MAX REMOVAL .020. L=10" W=1.0 D=.028. R & R SEAT TRACK IAW SRM 51-40-02. CLASSIFIED CATEGORY "A" MAJOR REPAIR.

ATA 5320

Part: FLOOR SUPPORT — CORRODED (BS 377-418) · corrosion level 2 · airframe 53,534 hrs · 22,034 cycles

FLOOR SUPPORT STA 377-418 RBL 25 CORRODED AND GOUGED REMOVED CORROSIN AND GOUGES AT STA 377-418 RBL 24 IAW SRM 51-10-02. REMOVED .010" FROM .071 ORIGINAL MATERIAL, OUT OF LIMITS IAW SRM 53-00-52 FIG 101 DET VIII,REMOVED AND REPLACED SUPPORT AT RBL 24,STA 365-418 IAW SRM 51-40-02. SUPPORT P/N141N5131-40 . MAJOR REPAIR

ATA 5310

Part: CREASE BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 53,534 hrs · 22,034 cycles

MAIN CABIN STA 1440-1460, RT SIDE CREASE BEAM WEB HAS CORROSION. REMOVED CORROSION AT MAIN CABIN STA 1440-1460 RT SIDE CREASE BEAM IAW SRM 51-10-02. BLENDED AREA L= 1.75",W=1.45",D=.008" ORIGINAL MAT. .040". MAT REMAINING .032" FOUND OUT LIMITS IAW SRM 53-00-13 FIG 101 DET II. R & R WEB IAW SRM 51-40-02. PN FX-146N5590-12 (WEB)-MAJOR REPAIR.

ATA 5347

Part: SEAT TRACK — GOUGED (BS 418-440) · airframe 53,534 hrs · 22,034 cycles

SEAT TRACK STA 418-440, RBL 45 IS GOUGED. BLENDED DAMAGED AREA ORIG MAT .080, AFTER BLEND, L-2.00, W-.900, D-.022, REMAINING MAT .058. FOUND TO BE OUT OF LIMIT IAW SRM 53-00-52, FIG 101, DET VII, FAB NEW SEAT TRACK OF PN 60-6549/24 BATCH NR 1541987 IAW SRM 53-10-52. FIG I, DET I, R & R SEAT TRACK IAW SRM 51-40-02. MAJOR REPAIR.

ATA 5347

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 53,534 hrs · 22,034 cycles

SEAT TRACK, STA 418-440, RBL 24 GOUGED, REMOVED GOUGE AT STA 418-440, RBL 24 IAW SRM 51-10-02. BLENDED AREA DIM L=2.5 W=.8 D=.026. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52 FIG 101 DETAIL VII. ORIG MATERIAL .080 AFTER REWORK .054. R & R SEAT TRACK IAW SRM 51-40- 02. CLASSIFIED CATEGORY "A" MAJOR REPAIR.

ATA 5315

Part: FLOORBEAM — DAMAGED (BS 1640) · airframe 53,534 hrs · 22,034 cycles

REMOVED FLOORBEAM STA 1640 IAW SRM 51-40-02, FABRICATED NEW FLOORBEAM STA 1640, FROM MAT TYPE PN BAC 1518-338/18A, BATCH 1783535 IAW DWG NR 146N5089, SH 3, REV B. INSTALLED FLOORBEAM IAW SRM 51-40-02. MAJOR REPAIR.

ATA 5347

Part: SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 53,534 hrs · 22,034 cycles

STA 365-418 RBL-45 SEAT TRACK SUPPORT. REMOVED CORROSION FROM SEAT TRACK SUPPORT IAW SRM 51-10-02. BLENDED AREA IS .011" DEEP, .5" WIDE, 1" LONG. ORIGINAL MATERIAL IS .070" OUT OF LIMITS IAW SRM 53-00-52 FIG 101 DET VIII. INSTALLED NEW SEAT TRACK SUPPORT AT RBL 45 STA 365-418 IAW SRM 51-40-02. MAJOR REPAIR.

ATA 5320

Part: WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 53,534 hrs · 22,034 cycles

AFT PIT FLOOR STRUCTURE WEBS (2EA) BS 1500-1520 BL0-RBL 5.5 LOWER SECTION HAS CORROSION. REMOVED CORROSION FROM WEB STA 1500-1520 BL0 TO RBL 5.5 IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53, FIG 101 DETAIL V. ORIGINAL MATERIAL .032 AFTER REWORK .024 L=3.5 W=1.0. R & R WEB IAW SRM 51-40-02. CLASSIFIED CATEGORY "A" MAJOR REPAIR.

ATA 5320

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 53,534 hrs · 22,034 cycles

AFT PIT FLOOR SUPPORT WEB BS 1600-1620 RBL 5.5 LOWER SECTION CORRODED. BLENDED OUT CORROSION ON WEB IN AFT CARGO STA 1600- 1620 AND CHECKED LIMITS, MATERIAL THICKNESS- 0.40, L=15", W=0.075, D=.10", AND FOUND OUT OF LIMIT IAW SRM 53-00-04, FIG 101. INSTALLED NEW WEB WITH PART NR 146N5451-9- N00307. ON AFT CARGO STA 1600-1620, RBL 5.5 IAW SRM 51-40-02. MAJOR REPAIR.

ATA 5322

Part: SHEAR TIE — CORRODED (BS 1620) · airframe 53,534 hrs · 22,034 cycles

INTERNAL LOWER FUSELAGE SKIN SHEAR TIE BS 1620 BL0 CORRODED. REMOVED CORROSION ON SHEAR TIE, STA 1620, BL0 IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-60-04, FIG 101, DETAIL II. ORIG MATERIAL .050 AFTER REWORK .040 L=1.0 W=1.0. R & R SHEAR TIE IAW SRM 51-40-02. CLASSIFIED CATEGORY "A" MAJOR REPAIR.

ATA 5310

Part: CREASE BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 53,534 hrs · 22,034 cycles

MAIN CABIN STA 1260, RT SIDE IB CREASE BEAM CHORD HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-02 BLEND AREA ORIG. MAT. .070 MAT. REMAINING .050 OUT OF LIMITS IAW SRM 53-30-13 FIG. 101 DET. 3, REMOVED AND REPLACED CREASE BEAM FROM STA 1180-1300 IAW SRM 51-40-05 AND 51-40-02. THIS IS A MAJOR REPAIR NO FOLOW-UP INSPECTION REQUIRED.

ATA 5310

Part: FRAME — GOUGED (ZONE 200) · airframe 53,534 hrs · 22,034 cycles

MAIN CABIN, STA 1280, STR 10R TO STR 14R, FRAME HAVE 4 EA GOUGES. BLENDED GOUGES BET 10R & 14R AT STA 1280 FRAME. BLEND OUT DM= L=28",W=1.0", D=.009" ORIGINAL MAT'L THICKNESS .071", FOUND OUT OF LIMITS IAW 53-00-07 FIG. 101 DET, II REPAIR IAW SRM 53-00-07 FIG 201, REPAIR NR 1. THIS IS A CLASS 'B' REPAIR WITH SUPPLEMENTAL INSPECTIONS REQUIRED IAW SRM 53-00-07, TABLE 203 ZN '3'. INSP THRESHOLD = 12,000 FC, 50,000 AIRFRAME FC'S WHICHEVER COMES FIRST, INSP METHOD=DVI,INTERVALS =12,000 FC. MAJOR REPAIR.

ATA 5310

Part: CREASE BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 53,534 hrs · 22,034 cycles

MAIN CABIN BETWEEN STA 740-760, RT SIDE CREASE BEAM WEB HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-02 BLEANDED AREA AL 2" X 0.5" XD=.008 MAT ORIG .056 REMAINING .048 OUT OF LIMITS IAW SRM 53-00-04 FIG 101 DET IV. REMOVED AND REPLACED CREASE WEB STA AT 740 TO STA 760 RT SIDE IAW SRM 51-40-02. MAJOR REPAIR

ATA 5311

Part: FRAME — GOUGED (ZONE 200) · airframe 53,534 hrs · 22,034 cycles

MAIN CABIN, INTERNAL STRUCTURE FRAME BS 180, STRG 14L, STRG 10L, HAVE GOUGES. REPAIR FRAME BS 1280 LT IAW SRM 53-00-07, FIG 201, REPAIR NR 1.THIS IS A CAT B REPAIR WITH SUPPLEMENTAL INSPECTIONS REQUIRED IAW TABLE 203 OF SRM 53-00-07, FIG 201, REPAIR NR 1. MAJOR REPAIR.

ATA 5310

Part: CREASE BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 53,534 hrs · 22,034 cycles

MAIN CABIN CREASE BEAM WEB BS 1380 S17L LOWER SURFACE HAS CORROSION. REMOVED CORROSION AT MAIN CREASE BEAM WEB STA 1380 S17L LOWER SURFACE IAW SRM 51-10-02. BLENDED AREA L=1",W=1.5",D=.023",ORIGINAL MAT. .063" MAT REMAINING .040" FOUND OUT THE LIMITS IAW SRM 53-40-13 FIG 101 DET III. REMOVED AND REPLACED WEB IAW SRM 51-40-02. MINOR REPAIR.

ATA 5310

Part: CREASE BEAM — CORRODED (BS 1380-1400) · corrosion level 2 · airframe 53,534 hrs · 22,034 cycles

MAIN CABIN, STA 1380-1400, STR 17R, WL 208, CREASE BEAM WEB HAS CORROSION. REMOVED CORROSION ON BETWEEN STA 1380-1400 RT IAW SRM 51-10-02 BLENDED AREA L=1.6",W=1.0" D=.021" ORIG. MATERIAL .063 MAT REMAINING .042 FOUND OUT LIMITS IAW B757 SRM 53-40-13 FIG 101 DET III. REMOVED AND REPLACED WEB ON RT STA 1380-1400 STR 17R, WL 208, IAW SRM 51-40-02. MAJOR REPAIR.

ATA 5315

Part: FLOORBEAM — CORRODED (BS 345) · airframe 53,534 hrs · 22,034 cycles

CABIN FLOORBEAM TEE AT STA 345.0 BETWEEN LBL 24.75 AND LBL 45.5 HAS CORROSION. REMOVED CORROSION FROM T-CAP STA 345, LBL24-45, IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51, FIG 101, DETAIL III. ORIG MATERIAL .125 AFTER REWORK .106. L=20" W=.5 R & R UPPER TEE LBL 50 TO RBL 30 IAW SRM 53-00-51, FIG 201, REPAIR 3. CLASSIFIED CATEGORY "A" MAJOR REPAIR.

ATA 5315

Part: FLOORBEAM — CORRODED (BS 365) · corrosion level 2 · airframe 53,534 hrs · 22,034 cycles

STA 365, FLOORBEAM CORRODED AND GOUGED FROM BL 0 RBL 55. REMOVED CORROSION AND GOUGES FROM FLOOR BEAM UPPER CHORD STA 365 BL0-RBL55 IAW SRM 51-10-02. BOTH FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51 FIG 101 DETAIL III. ORIG MATERIAL .125 REMOVED 0.017. L=1.0 W=0.5. REMOVED UPPER CHORD AND INSTALLED REPAIR PARTS AT STA 365 FROM LBL 14 - RBL 70. IAW SRM 53-00-51 FIG 201 REPAIR 3. CLASSIFIED CATEGORY "A" MAJOR REPAIR

ATA 5315

Part: FLOORBEAM — CORRODED (BS 377) · airframe 53,534 hrs · 22,034 cycles

CABIN FLOOR FRAME T-CAP AT STA 377.7 FROM LBL 50.22 TO BL-0 CORRODED. REMOVED CORROSION STA 377 UPPER CHORD IAW SRM 51-10-02. REMOVED .017 FROM ORIG MATERIAL .125 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51, FIG 101, DETAIL III. L=2.0 W=.1.5. R & R UPPER CHORD IAW SRM 53-00-01 REPAIR 3 FROM RBL 30 TO LBL 62. CLASSIFIED CATEGORY "A" MAJOR REPAIR.

ATA 5315

Part: FLOORBEAM — CORRODED (BS 700) · corrosion level 2 · airframe 53,534 hrs · 22,034 cycles

CABIN FLOORBEAM AT STA 700 IN BETWEEN LBL 45.50 AND 58.22 CORRODED. REMOVED CORROSION IAW SRM 51-10-02 BLENDED AREA ORIG. MAT. .125 MAT LOSS .009", L=.014", W=2.050", D=.009". FOUND TO BE WITHIN LIMIT IAW SRM 53-00-51 FIG 101 DETAIL II. TREATED & PRIMED FLOORBEAM IAW SRM 51-20-01,TOP COATED AREA IAW AMM 25-00-7. MINOR REPAIR.

ATA 5315

Part: FLOORBEAM — CORRODED (BS 740) · corrosion level 2 · airframe 53,534 hrs · 22,034 cycles

CABIN FLOORBEAM PANEL HOLES AT STA 740 BETWEEN LBL-24.75 AND LBL-58-22 HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-02. BLEND OUT DIM L=8.0 W=2.0 D=.016. ORIG MATERIAL .125 AFTER REWORK .109 FOUND OUT OF LIMITS IAW SRM 53-00-51 FIG 101 DETAIL III. REPAIRED FLOORBEAM UPPER TEE. IAW SRM 53-00-01 FIG 201 REPAIR 1. CLASSIFIED CATEGORY "A" MAJOR REPAIR.

ATA 5310

Part: CREASE BEAM — CORRODED (BS 1260-1280) · corrosion level 2 · airframe 53,534 hrs · 22,034 cycles

MAIN CABIN AREA. LT SIDE BET BS 1260-1280 INBD CREASE BEAM CHORD WITH CORROSION. REMOVED CORROSION IAW SRM 51-10-02, BLENDED AREA L=40'", W=2.0" D=.013 ORIG. MAT. .070, REMAINING .057 OUT OF LIMITS, IAW SRM 53-60-13 FIG 101 DET. III. REMOVED REPLACE CREASE BEAM STA 1180-1280 LT IAW SRM 51-40-02. MAJOR REPAIR

ATA 5340

Part: STAND OFF — CORRODED (ZONE 200) · corrosion level 2 · airframe 53,534 hrs · 22,034 cycles

MAIN CABIN, BETWEEN STA. 1580-1600, STR. 17R, WL 208, 1EA STAND-OFF HAS CORROSION. (ATTACHED TO CREASE BEAM)

ATA 5313

Part: STRINGER — CRACKED (ZONE 200) · airframe 53,534 hrs · 22,034 cycles

STRINGER 9L AT STA 439 IS CRACKED. REMOVED STR 9L AL STA 439 AND STRINGER CLIP AT STA 418 ON S-9L FOR ACCESS IAW: SRM 51-40-02. ROUTED AND RECEIVED FROM FAB SHOP, REPAIR STRINGER TRAV NR T10/843350. LOCATED AND DRILLED REPAIR STRINGER 9L AT STA 439 AND STRINGER CLIP AT 9L STA 418, IAW SRM 51-40-05. INSTALLED REPAIR STRINGER AT 9L STA 418, IAW SRM 51-40-02, STRINGER PN FX -141N3370-17-N00720. MAJOR REPAIR.