N236FE

Part: BATTERY PACK — INOPERATIVE (SLIDE LIGHT) · airframe 69,939 hrs · 48,799 cycles

EMERGENCY SLIDE LIGHT INOPERATIVE. REPLACED BATTERY PACK IAW AMM 33-50-121-2, OPS CHECKED OK.

Part: FLOORBEAM — CORRODED (BS 400) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

CORROSION ON TOP TEE OF FLOORBEAM STA 400, BL 0 TO LBL 25. REPAIRED IAW BSOPM 20-30-03, NO CORROSION NOTED IAW SRM 51-10-6.

Part: FLOORBEAM — CORRODED (BS 720) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

CORROSION ON FLOORBEAM TOP TEE STA 720D, BL0 - LBL25. REPAIRED FLOORBEAM ON NR N00625, NO CORROSION NOTED IAW SRM 51-10-6.

Part: FLOORBEAM — CORRODED (BS 480) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

CORRODED TOP TEE ON FLOORBEAM, STA 480, RBL 45 - RBL 61 ACCOMPLISHED BS 480 FLOORBEAM REPAIR IAW EA 7-5310-152436 ON NR N00460.

Part: FLOORBEAM — CORRODED (BS 480) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

CORROSION TOP TEE ON FLOORBEAM STA 480, LBL 25 - LBL 45 ACCOMPLISHED REPAIR AT BS 480 FLOORBEAM IAW FX EA 7-5310-152436 ON NR N00460.

Part: FLOORBEAM — CORRODED (BS 480) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

CORRODED TOP FLOORBEAM TEE BS 480 RBL 20-26. ACCOMPLISHED FLOORBEAM REPAIR IAW EA 7-5310-152436 & SDR 11-3319.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

CORROSION ON SEAT TRACK SPLICE PLATE BS 380 - 395, LBL 25. REPLACED SEAT TRACK SECTION IAW DWG 53FX1457 & SRM 53-10-2, FIG 7A.

Part: SEAT TRACK — CORRODED (BS 360-380) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

CORROSION SEAT TRACK SPLICE PLATE BS 360 -380 LBL 25. FABRICATED A NEW SEAT TRACK SECTION IAW DWG 53FX1497 & SRM 53-10-2, FIG 7A,

Part: SEAT TRACK — CORRODED (BS 381-399) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

CORRODED SEAT TRACK BS 381-399, LBL 25. REPLACED SEAT TRACK SECTION IAW SRM 53-10-2, FIG 7A.

Part: SEAT TRACK — CORRODED (BS 480-690) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

CORRODED SEAT TRACK FLANGE RBL 25 STA 530 - STA 590. REPLACED SEAT TRACK SECTION.

Part: SEAT TRACK — CORRODED (BS 480-690) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

CORRODED SEAT TRACK FLANGE AND SCALLOPS STA 590 TO STA 690 RBL 45. REPLACED SEAT TRACK SECTION .

Part: SEAT TRACK — CORRODED (BS 590-690) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

CORRODED SEAT TRACK FLANGE & SCALLOPS STA 590 - 690, RBL 25 REPLACED SEAT TRACK SECTION.

Part: SEAT TRACK — CORRODED (BS 430-480) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

CORROSION SEAT TRACK FLANGE STA 430 - 480, LBL 45. REPLACED SEAT TRACK SECTION.

Part: KEELBEAM — CORRODED (BS 740-870) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

KEELBEAM BREATHER WEB HAS SEVERE EXFOLIATION CORROSION INSIDE & OUT OF WEB AT ACCESS PANEL NR 3209L. BREATHER WEB REPLACED ON NR N00413, SDR 3481.

Part: SEAT TRACK — CORRODED (BS 480-690) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

CORRODED SEAT TRACK SPLICE STA 480 TO STA 500, RBL 45, REPAIRED SEAT TRACK SECTION AND SPLICE.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

CORRODED SEAT TRACK LBL 45 STA 630-690. REPLACED SEAT TRACK SECTION ON NR N00448, W/O 00052276.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

CORROSION TOP TEE OF FLOORBEAM S 440 BETWEEN LBL 45-61. REPAIRED BS 440 TEE ON NR N00443, W/O 00052276.

Part: FLOORBEAM — CORRODED (BS 620) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

CORROSION TOP TEE ON FLOORBEAM BS 620, LBL 12 TO LBL 25 ACCOMPLISHED FLOORBEAM REPAIR ON NR N00504, WO 00052276, AND SDR11-3440.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

LT W/W STR 18A SHELF IS CORRODED IN SPOTS BTWN BS 870 - 940. REPLACED LT. W/W STR 18A SHELF ON NR N00323, W/O 00052276 REF SDR TRACKING NR 11-3114 FOR TRACKING CRITERIA.

Part: KEELBEAM — CORRODED (BS 740-870) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

KEELBEAM BREATHER WEB HAS SEVERE EXFOLIATION CORROSION INSIDE & OUT OF WEB AT ACCESS PANEL NR 3211L. BREATHER WEB REPLACED ON NR N00413, SDR11-3481.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

CORROSION ON STRINGER 27R, BS 740. ACCOMPLISHED REPAIR ON BS 740 S27R ON NR N01246, W/O 00052276.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

AFT PIT CEILING, FLOORBEAM LOWER FLANGE CORRODED AT BS 1130 BTWN LBL 24- BLO. THIS REPAIR WAS ACCOMPLISHED ON SNRM N00850 WO 00052276. NO WORK ACCOMPLISHED ON THIS SNRM.

Part: STRINGER — CORRODED (BS 720F) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

CORROSION ON STRINGER 26L ON ATTACH FASTENERS RUNNING JUST FWD JUST AFT OF FS 720F. ACCOMPLISHED REPAIR AT BS 720F STR 26L ON NR N00694. SEE SDR TRACKING NR 11-3271.

Part: STRINGER — CORRODED (BS 1183-1166) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

STRINGER 19L IS CORRODED BETWEEN BS 1183-1166. REPAIR WAS ACCOMPLISHED.

Part: FRAME — CORRODED (BS 950E) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

AFT PIT STUB FRAME BS 950E, 5IN IS CORRODED AT BOTTOM RBL4. REMOVED DAMAGED STUB FRAME AT BS 950E PLUS 5" RBL 4, FABRICATED & INSTALLED NEW STUB FRAME IAW DWG 65-56129, SRM 53-10-2 FIG 5, SRM 51-30-5, SRM 51-30-2.

Part: STRINGER — CORRODED (BS 1010 S29L) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

AFT PIT S29L IS CORRODED ON INBD SIDE JUST AFT OF BS 1010. CUT OUT DAMAGED STRINGER IAW SRM 53-10-3 FIG 1. FABRICATED STRINGER AND 2 SPLICES IAW SRM 53-10-3 FIG 1. INSTALLED STRINGER REPAIR PARTS IAW SRM 53-10-3 FIG 1.

Part: STRINGER — CORRODED (BS 1183 S30R) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

CORROSION BS 1183 STRINGER 30 OB FLANGE. REMOVED DAMAGE STRINGER SECTION, FABRICATED NEW STRINGER REPAIR & SPLICES, LOCATED & DRILLED NEW FITTING & WEB, INSTALLED NEW STRINGER REPAIR PARTS, FITTING & WEB IAW SRM 53-10-3 FIG 1 & SRM 51-30-2.

Part: BEAM — CORRODED (BS 1183) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

BS 1183, RBL 17.8 VERTICAL BEAM IS CORRODED WITH EXFOLIATION AT LOWER ATTACHMENTS. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW EA 7-5310-152433

Part: FLOORBEAM — DAMAGED (BS 480) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

MAIN CABIN BS 480 LBL 62 - LBL 45 FLOORBEAM ATTACH FITTING HAS DOUBLE DRILLED FASTENER HOLES. REMOVED & REPLACED FLOORBEAM SUPPORT FITTING IAW DWG 53FX1469 & EA 7-5310-152436.

Part: STRINGER SPLICE — CORRODED (BS 1070-1090) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

STRINGER 22R IS CORRODED BETWEEN BS 1070 - 1090. REMOVED STRINGER SPLICE IAW SRM 51-30-2. FABRICATED, LOCATED AND DRILLED NEW STRINGER SPLICE IAW DRAWING 65-75465. INSTALLED NEW STRINGER SPLICE IAW DRAWING 65-75465.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

BS 950C SHEAR TIE CORRODED BTWN S29 - 30L FWD SIDE. CUT OUT DAMAGED SHEAR TIE IAW SRM 53-10-4 FIG 13. FABRICATED SHEAR TIE REPAIR IAW SRM 53-10-4 FIG 13. INSTALLED REPAIR PART IAW SRM 53-10-4 FIG 13.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

AFT CARGO BAY BS 1090 FRAME SHEAR TIE IS CORRODED ON FWD SIDE BTWN S30 - S29L. CUT OUT DAMAGE IAW SRM 53-10-4 FIG 15. FABRICATED SHEAR TIE REPAIR PER SRM 53-10-4 FIG 15 AND INSTALLED REPAIR ANGLES IAW SRM 53-10-4 FIG 15.

Part: STRINGER — CORRODED (BS 740 S26R) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

CORROSION ON STR 26R, BS 740. CUTOUT DAMAGE AREA , FABRICATED FILLER AND SPLICE AND INSTALLED IAW SRM 51-30-2 AND SRM 53-10-3 FIG 1.

Part: SHEAR TIE — CORRODED (BS 1166 S25-26L) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

BS 1166 SHEAR TIE CORRODED ON AFT SIDE BETWEEN S25-26L. REMOVED SHEAR TIE, FABRICATED, AND INSTALLED REPAIR PARTS IAW SRM 53-10-4 FIG 13.

Part: KEELBEAM — CORRODED (BS 740) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

FWD END OF UPPER KEELBEAM BREATHER WEB AT FS 740 CORRODED COMPLETELY THROUGH WEB, WITH SEVERAL MORE AREAS OF SEVERE CORROSION IN SAME VICINITY. REMOVED DAMAGED KEEL BEAM STIFFNER PLATE, LOCATED DRILLED & INSTALLED NEW STIFFNER PLATE IAW SRM 51-30-5, SRM 51-10-2, & SRM 51-30-2, AND DWG 65-23555.

Part: STRINGER — CORRODED (BS 950-950A) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

STRINGER 30 IS CORRODED BETWEEN BS 950- 950A. CUT OUT DAMAGED AREA OF STRINGER SECTION. FABRICATED REPAIR, LOCATED AND DRILLED, TREATED AND PRIMED. INSTALLED REPAIR IAW EA 7-5310-152442.

Part: SHEAR TIE — CORRODED (BS 500 S27-28L) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

FRAME SHEAR TIE CORRODED, BS 500, STRINGER 27-28L. REMOVED SHEAR TIE. FABRICATED REPAIR, AND INSTALLED IAW SRM 53-10-4 FIG 15.

Part: FLOORBEAM — CORRODED (BS 1110) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

CORROSION TOP FLOORBEAM TEE BL 0 - LBL 25 BS 1110. CUTOUT DAMAGE AREA, FABRICATED AND INSTALLED NEW UPPER TEE SECTION, ANGLES AND STRAP IAW SRM 53-10-8 FIG 3, SRM 51-30-2, SRM 51-10-2.

Part: SHEAR TIE — CORRODED (BS 950B S27-28L) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

FRAME IS CORRODED BTWN S27-28L BS 950B LOWER FLANGE. CUT OUT DAMAGE AREA, FABRICATED REPAIR PARTS, AND INSTALLED IAW SRM 53-10-4 FIG 15.

Part: STIFFENER — CORRODED (BS 870) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

LT WHEEL WELL BS 870 LBL 25 VERT STIFFENER CORRODED AT TOP AND APPROX HALF WAY TO SHELF. REMOVED VERTICAL STIFFENER DAMAGE IAW B727 SRM 51-30-2 LOCATED NEW STIFFENER DIM: 57 5/8" IAW B727 SRM 53-10-2 FIG 5, SRM 51-30-5, AND INSTALLED NEW VERTICAL STIFFENER IAW SRM 51-30-2 & DWG 65-16330.

Part: WEB — CORRODED (BS 940) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

RT W/W PRESSURE WEB CORRODED BS 940, RBL 36 TO RBL 53. FABRICATED REPAIR DOUBLER AND FILLER, LOCATED AND DRILLED, TREATED AND PRIMED AREA AND PARTS, INSTALLED REPAIR PARTS IAW EA 7-5310-152440.

Part: STRINGER — CORRODED (BS 950B S28L) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

STRINGER 28L IS CORRODED ON FWD SIDE OF FRAME AT BS 950B. CUT OUT DAMAGE, FABRICATED REPAIR PARTS, AND INSTALLED IAW SRM 51-30-2 REV 103.

Part: STRINGER — CORRODED (BS 1030-1050) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

STRINGER 30 CORRODED BETWEEN BS 1030 TO 1050. CUT OUT DAMAGE AREA ON STRINGER 30 IAW SRM 53-10-3 FIG 1. FABRICATED NEW STRINGER SECTION AND SPLICE IAW SRM 53-10-3 FIG 1. INSTALLED ALL REPAIR PART IAW SRM 53-10-3 FIG 1.

Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

KEELBEAM BREATHER WEB HAS SEVERE EXFOLIATION CORROSION INSIDE & OUT OF WEB AT ACCESS PANEL NR 3212R. REMOVED KEEL BEAM UPPER WEB SECTION FROM BS 740 - BS 870. FABRICATED NEW KEEL BEAM UPPER WEB AND KEEL BEAM WEB ASSY STIFFENERS (4). INSTALLED NEW KEEL BEAM UPPER WEB SECTION FROM BS 740 - BS 870. INSTALLED NEW STIFFENERS AT UPPER WEB KEEL BEAM SECTION IAW SRM 51-10-6, SRM 53-10-1 FIG 1, SRM 51-30-2, SRM 51-30-5, DRAWING 65-86185-1, DRAWING 65-86186-1, SRM 51-10-2, DRAWING 65-23555 AND SRM 51-30-02.

Part: SHEAR TIE — CORRODED (BS 400 S27L) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

CORROSION AT CIRCUMFERENTIAL ATTACHMENT UNDER FLOOR IN E & E COMPT AT STR 27L AT FS 400. FABRICATED & INSTALLED NEW SHEAR TIE IAW B727 SRM 53-10-4 FIG 15 & SRM 51-30-2.

Part: STIFFENER — CORRODED (BS 870) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

RT W/W VERTICAL ANGLE IS CORRODED AT BS 870, RBL 16 OTBD OF LOAD CONTROL VALVE. REMOVED , & FABRICATED STIFFNER IAW DRAWING 65-16330. LOCATED AND DRILLED, INSTALLED NEW VERTICAL STIFFNER IAW SRM 51-30-2 AND SRM 51-30-5.

Part: TORQUE BOX — CRACKED (BS 1233) · airframe 69,823 hrs · 48,693 cycles

AFT AIRSTAIRS, LT LOWER TORQUE BOX, INBD WEB, UPPER ROW OF RIVETS HAVE CRACK AT BS 1233. CUT OUT DAMAGED AREA IAW SRM 51-10-1 REV 103. FABRICATED FILLER AND DOUBLER IAW SRM 53-10-2 FIG 6 AND 51-40-2 FIG 1. INSTALLED FILLER AND DOUBLER IAW SRM 51-40-2 FIG 1.

Part: SHEAR TIE — CORRODED (BS 1148 S28-29L) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

BS 1148 FRAME SHEAR TIE IS CORRODED BETWEEN S28-29L. CUT OUT DAMAGE, FABRICATED REPAIR AND INSTALLED IAW SRM 53-10-4 FIG 11.

Part: SHEAR TIE — CORRODED (BS 950A S26-27L) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

AFT PIT BS 950A FRAME SHEAR TIE IS CORRODED ON FWD SIDE BETWEEN S26-27L. REMOVED SHEAR TIE IAW SRM 53-10-04 FIG 15. FABRICATED, HEAT TREATED, LOCATED & DRILLED NEW SHEAR TIE, & INSTALLED IAW SRM 51-10-06, SRM 53-10-01 FIG 1, SRM 53-10-04 FIG 15, SRM 51-10-02, FAS ER 2-37153-801.

Part: SHEAR TIE — CORRODED (BS 1166 S28-29L) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

BS 1166 FRAME SHEAR TIE IS CORRODED FWD SIDE BETWEEN S28-29L. REMOVED DAMAGE IAW SRM 51-30-2, FABRICATED SHEAR TIE REPAIR IAW SRM 53-10-4 FIG 15. INSTALLED REPAIR IAW SRM 53-10-4 FIG 15.

Part: SHEAR TIE — CORRODED (BS 990 S29-30L) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

FRAME BS 990 IS CORRODED ON FWD SIDE BETWEEN S29-30L. CUT OUT DAMAGED SHEAR TIE. FABRICATED SHEAR TIE REPAIR IAW SRM 53-10-4 FIG 15 AND INSTALLED SHEAR TIE REPAIR IAW SRM 53-10-4 FIG 15.

Part: ANGLE — CORRODED (BS 740 S26R) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

VERTICAL ANGLE CORRODED ABOVE S26R, BS 740. REMOVED VERTICAL ANGLE IAW SRM 51-30-02. CUTOUT DAMAGE DIM: 2" X 3" AND FABRICATED REPAIR ANGLES & STRAPS IAW SRM 51-40-4 FIG 1. INSTALLED REPAIR PARTS IAW SRM 51-30-02 & SRM 51-40-4 FIG 1.

Part: SHEAR TIE — CORRODED (BS 950D S29-30L) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

FRAME SHEAR TIE IS CORRODED ON AFT SIDE AT BS 950D BETWEEN S29-30L. CUT OUT DAMAGED SHEAR TIE IAW SRM 53-10-4 FIG 15. FABRICATED REPAIR ANGLE IAW SRM 53-10-4 FIG 15. REPAIR INSTALLED IAW SRM 53-10-4 FIG 15.

Part: FLOORBEAM — CORRODED (BS 680) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

CORRODED FLOORBEAM UPPER TEE, BL 0 TO RBL 25, BS 680. CUTOUT DAMAGED UPPER TEE, FABRICATED & INSTALLED REPAIR IAW SRM 53-10-8 FIG 8.

Part: SHEAR TIE — CORRODED (BS 700 S27-28R) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

SHEAR TIE CORRODED BS 700 BETWEEN S27-28R FWD SIDE. CUT OUT DAMAGE SHEAR TIE IAW SRM 53-10-4 FIG 11. FABRICATED SHEAR TIE IAW SRM 53-10-4 FIG 11. INSTALLED SHEAR TIE IAW SRM 51-30-2 REV 103.

Part: SHEAR TIE — CORRODED (BS 720F S26R) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

SHEAR TIE CORRODED, BS 720F, O/B OF S26R. REMOVED SHEAR TIE IAW SRM 51-30-2. FABRICATED NEW SHEAR TIE IAW SRM 53-10-4 FIG 15. INSTALLED NEW SHEAR TIE IAW SRM 51-30-2 REV 103.

Part: SHEAR TIE — CORRODED (BS 720F S26L) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

SHEAR TIE CORRODED, BS 720F, S26L. CUTOUT DAMAGED AREA OF SHEAR TIE, FABRICATED AND INSTALLED NEW SHEAR TIE IAW SRM 53-10-4 FIG 15.

Part: SEAT TRACK — CORRODED (BS 890-1010) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

SEAT TRACK FLANGE CORRODED BL 0, BS 890 - 1010. REMOVED SEAT TRACK IAW SRM 51-30-2, FABRICATED SEAT TRACK SECTION IAW SRM 53-10-5 FIG 1, INSTALLED SEAT TRACK SECTION IAW SRM 51-30-2.

Part: SHEAR TIE — CORRODED (BS 640 S28L-R) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

SHEAR TIE CORRODED, BS 640, STR 28L TO 28R. REMOVED SHEAR TIE IAW SRM 51-30-2 FIG 1, FABRICATED REPAIR IAW SRM 53-10-4 FIG 15. INSTALLED REPAIR IAW SRM 53-10-4 FIG 15.

Part: SHEAR TIE — CORRODED (BS 500 S28L-R) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

AFT SIDE OF FRAME CORRODED, BS 500, S28L-R. CUT OUT DAMAGED SHEAR TIE IAW SRM 53-10-4 FIG 13. FABRICATED SHEAR TIE REPAIR IAW SRM 53-10-4 FIG 13. INSTALLED SHEAR TIE REPAIR IAW SRM 53-10-4 FIG 13.

Part: STRINGER — CORRODED (BS 1183-1166) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

STRINGER 22R IS CORRODED BTWN BS 1183 -1166 WITH EXFOLIATION UNDER POWERED OUTFLOW VALVE. CUT OUT DAMAGED STRINGER IAW SRM 53-10-3 FIG 1. FABRICATED REPAIR PARTS IAW SRM 53-10-3 FIG 1 AND INSTALLED IAW SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 1010-1130) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

CORRODED SEAT TRACK BS 1130-1010, BL 0. REMOVED SEAT TRACK SECTION IAW SRM 51-30-2. FABRICATED SEAT TRACK SECTION DIM: 120" IAW SRM 53-10-5 FIG 1 AND IAW SRM 53-10-5 FIG 1. INSTALLED SEAT TRACK IAW SRM 51-30-2.

Part: FLOORBEAM — CORRODED (BS 620) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

CORRODED TOP FLOORBEAM TEE BS 620 BL 0-RBL 25. CUTOUT DAMAGED AREA, FABRICATED REPAIR, TEE, SUPPORT ANGLES AND REINFORCEMENT STRAPS IAW SRM 53-10-8 FIG 3, INSTALLED FLOORBEAM REPAIR IAW SRM 53-10-8 FIG 3 AND SRM 51-30-2.

Part: SKIN — CRACKED (EMER EXIT DOOR) · airframe 69,823 hrs · 48,693 cycles

SKIN CRACKED AROUND FASTENER TOP AFT CORNER LT AFT EMERGENCY HATCH, EXTERIOR SKIN. CUTOUT DAMAGED SKIN AREA, FABRICATED REPAIR DOUBLER & FILLER, & INSTALLED REPAIR IAW SRM 52-00-3, SRM 51-10-2.

Part: SHEAR TIE — CORRODED (BS 660 S26-27L) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

FRAME SHEAR TIE CORRODED AT BS 660 BETWEEN S26-27L. REMOVED SHEAR TIE IAW SRM 51-30-2. FABRICATED NEW SHEAR TIE IAW DRAWING 69-43683 AND INSTALLED IAW SRM 51-30-2 REV 103.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

AFT PIT S28L IS CORRODED AT SPLICE AND ON INBD SIDE BETWEEN BS 970 - 990. REMOVED SPLICE AFT PIT STR 28L IAW SRM 51-30-2. FABRICATED NEW SPLICE IAW SRM 53-10-2, FIG 9 AND 53-10-3, FIG 1. INSTALLED NEW SPLICE IAW IAW SRM 51-30-2, REV 103.

Part: SHEAR TIE — CORRODED (BS 660 S27-28L) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

FRAME SHEAR TIE CORRODED AT BS 660, BETWEEN S27-28L. CUTOUT DAMAGED AREA, FABRICATED, AND INSTALLED NEW SHEAR TIE IAW SRM 53-10-4 FIG 15.

Part: SHEAR TIE — CORRODED (BS 660) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

FWD PIT, FRAME SHEAR TIE CORRODED AT BS 660, BETWEEN S28L-R. REMOVED & FABRICATED SHEAR TIE IAW SRM 53-10-4 FIG 15 AND INSTALLED IAW SRM 51-30-2 REV 103.

Part: SHEAR TIE — CORRODED (BS 560 S27L-28R) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

FRAME SHEAR TIE CORRODED BS 560, S27L-28R. CUT OUT DAMAGE, FABRICATED REPAIR PARTS IAW SRM 53-10-4 FIG 13 AND INSTALLED IAW SRM 51-30-2 REV 103.

Part: STRINGER — CORRODED (BS 990-1030) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

AFT CARGO BAY STRINGER 30 RT IS CORRODED BETWEEN BS 990-1030. FABRICATED NEW STRINGER SPLICE IAW SRM 53-10-3 FIG 1. & INSTALLED IAW SRM 51-30-2 REV 103.

Part: STRINGER — CORRODED (BS 740 S25R) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

FWD PIT BS 740, STR 25R HAS CORROSION ON STRINGER CHANNEL & SPLICE. FABRICATED FILLER AND SPLICE IAW SRM 53-10-3 FIG 1 AND INSTALLED IAW SRM 51-30-2.

Part: SHEAR TIE — CORRODED (BS 950E S27-28L) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

AFT PIT FRAME, BS 950E, SHEAR TIE CORRODED ON AFT SIDE BETWEEN S27- 28L. CUT OUT DAMAGED ON SHEAR TIE IAW SRM 53-10-4 FIG 15, FABRICATED REPAIR PARTS IAW SRM 53-10-4 FIG 15 AND INSTALLED REPAIR IAW SRM 53-10-4 FIG 15.

Part: FLOORBEAM — CORRODED (BS 680) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

CORRODED FLOORBEAM TOP TEE, LBL 25 TO 45, BS 680. CUTOUT DAMAGE AREA, FABRICATED FLOORBEAM REPAIR & INSTALLED REPAIR IAW SRM 53-10-8, FIG 3 & SRM 51-30-2.

Part: FAILSAFE — CRACKED (BS 580) · airframe 69,823 hrs · 48,693 cycles

BS 580 FRAME FAIL SAFE HAS CRACK INDICATION. REMOVED DOUBLER AND ANGLE IAW SRM 51-30-2, FABRICATED DOUBLER AND ANGLE IAW DWG 65-15932, INSTALLED DOUBLER AND ANGLE IAW SRM 51-30-2

Part: STRINGER — CORRODED (BS 620-640 S28R) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

STRINGER 28R CORRODED, BS 620 TO BS 640. REMOVED STRAP IAW SRM 51-30-2. FABRICATED, LOCATED AND DRILLED NEW STRAP IAW DRAWING 69-45557-1. INSTALLED NEW STRAP IAW DRAWING 69-45557-1 AND SRM 51-30-2.

Part: SHEAR TIE — CORRODED (BS 950C S29L/R) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

AFT PIT FRAME, BS 950C, SHEAR TIE CORRODED BTWN S29L - S29R, FWD SIDE. CUT OUT DAMAGE AREA IAW SRM 53-10-4, FIG 15. FABRICATED SHEAR TIE REPAIR ANGLE IAW SRM 53-10-4, FIG 15. INSTALLED REPAIR IAW SRM 53-10-4, FIG 15.

Part: SHEAR TIE — CORRODED (BS 500 S27-28R) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

FORWARD SIDE OF FRAME CORRODED, BS 500, STRINGER 27-28R. CUT OUT DAMAGE SHEAR TIE IAW SRM 53-10-4 FIG 13. FABRICATED SHEAR TIE REPAIR AND DOUBLER IAW SRM 53-10-4 FIG 13. REPAIR INSTALLED IAW SRM 53-10-4 FIG 13 REV 103.

Part: SEAT TRACK — CORRODED (BS 950F) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

CORRODED SEAT TRACK STA 950F, PLUS 10" TO STA 1135, LBL 45. REMOVED DAMAGED AREA IAW SRM 51-30-2. FABRICATED SEAT TRACK SECTION IAW SRM 53-10-5 FIG 1 AND INSTALLED IAW SRM 51-30-2.

Part: SHEAR TIE — CORRODED (BS 520 S27L-28R) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

FRAME SHEAR TIE CORRODED, BS 520, STR 27L TO STR 28R. CUT OUT DAMAGE SHEAR TIE IAW SRM 53-10-4 FIG 13. FABRICATED REPAIR SHEAR TIE AND DOUBLER IAW SRM 53-10-4 FIG 13. INSTALLED REPAIR IAW SRM 53-10-4 FIG 13 REV 103.

Part: SHEAR TIE — CORRODED (BS 950D S29L/R) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

AFT PIT FRAME AT BS 950D SHEAR TIE IS CORRODED BTWN S29L - S29R FWD SIDE. CUT OUT DAMAGE IAW SRM 53-10-4 FIG 15. FABRICATED REPAIR ANGLE IAW SRM 53-10-4 FIG 15. INSTALLED REPAIR ON SHEAR TIE IAW SRM 53-10-4 FIG 15.

Part: SHEAR TIE — CORRODED (BS 500 S25-26R) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

SHEAR TIE CORRODED BS 500, STRINGER 26R TO STRINGER 25R. REMOVED & REPLACED SHEAR TIE IAW SRM 51-30-2 & DWG 65-15928.

Part: FLOORBEAM — CORRODED (BS 1110) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

FLOORBEAM LOWER FLANGE CORRODED AT BS 1110 BTWN RBL 10 - 30. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-10-8 FIG 8 REV 103.

Part: STRINGER — CORRODED (BS 720C-720D) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

STRINGER 27L CORRODED, BS 720C-720D. CUT OUT DAMAGE IAW SRM 53-10-3 FIG 1. FABRICATED REPAIR PARTS IAW SRM 53-10-3 FIG 1. INSTALLED IAW SRM 51-30-2 REV 103.

Part: STRINGER — CORRODED (BS 660-680 S27R) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

CORROSION ON STRINGER 27R, BS 660-680. CUTOUT DAMAGE IAW SRM 53-10-3 FIG 1. FABRICATED NEW STRINGER SECTION AND SPLICE IAW SRM 53-10-3 FIG 1. INSTALLED IAW SRM 53-10-3 FIG 3 REV 103.

Part: FLOORBEAM — CORRODED (BS 1070) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

FLOORBEAM LOWER FLANGE IS CORRODED AT BS 1070 BTWN BL 0 - RBL 24. FABRICATED AND INSTALLED REPAIR ANGLES AND FILLER IAW SRM 53-10-8 FIG 8 REV. 103.

Part: FLOORBEAM — CORRODED (BS 440) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

CORROSION TOP TEE OF FLOORBEAM, BS 440 BETWEEN LBL 24 TO LBL 45. CUTOUT DAMAGED AREA, FABRICATED FLOORBEAM UPPER TEE REPAIR & REPAIR PARTS AND INSTALLED IAW SRM 53-10-8 FIG 3.

Part: FLOORBEAM — CORRODED (BS 480) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

CORROSION TOP FLOORBEAM TEE BS 480 BL 0 - LBL 25. CUTOUT DAMAGED BS 480 UPPER FLOORBEAM TEE, FABRICATED & INSTALLED NEW UPPER TEE IAW EA 7-5310-152436.

Part: FLOORBEAM — CORRODED (BS 950) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

CABIN FLOORBEAM AT BS 950 IS CORRODED ON LOWER SURFACE AT NUTPLATES BTWN LBL 30-66 WITH EXFOLIATION AT LBL 66. REMOVED STRAP SUPPORT FROM FLOORBEAM LOWER TEE, FABRICATED STRAP SUPPORT AND INSTALLED IAW SRM 51-30-2, SRM 51-10-2, SRM 51-10-6, SRM 53-10-1, FIG 8, AND DWG NR65-16338.

Part: FRAME — CORRODED (BS 970) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

AFT PIT, FRAME AND LOWER WEB ARE CORRODED ON FWD SIDE OF BS 970 WITH EXFOLIATION BTWN S30 - S29R. CUT OUT SHEAR TIE IAW SRM 53-10-4 FIG 12. FABRICATED SHEAR TIE REPAIR IAW SRM 53-10-4 FIG 12. INSTALLED REPAIR PARTS IAW SRM 53-10-4 FIG 15, REV 103.

Part: FLOORBEAM — CORRODED (BS 560) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

CORROSION TOP TEE FLOORBEAM BS 560, LBL 12. CUTOUT DAMAGE AREA, FABRICATED REPAIR AND INSTALLED IAW SRM 53-10-8, FOG 8 AND SRM 51-30-2.

Part: FLOORBEAM — CORRODED (BS 680) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

CORRODED TOP TEE FLOORBEAM BS 680 BETWEEN RBL 25 TO RBL 45. CUTOUT DAMAGE, FABRICATED REPAIR & INSTALLED IAW SRM 53-10-8 FIG 3 & SRM 51-30-2.

Part: FLOORBEAM — CORRODED (BS 1130) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

AFT PIT CEILING, FLOORBEAM LOWER FLANGE IS CORRODED BTWN RBL 24-45 AT BS 1130. REMOVED FLOORBEAM LOWER FLANGE IAW SRM 53-10-8, FIG 10A, FABRICATED NEW LOWER FLANGE OF FLOORBEAM IAW SRM 53-10-8, FIG 10A, INSTALLED FLOORBEAM REPAIR IAW SRM 53-10-8, FIG 10A.

Part: STRINGER — CORRODED (BS 720F-740 S23R) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

STRINGER 23R IS CORRODED BTWN BS 720F-740. CUT OUT DAMAGED STRINGER IAW SRM 53-10-3 FIG 1. FABRICATED NEW STRINGER SECTION AND SPLICE IAW SRM 53-10-3 FIG 1 AND 53-10-2 FIG 9 INSTALLED NEW STRINGER SECTION AND SPLICE IAW SRM 53-10-3 FIG 1.

Part: STIFFENER — CORRODED (BS 740) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

KEELBEAM BREATHER WEB PLATE STA 740, LBL 15, LOWER ACFT BAY AREA (STIFFNER) CORRODED. FABRICATED NEW KEEL BEAM STIFFNER. LOCATED, DRILLED AND DEBURRED NEW KEEL BEAM STIFFNER. INSTALLED NEW KEEL BEAM STIFFNER IAW SRM 53-10-1 FIG 1, DRAWING 66-15125, SRM 51-30-5, SRM 51-10-2 AND SRM 51-30-2.

Part: FLOORBEAM — CORRODED (BS 1110) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

FLOORBEAM TEE BS 1110, BL 0 - RBL 25 CORRODED. CUTOUT DAMAGE AREA TEE, FABRICATED AND INSTALLED NEW TEE SECTION IAW SRM 53-10-8 FIG 3, SRM 51-30-2, SRM 51-10-2.

Part: SEAT TRACK — CORRODED (BS 690-740) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

CORRODED SEAT TRACK FLANGE, LBL 25, BS 690-740. REMOVED SEAT TRACK SECTION, FABRICATED SEAT TRACK AND REPAIR AND INSTALLED IAW SRM 51-30-2, SRM 53-10-5 FIG 1, & SRM 51-10-2.

Part: FLOORBEAM — CORRODED (BS 1030) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

CORRODED FLOORBEAM TOP TEE BS 1030 BL 0 - RBL 25. CUTOUT DAMAGED AREA, FABRICATED AND INSTALLED FLOORBEAM UPPER TEE REPAIR IAW SRM 53-10-8 FIG 3.

Part: FLOORBEAM — CORRODED (BS 930) · airframe 69,823 hrs · 48,693 cycles

BS 930, LBL 44-56 FLOORBEAM CORRODED. REMOVED CORROSION, FOUND WITHIN LIMITS IAW EA 7-5310-152438, NO CORROSION WAS NOTED IAW SRM 51-10-6.

Part: SHEAR TIE — CORRODED (BS 950F S28-29L) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

AFT PIT SHEAR TIE CORRODED, STA 950F BETWEEN STR 28L - 29L. REMOVED DAMAGED PREVIOUS REPAIR, FABRICATED AND INSTALLED NEW REPAIR PARTS IAW SRM 53-10-4 FIG 11.

Part: FLOORBEAM — CORRODED (BS 560) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

CORRODED TOP FLOORBEAM TEE, BS 560, RBL 45 - 61. REMOVED CORROSION IAW SRM 51-10-6 WITH ORIGINAL MATERIAL .125 AND MATERIAL REMAINING .114, FOUND TO BE WITHIN LIMITS IAW SRM 53-10-1, FIG 4B. TREATED AND PRIMED IAW SRM 51-10-2.

Part: SUPPORT FITTING — CORRODED (BS 740 KEEL) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

CORROSION ON FS 740, FITTING & ITS ASSOCIATED HARDWARE ON RT SIDE AT KEELBEAM INSIDE RT ACFT BAY. ALSO, AREAS OF CORROSION ON FUSELAGE CIRCUMFERENCE IN SAME VICINITY. REMOVED DAMAGED SUPPORT FITTING, FABRICATED & INSTALLED NEW SUPPORT FITTING AT BS 740, RT SIDE IAW DWG 69-64841, SRM 51-30-5, & SRM 51-30-2.

Part: FLOORBEAM — CORRODED (BS 720D) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

CORROSION ON TOP FLOORBEAM TEE, BS 720D, BL 0 TO RBL 12. CUTOUT DAMAGE AREA, FABRICATED REPAIR & INSTALLED REPAIR IAW SRM 53-10-8, FIG 3 & SRM 51-30-2.

Part: STRINGER — CORRODED (BS 740 S26L) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

CORROSION ON THE END OF STR 26L AND STRINGER TIE AT BS 740. CUTOUT DAMAGED AREA IAW SRM 53-10--3 FIG 1, FABRICATED FILLER AND SPLICES IAW SRM 53-10-3 FIG 1 AND INSTALLED FILLER AND SPLICE'S IAW SRM 51-30-2.

Part: STRINGER — CRACKED (BS 600 S26L) · airframe 69,823 hrs · 48,693 cycles

FWD PIT S26L IS CRACKED AT BS 600. CUT OUT DAMAGED SECTION OF STRINGER IAW SRM 53-10-3 FIG 1. FABRICATED REPAIR ANGLES & INSTALLED IAW SRM 53-10-3 FIG. 1, REV. 103.

Part: STRINGER SPLICE — CORRODED (BS 480 S28R) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

STRINGER SPLICE CORRODED, BS 480, STR 28R. REMOVED DAMAGED STRINGER SPLICE. FABRICATED NEW SPLICE, AND INSTALLED IAW SRM 51-30-2 & DWG 69-14492.

Part: SEAT TRACK — CORRODED (BS 848-870) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

BS 848-870, RBL 24 SEAT TRACK AND HARDWARE HAVE CORROSION. REMOVED DAMAGED SEAT TRACK IAW SRM 51-30-2. FABRICATED AND INSTALLED NEW SEAT TRACK IAW SRM 53-10-2 FIG 7A, DWG 53FX1497 REV S, AND DWG 65-34144 REV C.

Part: SHEAR TIE — CORRODED (BS 1030 S29-30R) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

AFT PIT FRAME SHEAR TIE IS CORRODED ON FWD SIDE AT BS 1030 BTWN S29 - 30R.

Part: SHEAR TIE — CORRODED (BS 1148) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

AFT PIT BS 1148 FRAME SHEAR TIE IS CORRODED BTWN S30-29L. REMOVED PREVIOUS REPAIR IAW SRM 51-30-2. FAB NEW SHEAR TIE REPAIR IAW SRM 53-10-4, FIG 13. INSTALLED NEW SHEAR TIE REPAIR IAW SRM 53-10-4, FIG 13.

Part: WEB — CORRODED (BS 950) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

AFT PIT CANTED BULKHEAD SHELF AT BS 950, UPPER SURFACE IS CORRODED FROM LBL 50 - RBL 50. REMOVED WEB IAW SRM 51-30-2. FABRICATED REPAIR DOUBLER AND FILLER IAW SRM 51-40-2 FIG 1. INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 51-40-2 FIG 1. INSTALLED WEB IAW SRM 51-30-2, REV. 103.

Part: SHEAR TIE — CORRODED (BS 620 S27L-28R) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

FRAME CORRODED, BS 620, STR 27L TO 28R. CUTOUT DAMAGED AREA, FABRICATED, AND INSTALLED NEW SHEAR TIE IAW SRM 53-10-4 FIG 15. AREA CLEANED IAW BSOPM 20-30-03 WITH NO CORROSION NOTED IAW SRM 51-10-1. TREATED AND PRIMED AREA, IAW SRM 51-10-2, REV 103.

Part: FRAME — CORRODED (BS 1176) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

CORRODED BS 1176 FRAME LBL 45 - LB 55 STR 17 LEVEL MAIN CABIN. CUTOUT DAMAGE, AND INSTALLED NEW AND SPLICE IAW EA 7-5310-152432.

Part: STRUCTURE — MISREPAIRED (BS 1183) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

LOCK FASTENERS WITH NO SPACING ON FWD SIDE OF STA 1183, LBL 12.0, WL 190. ACCOMPLISHED REPAIR IAW EA 7-5310-150074.

Part: STRINGER — CORRODED (BS 1166-1183) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

AFT PIT S22L IS CORRODED BTWN BS 1166 - 1183. REMOVED DAMAGED STRINGER IAW SRM 53-10-3 FIG 1. FABRICATED REPAIR PARTS IAW SRM 53-10-3 FIG 1. INSTALLED REPAIR PARTS IAW SRM 51-30-2, REV 103.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

CORRODED SEAT TRACK FLANGE/ SCALLOPS BS 480- 530, RBL 45. REMOVED SEAT TRACK SECTION, FABRICATED & INSTALLED NEW SEAT TRACK SECTION IAW SRM 53-10-5, FIG 1, SRM 51-30-2, & SRM 51-10-2.

Part: SHEAR TIE — CORRODED (BS 720D S25-26R) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

SHEAR TIE CORRODED AT BS 720D, STRINGER 25 TO 26R. REMOVED CORRODED SHEAR TIE IAW SRM 51-30-2. FABRICATED NEW SHEAR TIE IAW SRM 53-10-4 FIG 15. INSTALLED NEW SHEAR TIE IAW SRM 53-10-4 FIG. 15, REV 103.

Part: TRIPLER — CORRODED (BS 1166-1183) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

AFT PIT LAV PAN TRIPLIER IS CORRODED BTWN BS 1183 -1166. REMOVED TRIPLER AND SUPPORT ANGLES IAW SRM 51-30-2. FABRICATED NEW TRIPLER IAW DWG 65-25607. TRIPLER, LAV PAN AND SUPPORT ANGLES INSTALLED IAW SRM 51-30-2 REV 103.

Part: STRINGER SPLICE — CORRODED (BS 480 S28L) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

STRINGER SPLICE CORRODED, BS 480, STR 28L. REMOVED SPLICE IAW SRM 51-30-2 REV. 103. FABRICATED NEW SPLICE IAW DRAWING 69-14492. INSTALLED NEW SPLICE IAW SRM 51-30-2.

Part: SHEAR TIE — CORRODED (BS 720E S26R) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

SHEAR TIE CORRODED, BS 720E, OTBD OF STRINGER 26R. REMOVED CORRODED SHEAR TIE IAW SRM 53-10-2. FABRICATED NEW SHEAR TIE REPAIR IAW SRM 53-10-4 FIG 15. INSTALLED NEW SHEAR TIE REPAIR IAW SRM 53-10-4 FIG 15.

Part: FLOORBEAM — CORRODED (BS 380) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

CORROSION TOP FLOORBEAM TEE, BS 380, LBL 25 - 45. CUTOUT DAMAGE AREA, FABRICATED FLOORBEAM REPAIR & INSTALLED REPAIR IAW SRM 53-10-8, FIG 8 & SRM 51-30-2.

Part: SHEAR TIE — CORRODED (BS 1148 S29-30R) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

AFT PIT BS 1148, FRAME SHEAR TIE IS CORRODED BETWEEN S29-30R. REMOVED DAMAGE, FABRICATED AND INSTALLED NEW REPAIR PARTS IAW SRM 53-10-4 FIG 13.

Part: FRAME — CORRODED (BS 700 S28L) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

FRAME CORRODED BS700, STRINGER 28L AND INTERCOSTAL. REMOVED SHEAR TIE IAW SRM 51-30-2. FABRICATED SHEAR TIE IAW SRM 53-10-4 FIG 15. INSTALLED SHEAR TIE IAW SRM 51-30-2 REV 103. REMOVED, FABRICATED NEW INTERCOSTAL, AND INSTALLED INTERCOSTAL IAW SRM 53-10-2, FIG 3, 51-20-1 AND 51-30-2.

Part: SHEAR TIE — CORRODED (BS 700 S27-28R) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

SHEAR TIE CORRODED AT STA 700 BETWEEN STRINGER 27R TO 28R AFT SIDE. REMOVED CORRODED SHEAR TIE IAW SRM 51-30-2. FABRICATED NEW SHEAR TIE IAW SRM 53-10-4 FIG 15. INSTALLED NEW SHEAR TIE IAW SRM 51-30-2 REV 103.

Part: SHEAR TIE — CORRODED (BS 950E S28-29L) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

AFT PIT FRAME, BS 950E, SHEAR TIE CORRODED AFT SIDE BETWEEN STRINGER 28L AND 29L. REMOVED CORROSION FROM SHEAR TIE IAW SRM REV 103 53-10-1 UPON VISUAL INSPECTION FOUND SHEAR TIE TO BE OUT OF LIMITS IAW SRM 51-10-6. REMOVED SHEAR TIE IAW SRM 53-10-4 FIG 13. FABRICATED NEW SHEAR TIE IAW SRM 53-10-4 FIG 13 HEAT TREATED TO T6 CONDITION IAW FORM FAS 0115 REV .001. FABRICATED DOUBLER, & INSTALLED IAW SRM 51-30-2 AND 53-10-4 FIG 13

Part: SEAT TRACK — CORRODED (BS 344-480) · airframe 69,823 hrs · 48,693 cycles

CORROSION ON SEAT TRACK FLANGE BL 0, STA 344 TO 480. REMOVED SEAT TRACK SECTION, FABRICATED & INSTALLED NEW SEAT TRACK SECTION IAW SRM 53-10-2, FIG 7A, SRM 53-10-5 FIG 1, SRM 51-30-2 & SRM 51-10-2, & DWG 53FX1497.

Part: SEAT TRACK — CORRODED (BS 380-480) · airframe 69,823 hrs · 48,693 cycles

CORROSION ON SEAT TRACK FLANGE STA 380 TO 480, LBL 25. REMOVED SEAT TRACK SECTION, FABRICATED AND INSTALLED NEW SEAT TRACK IAW SRM 53-10-5 FIG 1, 51-30-2, DWG 53FX1497, AND SRM 53-10-2 FIG 7A.

Part: SKIN — CORRODED (BS 950F S28-29L) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

AFT PIT FUSELAGE SKIN IS CORRODED WITH EXFOLIATION AT BS 950F, 3 IN BTWN S29L-S28L. CUT OUT DAMAGED SKIN, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-30-3 FIG 1.

Part: SEAT TRACK — CORRODED (BS 370-430) · airframe 69,823 hrs · 48,693 cycles

CORROSION ON SEAT TRACK FLANGE STA 370 TO 430 LBL 45. REMOVED SEAT TRACK , FABRICATED & INSTALLED NEW SEAT TRACK SECTION IAW SRM 53-10-2, FIG 7 & SRM 51-30-2 & SRM 51-10-2.

Part: SEAT TRACK — CORRODED (BS 344-480) · airframe 69,823 hrs · 48,693 cycles

CORRODED SEAT TRACK FLANGE, RBL 45 STA 344 TO 480. REMOVED DAMAGED SEAT TRACK SECTION, FABRICATED & INSTALLED NEW SEAT TRACK SECTION IAW SRM 53-10-5 FIG 1, SRM 53-10-2, FIG 7A, SRM 51-30-2, SRM 51-10-2, & DWG 53FX1497.

Part: SEAT TRACK — CORRODED (BS 720-720E) · airframe 69,823 hrs · 48,693 cycles

CORROSION ON SEAT TRACK FLANGE STA 720 TO 720E, 10" BL 0. REMOVED SEAT TRACK SECTION STA 720 TO STA 740 BL 0, IAW SRM 51-30-2. FABRICATED SEAT TRACK SECTION, IAW SRM 53-10-2, FIG 7A, INSTALLED SEAT TRACK SECTION, IAW SRM 51-30-2.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

AFT PIT S19L IS CORRODED AT HYD LINE ATTACH CLIP. REMOVED DAMAGED SECTION OF STRINGER IAW SRM 53-10-3 FIG 1. FABRICATED REPAIR PART IAW SRM 53-10-3 FIG 1. INSTALLED REPAIR PARTS IAW SRM 51-30-2 REV 103.

Part: SEAT TRACK — CORRODED (BS 480-600) · airframe 69,823 hrs · 48,693 cycles

CORRODED SEAT TRACK FLANGE BL 0, STA 480 TO 600. REMOVED DAMAGED SEAT TRACK SECTION, FABRICATED & INSTALLED NEW SEAT TRACK SECTION IAW SRM 51-30-2, SRM 51-10-2 & SRM 53-10-2, FIG 7A, DWG 53FX1492.

Part: SEAT TRACK — CORRODED (BS 480-590) · airframe 69,823 hrs · 48,693 cycles

CORRODED SEAT TRACK FLANGE RBL 25, STA 480 TO 590. REMOVED DAMAGED SEAT TRACK SECTION, FABRICATED & INSTALLED NEW SEAT TRACK SECTION IAW SRM 53-10-5, FIG 1, SRM 51-30-2, & SRM 51-10-2.

Part: SEAT TRACK — CORRODED (BS 370-430) · airframe 69,823 hrs · 48,693 cycles

CORROSION ON SEAT TRACK FLANGE STA 370 TO 430, LBL 45. REMOVED SEAT TRACK SECTION, FABRICATED & INSTALLED NEW SEAT TRACK SECTION IAW SRM 53-10-2, FIG 7AM, SRM 51-30-2 & SRM 51-10-2 & DWG NR 53FX1497.

Part: SEAT TRACK — CORRODED (BS 344-480) · airframe 69,823 hrs · 48,693 cycles

SEAT TRACK FLANGE CORRODED STA 344 TO 480, RBL 25. REMOVED DAMAGED SEAT TRACK SECTION, FABRICATED & INSTALLED NEW SEAT TRACK SECTION IAW SRM 53-10-5, FIG 1, SRM 51-10-2, SRM 53-10-2, FIG 7A, & DWG NR 53FX1497.

Part: SKIN — CORRODED (BS 700) · airframe 69,823 hrs · 48,693 cycles

CORROSION AROUND AND INSIDE FAIRING ATTACHMENT HOLES FORWARD OF RAM AIR INLETS AT APPROX FS 700. CUT OUT DAMAGED AREAS OF SKIN IAW SRM 53-30-3 FIG 3. FABRICATED REPAIR DOUBLER AND 3EA FILLERS IAW SRM 53-30-2 FIG 2 AND SRM 53-30-3 FIG 3. INSTALLED FILLERS AND REPAIR DOUBLER IAW SRM 51-30-2 REV 103.

Part: SKIN — DAMAGED (ZONE 100) · airframe 69,823 hrs · 48,693 cycles

UPON REMOVAL OF PREVIOUS REPAIR DOUBLER, FOUND NUMEROUS FASTENER HOLES WITH SHORT ED TO PREVIOUS REPAIR FILLER AND NUT PLATE RIVETS TO REPAIR FASTENER HOLES. APPROX BS 700, STR 28R SKIN REPAIR ACCOMPLISHED ON SNRM N00184, WO 00052276. NO MX WAS PERFORMED ON THIS SNRM. REF SDR TRACKING NR 11-3159 FOR REPORTING DOCUMENTATION.

Part: STRINGER — CORRODED (BS 700 S28R) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

STRINGER 28R CORRODED, BS 700. REMOVED STRINGER AND SPLICE IAW SRM 51-30-2 REV 103. FABRICATED NEW STRINGER SECTION AND SPLICE IAW SRM 53-10-3 FIG 1 AND 53-10-2 FIG 9. INSTALLED STRINGER SECTION AND SPLICE IAW SRM 51-30-2.

Part: STRINGER — CORRODED (BS 1166 S23R) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

UPON REMOVAL OF OUTFLOW VALVE, STR 23R, STA 1166 IS CORRODED AT CUTOUT. CUTOUT DAMAGED SECTION, FABRICATED STRINGER NEW STRINGER AND REPAIR SPLICE AND INSTALLED REPAIR PARTS IAW SRM 53-10-3 FIG1.

Part: STRINGER — CORRODED (BS 1166 S24R) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

UPON REMOVAL OF OUTFLOW VALVE, STR 24R, STA 1166 IS CORRODED AT CUTOUT. REMOVED STRINGER REPAIR AND SPLICE, FABRICATED NEW STRINGER AND SPLICE, AND INSTALLED NEW STRINGER AND SPLICE IAW SRM 51-30-2, SRM 53-10-3 FIG 1, AND SRM 51-10-2.

Part: WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

BS1183 "L" ANGLE AND WEB ARE CORRODED BETWEEN BL 0 TO LBL 8 ABOVE STR 30 AND 29L. REMOVED CORRODED ANGLE AND WEB. FABRICATED NEW WEB AND ANGLE AND INSTALLED IAW SRM 51-30-2, SRM 51-30-2, SRM 53-10-1 FIG 1, DWG 65C33041, SRM 51-10-2.

Part: ANGLE — CORRODED (BS 1183) · airframe 69,823 hrs · 48,693 cycles

BS 1183 "L" ANGLE AND WEB ARE CORRODED BETWEEN BL 0 TO LBL 8 ABOVE STR 30 AND 29L.

Part: SHEAR TIE — CORRODED (BS 1148) · airframe 69,823 hrs · 48,693 cycles

AFT PIT BS 1148, FRAME SHEAR TIE IS CORRODED ON FWD AND AFT SIDE WITH EXFOLIATION BETWEEN STR 28R -27R. CUTOUT DAMAGED AREA, FABRICATED & INSTALLED NEW SHEAR TIE IAW SRM 53-10-4 FIG 12.

Part: FLOORBEAM — CORRODED (BS 560) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

CORRODED FLOORBEAM TOP TEE, BL 0 TO RBL 25, STA 560. CUTOUT DAMAGE AREA, FABRICATED NEW REPAIR AND INSTALLED NEW REPAIR IAW SRM 53-10-8 FIG 3 & SRM 51-30-2.

Part: ANGLE — CORRODED (BS 1183) · airframe 69,823 hrs · 48,693 cycles

BS 1183 "L" ANGLE AND WEB ARE CORRODED BETWEEN BL 0 TO LBL 8 ABOVE STR 30 AND 29L.

Part: FRAME — PUNCTURED (BS 1110) · airframe 69,823 hrs · 48,693 cycles

AFT PIT BS 1110 FRAME, UPPER FLANGE IS PUNCTURED AND CRACKED ABOVE STR 27R. CUT OUT DAMAGE AREA IAW SRM 51-40-2, FIG 1. FABRICATED REPAIR PART IAW SRM 51-40-2, FIG 1. INSTALLED REPAIR DOUBLER IAW SRM 51-40-2, FIG 1.

Part: SHEAR TIE — CORRODED (BS 1130) · airframe 69,823 hrs · 48,693 cycles

AFT PIT BS 1130 FRAME SHEAR TIE IS CORRODED WITH EXFOLIATION BETWEEN STR 28-29R. CUT OUT DAMAGE AREA IAW SRM 53-10-4, FIG 13. FABRICATED SHEAR TIE REPAIR PARTS IAW SRM 53-10-4 FIG 13. INSTALLED SHEAR TIE REPAIR PARTS IAW SRM 53-10-4, FIG 13.

Part: WEB — CRACKED (BS 1243) · airframe 69,823 hrs · 48,693 cycles

AFT AIRSTAIR LOWER TORQUE BOX LT WEB CRACKED AT LIGHTING HOLE, BS 1243. CUT OUT DAMAGE IAW SRM SRM 51-10-1 REV 103, FABRICATED DOUBLER IAW SRM 51-40-2 FIG 1, INSTALLED DOUBLER IAW SRM 51-40-2 FIG 1.

Part: WEB — CRACKED (BS 1323) · airframe 69,823 hrs · 48,693 cycles

AFT AIRSTAIR, LT LOWER TORQUE BOX, AFT LOWER LIGHTING HOLE CRACKED, BS 1323. CUT OUT DAMAGE (CRACK) IAW SRM 51-10-1 REV 103. REMOVED PREVIOUS REPAIR DOUBLER IAW SRM 51-30-2. FABRICATED DOUBLER TO INCLUDE BOTH REPAIRS IAW SRM 51-20-1 FIG. 7 AND 51-30-5. INSTALLED REPAIR DOUBLER IAW SRM 51-30-2 AND 51-40-2 FIG 1.

Part: STRINGER — CORRODED (BS 540 S28L) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

STRINGER 28L CORRODED, AT BS 540 FRAME. CUT OUT CORRODED STRINGER SECTION IAW SRM 53-10-3 FIG 1. FABRICATED STRINGER SECTION, CHANNEL, AND REPAIR ANGLE IAW SRM 53-10-3 FIG 1. INSTALLED STRINGER SECTION, CHANNEL SECTION, AND REPAIR ANGLE IAW SRM 51-30-2 REV 103.

Part: FLOORBEAM — CORRODED (BS 400) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

CORRODED FLOORBEAM TEE, BL 0 TO RBL 25, BS 400. CUT OUT DAMAGE, FABRICATED AND INSTALLED UPPER TEE AND REPAIR PARTS IAW SRM 53-10-8, FIG 3, 51-10-2, AND 51-30-2.

Part: SEAT TRACK — CORRODED (BS 480-690) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

CORROSION SEAT TRACK FLANGE STA 480 - STA 690, LBL 25. REMOVED SEAT TRACK SECTION AND SPLICE IAW SRM 51-30-2. FABRICATED NEW SEAT TRACK SECTION AND SPLICE, INSTALLED SEAT TRACK AND SPLICE IAW SRM 53-10-5 FIG 1 AND SRM 51-30-2.

Part: KEELBEAM — CORRODED (BS 740-870) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

TWO SPOTS OF CORROSION ON KEELBEAM LWR SURFACE AT APPROX FS 760. ACCOMPLISHED REPAIR AT KEELBEAM LWR SURFACE AT FS 760 ON N00243.

Part: ACCESS PANEL — DAMAGED (LT ELEVATOR) · airframe 69,823 hrs · 48,693 cycles

LEFT ELEVATOR BOTTOM ACCESS PANEL SCREW HOLE HAS ELONGATED HOLE ON SKIN. FABRICATED REPAIR DOUBLER IAW SRM 55-20-3 FIG 1. INSTALLED DOUBLER IAW SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 690-720D) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

CORROSION SEAT TRACK FLANGE STA 690 - STA 720D, LBL 25. REMOVED SEAT TRACK SECTION IAW SRM 51-30-2. FABRICATED NEW SEAT TRACK SECTION AND INSTALLED IAW SRM 53-10-5 FIG 1 AND SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 480-630) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

CORROSION SEAT TRACK FLANGE STA 480 - STA 630, LBL 45. REMOVED SEAT TRACK SECTION FROM BS 480- 690 LBL 45, FABRICATED AND INSTALLED NEW SEAT TRACK SECTION AT BS 480 - 690 LBL 45 IAW SRM 53-10-5, FIG 1, SRM 51-10-2, SRM 51-30-2.

Part: STRINGER — CORRODED (BS 960-940 S18A) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

LEFT W/W STR 18A, SHELF IS CORRODED BETWEEN BS 930-940 AND HAS CORRODED HARDWARE ON UPPER SURFACE. REMOVED DAMAGED STRINGER 18A, FABRICATED NEW SHELF & INSTALLED NEW STR 18A IAW DWG NR 65-22419, SRM 51-30-2, SRM 51-20-1, SRM 51-30-5, & SRM 51-10-2.

Part: KEELBEAM — CORRODED (BS 804) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

EXFOLIATED CORROSION ON KEELBEAM LWR SURFACE AT LIGHTNING HOLE AT FS 804. REMOVED DAMAGED WEB AND "T" ANGLE FITTINGS (3) AT BS 740 -BS 870 BL0. FABRICATED NEW KEEL BEAM LOWER WEB. LOCATED, DRILLED, AND DEBURRED NEW TEE FITTINGS. INSTALLED NEW TEE FITTINGS AND NEW LOWER WEB (KEEL BEAM AREA) IAW SRM 51-30-2, SRM 53-10-1 FIG 1, SRM 53-10-2 FIG 1, SRM 51-30-5, SRM 51-10-2, AND DRAWING 65-23555.

Part: VERTICAL BEAM — CORRODED (BS 1183) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

BS 1183, LBL 8.0, VERTICAL BEAM IS CORRODED AND HAS CORRODED LOCK FASTENERS. REPAIRED IAW SRM 51-30-2, DWG 65C29080, SRM 51-10-2 AND SRM 51-30-2.

Part: SKIN — CRACKED (RT WING TE FLAP) · airframe 69,823 hrs · 48,693 cycles

RT INBD MID FLAP T/E FWD SURFACE IS CRACKED AT MECHANISM CUTOUT, WBL 100. REMOVED AND REPLACED RH I/B MIDFLAP ASSY IAW MM 27-51-001-4. OPERATIONAL CHECK PERFORMED IAW MM 27-51-001-5. NO DEFECTS NOTED.

Part: FAILSAFE — CORRODED (BS 1166) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

BS 1166, FAIL SAFE CHORD IS CORRODED WITH EXFOLIATION BETWEEN STR 29L - 28L. REMOVED FAIL SAFE CHORD IAW DWG NR 65-16349. FABRICATED NEW FAIL SAFE CHORD IAW DWG 65-16349. INSTALLED NEW FAIL SAFE CHORD IAW DWG 65-16349.

Part: STRINGER — CORRODED (BS 740 S23L) · corrosion level 2 · airframe 69,823 hrs · 48,693 cycles

STR 23L IS CORRODED COMPLETELY THROUGH AT SHEAR TIE JUST FWD OF FS 740 BULKHEAD IN ACFT DIST COMPT. CUT OUT DAMAGE AREA IAW SRM 53-10-3 FIG 1. FABRICATED REPAIR PARTS IAW SRM 53-10-3 FIG 1 AND INSTALLED REPAIR PARTS IAW SRM 51-30-2.

Part: SWITCH — FAILED (ESCAPE SLIDE) · airframe 69,780 hrs · 48,654 cycles

OPEN RT FOUND EMERGENCY SLIDE LIGHT SWITCH CABLE BALL OUT OF SOCKET. LIGHT EXTINGUISHED. TRIED NEW BATTERY PACK, NO HELP. REINSTALLED ORIGINAL BATTERY PACK IAW MM 33-50-121-2. RELAMPED, NO HELP. REMOVED BATTERY & CHECKED WIRING AT BATTTERY CONNECTORS, SHOWS OPEN WITH BALL, REMOVED FROM SWITCH. SUSPECT SWITCH. RELEASED FOR SERVICE IAW MEL: 33-16-02-A. R & R BALL SWITCH ASSY. IAW AMM 33-50-121-2 & CLOSED UP L1 DOOR IAW SMP. OPS NORMAL.

Part: CHARGER — OVERHEATED (E & E BAY) · airframe 62,638 hrs · 43,292 cycles

THE BATTERY CHARGER STARTED TO SMOKE AND THE BATTERY GOT VERY HOT 170 DEGREES. THE AIRCRAFT WAS IN THE HANGAR HAVING AN ALL LANDING GEAR CHANGE AND ON JACKS.

Part: FIRE DETECTOR — FALSE ACTIVATION (NR 4 CARGO BAY) · airframe 62,474 hrs · 43,164 cycles

DURING CLIMBOUT FROM ONT A/C HAD FIRE WARNING WITH CORRESPONDING NR 4 MAIN CARGO LIGHT ILLUMINATED. PERFORMED QRH & RETURNED TO ONT. SMOKE LIGHT REMAINED ON UNTIL PULLING INTO THE ONT RAMP. VISUAL INSPECTION AFTER LANDING REVEALED NO INDICATION OF FIRE OR SMOKE.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 62,437 hrs · 43,141 cycles

BULKHEAD 870 SUPPORT ANGLE IN RT WHEEL WELL IS CRACKED WL 180 RBL 8 BS 870 FOUND ON FED EX QA WALK. REMOVED AND REPLACED 870 BULKHEAD SUPPORT ANGLE RT WHEEL WELL, LEAK CHECK GOOD ON DUCTS. REINSTALLED ALL ITEMS REMOVED FOR ACCESS IAW FED EX MM 36-00-000-5 AND SRM 51-30-2, 51-10-1, 51-30-5.

Part: SKIN — CORRODED (FUSELAGE) · airframe 62,437 hrs · 43,141 cycles

SKIN PILLOWING STA 1040 - 1060 STR 28L. REPAIRED SKIN AT BS 1010 TO 1100 STR 26R TO 26L PER FED EX EA 7-5330-55202 AND SRM 53-30-3 FIG 12.

Part: SKIN — DENTED (LT WING) · airframe 62,437 hrs · 43,141 cycles

DENT ON LT WING FIXED L/E SKIN AT NR 3 SLAT TAI DUCT. DENT ON L/W FIXED L/E SKIN AT NR 3 SLAT TAI DUCT, FOUND TO BE OUT OF LIMITS IAW SRM 57-20-1. REPAIRED DENT IAW SRM 57-30-4 PG 2

Part: DOOR FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,437 hrs · 43,141 cycles

CORROSION 1) NR 1 CARGO DOOR CUTOUT FWD FRAME BETWEEN WEB AND I/B CHORD STA 560 RBL 26 WL 166. CORROSION NR 1 CARGO DOOR CUT OUT FWD FRAME BETWEEN WEB AND I/B CHORD STA 560, RBL 26, WL 166, FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REPAIRED DAMAGE AREA PER EA 7-5310- 70612.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,437 hrs · 43,141 cycles

CORROSION (C53-113-01(1) FWD CARGO BAY BS 720 SHEAR TIE CORRODED, BETWEEN STR 27R - 28R WL 149 AFT SIDE OF FRAME. REMOVED CORROSION FROM SHEAR TIE AT BS 720 BETWEEN STR 27R AND 28R WL 149 MATERIAL LOSS WAS .010 DEEP X 1 X 1.25 FROM AN ORIGINAL THICKNESS OF .050 AND IS OUT OF LIMITS IAW SRM 53-10-1. CUT OFF DAMAGED SHEAR TIE AND INSTALLED REPAIR IAW SRM 53-10-4 FIG 13.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,437 hrs · 43,141 cycles

CORROSION IN FWD CARGO BAY BS 640 SHEAR TIE CORRODED BETWEEN STR 27R - 26R WL 149 AFT SIDE OF FRAME. REMOVED CORROSION FROM SHEAR TIE AT BS 640 BETWEEN STR 27R AND 26R. MATERIAL LOSS WAS .017 DEEP X 1 X 4 INCHES FROM AN ORIGINAL THICKNESS OF .058 AND IS OUT OF LIMITS IAW SRM 53-10-1. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-30-2.

Part: SLIDE — MISINSTALLED (CABIN) · airframe 62,437 hrs · 43,141 cycles

UPON INCOMING INSPECTION FOUND ESCAPE SLIDE STILL HAD SAFETY STRAP FOR SHIPPING INSTALLED. REMOVED SAFETY STRAP PER FED EX M.M. 25-60-015-2

Part: SKIN — DENTED (FUSELAGE) · airframe 62,437 hrs · 43,141 cycles

DENT ON FUSELAGE SKINS AT 1090 BELOW STR 20L. DENT ON FUSELAGE SKIN BS 1090 BELOW STR 20 LT FOUND TO BE OUT OF LIMITS PER SRM 53-30-1. REPAIRED DAMAGED AREA PER SRM 53-30-3.

Part: SKIN — CORRODED (FUSELAGE) · airframe 62,437 hrs · 43,141 cycles

SKIN PILLOWING STA 1110 - 1130 STR 28L. REMOVED CORROSION FROM SKIN BS 1115 UNDER STR 28L AREA 1X2X.025 FROM ORIGINAL .052 FOUND OUT OF LIMITS PER SRM 53-30-1. REMOVED CORROSION FROM STR 28L AREA 1X1 X 100 PERCENT MATERIAL LOSS AT BS 1115 FOUND OUT OF LIMITS PER SRM 53-10-1. REPAIRED SKIN PER SRM 53-30-03 FIG 3. REPAIRED STRINGER 28L PER SRM 53-10-3 FIG 1

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,437 hrs · 43,141 cycles

CORROSION ON SKIN STA 1090 STR 27R - 29R. REMOVED CORROSION ON SKIN AT BS 1090, STR 27R-29R AND INSTALLED REPAIR DOUBLER PER SRM 53-30-3 FIG 3.

Part: ENGINE — MALFUNCTIONED (NR 2) · airframe 62,009 hrs · 42,789 cycles

AT FL330, NR 2 ENGINE OIL TEMP ROSE TO HIGH IN THE YELLOW RANGE. ADDING FUEL FLOW BY INCREASING THROTTLE DID NOT HELP. AFTER 15 MINS IN YELLOW BAND, SHUTDOWN NR 2 ENGINE IAW ENGINE FAILURE/SHUTDOWN CHECKLIST. WHEN THROTTLE RETARDED TO IDLE, NR 2 ENG OIL TEMP ROSE ABOVE RED LINE BY 10 DEGREES. SHUTDOWN SUCCESSFUL, LANDED AT KCLE WITH NO FURTHER INCIDENT. IAW WORK CARD 70TOOO2 REPLACED NO.2 ENGINE.

Part: TRANSFORMER — FAILED (WEATHER RADAR) · airframe 61,977 hrs · 42,767 cycles

ON THE 20-40 MILE RANGE THE FAIL MESSAGE APPEARS WITH NO RETURNS. AT THE 80 MILE RANGE IT WOULD WORK INTERMITTENLY. REMOVED AND REPLACED WX RADAR R/T IAW 727 M/M 34-41-041-4. OK FOR SERVICE.

Part: INDICATOR — FAILED (TAT) · airframe 61,860 hrs · 42,689 cycles

TAT INDICATOR INTERMITTANT. INDICATOR FAILED ON CLIMBOUT WITH OFF FLAG CYCLING FOR 30 SEC. THEN FAILED WITH SOLID OFF FLAG FOR 60 MIN. INDICATOR CAME BACK ON DURING APPROACH. REMOVED AND REPLACED TAT INDICATOR & OPS CHECKED PER 727-200 MM 34-13-000-5. ALL INDICATIONS NORMAL.

Part: INDICATOR — MALFUNCTIONED (TE FLAPS)

AFTER TAKE OFF, HAD INDICATION OF ASYMMETRICAL OUTBOARD FLAPS LOCKED OUT. R&R INDICATOR PER MM 27-52-021-2.

Part: TRANSMITTER — INOPERATIVE (LH OB FLAP)

02-35 REPEAT AFTER T/O HAD IND OF ASYMMETRICAL OUTBOARD FLAPS LOCKED OUT. R&R OUTBOARD POS TRANSMITTER PER MM 27-52-013-4.

Part: DUCT

N1275 TEST FLT LWR AFT CARGO SMOKE WARN @ FL 230 HAD ENGINE & WING ANTI ICE TURNED ON, WENT OUT WHEN PWR WAS REDUCED. S/D TESTED TAI & ENG ANTIICE, CND WORK DONE PER SRM 20-50-01, MM 30-13-000-5 & 30-21-001-5.

Part: SHEAR TIE — CORRODED (FUSELAGE)

CORROSION (C53-111-02, 2) FWD CARGO BAY BS 700, RBL 9, WL 148 SHEAR TIE FWD & AFT SIDE OF FRAME. REMOVED AND REPLACED SHEAR TIE PER SRM 53-10-4 FIG 15.

Part: FRAME — DAMAGED (FUSELAGE)

BS 1070 FRAME IS CRUSHED OVER STR 26R. REMOVED AND REPLACED FRAME PER SRM 51-40-3.

Part: FRAME — CORRODED · corrosion level 2

N 701 CORROSION ON FRAME BS 580, RBL 10, WL 148. ** S/D ** COMING

Part: SKIN — TORN (RUDDER)

UPPER FWD LT CORNER OF LWR RUDDER HAS SECTION OF OUTER SKIN TORN. REMOVED AND REPLACED RUDDER PER EA 7-5540-58476.

Part: SHEAR TIE — CORRODED (FRAME)

N 701 CORROSION ON FRAME BS 580, RBL 10, WL 148. ** S/D ** R&R SHEAR TIE PER SRM 53-10-4 FIG 14.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2

CORROSION (C53-111-02, 2) FWD CARGO BAY BS 720D, RBL 16, WL 150 SHEAR TIE. *S/D* REMOVED AND REPLACED SHEAR TIE PER SRM 53-10-4 FIG 15.

Part: SHEAR TIE — CORRODED · corrosion level 2

N 671 CORROSION EMANATING UNDER SHEAR TIE AT BS 1148 BETWEEN STR 27 AND 28L. ** S/D ** COMING

Part: SHEAR TIE — CORRODED

N 1008 CORROSION ON SHEAR TIE AT BS 720C BL0, WL 148 R&R SHEAR TIE PER IAW SRM 51-20-1.

Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2

CORROSION ON VERTICAL STIFFENER AT BS 740 BULKHEAD JUST O/B OF STR 26R, WL 145 - 151. *S/D* REMOVED AND REPLACED PER SRM 51-10-2, 51-30-2.

Part: FLOORBEAM — CORRODED (FUSELAGE)

CORROSION ON TOP OF FLOORBEAM BS 950, BL 0-RBL 25, WL 208. *S/D* REMOVED AND REPLACED FLOORBEAM PER SRM 53-10-1, 51-30-2, 51-30-5, 51-30-8.

Part: SHEAR TIE — CORRODED (FUSELAGE)

CORROSION (C53-113-01-1) ON SHEAR TIE BS 660 BETWEEN STR 25R & 26R. *S/D* REMOVED AND REPLACED SHEAR TIE PER SRM 51-30-5.

Part: FRAME — DENTED (UPPER FLANGE)

N 852 DENT IN UPPER FLANGE OF FRAME AT BS 970, WL 150, LBL 30. ** S/D ** COMING

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2

CORROSION FWD CARGO BAY BS 640, RBL 3, WL 147 SHEAR TIE. *S/D* REMOVED AND REPLACED SHEAR TIE PER SRM 53-10-4.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2

CORROSION ON FLOORBEAM BS 1070, WL 200, LBL 65-RBL 65. *S/D* REMOVED AND REPLACED FLOORBEAM PER SRM 53-10-8, 51-30-2.

Part: SHEAR TIE — CRACKED

N 992 CRACKED SHEAR TIE BS 720, LBL 4, WL 148. ** S/D ** R&R SHEAR TIE.

Part: WEB — CRACKED (RH STUB BEAM)

N 795 R/H STUB BEAM FWD AND AFT WEB CRACKED BS 848, RBL 60, WL 202. ** S/D ** COMING

Part: STRINGER CLIP — CRACKED

N 1017 FUSELAGE STR CLIP AT STR 232 IS CRACKED AT BS 580. R&R CLIP.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · corrosion level 2

STRINGER CLIP CRACKED BS 804.5, STR 7L. *S/D* REMOVED AND REPLACED CLIP PER SRM 51-30-2.

Part: FLOORBEAM — CORRODED (FUSELAGE)

CORROSION (C53-224-01, 3) ON TOP OF FLOORBEAM BS 950, BL 0 TO RBL 25, WL 208. *S/D* REMOVED AND REPLACED FLOORBEAM PER SRM 51-30-2, 51-30-5, 51-30-8.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2

CORROSION ON STRINGER 23R, BS 397. *S/D* REMOVED AND REPLACED STR PER SRM 53-10-3 & EA 7-5310-58479.

Part: FRAME — DENTED (UPR FLANGE)

N 852 DENT IN UPR FLANGE OF FRAME BS 970, WL 150, LBL 30. ** S/D ** COMING

Part: FRAME — CORRODED (UPPER FLANGE) · corrosion level 2

N 669 UPR FLANGE OF BS 1130 FRAME HAS 2 EA OPEN HOLES WITH CORROSION UNDER L/H FLOOR TO SIDEWALL SUPPORT C53-111-01(3). ** S/D ** COMING

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2

CORROSION AT STR 25R AT BS 415 AT STR 9. *S/D* REMOVED AND REPLACED SKIN PER EA 7-5310-58485.

Part: STRINGER — DAMAGED (FUSELAGE)

BS 480, STR 8L DOUBLE HOLES AND DAMAGE. REMOVED AND REPLACED STR PER EA 7-5310-59211 & SRM 53-10-3.

Part: SPLICE — CORRODED (FUSELAGE) · corrosion level 2

CORROSION (C53-111-02, 2) FWD CARGO BAY BS 640 - 644, RBL 23, WL 150 STR 26R. *S/D* REMOVED AND REPLACED STRINGER SPLICE.

Part: STRINGER — CRACKED (FUSELAGE)

AFT STRINGER ATTACHMENT ON LT LEADING EDGE WING ILLUM LIGHT IS CRACKED. *S/D* REMOVED AND REPLACED STR ON LEFT L/E WING LIGHT PER SRM 53-10-3.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2

BS 1148 FRAME HAS BULGE IN CENTER WEB OF STR 29R. *S/D* REMOVED AND REPLACED FRAME PER SRM 53-10-3.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2

FUSELAGE STR CHANNEL STR 27L IS CORRODED AT BS 474 ON O/B SIDE (C53-111-01, 2). *S/D* REMOVED AND REPLACED STR PER MM 52-20-011-7, SRM 51-30-2.

Part: FRAME — DENTED (FUSELAGE)

DENT IN TOP FLANGE OF FRAME AT BS 970, LBL 46, WL 162 AFT CARGO BAY. *S/D* REMOVED AND REPLACED FRAME PER SRM 51-40-3.

Part: FRAME — CORRODED (BS 1110) · corrosion level 2

HOLE & CORROSION IN UPR FLANGE OF FRAME AT BS 1110. R&R FRAME PER SRM 51-40-3.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2

FUSELAGE STR 27L HAS GOUGE ON O/B SIDE WITH CORROSION AT BS 482 (C53-111-01, 2). *S/D* REMOVED AND REPLACED STR PER SRM 57-40-3.

Part: FRAME — CORRODED (FUSELAGE)

UPPER FLANGE OF BS 1090 FRAME HAS OPEN HOLE WITH CORROSION UNDER LT FLOOR TO SIDEWALL SUPPORT.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2

CORROSION (C53-111-02, 2) FWD CARGO BAY BS 660, BL 0, WL 147 SHEAR TIE. *S/D* REMOVED AND REPLACED SHEAR TIE PER SRM 53-10-4 FIG 15.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2

UPON REMOVAL OF STR ON N1173 FOUND CORROSION ON INNER SKIN AT BS 950A+3 TO 950A+6 AT STR 25L (C53-111-01-3). *S/D* REMOVED AND REPLACED SKIN PER SRM 53-30-3 FIG 3.

Part: FRAME — DAMAGED (FUSELAGE)

FUSELAGE FRAME BS 580 UPPER FLANGE HAS DAMAGE BETWEEN STR 23L & 25L. *S/D* REMOVED AND REPLACED FRAME PER SRM 51-4-3 PG 1-6.

Part: SKIN — CRACKED (FUSELAGE)

CRACK IN FUSELAGE SKIN AT BS 1097.5 1 INCH RIGHT OF STRINGER 1. *S/D* REMOVED AND REPLACED SKIN PER EA 7-5310-58485.

Part: FLOORBEAM — DAMAGED (FUSELAGE)

BS 740 FLOORBEAM IS DAMAGED UNDER NUT PLATE LBL 52, AFT FLANGE. *S/D* REMOVED AND REPLACED FLOORBEAM PER SRM 53-10-4 FIG 4.

Part: SKIN — CHAFED (FUSELAGE)

FUSELAGE SKIN CHAFED BS 720D+15, STR 19 RT. R&R SKIN PER SRM 51-30-1, 53-30-2.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2

CORROSION (C53-224-01, 3) ON FLOORBEAM AT 950D AND RBL 20-25. *S/D* REMOVED AND REPLACED FLOORBEAM PER SRM 53-10-8.

Part: FRAME — CORRODED (UPPER FLANGE) · corrosion level 2

N 665 UPR FLANGE AT BS 1090 FRAME HAS OPEN HOLE WITH CORROSION UNDER R/H FLOOR TO SIDEWALL SUPPORT (C53-111-01(3)). ** S/D ** COMING

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2

CORROSION (C53-224-01, 1) BS 344, WL 208, LBL 50-RBL 25. *S/D* REMOVED AND REPLACED FLOORBEAM PER SR DWG 27-53-007.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2

CORROSION (C53-111-01, 2) ON STR 28 LT BS 600. *S/D* REMOVED AND REPLACED STR PER SRM 53-10-3 FIG 1.

Part: SKIN — CHAFED (FUSELAGE)

OUTER SKIN CHAFED LT SIDE BS 720D+15, STR 19L. R&R SKIN PER SRM 53-30-1, 53-30-3.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2

CORROSION (C53-224-01, 1) BS 328, WL 208, LBL 24. *S/D* REMOVED AND REPLACED FLOORBEAM PER SRM 53-10-8 FIG 9.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2

CORROSION (C53-111-01, 2) ON STR 28 RT BS 500. *S/D* REMOVED AND REPLACED STR PER SRM 53-10-3 FIG 1.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2

WHILE WORKING CARD N 734 DISCOVERED CORROSION ON TOP CHORD OF FLOORBEAM AT BS 328, RBL 15, WL 208. *S/D* REMOVED AND REPLACED FLOORBEAM PER SRM 53-10-8, 51-10-2, 51-30-2.

Part: SHEAR TIE — CRACKED (VERTICAL STAB)

CRACKED SHEAR TIE FOR VERTICAL STAB SKIN AT RIB NR 3 BETWEEN STR 6R & 7R. *S/D* REMOVED AND REPLACED SHEAR TIE PER SRM 51-30-2.

Part: FRAME — BENT (FUSELAGE)

FRAME BENT AT STR 22R. *S/D* REMOVED AND REPLACED FRAME PER SRM 51-40-3.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2

CORROSION (C53-111-02, 2) FWD CARGO BAY BS 720C, RBL 25, WL 150 SHEAR TIE AFT SIDE OF FRAME. *S/D* REMOVED AND REPLACED SHEAR TIE PER SRM 51-30-5, 51-30-2 & MM 51-20-011-7.

Part: FRAME — BENT (FUSELAGE)

FRAME BENT BS 680 ABOVE STR 24L. *S/D* REMOVED AND REPLACED FRAME PER SRM 51-40-3.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2

CORROSION (C53-111-02, 2) FWD CARGO BAY BS 720A, RBL 25, WL 150 SHEAR TIE AFT SIDE OF FRAME. *S/D* REMOVED AND REPLACED SHEAR TIE PER SRM 51-30-5, 51-30-2, 53-10-4.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2

CORROSION (C53-224-04) IN AND AROUND NUT PLATE HOLES ON LWR CHORD OF BS 1110 FLOORBEAM, RBL 12, 22, 32, WL 200. *S/D* REMOVED AND REPLACED FLOORBEAM PER SRM 53-10-8 FIG 8.

Part: FRAME — DENTED (FUSELAGE)

DENT IN TOP FLANGE OF FRAME. *S/D* REMOVED AND REPLACED FRAME PER SRM 51-40-3.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2

UPPER FLANGE OF BS 1050 FRAME HAS OPEN HOLE AND CORROSION UNDER LT FLOOR TO SIDEWALL SUPPORT. EXCEED SRM LIMITS PER 53-10-01. *S/D* REMOVED AND REPLACED FRAME PER SRM 51-20-2, 51-40-3, 51-30-2.

Part: FRAME — DENTED (FUSELAGE) · corrosion level 2

THREE DENTS IN TOP FLANGE OF BS 950F FRAME LBL 28-36, WL 150. *S/D* REMOVED AND REPLACED FRAME PER IAW SRM 51-40-3 FIG 1.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2

UPPER FLANGE BS 1050 FRAME HAS OPEN HOLE WITH CORROSION UNDER RT FLOOR TO SIDEWALL SUPPORT. *S/D* REMOVED AND REPLACED FRAME PER SRM 51-40-3 FIG 1 & EA. 7-5310-58481.

Part: FRAME — DENTED (FUSELAGE)

FUSELAGE FRAME AT BS 560 HAS DENTS ON UPPER FLANGE ADJACENT TO STR 24L. *S/D* REMOVED AND REPLACED FRAME PER IAW SRM 51-40-3.

Part: KEELBEAM — CRACKED (FUSELAGE)

RIGHT KEEL BEAM HAS CRACK AT BS 870 LOWER CHORD VERTICAL FLANGE. *S/D* REMOVED AND REPLACED KEEL BEAM PER EA 7-5310-58491.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2

CORROSION ON UPPER CHORD BS 1050 FLOORBEAM RBL 35, RBL 12, RBL 18, WL 208. *S/D* REMOVED AND REPLACED UPPER CHORD PER SRM 53-10-8.

Part: FLOORBEAM — CORRODED (FUSELAGE)

CORROSION ON UPPER CHORD OF BS 1030 FLOORBEAM RBL 55, RBL 15 - LBL 13. *S/D* REMOVED AND REPLACED FLOORBEAM PER SRM 53-10-8 FIG 3.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2

CORROSION FWD BAY BS 720D, LBL 25, WL 150 SHEAR TIE. *S/D* REMOVED AND REPLACED SHEAR TIE PER SRM 53-10-4.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2

CORROSION IN AND AROUND NUT PLATE HOLES ON LOWER CHORD OF BS 1130 FLOORBEAM RBL 50 - LBL 25, WL 200. REMOVED AND REPLACED FLOORBEAM PER IAW FEDEX EA 7-5310-59209.

Part: FRAME — DENTED (FUSELAGE)

FUSELAGE FRAME BS 600 UPPER FLANGE HAS DENTS FROM STR 23L TO MIDPOINT STR 24L AND 25L. REMOVED AND REPLACED FRAME PER SRM 51-40-3.

Part: STRUCTURE — CHAFED (VERTICAL STAB)

CHAFE AT VERT STAB L/E RIGHT FRONT SPAR FIN BS 55.8 TO 47.0 O/B SIDE.

Part: SPAR — CHAFED (VERTICAL STAB)

CHAFE AT VERT STAB L/E RIGHT FRONT SPAR FIN BS 55.8 TO 47.0 O/B SIDE. REMOVED AND REPLACED STAB PER IAW EA 7-5530-58486.

Part: FRAME — DAMAGED (FUSELAGE)

DAMAGE ON FRAME, BS 380 BETWEEN STR 11-12L. *S/D* REMOVED AND REPLACED FRAME PER SRM 53-10-4.

Part: DOOR — MISSING (HYD SERVICE)

ON ARRIVAL FOUND HYDRAULIC SERVICING BAY DOOR TORN OFF & MISSING. INSTALLED BODY FAIRING 3519 PER SRM 51-30-02.

Part: ACCESSORY UNIT — FAILED (E/E BAY)

REPEAT WRITE-UP GEAR WARN HORN & CARGO SMOKE LIGHT COME ON CONTINUOUSLY DURING DESCENT. *S/D* REMOVED AND REPLACED LAND GEAR MODULE. PERF TEST PER MM 32-09-121. NO DEFECTS NOTED. AC OK TO CONTINUE.

Part: BULB — FAILED (LT MLG)

99-159 - WHEN LAND GEAR 1ST LOWER NO DOWN IND ON LEFT MAIN. REMOVED AND REPLACED BULB. CK PROXIMITY SENSORS PER MM 32-61, OPS CK NORMAL.

Part: SHEAR TIE — CORRODED (BS 520)

CORROSION (C53-113-01,1) ON FWD CARGO BAY SHEAR TIE BS 520, STR 27-28 RT. *S/D* REMOVED AND REPLACED SHEAR TIE BS 520, STR 27-28R IAW FEDEX 51-30-2 AND DWG NR 65-15929.

Part: STRINGER — CORRODED (BS 580)

CORROSON ON STR 28L, BS 580. *S/D* REPAIRED STRINGER 28L AT BS 580 PER FEDEX SRM 53-10-3.

Part: CLIP — CORRODED (BS 440)

CORROSION (C53-224-03-1/2) ON STRINGER CLIP STR 26L, BS 440 (MARKED). *S/D* REMOVED AND REPLACED WITH NEW CLIP TO FRAME, NEW STR CLIP WAS INSTALLED IAW FEDEX SRM 51-10-1, 51-30-2 AND FEDEX MM 51-20-0.

Part: BEAM — CORRODED (BS 268)

WHILE WORKING FEDEX EO NR 7-5300-7-2305 L3 PT 2 CORROSION ON G-BEAM BS 268, LBL 3, WL 208. *S/D* REMOVED AND REPLACED 25 G-BEAM BS 26.75, LBL 8 TO RBL 18, WL 208 IAW FEDEX DWG 65-17593 AND FEDEX SRM 51-30-2, 53-10-1.

Part: SKIN — CORRODED (BS 760)

NR 0167 - CORROSION (C53-224-05) WING CTR SECTION UPPER SKIN, UPPER SURFACE BS 760, RBL 65, WL 204. REMOVED AND REPLACED CORROSION AT BS 758, RBL 62.64, WL 204 UP TO .039 OF MATERIAL IN A 1 BY 1 AREA. UPPER SKIN WAS FOUND TO BE OUT OF LIMITS PER FEDEX SRM 57-30-1. REPAIR SKIN PER FEDEX EA 7-5330-43175A.

Part: SHEAR TIE — CORRODED (BS 720)

NR 581 CORROSION (C53-113-01,1) ON FWD CARGO BAY SHEAR TIE BS 720F, LBL 9, WL 149. *S/D* REMOVED AND REPLACED SHEAR TIE BS 720F, LBL 9, WL 149 IAW FEDEX SRM 53-10-4 FIG 15.

Part: SKIN — CRACKED (CARGO DOOR)

NR 369 FCD INNER SKIN IS CRACKED 8 INCHES FWD OF AFT FRAME 1 INCH ABOVE NR 3 TRANSVERSE BEAM. *S/D* REMOVED DAMAGE AT FCD INNER SKIN AND FABRICATED AND INSTALLED REPAIR DOUBLER IAW FEDEX SRM 52-00-3 FIG 3.

Part: CHORD — CORRODED (BS 1176)

NR 186 - CORROSION C53-224-08 ON 1176, REINFORCEMENT CHORD LBL 56-LBL 16 AND CORROSION AND MECHANICAL DAMAGE RBL 24-LBL 18, WL 208, BS 1176. REMOVED AND REPLACED CORROSION PER FEDEX 727 SRM 53-10-1, 51-10-2, 51-10-6, 57-30-2 AND FEDEX MM 57-20-151.

Part: FRAME — CRACKED (BS 970)

NR 564 - AFT CARGO BAY BS 970 FRAME IS CRACKED AT STR 26L. REMOVED AND REPLACED FLOOR SIDEWALL SUPT AT BS 950C TO BS 1000, LBL 24, WL 146 IAW FEDEX SRM 51-30-2. REPAIRED FRAME. AFT CARGO BAY PER FEDEX SRM 51-40-3.

Part: FLOORBEAM — CORRODED (BS 1130)

NR 195 - WHILE WORKING NR 195, FOUND CORROSION ON BS 1130 FLOORBEAM RBL 22-30, WL 208. REPAIRED FLOORBEAM IAW FEDEX EA NR 7-5310-43176A.

Part: STRINGER — DENTED (BS 380-389)

NR 145 BS 380+9 STR 24 RT UPPER FLANGE OF STRINGER IS DENTED. *S/D* REMOVED DAMAGE, FAB, ALODINED, PRIMED AND INSTALLED REPAIR PER FEDEX MM 51-20-151 AND FEDEX SRM 53-10-3, FEDEX EA NR 7-5310-43150.

Part: FRAME — CORRODED (BS 950)

NR 163 CORROSION C53-113-01(2) AFT CARGO BAY STUB FRAME AT BS 950E+6 STR 29R. REMOVED AND REPLACED AFT CARGO BAY STUB FRAME IAW FEDEX SRM 51-30-2 AND FEDEX DWG 65-56129.

Part: SHEAR TIE — CORRODED (BS 580)

CORROSION (C53-113-01,1) ON FWD CARGO BAY SHEAR TIE BS 380, LBL 4 RBL 4, WL 148. *S/D* REMOVED AND REPLACED SHEAR TIE BS 580 IAW FEDEX SRM 53-10-4, DWG 65-15932.

Part: STRINGER — DAMAGED (BS 380)

NR 144 BS 380+12, STR 23 LT UPPER FLANGE OF STRINGER IS DENTED. *S/D* REPAIRED STR IAW FEDEX SRM 53-10-3, FEDEX EA 7-5310-43152.

Part: FLOORBEAM — CORRODED (BS 1110)

NR 187 CORROSION C53-224-04 ON FLOORBEAM UPPER CHORD BS 1110, LBL 11 TO RBL 43, WL 208. REMOVED DAMAGE, FABRICATED, LOCATED, DRILLED ALODINED, PRIMED, PAINTED AND INSTALL FLOORBEAM SEGMENT AND REPAIR PARTS IAW FEDEX SRM 53-10-8, 51-30-2 AND FEDEX MM 51-20-151.

Part: SWITCH — DIRTY (RT MLG DOOR)

RIGHT GEAR DOOR LIGHT REMAINED ON AFTER GEAR RETRACTION. RAN RED TABS AND RECYCLE GEAR, DOOR LIGHT EXTINGUISHED. CLEANED RIGHT GEAR DOOR LIGHT SWITCH. OPERATED SEVERAL TIMES, OPER CHECKED NORMAL.

Part: ACTUATOR — LEAKS (NR 1 LE SLAT)

NR 1 SYS-A HYDRAULIC PRESSURE LIGHT ILLUMINATED DURING TAKEOFF ROLL. WHEN GEAR LEVER WAS POSITIONED TO UP NR 2 SYS-A LIGHT ILLUMINATED AND HYDRAULIC QUANTITY RAPIDLY FELL TO 0 GALLONS. PRESSURE DROPPED TO 0 PSI. ACCOMPLISHED APPROPRIATE ABNORMAL PROCEDURES. FOUND NR 1 SLAT ACTUATOR LEAKING. ACTUATOR ARM BLOWN OUT, SEAL RUPTURED. REMOVED AND REPLACED NR 1 SLAT ACTUATOR PER MAINTENANCE MAN UAL 27-81-32 PAGE 401 TO 406. OPERATIONAL CHECK AND LEAK CHECK GOOD HYDRAULIC SYSTEMS SERVICED.

Part: FIRE LIGHT — ILLUMINATED (NR 2 ENGINE)

ON CLIMBOUT, THE NR 2 FIRE SYSTEM SOUNDED AND THE WARNING LIGHTS ON THE GLARE SHIELD ILLUMINATED FOR ABOUT 3 TO 4 SECONDS AND THEN WENT OUT. THE WARNING SOUNDED AGAIN ABOUT 30 SECONDS LATER FOR 3 TO 4 SECONDS AND THEN WENT AWAY. ALL ENGINE PARAMETERS WERE NORMAL. NORMAL POWER SETTINGS WERE IN USE. FIRE SYSTEM TESTED GOOD. INSPECTED EXTERIOR OF ENGINE FOR PNEUMATIC LEAKS AND RAN ENGINE AT IDLE TO CHECK DUCTS, NO LEAKS FOUND. RAN NR 2 ENGINE AT HIGH POWER FOR 2 MINUTES, NO FIRE WARNING DETECTED. TESTED FIRE WARNING SYSTEM, OPERATIONAL CHECK GOOD.

Part: DUCT — LOOSE (NR 1 ENGINE)

ENGINE NR 1 STRUT OVERHEAT. 1ST LIGHT WENT OUT BEFORE CHECKLIST WAS RUN. 2ND LIGHT WENT OUT WHEN ENGINE NR 1 WING ANTI-ICE SWITCH TURNED OFF. AIRCRAFT DE-ICED AT IND ON THE GROUND PRIOR TO FLIGHT. RAN NR 1 ENGINE FOUND LEAKS IN STRUT AREA. TIGHTENED FLANGES ON DUCT, OPERATIONAL CHECKED GOOD ON GROUND.