N488FE

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 43,478 hrs · 29,519 cycles

DURING SERVICE CHECK FOUND FLIGHT COMPARTMENT EMERGENCY LIGHT DIM. R & R BATTERIES IAW SMP AND MM 33-50-001-2-0. OP'S CHECKED GOOD. FINAL CLOSED.

Part: SKIN — CORRODED (BS 950F S28R) · airframe 42,978 hrs · 29,096 cycles

CORROSION ON FUSELAGE SKIN AFT OF FRAME AT BS 950F, OTBD ON STR 28R, FOUND DURING PREP TO REINSTALL AFT PIT FRAMES. CUT OUT DAMAGED AREA. FABRICATED REPAIR DOUBLER USING 2024T3 .090 DIMS 50" X 31", FABRICATED 2 EACH STRUCTURAL FILLERS USING 2024T3 .071 DIMS 55" X 14" AND 51" X 13", FABRICATED 1 EACH FILLER USING 2024T3 .080 DIMS 5" X 3 3/4", FABRICATED 1 EACH FILLER USING 2024T3 .160 MILLED TO .140 DIMS 16 1/4" X 1 1/4" AND INSTALLED ALL REPAIR PARTS IAW EA 7-5330-143917. REFERENCE SDR 10-4626.

Part: FRAME — DAMAGED (BS 950C) · airframe 42,978 hrs · 29,096 cycles

2 EACH OPEN HOLES IN FRAME AND REPAIR DOUBLER - STA 950C AT STR 24L. REMOVED REPAIR DOUBLER IAW SRM 51-30-2 REV 103 FORMED NEW REPAIR DOUBLER FROM 7075 O .080" DIM 8" X 4 1/2" IAW SRM 53-10-2 FIG 5 AND 51-20-1 FIG 7 INSTALLED REPAIR DOUBLER IAW SRM 51-30-2 REV 103

Part: SHEAR TIE — CRACKED (BS 990 S28-29R) · airframe 42,978 hrs · 29,096 cycles

UPON REMOVAL OF SHEAR TIE FOR FRAME REMOVAL, FOUND SHEAR TIE CRACKED ON OTBD UPPER CORNER, BS 990, BETWEEN STRINGER 28R AND 29R. REMOVED SHEAR TIE IAW SRM 51-30-2 REV 103 FABRICATED NEW SHEAR TIE FROM BAC1505-39042 7075-T6511 7" LONG IAW BAC DWG 65-16340 AND SRM 51-30-5 REV 103 INSTALLED SHEAR TIE IAW B727 SRM 51-30-2

Part: STRINGER — DAMAGED (BS 1160-1181) · airframe 42,978 hrs · 29,096 cycles

STRINGER 4L AT BS 1180 TENSION TIE DAMAGED. CUT-OUT DAMAGED AREA ON STRINGER 4L FROM 1160 TO 1181.1250, DIM 21.1250", FABRICATED AND INSTALLED REPAIR AND STRINGER SECTION FROM STR. BAC 1498-145 7075T6-2, DIM 21.1250" AND 5EA REPAIR PLATES NR1 FROM 2024T3 0.250" DIM 12" X 0.98", NR2 (2EA) FROM 2024T3, 0.125" DIM 10" X 1" AND NR3 (2EA) FROM 2024T3 0.100" DIM 8" X 1" IAW SRM 53-10-3, FIG 3, 51-30-2, 51-30-5, AND 51-10-2, REV 103.

Part: SEAT TRACK — CORRODED (BS 360-480) · corrosion level 2 · airframe 42,978 hrs · 29,096 cycles

SEAT TRACK CORRODED STA 360 TO 480, RBL 25. REMOVED, FABRICATED, AND INSTALLED NEW SEAT TRACK SECTION IAW SRM 53-10-2 FIG 7, 51-30-5, 51-10-1, 51-10-2, AND 51-30-2.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 42,978 hrs · 29,096 cycles

SEAT TRACK CORRODED STA 480 TO 690 LBL 45. REMOVED, FABRICATED, AND INSTALLED NEW SEAT TRACK SECTION AT BS 480 TO 690 LBL 45 FROM BAC 1520-792-7178T6 DIM 209.375" LONG IAW B727 SRM 53-10-2 FIG 7, 51-30-5, 51-10-1, 51-10-2, AND 51-30-2 REV 103.

Part: SEAT TRACK — CORRODED (BS 1010-1130) · corrosion level 2 · airframe 42,978 hrs · 29,096 cycles

SEAT TRACK CORRODED STA 1010 TO 1130 BL 0. REMOVED DAMAGED SEAT TRACK. FABRICATED NEW SEAT TRACK USING BAC1520-792-7178T6 DIMS 10' AND INSTALLED IAW SRM 53-10-2, SRM 51-10-1 AND SRM 51-30-2.

Part: SKIN — CHAFED (EMERGENCY EXIT) · airframe 42,978 hrs · 29,096 cycles

LEFT FORWARD OVERWING EMERGENCY EXIT HATCH PREVIOUS REPAIR AT TOP AFT EDGE HAS CHAFFING DAMAGE. REMOVED PREVIOUS REPAIR AND FILLER. FABRICATED NEW DOUBLER REPAIR USING 2024T-3 .050 DIMS 8 1/8" X 4 1/8" AND FILLER USING 2024T-3 .050 DIMS 1 5/8" X 1 3/8" AND INSTALLED IAW SRM 51-30-2, SRM 52-00-3 AND SRM 52-20-1.

Part: SEAT TRACK — CORRODED (BS 480-610) · corrosion level 2 · airframe 42,978 hrs · 29,096 cycles

SEAT TRACK CORRODED STA 480 TO 610 RBL 25. REMOVED, FABRICATED, AND INSTALLED NEW SEAT TRACK SECTION AT BS 480 TO 690 RBL 24.75 AND SPLICE AT BS 690, SEAT TRACK FROM BAC 1520-792-7178T6 DIM. 209 1/2" LONG, SPLICE FROM BAC 1503-100122-7178 DIM. 14 3/4" LONG 2EA, AND PLATE FROM 7075T6 0.250" DIM. 8 3/4" X 2" IAW SRM 53-10-2 FIG 7,51-30-5, 51-10-1, 51-10-2, 53-10-5 FIG 1, AND 51-30-2.

Part: FLOORBEAM — CORRODED (BS 560) · corrosion level 2 · airframe 42,978 hrs · 29,096 cycles

FLOORBEAM CORRODED STA 560, LBL 25 TO LBL 45. CUT-OUT DAMAGED AREA TOP TEE CAP FLOORBEAM BS 560 LBL 36.40 TO 39 APPROX DIM. 2.6" X .90", FABRICATED REPAIR PARTS 2EA ANGLES FROM BAC 1490-2888-7075T6 DIM.19.5" X 0.90" AND 9.6" X .080". REPAIR FILLER FROM 2024T3 0.125" DIM. 2.5" X 0.85" AND INSTALLED REPAIR PARTS IAW SRM 53-10-8 FIG 8, 51-10-2, AND 51-30-2 REV 103.

Part: SEAT TRACK — CORRODED (BS 360-480) · corrosion level 2 · airframe 42,978 hrs · 29,096 cycles

SEAT TRACK CORRODED STA 360 TO 480 LBL 25. REMOVED, FABRICATED, AND INSTALLED NEW SEAT TRACK SECTION IAW SRM 53-10-2 FIG 7, 51-30-5, 51-10-1, 51- 10-2, AND 51-30-2 REV 103.

Part: FRAME — GOUGED (ZONE 100) · airframe 42,978 hrs · 29,096 cycles

FRAME GOUGED STA 1070 STR 27L, AT RADIUS OF UPPER CHORD FLANGE CUT OUT DAMAGED SECTION OF UPPER FRAME DIM 3/4" X 2 1/2 " IAW SRM 51-40-3, FIG 1. FABRICATED REPAIR DOUBLER, MATERIAL USED 7075 O .071" DIM 14" X 6" IAW SRM 53-10-2, FIG 5 AND 51-40-3, FIG 1 LOCATED AND DRILLED IAW SRM 51-30-5 AND FILLER FROM 7075 O .071" DIM 1" X 2.5" IAW SRM 51-40-3. INSTALLED REPAIR PARTS IAW SRM 51-30-2, REV 103.

Part: STRINGER — CORRODED (BS 950C-950D) · airframe 42,978 hrs · 29,096 cycles

STRINGER CORRODED STA 950C TO 950D, STR 29L. R & R STRINGER 29L FROM BS 950 TO 1010 IAW SRM 51-30-5 AND 51-30-2 REV 103 AND DWG NR65-56441.

Part: FLOORBEAM — CORRODED (BS 380) · corrosion level 2 · airframe 42,978 hrs · 29,096 cycles

FLOORBEAM CORRODED STA 380, RBL 25 TO RBL 45. CUT OUT DAMAGED AREA DIMS 2.3" X .90". FABRICATED 2 REPAIR ANGLES USING BAC1490- 2888-7075T6 DIMS 13.4" X 2.7" AND 10.2" X 2.6" AND INSTALLED IAW SRM 53-10-8 AND SRM 53-10- 2.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 42,978 hrs · 29,096 cycles

SEAT TRACK CORRODED STA 500 TO 690 RBL 45. REMOVED, FABRICATED AND INSTALLED NEW SEAT TRACK SECTION AT BS 480 TO 690 RBL 45 FROM BAC 1520-792-7178T6 DIM. 18 FEET IN LENGTH, 2EA SPLICE REPAIR FROM BAC 1503- 100122 -7178 DIM. 15" AND STRAP FROM 7075T6 0.250 DIM. 8 5/8" X 2" IAW SRM 53-10-2 FIG 7, 53-10-5 FIG 1, 51-10-2 AND 51-30-2 REV 103.

Part: SKIN — BULGED (CARGO DOOR) · airframe 42,978 hrs · 29,096 cycles

C2 DOOR EXTERIOR SKIN HAS A BULGE AFT CORNER. CUT OUT DAMAGED AREA DIMS 1 1/4" X 2". FABRICATED DOUBLER USING 2024T-3 .080 DIMS 10" X 5" AND INSTALLED IAW SRM 52-00-3.

Part: STRUCTURE — CRACKED (LT WING TE FLAP) · airframe 42,978 hrs · 29,096 cycles

LEFT INBD MID FLAP AFT LOWER CHORD IS CRACKED AT 3 CUTOUTS. REMOVED CRACKED CHORD SECTION. FABRICATED NEW SECTION USING BAC1503-100046 7075 T6 DIMS 77" AND INSTALLED ALL REPAIR PARTS IAW SRM 57-50-2, 51-30-5 AND 51-30-2.

Part: SEAT TRACK — CORRODED (BS 360-480) · corrosion level 2 · airframe 42,978 hrs · 29,096 cycles

SEAT TRACK CORRODED STA 360 TO 480 BL 0. REMOVED, FABRICATED, AND INSTALLED NEW SEAT TRACK SECTION FROM BAC 1520-792-7178T6 DIM. 136" LONG IAW SRM 53-10-2 FIG 7A REV D AND SRM 51-30-5, 51-10-1, 51-10-2 AND 51-30-2 REV 103.

Part: SEAT TRACK — CORRODED (BS 690-740) · corrosion level 2 · airframe 42,978 hrs · 29,096 cycles

SEAT TRACK CORRODED STA 690 TO 740, LBL 45. REMOVED, FABRICATED, AND INSTALLED NEW SEAT TRACK SECTION FROM BAC 1520-792-7178- T6 DIM. 172" LONG, 2EA ANGLES FROM BAC 1503-100122-7178-T6511 DIM. 16" LONG, AND STRAP FROM 7075T6 0.250" DIM. 8" X 2" IAW SRM 53-10-2 FIG 7, 53-10-5 FIG1, 51-10-2 AND 51-30-2 REV 103 AT BS 690 TO 740 LBL 45.

Part: SKIN — GOUGED (BS 620) · airframe 42,978 hrs · 29,096 cycles

MCD INNER SURROUND SKIN GOUGED STA 620, STR'S 6L AND 10L. REMOVED MCD INNER SKIN AND SPLICES AT BS 594 TO 640 STR 2R TO 6L, FABRICATED INNER SKIN AND SPLICES FROM 2024T3 0.125" APPROX DIM 80" X 48" AND 22" X 11" AND INSTALLED INNER SKIN AND SPLICES IAW SRM 51-30-2, 51-30-5, 51-10-1, 51-10-2, AND SRM 53-10-2, FIG 3A.

Part: FLOORBEAM — CORRODED (BS 440) · corrosion level 2 · airframe 42,978 hrs · 29,096 cycles

FLOORBEAM CORRODED STA 440, LBL 25 TO BL 0. CUT OUT DAMAGED AREA DIMS 2.5" X 2". FABRICATED UPPER CHORD USING BAC1505-100617-7075T3 DIMS 15.10", SUPPORT ANGLE USING BAC1490-2785-7075T6 DIMS 15.10", SUPPORT ANGLE USING BAC1490-2831-7075T6 DIMS 11.65", REINFORCEMENT STRAP USING BAC1512-3396 DIMS 15.10" X .90", REINFORCEMENT STRAP USING BAC1512-3396 DIMS 11.65" X .90" AND INSTALLED ALL PARTS IAW SRM 53-10-8.

Part: SEAT TRACK — CORRODED (BS 360-480) · corrosion level 2 · airframe 42,978 hrs · 29,096 cycles

SEAT TRACK CORRODED STA 360 TO 480 LBL 45. REMOVED, FABRICATED, AND INSTALLED NEW SEAT TRACK SECTION AT BS 344 TO 480 LBL 45 FROM BAC 1520-792-7178T6 DIM 136.5" LONG IAW SRM 53-10-2 FIG 7, 51-30-5, 51-10-1 51-10-2 AND 51-30-2 REV 103.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 42,978 hrs · 29,096 cycles

FLOORBEAM CORRODED STA 620 LBL 45 TO LBL 25. REMOVED PREVIOUS REPAIR AND CUT-OUT FLOORBEAM DIM. 28.75". FABRICATED AND INSTALLED REPAIR UPPER CHORD AND SPLICES FROM BAC 1505-100617 7075T73511 DIM. 105" LONG, SPLICE FROM BAC 1490-2831 7075T62 DIM. 7.3" LONG, ANGLE SUPPORT FROM 7075T6 0.050" DIM. 11" X 2.9", REINFORCEMENT STRAP FROM BAC 1512-3396 7075T6 DIM. 11" LONG, AND REINFORCEMENT STRAP FROM BAC 1512-3353 7075T6 DIM. 7.25" IAW SRM 53-10-8 FIG 3, 51-20-1 FIG 3, 51-30- 5, 51-10-1, 51-10-2, 51-30-2 REV 103, AND DWG 53 1547.

Part: SKIN — GOUGED (BS 1177 S4L) · airframe 42,978 hrs · 29,096 cycles

INNER SKIN GOUGED STA 1177, STR 4L. CUT-OUT DAMAGED AREA AT BS 1177 ON STR 4L DIM. 1.125" DIA., FABRICATED REPAIR DOUBLER AND LAP FILLER FROM 2024T3 0.063" DIM. DOUBLER 10" X 6.8750" FILLER 11" X 4.5", AND INSTALLED DOUBLER AND FILLER IAW EA 7-5330-143918.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 42,978 hrs · 29,096 cycles

SEAT TRACK CORRODED STA 480 TO 600 BL0. REMOVED, FABRICATED, AND INSTALLED NEW SAET TRACK SECTION AT BS 480 TO 600 BL0 FROM BAC 1520-792-7178T6511 DIM. 120" LONG IAW FEDEX B727 P-F SRM 53-10-2 FIG 7A AND B727 SRM 51-30-5, 51-30-8, 51-10-1, 51-10-2, AND 51-30-2 REV 103.

Part: SKIN — DENTED (BS 1100-1148) · airframe 42,978 hrs · 29,096 cycles

DENT EXTERIOR FUSELAGE SKIN STA 1100 TO 1148 STR 22R. CUT OUT DAMAGED AREA DIMS 40 1/2" X 3 7/8". FABRICATED REPAIR DOUBLER USING 2024T-3 .071 DIMS 49 7/8" X 11 1/2", 3 SHIMS USING 2024T-3 .063 DIMS 40 1/2" X 1" EACH, 2 SHEAR TIE SHIMS FOR STA 1148 USNIG 2024T-3 .063 DIMS 2 5/8" X 1 3/4" EACH, 3 SHEAR TIE SHIMS FOR STA 1130 USING 2024T-3 .063 DIMS 1 5/8" X 7/8" EACH AND INSTALLED ALL REPAIR PARTS IAW SRM 53-30-1, 51-30-2, 53-30-3, 51-10-2 AND 51-30-5.

Part: SEAT TRACK — CORRODED (BS 360-480) · corrosion level 2 · airframe 42,978 hrs · 29,096 cycles

SEAT TRACK CORRODED STA 360 TO 480 RBL 45. REMOVED, FABRICATED AND INSTALLED NEW SEAT TRACK SECTION AT BS 344 TO 480 RBL 45 FROM BAC 1520-792-7178T6 DIM. 136" LONG IAW SRM 53-10-2 FIG 7, 51-30-5, 51-10-1, 51-10-2, AND 51-30-2 REV 103.

Part: SEAT TRACK — CORRODED (BS 480-680) · corrosion level 2 · airframe 42,978 hrs · 29,096 cycles

SEAT TRACK CORRODED STA 480 TO 680 LBL 25. REMOVED, FABRICATED, AND INSTALLED NEW SEAT TRACK SECTION AT BS 480TO 690 LBL 25 FROM BAC 1520-792-7178T6 DIM. 209.5" LONG, SPLICE REPAIR 2EA. FROM 1503-100122 7178T6 DIM 14.375" , AND STRAP FROM 7075T6 0.250" DIM. 8.5" X 2" IAW SRM 53-10-2 FIG 7, 53-10-5 FIG 1, 51-10-2, AND 51-30-2 REV 103.

Part: SKIN — GOUGED (BS 950E S26R) · airframe 42,978 hrs · 29,096 cycles

GOUGE EXTERIOR FUSELAGE BOTTOM FWD CORNER OF C2 CUT OUT STA 950E, STR 26R. CUT OUT DAMAGED AREA. FABRICATED REPAIR DOUBLER USING 2024T3 .090 DIMS 50" X 31", FABRICATED 2 EACH STRUCTURAL FILLERS USING 2024T3 .071 DIMS 55" X 14" AND 51" X 13", FABRICATED 1 EACH FILLER USING 2024T3 .080 DIMS 5" X 3 3/4", FABRICATED 1 EACH FILLER USING 2024T3 .160 MILLED TO .140 DIMS 16 1/4" X 1 1/4" AND INSTALLED ALL REPAIR PARTS IAW EA 7-5330-143917. REFERENCE SDR 10-4626.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 42,978 hrs · 29,096 cycles

CORROSION ON SHEAR TIE AT STA 720D BETWEEN STR'S 25L AND 26L. REMOVED PREVIOUS SHEAR TIE REPAIR DOUBLER IAW SRM 51-30-2 FABRICATED NEW SHEAR TIE REPAIR DOUBLER FROM 7075 O .071" DIM 5" X 2" IAW SRM 53-10-2 FIG 3, 51-20-1 FIG 7, AND 53-10-4 FIG 15. INSTALLED REPAIR DOUBLER IAW SRM 51-30-2 AND 53-10-4 FIG 15 REV 103.

Part: STRUCTURE — MISINSTALLED (BS 358-398) · airframe 42,978 hrs · 29,096 cycles

L1 DOOR RAIN GUTTER FWD ATTACMENT HAS 2 FASTENERS WITH IMPROPER SPACING STA 300 TO STA 312. CUT-OUT AFFECTED AREAS IAW EA 7-5330-143916. FABRICATED FREEZE PLUGS, FILLERS, AND DOUBLER IAW EA 7-5330-143916. INSTALLED REPAIR PARTS IAW EA 7-5330-143916 AT L-1 DOOR RAIN GUTTER BETWEEN BS 298 TO 358 LT SIDE.

Part: WEB — CRACKED (TORQUE BOX) · airframe 42,978 hrs · 29,096 cycles

AFT AIRSTAIRS AREA RIGHT HAND LOWER TORQUE BOX LIGHTNING HOLE IS CRACKED STA 1223 RBL 25 CUT OUT DAMAGED AREA DIM 1" X 0.6" IAW SRM 51-10-1 FABRICATED WEB REPAIR FROM 7075 T6 .032" DIM 2.6" X 2" IAW 53-10-2 FIG 6 AND 51-40-2 FIG 1 TREATED AND PRIMED IAW SRM 51-10-2 INSTALLED WEB REPAIR IAW SRM 51-40-2 FIG 1 REV 103

Part: STRINGER CLIP — DAMAGED (FUSELAGE) · airframe 41,722 hrs · 28,113 cycles

STRINGER CLIP DAMAGED AT STR 26L, FS 540, LBL 23, WL 152. REMOVED AND REPLACED STRINGER CLIP AT STA 540 STRINGER 26L LBL 23 REF SRM 51-30-2 PG 5. THIS IS CLASSIFIED AS A MAJOR REPAIR.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 41,722 hrs · 28,113 cycles

STRINGER DAMAGED AT BS 540 WL 152 LBL 23. FABRICATED NEW STRINGER SECTION AND TWO SPLICE REPAIRS ON STRINGER 26L BS 540 LBL 23 REF SRM 53-10-3 FIG 1. TREATED, PRIMED AND INSTALLED REF SRM 51-10-2 PG 1-7, 51-30-2 PG 2, 51-10-3 FIG 1. THIS IS CLASSIFIED AS A MAJOR REPAIR.

Part: FRAME — DAMAGED (ZONE 200) · airframe 41,722 hrs · 28,113 cycles

RT AFT EMERGENCY EXIT HATCH CUTOUT, AFT FRAME DAMAGED AT RIVET LOCATION BLENDED AREA OF FRAME, FABRICATED REPAIR PARTS, CAD PLATED, TREATED, PRIMED AS NEEDED. INSTALLED ALL PARTS AND REMOVED FASTENERS AND SIDEWALLS FOR ACCESS REF EA 7-5310-114033.

Part: RETAINER — CORRODED (LT WING) · corrosion level 2 · airframe 41,722 hrs · 28,113 cycles

LT WING REAR SPAR LWR CHORD APPROX STA 182, SEAL RETAINER CORRODED REMOVED SEAL RETAINER REF SRM 51-30-2. FABRICATED NEW RETAINER REF DWG 65-21656. TREATED AND PRIMED REF SRM 51-10-2 PGS 1-3. INSTALLED SEAL RETAINER REF SRM 51-30-2 PG'S 1-3. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: RETAINER — CORRODED (ZONE 500) · corrosion level 2 · airframe 41,722 hrs · 28,113 cycles

LT WING SPAR UNDERWING PANEL SEAL RETAINER HAS CORROSION O/B OF APU FIRE BOTTLE AT WS 182 TO 200. FABRICATED SEAL RETAINER REF DWR 65-21656. TREATED AND PRIMED REF SRM 51-10-2 PG 1- 9. INSTALLED SEAL RETAINER REF 51-30-2 P1-3. THIS IS A CLASSIFIED A MINOR REPAIR.

Part: FRAME — CRACKED (ZONE 500) · airframe 41,722 hrs · 28,113 cycles

RT WING, I/B AILERON LOWER T/E PANEL FRAME CRACKED WITH MISSING ATTACH FASTENER AT AFT END OF FRAME 10 INCH O/B FROM I/B END OF AILERON REMOVED DAMAGED PANEL FRAME REF SRM 51-30-2. VERIFIED MATERIAL OF FRAME TO BE BAC1506-1625 7075-T6. FABRICATED REPLACEMENT FRAME REF DWG 65-19288. TREATED AND PRIMED FRAME REF SRM 51-10-2. INSTALLED FRAME REF SRM 51-30-2. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: CHANNEL — CRACKED (ZONE 600) · airframe 41,722 hrs · 28,113 cycles

RT WING, I/B AILERON O/B L/E SEAL MOUNT BRACKET/UNDERWING PANEL MOUNT BRACKET CRACKED 10 INCH I/B FROM O/B END OF AILERON REMOVED SEAL MOUNT BRACKET AND ATTACH ANGLE, FABRICATED NEW "U" CHANNEL. FABRICATED NEW ATTACH ANGLE, HEAT TREATED TO T4 CONDITION. U CHANNEL AND ATTACH ANGLE WERE TREATED, PRIMED, AND TOP COATED. U CHANNEL AND ATTACH ANGLE INSTALLED REF SRM 51-30-2. DWR 69-22241, 65-19288, GMM 7-0-1-001. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,722 hrs · 28,113 cycles

CORROSION ON SEAT TRACK ATTACH FLANGE, FS 1171 TO 1162, LBL 1, WL 208 REMOVED CORROSION, NDT VERIFIED MATERIAL LOSS AND CHECK FOR DEFECTS. NO DEFECTS WERE FOUND, ORIGINAL THICKNESS .190 INCH, REMAINING .174 INCH, MATERIAL LOSS .016 WITHIN LIMITS, REF EA 7-5310-144031. TREATED AND PRIMED AREA REF SRM 51-10-02. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,722 hrs · 28,113 cycles

CORROSION ON TOP OF SEAT TRACK ATTACH FLANGE, FS 1140-1173, RBL1, WL 208. REMOVED CORROSION, NDT VERIFIED MATERIAL LOSS AND DEFECTS, NO DEFECTS FOUND. ORIGINAL THICKNESS .190, .175 REMAINING, MATERIAL LOSS .015 WITHIN LIMITS REF EA 7-5310-11403. TREATED AND PRIMED AREA REF SRM 53-10-02. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,722 hrs · 28,113 cycles

SEAT TRACK DAMAGED AT FS 1164 TO FS 1160, BL 0, WL 208 REMOVED DAMAGED, NDT VERIFIED MATERIAL LOSS AND CHECKED FOR DEFECTS, NO DEFECTS FOUND. ORIGINAL THICKNESS .175 REMAINING.167 MATERIAL LOSS .008" WITHIN LIMITS REF EA 7-5310-114031. TREATED AND PRIMED AREA REF SRM 51-10-02. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,722 hrs · 28,113 cycles

CORROSION ON SEAT TRACK I/B FLANGE FROM FS 1171 - FS 1146, LBL 24, WL 208. REMOVED CORROSION ON SEAT TRACK, NDT VERIFIED MATERIAL LOSS AND CHECKED FOR DEFECTS, NO DEFECTS WERE FOUND. ORIGINAL THICKNESS .135 INCH REMAINING .127 INCH MATERIAL LOSS .008 INCH WITHIN LIMITS REF EA 7-5310-114032. TREATED AND PRIMED AREA. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,722 hrs · 28,113 cycles

LWR EXT FUSE WING BODY FRG SUPPORT FRAME INTERCOSTAL ASSY INT SURF IS CORRODED BS 773, LBL9- RBL 9, WL 140. FABRICATED NEW SPLICE PLATE AND INSTALLED, REF BOEING DWG 65-58504. REMOVED FRAME SUPPORT, REMOVED CORROSION ON SLICE PLATE MATERIAL LOSS 50 PERCENT OUT OF LIMITS. INSTALLED NEW SPLICE PLATE TO THE FRAME SUPPORT, INSTALLED FRAME SUPPORT AT BS 773, LBL 9-RBL 9, WL 140. INSTALLED TWO NEW BLOCK AND ROD ASSY ON FRAME SUPPORT REF SRM 51-30-02 PG 2-15.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,722 hrs · 28,113 cycles

CORROSION AT ATTACH FASTENER ON SEAT TRACK, FS 1174, LBL25, WL 208 REMOVED CORROSION, NDT VERIFIED MATERIAL LOSS AND CHECK FOR DEFECTS, NO DEFECTS WERE FOUND. ORIGINAL THICKNESS .065 INCH REMAINING .061 INCH MATERIAL LOSS .004 INCH WITHIN LIMITS. REF EA NR 7-5310-114032. TREATED AND PRIMED AREA REF SRM 51-10-02. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: SKIN — DAMAGED (ZONE 100) · airframe 41,722 hrs · 28,113 cycles

DURING STRINGER REPAIR AT FS 550 AND STR 26L EXISTING HOLE LOCATED IN STRINGER ONLY WAS DRILLED THRU FUSELAGE SKIN. THE HOLE THRU THE SKIN IS BETWEEN 2 MANUFACTURING SKIN FALLING ON THE EDGE OF THE FWD SKIN LEAVING NO EDGE DISTANCE. FABRICATED REPAIR DOUBLER AND FILLER FOR SKIN DOUBLER STA 550 STR 26L REF P-F SRM 53-30-2 PG 6-8 FIG 1A. TREATED, PRIMED AND INSTALLED REPAIR DOUBLER, FILLER REF SRM 51-10-6 PG 1-7, 53-30-2 FIG 1A 53-30-2 PG 2. THIS IS CLASSIFIED AS A MINOR REPAIR. CAT "B" REPAIR. SEE SRM 53-30-3 P7 TABLE III FOR INSPECTION REQUIREMENTS.

Part: SKIN — CRACKED (L1 DOOR) · airframe 41,722 hrs · 28,113 cycles

DOOR L-1, INTERIOR AFT SKIN CRACKED AT 2 STOP PIN LOCATIONS (MKD). REPAIRED 2 DAMAGE AREA'S AT DOOR L-1 INTERIOR AFT SKIN STOP PIN LOCATIONS. HFEC IAW NDT MANUAL PART 6 51-00-00 FIG 23. TOOLING ID NR 0065 19 SEP 08. FOUND CRACKED. REMOVED DAMAGE AND REPAIR 2 AREA WITH DOUBLERS REF SRM 51-40-2 PG 1-6 FIG 1 AND REF SRM 52-10-1 PG 1 FIG 1 ITEM 15. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: FRAME — DAMAGED (ZONE 100) · airframe 41,722 hrs · 28,113 cycles

TOP OF FRAME DAMAGED UNDER "Z" FLOOR SUPPORT, FS 520, RBL 7, WL 155. REMOVED DAMAGE AT TOP OF FRAME. NDT VERIFIED DAMAGE REMOVAL, FABRICATED REPAIR DOUBLER, TREATED AND PRIMED DOUBLER AND DAMAGE CUT OUT. INSTALLED REPAIR DOUBLER, REF SRM 51-40-3 FIG 1, NDT MAN PART 6, 51-00-00 FIG 23. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: FRAME — DAMAGED (ZONE 100) · airframe 41,722 hrs · 28,113 cycles

TOP OF FRAME DAMAGED UNDER "Z" FLOOR SUPPORT FS 540, RBL 7, WL 155. REMOVED DAMAGE AT TOP OF FRAME, NDT VERIFIED DAMAGE REMOVAL. FABRICATED REPAIR DOUBLER, TREATED AND PRIMED DOUBLER AND DAMAGED CUT OUT. INSTALLED REPAIR DOUBLER. REF SRM 51-40-3, FIG 1/ NDT MAN, PART 6 51-00-00, FIG 23 THIS IS CLASSIFIED AS A MAJOR REPAIR.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,722 hrs · 28,113 cycles

LOWER FUSELAGE STATION 1010 STRINGER 30 HAS AREA OF CORROSION ON EXTERIOR. REMOVED CORROSION AREA DAMAGED BEYOND LIMITS. NDT VERIFIED ORIG MATERIAL THICKNESS TO BE .071 "MATERIAL LOSS IS .009" REMAINING MATERIAL IS .062". FABRICATED REPAIR DOUBLER AND FILLER REF SRM 53-30-3, FIG 3A/NDT MAN PART 6, 51-00-00, FIG 23, SRM 51-10-2 PG 2-7. THIS IS CLASSIFIED AS A MAJOR REPAIR.

Part: RMI — MALFUNCTIONED (COCKPIT) · airframe 39,796 hrs · 26,604 cycles

FIRST OFFICERS HSI HAS A -HEADING- FLAG APPEARING ON TAXI. CAPTAIN`S RMI, HSI & F/O RMI APPEAR TO INDICATE THE SAME HEADING. *S/D* REMOVED & REPLACED CAPT'S RMI IAW FEDEX M/M 34-21-051-4.

Part: CONTROL ROD — STIFF (NLG STEERING) · airframe 39,794 hrs · 26,598 cycles

TEST FLIGHT NWS EXTREMELY STIFF TURNING RIGHT. ADJUSTED NWS SYSTEM AND REMOVED AND REPLACED RUDDER PEDAL STEERING CONTROL ROD PER FED EX MM 32-51-000-5.

Part: SHEAR TIE — DAMAGED (VERTICAL STAB) · airframe 39,793 hrs · 26,597 cycles

WHILE WORKING CARD 73C023-00, FOUND VERT FIN AFT SHEAR TIE FITTING TO HAVE MECHANICAL DAMAGE ON LOWER SURFACE AT LEFT AFT VERT BOLT HOLE. *S/D* REPAIRED VERT FIN AFT SHEAR TIE FITTING LWR SURFACE IAW FEDEX EA 7-5530-96604.

Part: ATTACH FITTING — CORRODED (T/E FLAP) · airframe 39,793 hrs · 26,597 cycles

RIGHT WING, NR 7 FLAP TRACK FORWARD ATTACH FITTING IS CORRODED.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 39,793 hrs · 26,597 cycles

EXTERNAL DOUBLER REPAIR APPROX 35" BY 8" RT LWR FUSE STA 565 TO STA 600 STRINGER 26R TO 27R. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. INVESTIGATED EXTERNAL REPAIR BS 565 TO 600 STR 260-27R AND FOUND NOT TO BE INSTALLED PER APPROVED DATA. REMOVED AND REPLACED DOUBLER PER FED EX EA 7-5330-96612.

Part: RIB — CORRODED (VERTICAL) · airframe 39,793 hrs · 26,597 cycles

N00716 VERTICAL FIN TENSION TIE RIB, R/H AFT VERTICAL BOLT HOLE HAS CORROSION. REPAIRED PER FED EX EA 7-5530-99604 MAJOR REPAIR.

Part: RIB — GOUGED (VERTICAL STAB) · airframe 39,793 hrs · 26,597 cycles

VERTICAL FIN TENSION TIE RIB, RIGHT FWD VERTICAL BOLT HOLE IS GOUGED. REPAIRED PER FED EX EA 7-5530-99604 MAJOR REPAIR.

Part: RIB — CORRODED (VERTICAL) · airframe 39,793 hrs · 26,597 cycles

VERTICAL FIN TENSION TIE RIB, LT AFT VERTICAL BOLT HOLE HAS CORROSION. REPAIRED PER FED EX EA 7-5530-99604 MAJOR REPAIR

Part: SHEAR TIE — CORRODED (VERTICAL STAB) · airframe 39,793 hrs · 26,597 cycles

FOUND VERT FIN TENSION TIE RIB, AFT SHEAR FITTING, LWR SURFACE HAS CORROSION. *S/D* REPAIRED PER FED EX EA 7-5530-99604 MAJOR REPAIR.

Part: SHEAR TIE — CORRODED (VERTICAL) · airframe 39,793 hrs · 26,597 cycles

WHILE WORKING CARD NO. N00718, FOUND VERT. FIN AFT SHEAR TIE FITTING, UPPER SURFACE HAS CORROSION. REPAIRED PER FED EX EA 7-5530-96604 REPAIR CONSIDERED A MAJOR.

Part: RIB — GOUGED (VERTICAL) · airframe 39,793 hrs · 26,597 cycles

VERTICAL FIN TENSION TIE RIB, LT FWD VERTICAL BOLT HOLE IS GOUGED. COMING REPAIRED PER FED EX EA 7-5530-99604 MAJOR REPAIR.

Part: WEB — CRACKED (VERTICAL STAB) · airframe 39,793 hrs · 26,597 cycles

WHILE WORKING RUDDER TRIM ACTUATOR REPLACEMENT, FOUND VERTICAL FIN WEB CRACKED UNDER WASHER HOLDING THE PRESSURE SEAL FOR THE RTB CABLE AT FIN STA 87. *S/D* REPAIRED PER FEDEX EA 7-5330-96598.

Part: FITTING — CORRODED (BS 1183) · airframe 39,793 hrs · 26,597 cycles

WHILE WORKING WORK INSTRUCTION CARD 71C716-00 FOUND 2 FASTENER HOLES TO HAVE CORROSION AND TO BE OVERSIZED AT BS 1183 STR 27L AND 27R. *S/D* COMPLIED WITH FED EX EA 7-5310-96599.

Part: SKIN — UNKNOWN (BS 680-740) · airframe 39,793 hrs · 26,597 cycles

REMOVE AND REPLACE SKIN FROM BS 680 TO 740 STR 4L TO 4R. *S/D* REMOVED AND REPLACED SKIN AT BS 680 TO 740 STR 4L TO 4R IAW SRM 51-30-2, 51-10-2.

Part: STRINGER — CORRODED (BS 620-720E) · corrosion level 2 · airframe 39,793 hrs · 26,597 cycles

INTERIOR FUSELAGE, STR 4R HAS CORROSION FROM BS 620 TO BS 720E. *S/D* REPAIRED STRINGER AT BS 620 TO BS 720E STR 4R IAW SRM 53-10-3 FIG 3.

Part: STRINGER CLIP — CORRODED · airframe 39,793 hrs · 26,597 cycles

N00370 STRINGER CLIP AT BS 804 AND STR 4R HAS SURFACE CORROSION. REMOVED AND REPLACED STR CLIP BS 804 STR 4R IAW SRM 51-10-1.

Part: STRINGER — CORRODED (BS 740-826) · airframe 39,793 hrs · 26,597 cycles

N00364 STR 2R HAS SURFACE CORROSION BETWEEN BS 740- BS 826. REMOVED AND REPLACED STR 2R BS 740-870 IAW SRM 53-10-1, 51-30-2, 51-20-1 AND 51-10-2.

Part: RIB — CHAFED (NR 2 SLAT) · airframe 39,793 hrs · 26,597 cycles

NR 2 SLAT I/B END RIB HAS CHAFING DAMAGE. *S/D* REPAIRED I/B RIB IAW SRM 51-30-2.

Part: STRINGER — CORRODED (BS 700-740) · airframe 39,793 hrs · 26,597 cycles

INTERIOR FUSELAGE, STR 3R HAS CORROSION FROM BS 700 TO BS 740. *S/D* REPAIR TO STRINGER TO BE ACCOMPLISHED ON NRC N00880 PER SRM 53-10-1.

Part: FLOORBEAM — CORRODED (BS 720) · airframe 39,793 hrs · 26,597 cycles

CORROSION ON FLOORBEAM BS 720 RBL 10 LWR FLANGE AT NUT PLATE HOLES. *S/D* REPAIRED PER FED EX SRM SR27-53-034.

Part: STRINGER CLIP — CORRODED (BS 784) · airframe 39,793 hrs · 26,597 cycles

STRINGER CLIP AT BS 784 AND STR 4R HAS SURFACE CORROSION. REPLACED STR CLIP PER SRM 51-30-2.

Part: WEB — CRACKED (VERTICAL STAB) · airframe 39,793 hrs · 26,597 cycles

WHILE WORKING RUDDER TRIM ACTUATOR REPLACEMENT FOUND VERTICAL FIN WEB CRACKED UNDER WASHER HOLDING THE PRESSURE SEAL FOR THE RTB CABLE AT FIN STA 87. REPAIRED PER FED EX EA 7-5530-96598.

Part: STRINGER — CORRODED (BS 660-740) · corrosion level 2 · airframe 39,793 hrs · 26,597 cycles

FOUND INTERIOR FUSELAGE, STR 2L HAS CORROSION FROM BS 660 TO 740.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 39,793 hrs · 26,597 cycles

CORROSION ON STR 4 RT BS 700 TO BS 720C. REMOVED CORROSION FROM STR 4 R/H BS 700 TO 720C, FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. STRINGER SECTION TO BE REPLACED ON N00343 BS 620-720E.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 39,793 hrs · 26,597 cycles

INTERIOR FUSELAGE, STR CLIP 4R HAS CORROSION BS 720A. REMOVED CORRODED STR CLIP & WILL BE REPLACED ON N00343.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 39,793 hrs · 26,597 cycles

CORROSION ON STRINGER CLIP AT BS 720B STR 4 RT. REPLACED STR CLIP PER SRM 51-30-2.

Part: FRAME — MISDRILLED (BS 660) · airframe 39,793 hrs · 26,597 cycles

STA 660 STR 25 LT TWO DOUBLE DRILLED HOLES THROUGH FRAME AND DOUBLER. *S/D* REMOVED DAMAGED DOUBLER AND DAMAGE ON FRAME AT STA 660 STR 25 LT, FABRICATED NEW DOUBLER, INSTALLED IAW SRM 51-40-03, 51-20-02 AND FED-EX MM 51-20-151 MAJOR REPAIR.

Part: STRINGER — CRACKED (WS 656) · airframe 39,793 hrs · 26,597 cycles

LEFT WING INTERNAL FUEL CELL, UPPER STIFFENER 9 IS CRACKED AT WS 656.50. REPAIRED PER FED EX EA 7-5710-96588.

Part: SKIN — GOUGED (FUSELAGE) · airframe 39,793 hrs · 26,597 cycles

EXTERNAL SKIN AFT OF AFT CARGO DOOR GOUGED 21" UP FROM LWR CORNER 1.5" FROM SKIN EDGE.

Part: FLAP TRACK — CORRODED (TE FLAPS) · airframe 39,793 hrs · 26,597 cycles

NR 2 FLAP TRACK CORRODED AT AFT MOUNT PAD. REPLACED PER CARD 27X5706-03.

Part: SKIN — CHAFED (BS 720E) · airframe 39,793 hrs · 26,597 cycles

CHAFE AT BS 720E RBL 48 WL 178 EXT SKIN JUST FWD OF RT LANDING LIGHT.

Part: FLAP TRACK — CORRODED (LT WING) · airframe 39,793 hrs · 26,597 cycles

LEFT WING, NR 3 FLAP TRACK IS CORRODED AT THE SPOILER BEAM MOUNT AND THE MAIN MOUNT PADS. *S/D* REMOVED AND REPLACED CORRODED LT WING NR 3 FLAP TRACK IAW CARD 27X5705-01 AND CARD 27X5705-03.

Part: FLAP TRACK — CRACKED (TE FLAPS) · airframe 39,793 hrs · 26,597 cycles

RIGHT WING NR 6 FLAP TRACK CORRODED AT SPOILER BEAM PAD, MAIN MOUNTING PAD AND CRACKS EMMITTING FROM FAILSAFE BOLT HOLE. *S/D* REMOVED & REPLACED NR 6 FLAP TRACK PER FED EX CARD 27X5708-01 & 27X5708-03.

Part: SKIN — DENTED (FUSELAGE) · airframe 39,793 hrs · 26,597 cycles

SKIN FWD OF TAIL STAND JACK ACCESS DOOR DENTED. *S/D* REMOVED AND REPLACED SKIN IAW SRM 51-30-02.

Part: REPAIR — UNKNOWN (FUSELAGE) · airframe 39,793 hrs · 26,597 cycles

EXTERNAL FLUSH REPAIR APPROX 2.5 X 2.5 INCH RT LWR FUSE STA 302 STRINGER 24R. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. *S/D* REPAIRED PER SRM 53-30-3, 51-30-2 MAJOR REPAIR.

Part: SPAR — CHAFED (VERTICAL STAB) · airframe 39,793 hrs · 26,597 cycles

RT VERT FIN MIDSPAR CHORD CHAFED AT FIN STA 225. REPAIRED PER FED EX EA 7-5530-96609.

Part: FLOORBEAM — CORRODED (BS 480) · airframe 39,793 hrs · 26,597 cycles

FOUND BS 480 RBL 65 TO LBL 65 FLOORBEAM IS CORRODED AT NUT PLATE HOLES. REPAIRED FLOORBEAM AT BS 480 LBL 65 TO RBL 65 IAW SRM 53-10-8.

Part: REPAIR — UNKNOWN (FUSELAGE) · airframe 39,793 hrs · 26,597 cycles

EXTERNAL DOUBLE REPAIR APPROX 5" BY 7" RT LWR FUSE STA 1152 TO STA 1160 STRINGER 29R. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED & REPLACED EXTERNAL DOUBLER AT STA 1060 TO STA 1152 STR 27R IAW SRM 53-30-3.

Part: SPAR — CHAFED (VERTICAL STAB) · airframe 39,793 hrs · 26,597 cycles

LT VERT FIN MIDSPAR CHORD CHAFED AT FIN STA 225. REPAIRED THE LT VERTICAL FIN MIDSPAR AT FIN STA 225 IAW FED-EX EA 7-5530-96609.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 39,793 hrs · 26,597 cycles

FLOORBEAM IS CORRODED ON LWR FLANGE AT NUT PLATE HOLE BS 640 RBL 48. REPAIRED PER SRM 53-10-8 MAJOR REPAIR.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 39,793 hrs · 26,597 cycles

LWR FUSELAGE SKIN HAS MULTIPLE NICKS AND GOUGES BETWEEN STA 1030 AND STA 1045 FROM STR 25R TO STR 30R. BLENDED SKIN STA 1030 AND 1045 STR 25R TO 30R FABRICATED & INSTALLED REPAIR DOUBLER IAW EA 7-5330-96596. THIS IS A MAJOR REPAIR.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,793 hrs · 26,597 cycles

AFT CARGO BAY, FRAME UPPER FLANGE IS DENTED, BS 950B, BETWEEN STRINGERS 23L AND 24L. REPAIRED PER SRM 51-40-3.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,793 hrs · 26,597 cycles

AFT CARGO BAY, FRAME UPPER FLANGE IS DENTED, BS 1070, AT STR 26R. REPAIRED FRAME AT BS 1070 STR 26R IAW SRM 51-40-3.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,793 hrs · 26,597 cycles

AFT CARGO BAY, FRAME UPPER FLANGE IS DENTED, BS 970, BETWEEN STR 25L AND 26L. REPAIRED FRAME BS 970 BETWEEN STR 25L AND 26L IAW SRM 51-40-3.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,793 hrs · 26,597 cycles

AFT CARGO BAY, FRAME UPPER FLANGE IS DENTED, BS 950F, BETWEEN STRINGERS 23L AND 26L. DENT FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REPAIRED FRAME BS 950F BETWEEN STR 23L TO 26L USING 7075-T6 .071 M672773 PER SRM 51-40-3. FOUND TO BE A MAJOR REPAIR.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,793 hrs · 26,597 cycles

AFT CARGO BAY, FRAME UPPER FLANGE IS DENTED, BS 990, BETWEEN STR 25L AND 26L. REPAIRED FRAME AT BS 990, BETWEEN STR 25L AND 26L PER SRM 51-40-3.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,793 hrs · 26,597 cycles

AFT CARGO BAY, FRAME UPPER FLANGE IS DENTED, BS 1050 ABOVE AND BELOW STR 26R. REPAIRED FRAME AT BS 1050 ABOVE & BELOW STR 26R IAW SRM 51-40-3.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,793 hrs · 26,597 cycles

AFT CARGO BAY, FRAME UPPER FLANGE IS DENTED, BS 950C, BETWEEN STRINGERS 26R AND 27R. REPAIRED PER SRM 51-40-3 MAJOR REPAIR.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 39,793 hrs · 26,597 cycles

STIFFENER BETWEEN BS 849 - BS 870, STR 3R-STR 4R, HAS SURFACE CORROSION. BS 849 - 870 STR 3R TO 4R, FOUND ONLY SLIGHT SURFACE CORROSION WITHIN LIMITS PER SRM 53-10-1.

Part: FRAME — CORRODED (FUSELAGE) · airframe 39,793 hrs · 26,597 cycles

CORROSION, UPPER FUSELAGE, BS 740 FRAME, AFT SIDE, STR 3L ATTACH CLIP HAS CORROSION. BS 740 FRAME, AFT SIDE STRINGER 3L CLIP CORROSION REMOVAL WITHIN LIMITS PER SRM 53-10-1.

Part: STRINGER CLIP — CORRODED (BS 640) · airframe 39,793 hrs · 26,597 cycles

CORROSION STRINGER CLIP BS 640 S7R. REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-30-1, 51-30-2.

Part: FLOORBEAM — CORRODED (BS 440) · airframe 39,793 hrs · 26,597 cycles

CORROSION ON FLOORBEAM STA 440, RBL 10, WL 208. REPAIRED FLOORBEAM IAW SRM 53-10-1, 53-10-4, 51-30-02.

Part: STRINGER CLIP — CORRODED (BS 640) · airframe 39,793 hrs · 26,597 cycles

CORROSION ON STRINGER CLIP BS 640 STR 6 RT. REMOVED AND REPLACED STRINGER CLIP IAW SRM 53-10-1, 51-30-2.

Part: STRINGER CLIP — CORRODED (BS 640) · airframe 39,793 hrs · 26,597 cycles

CORROSION ON STRINGER CLIP BS 640 STR 8RT . REMOVED AND REPLACED STRINGER CLIP IAW SRM 53-10-1, 51-30-2.

Part: STRINGER CLIP — CORRODED (BS 700) · airframe 39,793 hrs · 26,597 cycles

CORROSION ON STRINGER CLIP AT BS 700 STR 4 RT. *S/D* REPLACED STRINGER CLIP PER SRM 51-30-2.

Part: FRAME — DENTED (BS 580) · airframe 39,793 hrs · 26,597 cycles

FRAME DENTED AT BS 580 BETWEEN STR 23L & STR 25L IN THE FWD CARGO COMPARTMENT. REPAIRED FRAME AT BS 580 BETWEEN STR 23L-25L IAW SRM 51-40-3.

Part: WEB — CORRODED (FUSELAGE) · airframe 39,793 hrs · 26,597 cycles

CORROSION ON WEB BS 647 LBL 70 WL 208. REMOVED AND REPLACED WEB AT BS 647 LBL 70 WL 208 IAW SRM 53-10-1, 51-30-02 AND 51-30-5.

Part: FLOORBEAM — CORRODED (BS 1110) · airframe 39,793 hrs · 26,597 cycles

WHILE PREPPING TO CLOSE FLOORBOARDS FOUND CORROSION ON UPPER FLOORBEAM AT BS 1110 BL 0 - RBL 25. *S/D* REPAIRED UPPER FLOORBEAM AT BS 1110 BL 0 - RBL 25.

Part: FRAME — DENTED (BS 1110) · airframe 39,793 hrs · 26,597 cycles

AFT CARGO FRAME DENTED AT BS 1110 STR 25R. *S/D* CUT OUT DENTED SECTION OF BS 1110 FROM 25R-26R, 1 X 3 INCH. REPAIRED FRAME PER SRM 51-40-3 USING 7075-T6 .063 LOT 666612.

Part: FRAME — DENTED (BS 600) · airframe 39,793 hrs · 26,597 cycles

FRAME DENTED AT BS 600 BETWEEN STR 22L AND 25L FWD CARGO BAY. *S/D* REPAIRED DENT BS 600 BETWEEN STR 22L & 25L IAW SRM 51-40-3, SRM 51-10-1 FIG 1.

Part: FRAME — DAMAGED (BS 640) · airframe 39,793 hrs · 26,597 cycles

BS 640, RBL 3 WHILE WORKING CARD N00935 FOUND FRAME AT BS 640 RBL 3 DAMAGED. *S/D* REMOVED DAMAGE FROM FRAME, FABRICATED ALODINED PRIMED & INSTALLED REPAIR PER SRM 51-40-3.

Part: SKIN — DENTED (FUSELAGE) · airframe 39,793 hrs · 26,597 cycles

AFT AIR STAIRS EXTERNAL SKIN DENTED 17 INCHES FROM TRAILING EDGE LBL 6. REPAIRED AFT AIR STAIR EXTERNAL SKIN IAW SRM 52-10-1, 53-30-3.

Part: SKIN — CORRODED (FUSELAGE) · airframe 39,793 hrs · 26,597 cycles

INTERIOR FUSELAGE UPPER SKIN HAS CORROSION IN BETWEEN STR 2L TO STR 4R BS 700 TO 720C. REMOVED AND REPLACED SKIN BS 680 TO BS 740 STR 4L TO 4R IAW SRM 51-30-2.

Part: STRINGER CLIP — CORRODED (BS 700) · airframe 39,793 hrs · 26,597 cycles

CORROSION ON STRINGER CLIP AT BS 700 STR 3RT. *S/D* REMOVED AND REPLACED STRINGER CLIP BS 700 STR 3R IAW SRM 51-30-2.

Part: FRAME — DENTED (BS 660) · airframe 39,793 hrs · 26,597 cycles

FRAME DENTED AT BS 660 STR 22R IN FWD CARGO COMPARTMENT. *S/D* REPAIRED FRAME AT BS 660 STR 22R IAW SRM 51-40-3.

Part: WEB — CORRODED (BS 720C) · airframe 39,793 hrs · 26,597 cycles

CORROSION ON WEB BS 720C 4 LBL 68 WL 208.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,793 hrs · 26,597 cycles

N00519 FRAME DENTED AT BS 520 BETWEEN STR 22L AND STR 24L IN THE FWD CARGO COMPARTMENT. REPAIRED FRAME AT BS 520 BETWEEN STR 22L-STR 24L IAW SRM 51-40-3.

Part: SKIN — CORRODED (BS 720F-740) · airframe 39,793 hrs · 26,597 cycles

INTERIOR FUSELAGE, BS 720F TO BS 740 BETWEEN STR 4L AND STR 4R SKIN HAS CORROSION. *S/D* REPAIR TO BE ACCOMPLISHED ON CUSTOMER ID N01334.

Part: WEB — CORRODED (BS 720B) · airframe 39,793 hrs · 26,597 cycles

CORROSION ON WEB BS 720B 2 LBL 68 WL 208.

Part: FRAME — DENTED (BS 640) · airframe 39,793 hrs · 26,597 cycles

BS 640 RBL 13 WHILE WORKING CARD N00935 FOUND FRAME AT BS 640 RBL 13 DAMAGED. *S/D* REMOVED DAMAGE FROM FRAME, FABRICATED, ALODINED, PRIMED & INSTALLED REPAIR PARTS ON FRAME PER SRM 51-40-3.

Part: SKIN — CORRODED (BS 700-720C) · airframe 39,793 hrs · 26,597 cycles

CORROSION ON INNER SKIN STR 2 RT TO STR 4 RT BS 700 TO BS 720C. ALL WORK WILL BE ACCOMPLISHED ON CARD N01334, 714384 FUSE 5360.

Part: FRAME — DENTED (BS 560) · airframe 39,793 hrs · 26,597 cycles

FRAME DENTED AT BS 560 BETWEEN STR 24L & STR 25L FWD CARGO BAY. REPAIRED FRAME BS 560 FETWEEN STR 24L & STR 25L IAW SRM 51-40-3.

Part: FRAME — DENTED (BS 680) · airframe 39,793 hrs · 26,597 cycles

FRAME DENTED AT BS 680 BELOW STR 22L IN FWD CARGO COMPARTMENT. *S/D* REPAIRED FRAME AT BS 680 BELOW STR 22L IAW SRM 51-40-3.

Part: STRINGER CLIP — CORRODED (BS 720C) · corrosion level 2 · airframe 39,793 hrs · 26,597 cycles

CORROSION ON STRINGER CLIP AT BS 720C S2R. REMOVED CORROSION FOUND OUT OF LIMITS, R & R NEW STRINGER CLIP IAW SRM 51-30-2.

Part: STRINGER CLIP — CORRODED (STR2, RT BS720A) · corrosion level 2 · airframe 39,793 hrs · 26,597 cycles

CORROSION ON STRINGER CLIP AT STR 2 RT BS 720A. REMOVED CORROSION FOUND OUT OF LIMITS R/R NEW STRINGER CLIP PER SRM 51-30-2.

Part: STRINGER CLIP — CORRODED (BS 680) · corrosion level 2 · airframe 39,793 hrs · 26,597 cycles

CORROSION ON STRINGER CLIP AT STR 2 RT BS 680. FOUND CORROSION OUT OF LIMITS. REMOVED AND REPLACED STR CLIP AT BS 680 STR 2 RT PER SRM 51-30-2.

Part: STRINGER CLIP — CORRODED (STR4, RT BS680) · corrosion level 2 · airframe 39,793 hrs · 26,597 cycles

CORROSION ON STRINGER CLIP AT STR 4 RT BS 680. REPAIRED PER SRM 51-30-2.

Part: STRINGER CLIP — CORRODED (BS 720A) · airframe 39,793 hrs · 26,597 cycles

CORROSION ON STRINGER CLIP AT BS 720A, STR 7RT. REMOVED AND REPLACED STRINGER CLIP FOUND TO BE OUT OF LIMITS ALL WORK DONE IAW SRM 53-10-1, 51-30-2

Part: STRINGER CLIP — CORRODED (STR3,RT BS680) · corrosion level 2 · airframe 39,793 hrs · 26,597 cycles

CORROSION ON STRINGER CLIP AT STR 3 RT BS 680. FOUND CORROSION OUT OF LIMITS R/R NEW STR CLIP PER SRM 51-30-2.

Part: STRINGER CLIP — CORRODED (BS 720C) · corrosion level 2 · airframe 39,793 hrs · 26,597 cycles

CORROSION ON STRINGER CLIP AT BS 720C S3R. CORROSION FOUND OUT OF LIMITS R & R NEW STRINGER CLIPS IAW SRM 51-30-2.

Part: STRINGER CLIP — CORRODED (STR 5 BS 720C) · corrosion level 2 · airframe 39,793 hrs · 26,597 cycles

CORROSION ON STRINGER CLIP AT STR 5 RT BS 720C. REMOVED CORROSION FOUND OUT OF LIMITS R/R NEW STR CLIP PER SRM 51-30-2, 51-10-2.

Part: STRINGER CLIP — CORRODED (STR4, RT BS720C) · corrosion level 2 · airframe 39,793 hrs · 26,597 cycles

CORROSION ON STRINGER CLIP AT STR 4 RT BS 720C. REPLACED PER SRM 51-30-6.

Part: FRAME — DENTED (BS1130,STR26R) · airframe 39,793 hrs · 26,597 cycles

N00608 AFT CARGO FRAME DENTED AT BS 1130, STR 26R. REPAIRED PER SRM 51-40-3.

Part: FRAME — DENTED (BS500,STR23-24R) · airframe 39,793 hrs · 26,597 cycles

FRAME DENTED AT BS 500 BETWEEN STR 23R AND STR 24R IN THE FWD CARGO COMPARTMENT. DENTS IN FRAME AT BS 500 BETWEEN STR 23R & 24R IN FLANGE & RADIUS FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED AREA FABRICATED REPAIR PARTS, ALODINED & PRIMED ALL WORK DONE IAW SRM 53-10-1, 51-40-3, 51-10-2.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 39,793 hrs · 26,597 cycles

STRINGER CLIP CRACKED AT BS 720C STR 7 RT. REMOVED CRACKED STR CLIP, FOUND OUT OF LIMITS. INSTALLED NEW CLIP IAW SRM 51-30-06.

Part: FRAME — DENTED (BS1110,STR26L) · airframe 39,793 hrs · 26,597 cycles

AFT CARGO FRAME DENTED AT BS 1110, STR 26L. REPLACED PER SRM 51-40-3, 51-10-2, 51-30-2.

Part: SHEAR WEB — CORRODED (BS 682) · airframe 39,793 hrs · 26,597 cycles

CORROSION ON WEB BS 682 RBL 68 WL 208. REPAIRED WEB AT BS 682 RBL 68 WL 208 IAW SRM 51-10-2, 53-10-01.

Part: STRINGER CLIP — CORRODED (BS 720B) · airframe 39,793 hrs · 26,597 cycles

CORROSION ON STRINGER CLIP AT BS 720B STR2 RT. REMOVED AND REPLACED STRINGER CLIP PER SRM 53-10-1, 51-30-2.

Part: STRINGER CLIP — CORRODED (BS 680) · airframe 39,793 hrs · 26,597 cycles

CORROSION ON STRINGER CLIP AT BS 680, S5 RT. REMOVED AND REPLACED STRINGER CLIP PER SRM 51-30-2.

Part: STRINGER CLIP — CORRODED (BS 720A) · airframe 39,793 hrs · 26,597 cycles

CORROSION ON STRINGER CLIP AT BS 720A STR5 RT. REMOVED AND REPLACED STRINGER CLIP PER SRM 53-10-1, 51-30-2.

Part: STRINGER CLIP — CORRODED (BS 660) · corrosion level 2 · airframe 39,793 hrs · 26,597 cycles

CORROSION ON STRINGER CLIP AT STR 2 RT BS 660. *S/D* REMOVED AND REPLACED STRINGER CLIP STR 2 RT BS 660 IAW SRM 51-30-2 FIG 7.

Part: SHEAR WEB — CORRODED (BS 705) · airframe 39,793 hrs · 26,597 cycles

CORROSION ON WEB BS 705 RBL 68 WL 208. REPAIRED WEB BS 705 RBL 68 WL 208 IAW SRM 51-10-2, 53-30-2.

Part: STRINGER CLIP — CORRODED (BS 720B) · airframe 39,793 hrs · 26,597 cycles

CORROSION ON STRINGER CLIP AT BS 720B STR3 RT. REMOVED AND REPLACED STRINGER CLIP PER SRM 51-30-2.

Part: STRINGER CLIP — CORRODED (BS 680) · airframe 39,793 hrs · 26,597 cycles

CORROSION ON STRINGER CLIP AT STR 6 RT BS 680. *S/D* REMOVED AND REPLACED STRINGER CLIP PER SRM 51-30-2.

Part: STRINGER CLIP — GOUGED (BS 849) · airframe 39,793 hrs · 26,597 cycles

STRINGER CLIP GOUGED AT BS 849 S5R. REPAIRED PER SRM 51-30-2.

Part: STRINGER CLIP — CORRODED (BS 660) · corrosion level 2 · airframe 39,793 hrs · 26,597 cycles

CORROSION ON STRINGER CLIP AT STR 7 RT BS 660. REMOVED AND REPLACED STRINGER CLIP AT STR 7 RT BS 660 IAW SRM 51-30-2 FIG 7.

Part: FRAME — DENTED (BS 950B) · airframe 39,793 hrs · 26,597 cycles

AFT CARGO FRAME DENTED AT BS 950B BETWEEN STR 25 & 26 L. REPAIRED AFT CARGO BAY FRAME AT BS 950B BETWEEN STR 25L - 26L PER SRM 51-40-3.

Part: STRINGER CLIP — CORRODED (BS 660) · corrosion level 2 · airframe 39,793 hrs · 26,597 cycles

CORROSION ON STRINGER CLIP AT STR 6 RT BS 660. REMOVED AND REPLACED STRINGER CLIP AT STR 6 RT BS 660 PER SRM 51-30-2 FIG 7.

Part: STRINGER CLIP — CORRODED (BS 700) · corrosion level 2 · airframe 39,793 hrs · 26,597 cycles

CORROSION ON STRINGER CLIP AT BS 700 STR5 RT. REMOVED AND REPLACED STRINGER CLIP AT BS 700 STR 5 RT PER SRM 51-30-2 FIG 7.

Part: STRINGER CLIP — CORRODED (BS 660) · corrosion level 2 · airframe 39,793 hrs · 26,597 cycles

CORROSION (C53-224-01, 1) ON STRINGER CLIP AT STR 4 RT BS 660. REMOVED AND REPLACED STRINGER CLIP STR 4 RT BS 660 PER SRM 51-30-2 FIG 7.

Part: STRINGER CLIP — CORRODED (BS 700) · corrosion level 2 · airframe 39,793 hrs · 26,597 cycles

CORROSION ON STRINGER CLIP AT BS 700 STR 6 RT. REMOVED AND REPLACED STRINGER CLIP AT BS 700 STR 5 RT PER SRM 51-30-2 FIG 7.

Part: STRINGER CLIP — CORRODED (BS 700) · corrosion level 2 · airframe 39,793 hrs · 26,597 cycles

CORROSION ON STRINGER CLIP AT STR 7 RT BS 700. REMOVED AND REPLACED STRINGER CLIP AT BS 700 STR 7 RT PER SRM 51-30-2 FIG 7.

Part: FRAME — DENTED (BS 950C) · airframe 39,793 hrs · 26,597 cycles

AFT CARGO FRAME DENTED AT BS 950C BETWEEN STR 25 AND 26L. REPAIRED PER SRM 53-10-1, 53-10-2, 51-40-3.

Part: STRINGER CLIP — CORRODED (BS 660) · corrosion level 2 · airframe 39,793 hrs · 26,597 cycles

CORROSION ON STRINGER CLIP AT STR 5 RT BS 660. REMOVED AND REPLACED STRINGER CLIP AT STR 5 RT BS 660 IAW SRM 51-30-2 FIG 7.

Part: STRINGER CLIP — CORRODED (BS 660) · corrosion level 2 · airframe 39,793 hrs · 26,597 cycles

CORROSION ON STRINGER CLIP AT STR 8 RT BS 660. REMOVED AND REPLACED STRINGER CLIP STR 8 RT BS 660 PER SRM 51-30-2 FIG 7.

Part: STRINGER CLIP — CORRODED (BS 660) · corrosion level 2 · airframe 39,793 hrs · 26,597 cycles

CORROSION ON STRINGER CLIP AT STR 3 RT BS 660. REMOVED AND REPLACED STRINGER CLIP STR 3 RT BS 660 IAW SRM 51-30-2 FIG 7.

Part: HOUSING — CRACKED (CEILING LIGHT) · airframe 39,793 hrs · 26,597 cycles

FWD CARGO COMPT CEILING LIGHT HOUSING CRACKED IN SEVERAL PLACES AT BS 608 LBL 32 WL 202. REMOVED AND REPLACED FWD CARGO COMPT. CEILING LIGHT HOUSING AT BS 608 LBL 32 WL 202. IAW IPC 33-30-00-02.

Part: FRAME — DENTED (BS 680) · airframe 39,793 hrs · 26,597 cycles

FRAME DENTED AT BS 680 BELOW STR 23R IN THE FORWARD CARGO COMPARTMENT. REPAIRED FRAME AT BS 680 BELOW STR 23R IAW SRM 51-40-3.

Part: REPAIR — MISMANUFACTURED (BS 577-595) · airframe 39,793 hrs · 26,597 cycles

DOUBLER REPAIR AT FLOOR SUPPORT STRUCTURE STA 577 TO 595 LBL 9.00 LWR FWD CABIN REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EVALUATED DOUBLER REPAIR AT FLOOR SUPPORT STRUCTURE BS 577-595 LBL 9 IN FWD CARGO BAY, DETERMINED NOT TO BE ACCOMPLISHED PER FAA APPROVED DATA REMOVED, FABRICATED REPAIR PARTS USING BSC1517-1507 7075F6511 LOT 661129 AND BAC1490-2738. 7075T6511 LOT 661133, INSTALLED REPAIR PARTS. ALL WORK DONE IAW SRM 51-40-4, 51-30- 2, 51-10-2. THIS IS CONSIDERED A MAJOR REPAIR.

Part: SKIN — GOUGED (BS 220) · airframe 39,793 hrs · 26,597 cycles

EXTERNAL FUSELAGE SKIN GOUGED BS 220 WL 218 LT SIDE. REPAIRED PER SRM 53-30-3, 53-30-1, 53-30-2, MAJOR REPAIR

Part: BEAR STRAP — CORRODED (BS 720A) · airframe 39,793 hrs · 26,597 cycles

BEAR STRAP CORRODED AT BS 720A BETWEEN STR 2 RT AND STR 4 RT. *S/D* REMOVED CORROSION ON BONDED DOUBLER IS IN LIMITS IAW SRM 53-30-01.

Part: BEAR STRAP — CORRODED (BS 720) · airframe 39,793 hrs · 26,597 cycles

BEAR STRAP CORRODED AT BS 720 BETWEEN STR 2R AND STR 4 RT. REMOVED CORROSION ON BONDED DOUBLER AT SB 720 BETWEEN STR 2 RT AND 4 RT IAW SRM 53-30-1.

Part: SKIN — BULGED (BS 212) · airframe 39,793 hrs · 26,597 cycles

BS 212, STR 26-27R, BULGE IN SKIN. REPAIRED BULGE IN SKINJ PER SRM 53-30-3.

Part: STRINGER CLIP — CRACKED (BS 680) · airframe 39,793 hrs · 26,597 cycles

INTERIOR FUSELAGE STRINGER CLIP 7L IS CRACKED BS 680. *S/D* REMOVED AND REPLACED STRINGER CLIP 7L AT BS 680 IAW SRM 51-30-2.

Part: STRINGER CLIP — CORRODED (BS 720A) · airframe 39,793 hrs · 26,597 cycles

CORROSION ON STRINGER CLIP AT BS 720A STR 3 RT. *S/D* REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-30-2.

Part: SKIN — CORRODED (BS 680) · airframe 39,793 hrs · 26,597 cycles

CORROSION ON INTERNAL BONDED DOUBLER BS 680 STR 4 RT - 4 LT. REMOVED CORROSION ON INTERNAL BONDED DOUBLER AT BS 680 BETWEEN STR 4 R/H TO STR 4 L/H IAW SRM 53-30-1.

Part: BEAR STRAP — CORRODED (BS 700) · airframe 39,793 hrs · 26,597 cycles

BEAR STRAP CORRODED AT BS 700 BETWEEN STR 2 RT AND STR 4 RT. *S/D* REMOVED CORROSION AND IS IN LIMITS IAW SRM 53-30-01.

Part: SKIN — CORRODED (BS 660-680) · airframe 39,793 hrs · 26,597 cycles

CORROSION ON INTERNAL SKIN BS 660 - 680 STR 2-3 LT. BLENDED CORROSION ON SKIN BS 660-680 AND STR 2-3 LT FOUND TO BE WITHIN LIMITS, ALODINE AND PRIMED AREA, ALL IAW SRM 53-30-1 AND 51-10-2.

Part: SKIN — CORRODED (BS 640-680) · airframe 39,793 hrs · 26,597 cycles

CORROSION ON INTERNAL SKIN BS 640-680 STR 4-5 RT. *S/D* REPAIRED PER SRM 53-10-1.

Part: BEAR STRAP — CORRODED (BS 720B) · airframe 39,793 hrs · 26,597 cycles

BEAR STRAP CORRODED AT BS 720B BETWEEN STR 2 RT AND STR 4 RT. *S/D* REMOVED CORROSION AND IS IN LIMITS IAW SRM 53-30-01.

Part: REPAIR — CORRODED (BS 784) · airframe 39,793 hrs · 26,597 cycles

PREVIOUS REPAIR AT BS 784 BETWEEN STRINGERS 7 & 8 FASTENERS ARE CORRODED. REMOVED AND REPLACED FASTENERS PER SRM 51-30-2.

Part: SKIN — CORRODED (BS 680-700) · airframe 39,793 hrs · 26,597 cycles

CORROSION ON INTERNAL SKIN BS 680-700 STR 4 RT - 4 LT. REMOVED AND REPLACED SKIN BS 680-BS700 STR 4R TO 4L IAW SRM 51-30-2.

Part: DOUBLER — CORRODED (BS 660) · airframe 39,793 hrs · 26,597 cycles

CORROSION ON INTERNAL BONDED DOUBLER BS 660 BETWEEN STR 3 - 4 LT. REMOVED CORROSION ON INTERNAL BONDED DOUBLER AT BS 660 BETWEEN STR 3 & 4 LT IAW SRM 53-30-1.

Part: STRINGER CLIP — CORRODED (BS 700) · airframe 39,793 hrs · 26,597 cycles

INTERIOR FUSELAGE, STR CLIPS HAS CORROSION BETWEEN BS 700 TO BS 720, STR 2L. REMOVED AND REPLACED THREE STR CLIPS AT STR 2L BS 700, BS 703 AND BS 713 IAW SRM 51-30-2.

Part: SKIN — CORRODED (BS 740-870) · airframe 39,793 hrs · 26,597 cycles

UPPER CROWN SKIN HAS SURFACE CORROSION ON INNER SIDE, BS 740-BS 870, STR 1 - STR 4R.

Part: STRINGER — CORRODED (BS 620-700) · airframe 39,793 hrs · 26,597 cycles

CORROSION ON STRINGER 4 RT BS 620-700. CORROSION OUT OF LIMITS, STRINGER SECTION BS 660 - 720E TO BE REPLACED ON CARD N00343.

Part: STRINGER — CORRODED (BS 620-700) · airframe 39,793 hrs · 26,597 cycles

CORROSION ON STRINGER 3 RT BS 620-700.

Part: STRINGER — CORRODED (BS 640-700) · airframe 39,793 hrs · 26,597 cycles

CORROSION ON STRINGER 2 LT BS 640-700. CORROSION OUT OF LIMITS, STRINGER SECTION TO BE REPLACED ON CARD N00346.

Part: STRINGER CLIP — CORRODED (BS 720A) · airframe 39,793 hrs · 26,597 cycles

INTERIOR FUSELAGE, STR CLIP 5R HAS CORROSION BS 720A. *S/D* REMOVED AND REPLACED STR CLIP 5R BS 720A IAW SRM 51-30-2.

Part: STRINGER CLIP — CORRODED (BS 720A) · airframe 39,793 hrs · 26,597 cycles

INTERIOR FUSELAGE, STR CLIP 3R HAS CORROSION BS 720A. *S/D* REMOVED AND REPLACED STR CLIP 3R BS 720A IAW SRM 51-30-2.

Part: STRINGER CLIP — CORRODED (BS 720A) · airframe 39,793 hrs · 26,597 cycles

INTERIOR FUSELAGE, STR CLIP 3L HAS CORROSION BS 720A. *S/D* REMOVED AND REPLACED STR CLIP 3L BS 720 IAW SRM 51-30-2.

Part: STRINGER CLIP — CRACKED (BS 680) · airframe 39,793 hrs · 26,597 cycles

INTERIOR FUSELAGE, STR CLIP 4L IS CRACKED, BS 680. *S/D* REMOVED AND REPLACED CRACKED STR CLIP 4L AT BS 680 IAW SRM 51-30-2.

Part: STRUCTURE — CORRODED (CARGO CEILING) · airframe 39,793 hrs · 26,597 cycles

AFT CARGO CEILING SUPPORT STRUCTURE CORRODED AT BS 1070 LBL 25 WL 201. REMOVED CORROSION FROM SUPPORT FOUND TO BE OUT OF LIMITS FABRICATED NEW SUPPORT INSTALLED REPAIR PART ALL WORK DONE IAW 53-10-1 51-20-1 53-10-8 51-30-2 & 51- 10-2

Part: FLOORBEAM — CORRODED (CARGO BAY) · airframe 39,793 hrs · 26,597 cycles

AFT CARGO, FLOORBEAM LOWER FLANGE CORRODED AT BS 1070, LBL 28, WL 201. REPAIRED PER SRM 53-10-8.

Part: COMPRESSOR — STALLED (NR 2 ENGINE) · airframe 39,433 hrs · 26,277 cycles

ON TAKEOFF ROLL THROTTLES SMOOTHLY ADVANCED TO T/O PWR NR 2 ENGINE HAD AVERY PRONOUNCED COMPRESSOR STALL APPROX. 5-8 SEC. INTO TAKEOFF ROLL REJECTED T/O AND CLEARED RUNWAY. INSPECTED INLET AND EXHAUST NO DAMAGE NOTED. PERFORMED TAKEOFF POWER EPR TEST REF TO 727 JRH CHAP 4. ALL NR 2 ENGINE PARAMETERS NORMAL NO STALLS NOTED ON 2 RUN UPS.

Part: WARNING LIGHT — ILLUMINATED (COCKPIT) · airframe 39,070 hrs · 25,997 cycles

AFTER DEPARTURE MEM NR 4 SLAT INDICATED EXTENDED WITH FLAPS SELECTED TO 2 DEGREES. AMBER L/E FLAPS LIGHT ILLUMINATED ON FOWARD PANEL. GREEN NR 4 SLAT ANNUNCIATOR LIGHT ILLUMINATED DN F/E AUX PANEL. COMPLIED WITH CHECKLIST PROBLEM. RETURNED FOR LANDING. CYCLED LEADING EDGE SLAT & OVERIDE SWITCHES S1010 & S1011, CYCLED SLATS SEVERAL TIMES NR 4 SLAT AMBER & GREEN LIGHTS OPS CHECK SATISFACTORY ON FWD & AFT PANELS. A/C OK FOR SERVICE. ALSO VISUAL CHECK OF SLATS OPS CHECK NORMAL.

Part: WARNING LIGHT — ILLUMINATED (SLATS) · airframe 39,070 hrs · 25,997 cycles

AFTER DEPARTURE MEM NR 4 SLAT INDICATED EXTENDED WITH FLAPS SELECTED TO 2 DEGREES. AMBER L/E FLAPS LIGHT ILLUMINATED ON FORWARD PANEL. GREEN NR 4 SLAT ANNUNCIATOR LIGHT ILLUMINATED DN F/E AUX PANEL. COMPLIED WITH CHECKLIST PROBLEM. RETURNED FOR LANDING. CYCLED LEADING EDGE SLAT & OVERIDE SWITCHES S1010 & S1011, CYCLED SLATS SEVERAL TIMES NR 4 SLAT AMBER & GREEN LIGHTS OPS CHECK SATISFACTORY ON FWD & AFT PANELS. A/C OK FOR SERVICE. ALSO VISUAL CHECK OF SLATS OPS CHECK NORMAL.

Part: WIRE — FAILED (TE FLAPS) · airframe 37,256 hrs · 24,588 cycles

ON ARRIVAL, WHEN TRAILING FLAPS EXTENDED TO 5 DEG, THE AMBER LEADING EDGE FLAPS LIGHT REMAINED ILLUMINATED ON FO PANEL AND THE NR 5 LEADING EDGE FLAP LIGHT (BOTH GREEN AND AMBER), DID NOT ILLUMINATE ON SO PANEL. RAN QRH PROCEDURE AND DIVERTED. ON ARRIVAL, FLAPS/SLATS EXTENDED NORMALLY. INSTALLED LEADING EDGE FLAP JUMPER SWITCH FOR NR 5 LEADING EDGE FLAP SWITCH. OPERATED FLAP SYSTEM SEVERAL TIMES AND SYSTEM CKS GOOD IAW MM. REQUIRES JUMPER, REMOVED AND FLAP SWITCH REPLACED AS TIME PERMITS.

Part: INDICATOR — MALFUNCTIONED (COCKPIT)

AFTER DEPARTURE NR 5 LED WOULD NOT RETRACT. RAN RED TABS, NO RELIEF. REMOVED AND REPLACED SLAT-FLAP DISPLAY MODULE PRECAUTION PER MM 27-82-031-4.

Part: ACCESSORY UNIT — FALSE ACTIVATION (E&E BAY)

RIGHT GEAR UNSAFE LIGHT CAME ON WITH GEAR HANDLE IN OFF POS. REMOVED AND REPLACED LAND GEAR ASSY UNIT PER MM 32-09-121. SYS TEST GOOD.

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

00-346 WHEN FLAPS 15 SEL ALL 3 GEAR DOOR LIGHTS ILLUM. R&R LAND GEAR ACCESSORY UNIT. PERF TEST PER B 727 MM 32-09-122-5, AND EA 7-3209-40871, FUNC. TEST NORMAL.

Part: SOCKET — FAILED (CARGO DOOR)

99-215 - MAIN CARGO DOOR LIGHT ILLUM 25 MIN INTO FLT AT FLT LEVEL 330. REMOVED AND REPLACED SOCKET ASSY AND OPER CK MAIN CARGO DOOR PER MM 53-34-000-5. OPER CK NORM.

Part: DUCT — CRACKED (AFT AIRSTAIRS)

LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED 5 MINUTES AFTER TAKEOFF WITH WING AND ENGINE ANTI-ICE OPEN. ALTITUDE 10,000 FEET AT CLIMB. POWER LIGHT EXTINGUISHED ONE MINUTE AFTER CLOSING WING ANTI-ICE. CRACKED DUCT FOUND IN AFT AIRSTAIRS AREA. CANNIBALIZED DUCT FROM AIRCRAFT 199 TO BE INSTALLED ON AIRCRAFT. INSTALLED DUCT, LEAK CHECK GOOD.

Part: SEAT TRACK — CORRODED (BS 950)

CORROSION (C53-224-04), ON SEAT TRACK AT CLIP NUTHOLES BS 950E PLUS 18 RBL 1. REPLACED SEAT TRACK AND INSTALLED REPAIR STRAP IAW FEDEX SRM 53-10-05.

Part: K-FLAP — CORRODED (NR 5 LE FLAP)

NR 5 K-FLAP O/B LUB O/B SIDE UPPER MOUNT BOLT HAS CORROSION UNDER NUT. CORROSION WAS FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED NR 5 K-FLAP AND FUNCTIONAL CHECK IAW FEDEX MM 27-81-1.

Part: STRINGER CLIP — CRACKED (BS 440)

CRACKED STR CLIP AT BS 440 STR 1L. UPON REMOVAL OF CRACKED STR CLIP FOUND STR NR 1 TO BE DAMAGED AT BS 441. PERFORMED STR REPAIR BS 436 TO 446 STR NR 1 IAW FEDEX SRM 53-10-3 AND INSTALLED NEW STR CLIP BS 440 STR NR 1.

Part: KEEL BEAM — CORRODED (BS 950)

CORROSION ON LT KEEL BEAM OUTBOARD FLANGE AT BS 950D PLUS 3, LBL 10. REMOVED CORROSION ON LT KEEL BEAM OUTBOARD FLANGE AND REPAIRED PER FEDEX EA 7-5310-26837.

Part: STRINGER — CORRODED (BS 720)

CORROSION (C53-224-01), ON STR FLANGE AT BS 720 STR 4L. REMOVED DAMAGED SECTION OF STR, FABRICATED AND INSTALLED REPAIR PARTS PER FEDEX SRM 53-10-3.

Part: FRAME — DAMAGED (BS 600)

DAMAGED FRAME AND STR CLIP AT BS 600 RT STR 7. REPAIRED FRAME AT BS 600 STR 7 TO 8R IAW FEDEX SRM 53-10-4. REMOVED DAMAGED STR CLIP AND INSTALLED NEW STR CLIP AT BS 600 STR 7R.

Part: STRINGER — DAMAGED (BS 660)

DAMAGED STR AT BS 660 STR 7L. REPAIRED DAMAGED STR 7L BS 660 PER FEDEX SRM 53-10-3, BY REMOVING DAMAGED SECTION AND FABRICATING REPAIR PARTS AND INSTALLING THEM.

Part: LUG — CORRODED (NR 5 LE FLAP)

NR 5 K-FLAP O/B LUG O/B SIDE UPPER MOUNT BOLT HAS CORROSION UNDER NUT. CORROSION WAS FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED NR 5 K-FLAP AND FUNCTIONAL CHECKED IAW FEDEX MM 27-81-1.

Part: STR CLIP — DAMAGED (BS 950)

DAMAGED STR CLIP, BS 950F STR 7L. REMOVED AND REPLACED STR CLIP BS 950F STR 7L PER FEDEX SRM 51-30-2.

Part: FLOOR BEAM — CORROSION (BS 400)

CORROSION (C53-224-01-1), ON FLOOR BEAM AT FASTENER HOLE BS 400 RBL 35 WL 207.9. PERFORMED FLOOR BEAM REPAIR AT BS 400 RBL 29 TO 42 WL 207.9 IAW FEDEX SRM 53-10-8, 51-40.

Part: FLOORBEAM — CORRODED (BS 360)

CORROSION (C53-224-01-1) ON FLOORBEAM AT CLIP NUT HOLE BS 360 RBL 12 WL 208. REMOVED CORROSION ON FLOORBEAM BS 360 RBL 12 WL 208 FOUND TO BE OUT OF LIMITS, ORIGINAL .130 AND REMOVED .032 FROM 1 INCH BY 2 INCH AREA. FABRICATED AND INSTALLED REPAIR ANGLES FOR FLOORBEAM AT BS 360 RBL 12 WL 208 PER FEDEX SRM 53-10-8, ALODINED AND PRIMED.

Part: FRAME — CRACKED (BS 380)

FRAME CRACKED AT STA 380 WL 278 RBL 65. REMOVED DAMAGED SECTION OF FRAME AT BS 380 WL 278 RBL 65. FABRICATED REPAIR ANGLE AND DOUBLERS, ALODINED, PRIMED AND INSTALLED WET. ALL WORK DONE PER FEDEX SRM 53-10-4.

Part: CLIP — CRACKED (BS 660)

CORROSION (C53-224-01) IN STR AND STR CLIP AT BS 660 STR 3R. REMOVED CORROSION AT STR 3 BS 660 RT. ORIGINAL THICKNESS .045, REMOVED .002, 5 INCH BY 1 INCH AREA WITHIN LIMITS PER FEDEX SRM 53-10-1, ALODINED AND PRIMED AREA. REMOVED STR CLIP AT BS 660 RT DUE TO CRACK. REPLACED STR CLIP PER FEDEX SRM 53-10-1.

Part: FRAME — DAMAGED (BS 560)

CRACKED IN FRAME BS 560 RT BETWEEN STR 7 AND 8. REPAIRED DAMAGED FRAME BS 560 RT BETWEEN STR 7 AND 8 IAW FEDEX SRM 53-10-4. FRAME WAS FOUND NOT TO HAVE INDICATION IAW D6-48875 PT6, 51-00-00 FIG 23.

Part: STRINGER — DAMAGED (BS 757-759)

MECH DAMAGE AND FASTENERS MISSING IN STR 7L BS 757 TO 759. ACCOMPLISHED STR REPAIR AT STA 740 TO 770 STR 7L PER FEDEX SRM 53-10-1, 53-10-2 AND 53-10-3.

Part: STRINGER — CORROSION (BS 720)

CORROSION (C53-224-01), ON STR FLANGE AT BS 720 LT STR 4. REMOVED DAMAGED SECTION OF STR, FABRICATED AND INSTALLED REPAIR PARTS PER FEDEX SRM 53-10-3.

Part: SEAT TRACK — CORRODED (BS 950)

CORROSION (C53-224-04), ON SEAT TRACK AT CLIP NUT HOLES BS 950E PLUS 18 RBL 1. REPLACED SEAT TRACK AND INSTALLED REPAIR STRAP IAW FEDEX SRM 53-10-05.

Part: FLOOR BEAM — CORROSION (BS 720)

CORROSION ON LOWER FLANGE OF FLOOR BEAM AT BS 720 WL 200 LBL 45 TO RBL 45. REPAIRED FLOOR BEAM AT BS 720 WL 200 LBL 45 TO RBL 45.