N490FE

Part: SKIN — GOUGED (ZONE 100) · airframe 43,394 hrs · 28,778 cycles

REWORK - NUMEROUS GOUGES MCD INNER SURROUND SKIN STA 620-640, S11-17L. REF: SNRM N00698 - EA 7-5330-143901 MCD SURROUND INNER SKIN REVISED. ACCOMPLISHED REPAIR ON MCD INNER AFT LOWER SKIN IAW FEDEX EA# 7-5330-143901 CUTOUT INNER SKIN SECTION DIM: 22" X 17" AND FABRICATED 2 EA. REPAIR WEBS 22" X 17" & 40 1/4" X 22", 2 EA. REPAIR SPLICE 22" X 5" EACH FROM 2024-T3 .125 IAW EA 7-5330- 143901, TREATED, PRIMED AND INSTALLED REPAIR PARTS & MCD INNER SKIN BS 620- 640 S11-17L IAW B727 51-10-2 & 51-30-2 & EA 7-5330-143901.

Part: WEB — DAMAGED (HORIZONTAL STAB) · airframe 43,394 hrs · 28,778 cycles

LT HORIZ STAB INTERNAL WEB AT STAB STA 151.81 DAMAGED. CUTOUT DAMAGED AREA, FABRICATED REPAIR DOUBLER & FILLER, INSTALLED REPAIR DOUBLER & FILLER AT LT HORIZONTAL STAB STA 151.81 IAW SRM 55-10-2, FIG 2, SRM 53-10-9, FIG 4, SRM 51-30-2, & SRM 51-10-2.

Part: SKIN — GOUGED (HORIZONTAL STAB) · airframe 43,394 hrs · 28,778 cycles

LT SIDE LWR SKIN HORIZ STAB APPRX STA 140 TO 155 HAS GOUGE & DENT CAUSED BY HIGH REACH. CUTOUT DAMAGED SECTION OF SKIN ON LT LWR SKIN OF HORIZ STAB AT APPROX STA 140 TO 155, 8.2500" X 9.2500" IAW EX SRM REV 103, 55-10-3 FIG 4. FABRICATED REPAIR DOUBLER FROM 2024T3, .071" X 14.1250" X 13.2500" AND FILLER FROM 2024T3 .050" X 8.2500" X 9. 2500" IAW SRM 55-10-3, FIG 4. INSTALLED DOUBLER AND FILLER IAW SRM 55-10-3, FIG 4.

Part: RIB — DAMAGED (HORIZONTAL STAB) · airframe 43,394 hrs · 28,778 cycles

LT HORIZ STAB RIB AT LWR STAB STA 151.81 DAMAGED. CUTOUT DAMAGED SECTION OF LT HORIZ RIB LOWER CHORD AT STAB STA 151.81, 13.6250 " LONG IAW SRM REV 103, 55-10-4 FIG 1. FABRICATED REPAIR ANGLES FROM 2024-O, .071" X 24" X 4", QTY 2, IAW SRM 55-10-4, FIG 1 AND FILLER FROM 2024T3, .063" X 13.7500" X 1.5" IAW SRM 55-10-4, FIG 1. INSTALLED REPAIR FILLER AND ANGLES IAW SRM 55-10-4, FIG 1. HEAT TREATED 2024-0 TO T4 CONDITION IAW ENGINEERING REPORT 2-37153-801, REV A.

Part: FLOORBEAM — CORRODED (BS 720) · corrosion level 2 · airframe 43,394 hrs · 28,778 cycles

CORROSION - STA 720 FLOORBEAM, LWR FLANGE LWR SURFACE RBL 24.75 - RBL 37. CUT OUT APPROX 4.0" AREA OF BS 720 FLOORBEAM LWR FLANGE AT RBL 36 IAW SRM, REV 103, 53-10-8, FIG 2. FABRICATED (2) REPAIR ANGLES USING 7075-0, .063" X 3" X 15", FILLER USING BAC1505-100797, 7075-T6, 2" X 4" AND STRAP USING 7075-T6, .10" X 2" X 13" IAW SRM 53-10-8, FIG 2. INSTALLED REPAIR PARTS IAW SRM REV 103, 53-10-8 FIG 2.

Part: FLOORBEAM — CORRODED (BS 720) · corrosion level 2 · airframe 43,394 hrs · 28,778 cycles

CORROSION - STA 720 FLOORBEAM, LOWER FLANGE, LOWER SURFACE, RBL 12 TO LBL 12. CUT OUT (2) SECTIONS OF BS 720 FLOORBEAM LOWER FLANGE 5.75" AND 7.5" AT RBL 6.5 AND LBL 3.0 IAW SRM, REV 103, 53-10-8 FIG 2. FABRICATED (2) REPAIR ANGLES USING 7075-0, .063" X 35" X 2 5/8", (2) FILLERS USING BAC1505-100797, 7075T-6, 5.75" IN LENGTH AND 7.5" IN LENGTH, AND STRAP USING 7075-T6, .100" X 33 1/8" X 2.1250" IAW SRM 53-10-8, FIG 2. INSTALLED ANGLES, FILLERS AND STRAP IAW SRM 53-10-8, FIG 2.

Part: FLOORBEAM — CORRODED (BS 950D) · corrosion level 2 · airframe 43,394 hrs · 28,778 cycles

CORROSION LOWER SURFACE OF FLOORBEAM LOWER FLANGE, STA 950D, LBL 25 - LBL 45 CUT OUT DAMAGE IN LOWER CHORD OF FLOORBEAM 23 1/4" LONG IAW SRM REV 103, 53-10-8 FIG 2. FABRICATED 2 REPAIR ANGLES FROM 7075-T6, .063" X 31 1/2" X 2 5/8", FILLER FROM BAC 1505-100797, 23 1/4" X 2 3/8", STRAP FROM 7075-T6 .063" X 33 5/8" X 2 1/8" IAW SRM 53-10-8 FIG 2, INSTALLED ANGLES, FILLER AND STRAP IAW SRM 53-10-8 FIG 2.

Part: FLOORBEAM — CORRODED (BS 1130) · corrosion level 2 · airframe 43,394 hrs · 28,778 cycles

CORROSION - LOWER FLANGE, LOWER SURFACE OF FLOORBEAM - STATION 1130, RBL 3. CUT OUT DAMAGE ON LOWER FLANGE OF FLOORBEAM 8" X 3/4" IAW B727 SRM 53-10-8 FIG 10. FABRICATED ANGLE FROM 7075-O, .050" X 2.9" X 30", STRAP FROM 7075-T6 .063" X 2" X 17 3/8" AND FILLERS FROM AND10134-2007, 7075-T6511, 8" X 3/4" AND 4 1/2" X 1" IAW SRM REV 103, 53-10-8 FIG 10 DETAIL 5. INSTALLED ANGLE, STRAP AND FILLERS IAW SRM 53-10-8 FIG 10.

Part: SEAT TRACK — CORRODED (BS 690-740) · corrosion level 2 · airframe 43,394 hrs · 28,778 cycles

CORROSION SEAT TRACK FLANGE/SCALLOPS MAIN CABIN RBL 25 BS 690 - BS 740. REMOVED DAMAGED SEAT TRACK SECTION FROM BS 690 - BS 740 RBL 25, FABRICATED NEW SEAT TRACK SECTION & INSTALLED SEAT TRACK IAW SRM 53-10-5 FIG 1 AND SRM 51-30-2.

Part: SKIN — GOUGED (BS 620-640) · airframe 43,394 hrs · 28,778 cycles

NUMEROUS GOUGES MCD INNER SURROUND SKIN STA'S 620-640 S11-17L. CUTOUT DAMAGED SKIN SECTIONS (3 EA.), FABRICATED NEW SKIN SECTION & SPLICE & FABRICATED REPAIR DOUBLER INSTALLED NEW SKIN SECTION, SPLICE & REPAIR DOUBLER AT AFT LWR MCD INNER SKIN IAW EA 7-5330-143901. REWORK REQUIRED IAW THE SNRM AND SNRM N01103. EA 7-5330-143901 "MCD SURROUND INNER SKIN REVISED".

Part: SKIN — GOUGED (BS 565 S4L) · airframe 43,394 hrs · 28,778 cycles

GOUGE, MCD INNER SURROUND SKIN STA 565, STR 4L. REMOVED DAMAGED MCD INNER SKIN, FABRICATED NEW INNER SKIN & INSTALLED NEW INNER SKIN AT BS 506 - BS 594, MCD INNER SKIN IAW SRM 53-10-2 FIG 3A, SRM 51-30-5, SRM 51-30-2.

Part: SKIN — CRACKED (LT WING TE FLAP) · airframe 43,394 hrs · 28,778 cycles

POSSIBLE CRACK OR DEBONDED L/E INBD FOREFLAP LT WING AT NR4 FLAP ASSY ATTACHMENT. CUTOUT DAMAGE DIM: 1" X 1" AND FABRICATED DOUBLER DIM: 5" X 5 1/4" AND INSTALLED DOUBLER IAW SRM 57-50-4 FIG 1, SRM 51-10-2, SRM 51-30-2, AND NDTM 51-00-00.

Part: SEAT TRACK — CORRODED (BS 390-480) · corrosion level 2 · airframe 43,394 hrs · 28,778 cycles

CORROSION SEAT TRACK RBL 25 BS 390 - BS 480 ON FLANGE AND SCALLOPS REMOVED SEAT TRACK SECTION FROM BS 390 BS 480 RBL 25, FABRICATED NEW SEAT TRACK & SPLICE, INSTALLED NEW SEAT TRACK & SPLICE IAW SRM 53-10-5 FIG 1 & SRM 51-30-2.

Part: RIB — CRACKED (NR 5 SLAT) · airframe 43,394 hrs · 28,778 cycles

UPON REMOVAL OF AFT ACCESS PANEL, FOUND NR 5 SLAT TO HAVE 1 CRACKED RIB ON THE OUTBD SIDE. REMOVED DAMAGED RIBS IB & OB, FABRICATED NEW IB & OB RIBS & INSTALLED NEW IB & OB RIBS AT NR 5 SLAT IAW SRM 51-30-5, SRM 51-30-2, SRM 51-10-2, & DWG NR 65-17294 & FAS ER 2-37153-801, REV A.

Part: SEAT TRACK — CORRODED (BS 390-480) · corrosion level 2 · airframe 43,394 hrs · 28,778 cycles

CORROSION SEAT TRACK FLANGE MAIN CABIN LBL 25 BS 390- 480 REMOVED & REPLACE SEAT TRACK FROM BAC 1520-792-7178-T6511 APPROX DIM 89.5" IAW SRM 53-10-5 FIG 1, SRM 51-30-2, & SRM 51-10-2.

Part: RIB — CRACKED (LT WING TE FLAP) · airframe 43,394 hrs · 28,778 cycles

RIB CRACKED LT WING IB FOREFLAP REMOVED LH IB FORE FLAP OB END RIB IAW SRM 51-30-2 AND FABRICATED NEW RIB FROM 2024O .040 HEAT TREATED TO T4 CONDITION DIM: 7" X 5 1/2" IAW ER 2-37153-801 REV A AND SRM 51-20-1 AND SRM 57-50-2 FIG 5. INSTALLED NEW RIB LT IB FOREFLAP OB END IAW SRM 51-30-2 AND EA 7-5750-143908.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 43,394 hrs · 28,778 cycles

CORROSION TOP TEE CAP FLOORBEAM, BL 0 TO RBL 25. CUTOUT DAMAGE AREA APPROX DIM: 2" X 6.6". FABRICATED UPPER TEE FROM BAC 1505-100617-7075T6 APPROX DIM 18" X 2", SUPPORT ANGLES AND REINFORCEMENT STRAPS. INSTALLED REPAIR PARTS IAW SRM 53-10-8 FIG 3, 51-20-01 AND 51-30-2.

Part: FLOORBEAM — CORRODED (BS 720D) · corrosion level 2 · airframe 43,394 hrs · 28,778 cycles

CORROSION TOP TEE CAP FLOORBEAM MAIN CABIN BS 720D LBL 25 - BL 0. CUTOUT DAMAGE TEE CAP FLOORBEAM DIM: 2" X 9.2" BS 720D LBL 2.8 TO LBL 12, FABRICATED TEE CAP FLOORBEAM FROM BAC 1505-100617-7075T6 DIM: 23.125" X 2" AND UPPER CHORD, SUPPORT ANGLES AND REINFORCEMENT STRAPS. INSTALLED REPAIR PARTS IAW SRM 53-10-8 FIG 3, SRM 51-20-1 & SR, 51-30-2.

Part: RIB — CHAFED (NR 2 SLAT) · airframe 43,394 hrs · 28,778 cycles

NR 2 SLAT OUTBOARD EDGE WEB AND RIB ARE CHAFFED. REMOVED AND REPLACED NOSE WEB, REMOVED RIB, FABRICATED NEW RIB FROM 2024O .032 APPROX DIM: 15" X 15 1/2" HEAT TREATED TO T4 CONDITION & INSTALLED NEW RIB AT NR 2 SLAT OB EDGE IAW SRM 51-30-5, SRM 51-30-2, DWG NR 65-17319, & EA 7-5750-143906.

Part: SKIN — GOUGED (BS 460-480) · airframe 43,394 hrs · 28,778 cycles

GOUGES MCD INNER SURROUND SKIN STA 460-480, STR 4L. REMOVED DAMAGED SKIN SECTION FROM BS 460 - BS 505, FABRICATED NEW FWD INNER SKIN & INSTALLED NEW INNER SKIN IAW SRM 51-30-2, SRM 51-30-5, & SRM 53-10-2 FIG 3A.

Part: SEAT TRACK — CORRODED (BS 610-690) · corrosion level 2 · airframe 43,394 hrs · 28,778 cycles

SEAT TRACK CORRODED, STA 610 TO STA 690, RBL25. REMOVED SEAT TRACK SECTION IAW SRM 51-30-2. FABRICATED NEW SEAT TRACK MATERIAL USED BAC 1520-792-7178-T6511 DIMENSIONS: 17FT AND 30 INCHES IAW SRM 53-10-5 FIG 1. INSTALLED NEW SEAT TRACK RBL 25 BS 480 TO BS 690 IAW SRM 51-30-2.

Part: STRINGER — DENTED (BS 970-990 S20L) · airframe 43,394 hrs · 28,778 cycles

STRINGER 20L FLANGE DENTED - BETWEEN STATION 970 - 990. REMOVED DAMAGED SECTION OF STRINGER 20L BS 970 - 990 IAW SRM 53-10-3 FIG 1. FABRICATED STRINGER 20" LONG AND 2 SPLICES 18" LENGTH LONG IAW SRM 53-10-3 FIG 1 REV 103. INSTALLED STRINGER AND SPLICES IAW SRM 53-10-3 FIG 1 REV 103.

Part: BRACKET — DAMAGED (BS 510 S27L) · airframe 43,394 hrs · 28,778 cycles

FWD PIT - STAND OFF BRACKET FOR ELEC LEADS IS DAMAGED AT BS 510, STR 27L. FABRICATED STRINGER REPAIR PARTS & INSTALLED STRINGER REPAIR AT BS 510 STR 27L IAW SRM 53-10-3 FIG 1 DETAIL 2 & SRM 51-10-2.

Part: SEAT TRACK — CORRODED (BS460-500) · corrosion level 2 · airframe 43,394 hrs · 28,778 cycles

CORROSION SEAT TRACK SPLICE MAIN CABIN LBL 25 BS 460-500. REMOVED & REPLACED SEAT TRACK IAW SRM 53-10-5 FIG 1 53-10-2 FIG 1 IAW 51-30-2

Part: VERTICAL BEAM — DAMAGED (BS 1183) · airframe 43,394 hrs · 28,778 cycles

MISSED DRILLED HOLES VERTICAL BEAM LBL 20 AFT CARGO PIT BS 1183. REPAIRED MISDRILLED HOLES AT VERTICAL BEAM IAW E.A. 7-5310-135599. REMOVED PREVIOUS STRAP & DOUBLER IAW SRM 51-30-2, TRIMMED OUT BEAM APT FLANGE (DIM: 33 1/4") & WEB (MISDRILLED AREAS, 8 TOTAL), FABRICATED 8 EA. WEB FILLERS & DOUBLER FOR BULKHEAD WEB AND REPAIR TEE, IB & OB REPAIR ANGLES & FILLERS FOR BEAM IAW EA 7-5310-135599, TREATED, PRIMED AND INSTALLED REPAIR PARTS AT VERTICAL BEAM LBL 20 AFT CARGO PIT BS 1183 IAW SRM 51-10-2, 51-30-2 & EA 7-5310-135599.

Part: FLOORBEAM — CORRODED (BS 950) · corrosion level 2 · airframe 43,394 hrs · 28,778 cycles

CORROSION TOP TEE CAP FLOORBEAM BS 950 LBL 45 - 61 REMOVED DAMAGED UPPER TEE CAP FLOORBEAM BS 950 LBL 63 - RBL 63, FABRICATED NEW FLOORBEAM TEE CAP & INSTALLED NEW CAP IAW DWG NR 65-16338, SRM 51-30-2 & SRM 51-10-2.

Part: FLOORBEAM — CORRODED (BS 720A) · corrosion level 2 · airframe 43,394 hrs · 28,778 cycles

CORROSION TOP "T" CAP FLOORBEAM MAIN CABIN BS 720A LBL 25 - BL 0. CUTOUT DAMAGE AREA AT TOP "T" CAP FLOORBEAM BS 720A LBL 25 TO BL 0 (ON 720A DIM 1.85" X 0.90" LBL 5.5" TO 7.35") IAW SRM 53-10-8, FIG 8, FABRICATED 2 ANGLES FROM 7075O .090 HEAT TREAT TO T6 CONDITION DIM 19.5" X 2.65" & 14.65" X 2.50", SHIM FROM 2024T3 .125" DIM 1.85" X .090 AND INSTALLED REPAIR IAW SRM 53-10-8, FIG SRM 51-10-2 & 51-50-2 REV 103 AND ER 2-37153-801, REV A.

Part: SEAT TRACK — CORRODED (BS 690-740) · corrosion level 2 · airframe 43,394 hrs · 28,778 cycles

CORROSION SEAT TRACK FLANGE & SCALLOP MAIN CABIN LBL 45 BS 690 - BS 740. REMOVED & REPLACED SEAT TRACK SECTION AT LBL 45 BS 740 - BS 690 & FABRICATED NEW SPLICE AT LBL 45 BS 690 IAW SRM 53-10-5 FIG 1. FABRICATED SEAT TRACK FROM BAC 1520-792-71787T6511 DIM: 171 7/8" PER SRM 53-10-5 FIG 1.

Part: SEAT TRACK — CORRODED (BS 440-480) · corrosion level 2 · airframe 43,394 hrs · 28,778 cycles

CORROSION SEAT TRACK FLANGE BL 0 BS 440 - 480 REMOVED DAMAGED SEAT TRACK SECTION FROM BS 480 - 390 BL 0. FABRICATED NEW SEAT TRACK SECTION FROM BAC1520-792T6511, APPROX DIM: 89 1/4". FABRICATED SEAT TRACK SPLICES (2 EACH) FROM BAC 1503-1001227178T6511 APPROX DIM: 12 3/4". FABRICATED SPLICE PLAT FROM 7075T6 .250" APPROX DIM: 8" X 2". INSTALLED NEW SEAT TRACK SECTION AND SPLICES IAW SRM 51-30-2, SRM 53-10-5 FIG 1 AND SRM 51-10-2.

Part: FRAME — DAMAGED (BS 1070 S27R) · airframe 43,394 hrs · 28,778 cycles

.375" FASTENER HOLE IN FRAME FLANGE, STATION 1070 AT STRINGER 27R. CUT OUT DAMAGED UPPER FLANGE OF BS 1070 FRAME AT STRINGER 27R, 1 3/8" X 5" IAW SRM, REV 103, 51-10-1. FABRICATED DOUBLER USING 7075-0, .071" X 11 1/4" X 4 1/4" AND FILLER USING 7075-0, .063" X 1 3/8" X 5" IAW SRM 51-40-3 FIG 1 AND 53-10-2 FIG 5. INSTALLED DOUBLER AND FILLER IAW SRM 51-40-3 FIG 1.

Part: SEAT TRACK — CORRODED (BS 950-1140) · corrosion level 2 · airframe 43,394 hrs · 28,778 cycles

CORROSION SEAT TRACK FLANGE LBL 25 BS 1140 - BS 950 PLUS 10" REMOVED SEAT TRACK LBL 25 BS 950 PLUS 10" TO 1140 IAW B727 SRM 51-30-2, FABRICATED NEW SEAT TRACK LBL 25 BS 950 PLUS 10" TO 1140, IAW B727 53-10-5 FIG 1 AND INSTALLED NEW SEAT TRACK LBL25 BS 950 PLUS 10" TO 1140 IAW B727 SRM 51-30-2. SEAT FAB FROM BAC 1520-7178T6 DIM: 115 1/2".

Part: SEAT TRACK — CORRODED (BS 550-670) · corrosion level 2 · airframe 43,394 hrs · 28,778 cycles

CORROSION SEAT TRACK FLANGE BL 0 BS 550 - BS 670. REMOVED DAMAGED SEAT TRACK SECTION, FABRICATED NEW SEAT TRACK SECTION & INSTALLED SEAT TRACK IAW SRM 51-30-2 AND SRM 53-10-5 FIG 1.

Part: SHEAR TIE — CORRODED (BS 720 S28L/R) · corrosion level 2 · airframe 43,394 hrs · 28,778 cycles

CORROSION ON SHEAR TIE AT BS 720 BETWEEN STRINGERS 28R AND 28L. CUT OUT DAMAGED SHEAR TIE AT BS 720 BETWEEN STRINGER 28R AND 28L 10" X 1 7/8" IAW SRM, REV103, 53-10-4 FIG 13. FABRICATED REPAIR DOUBLER USING 7075-T6, .063" X 11 1/4" X 3 3/8", RADIUS FILLER USING 7075-T6, .063" X 10" X 3/4" PO NO 90010179 AND SHEAR TIE USING 7075-T6, .050" X 10" X 1 7/8" PO NR 90010289 IAW SRM 53-10-2 FIG 3 AND 53-10-4 FIG 13. INSTALLED SHEAR TIE REPAIR IAW B727 SRM 53-10-4 FIG 13 AND 51-30-2.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 43,394 hrs · 28,778 cycles

CORROSION SEAT TRACK FLANGE & SCALLOPS MAIN CABIN RBL 45 BS 420 - 480. REMOVED SEAT TRACK SECTION FROM BS 420 - BS 480 RBL 45. FABRICATED NEW SEAT TRACK SECTION FROM BAC 1520-792-7178T6, APPROX DIM: 60". INSTALLED NEW SEAT TRACK SECTION FROM BS 420 - BS 480 RBL 45 IAW SRM 51-30-2, SRM 53-10-5 FIG 1, SRM 51-30- 5, SRM 51-10-2 AND SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 480-690) · corrosion level 2 · airframe 43,394 hrs · 28,778 cycles

CORROSION SEAT TRACK FLANGE MAIN CABIN LBL 45 BS 480 - 690 REMOVED AND REPLACED SEAT TRACK SECTION AT LBL 45 BS 690 - 480 IAW SRM 53-10-5 FIG 1 DIM: 209 1/2" FROM BAC 1520-792-7178-T6511.

Part: SEAT TRACK — CORRODED (BS 690-720) · corrosion level 2 · airframe 43,394 hrs · 28,778 cycles

CORROSION SEAT TRACK FLANGE AND SCALLOPS MAIN CABIN RBL 45 BS 690 - 720 REMOVED & REPLACED SEAT TRACK RBL 45 BS 690 - 740 APPR0X DIM: 172" IAW SRM 53-10-3 FIG 1, SRM 53-10-02 FIG 7A, & SRM 51-30-2.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 43,394 hrs · 28,778 cycles

CORROSION SEAT TRACK SPLICE MAIN CABIN LBL 45 BS 460 - BS 490. REMOVED SEAT TRACK FROM BS 480 - 390, FABRICATED NEW SEAT TRACK SECTION, CLEANED & EVALUATED SEAT TRACK SPLICE AT BS 490, FOUND NO CORROSION. INSTALLED NEW SEAT TRACK SECTION IAW SRM 53-10-5 FIG 1, SRM 51-10-1, SRM 51-10-6 & SRM 51-30-2.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 43,394 hrs · 28,778 cycles

CORROSION SEAT TRACK FLANGE & INSIDE SCALLOPS LBL 25 BS 850 - 760. REMOVED SEAT TRACK SECTION LBL 25 BS 850 - 760 IAW SRM 51-30-2 AND FABRICATED NEW SEAT TRACK SECTION FROM BAC 1520-841-7178-T6 IAW SRM 51-30-5, SRM 53-10-2 FIG 7 & SRM 51-10-2 AND INSTALLED SEAT TRACK SECTION IAW SRM 51-30-2.

Part: STRINGER — CORRODED (BS 685 S27L) · corrosion level 2 · airframe 43,394 hrs · 28,778 cycles

CORROSION ON STRINGER 27L PRODUCTION SOLICE AT BS 685. REMOVED PRODUCTION SPLICE AT BS680 STRINGER 27L IAW SRM, REV 103, 51-30-2. CUT OUT SECTION OF STRINGER 27L 11 3/4" LONG IAW SRM 53-10-3 FIG 1. FABRICATED STRINGER USING BAC1498-144, 7075-T6 11 3/4" IN LENGTH AND REPAIR SPLICE USING BAC1498-132, 7075-T6, 14" IN LENGTH IAW SRM 53-10-3 FIG 1 AND 53-10-2 FIG 9. INSTALLED STRINGER, REPAIR SPLICE AND NEW PRODCTION SPLICE IAW SRM 53-10-3 FIG 1 AND 51-30-2.

Part: SEAT TRACK — CORRODED (BS 690-740) · corrosion level 2 · airframe 43,394 hrs · 28,778 cycles

CORROSION SEAT TRACK FLANGE MAIN CABIN LBL 25 BS 690-740. REMOVED DAMAGED SEAT TRACK SECTION FROM BS 690 - BS 740 LBL 25, FABRICATED NEW SEAT TRACK SECTION & SPLICES & INSTALLED NEW SEAT TRACK SECTION & SPLICES IAW SRM 51-30-2, SRM 53-10-5 FIG 1, & SRM 51-10-2.

Part: SHEAR TIE — CORRODED (BS 720 S27-28R) · corrosion level 2 · airframe 43,394 hrs · 28,778 cycles

CORROSION ON SHEAR TIE AT BS 720 BETWEEN STRINGERS 28R AND 27R. CUT OUT DAMAGED SECTION OF BS 720 SHEAR TIE BETWEEN STR 28R AND 27R, 6" X 3 1/4" IAW SRM, REV 103, 53-10-4 FIG 12. FABRICATED SHEAR TIE USING 7075-0, .063" X 12" X 7 1/4", FILLER USING 7075-T6, .050" X 5 3/4" X 1", AND (2) FILLERS USING 7075-T6, .063" X 3" X 3/4" AND .063" X 2 3/4" X 3/4" IAW SRM 53-10-4 FIG 12 AND 53-10-2 FIG 3. INSTALLED SHEAR TIE AND REPAIR FILLERS IAW SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 760-850) · corrosion level 2 · airframe 43,394 hrs · 28,778 cycles

CORROSION INSIDE AND AROUND SCALLOPS SEAT TRACK LBL 45 BS 850-760. REMOVED 95" SEAT TRACK SECTION LBL 45 BS 850-760 IAW SRM 51-30-2, FABRICATED NEW SEAT TRACK SECTION FROM BAC 1520-841-7178 T6 DIMS 95" IAW SRM 53-10-2 FIG 7 & 51-30-5 AND INSTALLED NEW SEAT TRACK SECTION IAW SRM 51-30-2, 51-20-2 FIG 21 & 51-10-2 REV 103.

Part: SHEAR TIE — CORRODED (BS 660 S28-29L) · corrosion level 2 · airframe 43,394 hrs · 28,778 cycles

CORROSION ON SHEAR TIE AT BS 660 BETWEEN STRINGERS 29L AND 28L. CUT OUT DAMAGED SHEAR TIE: 7/8" X 9 7/8" ON BS 660 FRAME BETWEEN STRINGER 28L AND 28R IAW SRM, REV 103, 53-10-4 FIG 15. FABRICATED SHEAR TIE REPAIR DOUBLER USING 7075-0, .063" X 11 1/4" X 3 1/4" IAW SRM 53-10-4 FIG 15 AND 53-10-2. INSTALLED REPAIR DOUBLER IAW SRM 51-30-2 AND 53-10-4 FIG 15.

Part: SEAT TRACK — CORRODED (BS 480-690) · corrosion level 2 · airframe 43,394 hrs · 28,778 cycles

CORROSION FLANGE AND SCALLOPS SEAT TRACK MAIN CABIN RBL 45 BS 480-690. REMOVED AND REPLACED SEAT TRACK & SPLICE RBL 45 BS 480 - 690 APPROX DIM: 209.5" IAW SRM 53-10-5 FIG 1, 53-10-02 FIG 7A & 51-30-2.

Part: SKIN — GOUGED (LT WING TE FLAP) · airframe 43,394 hrs · 28,778 cycles

LT INBD FORE FLAP LE IS GOUGED AT WBL 237. CUTOUT DAMAGED AREA DIM: 1 1/8" X 1 5/8" IAW B727 SRM 51-10-1 AND FABRICATED DOUBLER FROM 2024T3 .063 DIM: 5 3/8" X 4" IAW SRM 57-50-4 FIG 1 AND INSTALLED DOUBLER IAW SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 950-1100) · corrosion level 2 · airframe 43,394 hrs · 28,778 cycles

SEAT TRACK CORRODED LBL 45 STATION 950 PLUS 10" TO STATION 1100. REMOVED SEAT TRACK BS 950 PLUS 10" - 1100 LBL 45 IAW SRM 51-30-2. FABRICATED NEW SEAT TRACK FROM BAC 1520-7-92-7178-T6-511, DIMENSION 295 1/2" AND TWO (2 EA) ANGLES FROM BAC 1503-100122-7178-T6-511, DIMENSION 14 3/4" X 2 1/2" AND ONE STRAP 7075T6 .250 IAW SRM 53-10-5 FIG 1 & INSTALLED NEW SEAT TRACK TRACK IAW SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 950C-1010) · corrosion level 2 · airframe 43,394 hrs · 28,778 cycles

SEAT TRACK CORRODED BL0 STATION 950C TO STATION 1010. REMOVED DAMAGED SEAT TRACK SECTION. FABRICATED NEW SECTION USING BAC1520-792 7178-T6511 DIMS 120" AND INSTALLED IAW SRM 53-10-5 AND SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 720B-720E) · airframe 43,394 hrs · 28,778 cycles

SEAT TRACK CORRODED BL0 STATION 720B PLUS 10" TO STATION 720E PLUS 10". REMOVED DAMAGED SEAT TRACK SECTION FROM BS 720 -740 BL 0, FABRICATED NEW SEAT TRACK SECTION DIM: 141 1/2" FROM BAC 1520792-7178T6511& INSTALLED NEW SEAT TRACK SECTION IAW SRM 53-10-2, SRM 51-30-5, & SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 870-950C) · corrosion level 2 · airframe 43,394 hrs · 28,778 cycles

SEAT TRACK CORRODED BL0 STATION 870 TO STATION 950C. REMOVED SEAT TRACK SECTION IAW SRM 51-30-2, FABRICATED NEW SEAT TRACK SECTION FROM BAC 1520792-7178T6511 DIM: 141 3/4" IAW SRM 53-10-1 FIG 3 & 53-102 FIG 7A , INSTALLED NEW SEAT TRACK SECTION IAW SRM 51-30-2 AT BS 870 TO BS 950C BL 0.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 43,394 hrs · 28,778 cycles

EXTERIOR SKIN BULGE WITH PULLING FASTENERS, STR 22L, STA 1166, AT LOWER FWD RADIUS OF LT AFT LAV SERVICE PANEL. REMOVED LAV PAN INTERNAL TRIPLER AT STRINGER 22L, BS 1166 IAW SRM, REV 103, 51-30-2. FABRICATED NEW TRIPLER USING 7075-T6, .071" X 20 1/8" X 20 3/8" IAW DWG 65-25607. INSTALLED TRIPLER IAW DWG 65-54583 AND SRM 51-30- 2.

Part: SKIN — GOUGED (BS 620-640) · airframe 43,394 hrs · 28,778 cycles

NUMEROUS GOUGES MCD INNER SURROUND SKIN STATIONS 620-640, STRINGERS 4L TO 9L. REMOVED MCD INNER SKIN BS 594 - 640, FABRICATED NEW INNER SKIN & INSTALLED NEW SKIN AT MCD SURROUND BS 640 - 594 IAW SRM 53-10-2 FIG 3A, SRM 51-30-2, SRM 51-30-5, SRM 51-10-2.

Part: STRUCTURE — CRACKED (RT WING) · airframe 43,394 hrs · 28,778 cycles

RIGHT INBD MID FLAP INBD ACTUATING MECHANISM PUSH ROD CUTOUT CRACK. CUT OUT DAMAGED AREA OF R/H INBD MIDFLAP T/E CHORD 47 1/2" LONG IAW FED EX B727 SRM REV 103 51-10-1 FABRICATED REPAIR FROM BAC1503-100046 7075 T6 DIM 47 1/2" LONG AND SPLICE FROM BAC1503-100046 7075 T6 DIM 9" LONG IAW B727 SRM 57-50-2 INSTALLED T/E CHORD SECTION AND SPLICE IAW SRM 51-30-2

Part: SUPPORT BRACKET — CRACKED (ZONE 500) · airframe 43,394 hrs · 28,778 cycles

CRACK ANGLE CHORD AT NUMBER 7 SPOILER ACTUATOR SUPPORT BRACKET FALSE SPAR. CUT OUT SECTION OF L/H FALSE SPAR WEB 9 1/2" X 12 1/4" AND LOWER CHORD 20.33" IN LENGTH IAW FED EX B727 DWG NO. SR27-57-038 REV C. FABRICATED CHORD SPLICE ANGLES (2)EA, USING 7075-0, .071" X 12 1/2" LONG AND 15" LONG, STRAP USING 7075-T6, .090" X 11 1/2" X 1 1/2", DOUBLER USING 2024-T3, .050" X 12" X 9", WEB USING 7075-T6, .032" X 12 1/4" X 9 1/2", LOWER CHORD USING BAC1514-1437, 7075-T6511, 20.33" IN LENGTH, AND (2) SHIMS USING 7075-T6, .160" X 2 1/2" X 1" IAW DWG SR27-57-038 REV C. INSTALLED ANGLES, CHORD, STRAP, SHIMS, DOUBLER AND WEB IAW DWG SR27-57-038 REV C.

Part: SKIN — CORRODED (BS 490 S27-28L) · airframe 43,394 hrs · 28,778 cycles

CORROSION EXTERIOR FUSELAGE BS 490 STR 27L-28L. REPAIRED IAW EA 7-5330-135598. REMOVED PREV REPAIR IAW SRM 51-30-2, CUTOUT DAMAGED AREAS 20.5" X 10.5", FABRICATED 2 EA FILLERS, 1 LAP FILLER & TRIPLER, TREATED AND PRIMED AND INSTALLED REPAIR & FUSELAGE BS 490, STR 27L IAW EA 7-5330-135598 & SRM 51-10-2 & SRM 51-30-2.

Part: STRINGER — CORRODED (BS 1008 S28L) · corrosion level 2 · airframe 43,394 hrs · 28,778 cycles

BULGE EXTERIOR FUSELAGE SKIN BS 1008 STRINGER 28L CUT OUT DAMAGED SECTION OF STR 28L AT BS 1008, 11" LONG IAW SRM 53-10 3 FIG 1 AND 51-30-2. FABRICATED STRINGER SECTION. FABRICATED SPLICE IAW B727 SRM 53-10-3 FIG 1. INSTALLED STRINGER AND SPLICE IAW SRM 51-30-2 REV 103.

Part: SKIN — CHAFED (BS 720E S19R) · airframe 43,394 hrs · 28,778 cycles

FUSELAGE SKIN CHAFFED FWD OF BS720E AT STRINGER 19R. CUT OUT DAMAGED SECTION OF SKIN 4 5/16" X 2 5/8" IAW SRM, REV 103, 53-30-3 FIG 5. FABRICATED REPAIR PARTS: DOUBLER AND FILLER IAW SRM 53-30-3 FIG 5. INSTALLED DOUBLER AND FILLER IAW SRM 53-30-3 FIG 5 AND 51-30-2.

Part: STRINGER — CORRODED (BS 490 S28L) · corrosion level 2 · airframe 43,394 hrs · 28,778 cycles

STRINGER 28L CORRODED AT BS 490. CUT OUT SECTION OFSTRINGER 28L AT BS490, 25" IN LENGTH IAW FED EX B727 SRM, REV 103, 53-10-3 FIG 1 DETAIL 2. FABRICATED STRINGER SECTION, CHANNEL , 2 "J" ANGLES, AND 2 FILLERS IAW SRM 53-10-3 FIG 1 DETAIL 2 AND 53-10-2 FIG 3. INSTALLED STRINGER AND REPAIR PARTS IAW SRM 51-30-2.

Part: MODULE — INOPERATIVE (CABIN PRESSURE) · airframe 43,115 hrs · 28,567 cycles

DURING CLIMBOUT, CABIN FAILED TO STABILIZE AT 5200FT. CABIN ALTITUDE FOR CRUISE FLT 340 AT CRUISE FLT (340), CABIN ALT EXCEEDED 10000FT. DESCENT INITIATED AND MANUAL PRESSURIZATION WAS SELECTED AND OUTFLOW VLV WAS FULL CLOSED, CARGO HEAT VLV WAS CLOSED, 2 PACKS WERE OPERATING AND THE CABIN REMAINED UNCONTROLLABLE COULD NOT DECREASE CABIN ALT UNTIL DESCENT BELOW 17000FT. CABIN ALT AND ACFT ALTITUDE EQUALIZED AT 10000FT. DURING PRESSURIZATION TROUBLESHOOTING FOUND RT PACK SWITCH FAULTY. REPLACED ACFT AND PRESSURIZATION ASSY MODULE IAW MM REF 31-00-011-4. DECAY CHK IAW JRH GOOD. PANEL OPS CHK GOOD.

Part: SEAL — FAILED (ACM) · airframe 43,108 hrs · 28,562 cycles

ALTITUDE WAS CLIMBING UNCONTROLLABLE CABIN WITH OUTFLOW VALVE CLOSED/DESCENDED TO FL190 IN ORDER TO MAINTAIN A CABIN ALTITUDE BELOW 100,000 FT. COMPLIED WITH QRH AND RAN PRESSURIZATION ON STBY AND MANUAL WITH NO CHANGE. R & R RUBBER SEAL JUST AFT OF THE ACM, IAW SMP. RESEALED AREA'S AROUND AFT LOWER MAIN CARGO DOOR, IAW SMP. OPS CHECK CABIN PRESSURE SYS IAW JRH CHPT, SECTION 8-47. ALL CHECKS GOOD.

Part: VALVE — MALFUNCTIONED (LT A/C PACK) · airframe 43,066 hrs · 28,533 cycles

ACFT WOULD NOT PRESSURIZE. TROUBLESHOOTING RAN NR 3 ENGINE PRESSURIZED AC PERFORMED CABIN DECAY. CHECK IAW JRH DECAY CHECK GOOD. PERFORMED BLEED SYS CHECK IAW JRH AND SYS CHECKED GOOD. AC PRESSURIZED TO 6 PSID NORMALLY NO FAULTS NOTED. LT FWD PACK VALVE WAS R & R ON ANOTHER WRI 21-50/1932.

Part: LINKAGE — LOOSE (LE FLAP) · airframe 42,172 hrs · 27,838 cycles

NUMBER 4 LE FLAP ON RIGHT SIDE DID NOT RETRACT AFTER TAKEOFF DURING FLAP/SLAT RETRACTION. RAN QRH. EXTENDED NORMALLY AND DID NOT RETRACT SECOND TIME. FOUND LOOSE LINKAGE ON NR 4 LE FLAP SWITCH. SECURED LINKAGE, OPERATED FLAPS AND OPS CHECKED GOOD IAW MM 27-82-000-1. ACFT OK FOR FLIGHT. SWITCH REF. IPC ITEM 085, PART NUMBER 10-60819-18, IPC REF 27-80-00-14. LOOSE LINKAGE TO SWITCH FOUND, SECURED IAW AMM 27-82-000-1, OPS CHECK GOOD.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,944 hrs · 27,669 cycles

FWD CARGO COMPARTMENT, STRINGER 27R CORRODED BETWEEN STA 720A AND 720C REMOVED BODY FAIRINGS NR 3420 AND 3437 IAW SRM 51-30-2, REMOVED PREVIOUS REPAIR IAW SRM 51-30-2. CUT OUT DAMAGE AREA (DIM 47 INCHES LONG ) AND FABRICATED NEW STRINGER FROM BAC1498-145 AND NEW SPLICE FROM BAC1498-131 IAW SRM 53-10-3, FIG 1. TREATED AND PRIMED PARTS IAW SRM 51-10-2. INSTALLED PARTS AND REINSTALLED BODY FAIRINGS IAW SRM 53-10-3 FIG AND 51-30-2. FOR REFERENCE SEE N/R N00861.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,944 hrs · 27,669 cycles

AFT CARGO COMPARTMENT, SHEAR TIE CORRODED AND FASTENERS PULLING THROUGH AT BS 116 BETWEEN STRINGER 30 AND 29R AFT SIDE.

Part: SKIN — DELAMINATED (ZONE 500) · airframe 41,944 hrs · 27,669 cycles

LT OB FORE FLAP WBL 478 ON T/E IS DELAMINATED CUT OUT DELAMINATED AREA 4 1/2 BY 9 INCH ON LT O/B FOREFLAP WBL 478. FABRICATED FILLER 4 1/2 BY 9 INCH AND DOUBLER 6 INCH BY 12 INCH FROM 0.016" 2024-T3 PO NR 9004174 IAW B727 SRM 57-50-2. BONDED FILLER AND DOUBLER, CLEANED, SEALED AND PRIMED IAW B727 SRM 51-40-20.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,944 hrs · 27,669 cycles

INTERNAL FUSELAGE FWD CARGO COMPARTMENT, STRINGER 28R CORRODED AT BS 500. REMOVED INTERCOSTAL AT BS 480-500 STR 28 RT IAW B-727 51-30-2, CUT-OUT DAMAGE STRINGER, (DIM 23 1/2 INCH LONG). FABRICATED STRINGER FILLERS FROM BAC1498-205 PO NR 642842 (DIM 13 INCH LONG AND 10 5/8 INCH LONG) IAW B-727 SRM 53-10-3 FIG 1 AND 53-10-2 FIG 9, CUT-OUT DAMAGED SKIN (DIM 8 INCH BY 3 1/4 INCH) AND FABRICATED SKIN DOUBLER FROM 2024-T3 0.090 INCH PO NR 9006027 (DIM 19 1/4" BY 11") AND REPAIR FILLER FROM 2024-T3 0.080 INCH PO NR 9006377 (DIM. 8" BY 3 1/4") IAW B-727 SRM 53-30-3 FIG 3 AND 53-30-2 FIG 2, INSTALLED REPAIR PARTS AND REINSTALLED INTERCOSTAL IAW B-727 SRM 51-30-2.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,944 hrs · 27,669 cycles

FWD CARGO COMPARTMENT HAS STRINGER 27 RT CORRODED BETWEEN STA 720E AND 720F CUT OUT DAMAGED AREA (DIM 17" LONG) AND FABRICATED NEW FILLER FROM BAC 1498-147, 0.090 PO NR 8150104 (DIMENSION 17 INCH LONG) AND SPLICE FROM BAC-1498-131 7075-T6 PO NR 9006222 (DIMENSION 13 INCHES LONG ) IAW B-727 SRM 53-10-3 FIGURE 1 AND 53-10-2 FIGURE 9. TREATED AND PRIMED PARTS IAW B-727 SRM 51-10-2 AND INSTALLED REPAIR PARTS AT FWD CARGO COMPARTMENT STRINGER 27 RT BETWEEN STA 720E-720F IAW B-727 SRM 51-30-2 AND 53-10-3 FIGURE 1.

Part: SKIN — DENTED (ZONE 100) · airframe 41,944 hrs · 27,669 cycles

LOWER FUSELAGE, SEVERAL DENTS WITH BULGING SKIN BETWEEN STA 1050 AND 1070, BETWEEN STR 28R AND 26R LOWER FUSELAGE SEVERAL DENTS WITH BULGING BTW STA 1015 TO 1070 STR 28R - 26R; CUT OUT 2 EA DAMAGE AREA DIM (12 INCH BY 6 1/2 INCH), (2 1/2 BY 1 1/2) IAW SRM 53-30-3 FIG 3. FAB DOUBLER REPAIR MAT USED 2024T3.071" PO NR 9001282 DIM (24 1/2 INCH BY 17 1/2 INCH) AND 2 EA FILLER MAT USED 2024T3.063" PO NR 9006767 DIM (8" BY 3"), (6 1/2" BY 2") IAW SRM 53-30-3 FIG 3 AND 53-30-2 FIG. REMOVED 2EA INTERNATIONAL AND ANTENNA SUPPORT IAW SRM 51-30-2. TREATED AND PRIMED PARTS IAW SRM 51-10-2, INSTALLED COUNTER SINK WASHER IAW SRM 51-30-8. INSTALLED DOUBLER REPAIR AND PARTS," INTERCOSTAL 2 EA, AND ANTENNA SUPPORT.

Part: BEAM — CRACKED (ZONE 600) · airframe 41,944 hrs · 27,669 cycles

RT WING UPPER TRAILING EDGE "J " BEAM IS CRACKED AT WBL 118, WS 155 - WS 160 REMOVED NR 8 SPOILER FITTING FOR ACCESS IAW B727 SRM 51-30-2. TRIMMED OUT CRACK (DIMENSION 0.280 INCH IN LENGTH ) IAW B727 SRM 51-10-1 AND FEDEX DRAWING SR 27-57-025 REV A. TREATED AND PRIMED AREA IAW FEDEX DRAWING SR 27-57-025 AND 51-10-2 AND REINSTALLED NR 8 SPOILER FITTING AT RT WING UPPER T/E AREA WBL 118 IAW B727 SRM 51-30-2.

Part: SKIN — CRACKED (NR 4 SLAT) · airframe 41,944 hrs · 27,669 cycles

NR 4 SLAT UPPER SURFACE ON AFT HOOK ATTACHMENT SCREW HAS SKIN CRACKED REMOVED HOOK AS REQ IAW B727 SRM 51-10-2. FAB REPAIR PLATE MAT USED 2024T3-.125 PO NR 810563. DIM (5" BY 4") IAW B727 SRM 57-50-3 FIG 10, TREATED AND PRIMED IAW B727 SRM 51-10-2, C/W HFEC IAW B727 NDTM PT 6. 51-00-00 FIG 23. CRACK TERMINATES IN FASTENER HOLES. INSTALLED REPAIR PART IAW B727 SRM 51-30-2. INSTALLED HOOK WITH BOLTS IAW B727 SRM 51-30-2.

Part: STRINGER — CORRODED (BS 735-740 S28L) · corrosion level 2 · airframe 41,944 hrs · 27,669 cycles

FWD CARGO COMPARTMENT, STR 28L HAS BULGING SEAL ON O/B SIDE JUST FWD OF STA 740 EVIDENCE OF CORROSION REMOVED SEALANT AND CLEANED AREA. NO CORROSION NOTED IAW BSOPM 20-30-03. TREATED AND PRIMED AREA IAW B727 SRM 51-10-2. RESEALED AREA IAW FX 727-200 51-31-000-2.

Part: STRINGER — CORRODED (BS 735-740 S27R) · corrosion level 2 · airframe 41,944 hrs · 27,669 cycles

FWD CARGO COMPARTMENT, STR 27R IS CORRODED FWD OF STA 740 REMOVED FASTENERS IAW B-727 SRM 51-30-2, CUT-OUT DAMAGED AREA (DIM 9 1/4 INCH LONG) AND FABRICATED FILLER FROM BAC1498-147 0.090" PO NR 8150104 ( DIM 9 1/4" LONG ) AND STRINGER SPLICE FROM BAC1498-131 7075-T6 PO NR 9006522 (DIM 11 INCH LONG) IAW B-727 SRM 53-10-3 FIG 1 AND 53-10-2 FIGURE 9. TREATED AND PRIMED PARTS IAW B-727 SRM 51-10-2 AND INSTALLED REPAIR PARTS AT FWD CARGO COMPT STR 27 RT FWD OF STA 740 IAW B-727 SRM 53-10-3 FIGURE 1 AND 51-30-2.

Part: SKIN — DENTED (ZONE 100) · airframe 41,944 hrs · 27,669 cycles

RT FUSELGE EXTERNAL 2 EA OLD REPAIRS AT STA 416 BETWEEN STR 21R AND STR 22R HAVE DENTS.

Part: ELECTRICAL SYS — CONTAMINATED · airframe 40,855 hrs · 26,787 cycles

DURING MAIN DECK LOADING EXCESSIVE WATER RAN INTO E/E COMPARTMENT POPPING CABIN AIR FLOW C/B, CABIN SMOKE C/B, CARGO DOOR CONTROL C/B, AND 3 C/B'S ON THE P-18 PANEL MAIN LIGHTS C/B'S. LOWER E/E HAS WATER DRIPPING ON THE WIRE BUNDLE OVERHEAD TOP AND TO LEFT OF E/E DOOR. WATER FOUND LEAKING AROUND RIGID BARRIER BOTH SIDES INTO E/E COMPARTMENT AND FROM L1 DOOR SILL INBBD TO THE COCKPIT DOOR AND R1 DOOR HAS A WATER LEAK ON THE SIDEWALL INTO THE E/E COMPT. SEALANT BMS 5-30B DID NOT CROSS TRYING TO CONTACT LAX FOR HOT WAX GUN. VACUUMED STANDING WATER FROM BOTTOM OF BELLY OF A/C IN FRONT OF GEN CONTROL BULKHEAD.

Part: STRAP — DAMAGED (ZONE 100) · airframe 40,855 hrs · 26,787 cycles

DURING WIRING REPAIR WORK, FOUND STABILIZER STRAP AT RBL 24.75 APPROX STA 312 BROKEN, DISOVERED DURING OTHER WORK. REPAIRED FLOOR STRAP PER SRM 53-10-8,FIG 6 P/N B27-53-071-1 STRAP, REPAIR DOUBLER P/N 65-17594-4.

Part: SKIN — NONE (FUSELAGE) · airframe 39,927 hrs · 26,075 cycles

ACCESS SEC 48 EXTERNAL SKIN BS 1326 - 1342 RT SIDE STR 4 - 7 FOR REPAIR OF VERTICAL FIN SKIN REPAIR. REMOVED SEC 48 SKIN AT BS 1326-1342 AND INSTALLED REPAIR PER FED-EX EA 7-5330-96576.

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 39,927 hrs · 26,075 cycles

VERTICAL FIN SKIN HAS POSSIBLE CRACK LT SIDE STR 10 ABOVE BODY TORQUE BOX BS 1342. REPAIRED CRACK AT BS 1342 STR 10 PER FED EX EA 7-5540-96829.

Part: FASTENER — DAMAGED (RT WING) · airframe 39,927 hrs · 26,075 cycles

RT WING AFT/LOWER INBOARD PANEL HAS ONE SCREW HEAD MISSING (LOG BOOK ENTRY REQUIRED). RT WING AFT LOWER I/B PANEL REPAIRED HOLE, AT #5 FLAP TRACK ATTACHMENT. IAW FED -EX EA 7- 5710-96555

Part: SKIN — DENTED (RUDDER) · airframe 39,927 hrs · 26,075 cycles

WHILE WORKING N01571 FOUND LT SKIN DENT AND GOUGE ON LOWER RUDDER. REPAIRED LOWER RUDDER PER SRM 55-40-3 FIG 1.

Part: SUPPORT FITTING — UNKNOWN (RUDDER) · airframe 39,927 hrs · 26,075 cycles

COMPLY WITH EO 7-5550-7-2302E SECTION 4B - RUDDER CENTER HINGE SUPPORT FITTING REPLACEMENT ON LOWER RUDDER. REPLACED HINGE SUPPORT FITTING PER E.O. 7-5550-7-2302E.

Part: SKIN — MISDRILLED (LT WING) · airframe 39,927 hrs · 26,075 cycles

DOUBLE DRILLED HOLE AT NUT PLATE IN LOWER SKIN OF LEFT WING BULLNOSE 9 INCHES I/B OF NR 3 SLAT O/B SLAT TRACK. *S/D* REPAIRED LOWER SKIN OF LEFT WING BULLNOSE IAW EA 7-5710-91433.

Part: FITTING — GOUGED (WING) · airframe 39,927 hrs · 26,075 cycles

WHILE WORKING N01382 FOUND NUMEROUS NICKS AND GOUGES IN RT 870 TERMINAL FITTING INNER BORE. *S/D* ACCOMPLISHED EA 7-5710-96554.

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 39,927 hrs · 26,075 cycles

VERTICAL FIN SKIN HAS POSSIBLE CRACK RT SIDE STR 10 ABOVE BODY TORQUE BOX BS 1342. REPAIRED RT VERTICAL FIN SKIN PER FED-EX E.A. 7-5540-96829.

Part: SHROUD — CORRODED (FUEL LINE) · airframe 39,927 hrs · 26,075 cycles

BS 1070, WL 205 WHILE WORKING CUSTOMER CARD N00935 FOUND CORROSION ON OUTBOARD SIDE OF FUEL LINE SHROUD BS 1070 RBL 60 WL 205. REPAIRED FUEL LINE SHROUD AT BS 1070 RBL 60 WL 205 IAW FED-EX E.A. 7-2822-96553.

Part: BEAM — CORRODED (MLG) · airframe 39,927 hrs · 26,075 cycles

WHILE WORKING FEDEX WORK CARD S00004 FOUND CORRODED T/E PANEL ATTACH BOLT HOLES IN THE MLG BEAM, 14 EA ON THE AFT SIDE OF THE BEAM AND 12 EA ON THE FWD SIDE. REPAIRED RT MLG BEAM T/E PANEL ATTACH BOLT HOLES IAW FED EX SR27-57-012 REV A.

Part: SKIN — CORRODED (BS 720F-740) · airframe 39,927 hrs · 26,075 cycles

WHILE WORKING CARD N00378 FOUND CORROSION ON SKIN AT BS 720F TO 740 BETWEEN STRINGER 2 LT TO 3 RT. ACCOMPLISHED REPAIR AT B.S. 720F TO 740 BETWEEN STRINGERS 2L TO 3R IAW FED EX EA 7-5330-96543.

Part: BEAM — DAMAGED (VERTICAL STAB) · airframe 39,927 hrs · 26,075 cycles

WHILE WORKING CARD N01209, FOUND VERTICAL FIN UPPER SPLICE BEAM, BUSHING BORE OVERSIZED & GOUGED. REPAIRED VERT. FIN UPPER SPLICE BEAM BUSHING BORE IAW EA 7-5530-96537.

Part: BEAM — DAMAGED (VERTICAL STAB) · airframe 39,927 hrs · 26,075 cycles

WHILE WORKING CARD N01210 (TAIL 5142), FOUND VERTICAL FIN T/E BEAM, UPPER SPICE FITTINGS, 8 EA I/B BUSHINGS WORN. REPAIRED VERTICAL FIN T/E BEAM IAW FED-EX EA 7-5530-96556.

Part: TIE — MISALIGNED (EMPENNAGE) · airframe 39,927 hrs · 26,075 cycles

FOUND THE AFT VERTICAL BOLT HOLES IN THE TENSION TIE AND ATTACH FITTING TO BE MISALIGNED. REPAIRED THE AFT VERT. BOLT HOLES IN THE TENSION TIE AND ATTACH FITTING IAW EA 7- 5530-96550.

Part: WEB — CHAFED (RT ELEVATOR) · airframe 39,927 hrs · 26,075 cycles

RIGHT ELEVATOR NR 1 BALANCE PANEL BAY I/B WEB IS CHAFED. *S/D* REMOVED AND REPLACED WEB PER FED EX EA 7-5510-96545.

Part: PANEL — CRACKED (HORIZONTAL STAB) · airframe 39,927 hrs · 26,075 cycles

PANEL 9220 IS CRACKED. *S/D* REPLACED PANEL PER FED EX EA 7-5510-96548.

Part: STRINGER — CRACKED (WS 629) · airframe 39,927 hrs · 26,075 cycles

LT WING, STA.629.00 THIRD STRINGER FROM REAR SPAR IS CRACKED. *S/D* REPAIRED LT WING, STA 629.00 THIRD STRINGER FROM REAR SPAR PER EA 7-5710-96299.

Part: RIB — CHAFED (VERTICAL STAB) · airframe 39,927 hrs · 26,075 cycles

WHILE WORKING VERTICAL CLOSE FOUND L/E ATTACH RIB AT LEADING EDGE FIN STA 55.8 CHAFED.

Part: REPAIR — UNKNOWN (BS 1323) · airframe 39,927 hrs · 26,075 cycles

EXTERNAL DOUBLER AROUND LT BLOW-OUT PANEL AT BS 1323, BELOW STR 14L, REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EXISTING REPAIR DETERMINED NOT TO BE PER FAA APPROVED DATA AND TO BE A MAJOR REPAIR. REMOVED EXISTING REPAIR AND INSTALLED NEW REPAIR IAW EA 7-5330-96567

Part: SKIN — GOUGED (HORIZONTAL STAB) · airframe 39,927 hrs · 26,075 cycles

LT HORIZONTAL STABILIZER UPPER T/E PANEL BEADED SKIN IS GOUGED AT ELEVATOR BALANCE PANEL BAY 5.

Part: ATTACH FITTING — CORRODED (VERTICAL STAB) · airframe 39,927 hrs · 26,075 cycles

FOUND PITTING IN THE LT FWD VERTICAL BOLT HOLE ON THE VERTICAL FIN TENSION TIE ATTACH FITTING (A/C SIDE).

Part: SKIN — GOUGED (TE FLAPS) · airframe 39,927 hrs · 26,075 cycles

LEFT WING O/B MIDFLAP UPPER SURFACE GOUGED AT I/B EDGE, APPROX 12 INCHES AFT OF THE LEADING EDGE OF FLAP. *S/D* REPAIRED FLAP PER FED EX EA 7-5710-96547.

Part: SKIN — CORRODED (BS 680-700) · airframe 39,927 hrs · 26,075 cycles

WHILE WORKING CARD N00378 FOUND CORROSION ON SKIN AT BS 680 TO BS 700 BETWEEN STR 2R AND 3L. *S/D* COMPLIED WITH FED EX EA 7-5330-91435.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 39,927 hrs · 26,075 cycles

LFEC SHOWS CRACK INDICATIONS AT MCD DOUBLER LOWER FASTNER ROW BS 523, 524, 525 BETWEEN STR 27L AND 28L. COMPLIED WITH FED EX EA 7-5330-95979.

Part: SHEAR WEB — FOM (FUSELAGE) · airframe 39,927 hrs · 26,075 cycles

NO1461 RT SHEAR WEB STA 1130-1140 NEEDS ACCESSED, CUT AND REPAIRED TO ACCOMIDATE 1130 FLOORBEAM UPPER CHORD REPLACEMENT REMOVED & REPLACED RT SHEAR WEB AT BS 1130-1140 IAW SRM 51-40-2 AND SRM 51-30-2.

Part: SHEAR WEB — FOM (FUSELAGE) · airframe 39,927 hrs · 26,075 cycles

NO1460 LT SHEAR WEB STA 1130-1140 NEEDS ACCESSED, CUT AND REPAIRED TO ACCOMIDATE 1130 FLOORBEAM UPPER CHORD REPLACEMENT. REMOVED & REPLACED LT SHEAR WEB BS 1130-1140 IAW 51-40-2 & 51-30-2.

Part: FITTING — CRACKED (NR 6 SPOILER) · airframe 39,927 hrs · 26,075 cycles

NR 6 SPOILER AFT ACTUATOR FITTING ON O/B UPPER FLANGE CRACKED. REMOVED AND REPLACED NR 6 SPOILER AFT ACTUATOR FITTING IAW MM 27-62-081-2 AND SRM 51-30-2.

Part: SKIN — TOOL DAMAGE (BS 347-353) · airframe 39,927 hrs · 26,075 cycles

FOUND STA 347-353 STR 10R DRILL STARTS IN SKIN. DRILL STARTS FOUND OUT OF LIMITS, REPAIRED WITH DOUBLERS PER FED EX EA 7-5330-96779.

Part: SKIN — TOOL DAMAGE (BS 347-353) · airframe 39,927 hrs · 26,075 cycles

FOUND STA 347-353 STR 16R DRILL STARTS ON SKIN. DRILL STARTS REPARIED IAW E.A. 7-5330-96779.

Part: SKIN — TOOL DAMAGE (BS 347-353) · airframe 39,927 hrs · 26,075 cycles

FOUND STA 347-353 STR 8R DRILL STARTS ON SKIN. DRILL STARTS REPAIRED IAW EA 7-5330-96779.

Part: SKIN — TOOL DAMAGE (BS 347-353) · airframe 39,927 hrs · 26,075 cycles

FOUND STA 347-353 STR 14R DRILL STARTS ON SKIN. DRILL STARTS REPAIRED IAW EA 7-5330-96779.

Part: SKIN — TOOL DAMAGE (BS 347-353) · airframe 39,927 hrs · 26,075 cycles

FOUND STA 347-353 STR 4R DRILL STARTS ON SKIN. DRILL STARTS REPAIRED IAW EA 7-5330-96779.

Part: FLOORBEAM — CORRODED (BS 1070) · airframe 39,927 hrs · 26,075 cycles

FOUND CORROSION ON FLOORBEAM LOWER FLANGE BS 1070 LBL 44- RBL 44 WL 201. REPAIRED FLOOR BEAM LWR FLANGE BS 1070 LBL 44 - RBL 44 WL 201 IAW SR27-53-034 REPAIR NR 8, AND SRM 51-30-2.

Part: MOUNT FLANGE — CORRODED (ANTENNA) · airframe 39,927 hrs · 26,075 cycles

FOUND MARKER BEACON ANTENNA MOUNT FLANGE HAS SPOTS OF CORROSION, JUST OTBD OF GROUND SERVICE AIR CONNECTION.

Part: SKIN — TOOL DAMAGE (BS 347-353) · airframe 39,927 hrs · 26,075 cycles

FOUND STA 347-353 STR 7R DRILL STARTS IN SKIN. DRILL STARTS REPAIRED IAW EA 7-5330-96779.

Part: FRAME — CORRODED (BS 720E) · airframe 39,927 hrs · 26,075 cycles

FOUND CORROSION ON FRAME AT BS 720E BETWEEN STRINGER 2 LT TO 2 RT.

Part: FLOORBEAM — CORRODED (BS 1130) · airframe 39,927 hrs · 26,075 cycles

FOUND CORROSION IB FLOORBEAM LOWER FLANGE BS 1130 LBL 44-RBL 44 WL 201. REPAIRED FLOORBEAM LOWER CHORD BS 12130 RBL 44 TO LBL 44 IAW SRM 51-10-2.

Part: FITTING — GOUGED (LT WING) · airframe 39,927 hrs · 26,075 cycles

AFTER REMOVAL OF L/W 870 TERMINAL PIN, DISCOVERED A GOUGE INSIDE THE TERMINAL PIN FITTING BORE, AT APPROXIMATELY THE ONE O'CLOCK POSITION NEXT TO THE TERMINAL PIN RETAINING NUT. REPAIRED L/W TERMINAL PIN FITTING BORE AT 87 PER FED EX EA 7-5310-91432.

Part: STRINGER — CRACKED (VERTICAL FIN) · airframe 39,927 hrs · 26,075 cycles

VERTICAL FIN TUNNEL STR 8RT CRACKED AT RIB 8. REPAIRED STRINGER PER SRM 55-30-4 FIG 1.

Part: REPAIR — UNKNOWN (FUSELAGE) · airframe 39,927 hrs · 26,075 cycles

FUSELAGE FLUSH REPAIR AT BS 1150, BL0, REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIRED SKIN PER SRM 53-30-3.

Part: SKIN — CORRODED (FUSELAGE) · airframe 39,927 hrs · 26,075 cycles

N01499 WHILE PREPPING FOR CLOSE FOUND INTERNAL FUSELAGE SKIN CORRODED AT BS 684 STR 26R. REPAIRED INTERNAL FUSELAGE SKIN AT BS 684 STR 26R IAW SRM 53-30-3.

Part: STRINGER — CRACKED (VERTICAL STAB) · airframe 39,927 hrs · 26,075 cycles

VERTICAL FIN TUNNEL STR 8 RT CRACKED AT RIB 7. REPAIRED VERTICAL FIN TUNNEL STR 8 RT AT RIB 7 IAW SRM 55-30-4 FIG 1.

Part: FLAP TRACK — CORRODED (TE FLAPS) · airframe 39,927 hrs · 26,075 cycles

N0108, CORROSION ON UPPER SURFACE OF NR 6 FLAP TRACK AROUND BOTH AFT MOUNT BOLT HOLES AND CNT OB MOUNT BOLT HOLE. COMING REPLACED NR 6 FLAP TRACK IAW WC27X5708-03

Part: FLOORBEAM — MISREPAIRED (BS 560) · airframe 39,927 hrs · 26,075 cycles

EVALUATED FLOORBEAM REPAIR AT BS 560 RBL 10 FOUND NOT TO BE DONE IAW SRM 53-10-8. REPAIRED FLOORBEAM IAW SRM 53-10-8 FIG 3.

Part: REPAIR — MISINSTALLED (BS 720A) · airframe 39,927 hrs · 26,075 cycles

EXTERNAL DOUBLER AT BS 720A, STR 19L - 21L REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED. REPAIRED DOUBLER PER SRM 53-30-3.

Part: REPAIR — MISINSTALLED (FUSELAGE) · airframe 39,927 hrs · 26,075 cycles

EVALUATED REPAIR AT BS 1050 STR 23R-24R FOUND NOT TO BE IAW SRM 53-30-3. REPLACED DOUBLER PER SRM 53-30-03 FIG 1.

Part: STOP FITTING — GOUGED (ENTRY DOOR) · airframe 39,927 hrs · 26,075 cycles

N00757 FORWARD ENTRY DOOR AFT LOWER STOP PIN FITTING GOUGED. COMPLIED WITH FED EX EA 7-5210-91434.

Part: FLAP TRACK — CORRODED (NR 2) · airframe 39,927 hrs · 26,075 cycles

NR 2 FLAP TRACK HAS CORROSION AT BOLT HOLES. REPLACED NR 2 FLAP TRACK ON CUSTOMER CARD 27X5706-03.

Part: FRAME — DENTED (BS 560) · airframe 39,927 hrs · 26,075 cycles

FWD CARGO BAY FRAME IB FLANGE DENTED AT BS 560 BETWEEN STR 24 LT AND STR 25 LT. REPAIRED FRAME PER SRM 51-40-3.

Part: REPAIR — MISINSTALLED (FLOORBEAM) · airframe 39,927 hrs · 26,075 cycles

REPAIR ON MAIN DECK FLOORBEAM UPPER FLANGE BS 480, LBL 5 TO RBL 24. REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED TO NOT BE IAW SRM 53-10-8. REMOVED AND REPLACED REPAIR IAW SRM 53-10-8 FIG 1.

Part: FLOORBEAM — CORRODED (BS 1010) · airframe 39,927 hrs · 26,075 cycles

CORROSION ON FLOORBEAM LOWER FLANGE BS 1010 BBL0-LBL44 WL 201. CORROSION WAS OUT OF LIMITS REF SRM 53-10-1. REMOVED DAMAGE FROM RBL 5 TO LBL 44. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-10-8.

Part: FRAME — DENTED (BS 680) · airframe 39,927 hrs · 26,075 cycles

FWD CARGO BAY FRAME IB FLANGE DENTED AT BS 680, BETWEEN STR 21RT AND 24RT. REPAIRED FRAME AT BS 680 BETWEEN STR 21R-24R PER SRM 51-40-3.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 39,927 hrs · 26,075 cycles

CHORD DAMAGED AND RUB STRIP MISSING ON LWR EDGE BELOW NR 2 ENGINE BS 1352.

Part: SHEAR TIE — CORRODED (BS 1009) · airframe 39,927 hrs · 26,075 cycles

CORROSION ON AFT CARGO BAY SHEAR TIE BS 1009 WL 136 RBL 2.

Part: CHANNEL — DEFORMED (HORIZONTAL STAB) · airframe 39,927 hrs · 26,075 cycles

RT HORIZONTAL STABILIZER T/E, NR 5 ELEVATOR BALANCE PANEL SUPPORT 'U' CHANNEL IS DEFORMED ON O/B SIDE. REPLACED RT HORIZONTAL STAB TE NR 5 BALANCE PANEL SUPPORT CHANNEL PER SRM 51-30-2.

Part: FRAME — DENTED (BS 500) · airframe 39,927 hrs · 26,075 cycles

FWD CARGO BAY FRAME I/B FLANGE DENTED AT BS 500, BETWEEN STR 23RT AND 24RT. *S/D* REPAIRED FRAME AT BS 500, STR 23R-24R PER SRM 51-40-3.

Part: SHEAR TIE — CORRODED (BS 1009) · airframe 39,927 hrs · 26,075 cycles

CORROSION ON AFT CARGO BAY SHEAR TIE BS 1009 WL 136 LBL 4. *S/D* CUT OUT DAMAGED SECTION OF SHEAR TIE AN AREA 1 X 3 INCH IN AFT CARGO BAY BS 1009 WL 136 LBL 4. FABRICATED NEW REPAIR DOUBLER FROM 7075T6 .080 LOT 655633. INSTALLED NEW REPAIR DOUBLER ALL IAW SRM 51-40-3.

Part: KEELBEAM — CORRODED (BS 980) · airframe 39,927 hrs · 26,075 cycles

REWORK REQUIRED FROM CARD N00363. REPAIR DOUBLER AT BS 980, STR 29R HAS PILLOWING AND CRACKED FASTENER HEADS. SUSPECT CORROSION ON INTERNAL BEAM. PILLOWING SEALANT STILL EXISTS ALONG INTERNAL BEAM. REPAIRED PER FED EX EA 7-5310-96552.

Part: FRAME — DENTED (BS 720) · airframe 39,927 hrs · 26,075 cycles

FOUND FWD CARGO BAY FRAME IB FLANGE DENTED AT BS 720, STR 24RT. REPAIRED FRAME AT B.S. 720 STR 24R PER SRM 51-40-3.

Part: FRAME — DENTED (BS 540) · airframe 39,927 hrs · 26,075 cycles

FWD CARGO BAY FRAME IB FLANGE DENTED AT BS 540, STR 24LT. REPAIRED FRAME AT BS 540 STR 24L PER SRM 51-40-3.

Part: STRINGER CLIP — CUT (BS 620) · airframe 39,927 hrs · 26,075 cycles

FOUND FWD CARGO BAY STR CLIP CUT AT BS 620, STR 25LT. REPLACED STRINGER CLIP PER SRM 51-30-2.

Part: FRAME — DENTED (BS 500) · airframe 39,927 hrs · 26,075 cycles

FWD CARGO BAY FRAME IB FLANGE DENTED AT BS 500, BETWEEN STR 24LT AND STR 25LT. REPAIRED FRAME AT BS 500 STRINGER 24L-25L PER SRM 51-40-3.

Part: KEELBEAM — CORRODED (BS 950C) · airframe 39,927 hrs · 26,075 cycles

FOUND CORROSION ON KEELBEAM BS 950C PLUS 8" STR29 RT. REMOVED CORROSION AND RESTORED TO NORMAL ON KEELBEAM BS 950C 8" IAW DWG SR 27-53-013-REV A.

Part: KEELBEAM — CORRODED (BS 950F-970) · airframe 39,927 hrs · 26,075 cycles

FOUND CORROSION ON KEELBEAM BS 950F-970 STR 29 LT. REMOVED CORROSION AND RESTORED TO NORMAL ON THE KEEL BEAM BS 950F-970 STR 29 LT IAW DWG #SR27-53-013-REV A.

Part: FLOORBEAM — TOOL DAMAGE (BS 520) · airframe 39,927 hrs · 26,075 cycles

MECHANICAL DAMAGE (DRILL START) TO FLOORBEAM BS 520 RBL 10.5 WL 208. REPAIRED FLOORBEAM PER SRM 53-10-8.

Part: STRINGER CLIP — GOUGED (BS 540) · airframe 39,927 hrs · 26,075 cycles

FWD CARGO BAY STR CLIP GOUGED AT BS 540, STR 24LT. REPLACED STRINGER CLIP PER SRM 51-30-2.

Part: SKIN — DAMAGED (BS 1184) · airframe 39,927 hrs · 26,075 cycles

BS 1183 SECTION 48 RIGHT SIDE OUTER SKIN CREASED AT BS 1184 NEXT TO THE TAIL SKID. REMOVED AND REPLACED SKIN PANEL IAW SRM 51-30-2.

Part: FRAME — DENTED (BS 520) · airframe 39,927 hrs · 26,075 cycles

FWD CARGO BAY FRAME IB FLANGE DENTED AT BS 520, BETWEEN STR 24LT AND STR 25LT. REPAIRED FRAME PER SRM 51-40-3.

Part: SEAT TRACK — CORRODED (BS 640-660) · corrosion level 2 · airframe 39,927 hrs · 26,075 cycles

FOUND CORROSION C53-224-01, STA 640 - 660 BL 0 WL 208 CORROSION ON SEAT TRACK. REPLACED SEAT TRACK PER SRM 53-10-5.

Part: SKIN — GOUGED (FUSELAGE) · airframe 39,927 hrs · 26,075 cycles

NR 4 JACKSCREW FAIRING FUSELAGE GUIDE HOOK FITTING, FUSELAGE SKIN IS GOUGED 1 INCH BELOW. REPAIRED FUSELAGE SKIN PER SR 27-53-140A.

Part: KEELBEAM — CORRODED (BS 950D) · airframe 39,927 hrs · 26,075 cycles

FOUND CORROSION ON KEELBEAM REPAIR STRAP BS 950D PLUS 5" STR 29 LT. REMOVED AND REPLACED REPAIR STRAP PER DWG SR27-53-023, REV A.

Part: FRAME — DAMAGED (BS 720E) · airframe 39,927 hrs · 26,075 cycles

FOUND STA 720E STR 7R DOUBLE HOLE IN FRAME WEB. REPAIRED FRAME AT BS 720E, STR 7R PER SRM 51-40-3 FIG 1.

Part: STRINGER CLIP — BENT (BS 950F) · airframe 39,927 hrs · 26,075 cycles

STRINGER CLIP, IN MAIN CABIN, IS BENT AND HAS THREE OPEN HOLES AT STA 950F STR 7R. *S/D* REMOVED AND REPLACED STR CLIP AT BS 950F STR 7R IAW SRM 51-30-2.

Part: FLOORBEAM — CORRODED (BS 950D) · airframe 39,927 hrs · 26,075 cycles

FOUND CORROSION C53-111-01 (3) ON FLOORBEAM LOWER FLANGE BS 950D BBL0-LBL44 WL 201. REPAIRED FLOORBEAM LOWER FLANGE BS 950D, BL 0 LBL 44, WL 201 PER SRM 53-10-8, 51-10- 2.

Part: SEAT TRACK — CORRODED (BS 620-640) · corrosion level 2 · airframe 39,927 hrs · 26,075 cycles

FOUND CORROSION, STA 620 - 640 BL 0 WL 208 CORROSION ON SEAT TRACK. STRINGER TO BE REPLACED ON CUST ID N00436

Part: FLOORBEAM — CORRODED (BS 1130) · airframe 39,927 hrs · 26,075 cycles

FOUND FLOORBEAM UPPER CHORD CORRODED, BS 1130 , RBL 50, WL 208. REPAIRED FLOORBEAM UPPER CHORD PER FEDEX EA 7-5310-96828A.

Part: SEAT TRACK — CORRODED (BS 570) · airframe 39,927 hrs · 26,075 cycles

FOUND CORROSION C53-224-01, STA 570 RBL 1 WL 208 CORROSION ON SEAT TRACK. SEAT TRACK TO BE REPLACED ON CUST ID N00436.

Part: KEELBEAM — CORRODED (BS 976) · airframe 39,927 hrs · 26,075 cycles

FOUND CORROSION ON KEELBEAM REPAIR STRAP BS 976 STR29 LT. REPLACED KEEL BEAM REPAIR STRAP PER SR DRAWING 27-53-023A.

Part: FLOORBEAM — DENTED (BS 587) · airframe 39,927 hrs · 26,075 cycles

FOUND CARGO FLOORBEAM DENTED AT BS 587 LBL 8 WL 156. REMOVED AND FABRICATED CARGO FLOORBEAM AT BS 565-610, LBL 8, W/L 156 USING BAC1517-1507 PER SRM 51-40-3 AND INSTALLED PER SRM 51-30-2.

Part: FLOOR SUPPORT — CORRODED (BS 304) · airframe 39,927 hrs · 26,075 cycles

N00770 CORROSION (C53-221-01) BS 304, WL 208, LBL 12 TO 50 HOZ FLOOR SUPPORT UPPER FLANGE. REPAIRED FLOOR SUPPORT IAW SRM 51-30-2.

Part: FLOOR SUPPORT — CORRODED (BS 297-304) · airframe 39,927 hrs · 26,075 cycles

CORROSION BS 297-304, WL 208, LBL 12-14. UPPER FLANGE OF FLOOR SUPPORT. REMOVED AND REPLACED FLOOR SUPPORT BS 294-BS312 IAW SRM 51-30-2, SRM 51-10-2.

Part: FLOORBEAM — GOUGED (FUSELAGE) · airframe 39,927 hrs · 26,075 cycles

CORROSION BS 304, WL 280, LBL 14 GOUGE ON TOP FLANGE, FLOORBEAM. REMOVED AND REPLACED FLOORBEAM IAW SRM 51-30-2 AND SRM 51-10-2.

Part: STRAP — CORRODED (TENSION STRAP) · airframe 39,927 hrs · 26,075 cycles

CORROSION ON TENSION STRAP BS 1070 RBL 45 WL 201. REPAIRED TENSION STRAP IAW SRM 53-10-8 FIG 6.

Part: CONNECTOR — LOOSE (TE FLAPS) · airframe 39,732 hrs · 25,915 cycles

ON DEPARTURE GOING FROM FLAPS 5 TO 2 THE INBOARD FLAP INDICATOR SHOWED FLAPS REMAINED AT 5. RAN QRH WITH NO CHANGE. AIRCRAFT HAD NO ADVERSE FLIGHT FEEL. RIGHT I/B FLAP POSITION TRANSMITTER CONNECTOR FOUND LOOSE. RESECURED AND SAFETIED IAW SMP. CYCLED FLAPS SEVERAL TIMES AND INDICATIONS WERE NORMAL. REF: AMM 27-52-000-0.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 39,598 hrs · 25,809 cycles

APPROX 1 00 INTO THE FLT APPROX 2000' AGL ON FINAL APPROACH, THE AFT MOST LIGHT IN THE MAIN CARGO SMOKE ILLUMINATED WITH CORRESPONDING FIRE BELL AND LIGHT INTERMITTENTLY SOUNDED AND LIT RAN QRH FOR MAIN CARGO SMOKE AS WELL AS FIRE. NO SMOKE OR FUMES IN COCKPIT, NO HIGH ENERGY STOP, TAXIED CLEAR OF RUNWAY. EVACUATED A/C USING CREW ENTRY SLIDE PULLED CVR FDR. UPON ENTRY ON ACFT THE SMOKE DETECTOR NR 6 WAS ILLUMINATING WITH CORRESPONDING BELL. DISCONNECTED NR 6 SMOKE DETECTOR C/P; INDICATION EXTINGUISHED AND BELL SILENCED. SUSPECT BAD DETECTOR. REMOVED AND REPLACED NR 6 SMOKE DETECTOR OPS CHECKED NORMAL REF AMM 26-16-011-4 & 26-16-00-5.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 39,266 hrs · 25,607 cycles

TOTALLY LOST SYS A-HYDRAULIC FLUID WHEN RAISING GEAR HANDLE ON DEPARTURE. SYSTEM A-HYDRAULIC PUMPS RAN W/O FLUID. FLUID SHUTOFF SWITCHES OFF FOR APPROX 40 MIN. HYDRAULIC LINE REPAIR AT RIGHT WHEEL WELL FAILED.

Part: PUMP — MALFUNCTIONED (HYD SYSTEM) · airframe 39,266 hrs · 25,607 cycles

TOTALLY LOST SYS A HYDRAULIC FLUID WHEN RAISING GEAR HANDLE ON DEPARTURE. SYSTEM A HYDRAULIC PUMPS RAN W/O FLUID. FLUID SHUTOFF SWITCHES OFF FOR APPROX 40 MIN HYDRAULIC LINE REPAIR AT RIGHT WHEEL WELL FAILED. MPN 65-17840-487 REPLACED NR 1 ENGINE HYDRAULIC PUMP IAW 727 AMM 29-11-033-4, AND REPLACED NR 1 AND NR 2 ENGINE CASE DRAIN FILTERS IAW 727 AMM 29-11-041-2. REMOVED AND REPLACED NR 2 A SYSTEM HYDRAULIC PUMP PER 29-11-033-4. FLUSH SYSTEM PER STEP 7 MM 29-11-000-2. RAN NR 1 AND NR2 ENG PER JRH TO BLEED HYD SYSTEM. SERVICED HYD SYS TO FULL PER 12-12-000-2. SYS OPS AND LEAK CHECKS, NO DEFECTS NOTED. OK FOR SERVICE.

Part: WARNING LIGHT — ILLUMINATED (NR 3 STRUT) · airframe 38,521 hrs · 25,061 cycles

NR 3 STRUT OVERHEAT LIGHT ILLUMINATED APPROX 2 MIN AFTER T/O AT 2000 AGL, QUIET EPR PWR NR 3 ENG PWR PULLED TO IDLE AND OUR HEAT LIGHT WENT OUT APPROX 1 1/2 MIN AFTER POWER PLACED AT IDLE. NORM LANDING WITH NR 3 ENG AT IDLE POWER. A/C CALLED IN EMERGENCY, AND MADE NORMAL LANDING.

Part: CHANNEL — CORRODED (LT MLG WW) · corrosion level 2 · airframe 37,556 hrs · 24,302 cycles

CORROSION LT WHEEL WELL BS 927-932 LBL 65 WL 188 STR 18A SHELF. REMOVED AND REPLACE SILL CHANNEL BS 870-936, WL 188, LBL 65 AT STR 18A PER SRM 51- 30-2, 51-30-5.

Part: TRANSMITTER — READS HIGH (NR 2 ENGINE) · airframe 37,524 hrs · 24,276 cycles

NR 2 OIL PRESSURE AT 54 PSI TUS RWY 29R WIND 280/11 25' C WITH STANDARD POWER SET. OIL PRESSURE 5 PSI HIGHER THAN NR 3 AND 10 PSI HIGHER THAN NR 1 ENTIRE FLIGHT. REPLACED NR 2 PRESSURE TRANSMITTER PER M/M 79-33-001-4, NO HELP. ADJUSTED NR 2 OIL PRESSURE RELIEF VALVE PER P/W JT8D M/M 72-61-00. 32 OIL PRESSURE READS 44 PSI AT IDLE. NO LEAKS NOTED, ENG NR 2 COWLINGS CLOSED.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 37,144 hrs · 23,954 cycles

ON TAKEOFF, GEAR RETRACTED NORMALLY, ALL LIGHTS OUT. WHEN GEAR HANDLE MOVED TO OFF, RED DOORS LIGHT ILLUMINATED, NO INDICATION ON S/O PANEL. LIGHT WENT OUT WHEN HANDLE MOVED TO UP. REPEAT, GAVE SAME INDICATIONS. THIRD ATTEMPT, GEAR HANDLE OFF, ALL LIGHTS OUT.

Part: RELIEF VALVE — OUT OF ADJUST (NR 2 ENGINE) · airframe 36,832 hrs · 23,712 cycles

NR 2 OIL PRESSURE READ 60 PSI DURING INITIAL CLIMBOUT. AFTER REACHING 5K NR 2 THROTTLE PULLED TO IDLE IAW RED TAB PROCEDURE. OIL PRESSURE DROPPED TO 58 PSI INITIALLY THEN SLOWLY DROPPED INTO GREEN BAND APPROX 52 PSI AT IDLE AND REMAINED THERE DURING APPROACH INTO MEM. ADJUSTED OIL PRESS RELIEF VALVE AND BROUGHT OIL PRESSURE IN LIMITS. RAN ENGINE AT HIGH POWER SETTING OIL PRESSURE WENT TO APPROX 48-49 PSI, 42 PSI AT IDLE. ALSO FOUND OIL TANK OVER SERVICED. SERVICED TO PROPER LEVEL PER SMP REF PW ENGINE MANUAL 72-61-6.

Part: ENGINE — LEAKING (NR 3 ENGINE)

NR 3 ENG DURING CLIMBOUT, LOW OIL PRESS/FILTER BYPASS LIGHT ILLUM. FOLLOWED RED TAB THRU ENG SHUTDOWN. PREVIOUS WRITE-UP ON NR 3 OIL PRESS. *S/D* REMOVED AND REPLACED NR 3 ENG PER WORK CARD 70T0001-03.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 35,560 hrs · 22,707 cycles

DURING ROUTINE INSP, TIE CLIP AT BS 660, STR 3L FOUND CRACKED. REMOVED AND REPLACED PER IAW BAC 727 SRM 51-30-2.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,560 hrs · 22,707 cycles

DURING ROUTINE INSP, MAIN CABIN FLOOR TRACK AT LBL 24 FOUND CORRODED FROM BS 372 - 384. REMOVED, REPLACED AND FAB PER IAW BAC 727 SRM 53-10-1, 53-10-5.

Part: SEAT TRACK — CORRODED (FUSLEAGE) · airframe 35,560 hrs · 22,707 cycles

DURING ROUTINE INSP, NR 6 MAIN CABIN SEAT TRACK FOUND CORRODED FROM BS 880 - 910. REMOVED, REPLACED AND FAB PER IAW BAC 727 SRM 51-20-1, 51-30-2.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 35,560 hrs · 22,707 cycles

DURING ROUTINE INSP, TIE CLIP BS 660, STR 3R FOUND CRACKED. REMOVED AND REPLACED PER IAW BAC 727 SRM 51-30-2.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 35,560 hrs · 22,707 cycles

DURING ROUTINE INSP, BS 560 CABIN FLOORBEAM FOUND CORRODED BETWEEN NR 4 AND NR 5 SEAT TRACKS. REMOVED, REPLACED AND FAB PER IAW BAC 727 SRM 53-10-8.

Part: SMOKE WARNING — ILLUMINATED (CARGO BAY)

AFT CARGO SMOKE LIGHT CAME ON DURING CLIMBOUT. REMOVED AND REPLACED AFT NR 1 SMOKE DETECTION UNIT PER FEDEX MM 26-17-011-2. SYS TEST GOOD.

Part: SMOKE DETECTOR — INOPERATIVE (E & E COMPT)

NR 4 POS SMOKE DETECTOR LIGHT ILLUM WITH AN ASSOCIATED FIRE BELL. REMOVED AND REPLACED COCKPIT VOICE RECORDER FOR BENCH READ-OUT PER MM 23-70-012-4, OPS CK GOOD. REMOVED AND REPLACED NR 4 SMOKE DETECTOR PER MM 26-16-11.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO COMPT)

CREW REPORTED NR 3 CARGO SMOKE DETECTOR LIGHT ON. MADE A TURN AROUND AND LANDED WITH NO INCIDENT. *S/D* CHANGED NR 3 SMOKE DETECTOR, MAIN CARGO SMOKE PANE AS PRECAUTION. REMOVED AND REPLACED SMOKE DETECTOR MODULE FOR PRECAUTION. CK GOOD PER MM 21-22-00.

Part: ANTI-ICE VALVE — LEAKING (NR 1 ENGINE)

ENGINE 1 STRUT OVERHEAT LIGHT CAME ON DURING CLIMBOUT. FOLLOWED THE RED TAB PROCEDURES AND LIGHT EXTINGUISHED. REMOVED AND REPLACED NR 1 ENGINE ANTI-ICE VALVE GASKET ON TOP SIDE OF VALVE. LEAK CHECK GOOD. REMOVED AND REPLACED NR 1 ENGINE STRUT OVERHEAT SENSE LINE PER MAINTENANCE MANUAL 26-14-1. GROUND RUN OPERATIONAL CHECK GOOD. RAN AIRCRAFT AT TAKEOFF POWER FOR 5 MINUTES NO DEFECTS NOTED.

Part: FIRE LOOP — LEAKS (NR 1 ENGINE)

ENGINE 1 STRUT OVERHEAT LIGHT CAME ON DURING CLIMBOUT. FOLLOWED THE RED TAB PROCEDURES AND LIGHT EXTINGUISHED. FOUND FIRE LOOP NEAR TO AIRFRAME IN TWO PLACES UNDER 5401 PANEL. REARRANGED LOOP. RAN ENGINE TO CHECK FOR AIR LEAKS. FOUND NO AIR LEAKS. CLOSED AND SECURED ALL OPEN PANELS.

Part: CLAMP — LOOSE (NR 1 ENGINE)

NR 1 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED ON CLIMBOUT. POWER ON NR 1 ENGINE WAS REDUCED AND LIGHT WENT OUT AT APPROXIMATELY 80 PERCENT AND REMAINED OUT. REPEAT WRITE-UP. REMOVED STUB WING PANELS AND INSPECTED PLUMBING. FOUND ONE CLAMP SLIGHTLY LOOSE. RETORQUED CLAMP AND REINSTALLED PANELS.

Part: DUCT — FAILED (NR 1 PYLON)

97-0255 - DURING TAKEOFF WITH CLIMB POWER SET NR 1 STRUT OVERHEAT LIGHT CAME ON. PULLED THRUST ON NR 1 BACK TO 80 PERCENT N1, NR 1 BLEED OPEN LEFT PACK ON LIGHT GOES OUT. FOUND 8TH STAGE DUCT LEAKING AT FLANGE WELD. REPLACED DUCT JUST OUT BOARD OF PYLON ON THE ENGINE. LEAK CHECKED AT IDLE, LEAK CHECK NORMAL. NEEDS HIGH POWER RUN.

Part: POSITION SWITCH — FAILED (NR 1 LE FLAP)

NUMBER 1 LEADING EDGE FLAP POSITION INDICATOR AND LEADING EDGE FLAPS ANNUNCIATOR LIGHT WOULD NOT EXTINGUISH DURING FLAP RETRACTION. RED TABS PROCEDURES FOLLOWED BUT DID NOT CORRECT PROBLEM. REMOVED AND REPLACED NR 1 LEADING EDGE FLAP POSITION SWITCH PER MAINTENANCE MANUAL 27-82-1, OPERATIONAL TEST NORMAL.

Part: WINDSHIELD — CRACKED (LT COCKPIT)

AT FLIGHT LEVEL 330, CAPTAIN'S OUTER WINDSHIELD L1 CRACKED ABRUPTLY. FOLLOWED RED TAB PROCEDURES, DESCENDED TO FLIGHT LEVEL 240 AND REDUCED CABIN PRESSURE. REMOVED AND REPLACED L1 WINDSHIELD PER MAINTENANCE MANUAL 56-11-11. ALSO, REMOVED AND REPLACED HEAT CONTROLLER. REINSTALLED ALL MOLDING AND OK FOR SERVICE.

Part: CONNECTOR — DIRTY (NR 2 LE FLAP)

AFTER TAKEOFF AND CLEAR UP, SHORTLY THEREAFTER THE AMBER LEADING EDGE FLAPS LIGHT CAME ON. RAN CHECKLIST, NO HELP. THE NR 2 LEADING EDGE FLAP WAS AMBER ON SECOND OFFICER'S POSITION INDICATOR. RETURNED FOR LANDING. CLEANED CANNON PLUG ON THE NR 2 LEADING EDGE FLAP POSITION INDICATING SWITCH. SYSTEM TESTED NORMALLY. ALL DONE PER MAINTENANCE CONTROL AND MAINTENANCE MANUAL 27-82-0 PAGE 101.

Part: STRINGER — CORRODED (BS 690-701)

CORROSION (C53-111-01-2), ON STRINGER 28R FROM BS 690 TO 701 ON O/B SIDE OF U-CHANNEL. THE CORROSION WAS FOUND WHILE WORKING CUSTOMER CARD NRO0235. CORROSION WAS FOUND OUT OF LIMITS PER FEDEX SRM 53-10-1. CUT OUT DAMAGED STR 28R BS 680 TO 720, BACK DRILLED NEW STR, TREATED METAL AND INSTALLED.

Part: SKIN — CRACKED (BS 760)

HFEC INSPECTION OF 6 HOLES COMMON TO BS 760 RBL 70.5 WL 208, SHOWS CRACK INDICATION IN THE UPPER FWD HOLE AND THE UPPER OUTER HOLE. THE REMAINING HOLES SHOW TINY CORROSION INDICATIONS. REPAIRED DRILL START PER EA 7-5710-26288 AND REPAIR CARD EA 7-5710-26747.

Part: CLIP — CRACKED (BS 680)

STR CLIP IS CRACKED BS 680 STR 5L. REPLACED STR CLIP AND ACCOMPLISHED STR REPAIR, BS 680 STR 6L IAW FEDEX EA NR 7-5310-26289.

Part: CLIP — CRACKED (BS 660)

STR CLIP IS CRACKED BS 660, STR 9L. REMOVED CRACKED CLIP, BACK DRILLED NEW CLIP AND INSTALLED FASTENERS AT BS 660, STR 9L. CORRECTION ON A/C NR.

Part: INTERCOSTAL — CORRODED (BS 950-970)

CORROSION (C53-111-01-3), IN AFT CARGO BAY ON INTERCOSTAL BETWEEN BS 950F AND 970 LBL 16 WL 140. FABRICATED AND INSTALLED INTERCOSTAL BETWEEN BS 950F TO 970 LBL 16 WL 140 IAW FEDEX SRM 51-20-1, 51-30-2 AND 53-10-2.

Part: DOOR SKIN — CRACKED (GALLEY DOOR)

FORWARD GALLEY DOOR OUTER SKIN HAS CRACK ON THE UPPER HINGE CUT-OUT. REMOVED DAMAGE AND INSTALLED REPAIR DOUBLER ON FORWARD GALLEY DOOR OUTER SKIN UPPER CUT-OUT PER FEDEX SRM 52-00-3.

Part: G BEAM — CORRODED (BS 264-269)

WHILE WORKING NR0623, FOUND CORROSION ON G-BEAM BS 264-269, WL 208, BL 0 - LBL 8. FOUND CORROSION OUT OF LIMITS PER SRM 53-10-01, REMOVED AND REPLACED G-BEAM, REF FEDEX DWG 65-17588.

Part: FRAME — DENTED (BS 580)

FORWARD BAY FRAME DENTED AT BS 580, BETWEEN STR 25 - STR 22 LT. DENT FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS AND INSTALLED PER FEDEX SRM 53-10-1 AND SRM 53-10-4.

Part: STRINGER — DAMAGED (BS 753-756)

MECHANICAL DAMAGE ON STR 7L AT BS 753 TO 756. REPAIRED STR 7L AT 753 TO 756 PER FEDEX SRM 53-10-3.

Part: WEB — CRACKED (WS 70.5-80.5)

CRACKED WEB AND SUPPORT ANGLES BETWEEN WING STA 70.5 AND 80.5 IN LEFT WING PIE SECTION. REMOVED LEFT WING PIE SECTION, CRACKED WEB AND SUPPORT ANGLES BETWEEN WING STA 70.5 AND 80.5. FABRICATED NEW WEB, INSTALLED NEW WEB AND ANGLES AND REINSTALLED LEFT WING PER PIE SECTION.

Part: FLOORBEAM — CORROSION (BS 480)

WHILE WORKING NR0651, FOUND CORROSION (C53-224-01) UNDER C-TRACK BS 480 WL 208 RBL 45. REMOVED CORROSION ON FLOORBEAM BS 480 WL 208 RBL 45. CORROSION WAS FOUND TO BE OUT LIMITS PER SRM 53-10-1, AREA 1 INCH BY 1 INCH BY .004 INCH, ORIGINAL THICKNESS .180. REPAIRED FLOORBEAM PER FEDEX SA 7-5310-26726.

Part: CLIP — CRACKED (BS 660)

STR CLIP IS CRACKED BS 660, STR 4L. REMOVED CRACKED STR CLIP, BACK DRILLED NEW STR CLIP, AND INSTALLED FASTENER AT BS 660, STA 4L.

Part: FRAME — CRACKED (BS 1090)

FRAME CRACKED TOP FLANGE FOUND IN AFT CARGO BAY AT BS 1090, STR 27L. REPAIRED CRACK IN FRAME BS 1090, STR 27L PER FRI 111595TC1 AND FEDEX SRM 53-10-1 FIG 1 DETAIL IV.

Part: CLIP — CRACKED (BS 950)

CRACKED STR CLIP BS 950C, STR 7R. REPLACED STR CLIP AT BS 950C, STR 7R.

Part: FRAME — DENTED (BS 980)

IN AFT CARGO BAY, FRAME IS DENTED AT STA 980, STR 23L. DENTED FRAME WAS OUT OF LIMITS, CUT OUT DAMAGE, FABRICATED REPAIR DOUBLER AND INSTALLED PER FEDEX SRM 51-40-3, FRAME WAS OUT OF LIMITS PER FEDEX SRM 53-10-1.

Part: SHEAR TIE — CORROSION (BS 700)

FWD BAY, CORROSION (C53-111-01-2) ON SHEAR TIE AT BS 700 BETWEEN STR 28 AND 27R, AFT OF FRAME FOUND WHILE WORKING NR0413. CORROSION ON SHEAR TIE AT BS 700 BETWEEN STR 28 AND 27R WAS FOUND TO BE OUT OF LIMITS PER FEDEX SRM 53-10-1. REMOVED AND REPLACED SHEAR TIE ON AFT SIDE OF FRAME.

Part: FRAME — DENTED (BS 970)

FRAME DENTED IN AFT CARGO BAY AT STA 970, STR 23L. REPAIRED DENTED FRAME IN AFT CARGO BAY AT STA 970, STR 23L. ALL WORK DONE PER FEDEX SRM 51040-3.

Part: DOUBLER — DENTED (BS 985)

DENT ON WEB BS 985, BL ZERO, WL 205. ACCOMPLISHED REPAIR ON WEB BS 985, BL ZERO, WL 205, IAW FEDEX SRM 51-40-2.

Part: STRINGER — DAMAGED (BS 600)

WHILE WORKING NR 0137, FOUND DAMAGED STRINGER 24L AT BS 600.

Part: FRAME — DENTED (BS 600)

FWD BAY, FRAME DENTED AT BS 600 BETWEEN STR 22 TO 25L. REPAIRED DENTED FRAME IN FWD BAY AT BS 600 BETWEEN STR 22 TO 25L IAW FEDEX SRM 51-40-3.

Part: FLOORBEAM — DAMAGED (BS 600)

MECHANICAL DAMAGE TO FLOORBEAM LOWER SURFACE OF UPPER FLANGE BS 600 RBL 11 WL 207. THE DAMAGE WAS FOUND TO BE OUT OF LIMITS. REPAIRED FLOORBEAM AT BS 600 RBL 11 WL 207 PER FEDEX SRM 53-10-1 AND 53-10-8.

Part: CLIP — CRACKED (BS 660)

STR CLIP IS CRACKED BS 660 STR 15L. REPLACED OLD STR CLIP AT BS 660 STR 15L WITH NEW STR CLIP.

Part: FRAME — DENTED (BS 500)

FWD BAY FRAME DENTED AT BS 500 BETWEEN STR 23 TO 22L AND DENT FOUND TO BE OUT OF LIMITS. REPAIRED DENTED FRAME AT BS 500 BETWEEN STR 23 TO 22L PER FEDEX SRM 51-40-3 AND 53-10-1.

Part: WEB — CRACKED (WS 70.5-80.5)

CRACKED WEB AND SUPPORT ANGLES BETWEEN WING STA 70.5 AND 80.5 IN L/W PIE SECTION.

Part: FRAME — DENTED (BS 500)

FRAME DENTED AT BS 500 BETWEEN STR 24 TO 25R AND DENT WAS FOUND TO BE OUT OF LIMITS. REMOVED DAMAGE AREA FROM FRAME, FABRICATED, TREATED AND INSTALLED DOUBLER PER FEDEX SRM 53-10-1 AND 51-40-3.

Part: CLIP — CRACKED (BS 680)

STR CLIP IS CRACKED BS 680 STR 2L. REMOVED STR CLIP AT BS 680 STR 2L AND REPLACEMENT WITH NEW STR CLIP AT ABOVE AREA.

Part: FRAME — DENTED (BS 600)

FWD BAY, FRAME DENTED AT BS 600 BETWEEN STR 22 AND 25L.

Part: CLIP — CRACKED (BS 680)

STR CLIP IS CRACKED BS 680 STR 3L. REMOVED STR CLIP AT BS 680 STR 3L AND REPLACED WITH NEW STR CLIP AT ABOVE AREA.

Part: CLIP — CRACKED (BS 660)

STR CLIP IS CRACKED BS 660 STR 8L. REMOVED CRACKED STR CLIP AND REPLACED WITH NEW STR CLIP AT BS 660 STR 8L.

Part: FRAME — DENTED (BS 700)

FWD CARGO BAY BS 700 BETWEEN STR 22 TO 25R DENTED ON FRAME. REMOVED DAMAGED AREA OF FRAME AT BS 700 BETWEEN STR 22 TO 25R, FABRICATED AND INSTALLED REPAIR PARTS PER FEDEX SRM 51-40-3.

Part: SRTINGER — CORROSION (BS 765)

CORROSION (C53-224-01, 2), ON STR 4L AT BS 765. ACCOMPLISHED STR REPAIR AT BS 765 STR 4L IAW FEDEX SRM 53-10-3.

Part: SKIN — DENTED (LT AILERON)

DENT ON I/B UPPER SURFACE OF LEFT WING I/B AILERON. REMOVED, REPAIRED AND REINSTALLED SERVICEABLE LEFT WING I/B AILERON IAW FEDEX MM 27-10-1, FUNCTIONAL TESTED IAW FEDEX MM 27-10-00.

Part: BLKHD ANGLE — CORROSION (BS 720)

CORROSION (C53-111-01-2), ON BULKHEAD SUPPORT ANGLE AROUND NUTPLATE HOLES BS 720D LBL 28 WL 156. CORROSION WAS FOUND TO BE OUT LIMITS. REMOVED BULKHEAD SUPPORT AND INSTALLED NEW BULKHEAD SUPPORT ANGLE AT BS 720D LBL 28 WL 156.

Part: BLKHD ANGLE — CORROSION (BS 400)

CORROSION ON BULKHEAD SUPPORT ANGLE AT BS 480 RBL 24 TO 39 WL 155. CORROSION OUT OF LIMIT ON BULKHEAD SUPPORT ANGLE AT BS 480 RBL 24 TO 39. ROBBED SERVICEABLE BULKHEAD SUPPORT FROM N489FE AND REMOVED AND REPLACED SERVICEABLE BULKHEAD SUPPORT.

Part: STIFFENER — CORROSION (BS 308)

CORROSION (C53-111-014), ON HORIZONTAL STIFFENER AT BS 308 WL 170 LBL 13 RBL 13 (P/N 65-18417-5). REMOVED HORIZONTAL STIFFENER AT BS 309 WL 170 LBL RBL 13 AND INSTALLED NEXT STIFFENER.

Part: FRAME — DAMAGED (BS 1090)

PUNCTURED FRAME BS 1090 STR 7L WL 281. REPAIRED DAMAGED FRAME AT BS 1090 STR 7L WL 281 PER FEDEX SRM 53-10-4 FIG 2.

Part: FLOOR SUPPORT — CORROSION (BS 480)

CORROSION (C53-111-01-1), ON UNDERSIDE OF FLOOR SUPPORT AROUND RIVNUT BS 480 WL 155 LBL 13.5. REMOVED CORROSION ON UNDERSIDE OF FLOOR SUPPORT AROUND RIVNUT BS 480 WL 155 LBL 13.5. REMOVED .003 INCH BY 1 INCH BY 1.125 INCH FROM ORIGINAL THICKNESS OF .071. FOUND TO BE WITHIN LIMIT PER FEDEX SRM 53-10-1, ALODINED AND PRIMED.

Part: SKIN — CORRODED (BS 700)

CORROSION (C53-111-01-2), ON SKIN AT BS 700 WL 145 RBL 8 O/B OF STR 28R FOUND ON INNER SURFACE WHILE WORKING NR0235. CORROSION ON SKIN AT BS 700 WL 145 RBL 8 O/B OF STR 28R WAS FOUND TO BE OUT OF LIMITS PER FEDEX SRM 53-30-1. REMOVED DAMAGED AREA, FABRICATED DOUBLER, CLEANED, TREATED AND INSTALLED PER FEDEX 53-30-3.

Part: NUTPLATE STRIP — DAMAGED (BS 720)

CORROSION (C53-111-01-1), ON PRESSURIZATION NUTPLATE DOMES AT BS 720B LBL 5 TO RBL 5 IN BILGE. REMOVED NUTPLATE STRIP AT BS 720B LBL 5. REMOVED .5 INCH BY 1 INCH BY .026 INCH. CORROSION WAS DETERMINED TO BE OUT OF LIMITS IAW FEDEX SRM 53-10-6. FABRICATED NEW STRIP, CLEANED AND TREATED MNR4489073. INSTALLED NUTPLATES AND NEW NUTPLATE STRIP.

Part: SKIN — CORROSION (BS 720)

CORROSION (C53-111-01-1), ON EXTERIOR SKIN SURFACE AT BS 720A PLUS 10 TO 720C, BL 0 WL 145. CORROSION FOUND WHILE ACCESSING NR0481 BENEATH RAM AIR DOOR'S SPLITTER VALVE. BLENDED CORROSION ON EXTERIOR SKIN BS 720A TO 720C BL 0 WL 145 BENEATH RAM AIR SPLITTER VANE. CORROSION FOUND TO BE WITHIN LIMITS PER FEDEX SRM 53-30-1, CLEANED AND TREATED SKIN.

Part: FRAME — DENTED (BS 680)

FWD BAY FRAME DENTED AT BS 680 AT STR 24 L.

Part: FRAME — DENTED (BS 700)

FWD CARGO BAY BS 700 BETWEEN STR 22 TO 25R DENT ON FRAME.

Part: CHANNEL — CORRODED (BS 328)

CORROSION (C53-224-01), ON HAT CHANNEL BS 328 WL 208 RBL 13. REMOVED CORRODED HAT CHANNEL, FABRICATED AND INSTALLED HAT CHANNEL AT BS 303 TO 344 RBL 10 TO 15 WL 208.

Part: STRINGER — CORROSION (BS 720)

CORROSION (C53-111-01-1), ON STR 27R AT BS 720B PLUS 10, INSIDE BAY. REMOVED CORROSION 1 INCH BY 2 INCH BY .005 INCH DEEP AT BS 720 PLUS 10 STR 27R, ORIGINAL THICKNESS 0.89. FOUND WITHIN ALLOWABLE LIMITS PER FEDEX SRM 53-10-1, CLEANED AND TREATED.

Part: KEEL BEAM — CRACKED (BS 950)

POSSIBLE CRACK FOUND ON SIDE OF RT KEEL BEAM APPROX 2 INCHES LONG AT BS 950E PLUS 3 STR 29R WL 145. REPAIRED CRACKED KEEL BEAM AFT CARGO BAY BS 950E PLUS 3 STR 29R WL 145 PER PER EA 7-5310-26741.

Part: SKIN — CORRODED (BS 950)

CORROSION (53-111-01-3), ON SKIN AT BS 950F PLUS 10 STR 28L WHILE WORKING ON CARD NR0208, CORROSION OUT OF LIMITS. CUT OUT DAMAGE, FABRICATED DOUBLER AND FILLER, INSTALLED PER FEDEX SRM 53-30-3.

Part: SUPPORT — CORRODED (BS 720)

CORROSION (C53-111-01-1) ON UNDERSIDE OF FLOOR TO SIDEWALL SUPPORT PLATE BS 720D TO BS 720C, LBL 25, WL 155. CORROSION REMOVED AROUND NUTPLATES ON SIDEWALL SUPPORT PLATE BS 720D TO BS 720C, LBL 25, WL 155. IN FOUR PLACES, 1.50 INCH BY 1.50 INCH BY .004 INCH FROM ORGINAL THICKNESS OF .063 INCH, FOUND TO BE WITHIN LIMITS. CLEANED AND TREATED PER SRM 51-10.

Part: STRINGER — CORROSION (BS 720)

CORROSION (53-111-01-1), ON STR AT BS 720 A PLUS 10 STR 27R, INSIDE BAY. REMOVED CORROSION 1.5 INCH BY 1.5 INCH BY .011 INCH DEEP AT BS 720A PLUS 2 TO 720A PLUS 17 STR 27R, ORIGINAL THICKNESS .084. FOUND WITHIN ALLOWABLE LIMITS PER FEDEX SRM 53-10-1, CLEANED AND TREATED.

Part: STRINGER — CORRODED (BS 950)

CORROSION (C53-111-01-3), ON STR AT BS 950F PLUS 10, STR 28L, WHILE WORKING ON NR 0208.

Part: STRINGER — CORROSION (BS 720)

CORROSION (C53-111-01-1), ON STR AT BS 720 PLUS 10 STR 27R, INSIDE BAY.

Part: FRAME — DENTED (BS 1039)

IN THE AFT CARGO BAY THE FRAME IS DENTED AT STA 1039 BETWEEN STR 25 TO 26L. REPAIRED FRAME AT BS 1030 BETWEEN STR 25 TO 26L PER FEDEX SRM STR 40-3. ALODINED, PRIMED AND PAINTED, REPAIR DOUBLER FRAME WAS FOUND TO BE OUT OF LIMITS PER SRM 53-10-1.

Part: STRINGER — CORROSION (BS 720)

CORROSION (C53-111-01-1), ON STRINGER AT BS 720 PLUS 10 STR 27R, INSIDE BAY. REMOVED CORROSION AT BS 720 PLUS 10 STR 27R, REPAIRED DAMAGE PER FEDEX SRM 53-10-3 DETAIL 1. CUT OUT CORROSION AREA OUT OF LIMITS PER FEDEX 53-10-1.