N483FE

Part: CONNECTOR — DAMAGED (NR 2 ENGINE OIL) · airframe 43,800 hrs · 29,902 cycles

INFLIGHT ENG SHUTDOWN NR 2 OIL TEMP FLUCTUATED INTO YELLOW RANGE. RAN QRH REDUCED POWER LEVER TO IDLE, THEN TEMP WENT ABOVE RED RADIAL. TROUBLESHOOTING DISCOVERED BROKEN WIRE GROUNDING ON THE D530 PLUG (TEMP BULB CONNECTOR) REPINNED CONNECTOR IAW CHAP 20, AND WDM 79-33-01. RAN ALL ENGINE TO 90 PERCENT N1 IAW JRH, CHAP 6, ALL ENGINE PARAMETERS WERE NORMAL, NO FLUCTATION NOTED DURING IDLE OR POWER RUNS ON THE NR 2 OIL TEMP INDICATOR. ACFT OK FOR CONTINUED SERVICE.

Part: STRINGER CLIP — CORRODED (BS 1183 S26L) · airframe 43,547 hrs · 29,672 cycles

CORROSION - STRINGER 26L AT STA 1183 TENSION TIE FITTING, INSIDE CHANNEL. REMOVED SECTION OF STRINGER 26L AT STA 1183, 20" IN LENGTH IAW SRM, REV 102, 51-30-2, 51-10-1, AND 53-10-1 FIG 1. FABRICATED STRINGER USING BAC1498-145, 7075-T6, 20" IN LENGTH. FABRICATED SPLICE USING BAC1498-131 7075-T6, 14.5" IN LENGTH IAW SRM 53-10-3 FIG 1, 53-10-2 FIG 9. INSTALLLED STRINGER AND SPLICE IAW SRM 53-10-3, FIG 1.

Part: SEAT TRACK — CORRODED (BS 620) · corrosion level 2 · airframe 43,547 hrs · 29,672 cycles

CORROSION SEAT TRACK FLANGE MAIN CABIN BS. 620, RBL 24. REMOVED DAMAGED SEAT TRACK IAW SRM 51-30-2 AND FABRICATED NEW SEAT TRACK AT RBL 24 BS 540+10" FROM BAC 1520-792-7178-T6511 IAW SRM 53-10-5 FIG 1 REV 102 INSTALLED NEW SEAT TRACK IAW SRM 51-30-2.

Part: RIB — CRACKED (NR 2 SLAT) · airframe 43,547 hrs · 29,672 cycles

LT WING NR 2 L/E SLAT INBD & OTBD RIBS ARE CRACKED WHERE ACTUATOR ROD END MOUNTS. R & R INBD & OTBD ACTUATOR RIBS PN 65-17310-3 & 65-17310-4, FABRICATED 1 EA OTBD RIB APPROX WS 251 FROM 7075-O .040 DIM: 16.25" X 6" & FABRICATED NEW ACTUATOR RIB CHANNEL FROM 2024T3 .071 DIM: 9" .7500 X 5" .5 & INSTALLED NEW INBD & OTBD ACTUATOR RIBS, OTBD RIB & CHANNEL IAW SRM 51-30-2, SRM 51-20-1, SRM 51-10-2, FAS ER 2-37153-801 & DWG 65-17310.

Part: FLOORBEAM — CORRODED (BS 480) · corrosion level 2 · airframe 43,547 hrs · 29,672 cycles

CORROSION FLOORBEAM TOP MAIN CABIN BS 480 BL 0 TO RBL 25. CUT DAMAGE OUT AREA 2.5" X 2", FABRICATED UPPER CHORD FROM BAC 1505-100617 DIM: 14.5" AND INSTALLED FLOORBEAM REPAIR IAW SRM 53-10-8 FIG 3, REV 102 AND SRM 51-30-2.

Part: STRINGER — CRACKED (BS 1166-1183) · corrosion level 2 · airframe 43,547 hrs · 29,672 cycles

STRINGER 22L CORRODED, BETWEEN STA 1166 - 1183, UPPER SURFACE OF UPPER CHANNEL. CUTOUT DAMAGED SECTION OF STRINGER DIM: 25" .3750 AT STA 1166-1183 IAW SRM 53-10-3, FIG 1. FABRICATED STRINGER REPAIR FROM BAC 1498-143 7075T62 DIM: 25" .3750 & SPLICE FROM BAC 1498-132 7075T62 DIM: 15" .7500 IAW SRM 53-10-3, FIG 1 REV 102. INSTALLED STRINGER & SPLICE IAW SRM 51-30-2.

Part: SKIN — CORRODED (LAV SERVICE DOOR) · airframe 43,547 hrs · 29,672 cycles

CORROSION, EXTERIOR SURFACE - T/E LOWER RADIUS LIP AT LT AFT LAV SERVICE DOOR CUT OUT. APPROX BS 1180, ABOVE STR 22L. REMOVED SKIN TRIPLER AT EXTERIOR SKIN T/E LOWER RADIUS LIP AT AFT LAV SERVICE DOOR BS 1180 STR 22L IAW SRM 51-30-2 AND FABRICATED NEW SKIN TRIPLER FROM 7075T6 .071 DIM: 20" X 20.4" IAW DWG 65-25607 AND INSTALLED NEW SKIN TRIPLER IAW SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 850-870) · corrosion level 2 · airframe 43,547 hrs · 29,672 cycles

UPPER LOWER FLANGE OF MAIN CABIN SEAT TRACK HAS SURFACE CORROSION BS 850 - BS 870 RBL 45. REMOVED DAMAGED SEAT TRACK SECTION FROM BS 850 - BS 870 RBL 45, FABRICATED NEW SEAT TRACK SECTION FROM BAC 1520-1466-7178T6 DIM: 16" & INSTALLED NEW SEAT TRACK IAW SRM 53-10-2 FIG 7, REV 102, SRM 51-30-2, SRM 51-30-5, & SRM 51-10-2.

Part: SEAT TRACK — CRACKED (BS 995) · airframe 43,547 hrs · 29,672 cycles

CRACK SEAT TRACK MAIN CABIN RBL 24 BS 995 SECTION OF TRACK IS BS 950, 10" TO BS 1135. REMOVED DAMAGED SEAT TRACK BS 950, 10" TO BS 1135 RBL 24 IAW SRM 51-30-2 AND FABRICATED NEW SEAT TRACK FROM BAC 1520-7927178T6511 DIM: 25' LONG IAW SRM 53-10-5 FIG 1. INSTALLED NEW SEAT TRACK IAW SRM 53-10-5 FIG 1 AND 51-30-2.

Part: SEAT TRACK — CORRODED (BS 870-950) · corrosion level 2 · airframe 43,547 hrs · 29,672 cycles

SURFACE CORROSION MAIN CABIN SEAT TRACK BS 870 - BS 950, LBL 24. REMOVED SEAT TRACK SECTION, FABRICATION NEW SEAT TRACK SEC FROM BAC 1520-792 717896 DIM: 7' 19", INSTALLED NEW SEAT TRACK SECTION, IAW SRM 51-30-2, 53-10-5 FIG 1 AT MAIN CABIN BS 870 - 950 LBL 24.

Part: FRAME — CRACKED (BS 804.5 S14R) · airframe 43,547 hrs · 29,672 cycles

CRACK IN MAIN CABIN FRAME AT BS 804.50, STR 14R. REMOVED CRACKED ANGLE CHORD, FABRICATED NEW ANGLE CHORD FROM BAC 1490-2510, DIM: 38.1250" AND INSTALLED NEW ANGLE CHORD AT BS 804.5 STR 14R IAW SRM 51-30-2, SRM 53-10-2, FIG 5, SRM 51-10-2, SRM 51-30-2, AND ER 2-37153-801, REV A.

Part: ANGLE — CRACKED (NR 7 SLAT) · airframe 43,547 hrs · 29,672 cycles

SPLICE DOUBLER CRACKED - NR 7 SLAT T/E CHORD ANGLE BENEATH TAI DUCT, APPROXIMATE WING STA 619. REMOVED T/E CHORD ANGLE OF NR 7 SLAT IAW SRM, REV 102, 51-30-2. LOCATED, DRILLED, DEBURRED AND TRIMMED CHORD ANGLE, 114" LONG, IAW SRM 57-50-2 FIG 2 AND 51-30-5. INSTALLED CHORD, FABRICATED FROM BAC1514-1559, 2024-T3, 114" LONG IAW SRM 51-30-2.

Part: STRUCTURE — CRACKED (NR 4 SLAT) · airframe 43,547 hrs · 29,672 cycles

UPON REMOVAL OF T/E ACCESS PANELS, FOUND NR 4 SLAT T/E STRUCTURE CRACKED NEAR TAI DUCT CUTOUT. REMOVED T/E STRUCTURE IAW SRM 51-30-2. FABRICATED NEW STRUCTURE USING EXTRUSION, BAC1514-1559 2024 T3511, DIMENSIONS 120", IAW SRM 57-50-2 FIG 2, 51-30-5, AND 51-30-2. INSTALLED NEW T/E STRUCTURE IAW SRM 51-30-2, REV 102.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 43,547 hrs · 29,672 cycles

CORROSION BOTTOM FLANGE FLOORBEAM BS 720 RBL 38 MAIN CABIN. CUT OUT DAMAGED AREA AT FLOORBEAM, BS 720, RBL 38, DIM: 3" X 2" IAW SRM 53-10-8, FIG 2, FABRICATED 2 NEW ANGLES 7075T6 .063 DIM: 17" X 2.75", FILLER BAC 1505-100797 7075T6 DIM: 3" X 2", STRAP 7075T6 .100 DIM: 14.750" X 2" IAW SRM 53-10-8 FIG 2, AND INSTALLED REPAIR IAW SRM 53-10-8 FIG 2.

Part: SUPPORT ANGLE — CRACKED (BS 1263) · airframe 43,547 hrs · 29,672 cycles

CRACKED SUPPORT ANGLE - INSIDE RT TORQUE BOX, AFT SIDE OF STA 1263 AT AFT AIR STAIR ACTUATOR SUPPORT ASSY. REMOVED SUPPORT ANGLE FROM RT SIDE OF TORQUE BOX, AFT SIDE OF STA 1263 IAW SRM, REV 102, 51-30-2. LOCATED, DRILLED, DEBURRED AND CUT TO LENGTH EXTRUSION AND10136-3005, 7075-T6511, 9.5" LONG IAW SRM 51-30-5. INSTALLED SUPPORT ANGLE IAW SRM 51-30-2, 51-40-2, FIG 1.

Part: SKIN — CORRODED (BS 680-685) · corrosion level 2 · airframe 43,547 hrs · 29,672 cycles

FWD PIT - CORROSION ON SKIN AT BS 680 TO 685, BETWEEN STRINGERS 28R AND 27R. REMOVED CORROSION IAW SRM, REV 102, 51-10-6. FABRICATED REPAIR DOUBLER AND FILLER USING 2024-T3, FILLER DIMENSIONS: .071" X 1.1250" X 3.2500", DOUBLER DIMENSIONS: .080" X 12.7500" X 15.1250" IAW SRM 53-30-3, FIG 3A. INSTALLED DOUBLER AND FILLER IAW SRM 53-30-3. FIG 3A.

Part: SHEAR TIE — CORRODED (BS 1010 S29-30L) · airframe 43,547 hrs · 29,672 cycles

CORROSION ON SHEAR TIE AT BS 1010 BETWEEN STRINGERS 30 AND 29 L. REMOVED DAMAGE, .7500" X 3.5" IAW SRM, REV 102, 53-10-4 FIG 15. FABRICATED SHEAR TIE REPAIR DOUBLER FOR BS 1010 FRAME BETWEEN STRINGERS 30 AND 29L IAW SRM 53-10-4, FIG 15. INSTALLED DOUBLER IAW SRM 53-10-4, FIG 15. FABRICATED DOUBLER USING 7075 - 0, .071" X 3.6250" X 2" IAW SRM 53-10-4, FIG 15.

Part: STRINGER — CORRODED (BS 680-700 S28R) · corrosion level 2 · airframe 43,547 hrs · 29,672 cycles

FWD CARGO HAS EXFOLIATION CORROSION ON STRINGER 28R BETWEEN STA 680 TO 700. CUT OUT DAMAGED SECTION OF STRINGER 28R, 29.5" IN LENGTH IAW SRM, REV 102M 53-10-3 FIG 1 AND 51-10-1. FABRICATED (2) STRINGER SECTIONS USING BAC1498-143, 7075-T62, 18.5" AND 11" IN LENGTH, AND (2) SPLICES USING BAC1498-132, 7075-T6, 13.2500" AND 16.5" IN LENGTH IAW SRM 53-10-3, FIG 1, DETAIL 1. INSTALLED SPLICES AND STRINGER IAW SRM 53-10-3 FIG 1, DETAIL 1.

Part: SEAT TRACK — CORRODED (BS 870-950) · corrosion level 2 · airframe 43,547 hrs · 29,672 cycles

MAIN CABIN SEAT TRACK CORRODED BS 870-950 10, LBL 45. REMOVED DAMAGED SEAT TRACK SECTION IAW SRM 51-30-2 AND FABRICATED NEW SEAT TRACK SECTION FROM BAC 1520-7927178T6511 DIM: 91" LONG IAW SRM 53-10-5 FIG 1. INSTALLED NEW SEAT TRACK SECTION IAW SRM 51-30-2.

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 43,547 hrs · 29,672 cycles

SHEAR TIE CRACKED AT BS 344 BETWEEN STRINGERS 27 AND 26L CUT-OUT DAMAGE AREA DIM 3" X 1.2500" IAW SRM 53-10-4 FIG 14. FABRICATED DOUBLER REPAIR FROM 7075T6 .050 DIM 4.7500" X 4.3750" IAW SRM 53-10-4, FIG 14. INSTALLED REPAIR IAW SRM 53-10-4 AND 51-30-2, REV 102.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 43,547 hrs · 29,672 cycles

CORROSION FLOORBEAM TOP MAIN CABIN BS 950 RBL 45 TO RBL 62. CORROSION OUT OF LIMITS, R & R FLOORBEAM TOP BS 950 RBL 62.5 TO 62.5 FROM BAC 1505-100405 7075T6 DIM: 129.5" LONG IAW B. DWG NR 65-16338, SRN 53-10-1, FIG 8.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 43,547 hrs · 29,672 cycles

CORROSION FLOORBEAM TOP SECTION MAIN CABIN BS 1130, LBL 45 - LBL 24. CUT-OUT DAMAGED AREA 2 5/8" X 1 3/8" FLOORBEAM BS 1130 LBL 45 TO LBL 24 IAW SRM 53-10-8 FIG 10 REV 102. FABRICATED REPAIR PART FROM 7075T6 .050 DIM: 10 1/4" X 3 1/4" IAW SRM 53-10-8 FIG 10 REV 102. INSTALLED REPAIR PARTS IAW SRM 51-30-2 REV 102.

Part: SHEAR TIE — CORRODED (BS 990 S28-29L) · corrosion level 2 · airframe 43,547 hrs · 29,672 cycles

SHEAR TIE CORRODED ON BS 990 FRAME BETWEEN STRINGERS 29L AND 28L. CUT OUT DAMAGE, 4 1/4" X 3/4" IAW SRM, REV 102, 53-10-4, FIG 15. FABRICATED SHEAR TIE REPAIR DOUBLER USING 7075-0, .071" X 4 1/4" X 2 1/4" IAW SRM 53-10-2 FIG 5 AND 53-10-4 FIG 15. INSTALLED SHEAR TIE IAW SRM 53-10-4 FIG 15.

Part: SHEAR TIE — CORRODED (BS 990 S29-30L) · corrosion level 2 · airframe 43,547 hrs · 29,672 cycles

CORROSION ON SHEAR TIE AT BS 990 BETWEEN STRINGER 30 AND 29L. CUT OUT DAMAGED AREA DIMENSIONS 4 1/4" X 1 3/4" ON FRAME SHEAR TIE IAW SRM 53-10-4 FIG. 13, REV 102. FABRICATED REPAIR DOUBLER USING 7075 T-6 .071" DIM 3 1/4" X 6 1/2" IAW SRM 53-10-4 FIG 13 AND 53-10-2 FIG 5. INSTALLED REPAIR PARTS IAW SRM 51-30-2 AND 53-10-4 FIG. 13.

Part: SEAT TRACK — CORRODED (BS 1135-1177) · airframe 43,547 hrs · 29,672 cycles

CORROSION ON SEAT TRACK SPLICE ATTACHED ON FLOOR WEB, MAIN CABIN BS 1135 - 1177, LBL 24. REMOVED DAMAGED SEAT TRACK SECTION AND FABRICATED NEW SEAT TRACK FROM 7075T6. FLAT BAR DIM: 44.7500" & INSTALLED NEW SEAT TRACK FROM BS 1135 - BS 1177, LBL 24 IAW SRM 51-30-2, SRM 51-10-2 & DWG NR 53FX976.

Part: SEAT TRACK — CORRODED (BS 480-600) · airframe 43,547 hrs · 29,672 cycles

CORROSION SEAT TRACK SECTION BS 480 -BS 600 BL 0. NUMEROUS AREAS, MAIN CABIN. REMOVED DAMAGED SEAT TRACK SECTION FROM STA 480- STA 600 BL 0 IAW SRM 51-30-2 AND FABRICATED NEW SEAT TRACK SECTION FROM BAC 1520-792 1778 T6511 DIM: 120 ".5 IAW SRM 53-10-2, FIG 7A, REV 102. INSTALLED NEW SEAT TRACK SECTION FROM STA 480 - STA 600 BL 0 IAW SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 360-480) · airframe 43,547 hrs · 29,672 cycles

CORROSION SEAT TRACK BS 360 - 480 RBL 25. REMOVED DAMAGED SEAT TRACK SECTION FROM STA 360 RBL 25 IAW SRM 51-30-2. FABRICATED NEW SEAT TRACK SECTION FROM BAC 1520-792 7178 T6511 DIM: 135" .2500 IAW SRM 53-10-5, FIG 1. INSTALLED NEW SEAT TRACK SECTION FROM STA 360 - 480 RBL 25 IAW SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 880) · airframe 43,547 hrs · 29,672 cycles

CORROSION ON UPPER FLANGE OF MAIN CABIN SEAT TRACK BS 880, RBL 24. REMOVED SEAT TRACK AND FABRICATED NEW SEAT TRACK FROM BAC 1520 792-7178T6 DIM: 7 FT. X 7 IN. IAW SRM 53-10-5 FIG 1. INSTALLED NEW SEAT TRACK IAW SRM 53-10-5, PG 4, FIG 1, REV 102.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 43,547 hrs · 29,672 cycles

UPON REMOVAL OF RAIN GUTTER FASTENERS ABOVE L-1 DOOR, FOUND DOUBLE DRILLED HOLE THROUGH HUCKBOLT AT BS 328. ACCOMPLISHED EA 7-5330-135539 DATED 05/18/10.

Part: SKIN — CRACKED (BS 1100) · airframe 43,547 hrs · 29,672 cycles

CRACK EXTENDING FROM RIVET TAIL, LT SIDE OF STRINGER 1, STA 1100. ACCOMPLISHED REPAIR LT SIDE OF STRINGER 1 STA 1100 IAW EO NR 7-5330-7-2343 F1 PT2 WO NR 00048048.

Part: SEAT TRACK — CORRODED (BS 600-720) · airframe 43,547 hrs · 29,672 cycles

CORROSION SEAT TRACK SEGMENT NUMEROUS AREAS MAIN CABIN BS 720- BS 600, BL 0. REMOVED DAMAGED SECTION FROM STA 600 - STA 720 BL 0 IAW SRM 51-30-2 AND FABRICATED NEW SEAT TRACK SECTION FROM BAC 1520-792 7178 T6511 DIM: 120" IAW SRM 53-10-5 FIG 1, REV 102. INSTALLED NEW SEAT TRACK SECTION FROM STA 600 - STA 720 BL0 IAW SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 480-690) · airframe 43,547 hrs · 29,672 cycles

CORROSION SEAT TRACK SECTION NUMEROUS AREAS MAIN CABIN BS 690 - BS 480, RBL 45. REMOVED SEAT TRACK SECTION IAW SRM 51-30-2 AND FABRICATED SEAT TRACK FROM BAC 1520-792-7178-T6511 DIM: 209.5" IAW SRM 53-10-5, FIG 1. FABRICATED SPLICES ANGLES FROM BAC 1503-1001227178T6511 DIM; 13.5" X 2". FABRICATED STRAP FROM 7075T6 .250 DIM; 7.5" X 2" IAW SRM 53-10-5 FIG 1. INSTALLED SEAT TRACK AND SPLICES IAW SRM 53-10-5, FIG 1.

Part: FRAME — CRACKED (BS 540 S21-22L) · airframe 43,547 hrs · 29,672 cycles

LOWER STUB FRAME EXTENSIONS, BS 540 STR 21L - 22L, CRACK ON RADIUS CUT OUT. REMOVED STUB FRAME AT BS 540 BETWEEN STRINGERS 21L - 22L IAW B727 SRM 51-30-2, REV 102. FORMED STUB FRAME USING 7075-0, .063" X 16" X 6", PO NO. 9009327 IAW B727 SRM 51-20- 1 FIG 7 AND FED EX DWG 53FX1350. HEAT TREAT FROM 7075-0 TO 7075 T-6 IAW FAS ENGINEERING REPORT NO. 2-37153-801 REV. A. TREAT AND PRIMED IAW B727 SRM 51-10-2. INSTALLED NEW STUB FRAME IAW B727 SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 360-480) · airframe 43,547 hrs · 29,672 cycles

CORROSION SEAT TRACK BS 360 - BS480 BL 0. REMOVED DAMAGED SEAT TRACK SECTION FROM STA 360 - 480 BL 0 IAW SRM 51-30-2. FABRICATED NEW SEAT TRACK SECTION FROM BAC 1520-792 7178 T6511 DIM: 136" IAW SRM 53-10-2 FIG 7A. INSTALLED NEW SEAT TRACK SECTION STA FROM STA 360 - 480 BL 0 IAW SRM 51-30-2.

Part: WEB — CRACKED (TORQUE BOX) · airframe 43,547 hrs · 29,672 cycles

LT LOWER STAIR WELL TORQUE BOX BS 1228 HAS LIGHTENING HOLE CRACK. ROUTED OUT DAMAGED AREA .1875" X .5" IAW SRM, REV 102, 51-10-1. FABRICATED DOUBLER FROM MATERIAL 7075 T-6, .032" X 1" X 4" IAW SRM 53-10-2 FIG 6 AND 51-40-2 FIG 1. INSTALLED REPAIR DOUBLER IAW SRM 51-30-2.

Part: WEB — CRACKED (TORQUE BOX) · airframe 43,547 hrs · 29,672 cycles

LT STAIRWELL BS 1266 VERT TORQUE BOX WEB IS CRACKED ON LIGHTENING HOLE. ROUTED OUT DAMAGED AREA .3" X .3750" IAW SRM 51-10-1, REV 102. FABRICATED REPAIR DOUBLER USING 7075 T-6 .032", DIM 1" X 4" IAW SRM 53-10-2, FIG 6 AND 51-40-2 FIG 1. INSTALLED REPAIR DOUBLER IAW SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 1135-1177) · airframe 43,547 hrs · 29,672 cycles

CORROSION ON SEAT TRACK SPLICE ATTACHED ON FLOOR WEB, MAIN CABIN BS. 1135 - BS 1177, LBL 45. REMOVED SEAT TRACK SECTION IN MAIN CABIN IAW SRM 51-30-2 AND FABRICATED NEW SEAT TRACK DIM; 44.8750" AND FLAT BAR DIM; 4" X .5" FROM 7075T6 IAW DWG 53FX976. INSTALLED NEW SEAT TRACK SECTION AND PARTS IAW SRM 51-30-2.

Part: WEB — CRACKED (TORQUE BOX) · airframe 43,547 hrs · 29,672 cycles

LT STAIRWELL BS 1279 LOWER VERT TORQUE BOX WEB IS CRACKED AT LIGHTENING HOLE. REMOVED DAMAGED AREA IAW SRM 51-10-1, REV 102. FABRICATED NEW DOUBLER USING MATERIAL 7075 T-6 .032", PO NR. 9009134, DIM 1" X 4" IAW SRM 53-10-2 FIG 6 AND 51-40-1 FIG 1. INSTALLED NEW DOUBLER IAW SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 690-720E) · corrosion level 2 · airframe 43,547 hrs · 29,672 cycles

CORROSION NUMEROUS AREAS SEAT TRACK SECTION BS 690 - BS 720E PLUS 10" LBL 25. REMOVED DAMAGED SEAT TRACK SECTION IAW SRM 51-30-2. FABRICATED NEW SEAT TRACK SECTION FROM BAC 1520-792 7178T6511 DIM: 172" IAW SRM 53-10-5, FIG 1. INSTALLED NEW SEAT TRACK SECTION IAW SRM 51-30-2.

Part: SILL — DAMAGED (ZONE 200) · airframe 43,547 hrs · 29,672 cycles

DOUBLE DRILLED HOLE INBD SILL MAIN CABIN BS 500 STR 3L. REMOVED DAMAGED IB FWD SILL & INSTALLED NEW SILL PN 53FX1475-101 AT MAIN CARGO DOOR FWD IB UPPER SILL AREA IAW SRM 51-30-2, SRM 51-30-5, SRM 51-10-2 & DWG 53FX1475, REV E.

Part: SEAT TRACK — CORRODED (BS 890-950) · corrosion level 2 · airframe 43,547 hrs · 29,672 cycles

SURFACE CORROSION ON UPPER FLANGE OF MAIN CABIN SEAT TRACK BS 890 - 950, BL 0. REMOVED SEAT TRACK AND FABRICATED NEW SEAT TRACK FROM BAC 1520-792-7178 T6511 DIM: 10' IAW SRM 53-10-5 FIG 1, REV 102 AND INSTALLED SEAT TRACK SECTION IAW SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 870-950) · airframe 43,547 hrs · 29,672 cycles

UPPER FLANGE OF MAIN CABIN SEAT TRACK HAS SURFACE CORROSION BS 870 - 950, RBL 45. REMOVED DAMAGED SEAT TRACK FROM BS 870 - 950, 10" RBL 45, FABRICATED NEW SEAT TRACK SECTION FROM BAC 1520-7927178T6511 DIM: 7 FT 19 IN. & INSTALLED NEW SEAT TRACK SECTION IAW SRM 51-30-2, SRM 53-10-5 FIG 1 & SRM 51-10-2.

Part: SEAT TRACK — CORRODED (BS 480-690) · corrosion level 2 · airframe 43,547 hrs · 29,672 cycles

CORROSION SEAT TRACK NUMEROUS AREAS MAIN CABIN BS 690 TO BS 480, LBL 25. REMOVED DAMAGED SEAT TRACK SECTION FROM STA 480- 690 LBL 25 IAW SRM 51-30-2. FABRICATED NEW SEAT TRACK SECTION FROM BAC 1520-792-7178T6511 DIM: 209" .2500 AND FABRICATED ANGLE SPLICES FROM BAC 1503-100-1227178 DIM: 15" X 2" .2500 (EACH), FABRICATED STRAP SPLICE FROM 7075T6 .250 DIM: 7" X 2" IAW SRM 53-10-5 FIG 1. INSTALLED NEW SEAT TRACK SECTION, ANGLE SPLICES AND STRAP SPLICES IAW SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 360-480) · corrosion level 2 · airframe 43,547 hrs · 29,672 cycles

CORROSION SEAT TRACK BS 360 - 480 LBL 25. REMOVED DAMAGED SECTION FROM STA 360 - 480 LBL 25 IAW SRM 51-30-2 AND FABRICATED NEW SEAT TRACK SECTION FROM BAC 1520-792-7178 T6511 DIM: 136" IAW P - F SRM 53-10-2 FIG 7A. INSTALLED NEW SEAT TRACK SECTION FROM STA 360 - 480 LBL 25 IAW SRM 51-30-2 & 53-10-5 FIG 1, REV 102.

Part: FLOORBEAM — CORRODED (BS 380) · airframe 43,547 hrs · 29,672 cycles

CORROSION FLOORBEAM TOP MAIN CABIN BS 380, RBL 25 - RBL 45. CUT-OUT DAMAGED AREA DIM: 34" X 2", FABRICATED UPPER CHORD FROM BAC 1505-100617, DIM: 34" X 2.5". FABRICATED REINFORCEMENT STRAPS FROM BAC 1512 3396-7075-T6 AND BAC 1512-3353 7075-T6 DIM: 34" X 1" AND 30 3/8" X 1". INSTALLED UPPER CHORD AND REPAIR PARTS IAW SRM 53-10-8, FIG 3, REV 102, SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 480-690) · corrosion level 2 · airframe 43,547 hrs · 29,672 cycles

CORROSION SEAT TRACK SECTION BS 690 TO BS, 480 LBL 45. R & R SECTION SEAT TRACK FROM BAC 1520 792 7178T6511 DIM: 216" IAW SRM 53-10-5, FIG 1, REV 102 AND SRM 51-10-2.

Part: FRAME — CRACKED (BS 580 S21-22L) · airframe 43,547 hrs · 29,672 cycles

LOWER STUB FRAME EXTENSIONS, BS 580, STR 21L - 22L, CRACK ON RADIUS CUT OUT. REMOVED STUB FRAME AT BS 580 BETWEEN STR 21L AND 22L IAW SRM, REV 102, 51-30-2. FABRICATED STUB FRAME USING 7075 - 0, .063" X 6" X 17" IAW SRM 51-20-1 FIG. 7 AND DWG NR 53FX1350. INSTALLED STUB FRAME IAW SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 850-870) · airframe 43,547 hrs · 29,672 cycles

SURFACE CORROSION ON MAIN CABIN SEAT TRACK BS 850 - 870 LBL 24. REMOVED SEAT TRACK SECTION IAW SRM 51-30-2 AND FABRICATED NEW SEAT TRACK IAW SRM 53-10-2 FIG7 & 51-30-5 FROM BAC 1520-1466 DIM: 16" & INSTALLED NEW SEAT TRACK SECTION AT BS 850-870 LBL 24 IAW SRM 53-10-2, FIG 7.

Part: SEAT TRACK — CORRODED (BS 690-720E) · airframe 43,547 hrs · 29,672 cycles

CORROSION SEAT TRACK SECTION NUMEROUS AREAS BS 690 - BS 720E PLUS 10" LBL 45. REMOVED SEAT TRACK FROM STA 690 TO 740 LBL 45 IAW SRM 51-30-2 FABRICATED NEW SEAT TRACK FROM BAC 1520-792-7178-T6 DIM: 171.7500" IAW SRM 53-10-5, FIG 1, INSTALLED NEW SEAT TRACK IAW SRM 51-30-2, REV 102.

Part: STRINGER — DAMAGED (ZONE 100) · airframe 43,547 hrs · 29,672 cycles

STR REPAIR "17 X 11" REQUIRED EVALUATION AT STA 1166 - STA 1183, STR 23L IAW WORK CARD 7-5100-7-5005 PT 1. REMOVED DOUBLER IAW SRM, REV 102, 51-30-2. FABRICATED REPAIR DOUBLER USING 2024-T3, .100" X 23 1/2" X 21 5/8" IAW EA 7-5330-135540. INSTALLED REPAIR DOUBLER IAW EA NR 7-5330-135540 AND SRM 51-30-2,

Part: WEB — CRACKED (TORQUE BOX) · airframe 43,547 hrs · 29,672 cycles

LT STAIRWELL BS 1236 VERT TORQUE BOX WEB IS CRACKED AT FASTENER. CUT OUT DAMAGED AREA .7500" X 1.2500" AT BS 1236 VERT TORQUE BOX WEB IAW SRM, REV 102, 51-10-1. FABRICATED .7500" X 1.2500" FILLER USING 7075 T-6, .025" IAW SRM 51- 40-2 FIG 1. FABRICATED REPAIR DOUBLER USING 7075 T-6, .032" DIM. 3.3750" X 2" IAW SRM 51-40-2 FIG 1. INSTALLED FILLER AND REPAIR DOUBLER IAW SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 720) · airframe 43,547 hrs · 29,672 cycles

CORROSION SEAT TRACK MAIN CABIN BS 720 PLUS 18", RBL 45. REMOVED SEAT TRACK SECTION AT RBL 45 FROM BS 690 TO BS 740 IAW SRM 51-30-2, FABRICATED SEAT TRACK SECTION FROM BAC 1520-792 7178-T6511 DIM: 172" IAW SRM 53-10-5, FIG 1. INSTALLED SEAT TRACK SECTION AT RBL 45 FROM BS 690 TO BS 740 IAW SRM 53-10-5, FIG 1, REV 102.

Part: SEAT TRACK — CRACKED (BS 758) · corrosion level 2 · airframe 43,547 hrs · 29,672 cycles

BS 758 LBL 45 - SEAT TRACK END CRACKED AT LIGHTING HOLE. REMOVED SEAT TRACK AND "T" CHORD FROM BS 758 LBL 45 IAW SRM 51-30-2. FABRICATED NEW 'T" CHORD FROM BAC 1506-1108 7075T6 IAW SRM 53-10-2, FIG 7 AND INSTALLED NEW "T" CHORD IAW SRM 53-10-2, FIG 7, REV 102 AND SAME SEAT TRACK IAW SRM 51-30-2.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 43,547 hrs · 29,672 cycles

CORROSION SEAT TRACK SECTION NUMEROUS AREAS MAIN CABIN BS1135 - BS 1177, LBL 45. REPLACED SEAT TRACK SECTION ON NR N00750 AND SDR10-1283, WO 00048048.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 43,547 hrs · 29,672 cycles

CORROSION NUMEROUS AREAS ALONG SECTION SEAT TRACK MAIN CABIN BS 950, 10" TO BS 990, LBL 45. REPLACED SEAT TRACK SECTION ON NR N00750, SDR 10-1283, WO 00048048.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 43,547 hrs · 29,672 cycles

CORROSION NUMEROUS AREAS ALONG SEAT TRACK MAIN CABIN BS 950, 10" TO BS 1135 RBL 45. REMOVED DAMAGED SEAT TRACK SECTION FROM BS 950, 10" TO BS 1135 RBL 45 FROM BAC 1520-792-7778-T6511 DIM: 25FT & INSTALLED NEW SEAT TRACK IAW SRM 53-10-5 FIG 1, SRM 51-10-2, SRM 51-30-2 REV 102.

Part: STRINGER — CORRODED (BS 950A-950E) · airframe 43,547 hrs · 29,672 cycles

STRINGER 29L IS CORRODED AROUND FASTENERS FROM BS 950A TO 950E. R & R STRINGER 29 LT FROM PN65-56441-7 BETWEEN BS 950 TO BS 1008 IAW DWG 65-56441 AND IAW SRM 51-30-2.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 43,547 hrs · 29,672 cycles

CORROSION SEAT TRACK SECTION NUMEROUS AREAS MAIN CABIN BS 950, 10" TO BS 1135, LBL 24. REMOVED SEAT TRACK BS 950, 10" TO BS 1135 LBL 24 IAW SRM 51-30-2. FABRICATED NEW SEAT TRACK FROM BAC 1520-792-7178-T6 DIM: 24 FT 8 IN IAW SRM 53-10-5, FIG 1. INSTALLED NEW SEAT TRACK AT BS 950, 10" TO BS 1135 LBL 24 IAW SRM 53-10-5, FIG 1, REV 102.

Part: SILL — CRACKED (ZONE 200) · airframe 43,547 hrs · 29,672 cycles

MAIN CARGO DOOR UPPER SILL, BS 490, BETWEEN STRINGERS 3L AND 4L. CRACKS ORIGINATING FROM FASTENER HOLES. R & R MAIN CARGO DOOR UPPER OTBD FWD SILL PN 53FX1467-101 & ACCOMPLISHED EA 7-5330-135536 & SRM 51-30-2, SRM 51-10-2, SRM 51-30-5 & DWG 53FX1467.

Part: SEAT TRACK — CORRODED (BS 760-850) · airframe 43,547 hrs · 29,672 cycles

MAIN CABIN SEAT TRACK HAS SURFACE CORROSION BS 760 - 850, RBL 45. REMOVED TEE FITTING AT STA 740 - 850 RBL 45, FABRICATED NEW TEE FITTING FROM BAC 1506-1108 7075 T6 DIM: 109 1/2", AND INSTALLED NEW TEE FITTING IAW DWG NR 65-16279, AND SRM 51-30-2.

Part: SHEAR TIE — CORRODED (BS 950C S29-30R) · airframe 43,547 hrs · 29,672 cycles

CORROSION ON FRAME SHEAR TIE FLANGE, STA 950C BETWEEN STR 30 AND STR 29R. CUT OUT DAMAGE ON SHEAR TIE DIM 2.2500" X 4.1250" IAW SRM, REV 102, 51-10-1. FABRICATED REPAIR DOUBLER USING 7075-0, .080", DIM 5.3750" X 6.2500" IAW SRM 53-10-2, FIG 5 AND 53-10-4, FIG 12. INSTALLED REPAIR DOUBLER IAW SRM 51-30-2 AND 53-10-4, FIG 12.

Part: STRINGER — CORRODED (BS 950B) · airframe 43,547 hrs · 29,672 cycles

STRINGER 29R IS CORRODED AFT OF BS 950B. R & R STRINGER 29 RT FROM PN 65-56441-8, BETWEEN BS 950 TO BS 1008 IAW DWG NR 65-56441 AND SRM 51-30-2.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 43,547 hrs · 29,672 cycles

CORROSION SEAT TRACK NUMEROUS AREAS MAIN CABIN BS 990 - BS 1090, LBL 45. REMOVED SEAT TRACK SECTION FROM BS 950 10 - BS 1135 LBL 45, FABRICATED NEW SEAT TRACK FROM BAC 1520-792-7178-T6 DIM: 25', FABRICATED NEW SPLICE SECTION 2 EA ANGLES FROM BAC 1503-1001227 DIM: 15" X 3", LOWER STRAP FROM 7075-T6 .250 DIM: 9" X 2" & INSTALLED NEW SEAT TRACK SECTION & SPLICES IAW SRM 51-30-2, SRM 53-10-5, FIG 1 & SRM 51-10-2.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 43,547 hrs · 29,672 cycles

CORROSION SEAT TRACK MAIN CABIN BS 1130 - BS 1010, BL 0. REMOVED SEAT TRACK SECTION FROM BS 1010 - BS 1130 BL0, FABRICATED NEW SEAT TRACK SECTION FROM BAC 1520-792 7178-T6511, APPROX DIM: 10' FT & INSTALLED NEW SEAT TRACK SECTION IAW SRM 51-30-2, SRM 53-10-5 FIG 7, REV 102 & SRM 51-10-2, FX 727 P-F SRM 53-10-5.

Part: SHEAR TIE — CRACKED (BS 344 S26-27R) · airframe 43,547 hrs · 29,672 cycles

SHEAR TIE CRACKED AT BS 344 BETWEEN STRINGERS 27R AND 26R. CUT OUT DAMAGED SHEAR TIE 3.1250" X .7500" IAW SRM, REV 102, 53-10-4 FIG. 13. FABRICATED NEW SHEAR TIE REPAIR 4" X 4" IAW B727 SRM 53-10-4 FIG. 13. INSTALLED SHEAR TIE IAW SRM 53-10-4 FIG. 13.

Part: SKIN — CHAFED (ZONE 100) · airframe 43,547 hrs · 29,672 cycles

FUSELAGE EXTERIOR SKIN CHAFED AT LAP SEAM STA 720D 15" STR 19R. CUT-OUT DAMAGED AREA SIZE: 2.7500" X 3.7500" AT LAP SEAM IAW SRM 53-30-3, FIG 6. FABRICATED DOUBLER AND (2) EA TAPER SHIMS FROM 2024T3 .071 SIZES: 10.2500" X 8.7500" AND (2) EA 1" X 6" AND (2) EA FILLERS FROM 2024T3 .063 SIZES: 6.7500" X 10.2500" AND 2.7500" X 3.7500" IAW SRM 53-30-3, FIG 6. INSTALLED REPAIR PARTS IAW SRM 53-30-3, FIG 6.

Part: SEAT TRACK — CORRODED (BS 1135-1177) · airframe 43,547 hrs · 29,672 cycles

CORROSION ON SEAT TRACK ATTACHED TO FLOOR WEB MAIN CABIN BS 1177- BS 1135, BL0. REMOVED DAMAGED SEAT TRACK IAW SRM 51-30-2. FABRICATED NEW SEAT TRACK SECTION DIM: 44.7500" TO FLAT BAR DIM: 4" X .5" FROM 7075T6 IAW DWG 53FX976 AND INSTALLED NEW SEAT TRACK SECTION & PARTS IAW SRM 51-30-2.

Part: SHEAR TIE — CORRODED (BS 950C) · corrosion level 2 · airframe 43,547 hrs · 29,672 cycles

CORROSION IN SHEAR TIE AT BS 950C BETWEEN STRINGERS 30 AND 29L. CUT OUT SHEAR TIE 2.2500" X 4.1250" FROM BS 950C FRAME BETWEEN STRINGERS 30 AND 29L IAW SRM, REV 102, 51-10-1 AND 53-10-4 FIG 12. FABRICATED SHEAR TIE REPAIR DOUBLER USING 7075 -0, .080" X 7.2500" X 5.3750" IAW SRM 53-10-4 FIG 012. INSTALLED REPAIR DOUBLER IAW SRM, REV 102, 53-10-4, FIG 12 AND 51-30-2.

Part: FRAME — DAMAGED (ZONE 200) · airframe 43,547 hrs · 29,672 cycles

MAIN CARGO AREA BS 440 BETWEEN STR 3L AND 4L MULTIPLE HOLES ON FRAME. TRIMMED OUT DAMAGED AREA DIM: 2" X .8125" IAW SRM 53-10-4, FIG 1. FABRICATED "Z" FRAME REPAIR FROM 7075O DIM: 12" X 4" (2) EA CHANNELS IAW SRM 53-10-2, 53-10-4 FIG 1 AND HEAT TREATED TO T6 IAW FAS FORM NR FAS0115. REV 001. FABRICATED FILLER FROM 7075T6 .050 DIM: 2" X .8125" IAW SRM 53-10-4 FIG 1. INSTALLED "Z" FRAME REPAIR (CHANNELS, FILLER) AND STRINGER TIE AT BS 440 BETWEEN STR 3L AND 4L IAW SRM 53-10-4, FIG 1.

Part: SEAT TRACK — CORRODED (BS 360-480) · corrosion level 2 · airframe 43,547 hrs · 29,672 cycles

CORROSION SEAT TRACK BS 360-480, LBL 45. REMOVED DAMAGED SECTION FROM STA 360 - 480, LBL 45 IAW SRM 51-30-2 AND FABRICATED NEW SEAT TRACK SECTION FROM BAC1520-792-7178 T6511 DIM: 135" 7/8 IAW P-F SRM 53-10-2, FIG 7A. INSTALLED NEW SEAT TRACK SECTION FROM STA 360-480 LBL 45 IAW SRM 51-30-2 AND 53-10-5 FIG 1, REV 102.

Part: STRUCTURE — CRACKED (BS 294-360) · corrosion level 2 · airframe 43,547 hrs · 29,672 cycles

FWD LWR INTERIOR NOSE COMPARTMENT - "DOG HOUSE" - RT LWR NOSE CHORD LEVEL COMPOUND IS CRACKED AND SEPARATING BS 294.5 -360 BILGE. R & R NEW CHORD NOSE RT PN 65-19861-8 IAW SRM 51-30-2.

Part: SILL — CRACKED (BS 590) · airframe 43,547 hrs · 29,672 cycles

MAIN CARGO DOOR UPPER SILL, BS 590, BETWEEN STRINGERS 3L AND 4L, CRACKS ORIGINATING FROM FASTENER HOLES. R & R MAIN CARGO DOOR UPPER AFT SILL PN 53FX1467-102 IAW DWG 53FX1467, SRM 51-30-2, SRM 51-30-5, AND 51-10-2.

Part: SEAT TRACK — CORRODED (BS 360) · airframe 43,547 hrs · 29,672 cycles

CORROSION SEAT TRACK BS 360, RBL 45. REMOVED CORROSION AREA FOUND OUT OF LIMITS IAW B727 SRM 53-10-1 FIG 1, REMOVED SEAT TRACK SECTION BETWEEN STA 344 TO ST 480 RBL 45 IAW SRM 51-30-2. FABRICATED SEAT TRACK FROM BAC 1520-792-7178T6 DIM: 135.8750" IAW SRM 53-10-2, FIG 7A, REV D, INSTALLED SEAT TRACK AT RBL 45 FROM BS 344 TO BS 480 IAW SRM 53-10-2 FIG 7A, REV D.

Part: STRUCTURE — CRACKED (BS 294-340) · corrosion level 2 · airframe 43,547 hrs · 29,672 cycles

FWD LWR INTERIOR NOSE COMPARTMENT - "DOG HOUSE", LT LWR NOSE CHORD LEVEL COMPOUND IS CRACKED AND SEPARATING BS 294.5 TO 340 BILGE. R & R NEW CHORD NOSE LT PN 5715216 IAW SRM 51-30-2.

Part: SKIN — CHAFED (ZONE 100) · airframe 43,547 hrs · 29,672 cycles

FUSELAGE EXTERIOR SKIN CHAFED AT LAP SEAM STA 720D 15" STR 19L. CUT-OUT DAMAGE AREA SIZE: 2.7500" X 3.7500" AT LAP SEAM IAW SRM 53-30-3, FIG 6. FABRICATED REPAIR DOUBLER AND 2 EA, TAPER FILLER FROM 2024T3 .071 SIZES: 11.5 X 8.7500" AND 2 EA 1" X 6" AND 2 EA FILLERS FROM 2024T3 .063 SIZES: 6.1250" X 10.5" AND 3.7500" X 2.7500". INSTALLED REPAIR PARTS IAW SRM 53-30-3, FIG 6.

Part: DOOR FRAME — CRACKED (BS 620 S23R) · airframe 43,547 hrs · 29,672 cycles

NR 1 CARGO DOORWAY FRAME, BS 620, STR 23R, WEB CRACKED. REMOVED BS 620 WEB FROM STRINGER 15 - 28 RT IAW DWG 65-56101. FABRICATED NEW BS 620 WEB FROM STRINGER 15 -28 RT USING 7075 - T6, .071", DIMENSIONS 139.35" X 26" IAW DWG 65-56101 REV F. INSTALLED NEW BS 620 WEB FROM STRINGER 15-28 RT IAW DWG 65-56101 REV F AND SRM, REV 102, 51-30-2.

Part: STRINGER — CORRODED (BS 687 S27R) · airframe 43,547 hrs · 29,672 cycles

MISSING RIVET INCLUDING BULGE EXT FUSELAGE SKIN BS 687, STR 27R. REMOVED CORRODED SECTION OF STRINGER 27R AT BS 687, 11 7/8" IN LENGTH IAW SRM, REV 102, 51-10-1. FABRICATED STRINGER SECTION USING BAC1498-143, 7075-T62, 11.8750" IN LENGTH AND SPLICE USING BAC1498-132, 7075-T6, 13.6250" IN LENGTH IAW SRM 53-10-3 FIG 1, DETAIL 1. INSTALLED STRINGER AND SPLICE IAW SRM 53-10-3, FIG 1, DETAIL 1.

Part: SKIN — GOUGED (NR 2 SLAT) · airframe 43,547 hrs · 29,672 cycles

LT WING NR 2 LE SLAT UPPER T/E HAS (2) DEEP GOUGES ON SKIN BY THE OTBD HOOK. REMOVED HOOK AT NR 2 SLAT OTBD SIDE IAW SRM 51-30-2 AND FABRICATED REPAIR PLATE USING 7075T6 .125 DIM: 4" .7500 X 3" .2500 IAW SRM 57-50-3, FIG 10, REV 102. INSTALLED REPAIR PLATE IAW SRM 51-30-2. INSTALLED NR 2 SLAT HOOK OTBD SIDE IAW SRM 51-30-2 REV 102. OPS CHECK GOOD IAW MM 27-81-000-5.

Part: SPAR — CRACKED (WS 171) · airframe 43,547 hrs · 29,672 cycles

CRACKED FALSE SPAR AT NR 8 SPOILER ATTACHMENT, WS 171. REMOVED DOUBLER, TRIMMED WEB 12.2500" X 9.5", LOWER CHORD 20.5" LONG IAW DWG NR SR27-57-038 REV C. FABRICATED CHORD SPLICE ANGLES FROM 7075 - 0 .071" X 6" X 14" (2) RADIUS FILLERS FROM 7075 T6 .160" X 2" X .7500", DOUBLER FROM 2024 T3 .050" X 12" X 9" WEB FROM 7075 T6 .032" X 12.2500" X .090", CHORD FROM BAC1514-1437 7075 T6511 20.33" LONG, STRAP FROM 7075 T6 .090" X 11.5" X 1.7500" IAW DWG NR SR27-57-038. INSTALLED CHORD SPLICE ANGLES, RADIUS FILLERS, DOUBLER, WEB, CHORD AND STRAP IAW DWG NR 27-57-038 AND SRM 51-30-2, REV 102.

Part: DUCT — SEPARATED (ANTI-ICE SYS) · airframe 42,089 hrs · 28,536 cycles

DURING CLIMB-OUT WITH CLIMB POWER SET AND PASSING 3500 FT MSL, NR 2 ENG FIRE HANDLE AND BELL ACTIVATED. COMPLIED WITH QRH AND DUMPED 400 LBS OF FUEL. LANDED AT MEM. FOUND NR 2 ENG COWL ANTI-ICE DUCT SEPARATED AFT OF VALVE DUCT DAMAGED. REMOVED AND REPLACED NR 2 ENG LT A/I AFT DUCT SECTION PER MM 75-10-012-4. OPS AND LEAK CHECKS GOOD IN REFERENCE TO MM 75-10-000-2.

Part: CYLINDER — LEAKING (CARGO DOOR) · airframe 42,064 hrs · 28,512 cycles

ON CLIMBOUT, "MCD ARM" LIGHT AND "CARGO DOOR IN-TRANSIT" LIGHT ILLUMINATED, REPEAT WRITE UP.PRESSURIZATION WAS NORMAL THROUGHOUT FLIGHT. AT TIME OF LIGHT ILLUMINATION, PSID WAS 6. APPX ALTITUDE WAS 15,000. R & R MCD AFT LATCH CYLINDER PER 52-34-021-4. BLED AND OPS CHECKED NORMAL. RAN DOOR SEVERAL TIMES WITH PRESS IND. PLUMBED IN LINE AT PORT 2. PER DRAWING. NO LEAK DOWN NOTED. RESTORED A/C TO NORMAL. PRESSURIZED A/C TO CHECK FOR MIGRATION OF LOCK BAR. PRESS TO 5.0 D FOR APPROX 25 MIN. WITH NO LOCK BAR MOVEMENT NOTED. NO WARNING LIGHTS ILLUMINATED

Part: CONTROL VALVE — FAILED (HYD SYSTEM) · airframe 42,063 hrs · 28,511 cycles

ARM LIGHT AND CARGO DOOR IN TRANSIT LIGHT ILLUMINATED IN FLIGHT. PRESSURIZATION REMAINED NORMAL. REPLACED HYDRAULIC SOLENOID SHUTOFF VALVE PER MM 52-34-129-4. REPLACED HYDRAULIC CONTROL VALVE PER MM 52-34-101-4. OPS OK PER MM 52-34-009-5.

Part: COALESCER BAG — DIRTY (CABIN AIR) · airframe 41,870 hrs · 28,356 cycles

ON DESCENT PASSING THROUGH 17,000 FT, STRONG ODOR SIMILAR TO ELECTRICAL SMOKE DETECTED IN COCKPIT. ODOR SUBSIDED BUT RETURNED ON SHORT FINAL. INSPECTION OF A/C IN PROGRESS. INSPECTED A/C'S CB'S NONE WERE FOUND POPPED. NO LINGERING ODOR OF SMOKE ANYWHERE ON A/C WHEN IT ARRIVED AT THE GATE. INSPECTED E/E AND RADAR R/T COMPT, NO DEFECTS NOTED. RAN BOTH RT AND LT PACKS WITH ENG'S AND APU. SLIGHT ODOR USING RT PACK. FOUND COALESCER BAGS DIRTY. REMOVED AND REPLACED BOTH LT AND RT PER MM 21-55-051. A/C OK FOR SERVICE.

Part: ENGINE — DAMAGED (NR 1) · airframe 41,422 hrs · 27,974 cycles

AFTER TAKEOFF AT 1000 FT, CREW FELT A VERY PRONOUNCED THUMP ACCOMPANIED BY A LOUD NOISE. AUTO PACK TRIP ILLUMINATED. ENGINE INSTRUMENTS CHECKED NORMAL. WHILE TROUBLESHOOTING THE PROBLEM AND CLIMBING THROUGH 18,000FT. ANOTHER LOUD THUMP AND NOISE OCCURRED AND THE NR 1 ENGINE EPR DECREASED TO 1.5 EPR. RETARDED NR 1 THROTTLE RAN THE QRH CHECKLIST AND RETURNED TO PHL. FOUND APPROX 6 BLADES ON NR 1 ENGINE FAN DAMAGED CHECKING DAMAGE LIMITS.

Part: FIRE WARNING — ACTIVATED (NR 2 NACELLE) · airframe 41,138 hrs · 27,768 cycles

DURING CLIMBOUT PASSING 5000 FEET MSL,AFTER SETTING CLIMB POWER NR 2 ENGINE FIRE LIGHT AND FIRE BELL CAME ON. BELL WAS SILENCED. NR 2 ENGINE SHUTDOWN WITH START LEVER, LIGHT WENT OUT AFTER PULLING NR 2 ENG FIRE HANDLE. FIRE BOTTLES WERE NOT DISCHARGED. REMOVED AND REPLACED NR 2 ENGINE IAW WORK CARD 70T002. PERFORMED B727 ENGINE RUN-UP AFTER ENGINE CHANGE- NR 2 WORK CARD 70T0301-02. LEAK CHKS AND OP CHKS NORMAL.

Part: SKIN — MISREPAIRED (BS 227.8-237) · airframe 40,249 hrs · 26,998 cycles

EXTERNAL REPAIR. 9.2 INCHES X 3 INCHES AT BS 227.8 - 237, STR. 26L REQUIRES EVALUATION. DETERMINE IF THE REPAIR IS MAJOR OR MINOR AND IF THE REPAIR IS IN ACCORDANCE WITH FAA APPROVED DATA. REMOVED & REPAIRED EXTERNAL REPAIR AT BS 227-8-37 STR 6L PER FED EX EA 7-5330-91366 PREVIOUS REPAIR NOT ACCOMPLISHED PER SRM, FOUND TO BE A MAJOR REPAIR.

Part: STRAP — CRACKED (BS 229) · airframe 40,249 hrs · 26,998 cycles

WHILE WORKING FOUND INNER AND OUTER STRAPS CRACKED AT B.S 229 STR 26R. REPAIRED INNER AND OUTER STRAPS AT BS 229 STR 26R IAW FED EX EA 7-5330-91366 FOUND TO BE A MAJOR REPAIR.

Part: STRAP — CRACKED (BS 229) · airframe 40,249 hrs · 26,998 cycles

N01609 WHILE WORKING FOUND INNER AND OUTER STRAPS CRACKED AT B.S 229 STR 26L. REPAIRED INNER & OUTER STRAPS AT BS 229 STR 26L IAW FED EX EA 7-5330-91366 FOUND TO BE A MAJOR REPAIR.

Part: PANEL — GOUGED (HORIZONTAL STAB) · airframe 40,249 hrs · 26,998 cycles

RT HORIZONTAL STABILIZER UPPER T/E PANEL INNER SIDE IS GOUGED JUST 3 INCHES I/B OF NR 7 RIB. REPAIRED PER E.A. 7-5510-91362.

Part: STRUCTURE — CORRODED (NR 7 FLAP TRACK) · airframe 40,249 hrs · 26,998 cycles

AFTER REMOVAL OF NR 7 FLAP TRACK FWD FITTING ON N00421, FOUND EXISTING DAMAGE IN AFT INBOARD ATTACH FITTING HOLE. REPAIRED PER SRM 51-20-1, 51-30-2.

Part: WEB — CRACKED (VERTICAL STAB) · airframe 40,249 hrs · 26,998 cycles

VERTICAL STABILIZER 1303 WEB IS CRACKED AT LOWER LT CORNER. REPAIRED VERT STAB 1303 WEB IAW SRM 51-40-2.

Part: DEPRESSOR — DENTED (CARGO DOOR) · airframe 40,249 hrs · 26,998 cycles

NR 1 CARGO DOOR LWR CENTER SEAL DEPRESSOR DENTED AT AFT END. REPAIRED PER SRM 52-00-2.

Part: RIB — GOUGED (HORIZONTAL STAB) · airframe 40,249 hrs · 26,998 cycles

LEFT HORIZONTAL STAB NR 3 BALANCE BAY OB RIB IS GOUGED FROM CONTACT WITH IDLER HINGE PIN. REMOVED AND REPLACED L/HORIZ. STAB NO. 3 BALANCE BAY OUTBD RIB IAW EA 7-5510-70689, PART 1 AND 727 SRM 51-30-2 AND 51-30-5.

Part: SKIN — CRACKED (R1 DOOR) · airframe 40,249 hrs · 26,998 cycles

N00364 - R-1 DOOR SKIN IS CRACKED AT UPPER HINGE.

Part: SKIN — CRACKED (R1 DOOR) · airframe 40,249 hrs · 26,998 cycles

R-1 DOOR SKIN IS CRACKED AT UPPER HINGE.

Part: WEB — CRACKED (VERTICAL STAB) · airframe 40,249 hrs · 26,998 cycles

VERTICAL STABILIZER MAIN BOX WEB IS CRACKED AT FIN STA 133 JUST BELOW ACCESS CUTOUT. *S/D* INSTALLED DOUBLER AT FIN STA 133 PER EA 7-5530-91356.

Part: SKIN — CORRODED (BS 988) · airframe 40,249 hrs · 26,998 cycles

AFT CARGO COMP PREVIOUS REPAIR SKIN CUTOUT HAS CORRODED BS 988 RBL 11 BILGE. REPAIRED SKIN CUTOUT AT BS 988, RBL 11 PER FED-EX EA 7-5330-91368.

Part: SKIN — GOUGED (BS 990-1050) · airframe 40,249 hrs · 26,998 cycles

FUSELAGE SKIN HAS SEVERAL GOUGES FROM BS 990-1050 STRINGER 27L - 26R. REPAIRED PER SRM 53-30-3

Part: ATTACH FITTING — CORRODED (TE FLAPS) · airframe 40,249 hrs · 26,998 cycles

RIGHT WING, NR 7 FLAP TRACK FWD ATTACH FITTING INBOARD FACE CORRODED (27X5709-02). REPAIRED PER E.A. 7-5710-91348.

Part: SPAR — CRACKED (CENTER WING) · airframe 40,249 hrs · 26,998 cycles

CRACK FOUND DURING UT & HFEC INSP AT WING CENTER SECTION UPPER REAR SPAR WEB BS 870 LBL 6 - 7.5. REPAIRED UPPER REAR SPAR CHORD AT BS 870, LBL 6-7.5 PER EO 7-5710-7-3325.

Part: SKIN — DENTED (BS 1060) · airframe 40,249 hrs · 26,998 cycles

UPON FURTHER INVESTIGATION FOUND 2EA DENTS ON SKIN AT BS 1060, 2 INCH BELOW STR 29.

Part: FLOOR SUPPORT — CORRODED (BS 268) · airframe 40,249 hrs · 26,998 cycles

CORROSION ON COCKPIT FLOOR STRUCTURE BS 268 LBL 8 WL 207. REMOVED FABRICATED AND INSTALLED WEB AND TEE CHORD IAW SRM 51-30-3, 51-30-6 AND 51-10-3.

Part: FRAME — DENTED (BS 580) · airframe 40,249 hrs · 26,998 cycles

FORWARD CARGO BAY, FRAME IS DENTED AT BS 580 BETWEEN STRINGER LT 24 AND LT 23. REPAIRED FRAME IAW SRM 51-40-3.

Part: SUPPORT — CORRODED (COCKPIT FLOOR) · airframe 40,249 hrs · 26,998 cycles

CORROSION ON COCKPIT FLOOR STRUCTURE BS 268 LBL 8 WL 207. REMOVED FABRICATED AND INSTALLED WEB AND TEE CHORD IAW SRM 51-30-3, 51-30-6 AND 51-10-3.

Part: FLOOR SUPPORT — CORRODED (BS 266) · airframe 40,249 hrs · 26,998 cycles

CORROSION ON COCKPIT FLOOR STRUCTURE BS 266 LBL 2 WL 207. REMOVED, FABRICATED AND INSTALL REPAIR PER SRM 51-20-1

Part: KEELBEAM — CRACKED (BS 874) · airframe 40,249 hrs · 26,998 cycles

UPPER FLANGE ON KEELBEAM, IS CRACKED AT FASTENER HOLE, STA 874, LBL 6. FABRICATED & INSTALLED STEEL DOUBLER AT BS 870 LBL 6 PER ECA 7-5310-70687 AND BOEING SERVICE BULLITEN 727-53-0208.

Part: STRINGER — DENTED (FUSELAGE) · airframe 40,249 hrs · 26,998 cycles

WHILE WORKING N01449, FOUND STRINGER 20R BS 419 TO BE DENTED. REPAIRED PER SRM 53-10-3 FIG 1.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,249 hrs · 26,998 cycles

N01510 WHILE WORKING FED EX NON ROUTINE CARD 5184, FOUND THE FRAME TO BE CRACKED AT BODY STATION 420 STRINGER 20R ** SD ** COMING REPAIRED CRACK PER SRM 51-40-3, THIS IS A MAJOR REPAIR.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,249 hrs · 26,998 cycles

CORROSION ON SKIN AT NR 3 VHF ANTENNA MOUNTING BRACKET CUT OUT BS 1042 WL 138.5 (AFT CARGO COMPARTMENT) REMOVED CORROSION ON SKIN AT NR 3 VHF ANTENNA MOUNTING BRACKET CUTOUT BS 1042 BL 0 WL 138.5 FOUND TO BE WITHIN LIMITS ALL WORK DONE IAW SRM 53-30-1, 51-10-1

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 40,249 hrs · 26,998 cycles

AT STA 435 STR 19R, FOUND CRACK AT FASTENER HOLES, 2ND HOLE FWD OF STRINGER SPLICE. REPAIRED PER SRM 53-10-3, MAJOR REPAIR. [CLOSED]

Part: STRINGER CLIP — DAMAGED (UPPER LOBE) · airframe 40,249 hrs · 26,998 cycles

FUSELAGE, UPPER LOBE, STA 680 STR 2L, STRINGER CLIP DAMAGED. REPLACED STRINGER CLIP AT BS 680, STR 2L PER SRM 51-30-2.

Part: RIB — CRACKED (NR 5 SLAT) · airframe 40,249 hrs · 26,998 cycles

RIGHT WING, NR 5 SLAT, LEADING EDGE RIB CRACKED OUTBOARD OF OUTBOARD MAIN TRACK. REMOVED AND REPLACED RIB IAW SRM 51-30-5, 51-30-2.

Part: FRAME — BENT (FUSELAGE) · airframe 40,249 hrs · 26,998 cycles

FRAME BENT STA 1070 STR 25L - 2L. REMOVED DAMAGED AREA, FABRICATED REPAIR ANGLE, TREATED AND PRIMED, INSTALLED REPAIR IAW SRM 51-30-2, 51-40-3, 51-10-2.

Part: STRINGER — DAMAGED (BS 1090) · airframe 40,249 hrs · 26,998 cycles

STRINGER AT BS 1090 STR 7LT IS DAMAGED. REPAIRED STRINGER PER SRM 53-10-1, 53-10-3 FIG 3 MAJOR REPAIR.

Part: STRINGER CLIP — BROKEN (STA 660) · airframe 40,249 hrs · 26,998 cycles

FUSELAGE UPPER LOBE, STA 660, STRINGER CLIP 8L BROKEN. REMOVED AND REPLACED STRINGER CLIP AT STR 8L BS 660 IAW SRM 51-30-2.

Part: SKIN — CORRODED (FUSELAGE) · airframe 40,249 hrs · 26,998 cycles

CORROSION ON FUSELAGE SKIN IS BULGED AT BS 1015 STRINGER 30. REMOVED CORROSION SPEC C53-100-03 FUSELAGE SKIN AT B.S. 1015 STR 30 FOUND TO BE OUT OF LIMITS. INSTALLED STRINGER REPAIR PER SMR 51-30-2, 53-10-1. (CLOSED)

Part: STRINGER — DENTED (CARGO BAY) · airframe 40,249 hrs · 26,998 cycles

FORWARD CARGO BAY, FRAME IS DENTED AT BS 720 AT STRINGER LT 24. REPAIRED FRAME AT BS 720, STR 24L PER SRM 51-40-3

Part: SKIN — DENTED (FUSELAGE) · airframe 40,249 hrs · 26,998 cycles

FUSELAGE SKIN HAS A DENT AT BS 1171, 1 INCH ABOVE STRINGER 23L. REPAIRED PER SRM 53-30-3.

Part: FLOORBEAM — DAMAGED (CABIN) · airframe 40,249 hrs · 26,998 cycles

FLOORBEAM WEB DAMAGED AT BS 328, LBL 31, WL 207. REPAIRED DAMAGED FLOOR BEAM WEB PER SRM 51-10-1, 53-10-1, 51-40-2

Part: FRAME — GOUGED (CARGO DOOR) · airframe 40,249 hrs · 26,998 cycles

MAIN CARGO DOOR AFT SIDE FRAME GOUGED, CENTER OF FRAME. REPAIRED PER SRM 53-30-2.

Part: SKIN — DENTED (FUSELAGE) · airframe 40,249 hrs · 26,998 cycles

FUSELAGE SKIN HAS A DENT AT BS 1186, 1 INCH BELOW STRINGER 23L. REPAIRED SKIN AT BS 1186 PER SRM 53-30-3.

Part: SKIN — DENTED (FUSELAGE) · airframe 40,249 hrs · 26,998 cycles

FUSELAGE SKIN HAS A DENT AT BS 1141, 1 INCH ABOVE STRINGER 20L. REPAIRED FUSELAGE SKIN AT BS 1141 1 INCH ABOVE STR 20L PER SRM 53-30-3

Part: SKIN — GOUGED (FUSELAGE) · airframe 40,249 hrs · 26,998 cycles

EXTERNAL FUSELAGE SKIN GOUGED STA 1183 2" ABOVE STR 15L. REPAIRED SKIN AT BS 1183 2" ABOVE STR 15L PER SRM 53-30-3

Part: STRINGER — DENTED (CARGO BAY) · airframe 40,249 hrs · 26,998 cycles

FORWARD CARGO BAY, FRAME IS DENTED AT BS 600 BETWEEN STRINGER LT 24 AND LT 23. REPAIRED DENTED FRAME AT BS 600 STR 23LH TO 24LH IAW SRM 51-40-3. [CLOSED]

Part: FLOORBEAM — INTERFERENCE · airframe 40,249 hrs · 26,998 cycles

BS 344 FLOORBEAM SPLICE INTERFER'S WITH BL O SEAT TRACK TO COMPLY WITH BARRIER MOD.

Part: FRAME — PUNCTURED (CARGO DOOR) · airframe 40,249 hrs · 26,998 cycles

MAIN CARGO DOOR AFT SIDE FRAME PUNCTURED, 15" FROM LOWER CORNER. REPAIRED PER SRM 52-30-2.

Part: FRAME — DENTED (CARGO BAY) · airframe 40,249 hrs · 26,998 cycles

FORWARD CARGO BAY, FRAME IS DENTED AT BS 580 BETWEEN STRINGER LT 24 AND LT 23. REPAIRED PER SRM 51-40-3. [CLOSED]

Part: STRINGER — DENTED (CARGO BAY) · airframe 40,249 hrs · 26,998 cycles

FORWARD CARGO BAY, FRAME IS DENTED AT BS 520 BETWEEN STRINGER LT 25 AND LT 22. REPAIRED FRAME AT FWD CARGO BAY BS 520 BETWEEN STR 25L & 22L IAW SRM 51-40-3, 51-10-2.

Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,249 hrs · 26,998 cycles

AFT CARGO COMP KEEL BEAM HAS CORROSION ON OB FLANGE BS 950B-970 STR-29R. FABRICATED & INSTALLED REPAIR STRAP PER FED EX SR-27-53-023, REV. A., SR27-53-013A, SRM 53-10-4.

Part: STRINGER — DENTED (CARGO BAY) · airframe 40,249 hrs · 26,998 cycles

FORWARD CARGO BAY, FRAME IS DENTED AT BS 500 BETWEEN STRINGER LT 26 AND LT 23. REPAIRED FWD CARGO BAY FRAME PER SRM 51-40-3.

Part: STRINGER CLIP — DAMAGED (FUSELAGE) · airframe 40,249 hrs · 26,998 cycles

STRINGER CLIP AT BS 1010 STR 7 LEFT IS DAMAGED. REMOVED AND REPLACED STR CLIP BS 1010 STR 7L IAW SRM 51-30-02

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 40,249 hrs · 26,998 cycles

AFT CARGO COMP SHEAR TIE HAS CORROSION BS 985 RBL 9. REPAIRED PER SRM 53-10-1, 53-10-3 FIG. 1.

Part: STRINGER CLIP — DAMAGED (FUSELAGE) · airframe 40,249 hrs · 26,998 cycles

FUSELAGE, UPPER LOBE, STA 680 STR 4L, STRINGER CLIP DAMAGED. REMOVED, FABRICATED AND INSTALLED CLIP PER SRM 51-40-1, 51-10-1, 53-10-2 & FED EX MM 51-20-151-7.

Part: STRINGER CLIP — DAMAGED (FUSELAGE) · airframe 40,249 hrs · 26,998 cycles

FUSELAGE, UPPER LOBE, STA 680 STR 3L, STRINGER CLIP DAMAGED. OUT OF LIMITS, REMOVED, FABRICATED AND INSTALLED CLIP PER SRM 51-40-1, 51-10-1, 53-10-1, 51-30-2 & FED EX MM 51-20-151-7.

Part: SHEAR TIE — CORRODED (FUSLEAGE) · airframe 40,249 hrs · 26,998 cycles

CORROSION ON SHEAR TIE STA 1166 BETWEEN STR 27L & 29L. REPAIRED PR SRM 51-10-1, 51-10-3, 51-20-1, 51-30-2.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 40,249 hrs · 26,998 cycles

STRINGER CLIP AT BS 950C STR 7 LT IS CRACKED. REPLACED STRINGER CLIP AT BS 950C, STR 7LT PER SRM 51-30-2.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 40,249 hrs · 26,998 cycles

STRINGER CLIP AT BS 950D STR 7L IS CRACKED. REPLACED STRINGER CLIP AT BS 950D, STR. 7LT PER SRM 51-30-2.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 40,249 hrs · 26,998 cycles

STRINGER CLIP AT BS 950B STR 7LT IS CRACKED. REPLACED STRINGER CLIP AT BS 950B STR 7LT PER SRM 51-30-2

Part: SILL — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 40,249 hrs · 26,998 cycles

NR 2 LOWER CARGO DOOR, CORROSION AROUND NUTPLATES STA 950E-990 ON PRESSURE SEAL SILL. REPAIRED PER EA 7-5310-91351.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 40,249 hrs · 26,998 cycles

STRINGER CLIP AT BS 950F STR 7LT IS CRACKED. REPLACED STRINGER CLIP AT BS 950F, STR 7LT PER SRM 51-30-2

Part: STRINGER CLIP — DAMAGED (FUSELAGE) · airframe 40,249 hrs · 26,998 cycles

STRINGER CLIP AT BS 1010 STR 7 RT HAS 2 PREVIOUSLY DRILLED HOLES. REPAIRED PER SRM 51-20-1, 51-30-2.

Part: SKIN — GOUGED (FUSELAGE) · airframe 40,249 hrs · 26,998 cycles

GOUGES IN FUSELAGE SKIN STA 215, 5 ABOVE STR 17L. REPAIRED DAMAGE IN FUSELAGE SKIN AT STA. 251.5, ABOVE STR 17R IAW SRM 51-30-1, SRM 53- 30-3, 51-10-02, 51-30-02.

Part: FRAME — DENTED (FUSELAGE) · airframe 40,249 hrs · 26,998 cycles

FWD CARGO PIT FRAME AT BS 500 HAS A DENT BETWEEN STRINGER 23R AND 25R. REPAIRED FRAME IAW SRM 51-40-3 THIS IS A MAJOR REPAIR.

Part: FRAME — DENTED (FUSELAGE) · airframe 40,249 hrs · 26,998 cycles

DENT IN FRAME STA 970 STR 23L. REPAIRED FRAME AT STA 970 STR. 23L PER SRM 51-40-3 FIG 1.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,249 hrs · 26,998 cycles

BS 1263 LWR RT TORQUE BOX FRAME ANGLE CRACKED RBL 20 WL 192. REPAIRED FRAME ANGLE PER SRM 51-30-2. (CLOSED)

Part: WARNING LIGHT — ILLUMINATED (COCKPIT) · airframe 39,341 hrs · 26,259 cycles

WENT TO FIREWALL POWER ON TCAS ALERT AT 5000 FT, FIREWALL POWER LESS THAN 10 SECS. IN WORK ADDITIONAL TSI 34-55-6491 ISSUED TO REMOVE TCAS PROCESSOR FOR BENCH DOWNLOAD/READOUT. ADDITIONAL TSI 23-70-6490 ISSUED TO REMOVE CVR FOR BENCH READOUT. PER VERBAL INFO A/C WAS AT 5000 LEVEL. INTRUDER SINGLE ENG WAS AT 4000 AND CLIMBING. TYS TOWER CONFIRMED. 99 DAY HISTORY SHOWS NO TCAS RA PROBLEMS. COMPLETED INLET/EXHAUST INSPECTION AND FIREWALL AND/OR EMERGENCY ESCAPE CHECK PER JRH 6-38. ALL CHECKS OK, RETURNED TO SERVICE PER EA 7-7200-78554.

Part: ACCESSORY UNIT — FAILED (MLG) · airframe 38,899 hrs · 25,915 cycles

AFTER TAKEOFF, LANDING GEAR LEVER WOULD NOT RAISE PAST THE OFF POSTION. RT GEAR DOOR LIGHT WAS ILLUMINATED. PERFORMED LANDING GEAR LEVER LATCH FAILED TO RELEASE CHECKLIST. AURAL WARNING HORN SOUNDED WHEN CHECKLIST CALLED FOR RAISING FLAPS TO 2 DEG. RECONFIGURED AND LANDED AT DEPARTURE AIRPORT. LANDING GEAR ACCESSORY UNIT FAILED AIR SENSING TEST. SUSPECT LANDING GEAR ACCESSORY UNIT BAD OR AIR SENSING SWITCH IN GEAR WELL. ORDERED PARTS REF WDM 32-31-01 PAGE 5. RANG AIR SENSING SENSOR AT D1890B FROM PINS 35 AND 36. FOUND SENSOR NG REMOVED AND REPLACED AIR SENSOR PER 32-09-221-4. PERFORMED ALTERNATE TEST PROCEDURE PER EA 7-3210-75019. OPS CHECK WAS NORMAL.

Part: ACCESSORY UNIT — MALFUNCTIONED (MLG) · airframe 38,578 hrs · 25,658 cycles

AFTER TAKEOFF LANDING GEAR LEVER RAISED TO UP POSTION. LANDING GEAR WARNING HORN STAYS ON STEADY WITH RED UNSAFE LIGHTS IN NOSE, LT AND RT LANDING GEAR ANNUNCIATOR. COMPLIED WITH QRH. AFTER 5 MIN IN FLT LIGHTS EXTINGUISHED AND HORN STOPPED. RE-RACKED LANDING GEAR ACCESSORY BOX. MOISTURE FOUND, DRIED OUT. C/W SYS CHECK AND CHECKED GOOD. NOTIFIED MOCC. ALL IAW GMM 32-09-122-5.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 38,155 hrs · 25,317 cycles

GENERATED DUE TO NOSE LANDING GEAR DOWNLOCK ACTUATOR FITTING CRACKED. UPON REPLACEMENT OF SUPPORT, FOUND NOSE LANDING GEAR AFT BULKHEAD WEB AND CHANNEL SUPPORT CRACKED. WEB REPAIR WAS ACCOMPLISHED IAW EA NR 7-5310-64754.

Part: GCU — MALFUNCTIONED (NR 3) · airframe 37,717 hrs · 24,975 cycles

NR 3 GENERATOR BREAKER TRIPPED. RESET IAW CHECK LIST. RETRIPPED AFTER APPROXIMATELY 1 MINUTE. NR 2 FIELD AND NR 2 GENERATOR TRIPPED. ACCOMPLISHED CHECK LIST PROCEDURES. UNDER VOLTAGE INDICATED ON NR 2. REMOVED AND REPLACED NR 3 GENERATOR CONTROL UNIT IAW SMP. RAN ENGINE NR 3 PER 727 JRH. OP'S CHECK GOOD IAW MM 24-22-000-2. REMOVED AND REPLACED NR 2 GENERATOR CONTROL UNIT IAW SMP. RAN ENGINE IAW 727. OP'S CHECK GOOD IAW 24-22-000-2.

Part: WIRE — CHAFED (NR 3 ENGINE) · airframe 37,717 hrs · 24,976 cycles

REPEAT WRITE UP. NR 3 GENERATOR BREAKER TRIPPED, ACCOMPLISHED CHECKLIST PROCEDURES. RESET GENERATOR AND IT RE-TRIPPED AFTER 1 MINUTE. REMOVED AND REPLACED NR 3 ENG DRIVEN GENERATOR IAW 727 MM 24-20-001-4. FOUND FIELD EXCITATION WIRE (F) CHAFED THROUGH WIRE INSULATION ON GENERATOR BRACKET. REPAIRED WIRE AND REPOSITIONED TO PREVENT FUTURE CHAFING IAW STANDARD WIRING PRACTICES. REMOVED AND REPLACED NR 3 ENG GENERATOR CONTROL UNIT IAW 727 MM 24-22-000-2. OP'S CHECK FOUND WHEN A LOAD WAS PUT ON GENERATOR THE BUS TIE BREAKER WOULD TRIP. REMOVED AND REPLACED NR 3 BUS TIE BREAKER IAW 727 MM 24-20-041-4. RAN ENG AND OP'S CK'D PER 727 JRH. OPS CHECK GOOD.

Part: TRANSMITTER — FAULTY (T/E FLAP)

AFTER T/O ON FLAP RETRACT INBOARD FLAPS STUCK AT 2 DEG. R&R BOTH LT & RT INBD FLAP TRANSMITTERS PER MM 27-52-002-4. SAFTIED FLAP ARM SWITCH & GPWS FLAP INHIBIT SWITCH. OK FOR SERVICE.

Part: INDICATOR — FAILED (FLT DECK K)

02-71 ASYMMETRICAL INBD FLAPS DUR RETRACT STOPPED BETWEEN 5 DEG & 2 DEG. R&R INBD FLAP IND PER MM 27-52-021-2.

Part: SWITCH — DIRTY (COCKPIT)

WHEN PUTTING GEAR HANDLE IN OFF AFT T/O RED DOOR LIGHT AND RG DOOR LIGHT ILLUM. REPOSITIONED HANDLE TO UP AND LIGHTS WENT OUT. *S/D* FOUND SWITCH AND CANNON PLUG DIRTY. CLEANED, OPS CK OK.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY)

MAIN CARGO SMOKE DETECTED ZONE NR 3 LIGHT CAME ON. REMOVED AND REPLACED NR 3 CARGO SMOKE DETECTOR MM 26-16-11. OPS GOOD ON GROUND.

Part: WARNING SYSTEM — ILLUMINATED (MLG)

00-21 - ON T/O DUR GEAR RETRACT, RMG DOOR ON 2ND OFF PNL AND RED DOOR LIGHT ON GEAR LIGHT PNL REMAIN ILLUM. LIGHTS WENT OUT AFT RED TABS. TROUBLESHOT GEAR DOOR POSITION IND (WARNING) PER 727 MM 32-61-001-1 WITH NO DEFECTS NOTED. OK FOR SERVICE.

Part: BELL FRAME — DAMAGED (BS 660)

NR 0867 FWD CARGO BS 660 BELL FRAME IS DAMAGED ABOVE STRINGER 24 LT. REMOVED DAMAGED AREA, INSTALLED DOUBLER ON BELL FRAME PER SRM 51-40-3. SPLICE INSTALLED AT STRINGER 25 PER EA NR75310-29332.

Part: SPLICE — CRACKED (BS 680-686)

FWD CARGO STRINGER 27LT, BS 680 PLUS 6, LEVELING COMPOUND CRACKED AND LIFTED AT STRINGER SPLICE. REMOVED LEVELING COMPOUND, FOUND CORROSION. REMOVED CORROSION BY CUTTING OUT DAMAGED SECTION. INSTALLED STRINGER SPLICE PER SRM 53-10-3 PAGE 4A, FIG 1, TABLE II AND SRM 53-10-3 PAG 4B.

Part: FRAME — DENTED (BS 490)

AFT LWR CARGO BELL FRAME DENTED AND BENT AT BS 490 BETWEEN STR 25 AND 26L. FABRICATED AND INSTALLED DOUBLER PER SRM 53-10-4.

Part: SKIN — CORRODED (BS 720)

BS 720, STRINGER 28L, CORROSION ON FUSELAGE SKIN AROUND NUT PLATE AND AREA WHERE SEALANT IS POURED ON ACFT SKIN. REMOVED DAMAGED AREA, ALODINED AND PRIMED AREA, INSTALLED EXTERNAL REPAIR DOUBLER FROM .071 2024T3 MATERIAL, AS PER SRM 53-30-3 PAGE 8 AND 53-30-3 PAGE 14 TABLE I AND II.

Part: FRAME — DENTED (BS 680)

FWD CARGO BS 680, STR 23L FRAME HAS DAMAGED (DENT). INSTALLED 7075-T6 DOUBLER (15 INCHES) IN FWD CARGO BS 680, STR 23L FRAME PER SRM 53-10-4.

Part: STRINGER — CORRODED (BS 1010)

BS 1010, STR 27L CORRODED. FABRICATED AND INSTALLED DOUBLER PER SRM 53-10-3 AT BS 1010, STR 27L.

Part: CSD — FAILED (NR 3 ENGINE)

AFTER TAKEOFF, NR 3 GENERATOR LOW OIL PRESS LIGHT CAME ON. FOLLOWED ALL STEPS IN RED TABS, CONSTANT SPEED DRIVE WOULD NOT DISCONNECT. AFTER THE 10TH TRY IT DISCONNECTED. CONSTANT SPEED DRIVE RISE WAS OUT OF LIMITS. CONSTANT SPEED DRIVE DID NOT DISCONNECT UNTIL WELL ON OUR WAY BACK TO DFW. REMOVED AND REPLACED NR 3 CONSTANT SPEED DRIVE, COOLER AND FLUSHED LINES. RAN ENGINE AND SYSTEM OPERATIONAL CHECKS AND LEAK CHECKS OK PER MAINTENANCE MANUAL 24-00. RESET CIRCUIT BREAKER FOR COOLING FAN AND RESAFTIED DISCONNECT.

Part: CONNECTOR — LOOSE (RT MLG DOOR)

RIGHT MAIN GEAR DOOR LIGHT ILLUMINATED WHEN GEAR HANDLE WAS PLACED IN THE OFF POSITION. RIGHT MAIN WARNING LIGHT WOULD GO OUT WITH HANDLE IN THE UP POSITION. AFTER CYCLING HANDLE FROM UP TO OFF SEVERAL TIMES THE RIGHT MAIN DOOR LIGHT REMAINED OFF. FOUND LOOSE CANNON PLUG ON RIGHT MAIN GEAR DOOR SWITCH. CLEANED AND TIGHTENED CANNON PLUG CYCLED DOOR AND OPERATIONAL CHECKED OK.

Part: SKIN — CRACKED (BS 303)

FORWARD LT FUSELAGE SKIN CRACKED AT FWD ENTRY DOOR LOWER HINGE CUT OUT. FS 303, STR 13L. CRACK LENGTH .480 INCH INITIAL MEASUREMENT. NDT VERIFIED CRACK END IN FASTENER HOLE. COUNTER BORED FUSELAGE OUTER SKIN AT FASTENER HOLE. ROUTED OUT CRACK AND INSTALLED FILLER AND DOUBLER PER SRM 53-30-3, FIG 11 AND BOEING SB 53-727-53-0198, REV I FIG 4.

Part: FLOOR BEAM — CORRODED (BS 344)

MAIN CARGO INTERIOR, CORROSION ON TOP OF STA 344 FLOOR BEAM UPPER CHORD BETWEEN RBL 2 - 14. REMOVED CORROSION, INSTALLED REPLACEMENT CHORD AND SPLICE ANGLES PER STANDARD REPAIR DRAWING MANUAL SR 277-53-007.

Part: FLOOR BEAM — CORRODED (BS 344)

MAIN CARGO INTERIOR, CORROSION ON TOP OF STA 344 FLOOR BEAM UPPER CHORD, BETWEEN RBL 2 - 14. REMOVED CORROSION, INSTALLED REPLACEMENT CHORD AND SPLICE ANGLES PER STANDARD REPAIR DRAWING MANUAL SR 27-53-007.

Part: STRINGER — CRACKED (BS 720)

MAIN CARGO INTERIOR STRUCTURE. STR 16R CRACKED IN OUTER FLANGE, AFT OF STA 720B FRAME, FWD OF ICE LIGHT HOUSING. STOP DRILLED CRACK, INSTALLED REPAIR DOUBLER PER SRM 53-10-3 FIG 2.

Part: FLOOR BEAM — CORRODED (BS 344)

CORROSION ON TOP OF UPPER LOBE FLOOR BEAM STA 344, RBL 2-6.

Part: STRINGER — CRACKED (BS 720)

NR 0398 (PATTERN CARD 72C235-02) CRACK IN STR 15L AT FASTENER. FORWARD SIDE OF ICE LIGHT BETWEEN FUSELAGE STA 720B - 720C. STOP DRILLED CRACK. INSTALLED REPAIR DOUBLER PER SRM 53-10-3, FIG 2.

Part: STRINGER — CRACKED (BS 720)

CRACK IN STR 15L AT FASTENER AFT OF ICE LIGHT BOX BETWEEN STA 720B AND 720G. STOP DRILLED CRACK IN STR 15L AT FASTENER AFT OF ICE LIGHT. HFEC AROUND STOP DRILL, NO CRACKS FOUND PER NDT MANUAL. INSTALLED REPAIR PER SRM 53-10-3 / 7075-T6 .040 INCH, SRM 53-10-2.