N486FE

Part: LIGHT — INOPERATIVE (CABIN) · airframe 41,549 hrs · 31,272 cycles

EMERGENCY EXIT LIGHTS ABOVE COCKPIT DOOR INOPERATIVE. R & R PORTABLE EMERGENCY LIGHT ABOVE COCKPIT DOOR. OPS CHECKED GOOD REF MM 33-50-101-2-0. ACFT OK FOR FLT.

Part: UNKNOWN — ODOR (CABIN) · airframe 41,528 hrs · 31,257 cycles

SHORTLY AFTER TAKEOFF DETECTED A BURNING ODOR WHICH DECREASED BUT PERSISTED. NO VISIBLE SMOKE OR FIRE INDICATIONS. DONNED MASKS AND RETURNED TO AIRPORT. RAN ALL 3 ENGINES IAW JRH AT BOTH GROUND AND APPROACH IDLE. ISOLATED EACH PACK WITH EACH ENGINE AT BOTH POWER SETTINGS. NOTICED NO ODD OR FOUL ODORS OR ANY SIGN OF SMOKE. CHECKED ACM OIL LEVELS FOUND OK. PERFORMED EXTENDED HIGH POWER RUN WITH GENERATORS AT FULL LOAD AND RAN PACKS AT VARIOUS TEMP SETTINGS. NO SMOKE OR ODORS.

Part: LANDING GEAR — LACK OF LUBE (MAINS) · airframe 41,384 hrs · 31,110 cycles

RED GEAR LIGHT REMAINED ILLUMINED UPON GEAR RETRACTION. COMPLIED WITH QRH AND RETURNED TO DEPARTURE. NOTE 15' OF RT AILERON REG FOR LEVEL FLIGHT. NO FUEL DUMPED INSPECTED ACFT BOTH MAIN GEAR AND DOORS NO DAMAGE NOTED. JACKED ACFT IAW MM 07-11-000-2. PERFORMED MULTIPLE GEAR SWINGS WITH ALL INDICATIONS CORRECT ON ALL GEAR IAW MM 32-32-00-5. FOUND LT GEAR PIVOT POINTS VERY DRY. LUBED GEAR IAW MM 12-21-001-2-0. FOUND AFT TRUNNION VERY DRY. TOOK 1 WHOLE TUB OF GREASE BEFORE SEEPING STARTED OUT OF FWD SIDE OF BEARING. ALSO ALL POINTS HAD LARGE AMOUNTS OF WATER. CHANGED LANDING GEAR ACCESSORY UNIT PRECAUTIONARY IAW MM 32-09-122-5-0 AND ALL CHECKS GOOD. PERFORMED ANOTHER SWING AND ALL CHECKS GOOD IAW MM 32-32-000-5. OK FOR SERVICE.

Part: SEAL — FAILED (NLG) · airframe 41,170 hrs · 30,921 cycles

AFTER GEAR RETRACTION, RED GEAR DOOR LT ON FRONT PANEL WITH NOSE GEAR DOOR LT ON F/E PANEL REMAINED ILLUM. COMPLIED WITH QRH. RECYCLED GEAR NO HELP. RTN TO DEPARTURE. FOUND BULB SEAL ON FWD EDGE OF NOSE WHELL TORN AND FULL OF ICE. BULB WAS SOLID. R & R BULB SEAL, OPS CHECK GOOD ON RETRACTION. AMM 32-33-000-5.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 40,876 hrs · 30,688 cycles

EMERGENCY EXIT LIGHT BY L-1 DOOR IS INOP. R & R EMERGENCY EXIT LIGHT BATTERY PACK (MM 33-50-101-2). OPS CHECKED GOOD. OK TO CONTINUE. PREMATURE REMOVAL/INSTALLATION.

Part: LIGHT — FAILED (CABIN) · airframe 40,868 hrs · 30,683 cycles

CLOSE RT ENTRY DOOR EMERGENCY EXIT LIGHT INOP. R & R SAME IAW MM 33-50-101-2-0. OPS CHECK GOOD, ACFT GOOD FOR CONT SERVICE.

Part: SMOKE DETECTOR — INOPERATIVE (CARGO BAY) · airframe 40,865 hrs · 30,680 cycles

LOWER AFT CARGO SMOKE INDICATION AFTER T/O. DISCH BOTTLE 1 AND FOLLOWED QRH PROCEDURES AND LANDED. AFTER INITIAL INDICATION. ALARM SOUNDED 2 MORE TIMES BEFORE LANDING. RELEASED FOR SERVICE PER MEL: 26-19-C. AFTER BLOCK IN FIRE DEPT CHECKED VISUALLY AND WITH THERMAL GUN, FOUND NO INDICATION OF OVERHEAT. REF AMM 26-17-001-5 SYSTEM TESTS O.K. FINISHED LOWER CARGO BOTTLE INSTALLATION. 3 EACH ELECTRICAL CONNECTOR AND INSTALLED LOCKWIRE, CLOSED UP CARGO BAY REF MM 26-17-014-2. T/S SYS REF MM 26-17-001-1 WITH NO FAULTS. TESTED CARGO FIRE AND SMOKE DETECTION SYS OPS CHECK NORMAL REF MM 26-17-001-5 AND 26-17-001-5 .

Part: ACTUATOR — MALFUNCTIONED (TE FLAPS) · airframe 40,865 hrs · 30,681 cycles

DURING FLAP RETRACTION AMBER L/E FLAP REMAINED ILLUMINATED AT FLAPS 2DEG POSITION. S/O PANEL VERIFIED NR 5 SLAT REMAINED EXTENDED ROLLING MOMENT FELT IN YOKE. RAN QRH NO HELP. LANDED NORMAL MEM NO DUMP REQUIRED. REMOVED AND REPLACED NR 5 LEADING EDGE FLAP PANEL PER AMM 27-81-001-4,OPS CHECK AND GAP CHECK GOOD. ALSO, FOR PRECAUTIONARY REASONS, REMOVED AND REPLACED NR 5 LEADING EDGE FLAP ACTUATOR.OPS CHECK AND LEAK CHECKED GOOD,A/C OK TO CONTINUE.

Part: FRAME — CRACKED (BS 520 S23-24L) · airframe 40,827 hrs · 30,637 cycles

FWD PIT - FRAME UPPER FLANGE HAS DENT AT BS 520 BETWEEN STRINGERS 24L AND 23L. CUT- OUT DAMAGED AREA DIM 1" X .5" IAW SRM 51-10-1, FABRICATED DOUBLER FROM 7075 0 .063" DIM 7" X 4.5" IAW SRM 51-40-3 FIG 1 & INSTALLED REPAIR DOUBLER IAW SRM 51-40-3 FIG 1 REV 103.

Part: RIB — CRACKED (NR 1 INLET) · airframe 40,827 hrs · 30,637 cycles

NR 1 ENGINE INLET COWL INNER SUPPORT BRACKETS ARE CRACKED AT 6 OCLOCK POSITION CUT OUT DAMAGED AREA. FABRICATED FRAME SECTION USING 2024T-3 .063 DIMS 6 5/8" X 2 1/4" AND STRAP REPAIR USING 2024T-3 .071 DIMS 13 1/4" X 1 1/4" AND INSTALLED ALL REPAIR PARTS IAW SRM 54-10-3.

Part: SEAT TRACK — CORRODED (BS 950-950A) · corrosion level 2 · airframe 40,827 hrs · 30,637 cycles

MAIN CARGO CABIN STA 950 10 TO 950A, SEAT TRACK RBL 24 HAS CORROSION. FOUND TO BE OUT OF LIMITS. REMOVED SEAT TRACK SECTION FROM 950 PLUS 10" TO 950D PLUS 10". FABRICATED NEW SEAT TRACK SECTION USING BAC1520-792 7178T6511 DIMS 80", FABRICATED 4 SPLICES USING BAC1503-100122 7178 T6 DIMS 14.5", FABRICATED PLATES USING 7075T6 .250 DIMS 9" EACH AND INSTALLED ALL REPAIR PARTS IAW SRM 53-10-5, 51-10-2 AND 51-30-2.

Part: SKIN — GOUGED (CARGO DOOR) · airframe 40,827 hrs · 30,637 cycles

C-1 DOOR EXT. SKIN IS GOUGED AT FWD LOWER CORNER. CUT OUT DAMAGED AREA OF C-1 DOOR SKIN AT FWD LOWER CORNER (DIM. 9" X 1") IAW SRM 51-10-1. FABRICATED REPAIR DOUBLER FROM 2024 T-3 .080" DIM. 4" X 13.5" AND FILLER FROM 2024 T-3 .071" (DIM. 1" X 9") IAW SRM 52-00-3, FIG 3 AND 52-30-1, FIG 7. INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 51-30-2 REV. 103.

Part: SHEAR TIE — MISINSTALLED (BS 540 S27-28L) · airframe 40,827 hrs · 30,637 cycles

IMPROPER FASTENERS IN SHEAR TIE AT BS 540 BETWEEN S28 AND 27L. CUT OUT DAMAGED SHEAR TIE DIM: 6" X 2 1/4". FABRACATED NEW SHEAR TIE FROM 7075 O .063" DIM. 6" X 2 1/4" AND RADIUS FILLER FROM 7075 T-6 .063" DIM. 6" X 7/8" IAW SRM 53-10-4, FIG 14. INSTALLED SHEAR TIE AND RADIUS FILLER IAW SRM 51-30-2. CUT OUT ORIGINAL SKIN AND DOUBLER DIM. 1 7/8" X 1 3/4". FABRICATED REPAIR DOUBLER FROM 2024 T-3 .080" DIM. 9 3/8" X 10 5/8" AND FILLER FROM 2024 T-3 .063" DIM. 12 1/4" X 6 3/4" AND FILLER FROM 2024 T-3 .050" DIM. 1 7/8" X 1 3/4" IAW SRM 53-30-3 FIG. 1B. INSTALLED DOUBLER AND (2 EA.) FILLERS IAW SRM 51-30-2 REV 103 AND SRM 53-30-3 FIG 1B. REV H.

Part: SKIN — MISINSTALLED (BS 319-344) · airframe 40,827 hrs · 30,637 cycles

FASTENER WITH IMPROPER SPACING STA 344 STR 5L. TRIMMED OUT DAMAGED AREA DIM .750" CYLINDRICAL. FABRICATED 2EA CYLINDRICAL FREEZE PLUGS FROM 2024 T3 .112" AND .76" DIM .750". FABRICATED REPAIR DOUBLER FROM 2024 T3 .090" DIM 501/2" X 201/2". FABRICATED NEW RAIN GUTTER FROM 2024 T3 .040" DIM 57" X 13/4" IAW EA 7-5330-135554. FABRICATED NEW L-1 DOOR SEAL DEPRESSOR FROM 2024 0 .040" DIM 271/2" X 2" IAW SRM 51-20-1 FIG 7. INSTALLED REPAIR DOUBLER, 2EA FREEZE PLUGS, RAIN GUTTER AND SEAL DEPRESSOR IAW EA 7-5330-135554.

Part: FLOORBEAM — CORRODED (BS 720) · corrosion level 2 · airframe 40,827 hrs · 30,637 cycles

CORROSION ON LOWER FLANGE OF FLOORBEAM AT BS 720 AROUND FASTENER HOLES RBL 25 TO LBL 25 CORROSION OUT OF LIMITS. CUT OUT DAMAGED AREA DIMS 2.8" X .9", FABRICATED REPAIR ANGLES USING 2024-O .041 DIMS 14.3" X 2.2" AND 20.5" X 2.4", HEAT TREATED ANGLES TO T6 CONDITION IAW FASI ENG REPORT 2-37153-801 REV A, FABRICATED REPAIR FILLER USING 7075T-6 .125 DIMS 2.8" X .9", INSTALLED REPAIR PARTS IAW SRM 53-10-8, AND 51-10-2.

Part: SHEAR TIE — DAMAGED (BS 480 S27-28L) · airframe 40,827 hrs · 30,637 cycles

UPON REMOVAL OF SHEAR TIE AT BS 480 BETWEEN STR 27L AND 28L FOUND SHEAR TIE DAMAGED. CUT OUT DAMAGED SHEAR TIE DIM 8" X 3" IAW SRM 53-10-4 FIG 15. FABRICATED NEW SHEAR TIE FROM 7075 0 .071" DIM 8" X 3" IAW SRM 53-10-2 FIG 3 AND 53-10-4 FIG 15. INSTALLED NEW SHEAR TIE IAW SRM 51-30-2 AND 53-10-4 FIG 15 REV 103.

Part: SKIN — DAMAGED (BS 480 S27-28L) · airframe 40,827 hrs · 30,637 cycles

IMPROPER SPACING OF FASTENERS IN SKIN AT BS 480 BETWEEN STRINGERS 28L AND 27L. CUT OUT DAMAGED TEARSTRAP DIM 1" X 4" IAW SRM 53-30-4 FIG 6. FABRICATED TEARSTRAP REPAIR FROM 2024 T-3 .063" DIM 13 1/2" X 4 3/4" AND FILLER FROM 2024 T-3 .063" DIM 3 1/2" X 7/8" IAW SRM 53-30-4 FIG 6. INSTALLED TEARSTRAP REPAIR AND FILLER IAW SRM 51-30-2 AND 53-30-4 FIG 6 REV 103.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 40,827 hrs · 30,637 cycles

AFT PIT BS 1183 STR 18L IS CORRODED CUTOUT DAMAGED STRINGER SECTION APPROX DIM: 7 1/4", FABRICATED NEW STRINGER SECTION FROM BAC 1498-144 APPROX DIM: 7 1/4", FABRICATED STRINGER REPAIR SPLICE FROM BAC 1498-132 APPROX DIM: 14 1/2" & INSTALLED REPAIR PARTS AT BS 1183 STR 18L. IAW SRM 53-10-1 FIG 1, SRM 53-10-3 FIG 1, SRM 51-10-2 & SRM 51-30-2.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 40,827 hrs · 30,637 cycles

FLOORBEAM CORRODED STA 440, LBL 25 - LBL 45. CUT-OUT DAMAGED FLOORBEAM SECTION APPROX DIM: 2.6" X .9", FABRICATED REPAIR ANGLES (2 EA) FROM 7075O .090 APPROX DIM: 10.2" X 2.2" & 14.8" X 2.4" HEAT TREATED TO T6 CONDITION, FABRICATED FILLER FROM 7075T6 .125 APPROX DIM: 2.6" X .9". INSTALLED REPAIR PARTS IAW SRM 53-10-8 FIG 8, SRM 51-30-2, SRM 51-10-2, & FAS ER NR 2-37153-801 REV A.

Part: FLOORBEAM — CORRODED (BS 720A) · corrosion level 2 · airframe 40,827 hrs · 30,637 cycles

FLOORBEAM CORRODED STA 720A LBL 25 TO LBL 45. CUTOUT DAMAGED AREA, FABRICATED 2 EA. REPAIR ANGLES, HEAT TREATED TO T6 CONDITION. FABRICATED FILLER AND INSTALLED REPAIR PARTS IAW SRM 53-10-8, FIG 8, SRM 51-10-2, & FAS ER NR 2-37158-801, REV A.

Part: FLOORBEAM — CORRODED (BS 1010) · corrosion level 2 · airframe 40,827 hrs · 30,637 cycles

FLOORBEAM TEE CAP CORRODED STA 1010 LBL 45-60 CORROSION OUT OF LIMITS. CUT OUT DAMAGED AREA DIMS 6.6" X .9", FABRICATED REPAIR ANGLES USING 7075-O .071 DIMS 24.25" X 2.2" AND 28.45" X 2.4", HEAT TREATED PARTS TO T6 CONDITION IAW FASI ENG REPORT 2-37153-801 REV A, FABRICATED REPAIR FILLERS USING 7075T-6 .125 DIMS 8" X .9" AND 6.6" X .9" AND INSTALLED ALL REPAIR PARTS IAW SRM 53-10-8 AND 51-10-2. THIS IS A CATEGORY "B" REPAIR.

Part: SEAT TRACK — CORRODED (100) · corrosion level 2 · airframe 40,827 hrs · 30,637 cycles

SEAT TRACK CORRODED BS 690-740 LBL 45. CORROSION OUT OF LIMITS. REMOVED DAMAGED SEAT TRACK SECTION. FABRICATED NEW SECTION USING BAC1520-792 7178 T6511 DIMS 14' 2" AND INSTALLED REPAIR PARTS IAW SRM 53-10-5 AND 51-10-2.

Part: SEAT TRACK — CORRODED (BS 690-740) · corrosion level 2 · airframe 40,827 hrs · 30,637 cycles

CORROSION ON SEAT TRACK BS 690-740 LBL25 CORROSION OUT OF LIMITS. REMOVED DAMAGED SEAT TRACK SECTION. FABRICATED NEW SECTION USING BAC1520-792 7178 T6511, DIMS 172", FABRICATED ANGLE SPLICES 2 EA USING BAC1503-100122 7178 T6511 DIMS 13.1250" X 2.3750" EACH AND STRAP SPLICE USING 7075T6 .250 DIMS 7.5" X 2" AND INSTALLED REPAIR PARTS IAW SRM 53-10-5 AND 51-10-2.

Part: STRINGER — DAMAGED (BS 620 S27L) · airframe 40,827 hrs · 30,637 cycles

STR 27L AT BS 620 FOUND DAMAGE HOLES DURING HFEC INSPECTION. CUT OUT DAMAGE STRINGER SECTION AT BS 620 STR 27L DIM 15" LONG IAW SRM 51-10-1 AND 53 10-3 FIG 1. FABRICATED STR REPAIR MAT USED BAC 1498-141 7075-T6 DIM 15" LONG AND 2EA SPLICES MAT USED BAC 1498-132, 7075-T6 DIM 13 3/4" AND 14 1/4" LONG IAW SRM 53-10-2 FIG 9 AND 53-10-3 FIG1. TREATED AND PRIMED IAW SRM 51-10-2, INSTALLED STRINGER AND SPLICES IAW SRM 51-30-2 REV. 103.

Part: SEAT TRACK — CORRODED (BS 480-690) · corrosion level 2 · airframe 40,827 hrs · 30,637 cycles

SEAT TRACK CORRODED BS 540 LBL 45. CORROSION OUT OF LIMITS. REMOVED DAMAGED SEAT TRACK SECTION. FABRICATED NEW SECTION USING BAC1520-792 7178 T6511 DIMS 17' 6", FABRICATED ANGLE SPLICES 2 EA USING BAC1503-100122 7178-4811 DIMS 15.5" EA AND STRAP SPLICE USING 7075T6 .250 DIMS 9" X 2" AND INSTALLED REPAIR PARTS IAW SRM 53-10-5 AND 51-10-2.

Part: SKIN — DAMAGED (BS 480 S27L) · airframe 40,827 hrs · 30,637 cycles

FASTENER WITH DOUBLE DRILLED HOLE IN MCD DOUBLER STA 480, STR 27L. CUT OUT DAMAGE ON MCD DOUBLER (DIM. 21 1/4" X 1 3/4") AND SKIN (DIM. 5 5/8" X 2 1/4") IAW SRM 53-30-3, FIG 1B. FABRICATED STRUCTURAL FILLER FROM 2024 T-3 .063" DIM. 59 1/4" X 24 1/2" AND DOUBLER FROM 2024 T-3 .080" DIM. 57 1/4" X 29" AND 2 EA. FILLERS FROM 2024 T-3 .080" DIM 22 1/4" X 1 7/8" AND 5 1/2" X 1 1/4" IAW SRM 53-30-3, FIG 1B. INSTALLED STRUCTURAL FILLER, DOUBLER AND 2 EA. FILLERS IAW SRM 53- 30-3 FIG 1B, REV J AND SRM 51-30-2, REV 103.

Part: STRINGER — CORRODED (BS 720F S27R) · airframe 40,827 hrs · 30,637 cycles

CORROSION ON UPPER FLANGE OF STRINGER 27R AT BS 720F. REMOVED STR 27R AT BS 720F TO 740 IAW B727 SRM 53-10-5 FIG 1. FABRICATED STRINGER SECTION FROM BAC 1498-147 7075 T6 DIM: 26.75" AND 2EA SPLICES FROM BAC 1498-131 7075 T6 DIM" 9" AND 13.5" IAW B727 SRM 53-10-2, 53-10-3 FIG 1 AND 53-30-5. INSTALLED STRINGER SECTION AND 2EA SPLICES IAW B727 SRM 51-30-2 REV 103.

Part: SHEAR TIE — CORRODED (BS 720D S25-26R) · corrosion level 2 · airframe 40,827 hrs · 30,637 cycles

CORROSION ON SHEAR TIE AT BS 720D (FWD SIDE) BETWEEN STRINGER 26R AND 25R. REMOVED SHEAR TIE CLIP AT BS 720D BETWEEN STR 26R-25R IAW SRM 51-30-2. FABRICATE NEW CLIP FROM 7075-T6 .063" DIM: 5.25"X1.75" IAW DRAWING 69-43668, SRM 51-20-1, FIG 7 AND 51-30-5. INSTALLED NEW SHEAR TIE CLIP IAW SRM 51-30-2 REV 103.

Part: STRINGER — CORRODED (BS 685 S27L) · corrosion level 2 · airframe 40,827 hrs · 30,637 cycles

FUSELAGE SKIN HAS CORROSION BULGE AT BS 685 S27L. CUT OUT DAMAGED STRINGER 27L BETWEEN BS 680 - 700, DIM. 10" LONG IAW SRM 53-10-3, FIG. 1. FABRICATED STRINGER SECTION FROM BAC1498-143 7075-T62 DIM. 10" LONG AND NEW SPLICE FROM BAC 1498-131 7075-T62 DIM. 11 3/4" LONG IAW SRM 53-10-3, FIG. 1, DETAIL I. INSTALLED NEW STRINGER SECTION AND SPLICE IAW SRM 51-30-2 AND 53-10-3, FIG. 1.

Part: STRINGER — CORRODED (BS 1166-1183) · corrosion level 2 · airframe 40,827 hrs · 30,637 cycles

CORROSION ON TENSION TIE BETWEEN STA 1166 AND 1183 STR 19L CUTOUT DAMAGED STRINGER SECTION APPROX DIM: 7", FABRICATED NEW STRINGER SECTION FROM BAC 1498-144 APPROX DIM: 7", FABRICATED SPLICE FROM BAC 1498-132 APPROX DIM: 14 1/2". INSTALLED STRINGER REPAIR PARTS IAW SRM 53-10-3 FIG 1, SRM 51-10-2, & SRM 51-30-2.

Part: SHEAR TIE — CORRODED (BS 1183 S18L) · corrosion level 2 · airframe 40,827 hrs · 30,637 cycles

CORROSION ON SHEAR TIE STA 1183 STR 18L REMOVED DAMAGED TENSION TIE AT BS 1183 STR 18L, FABRICATED NEW TENSION TIE FROM 2024T3 APPROX DIM: 6" X 3 1/2" & INSTALLED NEW TENSION TIE AT BS 1183 STR 18L IAW SRM 53-10-1 FIG 1, SRM 51-30-5 & SRM 51-10-2, & DWG. 65-24276.

Part: SHEAR TIE — MISINSTALLED (BS 620 S27-28L) · airframe 40,827 hrs · 30,637 cycles

IMPROPER SPACING OF FASTENERS IN SHEAR TIE AT BS 620 BETWEEN STRINGERS 27L AND 28L. CUT OUT DAMAGED SHEAR TIE IAW SRM 53-10-4 FIG 15. CUT OUT DAMAGED SECTION OF SKIN AND DOUBLER DIM" 2" X 1" IAW SRM 53-30-3 FIG 1B. FABRICATED NEW SHEAR TIE FROM 7075 0 .063" DIM" 6" X 2" IAW SRM 53-10-4 FIG 15 AND DRAWING 65-17663. FABRICATED SKIN DOUBLER FROM 2024 T3 .080" DIM: 12" X 11 5/8" AND FILLER FROM 2024 T3 .063" DIM: 13" X 9" IAW SRM 53-30-3 FIG 1B. INSTALLED SHEAR TIE, DOUBLER AND FILLER IAW SRM 53-10-4 FIG 15 REV 103 AND SRM 53-30-3 FIG 1B REV H.

Part: SEAT TRACK — CORRODED (BS 600-740) · corrosion level 2 · airframe 40,827 hrs · 30,637 cycles

SEAT TRACK CORRODED STA 720A PLUS 10" BL0. REMOVED (2EA) SEAT TRACK SECTIONS FROM BS 600-720A AND 720A-740 IAW SRM 51-30-2. LOCATED AND DRILLED (2EA) SEAT TRACKS SECTIONS MATERIAL IAW SRM 53-10-2 FIG 7A REV D AND 51-30-5. INSTALLED (2EA) SEAT TRACK SECTIONS IAW SRM 51-30-2 REV 103.

Part: SHEAR TIE — MISINSTALLED (BS 640 S27-28L) · airframe 40,827 hrs · 30,637 cycles

IMPROPER SPACING OF FASTENERS IN SHEAR TIE AT BS 640 BETWEEN STRINGERS 28L AND 27L. CUT OUT DAMAGED SHEAR TIE IAW SRM 53-10-4 FIG 15. CUT OUT ORIGINAL SKIN AND MCD DOUBLER DIM: 1 1/2" X 1" IAW SRM 53-30-3 FIG 1B. FABRICATED SHEAR TIE FROM 7075 0 .063" DIM: 6" X 2" IAW SRM 53-10-4 FIG 15 AND DRAWING 65-17663. FABRICATED SKIN DOUBLER FROM 2024 T3 .080" DIM: 12 1/2" X 12 1/4" AND FILLER FROM 2024 T3 .063" DIM" 13 1/2" X 8 5/8" IAW SRM 53-30-3 FIG 1B. INSTALLED SHEAR TIE, SKIN DOUBLER AND FILLER IAW SRM 53-10-4 FIG 15 REV 103 AND SRM 53-10-3 FIG 1B REV H.

Part: SEAT TRACK — CORRODED (BS 690-720D) · corrosion level 2 · airframe 40,827 hrs · 30,637 cycles

SEAT TRACK CORRODED STA 690-720D BL0. REMOVED (2EA) SEAT TRACK SECTIONS FROM BS 600-720A AND BS 720A-740 IAW SRM 51-30-2. LOCATED AND DRILLED (2EA) SEAT TRACKS SECTIONS MATERIAL USED BAC 1520-792 7178 T6511DIM 120" AND 141 1/2" IAW P-F SRM 53-10-2 AND SRM 51-30-5. INSTALLED (2EA) SEAT TRACK SECTIONS IAW SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 950-1110) · corrosion level 2 · airframe 40,827 hrs · 30,637 cycles

SEAT TRACK CORRODED STA 950F-1110 LBL 45 REMOVED CORRODED SEAT TRACK AT LBL 45 FROM BS 950 TO 1130 IAW SRM 51-30-2. LOCATED AND DRILLED NEW SEAT TRACK SECTION. FABRICATED NEW SPLICE ANGLES (2EA) AND PLATE IAW SRM 53-10-5 FIG 1 AND 53-30-5. INSTALLED NEW SEAT TRACK AND SPLICES IAW SRM 51-30-2 AND 53-10-5 FIG 1 REV 103.

Part: TORQUE BOX — CRACKED (ZONE 100) · airframe 40,827 hrs · 30,637 cycles

AFT AIRSTAIRS, RT LOWER TORQUE BOX INNER WEB HAS CRACK AT UPPER FASTENER ROW AT BS 1236. CUT OUT DAMAGED AREA DIMS 3/4" X 2 1/4". FABRICATED REPAIR DOUBLER USING 7075T-6 .032 DIMS 2 1/2" X 5 1/2" AND FILLER USING 7075T-6 .025 DIMS 3/4" X 2 1/4" AND INSTALLED SRM 51- 30-2, 53-10-2 AND 51-40-2.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 40,827 hrs · 30,637 cycles

SEAT TRACK CORRODED STA 950C-1030 BL0 CORROSION OUT OF LIMITS. REMOVED DAMAGED SEAT TRACK SECTION. FABRICATED NEW SECTION USING BAC1520-792-7178T6511 DIMS 289 1/4", SPLICE USING BAC1503-100122 7178-4811 DIMS 14" X 2" AND PLATE USING 7075T-6 .250 DIMS 7" X 2" AND INSTALLED IAW SRM 53-10-2 AND 53-10-5.

Part: TORQUE BOX — CRACKED (AIRSTAIR) · airframe 40,827 hrs · 30,637 cycles

AFT AIRSTAIR, LT LOWER TORQUE BOX INNER WEB LIGHTING HOLE IS CRACKED AT BS 1223. CUT OUT DAMAGED AREA DIMS 3/4" X 3/4". FABRICATED REPAIR DOUBLER USING 7075T-6 .032 DIMS 2" X 7" AND INSTALLED IAW SRM 51-30-2, 53-10-2 AND 51-40-2.

Part: SEAT TRACK — CORRODED (BS 950-950A) · corrosion level 2 · airframe 40,827 hrs · 30,637 cycles

SEAT TRACK CORRODED STA 950-950A RBL 45 CORROSION OUT OF LIMITS. REMOVED SEAT TRACK SECTION, LOCATED AND DRILLED NEW SEAT TRACK SECTION, FABRICATED NEW SPLICE ANGLES AND STRAP SPLICE AND INSTALLED ALL REPAIR PARTS IAW SRM 53-10-2, 51-30-5, AND 51-30-2.

Part: SKIN — GOUGED (BS 620 S3L) · airframe 40,827 hrs · 30,637 cycles

GOUGE MCD INNER DOUBLER STA 620 STR 3L. DAMAGE OUT OF LIMITS. FABRICATED NEW INNER DOUBLER USING 2024T-3 .125 DIMS 79" X 48" AND INSTALLED IAW SRM 51-30-2 AND DWG 53FX1551 REV D AND DWG 53FX2022 REV C.

Part: SEAT TRACK — CORRODED (BS 870-950) · corrosion level 2 · airframe 40,827 hrs · 30,637 cycles

SEAT TRACK CORRODED STA 870-950 RBL 25 CORROSION OUT OF LIMITS. REMOVED DAMAGED SEAT TRACK SECTION. FABRICATED NEW SECTION USING BAC1520-792-7178 T6511 DIMS 91", FABRICATED NEW SPLICES USING BAC1503-100122 7178 DIMS 14" AND STRAP USING 7075T-6 .250 DIMS 9" X 2" AND INSTALLED ALL REPAIR PARTS IAW SRM 53-10-2 AND 53-10-5.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 40,827 hrs · 30,637 cycles

SEAT TRACK CORRODED STA 580-690 RBL 25. CORROSION OUT OF LIMITS. REMOVED SEAT TRACK SECTION, FABRICATED NEW SECTION USING BAC1520-792-7178-T6511 DIMS 219 1/2" X 3 3/8", FABRICATED 2 ANGLE SPLICES USING BAC1503-100122 7178 T6511 DIMS 13 1/2" X 2 3/8" EACH, FABRICATED STRAP SPLICE USING 7075T6 .250 DIMS 9 1/4" X 2 1/8" AND INSTALLED ALL REPAIR PARTS IAW SRM 53-10-5, 51-10-2 AND 51-30-2.

Part: SEAT TRACK — CORRODED (BS 480-580) · corrosion level 2 · airframe 40,827 hrs · 30,637 cycles

SEAT TRACK CORRODED STA 480-580 BL0. REMOVED SEAT TRACK SECTION BL0 BETWEEN STA 480-600 IAW SRM 51-30-2. LOCATED AND DRILLED NEW SEAT TRACK SECTION IAW SRM 53-10-2 FIG 7A REV D AND 51-30-5. INSTALLED SEAT TRACK SECTION IAW SRM 51-30-2 REV 103.

Part: FLOORBEAM — CORRODED (BS 950) · corrosion level 2 · airframe 40,827 hrs · 30,637 cycles

MAIN CARGO DECK STA 950 RBL 24 FLOORBEAM TEE CORRODED. CORROSION OUT OF LIMITS. REMOVED TEE FROM LBL 63 TO RBL 63. FABRICATED NEW TEE USING BAC1505-100405 7075T6 DIMS 127 3/8" IAW DWG 65-16338 AND INSTALLED IAW SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 600-620) · corrosion level 2 · airframe 40,827 hrs · 30,637 cycles

SEAT TRACK CORRODED STA 600-620 LBL 25 CORROSION OUT OF LIMITS. REMOVED DAMAGED SEAT TRACK SECTION. FABRICATED NEW SECTION USING BAC1520-792 7178 T6511 DIMS 209 1/2", AND INSTALLED REPAIR PARTS IAW SRM 53-10-5 AND 51-10-2.

Part: STRINGER — CORRODED (BS 485 S28L) · corrosion level 2 · airframe 40,827 hrs · 30,637 cycles

CORROSION ON STRINGER 28L AT SPLICE BS 485. CUT OUT DAMAGED SECTION OF STRINGER DIM 24 7/8" LONG IAW SRM 51-10-1. FABRICATED NEW STRINGER HAT SECTION FROM BAC1498-138 7075 T-6 DIM 24 7/8" LONG AND 2EA ANGLES FROM BAC1493-513 7075 T-6 DIM 11 1/2" LONG AND 1EA CHANNEL FROM BAC1493-412 7075 T-6 DIM 12 1/8" LONG IAW SRM 53-10-2 FIG 9 AND 53-10-3 FIG 1. INSTALLED NEW STRINGER, 2EA ANGLES AND 1EA CHANNEL IAW SRM 51-30-2 AND 53-10-3 FIG1 REV 103.

Part: SEAT TRACK — CORRODED (BS 720B-720E) · corrosion level 2 · airframe 40,827 hrs · 30,637 cycles

SEAT TRACK CORRODED STA 720B-720E RBL 45 REMOVED SEAT TRACK SECTION FROM BS 690 TO 740 IAW SRM 51-30-2. FABRICATED NEW SEAT TRACK SECTION FROM BAC 1520-792 7178- T6511 DIM: 172" IAW SRM 53-10-5 FIG 1. INSTALLED NEW SEAT TRACK SECTION AND SPLICES IAW B727 SRM 51-30-2 REV 103.

Part: SEAT TRACK — CORRODED (BS 500-690) · corrosion level 2 · airframe 40,827 hrs · 30,637 cycles

SEAT TRACK CORRODED STA 500-690 RBL 45 REMOVED SEAT TRACK SECTION AND SPLICE FROM BS 480 TO BS 680, RBL 45 IAW SRM 51-30-2. FABRICATED NEW SEAT TRACK SECTION FROM BAC 1520-792 7178-T6511 DIM: 209 1/2". FABRICATED NEW SPLICE ANGLES FROM BAC 1503-100122 7178-T6511 DIM: (2EA) 13" AND STRAP FROM 7075-T6 .250" DIM: 7 1/8" X 2 1/8" IAW SRM 53-10-5 FIG 1. INSTALLED SEAT TRACK AND SPLICES IAW SRM 51-30-2 REV 103.

Part: SKIN — GOUGED (BS 950-950D) · airframe 40,827 hrs · 30,637 cycles

PREVIOUS REPAIR AT STA 950-950D STR 28L-30 HAS DEEP GOUGES AND FASTENERS WITH NO EDGE DISTANCE. REMOVED PREVIOUS REPAIR. FABRICATED NEW REPAIR DOUBLER USING 2024T-3 .190 DIMS 66 1/4" X 13", AND FILLER USING 2024T-3 .190 MACHINED DOWN TO .180 DIMS 60 7/8" X 4 3/4" AND INSTALLED REPAIR PARTS IAW EA 7-5330-135553.

Part: FITTING — DAMAGED (LT WING) · airframe 40,827 hrs · 30,637 cycles

LOOSE AND MISSING SCREWS BOTTOM AFT FALSE SPAR CHORD LEFT WING AT NR 7 SPOILER FITTING CUT OUT DAMAGED WEB SECTION. TRIMMED LOWER CHORD DAMAGE. FABRICATED NEW WEB SECTION, NEW LOWER SPAR, & 2 ANGLES. HEAT TREATED PARTS IAW FASI ENG REPORT 2-37153-801 REV A, FABRICATED STRAP, 2 RADIUS FILLERS, DOUBLER AND INSTALLED ALL REPAIR PARTS IAW DWG SR-57-038 REV C.

Part: WEB — DAMAGED (RT WING) · airframe 40,827 hrs · 30,637 cycles

LOOSE AND MISSING SCREWS BOTTOM AFT FALSE SPAR CHORD RIGHT WING AT NR 8 SPOILER FITTING CUT OUT DAMAGED WEB SECTION. TRIMMED LOWER CHORD DAMAGE. FABRICATED NEW WEB SECTION, NEW LOWER CHORD, & 2 ANGLES. HEAT TREATED PARTS IAW FASI ENG REPORT 2-37153-801 REV A, FABRICATED STRAP, 2 RADIUS FILLERS, & DOUBLER. FABRICATED WEB REPAIR AND INSTALLED ALL REPAIR PARTS IAW DWG SR-57-038 REV C.

Part: SKIN — CORRODED (BS 1070 S28L) · corrosion level 2 · airframe 40,827 hrs · 30,637 cycles

SKIN BULGE STA 1070 STR 28L CORROSION OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED STRINGER REPAIR USING BAC1498-145 7075T6 DIMS 19 3/4", 2 SPLICES USING BAC1498-131 7075T6 DIMS 14" EACH, FABRICATED DOUBLER USING 2024T3 .063 DIMS 41 1/8" X 17 1/2", 2 FILLERS USING 2024T3 .050 DIMS 5 7/8" X 1" AND 4 7/8" X 1" AND INSTALLED ALL REPAIR PARTS IAW SRM 53-10-3, 53-30-3 AND 51-30-2.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,357 hrs · 29,437 cycles

MAIN DECK FLOOR SHEAR WEB IS CORRODED/MISDRILLED, BS 1130-1177, RBL 16-64, WL 208. REMOVED CORRODED/MISDRILLED RT SHEAR WEB. RECEIVED NEW SHEAR WEB, DRILLED AND INSTALLED. REFERENCE SRM 51-30-2/PAGE NR 2 CLASSIFIED AS A MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 39,357 hrs · 29,437 cycles

MAIN DECK FLOOR SUPPORT, BS 1166 - 1177, RBL 45, UPPER SURFACE HAS CORROSION AND VERTICAL FLANGE IS GOUGED. REMOVAL AND INSTALLATION OF FLOOR SUPPORT BETWEEN STA 1166 - 1177/RBL 45 IS ON SNRM NR N00493/JPF LINE ITEM NR 178 AND 179. FABRICATED FLOOR SUPPORT AND FLOOR SUPPORT FILLERS, LOCATED HOLES, TREATED AND PRIMED ALL PARTS. REFERENCE FED EX DRAWING 53FX939/ITEM NR -136, -38 AND -40. CLASSIFIED AS A MINOR REPAIR.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 39,357 hrs · 29,437 cycles

MAIN DECK, SEAT TRACK I/B FLANGE CORRODED, BS; 1110 - 1130, RBL 45 REMOVED CORROSION AND SEAT TRACK IS OUT OF LIMITS. FABRICATED NEW SEAT TRACK, DRILLED, TREATED AND PRIMED AND INSTALLED. REFERENCE BOEING DOCUMENT NR 65-86245/ID 000 FRAME NR 2 SRM 51-10-2/PAGE 2 AND SRM 51-30-2/ PAGE 2. CLASSIFIED AS A MINOR REPAIR.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 39,357 hrs · 29,437 cycles

AFT CABIN SEAT TRACK, (STA 1130 - 1168) RBL 45 IS CORRODED REMOVAL AND INSTALLATION OF RBL 45 SEAT TRACK FROM STA 1130 - 1177 IS ON SNRM NR N00493/JPF LINE ITEM NR 66 AND 67. FABRICATION OF SEAT TRACK IS ON SNRM NR N00839. DRILLED, TREATED AND PRIMED SEAT TRACK. REFERENCE FED EX DRAWING NR 53-FX939 AND SNRM NR N00839. CLASSIFIED AS A MINOR REPAIR.

Part: FLOORBEAM — DAMAGED (ZONE 200) · airframe 39,357 hrs · 29,437 cycles

MAIN DECK FLOORBEAM UPPER FLG IS DAMAGED BS 1148, RBL 43-49 , WL 208. REMOVED SURROUNDING STRUCTURE, REMOVED UPPER T-CAP, PREFORMED 10X VISUAL INSPECTION OF TRIMMED TREATED, PRIMED AREA. FABRICATED SURROUNDING STRUCTURE. REF SRM 51-30-2 PG 2. SRM 53-10-08 FIG 3, AND EA 7-5310-118248, CLASSIFIED AS A MAJOR REPAIR.

Part: FLOORBEAM — DAMAGED (ZONE 200) · airframe 39,357 hrs · 29,437 cycles

MAIN DECK FLOORBEAM BS 1166, RBL 44-50, WEB HAS SEVERAL DOUBLE DRILLED HOLES. REMOVED AND REPLACED. FABRICATED REPAIR PARTS AT LT AND RT FUEL SHROUD CUT OUTS AND INSTALLED. REFERENCE EA 7-5310-113796. CLASSIFIED AS A MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,357 hrs · 29,437 cycles

MAIN DECK FLOOR SEAT TRACK, BS 1124 - 1125, LBL 45 - 46, HAS CORROSION AROUND FASTENER HOLE, UPPER AND LOWER SURFACE. REMOVED AND REPLACED SEAT TRACK, IAW SRM 53-10-5. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 39,357 hrs · 29,437 cycles

MAIN DECK FLOORBEAM UPPER CAP LOWER SURFACE IS CORRODED NUTPLATE BS 1130, LBL 28-38. COMPLIED WITH EA 7-5310-113971 PART 1. CLASSIFIED AS A MAJOR REPAIR.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,357 hrs · 29,437 cycles

MAIN BODY FRAME ASSY CORRODED, BS 1166, STR 17L, WL 208. REMOVED CORROSION FROM BS 1166, S17L FRAME AND FOUND TO BE OUT OF LIMITS, REMOVED FRAME AND INSTALLED. REFERENCE SRM 51-30-2. CLASSIFIED AS MAJOR REAIR

Part: FRAME — CORRODED (WG TO BDY PANEL) · corrosion level 2 · airframe 39,357 hrs · 29,437 cycles

BODY TO WING FAIRING PANEL, NR 3218 BETWEEN PRIMARY HEAT EXCHANGER RT O/B FRAME WEB HAS CORROSION ON MATING SURFACE AT FS 825, RBL WL 138. RT O/B FRAME WEB FOUND TO HAVE 50 PERCENT MATERIAL LOSS, OUT OF LIMITS REF SRM 51-10-01. REMOVED AND REPLACED FRAME WEB REF SRM 51-30-2, THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: BULKHEAD — CHAFED (ZONE 100) · airframe 39,357 hrs · 29,437 cycles

NOSE W/W BS 351 BULKHEAD RBL 6", SKIN IS WORN FROM CONTACT WITH HYD HOSE CLAMP. BLENDED DAMAGE AREA AT NOSE W/W BS 351 BULKHEAD RBL 6. SKIN REF SRM 53-10-1 FIG 1, MEASURED THICKNESS, ORIGINAL "T" .073", MATERIAL REMAINING .058", FOUND TO BE WITHIN LIMITS REF EA NR 7-5310-113972. TREATED AND PRIMED AND PAINTED AREA REF SRM 51-10-2, THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,357 hrs · 29,437 cycles

CORROSION AND CRACK ON SIDEWALL "T" FRAME SUPPORT STA 1030 TO 1050, LT LOWER AFT PIT. REMOVED CORROSION ON "T' FRAME SUPPORT. REMOVED .022 INCH FROM ORIGINAL THICKNESS OF .065", REMAINING .043 INCH IS OUT OF LIMITS PER SRM 53-10-1 FIG 1. RECEIVED NEW PART, FABRICATED AND HEAT TREAT REF N/R N00866. DRILLED NEW PART REF. TREATED AND PRIMED REF SRM 51-10-2. INSTALLED NEW PART NUMBER FX 65-67247-51. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: ATTACH ANGLE — CRACKED (ZONE 200) · airframe 39,357 hrs · 29,437 cycles

INTERCOSTAL LOWER ATTACH ANGLE HAS ELONGATED HOLES, CRACK AND CORRODED AT 1110 TO FS 1130, BL 0. FABRICATED INTERCOSTAL LOWER ATTACH ANGLE AT FS 110 TO FS 1130 BL 0", REF DWG 69-4569. THIS IS CLASSIFIED AS A MINOR REPAIR

Part: ANGLE — CRACKED (ZONE 200) · airframe 39,357 hrs · 29,437 cycles

MAIN DECK FLOOR DITCH PAN ASSY FWD AND AFT CHORD ANGLES ARE CRACKED, BS 1177 - 1183, RBL 47-64", WL 208. REMOVED RT DITCHING PAN ASSY. FABRICATED ANGLES WITH PART NR`S 65-29548-11 AND 65-29548-55. FABRICATED AND HEAT ATTACH ANGLES (SHOP NR N00880/8130 FORM TRACKING NR 2008-02-231) PART NR 65-29548-18 AND INSTALLED DITCHING PAN ASSY REF BOEING DOCUMENT NR 65-29548. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: DEPRESSOR — CRACKED (CARGO DOOR) · airframe 39,357 hrs · 29,437 cycles

C2 DOOR AFT SEAL DEPRESSOR, 22 INCHES FROM UPPER CORNER IS CRACKED. REPLACED AFT SEAL DEPRESSOR REF SRM 51-30-02. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: DEPRESSOR — CRACKED (CARGO DOOR) · airframe 39,357 hrs · 29,437 cycles

C2 DOOR FWD SEAL DEPRESSOR, 22 INCHES FROM TOP CORNER IS CRACKED. REPLACED FWD SEAL DEPRESSOR REF SRM 51-30-2. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: SKIN — DAMAGED (ZONE 100) · airframe 39,357 hrs · 29,437 cycles

AFT FUSELAGE BS 1166 BETWEEN S19L S20L, FRAME AND SKIN HAVE OVER SIZED HOLE (APPROX 3/8 DIA.) NDT TO VERIFY MATERIAL THICKNESS .050". REMOVED DAMAGE ON SKIN. FABRICATED REPAIR DOUBLER AND FILLER 2024-T3 .063" A87331/P0 NR 1032671. OVERSIZED LAP SEAM HOLES AND NDT FOR 0 TIME, NO DEFECT FOUND. TREATED AND PRIMED REPAIR DOUBLER AND FILLER. INSTALLED DOUBLER AND FILLER. SEALED EDGES AND RESTORED FINISHES. REF SRM 53-30-2, SRM 51-10-1, SRM 51-10-2. THIS IS CLASSIFIED AS A MAJOR REPAIR CATEGORY "B" REPAIR.

Part: SUPPORT — CORRODED · airframe 39,357 hrs · 29,437 cycles

PANEL "T" SUPPORT BRACKET HAS CORROSION, BETWEEN LEFT AND RIGHT RAM AIR FIBERGLASS DUCTS, BETWEEN STA 720E AND 720F, LEFT SIDE. REMOVED PANELS FOR ACCESS, REMOVED "T" SUPPORT, REMOVED CORROSION, NDT FOR MATERIAL LOSS ORIG .058'", REMAINING .053' INCH, WITHIN LIMITS. TREAT AND PRIMED AND PAINTED "T" SUPPORT. INSTALL "T" SUPPORT AND PANELS REMOVED. REF SRM 53-10-1, 51-102, 51-30-2, MM51-20-151-7 51-10-6, THIS IS CLASSIFIED AS A MINOR REPAIR LEVEL 1 CORROSION.

Part: ANGLE — CRACKED (ZONE 100) · airframe 39,357 hrs · 29,437 cycles

MAIN DECK FLOOR DITCH PAN ASSY FWD AND AFT CHORD ANGLES ARE CRACKED BS 1177 - 1883, LBL 47 -64, WL 208. REPLACED FWD AND AFT CHORD ANGLES IAW DWG 65-29548. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: SKIN — DAMAGED (ZONE 100) · airframe 39,357 hrs · 29,437 cycles

FOUND FUSELAGE SKIN CORROSION AT FS 582, STR 28L, AFTER REMOVING WEB ON SNRM N00557 FOUND SERIES OF MISDRILLED HOLES ALONG INTERCOSTAL NEAR BOTTON EDGE OF MAIN CARGO DOOR DOUBLER COMPLIED WITH EA NR 7-5330-118244 PART NR 1. REMOVED INTERNAL STRUCTURE TO GAIN ACCESS. REMOVED DAMAGE AND CORROSION, FABRICATED REPAIR DOUBLER/FILLERS. TREATED PRIMED AND INSTALLED, REF SRM 53-30-3. THIS IS CLASSIFIED AS A MAJOR REPAIR.

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,357 hrs · 29,437 cycles

VERTICAL WEB AT FS 580 - 600, LBL 15 IS CORRODED REPLACED WEB AT STA 580 - 600, LBL 15 WITH NEW WEN REF SRM 51-30-2. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: THRESHOLD — CRACKED (ZONE 100) · airframe 39,357 hrs · 29,437 cycles

SEVERAL CRACKS AND DENTS IN THRESHOLD PLATE, FWD LOWER CARGO COMPT. THRESHOLD PLATED REPAIRED ON SHOP N/R N00123. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,357 hrs · 29,437 cycles

AFT LWR CARGO BAY AT BS 950D BETWEEN STR S-29L AND S-28L, AFT SURFACE OF FRAME AND LWR SURFACE OF LWR CHORD HAVE CORROSION REMOVED FASTENERS FROM STA 950D STR 28L - 30L, BLENDED CORROSION, ORIGINAL MATERIAL .071". REMAINING MATERIAL .058 INCH, MATERIAL REMOVED .031", OUT OF LIMITS, SRM 53-10-1 PG 2, TOOL ID NR IN22-0029, CAL DUE DATE 09/28/08. REMOVED STRINGER CLIPS FROM STR 28L - 30, STR 28L -30. FABRICATED NEW SHEAR TIE, SUPPORT ANGLE AND SUPPORT CHANNEL, MEASURED MATERIAL FOR FAIL/SAFE, ORIGINAL MATERIAL .071" REMAINING MATERIAL .067, LOSS OF .004. WITHIN LIMITS REF SRM 53-10-1 PG2. FABRICATED DOUBLER, TREATED AND PRIMED AND INSTALLED REF SRM 51-10-2, SRM 51-30-2, SRM 53-10-4, BOEING DWG 69-44109.

Part: FLOORBEAM — CORRODED (BS 1110) · corrosion level 2 · airframe 39,357 hrs · 29,437 cycles

MAIN DECK FLOORBEAM UPPER FLAG IS CORRODED/MISDRILLED BS 1110, LBL 27-34, WL 208. REMOVED CORROSION BS 1110, LBL 27 - LBL 31, MAT. THICK .125". REMOVED .116", REMAINING .009" OUT OF LIMITS REF 727-PF SRM 53-10-1 PG 25-41. AAR TOOL 18172, CAL DATE DUE 10/15/08. REMOVED DAMAGE AREA. FABRICATED TWO REPAIR ANGLE REF FED EX DWG SR 27-53-034 SHT 2 REPAIR NR 2. MAT ID 17-7PH-.090 A49316. P/O 102446. FAB`D FILLER MAT ID 7075-76 .125". HEAT TREATED REPAIR ANGLES 8130 NR 417102. CAD PLATED, DRILLED AND TRIMMED ALODINED AND PRIMED ANGLES. PAINTED FILLERS AND ANGLES REF SRM 51-10-2. INSTALLED REPAIR REF DWG SR27-53-036. THIS IS CLASSIFIED AS A MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,357 hrs · 29,437 cycles

AFT LWR CARGO BAY BS 1164 - 1166 FLOOR SUPPORT ANGLE AT LBL 11 HAS CORROSION ON UNDERSIDE. REMOVED DAMAGE AND FABED CHANNEL AND SPLICE REPAIR AT STA 1144 TO 1166. APPLIED ALODINE, PRIMER AND PAINT. INSTALLED NEW CHANNEL AND SPLICE, REF SRM 51-10-06, 53-10-05, 51-10-02. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: FRAME — DAMAGED (BS 600) · airframe 39,357 hrs · 29,437 cycles

FRAME SHEAR TIE AT FS 600 LBL 12 HAS MISDRILLED HOLES FROM PREVIOUS WORKMANSHIP REMOVED DAMAGED SHEARTIE REF SRM 53-10-4. FABRICATED NEW ANGLE REF SRM 53-10-4, TOP COAT ANGLE REF SRM 51-10-2 MM 51-20-151-7. INSTALLED ANGLE TIE REF SRM 53-10-4 FIG 15. THIS IS CLASSIFIED AS A MAJOR REPAIR.

Part: FAIRING — CRACKED (ZONE 600) · airframe 39,357 hrs · 29,437 cycles

RT WING O/B JACKSCREW TOP WING PANEL BRACKET CRACKED AT AFT I/B SIDE OF FAIRING. REMOVED FAIRING, REMOVED AND REPLACED DOUBLER ON FAIRING REF SRM 51-30-. REINSTALLED FAIRING REF SRM 51-30-2. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: STRINGER — CORRODED (ZONE 100) · airframe 39,357 hrs · 29,437 cycles

FWD PIT FLOORBOARD SUPPORT STRG AT (STA 645) RBL 12 IS CORRODED (MARKED ) REMOVED DAMAGED AT STA 645 AND FABED A REPAIR. APPLIED ALODINE, PRIMER AND PAINT. REINSTALLED FLOOR SUPPORT AND INSTALLED SPLICE AT STA 670. APPLIED ALODINE, PRIME AND PAINT, REF SRM 53-10-1 FIG 1. CLASSIFIED AS A MINOR REPAIR.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,357 hrs · 29,437 cycles

FWD LOWER CARGO COMPT FRAME TIE AT STA 580 LBL 20 CORRODED AT END VERIFIED MATERIAL FOR REPLACEMENT FRAME TIE REF DWG 69-14871 .050 7075 T-6. FABRICATED NEW FRAME TIE REF DWG 69-14871. TREATED PRIMED REF SRM 51-10-2. INSTALLED NEW FRAME TIE REF SRM 51-30-2, CLASSIFIED AS A MAJOR REPAIR.

Part: CHANNEL — CORRODED (ZONE 100) · airframe 39,357 hrs · 29,437 cycles

AFT LWR CARGO BAY CENTER LINE FLOOR ANGLE AT BS 1035-1037 HAS CORROSION ON THE UNDERSIDE VERFIED MATERIAL FOR REPAIR PARTS. FABRICATED REPAIR PARTS REF SRM 53-10-5, DWG SR27-53-039. REMOVED CORROSION, FOUND TO WITHIN LIMITS REF SRM 53-10-1 FIG 4. TREATED PRIMED REPAIR PARTS REF SRM 51-10-2 MM 51-20-151-7. INSTALLED REPAIR SPLICE ANGLES REF SRM 53-10-5 FIG 4 DWG SRM 27-53-039. ORIGINAL MAT .063 REMOVED .008 REMAIN .055, THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: FRAME — CRACKED (ZONE 400) · airframe 39,357 hrs · 29,437 cycles

NR 1 ENG UPPER COWL FWD I/B END FRAME CRACKED REMOVED INB END FRAME. FABRICATED INSTALLED DOUBLER IAW SRM 51-40-2. TREATED PRIMED DOUBLER IAW SRM 51-10-2. INSTALLED STRIKER PLATE IAW SRM 51-30-1. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 39,357 hrs · 29,437 cycles

MAIN DECK FLOORBEAM, UPPER FLANGE IS CORRODED, BS 1070, LBL 47-60, WL 208. REMOVED CORROSION ON MAIN DECK FLOORBEAM UPPER FLANGE, STA 1070, LBL 47"-60". FOUND TO BE OUT OF LIMITS, FABRICATED AND INSTALLED REPAIR, REF SRM 53-10-08 FIG 1. THIS IS CLASSIFIED AS A MAJOR REPAIR.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,357 hrs · 29,437 cycles

FWD CARGO COMPT CORROSION ON STA 580 TO SKIN, LBL 3" TO LBL 10". REPAIRED SHEAR TIE AT STA 580, LBL 3" TO 10". REF SRM 53-10-4 FIG 15. THIS IS CLASSIFID AS A MAJOR REPAIR.

Part: STRINGER — CORRODED (ZONE 100) · airframe 39,357 hrs · 29,437 cycles

FWD PIT (STA 582) STR 27L CORRODED (MARKED ) REMOVED DAMAGED SECTION OF STR 27L . VERIFIED ORIGINAL MATERIAL AS .040 7075-T6 REF SRM 53-10-2 FIG 9. REPLACEMENT CHANNEL SAME AS ORIGINAL, BAC1498-140, FX1376, PO1013862. VERIFIED MATERIAL FOR REPAIR SPLICES AS 7075-T6-.063 REF SRM 53-10-3 A 03332 PO 1015473. FABRICATED REPAIR PARTS REF SRM 53-10-3. TREATED AND PRIMED REF SRM 51-10-2. INSTALLED REF SRM 53-10-3 (CLASSFIED AS A MAJOR REPAIR).

Part: THRESHOLD — CRACKED (ZONE 200) · airframe 39,357 hrs · 29,437 cycles

AFT ENTRY DOOR THRESHOLD HAS AREAS OF DAMAGE (BOTH BULLNOSE PIECES CRACKED) PARTS OF THRESHOLD SENT TO BE FABRICATED AND HEAT TREATED IN SHOP, 8130-3 TRACKING NR 2008-02-125 AND 126. HEAT TREATED TO T4 CONDITION. THRESHOLD RECEIVED FROM SHOP FABRICATED AND IN T4 CONDITION, N00731. LOCATED AND DRILLED FASTENER HOLES AND TREATED AND PRIMED THRESHOLD (1EA FX65-23946-4/FX69-24780-2) REF BOEING DWG 65-23946 AND/SRM 51-10-1, PG 12/SRM 51-10-2. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: FRAME — CRACKED (ZONE 100) · airframe 39,357 hrs · 29,437 cycles

FWD CARGO PIT, FRAME EXTENSION AT BS 520 IS CRACKED IN UPPER RADIUS, ABOVE STRINGER 22L ON FWD SIDE OF FRAME, MARKED END OF CRACK WITH BLACK DOT, (CIRCLED) GENERATED FROM U/C 53F0020. REMOVED CRACKED FRAME EXTENSION. VERIFIED MATERIAL FOR FABRICATION OF NEW FRAME EXTENSION, 7075-O .063" A61578 PO NR 1026198. HEAT TREATED NEW FRAME EXTENSION PART NR 53FX1350-1 TO T-6 CONDITION. TREATED AND PRIMED AND INSTALLED NEW FRAME EXTENSION REF SRM 51-30-2, 51-10-2, AND STC DWG 53FX1350. THIS IS CLASSIFIED AS A MAJOR REPAIR.

Part: FRAME — CRACKED (ZONE 500) · airframe 39,357 hrs · 29,437 cycles

LEFT WING OUTBOARD T/E NR 1 TRACK CENTER FAIRING INTERNAL AFT FORMER FRAME IS CRACKED IN CENTER. REMOVED AFT FORMER FRAME, LOCATED AND DRILLED NEW AFT FORMER FRAME AND INSTALLED REF SRM 51-30-2 PG 1, THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,357 hrs · 29,437 cycles

FWD PIT BILGE ( STA 720 ), BL 0 LWR SKIN CORRODED UNDER LEVELING COMPOUND. REMOVED CORROSION FOUND TO BE OUT OF LIMITS. REMAINING THICKNESS OF .028 INCH. FABRICATED DOUBLER AND INSTALLED DOUBLER TO SKIN REF 53-30-3 PG 3-5.

Part: STIFFENER — CRACKED (NR 1 NACELLE) · airframe 39,357 hrs · 29,437 cycles

NR 1 ENG UPPER COWL STIFFENER CRACKED BETWEEN 2ND AN 3RD LOWER LATCH CUTOUTS. REMOVED SEAL AND SEAL RETAINER, REMOVED CRACKED COWL STIFFENER, VERIFIED MATERIAL ID. FABRICATED NEW COWL STIFFENER, TREATED AND PRIMED, INSTALLED NEW COWL STIFFENER. REINSTALLED RETAINER AND SEAL, AND WROTE PART NUMBER ON NEW COWL STIFFENER. REF DWG 65-19508-39, REF SRM 51-30-2 PG 1, REF SRM 51-20-1 PG 13 FIG 2, REF SRM 51-30-2 PG 7, REF GMM 7-0-1001 PG 1. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: STIFFENER — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,357 hrs · 29,437 cycles

A/C EQUIP BAY, FAIRING SUPPORT INTERCOSTAL HAS CORROSION, STA 780, 3 INCHES, BL 0, JUST BELOW DELTA BEAM (STIFFENER). REMOVED CORRODED STIFFENER AND STRAP AT STA 780 + 3". REMOVED CORROSION AND MATERIAL WAS OUT OF LIMITS, BEYOND 10 PERCENT ALLOWABLE DAMAGE. FABRICATED NEW STRAP (PN 65-59318) AND STIFFENER (65-59318-21). STIFFENER WAS HEAT TREATED TO T-6 CONDITION ON NR N00507. TREATED AND PRIMED AND INSTALLED NEW STRAP AND STIFFENER. REF BOEING DWG 65-59318/SRM 51-30-02 PG 2 AND 13 SRM 53-10-1 PG 2 SRM 51-10-1 PG 12. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: FRAME — CRACKED (ZONE 100) · airframe 39,357 hrs · 29,437 cycles

FWD CARGO PIT, FRAME EXTENSION AT BS 600 IS CRACKED IN UPPER RADIUS, ABOVE STR 22L ON FWD SIDE OF FRAME. MARKED END OF CRACK WITH BLACK DOT CIRCLE. GENERATED FROM W/C 53F0020. FABRICATED FRAME EXTENSION REF DWG 53FX1350. HEAT TREATED TO T-6 CONDITION ON 8130 NR 2008-02-083, TREATED AND PRIMED. INSTALLED FRAME EXTENSION. REF SRM 51-30-2/51-10-2. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: THRESHOLD — CRACKED (BS 312-340) · airframe 39,357 hrs · 29,437 cycles

MAIN ENTRY DOOR CUTOUT LWR AFT SS THRESHOLD CORNER PLATE HAS 2 CRACKS RECEIVED SERVICEABLE THRESHOLD PLATE REF A TAG FEX3650, AND 8130-3 5517-0000, PLATE WILL BE INSTALLED ON EO CARD NR 7-5310-7-3362 P3 CARD 3 STEP C-2, THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: SHEAR TIE — DAMAGED (ZONE 100) · airframe 39,357 hrs · 29,437 cycles

MAIN CARGO BAY BS 680 FRAME SHEAR TIE HAS HAS TOOLING DAMAGE IN THE RADIUS BETWEEN STR S 14L AND S 15L, GENERATED BY 530045 CHECK DAMAGE LIMITS, ORIG MAT'L .045", MAT'L LOSS .007' WITH .038 REMAINING. DAMAGE IS OUT OF LIMITS REF SRM 53-10-2 PG 12A FIG 3. CUT OUT DAMAGE AREA REF, REF 53-10-04 PG 43. FABRICATED REPAIR ANGLE REF SRM 53-10-7 PG 44, HEATED TREATED ANGLE, TREATED AND PRIMED ANGLE, REF SRM 51-10-2 PG 7. INSTALLED ANGLE REF 51-30-2 PG 2.

Part: FLOOR SUPPORT — CORRODED (BS 1164-1166) · corrosion level 2 · airframe 39,357 hrs · 29,437 cycles

AFT LWR CARGO BAY BS 1164 - 1166 FLOOR SUPPORT ANGLE AT LBL 16 HAS CORROSION ON UNDERSIDE REPLACED FLOOR SUPPORT ANGLE AT BS 1164 - 1166 LBL 16, SRM 53-10-5 FIG 4 AND SRM 51-30-2.

Part: FAIRING — CRACKED (ZONE 500) · airframe 39,357 hrs · 29,437 cycles

LT WING, I/B FLAP, I/B TRACK AFT FAIRING SKIN CRACKED OUT ON TOP SIDE I/B OF AFT ATTACH BOLT, BOLT MOUNT CUTOUT. REPLACED FAIRING WITH SERVICEABLE UNIT. NR 4 TRACK POSITION. INSTALLATION ACCOMPLISHED ON WORK CARD NR 75C001-01. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 39,357 hrs · 29,437 cycles

RT WING OUTBOARD AFT FLAP, LWR SURFACE 1 INCH FROM OUTBOARD END, SKIN DISBONDED. REPAIRED RT OUTBOARD AFT FLAP LOWER SURFACE 1 INCH FROM OUTBOARD END. REF 51-40-20 PAR 7, 8, 14, 15, 18, 20-22. THIS CLASSIFIED AS A MINOR REPAIR.

Part: INTERCOSTAL — CRACKED (ZONE 400) · airframe 39,357 hrs · 29,437 cycles

NR 1 ENG LOWER COWL FWD END INTERCOSTAL CRACKED AND WORN MANUFACTURED AND INSTALLED NEW INTERCOSTAL FWD END OF NR 1 ENG COWL REF 65-19507 AND SRM 51-30-2.

Part: SKIN — CORRODED (TE FLAP) · corrosion level 2 · airframe 39,357 hrs · 29,437 cycles

RT WING OUTBD T/E FLAP, LWR SURFACE OUTBD END, LIGHT SURFACE CORROSION REPAIRED RT OUTBOARD T/E FLAP LOWER SURFACE REF SRM 51-40-20 PAR 7, 8, 14, 15, 18, 20-22 AND APPLIED EXTERIOR PROTECTIVE PAINT FINISH REF MM 51-20-151-7, THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: STRUCTURE — CORRODED (BS 301-305) · airframe 39,357 hrs · 29,437 cycles

NOSE W/W AIRCRAFT INTERIOR SURFACE AT BS 301 TO 305 RBL 14", WL 169 TO 171 LONGITUDINAL CHORD ABOVE HORIZONTAL WALKWAY IS CORRODED REMOVED FASTENERS, BLENDED CORROSION, FOUND TO BE WITHIN LIMITS, ORIGINAL MATERIAL .350", MATERIAL REMAINING .330' LOSS IS AT 5.7 PERCENT MAXIMUM LOSS IS 15 PERCENT, REF SRM 53-10-1 FIG 4 SHEET 2, ITEM E, NDT MAPPED BLENDED AREA REF D6-48875 PART 4 51-00-00 FIG 2. FLAP PEENED, TREATED, PRIMED AND CIC APPLIED. REF EA 7-5310-113970 PART 1 STEPS 7, 8, 9, 12. FASTENERS INSTALLED REF ESR 7-5310-113970 PART 1 STEP 11, SRM 51-30-4 FIG 1. REPLACED WIRE CHANNEL REF EA 7-5310-113970 PART 1 STEP 13. THIS IS CLASSIFIED AS MINOR REPAIR LEVEL 1 CORROSION.

Part: FLOOR SUPPORT — CORRODED (BS 1164-1166) · corrosion level 2 · airframe 39,357 hrs · 29,437 cycles

AFT LWR CARGO BAY BS 1164-1166 FLOOR SUPPORT ANGLE AT RBL 4, HAS CORROSION ON UNDERSIDE. REMOVED CORROSION ON AFT LWR CARGO BAY STA 1164 - 1166 FLOOR SUPPORT ANGLE AT RBL 4, REF SRM 51-10-6, MATERIAL LOSS OF 50 PERCENT, FOUND TO BE OUT OF LIMITS. REF SRM 53 10-1. FABRICATED REPAIR, REPAIR CHANNEL AND SPLICES REF SRM 53-10-5 FIG 4. TREATED AND PRIMED REPAIR PARTS REF SRM 51-10-2. INSTALLED REPAIR CHANNEL AND SPLICES, REF SRM 53-10-5 FIG 4 AND 51-30-2. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: SKIN — DENTED (ZONE 200) · airframe 39,357 hrs · 29,437 cycles

LOWER LEFT SIDE EXTERIOR FUSELAGE SKIN HAS DENT WITH SCRAPE STA 680 3 AND 7" BELOW STR 17L DENT WITHIN 10" OF PRODUCTION SEAM, REPAIR REQUIRED REF SRM 53-30-1 FIG 1. REMOVED DAMAGE IN REF TO SRM 53-30-1 HFEC FOR CRACKS AT CUT OUT . NONE FOUND. VERIFIED MATERIAL FOR REPAIR PLATE AS 2024 T3, .063 REF SRM 53-30-3 FIG 3A. FABRICATE DOUBLER IN REF TO 53-030-3 FIG 3A. INSTALLED DOUBLER IN REF TO 53-30-3 FIG 3A. THIS IS A CATEGORY "B" REPAIR, REFER TO SRM 51-00-6 GENERAL DATA REFER TO TABLE 3 FOR INSP INTERVALS THIS IS CLASSIFIED AS A MAJOR REPAIR.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 39,357 hrs · 29,437 cycles

LT EDGE SUPPORT CHANNEL FLOOR IS CRACKED AT CTR HOLE, STA 1030 TO 1070 FABRICATED NEW EDGE SUPPORT P/N 65-57570-1 AND SPLICE P/N 65-57570-3. TREATED AND PRIMED AND INSTALLED NEW EDGE SUPPORT AND SPLICE. REF BOEING DWG 65-57570/SRM 51-10-1 PG 12/SRM 51-10-2 PG 1/2, SRM 51-30-2 PG 5 AND 6. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: INDICATOR — INOPERATIVE (LT MLG) · airframe 38,324 hrs · 28,634 cycles

LT MAIN GEAR INDICATOR NOT WORKING. INSTALLED NEW LIGHT ASSEMBLY PER SMP, P/N 10-61803-49. LIGHT OPERATION CHECKS GOOD.

Part: REPAIR — UNKNOWN (ZONE 200) · airframe 37,578 hrs · 28,022 cycles

REPAIR LOCATED AT STA 303.9 STRINGER 15-L REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. ITEM NR 4, VISUALLY INSPECTED REPAIR AT STA 303.9 STRINGER 15-L. FOUND TO BE IAW SB 727-53A0198 AND EA 7-5330-92599 (FUSELAGE SKIN REPAIR DOUBLER HAS OVRSIZED FASTENERS - AD 98-11-03- R1) WITH RESPECT TO SIZE, SHAPE, SPACING, AND EDGE DISTANCE. THIS REPAIR WAS NOT REMOVED FOR THIS INSPECTION. THIS IS A MINOR REPAIR.

Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 37,578 hrs · 28,022 cycles

AFT PIT MAIN DECK FLOORBEAM HAS CORROSION AT FASTENER CLIP AT STA, BS 950F, LBL21.0. REMOVED CORROSION IAW SRM 51-10-6 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1 FIGURE 4. REMOVED AND REPLACED FLOORBEAM UPPER TEE CAP SECTION FROM LBL8 TO LBL70 IAW STANDARD REWORK DRAWING SR27-53- 034E. THIS IS A MAJOR REPAIR SIGNED BY MECH NR 1269 AND QC352. REF N00557.

Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 37,578 hrs · 28,022 cycles

MAIN CABIN FLOORBEAM HAS CORROSION AT FASTENER HOLES AT STA BS1130 BETWEEN RBL14 AND RBL40. REPAIRED OUT OF LIMTS SECTION OF STA BS 1130 FLOORBEAM IAW SRM 53-10-8 FIGURE 10. ALODINED AND PRIMED BARE METAL AREAS IAW SRM 51-10-2. INSTALLED REPAIR WITH WET FASTENERS IAW SRM 51-30-2. THIS IS A MAJOR REPAIR SIGNED BY MECH NR 98236 AND QC261. REFERENCE N00970.

Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 37,578 hrs · 28,022 cycles

REWORK OF FEDEX SNRM N00773 DUE TO IMPROPER SRM REPAIR APPLICABILITY MAIN DECK FLOORBEAM CORRODED ON TOP TWO PLACES AT STA BS 312 BETWEEN LBL 4 AND LBL 20. REMOVED IMPROPER REPAIR IAW B727 SRM 51-30-2. FABRICATED REPAIR ANGLES AND TEE CAP SECTION IAW B727 SRM 53-10-8 FIGURE 9. ALODINED AND PRIMED IAW B727 SRM 51-10-2. INSTALLED REPAIR IAW B727 SRM 53-10-8 FIGURE 9. THIS IS A MAJOR REPAIR.

Part: REPAIR — IMPROPER (ZONE 100) · airframe 37,578 hrs · 28,022 cycles

REPAIR LOCATED AT STA 950F - 970 STRINGER 29-R REQUIRES EVALUATION FOR MAJOR / MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED REPAIR AT STA BS 950F - 970 STRINGER 29R IAW B727 SRM 51-30-2. FABRICATED NEW REPAIR PARTS IAW B727 SRM 51-40-4 FIGURE 1 SHEET 6. ALODINED AND PRIMED IAW B727 SRM 51-10-2. INSTALLED REPAIR PARTS IAW B727 SRM 51-40-4 FIGURE 1 SHEET 6 AND 51-30-2. THIS IS A MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 37,578 hrs · 28,022 cycles

FORWARD CARGO COMPARTMENT STA BS 620 BOTTOM SURFACE OF FLOORBEAM UPPER TEE CAP HAS CORROSION AROUND SCREW HOLES LBL50 TO RBL50. REMOVED DAMAGED SECTION OF TEE CAP AT STA BS 620 BETWEEN LBL45 AND RT CUSP. FABRICATED NEW TEE CAP, SPLICES, SHIMS: ALODINED AND PRIMED; AND INSTALLED REPAIR PARTS IAW STANDARD REWORK DRAWING MM. SR27-53-034E SRM 51-10-2. THIS IS A MAJOR REPAIR, MECH NR 6709 AND QC298. REFERENCE N00713.

Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 37,578 hrs · 28,022 cycles

AFT PIT MAIN DECK FLOORBEAM HAS CORROSION STA BS 1130 LBL67.0 REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW B727 SRM 51-10-6 AND 53-10-1. FABRICATED REPAIR PARTS IAW B727 SRM 53-10-8 FIGURE 10. ALODINED AND PRIMED REPAIR PARTS IAW B727 SRM 51-10-2.INSTALLED REPAIR PARTS IAW B727 SRM 53-10-8 FIGURE 10 AND 51-30-2.REMOVED SEAT TRACK,1 EACH INTERCOASTAL AND 4 EACH GUSSET AND REINSTALLED AFTER REPAIR WAS COMPLETE IAW B727 SRM 51-30-2. THIS IS A MAJOR REPAIR SIGNED BY MECH #110188 AND QC303 REFERENCE SNRM N00490.

Part: FLOORBEAM — GOUGED (FUSELAGE) · airframe 37,578 hrs · 28,022 cycles

MAIN DECK TOP SIDE OF FLOORBEAM GOUGED AT STA BS680 LBL47 TO LBL57. REMOVED DAMAGED, FABRICATED REPAIR ANGLES FROM 17-7PH CRES STEEL .063 INCH, FABRICATED FILLER AND INSTALLED REPAIR ANGLES AND FILLER IAW SRM SR27-53-034 REV E. INSTALLED SEAT TRACK AT LBL65 BETWEEN STA BS660 AND STA BS720A IAW B727 SRM 51-30-2. THIS IS A MAJOR REPAIR SIGNED BY MECH NR 110569 AND QC178, REFERENCE N00807.

Part: HINGE FITTING — WORN (HORIZ STAB) · airframe 37,578 hrs · 28,022 cycles

RT HORIZONTAL STABILIZER IB NR1 ELEVATOR HINGE FITTING ON HORIZONTAL STABILIZER HAS IB FACE OF FITTING WORN. REMOVED BUSHING, SPOTTED FACE, HFEC INSPECTED LUG BORE FABRICATED AND INSTALLED REPAIR WASHER AND NEW BUSHING ALL IAW EA NR 7-5510-91317. THIS IS A MINOR REPAIR SIGNED BY MECH NR 4290 AND QC298 REF N01126.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 37,578 hrs · 28,022 cycles

CABIN FLOORBEAM UPPER TEE CAP CORRODED AT STA BS 344 BETWEEN LBL24 AND RBL24. CUT OUT CORRODED SECTION OF TEE CAP FROM LBL45 TO RBL24 IAW SRM 53-10-8 FIGURE 9. FABRICATED NEW TEE SECTION AND SPLICE ANGLES IAW SRM 53-10-8 FIGURE 9. ALODINED AND PRIMED REPAIR PARTS IAW SRM 51-10-2. INSTALLED REPAIR PARTS IAW SRM 51-30-2. THIS IS A MAJOR REPAIR SIGNED BY MECH NR 98629 AND QC281 REF SNRM N00598.

Part: BEAM — CORRODED (FUSELAGE) · airframe 37,578 hrs · 28,022 cycles

SEAT TRACK ATTACH TEE CAP HAS CORROSION OUT OF LIMITS AT LBL45 FROM STA BS760 TO STA BS850. REMOVED SEAT TRACK FROM BS 740 TO BS850 AT LBL45 IAW SRM 51-30-2. REMOVED, REPLACED AND INSTALLED NEW UPPER CHORD FROM STA BS 760 TO STA BS850 AT LBL45 IAW BAC DRAWING NR 65-16279 AND SRM 51-30-2. REINSTALLED SEAT TRACK SECTION FROM STA BS 740 TO STA BS850 AT LBL45 IAW B727 SRM 51-30-2. THIS IS A MAJOR REPAIR SIGNED BY MECH NR 110487 AND QC303 REF SNRM N01130.

Part: STRUCTURE — DAMAGED (ZONE 100) · airframe 37,578 hrs · 28,022 cycles

AFT CARGO DOOR, LOWER CHORD, UPPER TEE CAP AT STA BS 950D TO BS 950E, ABOVE STRINGER 27-R HAS SEVERAL HOLES WITH NO EDGE DISTANCE AND MINIMUM SPACING. REPAIRED DAMAGED CHORD IAW B727 SRM 51-40-4 FIGURE 1. REMOVED AND REINSTALLED 4 EACH CHORD FITTINGS, FILLER STRAPS, CHORD TEE AFTER REPAIR WAS ACCOMPLISHED IAW SRM 51-30-2.ALSO REMOVED AND REINSTALLED STA BS 950D TO BS990 TRANSITION PANEL IAW SRM 51-30-2 AND BAC DWG NR 65-56129. THIS IS A MAJOR REPAIR SIGNED BY MECH NR 7713 AND QC281 REFERENCE SNRM N00890.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 37,578 hrs · 28,022 cycles

MAIN CABIN, CENTER WING BOX UPPER SURFACE, SKIN IS CORRODED AT STA BS 820 LBL10. REPAIR CENTER WING BOX UPPER SURFACE OF SKIN IAW FEDEX EA7 5710-92595. "WINGS UPPER SKIN PANEL, CENTER TANK CORRODED, REPAIR ". ALODINED AND PRIMED BARE METAL IAW B727 SRM 51-10-2. INSTALLED FASTENERS WET IAW B727 SRM 51-30-2. CAP SEALED ALL FASTENERS IAW B727-200 MM 28-11-00-0-8. THIS IS A MAJOR REPAIR SIGNED BY TIMCO MECH NR 4315 AND QC298 REFERENCE FEDEX SNRM N01111.

Part: SKIN — GOUGED (ZONE 500) · airframe 37,578 hrs · 28,022 cycles

LEFT OUTBOARD MID FLAP OUTBOARD LEADING EDGE HAS 2 EACH GOUGES. REPAIRED FLAP LEADING EDGE IAW FEDEX EA7-5750-92591. WINGS - LEFT WING OUTBOARD MID FLAP LEADING EDGE SKIN HAS GOUGES. THIS IS A MINOR REPAIR BY TIMCO MECH 7153 AND QC303.

Part: FLAP TRACK — CORRODED (ZONE 500) · airframe 37,578 hrs · 28,022 cycles

LEFT WING INBOARD FLAP OUTBOARD TRACK FORWARD MOUNT HOLES (BORES) HAVE CORROSION. REMOVED CORROSION BY REAMING BORES C, D AND E. MAGNETIC PAR- TICLE INSPECTION AND FABRICATED BUSHINGS FOR BORES C, D AND E IAW FEDEX EA NR 7-5710-92592. ALSO, HEAT TREATED, CAD PLATED INSTALLED AND REAMED BUSHINGS IAW FEDEX E7-5710-92592. THIS IS A MINOR REPAIR REFERENCE FEDEX SNRM N00727, SIGNED BY TIMCO MECH NR 1281 AND QC300.

Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 37,578 hrs · 28,022 cycles

FOUND MAIN DECK FLOORBEAM HAS CORROSION AT STA BS 720A BETWEEN RBL4 AND RBL20. CLEANED AREA IAW B727 SRM 51-10-6, AND FOUND TO BE OUT OF LIMITS IAW B727 SRM 53-10-1. REMOVED DAMAGED UPPER CHORD IAW B727 SRM 53-10-8 FIGURE 4. FABRICATED UPPER CHORD, SUPPORT ANGLES, AND REINFORCEMENT STRAPS IAW B727 SRM 53-10-8 FIGURE 4. ALODINED AND PRIMED IAW B727 SRM 51-10-2. INSTALLED UPPER CHORD REPAIR IAW B727 SRM 53-10-8 FIGURE 4 AND 51-30-2. THIS IS A MAJOR REPAIR SIGNED BY TIMCO MECH NR 110174 AND QC303 REFERENCE FEDEX SNRM N00784.

Part: SKIN — DENTED (ZONE 100) · airframe 37,578 hrs · 28,022 cycles

REWORK OF FEDEX SNRM N00215 DUE TO WRONG MATERIAL USED. "FORWARD LOWER CARGO DOOR EXTERIOR SKIN IS DENTED". REMOVED DAMAGE AND FABRICATED REPAIR DOUBLER IAW SRM 52-00-3 FIGURE 3. ALODINED AND PRIMED REPAIR DOUBLER IAW B727 SRM 51-10-2. INSTALLED REPAIR DOUBLER IAW B727 SRM 51-30-2. REMOVED AND REINSTALLED LIGHT FIXTURE IAW B727 SRM 51-30-2. THIS IS A MAJOR REPAIR SIGNED BY TIMCO MECH NR 110290 AND QC401. REFERENCE FEDEX SNRM N01147

Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 375,782 hrs · 28,022 cycles

MAIN DECK FLOORBEAM CORRODED AT STA BS 720D FROM LBL27 TO LBL44. DAMAGE FOUND TO BE OUT OF LIMITS IAW B727 SRM 53-10-1 FIGURE 5. REMOVED STANCHION AND INTERCOSTAL BETWEEN STA BS 720D AND STA BS 720E TO FOM IAW B727 SRM 51-30-2. FABRICATED UPPER CHORD REPAIR IAW B727 SRM 53-10-8 FIGURE 4. ALODINED AND PRIMED REPAIR PARTS IAW B727 SRM 51-10-2. INSTALLED UPPER CHORD REPAIR IAW B727 SRM 53-10-8 FIGURE 4. REINSTALLED STANCHION AND INTERCOSTAL IAW B727 SRM 51-30-2. THIS IS A MAJOR REPAIR. REFERENCE FEDEX SNRM N00780, SIGNED BY TIMCO MECH NR 110174 AND QC261.

Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 37,578 hrs · 28,022 cycles

FOUND CABIN FLOORBEAM UPPER TEE CAP CORRODED AT STA BS400 BETWEEN BL 0 AND LBL 12. DAMAGE FOUND TO BE BEYOND LIMITS IAW B727 SRM 53-10-1 FIGURE 5. REMOVED DAMAGED UPPER CHORD IAW B727 SRM 53-10-8 FIGURE 3. FABRICATED REPAIR PARTS IAW B727 SRM 53-10-8 FIGURE 3. ALODINED AND PRIMED REPAIR PARTS IAW B727 SRM 51-10-2. INSTALLED REPAIR PARTS IAW B727 SRM 51-30-2. THIS IS A MAJOR REPAIR SIGNED BY TIMCO MECH NR 3476 AND QC261 REFERENCE FEDEX SNRM N00604.

Part: FLAP TRACK — CORRODED (ZONE 500) · airframe 37,578 hrs · 28,022 cycles

LEFT WING INBOARD FLAP OUTBOARD TRACK AFT MOUNT BOLT HOLES (BORES) HAVE CORROSION. REMOVED CORROSION BY REAMING FROM BORES G AND F WITH FINAL DIAMETER OF .3765 INCH FOR HOLE F AND .3765 INCH FOR HOLE G. FABRICATED REPAIR BUSHINGS FROM 15-5 PH STEEL PO 453539.1. HEAT TREATED BUSHINGS IAW BAC OVERHAUL MANUAL 57-40-01 AND CAD PLATED BUSHINGS IAW QQP-416 TYPE II CLASS 2 ON PO 510636.1. INSTALLED AND FINAL REAMED BUSHINGS TO .316 INCH ON BORES F AND G IAW BAC OVERHAUL MANUAL 57-40-01.

Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 37,578 hrs · 28,022 cycles

CABIN FLOORBEAM UPPER TEE CAP CORRODED AT STA BS 380 BETWEEN LBL24 AND LBL36. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW P-FSRM (ER 01-049) 53-10-1 FIGURE 4A. REMOVED DAMAGED AREA AND OBTAINED MATERIAL ID FOR UPPER CHORD AND REPAIR PARTS IAW B727 SRM 53-10-8 FIGURE 9. FABRICATED REPAIR PARTS IAW B727 SRM 53-10-8 FIGURE 9. ALODINED AND PRIMED PARTS IAW B727 SRM 51-10-2. INSTALLED UPPER CHORD AND REPAIR PARTS IAW B727 SRM 51-30-2 FIGURE 11. THIS IS A MAJOR REPAIR. REFERENCE FEDEX SNRM N00624 SIGNED BY TIMCO MECH NR 98629 AND QC261

Part: REPAIR — IMPROPER (ZONE 100) · airframe 37,578 hrs · 28,022 cycles

REPAIR LOCATED AT STA 1148 STR 30 REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA ITEM NR 17. ORIGINAL DOUBLER WAS NOT DONE USING THE B727 SRM 53-30-3 FIGURE 1. REMOVED DOUBLER IAW B727 SRM 51-30-2. FABRICATED A NEW DOUBLER IAW B727 SRM 53-30-3 FIGURE 1. ALODINED AND PRIMED DOUBLER IAW B727 SRM 51-10-2. INSTALLED DOUBLER IAW B727 SRM 53-30-3 FIGURE 1. THIS IS A MAJOR REPAIR SIGNED BY TIMCO MECH NR 6180 AND QC261.

Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 37,578 hrs · 28,022 cycles

FORWARD CARGO COMPARTMENT STA BS 560, BOTTOM OF FLOORBEAM HAS CORROSION BETWEEN RBL10 AND LBL40. REMOVED DAMAGE, FABRICATED 2 EACH REPAIR ANGLES, AND 1 EACH FILLER, AND 1 EACH LOWER STRAP IAW B727 SRM 53-10-8 FIGURE 2 ALODINED AND PRIMED REPAIR PARTS IAW B727 SRM 51-10-2. INSTALLED REPAIR PARTS IAW B727 SRM 51-30-2.

Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 37,578 hrs · 28,022 cycles

CABIN FLOORBEAM, UPPER T-CAP CORRODED AT STA BS 440 BL 0 - RBL 24. DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1 FIGURE 5. REMOVED DAMAGED T-CAP FROM RBL-8 TO LBL 8 STA BS 440 IAW SRM 53-10-8 FIGURE 3. REMOVED CORROSION FROM RBL 8 TO RBL 24 IAW SRM 51-10-6 AND FOUND WITHIN LIMITS IAW SRM 53-10-1 FIGURE 5. FABRICATED, LOCATED AND DRILLED THE UPPER CHORD SECTION, SUPPORT ANGLES AND REINFORCEMENT STRAPS IAW SRM 53-10-8 FIGURE 3. ALODINED AND PRIMED IAW SRM 51-10-2. PAINTED IAW SRM 51-10-2. INSTALLED REPAIR PARTS IAW SRM 51-30-2 AND 53-10-8 FIGURE 3.

Part: REPAIR — IMPROPER (ZONE 100) · airframe 35,578 hrs · 28,022 cycles

REPAIR LOCATED AT STA BS 251.6 TO BS 259 STRINGER STR 20-R REQUIRES EVALUATION FOR MAJOR / MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. FABRICATED DOUBLER IAW B727 SRM 53-30-2 FIGURE 1. ALODINED DOUBLER IAW B727 SRM 51-10-2. PRIMED DOUBLER IAW B727 SRM 51-10-2. INSTALLED DOUBLER IAW B727 SRM 53-30-2 FIGURE 1. MAJOR REPAIR.

Part: FRAME — CORRODED (ZONE 100) · airframe 37,578 hrs · 28,022 cycles

FORWARD CARGO COMPARTMENT, FRAME AT STA BS 720E BETWEEN STRINGER STR 26-R AND STR 25-R IS CORRODED. REMOVED DAMAGE AREA OF FRAME IAW SRM 53-10-4. FABRICATED INNER AND OUTER REPAIR DOUBLER AND FILLER IAW SRM 51-40-3 FIGURE 1. FABRICATED FRAME SECTION IAW MFG DRAWING 65-17663. ALODINED AND PRIMED REPAIR PARTS AND FRAME SECTION IAW SRM 51-10-2. INSTALLED REPAIR PARTS AND REPAIR FRAME SECTION IAW SRM 51-30-2.

Part: SKIN — CORRODED (ZONE 100) · airframe 37,578 hrs · 28,022 cycles

CORROSION AT LOWER FUSELAGE STA BS 480 STRINGER STR 29-L. REMOVED CORROSION IAW SRM 51-10-6. SKIN ORIGINAL THICKNESS .090 MATERIAL LOSS .022 MATERIAL REMAINING .068 FOUND OUT OF LIMITS IAW SRM 53-30-1 UT GAGE T8253C. DOUBLER AND FILLER MATERIAL ID 7075-T6 .090 PO 483543.2 IAW SRM 53-30-2 FIGURE 4 AND 53-30-3 FIGURE 2. REMOVED DAMAGE SKIN AREA IAW SRM 53-30-3 FIGURE 2. FABRICATED DOUBLER AND FILLER IAW SRM 53-30-3 FIGURE 2 AND 51-10-2. INSTALLED DOUBLER AND FILLER IAW SRM 53-30-3 FIGURE 2. REMOVED AND REPLACED FASTENERS IAW SRM 51-30-2.

Part: SKIN — DENTED (ZONE 100) · airframe 37,578 hrs · 28,022 cycles

RIGHT FUSELAGE EXTERNAL SKIN HAS A DENT AT STA BS 414 ON STRINGER STR 25-R. CHECKED DENT AND FOUND TO BE OUT OF LIMITS IAW B727 SRM 53-30-1. CUT OUT DAMAGE IAW B727 SRM 53-30-3. FABRICATED DOUBLER AND FILLERS IAW B727 SRM 53-30-3. ALODINED AND PRIMED REPAIR PARTS IAW B727 SRM 51-10-2. INSTALLED REPAIR DOUBLER AND FILLERS IAW B727 SRM 53-30-3. THIS IS A MAJOR REPAIR. SIGNED BY TIMCO MECH NR 110188 AND QC178.

Part: SKIN — CORRODED (ZONE 100) · airframe 37,578 hrs · 28,022 cycles

AFT PIT AT STA BS 1012 AT LBL 29 HAS CORROSION ON SKIN. REMOVED EXISTING REPAIR AND DAMAGED SKIN IAW B727 SRM 53-30-3 FIGURE 3A. FABRICATED NEW REPAIR IAW B727 SRM 53-30-3 FIGURE 3A. ALODINED AND PRIMED IAW B727 SRM 51-10-2; AND INSTALLED NEW REPAIR IAW B727 SRM 53-30-3 FIGURE 3A. THIS IS A MAJOR REPAIR. REFERENCE FEDEX NR N00434, SIGNED BY TIMCO MECH NR 6709 AND QC298.

Part: FLAP TRACK — CORRODED (ZONE 600) · airframe 37,578 hrs · 28,022 cycles

RIGHT WING INBOARD FLAP OUTBOARD TRACK FORWARD MOUNTING BOLT HOLES, BORES HAVE CORROSION. REAMED HOLES 2 EACH TO REMOVE CORROSION WITHIN LIMITS IAW. BAC OHM 57-40-01 NO CORROSION NOTED. FABRICATED AND CAD PLATED AND INSTALLED 2 EACH REPAIR BUSHINGS IAW OHM 57-40-01. REFERENCE FEDEX N/R N00730. SIGNED BY TIMCO MECH 4678 AND QC280.

Part: FLAP TRACK — CORRODED (ZONE 600) · airframe 37,578 hrs · 28,022 cycles

RIGHT WING O/B FLAR I/B TRACK AFT MOUNT CENTER BOLT HOLE HAS CORROSION. REPAIRED HOLE IAW BOEING OHM 57-40-01. REMOVED CORROSION FROM BORE IAW BOEING OHM 57-40-01. MAG PARTICLE INSPECTION OF BORE IAW BOEING OHM57-40-01. FABRICATED AND INSTALLED BUSHING IAW BOEING OHM 57-40-01 MECH: 7736 INSP:342 REFERENCE FED-EX NON ROUTINE NOO661.

Part: FLAP TRACK — CORRODED (ZONE 500) · airframe 37,578 hrs · 28,022 cycles

LEFT WING INBOARD FLAP TRACK FORWARD AND AFT MOUNTING FLANGES HAVE CORROSION. MACHINED FWD MOUNT PAD TO .250 REMOVING .020 TO REMOVE CORROSION. AFT PAD TO .260 REMOVING .015 TO REMOVE CORROSION IAW BAC OHM 57-40-01 PAGE 411 FIGURE 402. PERFORMED MAG PARTIAL INSPECTION IAW BAC OHM 57-40-01, NO DEFECTS. ROTO PEENED FORWARD AND AFT PADS IAW OHM 57-40-01 AND BAC SOPM 20-10-03. CAD PLATED MOUNT PADS IAW BAC SOPM 20-42-10 REV IR PRIMED FWD AND AFT PADS IAW SRM 51-10-2. SIGNED BY TIMCO MECH 1560 AND QC280.

Part: SMOKE DETECTOR — MALFUNCTIONED (MAIN CARGO) · airframe 35,406 hrs · 26,242 cycles

NR 5 MAIN CARGO SMOKE DETECTOR CAME ON, ON T/O ROLL AT APPROX 20 KTS. REMOVED AND REPLACED NR 5 MAIN CARGO SMOKE DETECTOR IAW FED EX M/M 26-16-001-4.

Part: FRAME — PUNCTURED (FUSELAGE) · airframe 35,406 hrs · 26,242 cycles

FRAME UPPER CHORD IS PUNCTURED BS 1070 RBL 24 WL 150.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 35,406 hrs · 26,242 cycles

WHILE WORKING FOUND SHEAR TIE CRACKED AT BS 950D LBL 6 WL 147. REMOVED DAMAGED SHEAR TIE AT BS 950D LBL 6 WL 147 FABRICATED, ALODINE, PRIMED AND INSTALLED REPAIR IAW 53-10-4 FIG 15 AND FED EX EA 7-5310-69479.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,406 hrs · 26,242 cycles

WHILE WORKING CARD N00303 FOUND CORROSION ON STR 27 LT FROM BS 1130-1040. \

Part: STRINGER CLIP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,406 hrs · 26,242 cycles

CORROSION ON STR CLIP BS 870 STR 27L.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,406 hrs · 26,242 cycles

CORROSION WHILE WORKING CARD N00303 FOUND CORROSION ON STRINGER RT BS 1090 AND BS 1110.

Part: BULKHEAD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,406 hrs · 26,242 cycles

CORROSION FWD CARGO BAY 740 LWR CHORD RBL 12 WL 148.5 UPPER SURFACE AROUND FASTENERS.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,406 hrs · 26,242 cycles

CORROSION WHILE WORKING CARD N00622 FOUND CORROSION ON STRINGER 26 RT BS 1166 TO BS 1148.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,406 hrs · 26,242 cycles

CORROSION WHILE WORKING CARD N00319 FOUND CORROSION ON - 27 LT AT BS 950D+6 AND +18, BS 950E+10, BS 950F+10. REPAIRED STR 27 LT IAW SRM 53-10-3.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,406 hrs · 26,242 cycles

CORROSION WHILE WORKING N00328 FOUND STRINGER CORRODED AT FASTENER HOLES COMMON TO STANDOFF BS 510 STR 27L.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,406 hrs · 26,242 cycles

CORROSION ON REINFORCEMENT FRAME FROM RBL 24 TO LBL 24, WL 208, STA 1176.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,406 hrs · 26,242 cycles

CORROSION (C53-113-01), FWD CARGO BAY INNER SURFACE OF OUTER SKIN AT BS 699 RBL 3 WL 148 AT NUT PLATE.

Part: SKIN — GOUGED (FUSELAGE) · airframe 35,406 hrs · 26,242 cycles

GOUGE ON INNER SKIN AT BS 1041 LBL 25 WL 146.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,406 hrs · 26,242 cycles

CORROSION AT STA 990, LBL 7, WL 140 FRAME HAS CORROSION. CORROSION ON FRAME BS 990 LBL 7 WL 140 FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1. REPAIRED FRAME IAW SRM 53-10-4 FIG 13.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,406 hrs · 26,242 cycles

STRINGER HAS CORROSION ON STR 29L BS 950E TO BS 1020. REMOVED AND REPLACED STR 29L (KEEL BEAM) IAW FED EX E.A. 7-5310-69472.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,406 hrs · 26,242 cycles

CORROSION ON FLOORBEAM STA 1130 BETWEEN LBL 45 TO RBL 45 WL 200.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,406 hrs · 26,242 cycles

N00344 CORROSION FWD CARGO BAY INNER SKIN AT B/S 720B+12 RBL 25. REPAIRED EXTERNAL SKIN AT B.S. 720B+12", RBL 25, WL 148 IAW SRM 53-30-3 AND FED EX E.A. 7-5330-54470.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,406 hrs · 26,242 cycles

STRINGER HAS CORROSION (C53-113-01-2) 28L BS 950E+3 LBL 16 WL 150. REPAIRED STR. 28L B.S. 950E+3 LBL1 6 WL 150 IAW SRM 53-10-3.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,406 hrs · 26,242 cycles

CORROSION (C53-113-01-2) ON INNER SKIN SURFACE BS 950F+1 TO 8 LBL-16. BLENDED SKIN OUT OF LIMITS PER SRM 53-30-1. SKIN REPAIR TO BE ACCOMPLISHED ON NR00317 FUSELAGE 5093.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 35,406 hrs · 26,242 cycles

BS 560 FRAME AND SHEAR TIE HAVE TWO FASTENER HOLES THAT HAVE BEEN DRILLED UP INTO THE VERTICAL PORTION OF THE FRAME LBL 12 WL 148. REPAIRED B.S. 560, LBL 12, W.L. 148 SHEAR TIE IAW SRM 53-10-4 FIG 13 AND FED EX E.A. 7-5310-54467.

Part: SKIN — CANNING (FUSELAGE) · airframe 35,406 hrs · 26,242 cycles

EXTERIOR SKIN OIL CANNED BS 1139 BETWEEN STR 23 AND 24 RT OIL CANNED EXTERIOR SKIN BS 1139 BETWEEN STR 23 AND 24 RT FOUND TO BE OUT OF LIMITS PER SRM 53-30-1. REMOVED DAMAGE IN AN AREA OF 3.6 X 4.4 INCH, FABRICATED, ALODINED, PRIMED AND INSTALLED REPAIR DOUBLER PER SRM 53-30-3.

Part: SKIN — CANNING (FUSELAGE) · airframe 35,406 hrs · 26,242 cycles

EXTERIOR SKIN OIL CANNED BS 1139 BETWEEN STR 23 AND 24 RT. OIL CANNED EXTERIOR SKIN BS 1139 BETWEEN STR 23 AND 24 RH FOUND TO BE OUT OF LIMITS PER SRM 53-30-1. REMOVED DAMAGE IN AN AREA OF 3.6" X 4.4 FABRICATED, ALODINED, PRIMED AND INSTALLED REPAIR DOUBLER PER SRM 53-30-3.

Part: PROXIMITY SWITCH — FAULTY (CARGO DOOR)

MAIN CARGO DOOR LIGHT ILLUM. PERFORMED QUICK REF HDBK PROC. DIVERT TO MSP. *S/D* REMOVED AND REPLACED MCD CTR PROX SW 29038 PER MM 52-34-009-5. AC OK FOR SERVICE.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,516 hrs · 24,685 cycles

N 470 DURING ROUTINE INSPECTION, NR 2 SEAT TRACK AT BS 950-950A FOUND CORRODED. R&R & FAB PER IAW BAC 727 SRM 53-10-5.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,516 hrs · 24,685 cycles

N 482 DURING ROUTINE INSP, NR 3 SEAT TRACK AT BS 420-440 FOUND CORRODED. R&R & FAB PER IAW BAC SRM 53-10-5.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,516 hrs · 24,685 cycles

N 687 DURING ROUTINE INSP, NR 6 SEAT TRACK AT BS 480-520 FOUND CORRODED. R&R & FAB PER IAW BAC 727 SRM 53-10-5.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 33,516 hrs · 24,685 cycles

N 834 DURING ROUTINE INSP, BS 400 FLOORBEAM FOUND CORRODED AT RBL 12. R&R & FAB PER IAW BAC 727 SRM 53-10-8.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,516 hrs · 24,685 cycles

N 467 DURING ROUTINE INSP, NR 2 SEAT TRACK FROM BS 950C-950D FOUND CORRODED. R&R & FAB PER IAW BAC 727 SRM 53-10-5.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 33,516 hrs · 24,685 cycles

N 444 DURING ROUTINE INSPECTION, SUPPORT ANGLE FROM BS 1050-1070, STR 27R FOUND CORRODED. R&R & FAB PER IAW BAC 727 SRM 51-20-1, 51-30-2.

Part: OVERHEAT LIGHT — ILLUMINAATED (LWR AFT BODY)

99-192 - AT CRUISE, LWR AFT BODY OVERHEAT LIGHT ILLUMINATED. RED TAB PROC INITIATED. RETARDING NR 1 THROTTLE EXITING LIGHT. NR 1 BLD AND LEFT PACK OFF REMAINDER OF FLT. COULD NOT DUPLICATE PROBLEM FOUND NOTHING WRONG.

Part: FIRE SENSOR — OUT OF POSITION (LWR AFT BODY)

99-179 - LWR AFT BODY OH LIGHT ILLUMINATED IN FLIGHT, AFTER THE NR 2 BLEED SWITCHES WERE CLOSED. THE LIGHT WENT OUT. TEST OF THE CIRCUIT WAS SUCCESSFUL. REPOSITIONED SENSOR AND RAN NR 2 ENG PER 727, JET RUN HDBK FOR 30 MIN. NO REPEAT, SENSOR TESTS NORM.

Part: STRINGER — CRACKED (BS 720)

UPPER LOBE STR 15L CRACKED STA 720B (AT ICE LIGHT). STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 53-10-3.

Part: STRINGER — CRACKED (BS 720)

UPPER LOBE STA 15L CRACKED STA 720B (AT ICE LIGHT). REPAIRED STR 15L CRACK IAW SRM 53-10-3 AND ATTACHED JOB PROGRESS FORM.

Part: FLOOR BEAM — CORRODED (BS 480)

UPPER LOBE FLOOR - CORR AROUND NUTPLATE HOLE STA 480, RBL 10. REMOVED DAMAGED SECTION OF FLOOR BEAM PER SRM 51-10-6 AND INSTALLED DOUBLER REPAIR SECTIONS PER SRM 53-10-6.

Part: STRINGER — CRACKED (BS 720)

MAIN CARGO STR 15R CRACKED STA 720B JUST FWD OF ICE LIGHT. INSTALLED REPAIR PER SRM 53-10-3, PG 4D.

Part: BELL FRAME — CRACKED (BS 800)

BELL FRAME IN MAIN CARGO STA 800 CRACKED AT STR 14R. STOP DRILLED CRACK, INSTALLED REPAIR PER SRM 51-40-1, PG 1. REJECTED AND BOUGHT ON NR 1207 PER 51-40-3.

Part: STR SPLICE — CRACKED (BS 600)

FORWARD CARGO STA 680, STA 28L SPLICE END CRACKED. REMOVED STR SPLICE - FABRICATED NEW SPLICE FROM 7075T6.063. INSTALLED SPLICE PER SRM 51-10-1.

Part: BOX SUPPORT — MISSING FASTENER (CARGO DOOR)

FORWARD CARGO DOOR HINGE BOX SUPPORT BOTH FWD AND AFT BOXES FASTENERS MISSING ON FWD AND AFT SIDE OF EACH BOX. INSTALLED FWD AND AFT WEBS AND DOUBLERS PER ESO 11782 DATED 12-07-95, EA 7-5310-26761 DATED 12-6-95.

Part: STRINGER — CRACKED (BS 407)

CRACK IN INNER FLANGE OF STR 3L, STA 407. STOP DRILLED CRACK TO .25 INCH AND INSTALLED REPAIR PART NR 1 53-10-3, PG 4D, FIG 2 (7075T6.040).

Part: FLOOR BEAM — CORRODED (BS 480)

UPPER LOBE CORROSION ON FLOOR BEAM LBL 10, STA LT 480. CLEANED AND BLENDED CORROSION. CORROSION REMOVAL OUT OF LIMITS PER SRM 51-10-6. CUT OUT CORRODED AREA AND INSTALLED REPAIR ON FLOOR BEAM PER SRM 53-10-8.