N233FE

Part: BRACKET — BROKEN (GIRT BAR) · airframe 70,901 hrs · 49,399 cycles

THE GIRT BAR BRACKET BROKE WHILE DISARMING THE SLIDE. REPLACED BRACKET IAW SMP, CHECKED GOOD.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 70,403 hrs · 48,987 cycles

EMERGENCY ESCAPE SLIDE LIGHT INOPERATIVE. R & R EMERGENCY ESCAPE SLIDE LIGHT BATTERY IAW AMM 33-50-121-2.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,294 hrs · 48,902 cycles

EMERGENCY EXIT LIGHT ABOVE ENTRY DOOR 1L DOES NOT TEST. REPLACED BATTERIES. NO HELP. REPLACED LIGHT ASSY AND BATTERIES. OPS CHECKED GOOD IAW AMM33-50-101. PREMATURE REMOVAL/INSTALLATION.

Part: CONTROL VALVE — LEAKING (RUDDER LIMIT) · airframe 70,126 hrs · 48,770 cycles

LOSS OF ALL SYS "A" HYD FLUID ON FLAPS 2 DEGREES SELECTION. PERFORM APPROPRIATE CHECKLISTS. REGAINED 1.2 GALLONS OF SYS A FLUID ON MANUAL GEAR EXTENSION. FOUND LWR RUDDER LOAD-LIMITING CONTROL VALVE LEAKING AT SEAL. R & R LOAD LIMITING CONTROL VALVE REF AMM 27-20-142, OPS AND LEAK CK GOOD REF AMM 27-20-000-5. RESERVICED "A" SYS HYD TO FULL, AND OK FOR SERVICE. PREMATURE REMOVAL/INSTALLATION.

Part: SEAT TRACK — CORRODED (BS 580-600) · corrosion level 2 · airframe 69,974 hrs · 48,638 cycles

CORRODED SEAT TRACK FLANGE STA 580-600, RBL 25. REMOVED DAMAGED SEAT TRACK SECTION. FABRICATED NEW SECTION USING BAC1520-792, 7178-T6511, DIMS 17' 5.3750", FABRICATED 2 SPLICES USING BAC1503-100122 DIMS 15.1250" AND 14.5", FABRICATED STRAP USING 7075T6 .250 DIMS 8.5" AND INSTALLED ALL REPAIR PARTS IAW SRM 53-10-5 AND SRM 51-30-2.

Part: FLOORBEAM — CORRODED (BS 720D) · corrosion level 2 · airframe 69,974 hrs · 48,638 cycles

CORROSION FLOORBEAM TOP "T" CAP STA 720D, RBL 45- LBL 25. REMOVED DAMAGED SEAT TRACK SECTION. FABRICATED UPPER CHORD, ANGLES AND STRAPS AND INSTALLED IAW SRM 53-10-8 AND SRM 51-30-2.

Part: SKIN — CRACKED · airframe 69,974 hrs · 48,638 cycles

FS 359 STR 28L EXTERNAL REPAIR CRACKED. CUT OUT DAMAGED SKIN AREA, FABRICATED REPAIR DOUBLER AND FILLER AND INSTALLED IAW EA 7-5330-123573.

Part: FLOORBEAM — CORRODED (BS 950B) · corrosion level 2 · airframe 69,974 hrs · 48,638 cycles

CORROSION TOP TEE CAP FLOORBEAM MAIN CABIN STA 950B, RBL 25- 45. CUT OUT DAMAGED AREA, FABRICATED REPAIR ANGLES, FILLERS AND INSTALLED IAW SRM 53-10-8 AND SRM 51-30-2.

Part: FLOORBEAM — CORRODED (BS 950D) · corrosion level 2 · airframe 69,974 hrs · 48,638 cycles

CORROSION TOP TEE CAP FLOORBEAM MAIN CABIN STA 950D, BL 0 TO RBL 25. CUT OUT DAMAGED AREA OF UPPER FLANGE, DIM (3 3/4" X 1") IAW SRM 53-10-8 FIG 8. FABRICATED 2EA ANGLES USING BAC1490-2888 7075-T6 (13 1/4" X 3") AND (9 1/4" X 3") AND 1EA FILLER USING BAC1505-100617, (3 3/4" X 1") IAW SRM 53-10-8 FIG 8; INSTALLED 2EA ANGLES AND REPAIR FILLER IAW B727 SRM 51-30-2, REV 103.

Part: STRINGER — CORRODED (BS 1080-1110) · corrosion level 2 · airframe 69,974 hrs · 48,638 cycles

CORROSION IN STRINGER 27L, FROM BS 1080 TO 1110. CUT OUT DAMAGED SECTION OF STR 27L, 21" LONG IAW SRM 53-10-3 FIG 1 REV 103 FABRICATED STRINGER SECTION FROM BAC1498-145, 7075 T62 21" LONG AND 2 SPLICES FROM BAC1498-131, 7075 T6 14 1/4" X 14 3/8" LONG IAW SRM 53-10-3 FIG 1 AND 53-10-2 FIG 9 INSTALLED STRINGER AND SPLICES IAW SRM 51-30-2 AND 53-10-3 FIG 1

Part: FLOORBEAM — CORRODED (BS 660) · corrosion level 2 · airframe 69,974 hrs · 48,638 cycles

CORROSION ON UPPER FLANGE OF FLOORBEAM AT BS 660, LBL 10. CUTOUT DAMAGED AREA APPROX DIM: 3" X 2" AND FABRICATED UPPER CHORD FROM BAC1505- 160617-7075T7 APPROX DIM: 16" LONG, FABRICATED 2 EA. ANGLES MATERIAL USED BAC1490 2785 7075T6 APPROX DIM: 16" X 2 3/4" AND FROM 1490 2831 7075T6 APPROX DIM: 11 1/2" X 2 3/4" AND FABRICATED 2 EA. STRAPS MATERIAL USED BAC 1512-3396 APPROX DIM: 12 1/2" X 1" AND 7075T6 .050 DIM: 16 1/4" X 1" IAW SRM 53-10-8 FIG 3 AND 51-30-5. INSTALLED REPAIR PARTS IAW SRM 51-30-2.

Part: FLOORBEAM — CORRODED (BS 950D) · corrosion level 2 · airframe 69,974 hrs · 48,638 cycles

CORROSION TOP TEE OF FLOORBEAM, BS 950D BL 0 TO LBL 25. CUT OUT DAMAGED AREA, FABRICATED NEW FLOORBEAM REPAIR IAW SRM 53-10-8 FIG 3 AND SRM 51-30-2 REV 103

Part: SEAT TRACK — CORRODED (BS 950-1080) · corrosion level 2 · airframe 69,974 hrs · 48,638 cycles

CORROSION SEAT TRACK FLANGE STA 950, PLUS 10" - STA 1010, LBL 25. REMOVED DAMAGED SEAT TRACK SECTION. FABRICATED NEW SECTION USING BAC1520-7927178-T65, DIMS 270" AND INSTALLED IAW SRM 53-10-5 AND SRM 51-30-2.

Part: SHEAR TIE — CORRODED (BS 1148 S26-27L) · corrosion level 2 · airframe 69,974 hrs · 48,638 cycles

UPON REMOVAL, FOUND SHEAR TIE CORRODED - AFT SIDE OF STA 1148 FRAME, STRINGER 27L TO 26L. REMOVED SHEAR TIE ON AFT SIDE OF BS1148 FRAME BETWEEN STRINGER 27L AND 26L IAW SRM, REV 103, 51-30-2. FABRICATED SHEAR TIE USING 7075-0, .063" X 2" X 6" IAW SRM 51-20-1, FIG 7. INSTALLED SHEAR TIE IAW SRM 51-30-2.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 69,974 hrs · 48,638 cycles

UPON REMOVAL, FOUND SHEAR TIE CORRODED - AFT SIDE OF STATION 1148 FRAME, STRINGER 26L TO 25L. REMOVED SHEAR TIE FROM AFT SIDE OF BS 1148 FRAME BETWEEN STRINGER 26L AND 25L IAW SRM REV 103, 51-30-2. FORMED SHEAR TIE USING 7075-0, .063" X 2" X 4" IAW SRM 51-20-1, FIG 7. INSTALLED SHEAR TIE IAW SRM 51-30-2.

Part: SHEAR TIE — CORRODED (BS 1148) · corrosion level 2 · airframe 69,974 hrs · 48,638 cycles

CORROSION - AFT SIDE OF FRAME SHEAR TIE, STATION 1148, STRINGER 28R TO STRINGER 27R. REMOVED SHEAR TIE FROM BS 1148 FRAME AFT SIDE BETWEEN STR 28R AND 27R IAW SRM 51-30-2 REV 103, FABRICATED SHEAR TIE FROM 7075 O .063" X 6" X 3" IAW SRM 51--20-1 FIG 7, INSTALLED SHEAR TIE IAW SRM 51-30-2 AND DRAWING 65-16348

Part: SUPPORT ANGLE — CRACKED (VERTICAL STAB) · airframe 69,974 hrs · 48,638 cycles

VERTICAL STAB INTERIOR AT BS 1343 HAS CRACK INDICATION ON RT UPPER WEB SUPPORT ANGLE, UNDERNEATH. REMOVED CRACKED SHEAR TIE. FABRICATED NEW SHEAR TIE USING 2024T-3 .050 DIMS 7 1/8" X 3 3/4" AND INSTALLED IAW SRM 51-20-1, SRM 55-30-2 AND SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 765-848) · corrosion level 2 · airframe 69,974 hrs · 48,638 cycles

CORROSION SEAT TRACK FLANGE STA 848 - STA 765, LBL 25. REMOVED DAMAGED SEAT TRACK SECTION. FABRICATED NEW SECTION USING BAC1506-1108-7075T6 DIMS 9.2', AND INSTALLED IAW DWG 65-16279 AND SRM 51-30-2.

Part: STRINGER — MISREPAIRED (BS 680 S28R) · airframe 69,974 hrs · 48,638 cycles

FS 680, STR 28R STRINGER REPAIR. REPAIR NON COMPLIANT IAW SRM 53-10-3. REMOVED EXISTING REPAIR, FABRICATED NEW STRINGER USING BAC1498-142 7075T-62 DIMS 27", FABRICATED REPAIR SPLICE USING BAC1458-132 7075T-6 DIMS 12" IAW SRM 53-10-2 AND SRM 53-10-3, FABRICATED STRINGER SPLICE USING BAC1458-132 7075T-6 DIMS 13.25" IAW DWG 65-56239 REV A AND INSTALLED REPAIR PARTS IAW SRM 51-30-2 AND SRM 53-10-3.

Part: FLAP TRACK — CRACKED (ZONE 600) · airframe 69,974 hrs · 48,638 cycles

RT INBD FLAP CUTOUT FOR AFT FLAP NR 2 TRACK CRACKED, WS 200. REMOVED R/H I/B MIDFLAP LOWER AFT CHORD IAW SRM 51-30-2 FABRICATED LOWER CHORD 3 SECTIONS FROM BAC1503-100046 7075 T6 47.5", 32.25" AND 96.75" LONG AND 2 SPLICES FROM BAC1503-100046 7075 T6, 8.1" AND 11" LONG IAW SRM 57-50-2 FIG 5 AND 51-40-4 FIG 1 INSTALLED LOWER CHORD IAW SRM 51-30-2 REV 103 AND 51-40-4 FIG 1.

Part: FLOORBEAM — CORRODED (BS 328) · corrosion level 2 · airframe 69,974 hrs · 48,638 cycles

CORROSION "T" CAP FLOORBEAM STA 328 LBL 50 - BL 0. CUTOUT DAMAGED SECTION SIZE 3" AT STA 328 AT LBL 10- LBL 13 IAW SRM 53-10-8, FIG 9. FABRICATED FILLER FROM BAC 1505-100246-7075-T6 SIXE 3" AND 4 EA SPLICE ANGLES FROM 7075-O .071 SIZES 13" X 2.2500" (2 EA) AND 11" X 2.2500" (2 EA) IAW SRM 53-10-8, FIG 9. HEAT TREATED TO 7075 -T6 IAW ENGINEERING REPORT 2-37153-801, REV A AND TREATED AND PRIMED AND INSTALLED REPAIR PARTS IAW SRM 53-10-8, FIG 9.

Part: SKIN — BULGED (BS 720E-720F) · corrosion level 2 · airframe 69,974 hrs · 48,638 cycles

BULGE EXTERIOR SKIN STA 720E- 720F STR 23R. CUT OUT DAMAGED PORTION OF STRINGER 23R, BS 720E PLUS 10" TO 720F PLUS 10" IAW SRM 53-10-3 FIG 1. FABRICATED TWO PORTIONS OF STRINGER USING BAC1498-142-7075T62 DIMENSIONS 17 7/8" AND 8 5/8", AND FABRICATED TWO SPLICES USING BAC1498-132-7075T6 DIMENSIONS 16 1/8" AND 14 1/8", IAW SRM 53-10-3 FIG 1. STRINGER REPAIR INSTALLED IAW SRM 53-10-3 FIG 1, REV 103.

Part: STRINGER — CORRODED (BS 870-920 S18AR) · airframe 69,974 hrs · 48,638 cycles

CORROSION RT WHEEL WELL OTBD SIDE STA 880, STR 18A. REMOVED DAMAGED STR 18A SHELF, FABRICATED NEW STR 18A SHELF AND INSTALLED IAW SRM 51-30-2, SRM 53-10-2, SRM 51-20-1 AND SRM 51-30-5.

Part: FLOORBEAM — CORRODED (BS 312) · corrosion level 2 · airframe 69,974 hrs · 48,638 cycles

CORROSION FLOORBEAM, STA 312 TEE CAP TOP LBL 55 - BL 0 L1 ENTRY. CUTOUT DAMAGED SECTION DIM: 3 1/2" IAW SRM 53-10-8 FIG 9 AND FABRICATED 4 EA. ANGLES FROM 7075-O .071 SIZES 15" X 2 3/4" AND 2 EA. 13" X 2 3/4" HEAT TREATED TO T6 CONDITION IAW ENG REPORT 2-37153-801 REV A. FABRICATED FILLER SIZE 3 1/2" FROM BAC 1505-29222-7075 T6 511. IAW SRM 53-10-8 FIG 9. TREATED AND PRIMED PARTS AND INSTALLED REPAIR PARTS IAW SRM 53-10-8 FIG 9 AND SRM 51-10-2.

Part: SKIN — DENTED (BS 1090-1110) · airframe 69,974 hrs · 48,638 cycles

DENTED EXTERIOR FUSELAGE STA. 1090 - 1110 S22-23R. CUTOUT DAMAGE AREA AND FABRICATED REPAIR DOUBLER IAW SRM 53-30-3 FIG 1. INSTALLED DOUBLER IAW SRM 51-30-2.

Part: FLOORBEAM — CORRODED (BS 480) · corrosion level 2 · airframe 69,974 hrs · 48,638 cycles

CORROSION FLOORBEAM TEE CAP TOP MAIN CABIN STA. 480 RBL 45 - 61 REMOVED CORROSION AT BS 480 RBL 45 - 61 AREA FOUND TO BE OUT OF LIMITS, CUTOUT DAMAGED AREA AT RBL 51. DIM: 2.5" X .90", FABRICATED NEW ANGLE REPAIRS ( 2 EACH) FROM BAC 1490-2888 7075T6. DIM: 16.8" & 11.6", FABRICATED FILLER FROM 2024T3 .125 DIM: 2.5" X .90", TREATED, PRIMED, AND INSTALLED NEW REPAIR PARTS ALL IAW SRM 51-10-6, SRM 53-10-1 FIG 4B, SRM 53-10-8 FIG 8, & SRM 51-10-2.

Part: SEAT TRACK — CORRODED (BS 765-848) · corrosion level 2 · airframe 69,974 hrs · 48,638 cycles

CORROSION SEAT TRACK FLANGE STA. 848 - STA. 765 LBL 45. REMOVED DAMAGED SEAT TRACK TEE AND FABRICATED NEW TEE FROM BAC 1506-1108-7075T6, AND INSTALLED IAW SRM 51-30-2, SRM 51-30-5, SRM 51-10-2, & DWG NR 65-16279.

Part: SKIN — CRACKED (LT WING TE FLAP) · airframe 69,974 hrs · 48,638 cycles

LT WING INBD AFT FLAP HAS CRACK ON LOWER SKIN AT FASTENER, WBL 203. REMOVED 6 EA FASTENERS AT AREA LT WING INBD AFT FLAP LOWER SKIN IAW SRM 51-30-2. FABRICATED REPAIR PLATE IAW SRM 57-50-4, FIG 5 AND INSTALLED REPAIR PLATE IAW SRM 51-30-2 AND 57-50-4, FIG 5.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 69,974 hrs · 48,638 cycles

CORROSION SEAT TRACK FLANGE MAIN CABIN STA 950 PLUS 10" TO STA 890, LBL 25. REMOVED DAMAGED SEAT TRACK SECTION. FABRICATED NEW SECTION USING BAC1520-792 7178T65 DIMS 3 1/4" X 69 1/2", FABRICATED 2 SPLICES USING BAC1503-100122 7178T6 DIMS 13 3/4" X 2 1/2" EACH AND 1 SPLICE USING 7075T6 .250 DIMS 7 1/4" AND INSTALLED IAW SRM 53-10-5 AND B727 SRM 51-30-2.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 69,974 hrs · 48,638 cycles

CORROSION SEAT TRACK FLANGE, MAIN CABIN STA 950 PLUS 10" TO STA 870, RBL 45. REMOVED SEAT TRACK SECTION. FABRICATED NEW SEAT TRACK & INSTALLED IAW SRM 53-10-5, FIG 1AND SRM 51-30-2, REV 103.

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 69,974 hrs · 48,638 cycles

VERT STAB INTERIOR AT BS 1303 VERT FRAME HAS 3 EA CRACKS ON LWR LT & RT WEB. CUTOUT DAMAGED AREAS AND FABRICATED REPAIR DOUBLERS & FILLERS & INSTALLED REPAIR DOUBLERS 2 EA & FILLERS 2 EA AT VERT STAB BS 1303 VERT FRAME WEB IAW SRM 53-10-9, FIG 4, SRM 55-30-2, FIG 2, SRM 51-10-2 & SRM 51-30-2.

Part: SHEAR TIE — CORRODED (BS 1148 S26-27L) · airframe 69,974 hrs · 48,638 cycles

CORROSION - FRAME SHEAR TIE FORWARD FLANGE, STATION 1148, STRINGER 27L TO STRINGER 26L. REMOVED CORROSION FROM SHEAR TIE WITH A MATERIAL LOSS OF .004, FOUND TO BE WITHIN LIMITS IAW SRM 53-10-1. TREATED AND PRIMED AREA IAW SRM 51-10-2.

Part: FLOORBEAM — CORRODED (BS 440) · corrosion level 2 · airframe 69,974 hrs · 48,638 cycles

CORROSION TOP "T" CAP FLOORBEAM STA 440, BL 0 - LBL 25, MAIN CABIN CUTOUT DAMAGE AREA AT FLOORBEAM BS 440, LBL 10 IAW SRM 53-10-8 FIG 8, FABRICATED (2) ANGLES REPAIR IAW SRM 53-10-8 FIG 8, & INSTALLED NEW ANGLES REPAIR AT LBL 5 - LBL 13 BS 440 IAW SRM 53-10-8 FIG 8 & SRM 51-30-2

Part: FLOORBEAM — CORRODED (BS 440) · corrosion level 2 · airframe 69,974 hrs · 48,638 cycles

CORROSION TOP "T" CAP MAIN CABIN STA 440, LBL 61- LBL 45 CUTOUT DAMAGE AREA IAW SRM 53-10-8, FIG 8, FABRICATED (2) ANGLES REPAIR FROM BAC 1490-2888-7075T6, & FILLER FROM 2024T3 .125 IAW SRM 53-10-8, FIG 8, INSTALLED NEW REPAIR AT LBL 45 - LBL 61, BS 440 IAW SRM 53-10-8, FIG 8 & SRM 51-30-2.

Part: SHEAR TIE — CORRODED (BS 950B S29-30R) · airframe 69,974 hrs · 48,638 cycles

CORROSION - FWD LOWER FLANGE OF FRAME 950B, SHEAR TIE, BETWEEN STRINGER 30 AND STRINGER 29R. CUT OUT DAMAGED AREA OF SHEAR TIE IAW SRM, REV 103, 53-10-4, FIG 12. FABRICATED SHEAR TIE, & FILLER IAW SRM 53-10-4, FIG 12 AND 53-10-2, FIG 5. INSTALLED SHEAR TIE REPAIR IAW SRM 53-10-4, FIG 12 AND 51-30-2.

Part: STRINGER — CORRODED (BS 1166 S22R) · airframe 69,974 hrs · 48,638 cycles

CORROSION - INSIDE CHANNEL, STRINGER 22R, FWD SIDE OF STA 1166 FRAME. REMOVED SECTION OF STRINGER 22R, 23" IN LENGTH IAW SRM, REV 103, 53-10-3, FIG 1. FABRICATED STRINGER SECTION USING BAC1498-144, 7075-T6, 23" IN LENGTH AND STRAP USING 2024-T3, .125" X 1" X 15" IAW SRM 53-10-3 FIG 1 AND 51-30-5. INSTALLED STRINGER AND STRAP IAW SRM 53-10-3, FIG 1 AND 51-30-2.

Part: DUCT — DENTED (NR 2 INTAKE) · airframe 69,974 hrs · 48,638 cycles

#2 ENGINE INLET "S" DUCT INTERIOR HAS DENT AT BS 1320, 9 O'CLOCK POSITION. CUTOUT DAMAGED AREA OF SKIN, CUTOUT CHANNEL SECTION, FABRICATED DOUBLER PLATE, FILLER PLATED, SHIMS, FABRICATED RIB REPAIR CHANNEL AND TWO ANGLES, LOCATED & DRILLED PARTS, TREATED AND PRIMED PARTS AND AREA. INSTALLED REPAIR PARTS, DOUBLER PLATE, FILLER PLATE, SHIMS, CHANNEL, AND TWO ANGLES AT BS 1320 "S" DUCT 9 O'CLOCK POSITION IAW SRM 54-10-3 FIG 10, SRM 51-30-2, SRM 51-30-5, AND SRM 51-10-2.

Part: STRINGER — GOUGED (BS 950A-950B) · airframe 69,974 hrs · 48,638 cycles

GOUGE INSIDE CHANNNEL - STRINGER 30, BETWEEN STA 950A - 950B. BLENDED GOUGE INSIDE STRINGER 30 BETWEEN BS950A- 950B IAW SRM REV 103, 51-10-1. C/W UT THICKNESS IAW NDTM, PT4, 51-00-00 FIG 2. ORIGINAL .130", REMOVED .027", REMAINING .103". FOUND TO BE WITHIN LIMITS IAW EA NR 7-5310-143924. TREATED AND PRIMED AREA IAW SRM 51-10-2 AND EA NR 7-5310-143924.

Part: SHEAR TIE — CORRODED (BS 720D) · corrosion level 2 · airframe 69,974 hrs · 48,638 cycles

CORROSION ON SHEAR TIE AT BS 720D (AFT SIDE OF FRAME) RBL 5 CUT OUT DAMAGED SHEAR TIE AT BS 720D RBL 5 IAW B727 SRM REV 103, 53-10-4 FIG 15. FABRICATED SHEAR TIE USING 7075-0, .071" X 2" X 4.7500" IAW SRM 53-10-4, FIG 15. INSTALLED SHEAR TIE IAW SRM 53-10-4, FIG 15.

Part: FRAME — DENTED (ZONE 100) · airframe 69,974 hrs · 48,638 cycles

FWD PIT UPPER FLANGE OF FRAME IS DENTED AT BS 720, RBL 35. CUT OUT DAMAGE AREA DIMENSION 1" X 1 1/2" IAW SRM 51-40-3 FIG 1. FABRICATED FRAME REPAIR USING 7075-0, .063" IAW SRM 51-40-3 FIG 1 AND 53-10-2 FIG 3. LOCATED AND DRILLED FRAME REPAIR DIMENSION 8 7/8" X 4" IAW SRM 51-40-3 FIG 1 AND 53-10-2 FIG 3. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED REPAIR IAW SRM 51-30-2.

Part: SKIN — CORRODED (BS 1015 S27L) · corrosion level 2 · airframe 69,974 hrs · 48,638 cycles

UPON REMOVAL STRINGER 27L STA. 1015 FOUND CORROSION ON INTERIOR SKIN. CUT OUT 2 AREAS AT BS 1010 STRINGER 28L DIM 10" X 5 7/8", AND BS 1010 STRINGER 27L DIM 7 1/2" X 3 1/4" IAW SRM 53-30-3 FIG 3A. FABRICATED DOUBLER USING 2024-T3 .080", DIM 21 1/2" X 14 1/2", FABRICATED 2 STRUCTURAL FILLERS USING 2024 T3 .071" DIM 4 3/4" X 6", AND 3 3/4" X 2 1/4", AND 2 FILLERS USING 2024 T3 .071" DIM 5 1/4" X 1 1/4" AND 2 1/2" X 1 1/2" ALL IAW SRM 53-30-3 FIG 3A AND 53-30-2 FIG 2. INSTALLED DOUBLER, FILLERS, AND STRUCTRUAL FILLERS IAW SRM 53-30-3 FIG 3A, REV 103.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 69,974 hrs · 48,638 cycles

CORROSION STRINGER 30 AT STA 1166, EXTERIOR SIDE OF LT CHANNEL RISER. REMOVED STRINGER SECTION FROM STATION 1142 TO 1183 AND 1EA SPLICE IAW SRM 51-30-2. FABRICATED 2 STRINGER REPAIR SECTIONS USING BAC1498-147 7075T6 19" LONG AND 19 1/2" LONG AND 2 SPLICES USING BAC1498-131 7075T6, 10 1/4" LONG IAW SRM 53-10-3 FIG 1. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED 2 STRINGER SECTIONS AND 2 SPLICES IAW SRM 51-30-2, REV 103.

Part: STRINGER SPLICE — CORRODED (ZONE 100) · corrosion level 2 · airframe 69,974 hrs · 48,638 cycles

AFT PIT STRINGER SPLICE CORRODED BS 1124 TO BS 1136 STR 30 CUT OUT DAMAGED STRINGER DIM.19" IAW SRM 53-10-3 FIG 1. FABRICATED STRINGER SECTION USING BAC1448-147, 7075T6 19" IN LENGTH AND SPLICES (2EA) USING BAC1498-131- 7075T6 10 1/4" LONG EA IAW SRM 53-10-3 FIG 1. TREATED AND PRIMED IAW SRM 51- 10-2, INSTALLED STRINGER AND 2EA SPLICES IAW SRM 51-30-2, REV 103.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 69,974 hrs · 48,638 cycles

CORROSION - INSIDE STRINGER 27L, STA 1010 - 1030. REMOVED STRINGER SECTION AND 2EA SPLICES FROM BS 1010 TO 1040 IAW SRM 51-30- 2. FABRICATED STRINGER USING BAC1498-145, 7075-T62, 29" IN LENGTH IAW SRM 53-10-3 FIG 1 AND 51-30-5. INSTALLED STRINGER SECTIN AND 2EA SPLICES IAW SRM 53-10-3 FIG 1, REV 103.

Part: STRINGER — CORRODED (BS 950D-1010) · corrosion level 2 · airframe 69,974 hrs · 48,638 cycles

CORROSION INSIDE STRINGER 27L, STA 950D - 1010. REMOVED SECTION OF STRINGER IAW SRM REV 103 51-30-2 AND 53-10-3, FIG 1 FABRICATED STRINGER SECTIONS, & SPLICES IAW SRM 53-10-3, FIG 1 AND 53-10-2, FIG 9 INSTALLED STRINGER AND SPLICES IAW SRM 51-30-2 AND 51-10-3, FIG 1.

Part: SEAT TRACK — CORRODED (BS 950-1010) · corrosion level 2 · airframe 69,974 hrs · 48,638 cycles

CORROSION SEAT TRACK STA 950, PLUS 10" TO STA 1010, RBL 25. REMOVED CORROSION FOUND OUT OF LIMITS IAW SRM 53-10-1 FIG 1, REMOVED SEAT TRACK IAW SRM 51-30-2, FABRICATED NEW SEAT TRACK FROM BAC 1520-792-7178-T6511 DIM: 20' X 3 3/8" IAW SRM 53-10-5 FIG 1, TREATED AND PRIMED IAW SRM 51-10-2, AND INSTALLED NEW SEAT TRACK IAW SRM 51-30-2 AT STA. 950 TO 1080 RBL 25 AT MAIN CABIN.

Part: FLOORBEAM — CORRODED (BS 950F) · corrosion level 2 · airframe 69,974 hrs · 48,638 cycles

CORROSION TOP TEE CAP FLOORBEAM MAIN CABIN STA 950F RBL 25 - RBL 45 CUT OUT DAMAGED AREA, FABRICATED REPAIR FILLER, ANGLES AND STRAPS, INSTALLED. REPAIR PARTS AT BS 950F, RBL 25 TO RBL 55 IAW SRM 51-30-2, SRM 51-10-2 AND SRM 53-10-8, FIG 1.

Part: FRAME — PUNCTURED (ZONE 100) · airframe 69,974 hrs · 48,638 cycles

FRAME UPPER FLANGE PUNCTURED - STA 1130 ABOVE STR 27L, BENEATH CARGO NET STANCHION FITTING. CUT OUT DAMAGED AREA DIMENSION 5 5/8" X 1" IAW SRM 51-40-3 FIG 1. FABRICATED FRAME REPAIR USING 7075-0, .063", DIMENSION 14 3/4" X 5 5/8" IAW SRM 51-40-3 FIG 1 AND 53-10-2 FIG 5. LOCATED AND DRILLED REPAIR IAW SRM 51-30-5. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED DOUBLER REPAIR IAW SRM 51-30-2, REV 103.

Part: STRINGER SPLICE — CORRODED (100) · corrosion level 2 · airframe 69,974 hrs · 48,638 cycles

STRINGER 27R STRAP CORRODED ON OTBD FLANGE AFT OF STA 1010 CORROSION OUT OF LIMITS. REMOVED STRAP. FABRICATED NEW STRAP USING 7075T6 FLAT BAR DIMS 20.5" X 1.3" AND INSTALLED IAW DWG 69-45584 AND SRM 51-30-2.

Part: FRAME — PUNCTURED (ZONE 100) · airframe 69,974 hrs · 48,638 cycles

FRAME UPPER FLANGE PUNCTURED - BS 1110 ABOVE STR 27R, BENEATH CARGO NET STANCHION FITTING. CUT OUT DAMAGED AREA DIM 3 7/8" X 1 3/4" IAW SRM 51-40-3 FIG 1. FABRICATED REPAIR USING 7075-0, .063", DIM. 14" X 5 3/4", LOCATED AND DRILLED PART IAW SRM 51-40-3 FIG 1, 53-10-2 FIG 5, AND 51-30-5. TREATED AND PRIMED IAW SRM 51-10-2, INSTALLED REPAIR IAW SRM 51-30-2, REV 103.

Part: FRAME — DENTED (BS 600 S25-26L) · airframe 69,974 hrs · 48,638 cycles

FWD PIT FRAME REPAIR DOUBLER IS DENTED AT BS 600, BETWEEN STR 25-26L. REMOVED FRAME REPAIR DOUBLER AT BS600 BETWEEN STRINGER 25L AND 26L IAW SRM, REV 103, 51-30-2. FABRICATED FRAME REPAIR USING 7075-0, .063" X 6.6" X 4.0" IAW DRAWING NR 69-43674. INSTALLED DOUBLER IAW SRM 51-30-2.

Part: FLOORBEAM — CORRODED (BS 440) · corrosion level 2 · airframe 69,974 hrs · 48,638 cycles

CORROSION MAIN CABIN FLOORBEAM TOP TEE CAP STA. 440 BL 0 - RBL 25 CUTOUT DAMAGED AREA, FABRICATED FLOORBEAM REPAIR PARTS & INSTALLED FLOORBEAM REPAIR AT BS 440 RBL 25 IAW SRM 51-10-6, SRM 53-10-1 FIG 4B, SRM 53-10-8 FIG 3, SRM 51-10-2, & SRM 51-30-2.

Part: FLOORBEAM — CORRODED (BS 560) · corrosion level 2 · airframe 69,974 hrs · 48,638 cycles

CORROSION TOP "T" CAP FLOORBEAM MAIN CABIN STA 560, LBL 61-LBL 45 CUT OUT DAMAGED AREA, FABRICATED NEW FLOORBEAM REPAIR AND FILLER AND INSTALLED IAW SRM 53-10-8 AND SRM 51-30-2.

Part: SKIN — DENTED (BS 405 S16-17L) · airframe 69,974 hrs · 48,638 cycles

DENT EXTERIOR FUSELAGE STA 405 STR 16-17L. CUTOUT DAMAGED AREA DIM: APPROX 1" DIAMETER IAW SRM 53-30-3 FIG 1 AND FABRICATED REPAIR DOUBLER FROM 2024T3 .063 DIM: 11 1/8" X 8 3/4" IAW SRM 53-30-3 FIG 1, INSTALLED COUNTERSINK WASHERS IAW SRM 53-30-1 FIG 1, TREATED AND PRIMED REPAIR PARTS IAW SRM 51-10-2, AND INSTALLED REPAIR PARTS IAW SRM 51-30-2.

Part: FRAME — DAMAGED (ZONE 100) · airframe 69,974 hrs · 48,638 cycles

FRAME UPPER FLANGE PUNCTURED - STA 1090 ABOVE STR 27R, BENEATH CARGO NET STANCHION FITTING CUT OUT DAMAGED AREA DIM. 3 3/8" X 1 1/4" IAW SRM 51-40-3 FIG 1. FABRICATED REPAIR DOUBLER USING 7075-0, .090". LOCATED AND DRILLED REPAIR, DIMENSION 12" X 4 1/2", FILLER, 7075-T6, .080" DIMENSION 3 3/8" X 1 1/4", AND WEB FILLER USING 7075-T6 DIMENSION 11 7/8" X 2 1/2" X .100" IAW SRM 51-40-3 FIG 1. TREATED AND PRIMED IAW SRM 51-10-2, INSTALLED REPAIR IAW SRM 51-30-2, REV 103.

Part: FLOORBEAM — CORRODED (BS 380) · corrosion level 2 · airframe 69,974 hrs · 48,638 cycles

CORROSION TOP "T" CAP FLOORBEAM MAIN CABIN STA 380 RBL45 - RBL 61. REMOVED PREVIOUS REPAIR. FABRICATED NEW T-CAP USING BAC1505-100617 7075T7 DIMS 76 5/8", FABRICATED 1 EACH SPLICE ANGLE USING BAC1490-2785 7075T6 DIMS 13 1/2", FABRICATED 1 EACH SPLICE ANGLE USING BAC1490-2831 7075T6 DIMS 9 3/8", FABRICATED STRAP USING 7075T6 .080 DIMS 9 3/8", FABRICATED STRAP USING 7075T6 .050 DIMS 13 3/4" AND INSTALLED ALL REPAIR PARTS IAW SRM 53-10-8 AND SRM 51-30-2.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 69,974 hrs · 48,638 cycles

CORROSION AFT SIDE OF FRAME SHEAR TIE STATION 950C BETWEEN STR 29L AND STR 28L. CUT OUT DAMAGED AREA OF BS950C FRAME SHEAR TIE AT STRINGER 29L TO STRINGER 28L, 3" X 6 3/8" IAW SRM REV 103, 53-10-4 FIG 12. FABRICATED SHEAR TIE USING 7075-0, .080" X 9 1/2" X 5 1/2", FILLER USING 7075-T6, .071" X 6 1/4" X 1" AND (3) FILLERS USING 7075-T6, .080" X 2 3/8" X 7/8", .080" X 2 1/8" X 7/8", .080" X 1 7/8" X 7/8" IAW SRM 53-10-4 FIG 12. INSTALLED SHEAR TIE REPAIR PARTS IAW SRM 53-10-4 FIG 12.

Part: SHEAR TIE — CORRODED (BS 950B S28-29L) · corrosion level 2 · airframe 69,974 hrs · 48,638 cycles

CORROSION FRAME SHEAR TIE FWD LOWER FLANGE STATION 950B, BETWEEN STR 29L TO STR 28L. CUT OUT DAMAGED SHEAR TIE BS 950B FRAME BETWEEN STRINGER 29L AND 28L, 6 3/8" X 3 5/8" IAW SRM, REV 103, 53-10-4 FIG 12. FABRICATED SHEAR TIE USING 7075-0, .080" X 10 5/16" X 6 1/4", FILLER USING 7075-T6, .071" X 6 3/8" X 1 1/8", (2) FILLERS USING 7075-T6, .080" X 1" X 1 1/4" AND FILLER USING 7075-T6, .080" X 1" X 2" IAW SRM 53-10-4 FIG 12 AND 53-10-2. INSTALLED SHEAR TIE REPAIR AND FILLERS IAW SRM 53-10-4 FIG 12 AND 51-30-2.

Part: FLOORBEAM — CORRODED (BS 950C) · corrosion level 2 · airframe 69,974 hrs · 48,638 cycles

CORROSION ON FLOORBEAM, STA 950C, RBL 25 TO RBL 45. CUT OUT DAMAGED FLOORBEAM, FABRICATED FLOORBEAM REPAIR, ANGLES AND FILLERS AND INSTALLED IAW SRM 51-30-2, SRM 51-10-2 AND SRM 53-10-8.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 69,974 hrs · 48,638 cycles

CORROSION ON SHEAR TIE AT BS 720A BETWEEN STRINGER 26R AND 25R. REMOVED T SHEAR TIE IAW SRM 51-30-2. FABRICATED, LOCATED, AND DRILLED NEW SHEAR TIE USING BAC1505-100044 7075-T6511 DIMENSION 6 1/4" LONG IAW DRAWING NR 69-43683 AND SRM 51-30-5. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED NEW SHEAR TIE IAW SRM 51-30-2.

Part: DUCT — CRACKED (NR 2 INLET) · airframe 69,974 hrs · 48,638 cycles

NR 2 ENGINE INLET "S" DUCT INTERIOR HAS A CRACK AT RIVET HOLE, BS 1342 11 0'CLOCK POSITION CUTOUT DAMAGED AREA IAW SRM 54-10-3 FIG 8, FABRICATED REPAIR PARTS ANGLE, PLATE, AND FILLER PLATE IAW SRM 54-10-3 FIG 8 AND SRM 54-10-2 FIG 5, LOCATED AND DRILLED PARTS IAW SRM 51-30-5, TREATED AND PRIMED AREA AND PARTS IAW SRM 51-10-2, INSTALLED REPAIR PARTS AT BS 1342 NR 2 ENGINE "S" DUCT AT 11 O'CLOCK IAW SRM 54-10-3 FIG 8 AND SRM 51-30-2.

Part: FLOORBEAM — CORRODED (BS 950) · corrosion level 2 · airframe 69,974 hrs · 48,638 cycles

CORROSION TOP TEE CAP FLOORBEAM MAIN CABIN STA 950, LBL 61 - 45. REMOVED DAMAGED UPPER TEE CAP FROM FLOORBEAM, LOCATED AND DRILLED NEW UPPER TEE CAP AND INSTALLED IAW SRM 51-30-5, SRM 51-30-2 AND DWG 65-16338.

Part: SKIN — GOUGED (BS 620 S8-16L) · airframe 69,974 hrs · 48,638 cycles

GOUGES INNER SURROUND SKIN STA 620, STR'S 8L-16L. CUT OUT DAMAGED SKIN SECTION, FABRICATED NEW SKIN SECTION USING 2024T-3 .125 DIMS 56" X 22" AND SPLICE USING 2024T-3 .125 DIMS 4" X 22" AND INSTALLED REPAIR PARTS IAW EA 7-5330-143921.

Part: FLOORBEAM — CORRODED (BS 1130) · corrosion level 2 · airframe 69,974 hrs · 48,638 cycles

CORROSION TEE CAP FLOORBEAM TOP STA 1130 BL0 - LBL 25. REMOVED DAMAGED UPPER CAP FROM BS 1130 FLOORBEAM, FABRICATED NEW CAP & INSTALLED NEW UPPER CAP IAW SRM 51-30-2 & EA 7-5310-142922.

Part: SEAT TRACK — CORRODED (BS 480) · corrosion level 2 · airframe 69,974 hrs · 48,638 cycles

CORROSION SEAT TRACK FLANGE STA 344 TO STA 480, LBL 45. REMOVED SEAT TRACK SECTION FROM BS 344 TO BS 480 LBL 45, FABRICATED NEW SEAT TRACK SECTION & INSTALLED NEW SEAT TRACK 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 69,974 hrs · 48,638 cycles

CORROSION SEAT TRACK FLANGE MAIN CABIN STA 480 - STA 690, LBL 45. REMOVED SEAT TRACK SECTION STA. 480 - STA. 690 LBL 45 IAW SRM 51-30-2 AND FABRICATED NEW SEAT TRACK SECTION FROM BAC1520-7927178T6 511 APPROX DIM: 209" IAW SRM 53-10-5 FIG 1. INSTALLED NEW SEAT TRACK IAW SRM 51-30-2.

Part: SKIN — DENTED (ZONE 100) · airframe 69,974 hrs · 48,638 cycles

DENT EXTERIOR FUSELAGE STA 378, STR 21L. CUTOUT DAMAGED AREA IAW SRM 53-30-3, FABRICATED DOUBLER REPAIR AND FILLER IAW SRM 53-30-2 FIG 2 AND SRM 53-30-3 FIG 3, INSTALLED FILLER AND REPAIR DOUBLER AT BS 378 STR 21L IAW SRM 53-30-3 FIG 3 AND SRM 51-30-2.

Part: SPAR — CRACKED (RT WING) · airframe 69,974 hrs · 48,638 cycles

CRACKED ANGLE CHORD FALSE SPAR RT WING AT NR8 SPOILER ACTUATOR SUPPORT MOUNT TRIMMMED WEB 12.2500" X 9.7500" AND LOWER CHORD 31" IN LENGTH AT RT WING FALSE SPAR IAW REPAIR DWG NR SR27-57-038, REV C. FABRICATED 2 SPLICE ANGLES USING 7075- 0, .071" X 16.2500" X 3.2500" AND .071" X 18.5" X 3.2500", WEB USING 7075-T6, .032" X 12.2500" X 9.7500 ", LOWER CHORD USING BAC1514-1437, 7075-T6, 31" IN LENGTH, STRAP USING 7075-T6, .090" X 16.5" X 2.2500", 2 FILLERS USING 7075-T6, .160" X 2.5" X 1", DOUBLER USING 2024-T3, .050" X 12" X 9" IAW DWG NR SR27-57-038, REV C. INSTALLED 2 SPLICE ANGLES, WEB, LOWER CHORD, STRAP, 2 FILLERS, DOUBLER IAW SRM 51-30-2, REV 103 AND DWG NR SR27-57-038, REV C.

Part: SEAT TRACK — CORRODED (BS 344-480) · corrosion level 2 · airframe 69,974 hrs · 48,638 cycles

CORROSION SEAT TRACK FLANGE STA. 360 - STA. 480 BL 0. REMOVED DAMAGED SEAT TRACK SECTION. FABRICATED NEW SECTION AND INSTALLED IAW SRM 53-10-2, SRM 51-30-2 AND SRM 53-10-5.

Part: SEAT TRACK — CORRODED (BS 706-740) · corrosion level 2 · airframe 69,974 hrs · 48,638 cycles

CORROSION SEAT TRACK FLANGE STA 706 - 740, RBL 25. REMOVED DAMAGED SEAT TRACK SECTION, FABRICATED NEW SEAT TRACK AND SPLICE SECTION, INSTALLED NEW SEAT TRACK AND SPLICE IAW SRM 51-30-2, REV 103, SRM 51-10-2 AND 53-10-5, FIG 1.

Part: SEAT TRACK — CORRODED (BS 460-480) · airframe 69,974 hrs · 48,638 cycles

CORROSION SEAT TRACK & SPLICE MAIN CABIN STA 460 - STA 480, LBL 25. REMOVED DAMAGED SEAT TRACK SECTION. FABRICATED NEW SECTION USING BAC1520-792, 7178 T6511 DIMS 136" AND INSTALLED IAW SRM 53-10-2 AND SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 380-440) · corrosion level 2 · airframe 69,974 hrs · 48,638 cycles

CORRODED SEAT TRACK FLANGE STA 380 - 440, RBL 25. REMOVED DAMAGED SEAT TRACK SECTION. FABRICATED NEW SECTION USING BAC1520-792 7178-T6511, DIMS 136 .1250" AND INSTALLED IAW SRM 53-10-2, SRM 51-30-5 AND SRM 53-10-5.

Part: SEAT TRACK — CORRODED (BS 380-480) · corrosion level 2 · airframe 69,974 hrs · 48,638 cycles

CORROSION SEAT TRACK FLANGE STA 380 - STA 480, RBL 45. REMOVED DAMAGED SEAT TRACK FABRICATED NEW SECTION USING BAC1520-792, 7178-T65 DIMS 135" AND INSTALLED IAW SRM 53-10-2 AND SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 600-690) · corrosion level 2 · airframe 69,974 hrs · 48,638 cycles

CORROSION SEAT TRACK FLANGE STA 600 - STA 690, RBL 45. REMOVED SEAT TRACK IAW SRM 51-30-2 AND FABRICATED NEW SEAT TRACK FROM BAC1520-792-7178-T6511, DIM: APPROX 172" IAW SRM 53-10-5, FIG 1. TREATED AND PRIMED SEAT TRACK IAW SRM 51-10-2 AND INSTALLED IAW SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 482-680) · corrosion level 2 · airframe 69,974 hrs · 48,638 cycles

CORROSION SEAT TRACK FLANGE STA 482-680, RBL 25. REMOVED SEAT TRACK SECTION FROM BS 480-690 RBL 25, FABRICATED NEW SEAT TRACK SECTION AND INSTALLED SEAT TRACK AT BS 480-690 RBL 25 IAW SRM 51-30-2; SRM 53-10-5 FIG 1 AND SRM 51-10-2, REV 103.

Part: SEAT TRACK — CORRODED (BS 500-540) · corrosion level 2 · airframe 69,974 hrs · 48,638 cycles

FWD PIT CABIN SEAT TRACK AT BL 0 IS CORRODED BETWEEN BS 500 - 540. REMOVED SEAT TRACK SECTION AND SPLICES IAW SRM 51-30-2. FABRICATED, LOCATED AND DRILLED SEAT TRACK SECTION IN LENGTH USING BAC1520-792 7178-T6511, AND INSTALLED SEAT TRACK SECTION AND SPLICES IAW P-F SRM 53-10-2, FIG 7A AND SRM 51-30-2, REV 103.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 69,974 hrs · 48,638 cycles

CORROSION SEAT TRACK FLANGE STA 1030 - STA 950, PLUS 10" LBL 45. REMOVED DAMAGED SEAT TRACK SECTION. FABRICATED NEW SECTION USING BAC1520-792 7178 T6511 DIMS 210 3/8" AND INSTALLED IAW SRM 53-10-5 AND SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 480-690) · corrosion level 2 · airframe 69,974 hrs · 48,638 cycles

CORROSION SEAT TRACK FLANGE MAIN CABIN STA 480 - STA 690, LBL 25. REMOVED SEAT TRACK SECTION AND SPLICE IAW SRM 51-30-2, LOCATED AND DRILLED SEAT TRACK SECTION, BAC 1520-792 7178 T6 DIM 210" LONG. FABRICATED SPLICE MAT USED 2EA ANGLES BAC 1503-100122 7178-4 DIM ( 14.3750" X 2.5" ), STRAP 7075 T6 .250" DIM (9" X 2" ) IAW SRM 53-10-5, FIG 1, INSTALLED SEAT TRACK SECTION AND SPLICE IAW SRM 51-30-2, REV 103.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 69,974 hrs · 48,638 cycles

CORROSION ON SKIN AT BS 720A PLUS 5" BETWEEN STRINGER 28R AND 27R. CUT OUT DAMAGED AREA, DIMENSION 5" X 2" IAW SRM 53-30-3 FIG 1. FABRICATED SKIN REPAIR USING 2024 T3, .080" X 14 3/4" X 9 1/4" IAW SRM 53-30-3 FIG 1. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED COUNTERSINK WASHERS IAW SRM 51-30-8. INSTALLED DOUBLER REPAIR IAW SRM 51-30-2, REV 103.

Part: SEAT TRACK — CORRODED (BS 1140-1160) · corrosion level 2 · airframe 69,974 hrs · 48,638 cycles

CORROSION SEAT TRACK MAIN CABIN STA 1160- STA 1140, RBL 25. REMOVED DAMAGED SEAT TRACK SECTION. FABRICATED NEW SECTION USING 7075T651 FLAT BAR DIMS 45" AND INSTALLED IAW DWG 53FX976 AND SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 720-720E) · corrosion level 2 · airframe 69,974 hrs · 48,638 cycles

SEAT TRACK CORRODED STA 720 TO 720E PLUS 10" BL 0 REMOVED DAMAGED SEAT TRACK SECTION. FABRICATED NEW SECTION USING BAC1520-792 7178-T6511 DIMS 141 3/8", AND INSTALLED REPAIR PARTS IAW SRM 53-10-5, SRM 53-10-2 AND SRM 51-30-2.

Part: STRINGER SPLICE — CORRODED (BS 1124-1136) · corrosion level 2 · airframe 69,974 hrs · 48,638 cycles

AFT PIT STRINGER SPLICE CORRODED BS 1124 TO 1136, STR 30. CUT OUT DAMAGED STRINGER, FABRICATED NEW STRINGER SECTION AND SPLICES AND INSTALLED IAW SRM 53-10-3, SRM 51-10-2 AND SRM 51-30-2.

Part: SKIN — CORRODED (BS 950D-950E) · corrosion level 2 · airframe 69,974 hrs · 48,638 cycles

CORROSION - INTERIOR FUSELAGE SKIN STATION 950D TO STA 950E OTBD SIDE OF STR 29L. REMOVED DAMAGED AREA OF SKIN IAW EA7-5330-123571 AND SRM 51-10-1, REV 103. FABRICATED DOUBLER, TRIPLER, & FILLERS IAW EA 7-5330-123571. INSTALLED DOUBLER, TRIPLER AND FILLERS IAW EA 7-5330-123571.

Part: SEAT TRACK — CORRODED (BS 870) · corrosion level 2 · airframe 69,974 hrs · 48,638 cycles

SEAT TRACK CORRODED STA 870 RBL25. REMOVED DAMAGED FLOATING SEAT TRACK SECTION. FABRICATED NEW SECTION USING BAC1520-1466-7178T6 DIMS 16", INSTALLED IAW SRM 53-10-2 AND SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 930-950) · corrosion level 2 · airframe 69,974 hrs · 48,638 cycles

SEAT TRACK CORRODED STA 930 TO 950 PLUS 10" LBL 45. REMOVED DAMAGED SEAT TRACK SECTION. FABRICATED NEW SECTION USING BAC1520- 7927178-T6511 DIMS 91", FABRICATED SPLICES USING BAC1503-100122-7178 DIMS 14 3/8" X 2 1/2" AND INSTALLED ALL REPAIR PARTS IAW SRM 53-10-5.

Part: SEAT TRACK — CORRODED (BS 950-1010) · corrosion level 2 · airframe 69,974 hrs · 48,638 cycles

SEAT TRACK CORRODED STA 950 PLUS 10" TO STA 1010, RBL 45. REMOVED DAMAGED SEAT TRACK SECTION, FABRICATED NEW SECTION AND INSTALLED IAW SRM 53-10-2, 51-30-2 AND 53-10-5 FIG 7.

Part: SEAT TRACK — CORRODED (BS 890-950C) · corrosion level 2 · airframe 69,974 hrs · 48,638 cycles

SEAT TRACK CORRODED STA 890 TO 950C BL 0. REMOVED DAMAGED SEAT TRACK SECTION. FABRICATED NEW SECTION USING BAC1520-792 7178T6511 DIMS 141 3/4" AND INSTALLED IAW SRM 53-10-5 AND SRM 51-30-2.

Part: SKIN — CORRODED (BS 970-990 S28L) · corrosion level 2 · airframe 69,974 hrs · 48,638 cycles

BULGE EXTERIOR FUSELAGE, INCLUDING SHEARED RIVET HEAD STA 990 - STA 970 STR 28L. CUTOUT DAMAGED SKIN DIM: 12 1/2" X 1 7/8 IAW SRM 53-30-3 FIG 3 AND 53-30-2 FIG 2. FABRICATED REPAIR DOUBLER AND FILLER FROM 2024 T3 .125" DIM 24 1/2" X 10 3/4" AND 12 1/2 X 1 1/2 IAW B727 SRM 53-30-3 FIG 3 AND 53-30-2 FIG 2. INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 53-30-3 FIG 3 AND 51-30-2 REV 103.

Part: STRINGER — CORRODED (BS 970-990) · corrosion level 2 · airframe 69,974 hrs · 48,638 cycles

STRINGER 28L CORRODED STA 990 - 970 CUTOUT DAMAGED STRINGER DIM: 19 1/2" IAW SRM 53-10-1 FIG 1 AND 53-10-3 FIG 1. FABRICATED STRINGER SECTION FROM BAC 1498-145 7075 T6 DIM: 19 1/2" IN LENGTH AND (2 EA. ) SPLICE SECTIONS FROM BAC 1498-131 7075 T6 DIM: 19 1/14" AND 18 1/4" IN LENGTH IAW SRM 53-10-3 FIG 1. INSTALLED NEW STRINGER SECTION AND 2 EA. SPLICES IAW SRM 53-10-3 FIG 1 AND 51-30-2 REV 103.

Part: LIGHT — FAILED (CABIN) · airframe 69,786 hrs · 48,483 cycles

MAINT PRE-FLT FOUND LT ENTRY DOOR, EMERGENCY LIGHT INOP. NEW BATTERIES NO HELP. REPLACED LIGHT ASSY IAW AMM 33-50-101-2-0. OPS CKS GOOD. PREMATURE REMOVAL/INSTALLATION OFF.

Part: SKIN — CHAFED (RT ELEVATOR) · airframe 83,901 hrs · 34,003 cycles

RIGHT OUTBD ELEVATOR L/E BULL NOSE LOWER SURFACE IS CHAFED AT STA XE 400 TO 482 REMOVED RUB STRIP IAW DC/MD-10 SRM 55-21-01; VOL II. ALODINED AND PRIMED NEW RUB STRIP IAW SRM 51-21-01; VOL II. INSTALLED NEW RUB STRIP IAW SRM 55-21-01; VOL II. RIGHT OUTBD ELEVATOR WAS DISPLACED TO ACCESS PANEL REMOVAL AND REINSTALLATION AND PERFORMED A BINDING AND GAP CHECK WITH NO DEFECTS IAW AMM 27-30-02-4.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,660 hrs · 43,792 cycles

CORROSION WHILE WORKING EO 7-5340-82473, FOUND CORROSION ON FLOORBEAM SPLICE AT BS 344, RBL 18. REPAIRED PER SRM 53-10-1, 51-10-2, 51-30-2, 51-30-5, 51-30-8, AND FED EX SRD 27-53-007.

Part: BEAM — CORRODED (FUSELAGE) · airframe 63,660 hrs · 43,792 cycles

CORROSION ON LONGITUDINAL BEAM BS 750 - 840, RBL 25, WL 208. REPAIRED PER SRM 53-10-1, 51-20-4, 51-30-2, 51-70-1.

Part: SHEAR TIE — DAMAGED (FUSELAGE) · airframe 63,660 hrs · 43,792 cycles

FOUND THE SHEAR TIE AT BS 380 BETWEEN STR 15 AND 16 TO REQUIRE REPLACEMENT DUE TO PREVIOUS CARGO NET BARRIER STRAP. INSTALLATION TO EXTEND UNDER THE FRAME AS OPPOSED TO OVER AS PER VENTURA AEROSPACE DWG 2987. REPAIRED PER SRM 53-10-4 FIG 11.

Part: SHEAR TIE — DAMAGED (FUSELAGE) · airframe 63,660 hrs · 43,792 cycles

FOUND THE SHEAR TIE AT BS 380 BETWEEN STR 14 AND 15 TO REQUIRE REPLACEMENT DUE TO PREVIOUS CARGO NET BARRIER STRAP. INSTALLATION TO EXTEND UNDER THE FRAME AS OPPOSED TO OVER AS PER VENTURA AEROSPACE DWG 2987. REPAIRED PER SRM 53-10-4 FIG 11.

Part: TEE FITTING — GOUGED (MLG) · airframe 62,581 hrs · 42,996 cycles

RT MLG I/B FORWARD TRUNNION MOUNT FITTING GOUGED. REPAIRED FORWARD TRUNNION MOUNT IAW FEDEX EA 7-5740-54980 DATED 09/17/03. REFERENCE SNRM N00419 / WO 00023911

Part: ATTACH FITTING — CORRODED (FLAP TRACK) · airframe 62,581 hrs · 42,996 cycles

NR 5 FLAP TRACK FORWARD ATTACH FITTING IS CORRODED AT BORE COMMON TO THE TRUNNION STUD. CLEANED AREA AND REINSPECTED AREA IAW BOEING SOPM 20-30-03. NO CORROSION NOTED AFTER CLEANING.

Part: WIRE — CHAFED (SMOKE DETECTION) · airframe 62,106 hrs · 42,612 cycles

MAIN CARGO SMOKE CONTROL, ACTIVATED IN FLIGHT (FL290) RESET, REACTIVATED, THEN ALARM SILENCED. ZONE 6 LIGHT REMAINED ON. DECLARED AN EMERGENCY AND LANDED. ALARM ACTIVATED FOUR TO SIX MORE TIMES DURING RECOVERY. NO SMOKE OR FUMES WERE DETECTED AT ANYTIME. DUE TO PREVIOUS NOTE ON JAN. 27 ABOUT WIRE BUNDLE RESTING ON SCREW (GROUND STUD) REMOVED WIRE W462-A42-20 BETWEEN D3828 AND D5370. INSPECTED WIRE FOR DEFECTS WITH NO DEFECTS NOTED. INSTALLED NEW WIRE FROM D3828 PIN 12 AND D5370 PIN 11 IAW MFG SWPM 20-10-11 AND 727-200 WDM 26-16-01. CARGO SMOKE TEST NORMAL, IAW B727-200 MM 26-16-001-5.

Part: CLAMP — LOOSE (NR 3 ENGINE)

NR 3 ENGINE STRUT O/H LIGHT ILLUMINATED. RED TABS ACCOMPLISHED. FOUND AIR LEAK ON INBOARD HEAT EXCHANGER CLAMP. LOOSENED ALL CLAMPS, TRYING TO PROPERLY SEAT INBD CLAMP. REMOVED INBD CLAMP PER STANDARD MAINT PRACT. REMOVED AND REPLACED SEALS AND DUCT ASSY PER STAND MAINT. NO LEAKS NOTED. OK FOR SERVICE.

Part: RIB — CRACKED (LT MLG) · airframe 60,668 hrs · 41,427 cycles

DURING ROUTINE INSP, LT MLG UPLOCK FRAME REINFORCING RIB AT BS 910 FOUND CRACKED. *S/D* REMOVED DOUBLER, STOP DRILL CRACK. REINSTALL DOUBLER PER IAW BAC 727 SRM 51-30-2.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 60,668 hrs · 41,427 cycles

DURING ROUTINE INSP THE FUSELAGE TIE CLIP AT BS 1070, STR 8L FOUND CRACKED. *S/D* REMOVED CLIP OUT OF ALLOWABLE LIMITS PER IAW BAC 727 SRM 53-10-1. TREATED AND PRIMED PER IAW BAC 727 SRM 51-10-2.

Part: WEB — CRACKED (TORQUE BOX) · airframe 60,668 hrs · 41,427 cycles

DURING ROUTINE INSP, AFT AIRSTAIR RT TORQUE BOX WEB LIGHTENING HOLE FOUND CRACKED AT BS 1223. *S/D* STOP DRILL CRACK PER BAC 727 SRM 51-40-2. FAB AND INSTALL PER IAW BAC 727 SRM 51-40-2.

Part: FLANGE — CRACKED (NR 2 ENG INTAKE) · airframe 60,668 hrs · 41,427 cycles

DURING ROUTINE INSP NR 2 ENG INTAKE FLANGE 1342 BULKHEAD FOUND CRACKED BY LFEC AROUND FLANGE BOLTS IN 16 PLACES FROM 3 O''CLOCK TO 10 O''CLOCK POSITION. *S/D* REMOVED AND REPLACED NR 2 ENG INTAKE DUCT MOUNTING FLANGE PER IAW FEDEX EO 7-5430-7-2303.

Part: SKIN — CRACKED (WING) · airframe 60,668 hrs · 41,427 cycles

DURING ROUTINE INSP, NR3 LEAD EDGE FLAP, OTBD GUIDE, WING LEAD EDGE CUTOUT WAS FOUND CRACKED. ** S/D ** STOP DRILL CRACK. FAB & INSTALL PER IAW BAC 727 SRM 57-30-4.

Part: SKIN — CRACKED (LT WING) · airframe 60,668 hrs · 41,427 cycles

DURING ROUTINE INSP, LT WING LEAD EDGE SKIN FOUND CRACKED NEAR NR 3 LEAD EDGE SLAT. ** S/D ** R&R & FAB PER IAW BAC 727 SRM 57-30-4.

Part: SUPPORT BRACKET — CRACKED (LE FLAP) · airframe 60,668 hrs · 41,427 cycles

DURING ROUTINE INSP, NR 1 LEAD EDGE FLAP ACTUATOR, FWD OTBD UPPER FITTING SUPPORT BRACKET FOUND CRACKED.*S/D* REMOVED AND REPLACED BRACKET PER IAW BAC 727 MM 27-81-001-4 AND BAC 727 SRM 51-10-1.

Part: CLAMP — LEAKING (NR 1 ENGINE)

ENGINE STRUT OVERHEAT NR 1 ILLUM DURING CLIMBOUT. EXECUTED RED TAB CKLIST AND LIGHT EXTINGUISHED AFT RETARD THROTTLE. RAN NR 1 ENG FOUND AIR LEAK AT 2 CLAMPS REPOSITIONED SAME AND RETORQUED PER MM 36-00-001-2. LEAK CHECK GOOD AS PER SAME.

Part: CLAMP — LOOSE (NR 1 ENGINE)

NR 1 ENGINE STRUT OVERHEAT LIGHT ILLUM AFT T/O. FOUND V-BAND CLAMP LOOSE AND LEAKING. TIGHTENED CLAMP PER MM 36-00-001-2. LEAK CHECK GOOD. SECURED ACCESS PANELS.

Part: CONNECTOR — CONTAMINATED (LANDING GEAR)

ON GEAR RETRACTION ALL IND NORM WITH GEAR HANDLE UP POSITION. WHEN GEAR HANDLE OFF, DOOR IND UNSAFE WITH RED DOOR LIGHTS. ACCOMPLISHED RED TAB PROC, LIGHT EXTINGUISHED WHEN GEAR HANDLE WAS IN UP POS. *S/D* REMOVED CANNON PLUG TO SWITCH, REMOVED FOREIGN OBJECT (GROMMET) AND RECONNECTED CANNON PLUG PER MM 32-62-011-5.

Part: EGT INDICATION — HIGH (NR 2 ENGINE)

NR 2 EGT HIGH INTO THE YELLOW BAND (640 DEG C) FOR MORE THAN 5 SEC. PULLED BACK TO 90 PERCENT N1. RETURN TO RDU. NR 2 FUEL FLOW WAS AT 3000 LBS PER HR AND EGT WAS STILL 100 DEG HOTTER THAN 1 AND 3. *S/D* INSTALLED BORESCOPE PLUGS AND IGNITER PLUGS. REMOVED AND REPLACED PS4 UPPER TUBE PER MM 75-31-31. ENG CK GOOD.

Part: LIGHT — INTERMITTENT (COCKPIT)

NR 0648 - COCKPIT EMERGENCY EXIT LIGHT INTERMITTENT. REMOVED AND REPLACED COCKPIT EMERGENCY EXIT LIGHT PER FEDEX M/M 33-50-101. EMERGENCY LIGHT TESTED GOOD PER FEDEX MM 33-50-101.

Part: STRINGER — CORRODED (BS 720)

CORROSION (C53-113-01,11) ON STR 27 RT AT BS 720B+10 FWD CARGO BAY. *S/D* REPAIRED STR 27 RT, BS 720 AT 14 TO 720B+12 PER FED-EX SRM 53-10-3 FIG 1.

Part: CHORD — CORRODED (BS 760-850)

CORROSION LUMINATING FROM UNDER SEAT TRACK AT BS 760 TO 850, LBL 25, WL 208. *S/D* REMOVED AND REPLACED LONGITUDINAL BEAM UPPER CHORD, BS 760 TO 850, LBL 25, WL 208 IAW DWG 65-16279 AND FEDEX SRM 51-30-2.

Part: FRAME — GOUGED (BS 1050)

DAMAGE TO THE TOP FLANGE OF THE BS 1050 FRAME AT LBL 20, WL 151. *S/D* REPAIRED DAMAGE TO THE TOP FLANGE OF THE BS 1050 FRAME AT LBL 20, WL 151 IAW FED-EX SRM 53-10-1.

Part: STRINGER — CORRODED (BS 484)

CORROSION ON STRINGER NR 27 RT, BS 484 FWD CARGO BAY.

Part: FRAME — CORRODED (BS 420)

WHILE WORKING NR 0164, FOUND CORROSION ON BS 420 FRAME LBL 15 - RBL 15, WL 135-133. *S/D* REPAIRED FRAME AT BS 420, LBL 15-RBL 15, WL 135-133 PER FED-EX SRM 51-40-3.

Part: SKIN — CRACKED (BS 351)

NR 0480, CRACK IN SKIN AT 351, LBL 22, WL 140 CIRCLED IN RED. REPAIRED CRACK IN SKIN AT BSA 351, LBL 22, WL 140 CIRCLED IN RED PER FEDEX SRM 51-10-1 AND PER 53-30-2. POURED LEVEL COMPOUND OVER INTERVAL PORTION OF FASTENERS PER FEDEX M/M 20-60-1.

Part: FRAME — CORRODED (BS 424)

CORROSION (C53-224-03-1/2) ON E & E BAY DOOR CUTOUT FWD FRAME. *S/D* REMOVED AND REPLACED E & E BAY DOOR CUTOUT FWD FRAME PER FED-EX SRM 51-30-2 AND FED-EX DRAWING 65-16351.

Part: WEB — CRACKED (CARGO DOOR)

WHILE WORKING NR-0059, FOUND 3RD WEB FROM FWD EDGE OF NR 1 CARGO DOOR TO BE CORROED. *S/D* REMOVED AND REPLACED 3RD WEB FROM FWD EDGE OF NR 1 CARGO DOOR IAW FEDEX SRM 51-10-1, 51-30-2.

Part: WEB — CORRODED (CARGO DOOR)

NR 1 CARGO DOOR HAS CORROSIOIN ON WEB 2ND FROM FWD EDGE OF DOOR, FOUND UPON REMOVAL OF SEAL DEPRESSOR ON NR-0059. *S/D* REMOVED AND REPLACED 2ND WEB FROM FWD EDGE OF NR 1 CARGO DOOR. WORK DONE IAW FED-EX SRM 51-30-2 AND 51-10-1.

Part: WEB — CRACKED (CARGO DOOR)

WHILE WORKING NR-0059, FOUND 4TH WEB FROM FWD EDGE OF NR 1 CARGO DOOR TO BE CRACKED. *S/D* REMOVED AND REPLACED 4TH WEB FROM FWD EDGE OF NR 1 CARGO DOOR IAW FED-EX SRM 51-10-1, 51-30-2.

Part: SKIN — DELAMINATED (RT TE AFT FLAP)

NR 0243 - RIGHT WING INBD AFT FLAP IS DELAMINATED AND DAMAGED AT INBD AND OUTBD ENDS.

Part: CHORD — CORRODED (BS 312-351)

CORROSION (C53-111-03-1/2) IN NUMEROUS AREAS OF MID NOSE CHORD HORIZ FLANGE BS 312 TO 351, LBL 15, WL 169. *S/D* REMOVED AND REPLACED NOSE CHORD BS 294 TO 351, WL 169, LBL 16 IAW DRW 65-18415 AND FEDEX SRM 51-30-2.

Part: FIRE LOOP — DIRTY (NR 2 ENGINE)

NR 2 FIRE PROTECTION SYS FAULT ILLUMINATED AND HORN SOUNDED INTERMITTENTLY AT THE TOP OF DESCENT. REMAINED OUT FOR THE REST OF THE FLIGHT. FOUND FIRE LOOP CONNECTIONS ON NR 2 ENG TO BE EXTREMELY DIRTY. REMOVED ALL FIRE LOOP AND HARNESS CONNECTIONS ON NR 2 ENGINE. CLEANED, INSPECTED AND REINSTALLED ALL CONNECTIONS. SYSTEM TESTS OK PER MAINTENANCE MANUAL 26-11-01.

Part: STICK SHAKER — ACTIVATED (E/E COMPT)

ON TAKEOFF, STALL WARNING STICK SHAKER ACTIVATED AT LIFT OFF. PULLED AND RESET CIRCUIT BREAKER, STALL WARNING CONTINUED. PULLED CIRCUIT BREAKER. INTERROGATED GROUND PROXIMITY WARNING SYSTEM, ANNUNCIATED ANGLE OF ATTACK INOPERATIVE. REPLACED ANGLE OF ATTACK SENSOR PER MAINTENANCE MANUAL 34-18-51. TESTED STALL WARNING SYSTEM PER MAINTENANCE MANUAL 34-18-01 PAGE 501-505 CHECK GOOD. NOTIFIED BY MAINTENANCE OPERATIONS THAT LEFT HAND INBOARD FLAP POSITION TRANSMITTER THAT WAS INSTALLED YESTERDAY HAD SAME PROBLEM ON AIRCRAFT 278. REPLACED AS A PRECAUTION PER MAINTENANCE MANUAL 27-52-2.

Part: CLOSING MECH — OUT OF ADJUST (PAX DOOR)

ALL MODES OF CABIN PRESSURIZATION SYS FAILED, NO DOOR LIGHT. WHEN A/C BLOCKED IN, FOUND FWD CABIN DOOR IMPROPERLY CLOSED, AFT PART ADJAR. OPS CHECKED DOOR, DOOR CLOSED PROPERLY. FOUND UPPER AFT PORTION OF DOOR REQ MODERATE PRESSURE WHILE CLOSING TO INSURE UPPER AFT ROLLER RAMPS PROPERLY IN CHANNEL DOOR, SAGS SLIGHTLY. SUSPECT UPPER HINGE BEARING WORN. *S/D* ADJUSTED UPPER ROD LINK ON L-1 DOOR IN ACCORDANCE WITH MAINTENANCE MANUAL 52.

Part: FLOORBEAM — CORRODED (BS 1110)

CORROSION AROUND FASTENER HOLES ON FLOORBEAM AT STA 1110 FROM 3 TO 20 RBL. REPAIRED PER SRM 51-10-6.