N491FE

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 41,577 hrs · 28,301 cycles

RT OTBD AFT FLAP HAS 1 DENT 1.5" X 3" .093 42" FROM INBD EDGE. REMOVED DAMAGED AREA IAW SRM 57-50-4, FIG 9 AND FABRICATED REPAIR DOUBLER IAW SRM 57-50-4, FIG 9 SHEET 1. INSTALLED REPAIR DOUBLER IAW SRM 51-30-2.

Part: DEPRESSOR — CHAFED (CARGO DOOR SEAL) · airframe 41,577 hrs · 28,301 cycles

C-2 DOOR MIDDLE LOWER SEAL DEPRESSOR IS CHAFED IN 5 PLACES. REMOVED SEAL DEPRESSOR IAW SRM 51-30-2 LOCATED, DRILLED & DEBURRED NEW SEAL DEPRESSOR IAW SRM 51-30-5. INSTALLED NEW SEAL DEPRESSOR IAW SRM 51-30-2.

Part: DEPRESSOR — DAMAGED (C-2 DOOR SEAL) · airframe 41,577 hrs · 28,301 cycles

C-2 DOOR FWD LOWER CORNER SEAL DEPRESSOR IS CHAFED. BLENDED CHAFE ON C-2 DOOR LWR FWD SEAL DEPRESSOR IAW SRM REV 103 51-10-1 OUT OF LIMITS. REMOVED SEAL DEPRESSOR IAW SRM 51-30-2. LOCATED, DRILLED NEW SEAL DEPRESSOR IAW SRM 51-30-5. INSTALLED SEAL DEPRESSOR IAW SRM 51-30-2.

Part: DEPRESSOR — CHAFED (C-2 DOOR SEAL) · airframe 41,577 hrs · 28,301 cycles

C-2 DOOR AFT LOWER CORNER SEAL DEPRESSOR IS CHAFED. REMOVED AFT CORNER SEAL DEPRESSOR IAW SRM 51-30-2 LOCATED , DRILLED & DEBURED NEW SEAL DEPRESSOR IAW SRM 51-30-5. INSTALLED SEAL DEPRESSOR IAW SRM 51-30-2.

Part: STRINGER — CRACKED (BS 720C S15L) · airframe 41,577 hrs · 28,301 cycles

CRACK AT FASTENER, STR 15L, STA 720C MAIN CABIN. CUTOUT DAMAGED AREA, FABRICATED CHANNEL FROM 7075T6 .040, FABRICATED TAPERED FILLER & RADIUS FILLER FROM 7075T6 .100 AND INSTALLED REPAIR PARTS IAW SRM 53-10-3, FIG 5, NDTM 51-00-00 FIG 23, SRM 51-10-2 & SRM 51-30-2.

Part: SUPPORT ANGLE — CRACKED (BS 1263) · airframe 41,577 hrs · 28,301 cycles

AFT AIR STAIRS, RT LOWER TORQUE BOX UPPER, SUPPORT ANGLE IS CRACKED AT BS 1263 REMOVED AND REPLACED RT TORQUE BOX UPPER SUPPORT ANGLE IAW SRM REV 103, 51-30-2.

Part: FITTING — CRACKED (BS 1263) · airframe 41,577 hrs · 28,301 cycles

AFT AIRSTAIR RT TORQUE BOX FITTING CRACKED AFT SIDE OF BS 1263 FRAME AT RBL 20. REMOVED AND REPLACED AFT AIRSTAIR , RT TORQUE BOX FITTING AN AFT AIDE OF BS 1263 AT RBL 20 IAW SRM REV 103, 51-30-2.

Part: FLOORBEAM — CRACKED (BS 760.9) · airframe 41,577 hrs · 28,301 cycles

MAIN CABIN OVEERWING FLOORBEAM TEE CRACKED AT RADIUS BS 760.9 LBL 24. REMOVED DAMAGED TEE, FABRICATED NEW TEE AND INSTALLED IAW DWG 65-16279, SRM 51-10-1, 51-10-2, AND 51-30-2.

Part: FRAME — CORRODED (CABIN WINDOW) · corrosion level 2 · airframe 41,577 hrs · 28,301 cycles

CORROSION WINDOW PLUG EXTERIOR FUSELAGE EDGE BS 794 LT. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 56-20-1 FIG 1. FABRICATED REPAIR DOUBLER IAW SRM 56-20-3 FIG 1 AND INSTALLED IAW B727 SRM 51-30-02.

Part: SEAT TRACK — CRACKED (BS 870-950) · airframe 41,577 hrs · 28,301 cycles

CRACKED SEAT TRACK FLANGE STA 870 - STA 950, LBL 25. REMOVED SEAT TRACK SECTION AND SPLICES, FABRICATED SEAT TRACK SECTION, FABRICATED SEAT TRACK SPLICES AND STRAP SPLICE, LOCATED AND DRILLED, INSTALLED NEW SEAT TRACK SECTION AT LBL 25 BS 870 - 950 INSTALLED SPLICES AT BS 950, LBL 25 IAW SRM 53-10-5, FIG 1, SRM 51-30-2, AND SRM 51-30-5, SRM 51-10-2.

Part: SKIN — CRACKED (LT WING TE FLAP) · airframe 41,577 hrs · 28,301 cycles

CRACK AT THE L/E INBD SIDE OF THE LT WING INBD FLAP FORE FLAP. REMOVED DAMAGED PANEL AT L/E LT WING FORE FLAP IAW SRM 51-30-2, FABRICATED NEW PANEL .040, 2024-O, HEAT TREATED TO T4 IAW FAS ER 2-37153-801, DRILLED TRIMMED IAW SRM 51-30-2 7 DWG 65-216-30, TREATED AND PRIMED PANEL IAW SRM 51-10-2, INSTALLED PANEL AT L/E FOREFLAP LT IAW SRM 51-30-2, SRM 57-50-2, FIG 3.

Part: FLOORBEAM — CRACKED (BS 760.9) · airframe 41,577 hrs · 28,301 cycles

MAIN CABIN OVERWING FLOORBEAM TEE CRACKED AT RADIUS BS 760.9 LBL45. REMOVED FLOORBEAM SECTION AT LBL45, BS 760.9 IAW SRM REV 103, 51-30-2. FABRICATED FLOORBEAM SECTION TEE IAW DWG 65-16279 & INSTALLED IAW SRM 51-30-2 AND DWG 65-16279.

Part: SKIN — GOUGED (CARGO DOOR) · airframe 41,577 hrs · 28,301 cycles

MCD INNER SURROUND SKIN GOUGED SEVERAL AREAS STA 620, STR 6L TO 9L. ACCOMPLISHED REPAIR IAW EA 7-5330-143950 FUSELAGE-AD 98-11-03 R1-MCD SURROUND STRUCTURE, INNER SKIN GOUGE REPAIR.

Part: STRINGER — CRACKED (BS 750B S15R) · airframe 41,577 hrs · 28,301 cycles

CRACK AT FASTENER STR 15R, STA 750B, MAIN CABIN. CABIN CUTOUT DAMAGED AREA, FABRICATED CHANNEL FROM 7075T6 .040, FABRICATED TAPERED FILLER & RADIUS FILLER FROM 7075T6 .100 AND INSTALLED REPAIR PARTS IAW SRM 53-10-3 FIG 5, AND SRM 51-10-2, AND SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 690-740) · corrosion level 2 · airframe 41,577 hrs · 28,301 cycles

CORRODED SEAT TRACK MAIN CABIN STA 690 - 740, LBL 24. REMOVED SEAT TRACK SECTION FROM BS 690-740, LBL 24 AND FABRICATED & INSTALLED NEW SEAT TRACK SECTION IAW SRM 51-20-2, SRM 51-10-2, SRM 51-30-2, SRM 53-10-5, FIG 1.

Part: FRAME — DENTED (CARGO BAY) · airframe 41,577 hrs · 28,301 cycles

FWD CARGO STA. 660 STR. 23R FRAME DENTED. CUTOUT DAMAGE FROM BS 660 FRAME ABOVE STR 23R, 1" X 1" IAW SRM 51-40-3 FIG 1. FABRICATED REPAIR DOUBLER IAW SRM REV 103 51-40-3 FIG 1. INSTALLED DOUBLER IAW SRM 51-30-2 AND 51-40-3 FIG 1.

Part: FLOORBEAM — CORRODED (BS 420) · corrosion level 2 · airframe 41,577 hrs · 28,301 cycles

CORROSION TOP TEE CAP FLOORBEAM MAIN CABIN STA 420, RBL 45 TO RBL 61. REMOVED CORROSION FROM FLOORBEAM IAW SRM 51-10-6 ORIG MAT. .125, LOSS, MAT. .015, REM MAT. .110, FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1, FIG 4B. CUTOUT DAMAGE AREA FABRICATED FILLER, FABRICATED DOUBLER FROM 7075-0, .090, INSTALLED IAW SRM 51-30-2, HEAT TREATED TO 7075T6 IAW ENGINEERING REPORT NR2-371533-801, REV A.

Part: SEAT TRACK — CORRODED (BS 690-740) · corrosion level 2 · airframe 41,577 hrs · 28,301 cycles

CORROSION SEAT TRACK FLANGE MAIN CABIN STA 690 - STA 740, RBL 45. REMOVED DAMAGED SEAT TRACK SECTION FROM BS 690- BS 740 RBL 45, FABRICATED NEW SEAT TRACK SECTION & INSTALLED NEW SEAT TRACK IAW SRM 53-10-5, FIG 1, SRM 51-30-2.

Part: SHEAR TIE — CORRODED (BS 950D) · corrosion level 2 · airframe 41,577 hrs · 28,301 cycles

AFT PIT HAS SURFACE CORROSION ON SHEAR TIE AT BS 950D STR. 29R. CUT OUT SHEAR TIE ON BS 950D FRAME AT STR 29R IAW SRM REV 103, 53-10-4 FIG 15. FABRICATED SHEAR TIE IAW SRM 53-10-4 FIG 15 AND 53-10-2 FIG 5. INSTALLED SHEAR TIE IAW SRM 51-30-2

Part: SEAT TRACK — CORRODED (BS 870-950) · corrosion level 2 · airframe 41,577 hrs · 28,301 cycles

CORROSION SEAT TRACK FLANGE MAIN CABIN STA 870 - STA 950 PLUS 10" RBL 25. REMOVED SEAT TRACK SECTION, FABRICATED NEW SEAT TRACK SECTION AND INSTALLED NEW SEAT TRACK SECTION BS 870 - BS 950 PLUS 10" RBL 25, AND REMOVED REPAIR, FABRICATED NEW REPAIR AND INSTALLED NEW REPAIR BS 950 TO 950A RBL 25 IAW SRM 51-30-2, SRM 53-10-5, FIG 1, AND SRM 51-30-5.

Part: SEAT TRACK — CORRODED (BS 848-870) · corrosion level 2 · airframe 41,577 hrs · 28,301 cycles

CORROSION FLOATING SEAT TRACK MAIN CABIN FLANGE STA. 870 - STA. 848.95 LBL 45 REMOVED FLOATING SEAT TRACK SECTION. FABRICATED NEW SEAT TRACK SECTION. INSTALLED IAW SRM 53-10-1 FIG 3, SRM 51-30-2, SRM 53-10-2 FIG 7A, SRM 51-10-2 AND SRM 51-30-2.

Part: FLOORBEAM — CRACKED (BS 760) · airframe 41,577 hrs · 28,301 cycles

MAIN CABIN OVERWING FLOORBEAM TEE CRACKED AT RADIUS BS 760.9 RBL 45. REMOVED MAIN CABIN OVERWING FLOORBEAM TEE, FABRICATED NEW TEE, AND INSTALLED IAW DWG 65-16279, SRM 51-30-2 AND 51-10-2.

Part: FRAME — GOUGED (BS 1070) · airframe 41,577 hrs · 28,301 cycles

AFT PIT FRAME AT BS 1070 UPPER FLANGE IS GOUGED ABOVE STR. 27L. CUT OUT DAMAGED AREA OF FRAME BS 1070 UPPER FLANGE ABOVE STR 27L IAW SRM 51-40-3 FIG 1. FABRICATED DOUBLER IAW SRM REV 103, 51-40-3 FIG 1 AND 51-30-5. INSTALLED DOUBLER IAW SRM 51-40-3 FIG 1.

Part: SEAT TRACK — CORRODED (BS 848-870) · corrosion level 2 · airframe 41,577 hrs · 28,301 cycles

CORROSION FLOATING SEAT TRACK FLANGE MAIN CABIN STA. 848.95 TO STA. 870 RBL 45 REMOVED DAMAGED FLOATING SEAT TRACK SECTION FROM BS 848.95 - 870 RBL 45. FABRICATED NEW SEAT TRACK SECTION. INSTALLED NEW FLOATING SEAT TRACK SECTION AT BS 848.95 - 870 RBL 45 IAW SRM 53-10-1 FIG 3, SRM 51-30-2, SRM 51-10-2, SRM 53-10-2 FIG 7A AND SRM 51-30-2.

Part: SEAT TRACK — GOUGED (BS 1130-1174) · airframe 41,577 hrs · 28,301 cycles

GOUGED SEAT TRACK SCALLOPS BL 0 STA. 1130 - STA . 1177 MAIN CABIN. REMOVED SEAT TRACK SECTION STA. 1130 - 1177 BL 0 IAW SRM 51-30-2, FABRICATED NEW SEAT TRACK FROM FLAT BAR PN 7075T6 DIM: 44 7/8" IAW DRAWING 53FX96, INSTALLED NEW SEAT TRACK SECTION IAW SRM 51-30-2 & DRAWING 53FX96.

Part: SKIN — CORRODED (BS 1015 S29L) · corrosion level 2 · airframe 41,577 hrs · 28,301 cycles

SKIN BULGE EXTERIOR FUSELAGE STA 1015, STR. 29L. CUT OUT AREA OF SKIN IAW SRM REV 103, 51-10-1. FABRICATED DOUBLER AND FILLER IAW SRM 53-30-3 FIG 3 AND 53-30-2. INSTALLED DOUBLER AND FILLER IAW SRM 53-30-3 FIG 3 AND 51-30-2.

Part: FRAME — CORRODED (BS 950B S27-28L) · corrosion level 2 · airframe 41,577 hrs · 28,301 cycles

AFT PIT, HAS SURFACE CORROSION ON FRAME BS 950B BETWEEN STR 28L & 27L. CUTOUT DAMAGE AREA, FABRICATED REPAIR DOUBLER & INSTALLED DOUBLER IAW SRM 51-40-3 FIG. 1 REV. 103.

Part: INTERCOSTAL — CRACKED (BS 294.5-303.9) · airframe 41,577 hrs · 28,301 cycles

INTERCOSTAL CRACKED STA. 294.5 TO 303.9 STR 16L. REMOVED CRACKED INTERCO IAW SRM 51-30-2. FABRICATED NEW AND INSTALLED IAW SRM 51-30-2 & DWG 65-17684.

Part: FRAME — GOUGED (BS 1070 S27L) · airframe 41,577 hrs · 28,301 cycles

AFT PIT FRAME AT BS 1070 UPPER FLANGE IS GOUGED ABOVE STR 27L. CUT OUT DAMAGED AREA OF FRAME BS 1070 UPPER FLANGE ABOVE STR 27L IAW SRM 51-40-3 FIG 1. FABRICATED DOUBLER IAW SRM REV 103, 51-40-3 FIG 1 AND 51-30-5. INSTALLED DOUBLER IAW SRM 51-40-3 FIG 1.

Part: INTERCOSTAL — CRACKED (BS 294.5-303.9) · airframe 41,577 hrs · 28,301 cycles

INTERCOSTAL CRACKS STA. 294.5 TO 303.9 STR 15L. REMOVED CRACKED INTERCOSTAL IAW SRM 51-30-2. FABRICATED NEW AND INSTALLED IAW SRM 51-30-2 & DWG 65-17684.

Part: NOSE COWL — DAMAGED (NR 3 NACELE) · airframe 41,577 hrs · 28,301 cycles

NR 3 ENGINE NOSE COWL DENTED AT 4:00 POSITION ON EXTERIOR SKIN CUT OUT DAMAGE ON NR 3 ENGINE NOSE COWL EXTERIOR SKIN AT 4:00 POSITION IAW SRM, REV 103, 51-10-1. FABRICATED FILLER AND 4 DOUBLERS IAW IAW SRM 54-30-3, FIG 2. INSTALLED DOUBLERS AND FILLER IAW SRM 54-30-3, FIG 2.

Part: SHEAR TIE — GOUGED (BS 500 S27R) · airframe 41,577 hrs · 28,301 cycles

FWD CARGO STA 500, STR 27R BOTTOM OF FRAME GOUGED AFT SIDE. REMOVED DAMAGED SECTION OF SHEAR TIE AT BS 500 BETWEEN STR. 27R AND 28R IAW FED EX B727 SRM REV. 103, 53-10-4 FIG. 13, FABRICATED SHEAR TIE, DOUBLER AND RADIUS FILLER IAW SRM 53-10-4 FIG. 13. INSTALLED DOUBLER AND RADIUS FILLER IAW B727 SRM 53-10-4 FIG 13 AND 51-30-2.

Part: SKIN — DAMAGED (NR 3 NACELLE) · airframe 41,577 hrs · 28,301 cycles

MISSING MATERIAL NR 3 ENGINE NOSE COWL OTBD AFT T/E 3 O'CLOCK POSITION. CUT OUT DAMAGE IAW SRM REV 103, 54-30-3 FIG 3A. FABRICATED FILLER AND DOUBLER FOR NR 3 ENGINE NOSE COWL IAW SRM 54-30-3 FIG 3A AND 54-30-2 FIG 1. INSTALLED DOUBLER AND FILLER IAW SRM 54-30-3 FIG 3A AND 51-30-2.

Part: SHEAR TIE — CORRODED (BS 1070 S27-28L) · corrosion level 2 · airframe 41,577 hrs · 28,301 cycles

BULGE SKIN EXTERIOR FUSELAGE STA 1070, STR 27L-28L. REMOVED SHEAR TIE IAW SRM REV 103, 51-30-2. FABRICATED SHEAR TIE IAW DWG 65-16344. INSTALLED SHEAR TIE IAW SRM 51-30-2.

Part: ANGLE — CORRODED (LT WING) · corrosion level 2 · airframe 41,577 hrs · 28,301 cycles

LEFT WING REAR SPAR ATTACHMENT, VERTICAL ZEE ANGLE IS CORRODED AT BOTTOM WBL 85, REMOVED CORRODED SECTION OF ZEE ANGLE IAW SRM REV 103 51-10-1. FABRICATED FILLER, 2 REPAIR DOUBLERS AND 2 SHIMS IAW SRM 51-40-4 FIG 1. INSTALLED REPAIR PARTS ON LT WING REAR SPAR VERTICAL ZEE ANGLE IAW SRM 51-30-2. LEAK CHECK NORMAL IAW MM 28-11-000-6.

Part: FLOORBEAM — CORRODED (BS 620) · corrosion level 2 · airframe 41,577 hrs · 28,301 cycles

CORROSION TOP TEE CAP FLOORBEAM MAIN CABIN STA 620 BL 0 - LBL 25. WORK ACCOMPLISHED ON NR N00384 AND SDR 11-0817.

Part: GUSSET — CRACKED (BS 825 FRAME) · airframe 41,577 hrs · 28,301 cycles

OVERWING LT FRAME AT BS 825, BELOW FLOOR LEVEL, GUSSET IS CRACKED AT INBD LOWER FASTENER. REMOVED GUSSET AT BS 825 LT BELOW FLOOR LEVEL IAW SRM 51-30-2, REV 103 FABRICATED GUSSET IAW EO 7-5310-7-3367, PART 9 INSTALLED GUSSET IAW EO 7-5310-7-3367, PART 9.

Part: FLOORBEAM — CORRODED (BS 560) · corrosion level 2 · airframe 41,577 hrs · 28,301 cycles

CORROSION TOP TEE CAP FLOORBEAM MAIN CABIN STA 560 LBL 25 - LBL 45. CUTOUT DAMAGED AREA, FABRICATED 2 ANGLES AND FILLER, TREATED AND PRIME PARTS AND AREA, INSTALLED FLOORBEAM REPAIR AT BS 560 BETWEEN LBL 25 - LBL 45 IAW SRM 53-10-8, FIG 8 AND SRM 51-30-5, SRM 51-10-2, AND SRM 51-30-2.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 41,577 hrs · 28,301 cycles

TWO CRACKED SKIN RIVETS, 1 UPPER SURFACE & 1 LOWER SURFACE, RT HORIZ STAB INTERIOR BOX APPX L/E STA 147, 8TH LTG HOLE INBD OF OTBD CLOSURE PANEL NEAR L/E. R & R 2EA RIVETS ON RT HORZ STAB SKIN IAW IAW SRM 51-30-2, REV 103. HFEC INSPECTED IAW NDTM PT6 51-00-00, FIG 23, NO CRACKS NOTED.

Part: SKIN — CORRODED (BS 1090 S28-29L) · corrosion level 2 · airframe 41,577 hrs · 28,301 cycles

UPON REMOVAL OF SHEAR TIE AT BS 1090 BETWEEN STR 29L AND 28L, FOUND SKIN TO BE CORRODED. CUT OUT AREA OF SKIN AT BS 1090 BETWEEN STR 29L AND 28L IAW SRM REV 103, 53-30-3 FIG 1. FABRICATED FILLER AND DOUBLER IAW SRM 53-30-3 FIG 1. INSTALLED DOUBLER AND FILLER IAW SRM 51-30-2.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,577 hrs · 28,301 cycles

BULGE TO THE EXTERIOR FUSELAGE STA 1090 STR 29L. REMOVED DAMAGED SHEAR TIE AT BS 1090 AND STR 29L IAW SRM REV 103, 51-10- 1. FABRICATED SHEAR TIE IAW SRM 53-10-4 FIG 15 AND 51-20-1 FIG 7. INSTALLED SHEAR TIE IAW SRM 53-10-4 FIG 15 AND 51-30-2.

Part: SEAT TRACK — CORRODED (BS 480-740) · corrosion level 2 · airframe 41,577 hrs · 28,301 cycles

CORROSION SEAT TRACK FLANGE MAIN CABIN STA. 480 - 740 RBL 45. REMOVED SEAT TRACK SECTION, FABRICATED & INSTALLED NEW SEAT TRACK SECTION IAW SRM 51-30-2, SRM 53-10-5 FIG 1, & SRM 51-10-2

Part: SEAT TRACK — CORRODED (BS 480-690) · corrosion level 2 · airframe 41,577 hrs · 28,301 cycles

CORROSION SEAT TRACK FLANGE MAIN CABIN STA 690 - 480 LBL 45. REMOVED SEAT TRACK SECTION, FABRICATED SEAT TRACK SECTION, FABRICATED SPLICES REPAIR, LOCATED AND DRILLED PARTS. INSTALLED SEAT TRACK SECTION, INSTALLED SPLICES REPAIR IAW SRM 53-10-5 FIG 1, SRM 51-30-5, SRM 51-10-2, AND SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 480-690) · corrosion level 2 · airframe 41,577 hrs · 28,301 cycles

CORROSION SEAT TRACK FLANGE STA. 690 - 480 LBL 25 MAIN CABIN. REMOVED SEAT TRACK SECTION FROM BS 480 - BS 690 AND SPLICES, FABRICATED NEW SEAT TRACK SECTION, FABRICATED 2 SPLICES ANGLES AND 1 STRAP SPLICE, LOCATED AND DRILLED PARTS, INSTALLED NEW SEAT TRACK SECTION AT LBL 25 BS 480 TO BS 690. INSTALLED SPLICES AT BS 690 IAW SRM 53-10-5 FIG 1 AND SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 380-480) · corrosion level 2 · airframe 41,577 hrs · 28,301 cycles

CORROSION SEAT TRACK FLANGE MAIN CABIN STA. 380 - 480 RBL 45. REMOVED SEAT TRACK SECTION. FABRICATED NEW SEAT TRACK, INSTALLED NEW SEAT TRACK SECTION IAW SRM 53-10-5 FIG 1, 51-30-2. SRM 53-10-2 FIG 7A

Part: SEAT TRACK — CORRODED (BS 360-480) · corrosion level 2 · airframe 41,577 hrs · 28,301 cycles

CORROSION SEAT TRACK FLANGE MAIN CABIN STA 360 - 480 BL 0. REMOVED SEAT TRACK FROM BS 360 - 480 BL 0, FABRICATED NEW SEAT TRACK SECTION, TREATED AND PRIMED. INSTALLED SEAT TRACK IAW SRM 53-10-2 FIG 7A AND SRM 53-10-5 FIG 1 SRM 51-30-2.

Part: FLOORBEAM — CORRODED (BS 620) · corrosion level 2 · airframe 41,577 hrs · 28,301 cycles

CORROSION TOP TEE FLOORBEAM MAIN CABIN STA. 620 LBL 25 - LBL 45. CUTOUT DAMAGED AREA IAW SRM 53-10-8 FIG 3. FABRICATED REPAIR PARTS IAW SRM 53-10-8 FIG 3. TREATED & PRIMED AREAS IAW SRM 51-10-2, INSTALLED REPAIR PARTS IAW SRM 53-10-8 FIG 3, INSTALLED STIFFENER IAW SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 360-480) · corrosion level 2 · airframe 41,577 hrs · 28,301 cycles

CORROSION SEAT TRACK FLANGE MAIN CABIN STA 360 - 480 LBL 25. REMOVED SEAT TRACK SECTION FROM BS 360 TO BS 480 LBL 25, FABRICATED SEAT TRACK SECTION, LOCATED AND DRILLED, TREATED AND PRIMED, INSTALLED SEAT TRACK SECTION, INSTALLED SPLICES IAW SRM 53-10-2 FIG 7A AND SRM 53-10-5 FIG 1 AND SRM 51-30-2.

Part: DOOR — UNSECURE (L1) · airframe 41,367 hrs · 28,147 cycles

ACFT WOULD NOT PRESSURIZE. LOUD NOISE AROUND MAIN ENTRY DOOR. NO DOOR LIGHTS. HANDLE IN PROPER POSITION. UPON ACFT ARRIVAL FOUND L-1 DOOR T/E NOT FULLY CLOSED. OPENED AND CLOSED DOOR SEVERAL TIMES WITH NO DEFECTS NOTED. PERFORMED INSP OF L-1 DOOR WITH NO DEFECTS NOTED. NO ACFT PRESSURIZATION DEFECTS NOTED. REF MM 21-31-000-5-0/ 52-11-001-6-0. ACFT OK FOR SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 41,365 hrs · 28,145 cycles

L1 DOOR EMERGENCY SLIDE LIGHT INOP. R & R SHIELD ASSY AND RELAMPED DUE TO CORROSION. NO HELP MM 33-50-041-2. R & R BATTERY PACK ASSY IAW MM 33-50-051-2. OPS CHECK NORMAL. PREMATURE REMOVAL/INSTALLATION.

Part: WINDOW — CRACKED (COCKPIT) · airframe 41,190 hrs · 28,003 cycles

L-2 COCKPIT WINDOW ARCING IN FLIGHT SUBSEQUENTLY SHATTERED. R & R L-2 (PILOTS SLIDING WINDOW ) IAW AMM 56-12-011-4. ADJUSTMENT AND TEST ACCOMPLISHED IAW AMM 56-12-011-5.

Part: SHEAR TIE — CRACKED (BS 950F) · airframe 40,187 hrs · 27,171 cycles

AFT CARGO COMPT SHEAR TIE AT BS 950F BETWEEN STR 28L AND 29L IS CRACKED. REMOVED SHEAR TIE IAW SRM 51-30-2. FAB NEW SHEAR TIE FROM 7075-O 0.080 INCH IAW SRM 53-10-2 FIG 5 AND 53-10-4 FIG 15. HEAT TREAT SHEAR TIE IAW FAS ENGINEERING REPORT NR 2-37153-807 REV A, TREAT AND PRIME NEW SHEAR IAW SRM 51-10-2. INSTALLED NEW SHEAR TIE AT BS 950F BETWEEN STR 28L AND 29L IAW SRM 51-30-2 AND 53-10-4 FIG 15.

Part: SHEAR TIE — CORRODED (BS 970) · corrosion level 2 · airframe 40,187 hrs · 27,171 cycles

CORROSION AT SHEAR TIE STR 30R AND STA 970 REMOVED DAMAGE SHEAR TIE IAW SRM 53-10-4 FIG 15. FAB NEW SHEAR TIE IAW SRM 53-10-4 FIG 15 AND 53-10-2 FIG 5. HEAT TREAT SHEAR TIE IAW FAS ENGINEERING REPORT NR 2-37153-801 REV A. TREAT AND PRIMED IAW SRM 51-10-2. INSTALLED SHEAR TIE IAW SRM 51-30-2.

Part: SKIN — DENTED (BS 180) · airframe 40,187 hrs · 27,171 cycles

DENT AROUND FASTENER STA 180 FWD OF LWR NOSE COMPT CUT-OUT. REMOVED FASTENER AT STA 180 LWR NOSE IAW SRM 51-30-2, FOUND AREA TO HAVE OIL CAN CONDITION AND OUT OF LIMITS IAW SRM 53-30-1 FIG 1. CUT OUT DAMAGE AREA, DIM 1 INCH BY 1 INCH IAW SRM 53-30-3 FIG 13. FABRICATED FILLER AND DOUBLER IAW SRM 53-30-3 FIG 13. TREATED AND PRIMED AREA AND DOUBLER REPAIR IAW SRM 51-10-20. INSTALLED DOUBLER REPAIR IAW SRM 53-30-3 FIG 13 AND 51-30-2.

Part: FRAME — CRACKED (ZONE 800) · airframe 40,187 hrs · 27,171 cycles

E/E COMPT DOOR CRACKED AT AFT FRAME. REMOVED INNER SKIN AND CRACKED FRAME, FABRICATED NEW FRAME. INSTALLED NEW FRAME AND SKIN IAW SRM 51-20-1, 52-40-1 FIG 2 AND 51-30-2.

Part: SKIN — DENTED (ZONE 100) · airframe 40,187 hrs · 27,171 cycles

DENT STA 324 STR 23L EVALUATED DENT AND FOUND OUT OF LIMITS IAW SRM 53-30-1 FIG 1. CUT OUT DAMAGED AREA DIMS 7/8 INCH BY 7/8 INCH. FABRICATED FILLER USING 2024-T3 .040 DIMS 7/8" BY 7/8" AND DOUBLER AND INSTALLED REPAIR PARTS IAW SRM 53-30-3 FIG 13 AND 51-30-2.

Part: FRAME — CHAFED (ZONE 200) · airframe 40,187 hrs · 27,171 cycles

FRAME AT STA 344 AND STR 5L CONTACTING 9G BULKHEAD. TRIMMED OUT FRAME AND FOUND OUT OF LIMITS IAW SRM 53-30-1 FIG 1. FABRICATED REPAIR IAW SRM 53-10-2 FIG 3 AND 53-10-4 FIG 2. TREATED AND PRIMED PARTS IAW SRM 51-10-2. INSTALLED REPAIR AT FRAME STA 344 STR 5L IAW SRM 53-10-4 FIG 2.

Part: SKIN — DAMAGED (BS 720-720D) · airframe 40,187 hrs · 27,171 cycles

FUSELAGE LT/RT, FWD WING TO BODY ATTACHMENT AREAS, SCRIBE MARKS IN SKIN STA 700, 72D STR 19L TO STR 19R. BLEND OUT DAMAGE IAW SRM 51-10-1 AND UT AREA IAW NDTM 51-00-00. FOUND SKIN OUT OF LIMITS IAW SRM 53-30-1. CUT OUT DAMAGE AREA LT SIDE & FABRICATED 1 DOUBLER AND 2 REPAIR FILLERS AND FILLER IAW SRM 53-30-3 FIG 1 & 53-30-2. INSTALLED REPAIR PARTS IAW SRM 53-30-3 & 51-30-2.

Part: SKIN — CRACKED (BS 640 S28R) · airframe 40,187 hrs · 27,171 cycles

FWD CARGO HAS CRACK AROUND RIVETS BACK TAIL AT STR 28R, STA 640. CUT OUT DAMAGED AREA AND REMOVED PREVIOUS SPLICE AS REQUIRED, FABRICATED REPAIR HAT SECTION AND ONE SPLICE AND INSTALLED REPAIR PARTS IAW SRM 53-10-3, 53 10-2, 51-10-2 AND 51-30-2.

Part: STRINGER — CORRODED (BS 950F-1110) · airframe 40,187 hrs · 27,171 cycles

CORROSION INSIDE OF STR 27L, STA 950F TO STA 1110. REMOVED CORROSION AND FOUND OUT OF LIMITS, REMOVED STRINGER SECTION FOR ACCESS AND REMOVED DAMAGED STRINGER SECTION, FABRICATED NEW STRINGER SECTION, FABRICATED REPAIR SPLICE. INSTALLED REPAIR PARTS AND STRINGER SECTION REMOVED FOR ACCESS IAW SRM 53-10-1, 51-10-6, 53-10-3, 53-10-2.

Part: SKIN — DENTED (BS 682) · airframe 40,187 hrs · 27,171 cycles

FUSELAGE SURFACE HAS DENT AT STA 682 S24L. COMPLIED WITH HFEC ON DENT IAW NDTM PT.6 51-00-00, CRACK INDICATED. CUT OUT DAMAGED AREA IAW SRM 53-30-3. FABRICATED REPAIR DOUBLER AND FILLER ACCOMPLISED IAW SRM 53-30-3 & 53-30-2. TREATED AND PRIMED AREA IAW SRM 51-10-2 AND INSTALLED REPAIR PART IAW SRM 51-30-2.

Part: SKIN — DENTED (BS 180) · airframe 40,187 hrs · 27,171 cycles

DENT AROUND FASTENER STA 180 FWD OF LWR NOSE COMPARTMENT CUTOUT.

Part: STRINGER — CORRODED (BS 950C-E) · airframe 40,187 hrs · 27,171 cycles

AFT CARGO COMPARTMENT, S29L HAS CORROSION AND PEELING PROTECTIVE FINISH BS 950C TO 950E. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-10-1, REMOVED FRAMES, INTERCOASTALS, FLOOR SUPPORTS, AND FAIRINGS FOR ACCESS IAW SRM 51-30-2 REMOVED AND REPLACED STRINGER 29L IAW SRM 51-30-2 REINSTALLED FRAMES, INTERCOASTALS, FLOOR SUPPORTS, AND FAIRINGS IAW SRM 51-30-2.

Part: SUPPORT BEAM — CRACKED (LT WING) · airframe 40,187 hrs · 27,171 cycles

LEFT WING NR 7 SPOILER FALSE SPAR LWR PANEL HAS LOOSE FASTENERS. EVALUATED AND FOUND SUPPORT BEAM CRACKED AT WS 251. REPAIRED IAW DRAWING SR27-57-038 REV C.

Part: SEAT TRACK — CORRODED (BS 880-920) · airframe 40,187 hrs · 27,171 cycles

MAIN CARGO COMPARTMENT, SEAT TRACK CORRODED AT STA 880 TO STA 920 , BL 0. REMOVED FLOOR BOARD IAW SRM 51-30-2, REMOVED SEAT TRACK OUT OF LIMITS IAW SRM 51-30-2; FABRICAETD NEW SEAT TRACK SECTION, LOCATED AND DRILLED. IAW SRM 53-10-5. DRAWING 53 FX 1497 REV TREATED AND PRIMED IAW SRM 51-10-2; INSTALLED NEW SEAT TRACK SECTION IAW SRM 51-30-2 AND DRAWING F 53 FX 1479 REV S INSTALL FLOOR BOARD IAW SRM 51-30-2.

Part: SKIN — DENTED (BS 392 S20L) · airframe 40,187 hrs · 27,171 cycles

FUSELAGE LT SIDE, PROTRUDING DENT AT STA 392 ,STR 20L. EVALUATED DENT AND FOUND OUT OF LIMITS IAW SRM 53-30-1, CUT OUT DAMAGED AREA. FABRICATED DOUBLER REPAIR INTERNAL FILLER AND EXTERNAL FILLER IAW SRM 53-30-3 AND SRM 53-30-2 AND INSTALLED REPAIR PARTS IAW SRM 51-30-2.

Part: SKIN — DENTED (BS 338) · airframe 40,187 hrs · 27,171 cycles

FUSELAGE LH SIDE, DENT ON LAP SEAM AT STA 338, STR 24R. DENT LOCATED ON LAP SEAM & FOUND OUT OF LIMITS IAW SRM 53-30-1. CUT OUT DAMAGE IAW SRM 53-30-3. FABRICATED FILLER AND DOUBLER IAW SRM 53-30-3. INSTALLED REPAIR WASHER IAW SRM 51-30-8, TREATED AND PRIMED AREA AND DOUBLER REPAIR IAW SRM 51-10-2, INSTALLED DOUBLER REPAIR IAW SRM 53-30-3 AND 51-30-2.

Part: INDICATOR — FAILED (COCKPIT) · airframe 39,234 hrs · 26,398 cycles

DURING CLIMB-OUT STBY ATT IND 5 MORE NOSE UP THAN CAT/FO ADI'S SHORTLY THERE AFTER STBY ATT IND RAPID PRECESSION TO -25 WITH INAPPRECIATE BANK INDICATIONS. FOR TROUBLESHOOTING RECAGED TWICE RESET BREAKER. PROBLEM REOCCURRED. REPLACED STANDBY ARTIFICIAL HORIZON PER 727 AMM 34-25 -011-4. CHECKS NORMAL. R/I FROM FACT PREMATURE REMOVAL/INSTALLATION OFF MFG H321AKM1, POS ONL SRL 8236, TAG 78861B ON MFG H321AKM1, SRL 7030 TAG 126A10.

Part: DOOR — LEAKING (MAIN PAX) · airframe 39,015 hrs · 26,226 cycles

APPEARED TO LOOSE PRESSURIZATION PASSING 12,000' LEVELED AT 14,000' CABIN AT 9500, DESCENDED TO 10,000 AND WAS UNABLE TO GET PRESSURE IN CABIN BELOW 8,000. HEARD LOUD AIR NOISE, CHECKED MAIN CABIN DOOR, FOUND AIR LEAKING AROUND DOOR. RETURNED TO MEM. ADJUSTED UPPER DOOR GUIDE ARM 1/2 TURN OUT IAW B727-200 AMM 52-411-001-5. REMOVED AND REPLACED THE TEFLON RUB STRIP AND MID CENTERING GUIDE ADJUSTED UPPER DOOR GUIDE ARM ROD END, REF 727-200MM 52-11-001-5. REINSTALLED ESCAPE SLIDE. OPS CHECKS GOOD.

Part: SERVO — UNKNOWN (AUTO PILOT) · airframe 38,923 hrs · 26,149 cycles

AFTER DEPARTING MIA WHILE CLEANING UP AIRCRAFT STAB CRUISE TRIM CIRCUIT BREAKER POPPED. CLIMBING THROUGH 17500 IT WAS DISCOVERED AIRCRAFT COULD NOT BE TRIMMED DOWN BELOW 0. REVIEWED QRH FOR GUIDANCE AND CONTACTED GOC AND MOCC FOR SUGGESTIONS. DECISION WAS MADE TO RETURN TO MIA BECAUSE OF AIRSPEED/ALTITUDE RESTRICTIONS, MODERATE TURBULENCE EN ROUTE AND UNCERTAINTY OF AIRCRAFT MALFUNCTION. REMOVED AND REPLACED AUTO PILOT STAB TRIM SERVO MOTOR PER MM 22-11-021-2, OPS CKS GOOD ON GROUND PER MM 22-11-021-2.

Part: STRINGER — CORRODED (BS 700-720 S26R) · airframe 38,301 hrs · 25,654 cycles

CORROSION FOUND AT STRINGER 26R BETWEEN STA 700 TO STA 720 WAS OUT OF LIMITS AFTER CORROSION REMOVAL. REMOVED DAMAGED AREA (SECTION OF STRINGER) IAW SRM 53-10-3, FIG 1. FABRICATED REPAIR PART IAW SRM 53-10-3, INSTALLED ALL REPAIR PARTS IAW SRM 51-30-2. REPAIR IS CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.

Part: REPAIR — UNKNOWN · airframe 38,290 hrs · 25,638 cycles

FOUND SINGLE RIVET REPAIR LOCATED AT STA 184 FWD OF NOSE ACCESS DOOR, REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA.

Part: REPAIR — MISINSTALLED (BS 1070) · airframe 38,290 hrs · 25,638 cycles

FOUND PREVIOUSLY REPAIR INSTALLED AT STA 1070, STR 21R IS NOT CONFORMED TO FAA APPROVED DATA, REMOVE EXISTING REPAIR AND FABRICATED REPAIR PARTS IAW SRM 53-30-3 FIG 3, INSTALLED ALL REPAIR PARTS IAW SRM 51-30-2 AND REPAIR IS CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.

Part: SKIN — BULGED (BS 500-520 S28R) · airframe 38,290 hrs · 25,638 cycles

FOUND FWD LOWER RT EXTERNAL FUSELAGE BETWEEN BS 500-520 STR 28R, SKIN BULGING. REPAIRED IAW SRM 53-10-1 AND 53-10-3 FIG 1, REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — DAMAGED (BS 500 S28-29R) · airframe 38,290 hrs · 25,638 cycles

FWD LOWER RT EXTERIOR FUSELAGE HAVE MULTIPLE LIGHTNING STRIKES BETWEEN BS 480-700 FROM STR 27R TO STR 30R, FURTHER EVALUATION FOUND DAMAGE AT STA 500 BETWEEN STR 28R TO STR 29R IS OUT OF LIMIT. REMOVE SKIN, INTERCOSTAL IAW SRM 51-30-2. FABRICATED DOUBLER, FILLER IAW SRM 53-30-3 AND REINSTALLED REPAIR PARTS IAW SRM 53-30-3. REPAIR IS CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.

Part: REPAIR — MISINSTALLED (CARGO DOOR) · airframe 38,290 hrs · 25,638 cycles

FOUND PREVIOUSLY REPAIR INSTALLED AT FWD CARGO COMPT DOOR EXTERNAL SKIN IS NOT CONFORMED WITH FAA APPROVED DATA. REMOVED EXISTING REPAIR, FABRICATED REPAIR DOUBLER IAW SRM 52-00-3, INSTALLED DOUBLER REPAIR IAW SRM 51-30-2, REPAIR IS CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.

Part: REPAIR — MISINSTALLED (BS 1166) · airframe 38,290 hrs · 25,638 cycles

FOUND PREVIOUSLY REPAIR INSTALLED AT STA. 1166 STR 30 IS NOT CONFORMED TO FAA APPROVED DATA. REMOVED EXISTING REPAIR, FABRICATED AND INSTALLED REPAIR IAW SRM 53-30-3, FIG 3. REPAIR IS CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.

Part: REPAIR — NONE · airframe 38,290 hrs · 25,638 cycles

FOUND PREVIOUSLY REPAIR INSTALLED AT STA 970 STR 29R WAS ACCOMPLISHED IAW S/B 727-53-0179 BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SIZE, SHAPE, FASTENER SPACING AND NUMBERS, MATERIAL TYPE AND THICKNESS, GENERAL WORKMANSHIP AND REPAIR IS CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.

Part: REPAIR — UNKNOWN · airframe 38,290 hrs · 25,638 cycles

FOUND PREVIOUSLY REPAIR INSTALLED AT STA 265 STR 17L WAS ACCOMPLISHED IAW SRM 53-30-3 FIG 1 BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, FASTENER SPACING AND NUMBERS, MATERIAL TYPE AND THICKNESS. GENERAL WORKMANSHIP AND REPAIR IS CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.

Part: REPAIR — NONE · airframe 38,290 hrs · 25,638 cycles

FOUND PREVIOUSLY REPAIR INSTALLED AT STA 950D STR 29R WAS ACCOMPLISHED IAW EA 7- 5310-27736 BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, FASTENER SPACING AND NUMBERS, MATERIAL TYPE AND THICKNESS, GENERAL WORKMANSHIP AND REPAIR IS CLASSIFED AS MAJOR PER FEDEX GMM 6-2-100.

Part: REPAIR — UNKNOWN · airframe 38,290 hrs · 25,638 cycles

FOUND PREVIOUSLY REPAIR INSTALLED FWD OF BOTH HINGE CUTOUTS OF THE LT MAIN ENTRY DOOR WAS ACCOMPLISHED IAW EO 7-5330-7-2345 PT2 BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SIZE AND SHAPE, FASTENER SPACING AND NUMBERS, MATERIAL TYPE AND THICKNESS. GENERAL WORKMANSHIP AND REPAIR IS CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.

Part: REPAIR — UNKNOWN · airframe 38,290 hrs · 25,638 cycles

FOUND PREVIOUSLY REPAIR INSTALLED ON STA 700 STR 29L WAS ACCOMPLISHED IAW SRM 53-30-3 FIG 3. BASED ON AN EXTERNAL VISUAL EVAUATION CONSISTS OF LOCATION, SHAPE, SIZE, FASTENER SPACING AND NUMBERS, MATERIAL TYPE AND THICKNESS. GENERAL WORKMANSHIP, REPAIR IS CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.

Part: REPAIR — MISINSTALLED (CARGO DOOR) · airframe 38,290 hrs · 25,638 cycles

FOUND PREVIOUSLY REPAIR INSTALLED AT AFT LOWER CARGO COMPT DOOR WAS NOT CONFORMED TO FAA APPROVED DATA, PERFORMED REPAIR IAW SRM 52-00-3 FIG 3 AND SRM 51-30-2, REPAIR IS CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.

Part: REPAIR — NONE · airframe 38,290 hrs · 25,638 cycles

FOUND PREVIOUSLY REPAIR INSTALLED AT STA 1130 STR 30 WAS ACCOMPLISHED IAW SRM 53-30-3 FIG 1 BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, FASTENER SPACING AND NUMBERS, MATERIAL TYPE AND THICKNESS, GENERAL WORKMANSHIP AND REPAIR IS CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.

Part: NONE — NONE · airframe 38,290 hrs · 25,638 cycles

FOUND PREVIOUSLY REPAIR INSTALLED AT STA 675 STR 18R WAS ACCOMPLISHED IAW SRM 53-30-3 FIG 1 BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, FASTENER SPACING AND NUMBERS, MATERIAL TYPE AND THICKNESS, GENERAL WORKMANSHIP AND REPAIR IS CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.

Part: NONE — NONE · airframe 38,290 hrs · 25,638 cycles

FOUND PREVIOUSLY REPAIR INSTALLED AT STA 277 STR 20R WAS ACCOMPLISHED IAW SRM 53-30-3 FIG 1 BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, FASTENER SPACING AND NUMBERS, MATERIAL TYPE AND THICKNESS, GENERAL WORKMANSHIP AND REPAIR IS CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.

Part: REPAIR — UNKNOWN · airframe 38,290 hrs · 25,638 cycles

FOUND PREVIOUSLY REPAIR INSTALLED AT NR 6 KRUGER FLAP WAS ACCOMPLISHED IAW SRM 57-50-3. BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, FASTENER SPACING AND NUMBERS, MATERIAL TYPE AND THICKNESS, GENERAL WORKMANSHIP AND REPAIR IS CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.

Part: REPAIR — NONE · airframe 38,290 hrs · 25,638 cycles

FOUND PREVIOUSLY REPAIR INSTALLED AT STA 1050 STR 27R WAS ACCOMPLISHED IAW EA 7- 5330-70493 BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, FASTENER SPACING AND NUMBERS, MATERIAL TYPE AND THICKNESS, GENERAL WORKMANSHIP AND REPAIR IS CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.

Part: NONE — NONE · airframe 38,290 hrs · 25,638 cycles

FOUND PREVIOUSLY REPAIR INSTALLED AT STA 320 STR 21R WAS ACCOMPLISHED IAW SRM 53-30-3 FIG 1 BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, FASTENER SPACING AND NUMBERS, GENERAL WORKMANSHIP AND REPAIR IS CLASSIFIED AS MAJOR PER FEDEX FEDEX GMM 6-2-100.

Part: NONE — NONE · airframe 38,290 hrs · 25,638 cycles

FOUND PREVIOUSLY REPAIR INSTALLED AT STA 243 STR 20R WAS ACCOMPLISHED IAW SRM 53-30-3 FIG 1 BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SIZE, SHAPE, FASTENER SPACING AND NUMBERS, MATERIAL TYPE AND THICKNESS, GENERAL WORKMANSHIP AND REPAIR IS CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.

Part: REPAIR — UNKNOWN · airframe 38,290 hrs · 25,638 cycles

FOUND PREVIOUSLY REPAIR INSTALLED ON NR 4 KRUGER FLAP WAS ACCOMPLISHED IAW SRM 57-50-3 FIG 3 BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, FASTENER SPACING AND NUMBERS, MATERIAL TYPE AND THICKNESS. GENERAL WORKMANSHIP, REPAIR IS CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.

Part: NONE — NONE (NONE) · airframe 38,290 hrs · 25,638 cycles

FOUND PREVIOUSLY REPAIR INSTALLED ON NR 5 KRUGER FLAP WAS ACCOMPLISHED IAW SRM 57-50-3 FIG 3 BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, FASTENER SPACING AND NUMBERS, MATERIAL TYPE AND THICKNESS. GENERAL WORKMANSHIP AND REPAIR IS CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.

Part: REPAIR — UNKNOWN · airframe 38,290 hrs · 25,638 cycles

FOUND PREVIOUSLY REPAIR INSTALLED ON STA 660 STR 26L WAS ACCOMPLISHED IAW EA 7-5330-55769A BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, FASTENER SPACING AND NUMBERS, MATERIAL TYPE AND THICKNESS. GENERAL WORKMANSHIP AND REPAIR IS CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.

Part: REPAIR — NONE · airframe 38,290 hrs · 25,638 cycles

FOUND PREVIOUSLY REPAIR INSTALLED AT AFT EDGE OF AFT LOWER CARGO DOOR CUTOUT WAS ACCOMPLISHED IAW EA 7-5330-56260 BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, FASTENER SPACING AND NUMBERS, MATERIAL TYPE AND THICKNESS, GENERAL WORKMANSHIP AND REPAIR IS CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.

Part: REPAIR — NONE · airframe 38,290 hrs · 25,638 cycles

FOUND PREVIOUSLY REPAIR INSTALLED AT STA 685 STR 29R WAS ACCOMPLISHED IAW SRM 53-30-3 FIG 3 BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, FASTENER SPACING AND NUMBERS, MATERIAL TYPE AND THICKNESS, GENERAL WORKMANSHIP AND REPAIR IS CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.

Part: REPAIR — UNKNOWN · airframe 38,290 hrs · 25,638 cycles

FOUND PREVIOUSLY REPAIR INSTALLED AT STA 1050 STR 29L WAS ACCOMPLISHED IAW SRM 53-30-3 FIG 3 BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SIZE, SHAPE, FASTENER SPACING AND NUMBERS, MATERIAL TYPE AND THICKNESS. GENERAL WORKMANSHIP AND REPAIR IS CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.

Part: REPAIR — UNKNOWN · airframe 38,290 hrs · 25,638 cycles

FOUND PREVIOUSLY REPAIR INSTALLED AT STA 988 STR 29L WAS ACCOMPLISHED IAW SB 727-53-0179 BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, FASTENER SPACING AND NUMBERS, MATERIAL TYPE AND THICKNESS. GENERAL WORKMANSHIP AND REPAIR IS CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.

Part: FIRE LOOP — FALSE ACTIVATION (NR 2 ENGINE) · airframe 38,122 hrs · 25,515 cycles

MASTER FIRE WARNING LIGHT ILLUMINATED IN FLIGHT INTERMITTENTLY. NO OTHER FIRE INDICATIONS. NR 2 ENGINE LOOP WILL NOT TEST REF AMM 26-11-000-1. REMOVED AND REPLACED ENG NR 2 SENSING ELEMENT IAW MM 26-11-012-4. OPS TEST NR 2 FIRE LOOP PER MM 26-11-000-5. OPS TEST NORMAL ON GROUND PER JRH RAN NR 2 ENG ALL INDICATION WERE NORMAL. OK TO CONTINUE.

Part: SWITCH — OUT OF ADJUST (CARGO DOOR) · airframe 37,541 hrs · 25,035 cycles

MAIN CARGO DOOR B LIGHT CAME ON AT 16,000 FT, DURING CLIMB. FLAPS WERE RETRACTED ALREADY. NO LOSS OF PRESSURIZATION. LIGHT WENT OUT AT 7000 FT DID NOT COME BACK ON. FOUND MAIN CARGO DOOR 'B' SWITCH OUT OF ADJUSTMENT ('A' DOOR LIGHT CAME ON BEFORE 'B' LIGHT) ADJUSTED 'B' SWITCH SO THAT BOTH 'A' AND 'B' COME ON AT THE SAME TIME AND ARE WITHIN SPECIFIED LIMITS PER NASI 727-MM14 SUPPLEMENT MANUAL. A/C OK FOR SERVICE. RII

Part: DOOR — OUT OF ADJUST (CARGO) · airframe 37,525 hrs · 25,019 cycles

ON CLIMBOUT AT FL230 AND 310 KTS MAIN CARGO DOOR-B ILLUMINATED. DECLARED EMERGENCY AND RTB. LIGHT WENT OUT DESCENDING THRU FL180 AND 250 KTS, MEL 09APR05. RELEASED FOR SERVICE PER MEL/CDL: 52-15-01 CATEGORY: C EXPIRATION: 19APR05 B-LOOP MEL'D REF MEL 52-15-01: MAIN CARGO DOOR WARNING LIGHT SYS B-INOP. VERIFY DOOR CLOSED AND LOCKED PRIOR TO EACH BLOCKOUT. CYCLED DOOR & VERIFED CLOSED AND LOCKED. ADJUSTED B-SWITCH AFT CABLE ASSY PER NASI MM 52-30-00. OPS CKS NORMAL.

Part: BATTERY — DISCHARGED (CABIN) · airframe 36,764 hrs · 24,434 cycles

COCKPIT EMERGENCY EXIT LIGHT REMAINS ON. INSTALLED NEW BATTERIES IN COCKPIT EMERGENCY LIGHT ASSY PER STD MX PRAC & SECURED LIGHT BRACKET WHICH WAS STARTING TO COME LOOSE. EMERGENCY LIGHTS OPS CHECK NORMAL.

Part: SKIN — GOUGED (FUSELAGE) · corrosion level 2 · airframe 36,154 hrs · 23,951 cycles

EMPENNAGE SKIN GOUGED, STA 1348, 12 INCHES ABOVE LEFT AFT AIRSTAIR CORNER. REMOVED DAMAGE AT SKIN AT BS 1348. FOUND TO BE OUT OF LIMITS. FABRICATED THE REPAIR DOUBLER, AND INSTALLED THE REPAIR PART IAW SRM 54-30-3.

Part: SKIN — DENTED (FUSELAGE) · airframe 36,154 hrs · 23,951 cycles

DENT IN SKIN AT EDGE OF MAIN CARGO DOOR CUTOUT BS 620 ABOVE STR 17L. REWORKED DENT IN SKIN AT EDGE OF MAIN CARGO DOOR CUTOUT, BS 620, ABOVE STR 17L PER EA 7-5330-70490.

Part: SKIN — DENTED (FUSELAGE) · airframe 36,154 hrs · 23,951 cycles

DENT IN SKIN BS 268 BETWEEN STR 16-17L. DENT IN SKIN AT BS 268 BETWEEN STR 16-17L WAS OUT OF LIMITS. AREA WAS REPAIRED PER SRM 53-30-3 FIG 1.

Part: PRESSURE PANEL — GOUGED (FUSELAGE) · airframe 36,154 hrs · 23,951 cycles

NOSE LANDING GEAR FWD RT PRESSURE ACCESS PANEL SKIN CUTOUT IS GOUGED. REPAIRED FWD RT PRESSURE ACCESS PANEL SKIN AT NOSE LANDING GEAR. ALL WORK DONE IAW SRM 51-40-2.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,154 hrs · 23,951 cycles

CORROSION ON FRAME AT STA 1010, STR 29R TO 29L, WL 138. BLENDED OUT CORROSION ON FRAME AT STA 1010, STR 29R TO 29L, WL 138. FOUND OUT OF LIMITS I.A.W. BOEING 727 SRM 53-10-1. REPAIRED BLEND OUTS PER BOEING 727 SRM 53-10-4, FIG 15, BOEING 727 SRM 51-10-6.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 36,154 hrs · 23,951 cycles

GRAVEL DAMAGE ON FUSELAGE BELLY SKIN, BS 1050-1060 BETWEEN STR 26R AND 28R. REMOVED DAMAGED SKIN AT BS 1050-1060 BETWEEN STR 26 RT AND 28 RT AND INSTALLED REPAIR DOUBLER PER SRM 53-30-3 & EA 7-5330-70493.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,154 hrs · 23,951 cycles

CORROSION ON WEB AT STA 986, STR 29R, WL 148 . REPAIRED WEB AT B.S. 986, STR 29R, WL 148 IAW SRM 53-10-4 FIG 15.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,154 hrs · 23,951 cycles

STRINGER HAS CORROSION, WHILE WORKING ON CARD NR N00150, FOUND CORROSION ON STRINGER 27R AT BS 1056.

Part: FITTING — CORRODED (NLG DOOR) · corrosion level 2 · airframe 36,154 hrs · 23,951 cycles

CORROSION ON UPPER SURFACE OF NLG DOOR UPPER FITTING ON BS 227.9 BULKHEAD LBL 8, WL 180. REMOVED NLG UPPER FITTING AND LOCATED AND BACK DRILLED NEW FITTING. INSTALLED FITTING WET WITH SEALANT IAW SRM 51-30-2.

Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,154 hrs · 23,951 cycles

CORROSION ON LT KEELBEAM CORD AT STA 950D, WL 148. ACCESSED LT KEELBEAM. REMOVED CORROSION ON L/HKEEL BEAM CORD AT BS 950D+15, WL 148. CORROSION FOUND TO BE OUT OF LIMITS. REPAIRED KEELBEAM IAW FED EX EA 7- 5310-72313. PERFOMRED SHEAR TIE REPAIR AND REINSTALLED. ALL ACCESS IAW SRM 51-30- 2, 53-10-1, 53-10-4.

Part: HYDRAULIC LINE — LOOSE (HYD SYSTEM) · airframe 35,260 hrs · 23,253 cycles

RIGHT GEAR FAILED TO RETRACT AFTER T/O. GEAR DOOR INTRANSIT LIGHT FLICKERED GREEN, RIGHT GEAR LIGHT REMAINED ILLUM'D WITH THE GEAR HANDLE IN THE OFF POSITION. SECURED LOOSE HYDRAULIC LINE ON SEQ VALVE AND RECENTERED RIGHT GEAR UPLOCK MECH MG, OPS CHECK OK PER MM 32-32-000-5.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 35,149 hrs · 23,154 cycles

AFTER GEAR RETRACT, GEAR HANDLE IN UP POSITION, R/GEAR RED WARN LIGHT REMAIN ON. PERFORMED TEST OF R/GEAR UPLOCK IND PER MM 32-61-081-4. OPS CHECK NORMAL. OK FOR SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE)

CORROSION ON PREVIOUS REPAIR TO FLOORBEAM UPPER FLANGE BS 360, RBL 8 - LBL 8, WL 208. *S/D* REMOVED AND REPLACED PER FEDEX EA 7-5310-5620.

Part: SEAT TRACK — CORRODED (CABIN)

CORROSION ON SEAT TRACK FLANGE AT LBL 24, WL 208 AT BS 774.5 - 779. *S/D* REMOVED AND REPLACED FLANGE ON LONGITUDINAL BEAM PER FEDEX EA 7-5310-56251.

Part: SHEAR TIE — CORRODED (FUSELAGE)

CORROSION C53-111-01-03 ON SHEAR TIE BS 1110, LBL 1, WL 145. *S/D* REMOVED AND REPLACED PER FEDEX SRM 51-10-6, 53-10-4, 53-30-3 AND EA 7-5310-56295.

Part: FLOORBEAM — CORRODED (FUSELAGE)

CORROSION (C53-113-01, 2) ON 1130 FLOORBEAM LOWER FLANGE, ON AND AROUND THE NUT CLIPS / FASTENER HOLES FROM LBL 40 TO RBL 50, WL 201. *S/D* REMOVED AND REPLACED FAB PER 51-20-1, 51-10-2, 51-30-2.

Part: SKIN — DENTED (FUSELAGE)

AFT LWR CORNER OF MAIN CARGO DOOR WAS DAMAGED BY LOADER DENT IN FUSELAGE JUST AFT AND BELOW MAIN CARGO DOOR. *S/D* REMOVED AND REPLACED PER IAW FEDEX SRM 53-30-1, EA 7-5330-55769A AND SRM 53-30-3 FIG 3.

Part: SKIN — DENTED (FUSELAGE)

DENT WITH CREASE IN SKIN BS 673, 3 INCHES BELOW STR 18R. REMOVED AND REPLACED PER FEDEX SRM 53-30-3 FIG 1. REMOVED AND REPLACED PER FEDEX SRM 53-30-3 FIG 1.

Part: FRAME — DENTED (FUSELAGE)

FRAME DENTED AT BS 1030 BETWEEN STR 25 & 26 RT SIDE. *S/D* REMOVED AND REPLACED PER FEDEX SRM 51-40-3.

Part: FRAME — MISDRILLED (FUSELAGE)

FIGURE EIGHT HOLE IN FRAME BS 700 AT STR 7R. *S/D* REMOVED AND REPLACED PER IAW FEDEX SRM 53-10-4.

Part: FRAME — DENTED (FUSELAGE)

FRAME DENTED AT BS 970, STR 25L. *S/D* REMOVED AND REPLACED PER FEDEX SRM 53-10-1, 51-40-3.

Part: FRAME — DENTED (FUSELAGE)

FRAME DENTED AT BS 950R, STR 25L. *S/D* REMOVED AND REPLACED PER FEDEX SRM 53-10-1, 51-40-3.

Part: FRAME — PUNCTURED (FUSELAGE)

FRAME PUNCTURED AT BS 1070, RBL 20, UNDER FLOOR TO SIDEWALL SUPPORT. *S/D* DRILLED UP PUNCTURES IN FRAME TO .1875 INCH DIA AND PLUGGED WITH RIVETS PER FEDEX SRM 53-10-1 DETAIL 4.

Part: FRAME — DENTED (FUSELAGE)

FRAME DENTED AT BS 1050, RBL 26. *S/D* REMOVED AND REPLACED PER FEDEX SRM 51-40-3, 53-10-1.

Part: FRAME — DENTED (FUSELAGE)

FRAME DENTED AT BS 1010, STR 26 RT SIDE. *S/D* REMOVED AND REPLACED PER IAW FEDEX SRM 53-10-1, 51-40-3.

Part: STRINGER — GOUGED (FUSELAGE)

STRINGER 6R IS DAMAGED IN RADIUS, BS 420 - 440. *S/D* REMOVED AND REPLACED STR 6R AND BEAR STRAP PER IAW FEDEX SRM 53-10-3, 53-30-3 AND EA 7-5310-56263.

Part: FRAME — GOUGED (FUSELAGE)

MECHANICAL DAMAGE ON FRAME, BS 440 AT STR 6R. *S/D* REMOVED, REPLACED AND FAB PER IAW FEDEX SRM 51-20-1, 51-10-2, 53-10-4, 51-30-2.

Part: CLAMP — LOOSE (NR 3 ENGINE)

DURING CLIMBOUT, AFT TURN ON ENG 3 BLEED AIR SWITCH FOR PRESS, AN ILLUMINATION OF THE ENG 3 STRUT OVERHEAT LIGHT. FOUND 2 LOOSE CLAMPS AT PRECOOLER, 2 MORE LOOSE FWD OF PRECOOLER. RAN ENG, NO LEAKS OR WARNING LIGHTS ON. OK FOR SERVICE.

Part: ENGINE — MALFUNCTIONED (NR 3)

99-154 - DURING CLIMB-OUT, NR 3 ENG OIL LOW PRESS/FILTER BYPASS LIGHT CAME ON. SHUT DOWN ENGINE IN FLT.

Part: BYPASS SWITCH — MALFUNCTIONED (NR 3 ENGINE)

99-155 - ON CLIMB-OUT PASS 7000 MSL, NR 3 ENGINE OIL PRESS LOW/FILTER BYPASS LIGHT CAME ON. REPLACED FILTER AND SEALS PER 79-00-00. REMOVED AND REPLACED OIL BYPASS SWITCH AS PERCAUTION.

Part: CONNECTOR — BENT (NR 5 LE SLAT)

AIR TURNBACK, FLT CREW REPORT LEAD EDGE SLAT NR 5 INTRANSIT LIGHT REMAINS ON. *S/D* FOUND BENT PIN CONN D5226P. REPLACED PER WIRING DIAGRAM MANUAL 31-31-04. OPER CK GOOD PER MM 27-82-000-0.

Part: ACTUATOR — FAILED (NR 2 LE SLAT)

DURING FLAP RETRACT, NR 2 SLAT ON LEFT WING WOULD NOT RETRACT. ACCOMPLISH RED TAB PROC, BUT NR 2 SLAT WOULD NOT RETRACT. *S/D* REMOVED AND REPLACED NR 2 LEAD EDGE SLAT ACTUATOR PER MM 27-81-032-4. LEAK AND OPERATION CHECK NORMAL.

Part: KEEL BEAM — CORRODED (BS 950-990)

NR 0444 - CORROSION ON LT KEEL BEAM AT BS 950F PLUS 5 TO BS 990, LBL 6, WL 138. REMOVED CORROSION ON LT KEEL BEAM AT BS 950F PLUS 5 TO BS 990, LBL 6, WL 138 PER SR 27-53-023. ALL REPAIR WORK ACCOMPLISHED PER EA 7-5310-39912A.

Part: SHEAR TIE — CORRODED (BS 970)

NR 0453 CORROSION (C53-113-02) SHEAR TIE AT BS 970, LBL 7, WL 138. REMOVED AND REPLACED SHEAR TIE AT BS 970, LBL 7, WL 138 IAW FEDEX SRM 53-10-4.

Part: SUPPORT — CORRODED (BS 740)

740 BULKHEAD IN A/C BAYS WHERE KEEL BEAMS ATTACH (BOTH LT AND RT KEEL BEAMS) IS CORRODED. * S/D* REMOVED AND REPLACED BS 740 RT SKIN FORMER FROM RBL 7 TO 15 PER FEDEX SRM 51-30-2. REMOVED AND CORROSION ON BS 740 LT AT LBL 7, WL 144. ALODINED AND RESTORED PROTECTIVE FINISH TO ALL BARE METAL PER FEDEX M/M 51-20-151.

Part: SKIN — CORRODED (BS 680-692)

NR-0510 - WHILE WORKING NRO434 FOUND CORROSION ON BELLY SKIN OUT OF LIMITS AT BS 680 - 692 WL 149 RBL 11-12 IAW FEDEX SRM 53-30-1. REPAIRED BELLY SKIN AT BS 680 TO 692 WL149, RBL 11-12 IAW FEDEX SRM 53-30-3.

Part: FLOORBEAM — CORRODED (BS 328)

WHILE WORKING NR 0170 FOUND CORROSION ON FLOORBEAM BS 328, RBL 14, WL 208. *S/D* REPAIRED FLOORBEAM BS 328, RBL 14, WL 208 PER FED-EX SRM 53-10-8 FIG 9.

Part: STRINGER — CORRODED (BS 700-720)

CORROSION ON STRINGER 28L BETWEEN BS 700 TO 720. *S/D* REPAIRED STR 28L BETWEEN BS 700 TO 720 IAW FED-EX SRM 53-10-3.

Part: FLOORBEAM — CORRODED (BS 344)

WHILE WORKING NR 0173 FOUND FLOORBEAM AT BS 344, RBL 14, WL 208.1 CORRODED. *S/D* REPAIRED FLOORBEAM AT BS 344, RBL 14, WL 208.1 PER FEDEX REPAIR DRAWING SR 27-53-007.

Part: STRINGER — CORRODED (BS 670-675)

CORROSION (C53-113-01,1) ON STR 28 RT, BS 670 TO 675 FWD CARGO BAY. *S/D* REPAIRED STR 28 RT, BS 666 TO 680 PER FEDEX SRM 53-10-3.

Part: STRINGER — CORRODED (BS 682)

CORROSION (C53-113-01,1) ON STRINGER 27 RT, BS 682 FORWARD CARGO BAY. *S/D* REPAIRED STR 27 RT, BS 680 TO 690 IAW FEDEX SRM 53-10-3 FIG 1, DETAIL 1.

Part: SHEAR TIE — CORRODED (BS 990)

CORROSION (C53-113-02) SHEAR TIE AT BS 990, LBL 18, WL 139. *S/D* REPLACED SHEAR TIE AT BS 990, LBL 18, WL 139 IAW FED-EX SRM 53-10-4.

Part: FRAME — CRACKED (BS 560)

CRACK IN FRAME BS 560, LBL 8, WL 155 FWD CARGO BAY. *S/D* REPAIRED CRACKED FRAME AT BS 560, LBL 8, WL 155 PER FEDEX SRM 51-40-3. ALODINED, PRIMED AND PAINTED PER FEDEX MM 51-20-151.

Part: BEAM — CRACKED (PAX DOOR)

FWD ENTRY DOOR LOWER GATE BEAM IS CRACKED ABOVE BOTTOM FWD STOP PIN FITTING. *S/D* REPAIRED FORWARD ENTRY DOOR LOWER GATE BEAM IAW FED-EX DRAWING SR 27-52-015.

Part: SHEAR TIE — CORRODED (BS 990)

CORROSION (C53-113-02) SHEAR TIE AT BS 990, RBL 2, WL 138. *S/D* REPAIRED SHEAR TIE AT 990, RBL 2, WL 138 PER FED-EX SRM 53-10-4.

Part: STRINGER — CORRODED (BS 670 - 672)

CORROSION (C53-113-01,1) ON STRINGER 28 LT, BS 670-672 FWD CARGO BAY. *S/D* STRINGER 28 LT, BS 680-480 WAS BEING REPLACED ON NR 140, NO FURTHER ACTION REQUIRED.

Part: STRINGER — CORRODED (BS 557)

CORROSION (C53-113-0,1) ON STRINGER 28 LT, BS 557 FWD CARGO BAY. *S/D* REMOVED AND REPLACED STR 28 LT, BS 480-680 IAW FEDEX SRM 51-10-3.

Part: ENGINE — FAILED (NR 1)

AFTER T/O AT 1,500 ABOVE GRD LEVEL, NR 1 ENG COMPRESSOR STALLED AND FLAMED-OUT. TEMP 0 ANTI-ICE ON. COMPRESSOR STALL OCCURRED AS THROTTLE WERE BEING REDUCED TO QUIET EPR ON SHORT FINAL APPROACH. SYS WENT TO ABOUT 1000 PSI WITH LO PRESS. LIGHTS ON SYS-A RETURNED TO NORM PRESS AFTER LANDING. INSPECTED NR 1 ENG INTAKE, NO DAMAGE. UPON INSPECTION OF EXHAUST SECT, FOUND SEVERE COMPRESSOR - TURBINE AREA DAMAGE. REQUIRES NR 1 ENG CHG, NR 1 ENG REMOVED AND REPLACED PER M/M WORK CARD 70T0001 PG 1-27 COMPLETED JT8D ENG. DEPRESERVATION WORK CARD 72T002. COMPLETED 727-200 INTERMIXED ENG WORK CARD 70T003. REQUIRED ITEM INSPECT REQUIRED.

Part: ENGINE MOUNT — CRACKED (BS 1183)

AIRSTAIRS, FWD ENGINE MOUNT CASTING ON 1183 BULKHEAD LT SIDE HAS APPROX 10 INCH CRACK. REPLACED NR 1 ENGINE FWD MOUNT IAW EA 7-5410-28015 DATED 3-19-96. THIS WAS IN TUL ON PAE CLARIFICATION.

Part: RIB CHORD — CRACKED (WS 760)

LEFT 760 RIB CHORD AT BL 70.5, TOP FWD HOLE IND CRACK. ENLARGED TOP FWD HOLE. INSTALLED REPAIR PER DRAWING 65-68492-17, ESO 11782, DATED 2-24-96 AND EA.

Part: SKIN — CORRODED (BS 723)

LOWER FWD CARGO COMPT FUSE SKIN CORRODED STA 723 BETWEEN STR 28 LT AND RT. REMOVED CORROSION, SKIN THICKNESS BEYOND LIMITS. CUT OUT DAMAGE AND INSTALLED DOUBLER PER SRM 53-30-3.

Part: RIB CHORD — CRACKED (BS 760)

RT 760 RIB CHORD AT BL 70.5 TOP FWD HOLE IS CRACKED. ENLARGED TOP FWD HOLE TO REMOVE CRACK, HOLE ENLARGED TO .5 INCH DIA. CRACK REMOVED, INSTALLED 7075-T6 FREEZE PLUG PER SRM 51-10-7. INSTALLED SECOND OVERSIZED HI-LOK AT PLUG LOCATIONS PER ESO 11782.

Part: ANGLE — CORRODED (FLIGHT DECK)

FLOOR PLATE BULGING 36 FWD OF FLIGHT DECK ENTRY DOOR AT BL 0. REPLACED CORRODED CHORD ANGLE FROM LBL 6 TO RBL 18 PER SRM 51-40-4.

Part: STRINGER — CORROSION (BS 1040-1050)

CORROSION LT SIDE OF STR 28L STA 1040 TO 1050 IN AFT CARGO. CORROSION REMOVED, DAMAGE BEYOND MM LIMITS. REMOVED DAMAGED MATERIAL, INSTALLED DOUBLER AND STR REPAIR PER SRM 53-10-3.

Part: SKIN — CORRODED (FS 683)

LOWER FWD CARGO COMPT FUSE BELLY SKIN CORRODED AT STA 683 O/B OF STR 28L. CUT OUT DAMAGED SECTION OF SKIN. INSTALLED REPAIR DOUBLER PER SRM 53-30-3 FIG 3A SHEET 3A.

Part: FLANGE — CORRODED (BS 950)

CORROSION ON O/B FLANGE OF STR 29R AFT SIDE STA 950E. CUT OUT DAMAGED AREA AND INSTALLED STR SPLICE AND SKIN DOUBLER PER ESO 11782 DATED 2-21-96, AUTHORIZED BY FEDEX EA 7-5310-27736 DATED 2-29-96.

Part: FRAME — BENT (BS 720)

FWD LOWER CARGO COMPT STA 720 FRAME BENT BETWEEN STR 23 TO 24L. INSTALLED DOUBLER PER SRM 53-10-4.

Part: FLOOR BEAM — CORROSION (BS 360)

UPPER LOBE CORROSION ON FLOOR BEAM STA 360 TOP CHORD, AFT FLANGE, BOTTOM SIDE LBL 8. INSTALLED REPAIR PER SRM 53-10-2 FIG 3.

Part: FLOOR BEAM — CORRODED (BS 344)

FLOOR BEAM UPPER CHORD LOWER SURFACE CORRODED STA 344, LBL 50 - RBL 10, WL 200. INSTALLED FLOOR BEAM REPAIR PER STANDARD REPAIR DRAWING MANUAL SR 27-53-007.

Part: FLOOR BEAM — CORRODED (BS 344)

FLOOR BEAM UPPER CHORD LWR SURFACE CORRODED STA 344 LBL 50 TO RBL 10 WL 200. *S/D* INSTALLED FLOOR BEAM REPAIR PER STANDARD REPAIR DRAWING MANUAL SRM 27-53-007, NR0346.