N718FD

Part: SPAR — DAMAGED (ZONE 600) · airframe 38,610 hrs · 37,133 cycles

RT FR47 REAR SPAR HOLE, UNKNOWN IF BUSH EXISTS IN REAR FITTING . BORE OK AFT FACE OF HOLE WITH SURFACE FINISH REMOVED IAW SRM 51-75-20, NO BUSH PRESENT. NEW BOLT FITTED IAW SRM 51-40-21 SURFACE FINISH RESTORED IAW SRM 51-23-10 AND EO 6-5710- 7-3305 P2.

Part: SPAR — DAMAGED (ZONE 600) · airframe 38,610 hrs · 37,133 cycles

RT FR47 REAR SPAR HOLE, UNKNOWN IF BUSH EXISTS IN REAR FITTING . BORE OK AFT FACE OF HOLE, SURFACE FINISH REMOVED IAW SRM 51-75-20, NO BUSH PRESENT. NEW BOLT FITTED IAW SRM 51-40-21 SURFACE FINISH RESTORED IAW SRM 51-23-10 AND EO 6-5710- 7-3305 P2.

Part: STRUCTURE — DAMAGED (NR 2 SPOILER) · airframe 38,608 hrs · 37,131 cycles

RT WING NR 2 SPOILER FWD POINT OF OTBD EDGE WORN. REPAIRED ON EA6-5771-157943, CAT B.

Part: SKIN — DENTED (ZONE 100) · airframe 38,608 hrs · 37,131 cycles

SHALLOW DENT EVIDENT BETWEEN AFT CARGO DOOR AND BULK CARGO DOOR FR 66, STR 38R-39R, FRAME 66 RT BETWEEN STR 38-39 DENT REPAIRED IAW SRM 53-10-12, FIG 228 MAJOR REPAIR WITH SMR REQUIRMENTS CAT B IAW SRI 53-10-12-2-009-00.

Part: FRAME — DAMAGED (ZONE 100) · airframe 38,605 hrs · 37,129 cycles

RIGHT FRAME 47 REAR SPAR HOLE 'G' SHOWS EVIDENCE OF A CRACK INDICATION . THIS IS A PREVIOSULY REWORKED HOLE. MATERIAL REMOVED UNTIL CRACK INDICATION REMOVED STARTING AT BORE DIAMETER 0.259" TO FINAL BORE DIAMETER 0.560" IAW SRM 51-40-30 AND EA 6-5710-162973, PAGE 9.

Part: FRAME — DAMAGED · airframe 38,605 hrs · 37,129 cycles

RIGHT FRAME 47 REAR SPAR HOLE H SHOWS EVIDENCE OF MECHANICAL DAMAGE AT 9 O'CLOCK THROUGH REAR SPAR DEPTH. MECHANICAL DAMAGE REMOVED FROM HOLE IAW SRM 51-40-30 FINAL BORE DIAMETER -0.499" AND THE MAXIMUM ALLOWED IN EO 6-5710-7-3305, PT 2 IS 0.499" REFER TO RDAS 70566845/003/2012 FOR DETAILS.

Part: SKIN — CRACKED (ZONE 500) · airframe 38,605 hrs · 37,129 cycles

LEFT WING LOWER SKIN HOLE G SHOWS EVIDENCE OF A CRACK INDICATION AND MECHANICAL DAMAGE IN THE MAIN BORE. THIS IS A PREVIOUSLY REWORKED HOLE. HOLE G REWORKED UNTIL MECHANICAL DAMAGE REMOVED AND NO CRACK INDICATION STARTING AT A BORE DIAMETER OF 0.530"/13.462MM TO FINAL DIAMETER OF 0.685"/17.399 IAW SRM EA 6-5710-162973, PAGE 4 AND SRM 51-40-30.

Part: SPAR — DAMAGED (ZONE 500) · airframe 38,605 hrs · 37,129 cycles

LEFT WING FRM 47 HOLE C, MECHANICAL DAMAGE FOUND IN INTERNAL BORE OF FASTENER HOLE. MECHANICAL DAMAGE REMOVED IAW SRM 51-40-30 FINAL HOLE C DIAMETER IS 0.561"/14.249MM. REWORKED IAW EA 6-5710-162973, PAGE 2.

Part: SKIN — CRACKED (ZONE 500) · airframe 38,605 hrs · 37,129 cycles

LEFT WING LOWER SKIN HOLE F SHOWS EVIDENCE OF A CRACK INDICATION. THIS HOLE IS A PREVIOUSLY DIA 0.529 HOLE F REWORKED UNTIL CRACK REMOVED IAW SRM 51-40-30 AND EA 6-5710-162973, PAGE 3. HOLE F FINAL DIAMETER IS 0.561"/14.249MM.

Part: SKIN — DAMAGED (ZONE 500) · airframe 38,605 hrs · 37,129 cycles

RT WING LOWER SKIN HOLE 'S' BUSHINGS TO BE FABRICATED IAW ORIGINAL RAS INSTRUCTION. RT HOLE 'S' REWORKED IAW JPF STEP 2 IAW SRM 51-40-21. 3 BUSHINGS INSTALLED AT 19.1MM DIA IAW RDAS 70566845-003-2012 INSTRUCTION FOR RT SIDE HOLE NR1.

Part: FRAME — DAMAGED (ZONE 100) · airframe 38,605 hrs · 37,129 cycles

LEFT FRAME 47 REAR SPAR HOLE 'N' SHOWS EVIDENCE OF MECHANICAL DAMAGE AT 5 O'CLOCK THROUGH THE FORWARD FITTING AND MAIN SPAR DEPTHS. MECHANICAL DAMAGE REMOVED FROM HOLE "N" IAW SRM 51-40-30 AND THE FINAL BORE DIAMETER IS 0.5605". THE MAXIMUM ALLOWED IN EO 6-5710-7-3305 PT1 IS 0.562". REWORK ACCOMPLISHED IAW EA 6-5710-162973, PAGE 8.

Part: SPAR — DAMAGED (RT WING) · airframe 38,605 hrs · 37,129 cycles

RT WING FR47 REAR SPAR HOLE V POSSIBLE BUSH WITH X4 IMPACT DAMAGE MARKS IN REAR FITTING. NO BUSH WAS FOUND AND HOLE V REMOVED. MECHANICAL DAMAGE IAW SRM 51-40-30 AND EA 6-5710-162973, PAGE 11. FINAL DIAMETER IS 0.584"/14.834 MM.

Part: FRAME — DAMAGED (ZONE 100) · airframe 38,605 hrs · 37,129 cycles

LEFT FRAME 47 REAR SPAR HOLE 'H' SHOWS EVIDENCE OF MECHANICAL DAMAGE AT 6 O'CLOCK AND 12 O'CLOCK THROUGH THE FULL BORE DEPTH. MECHANICAL DAMAGE REMOVED IAW SRM 51-40-30. DAMAGE REMOVAL IN LIMITS WITH EO 6-5710-7-3305 P1 CARD 11 OF 42 ITEM 10.

Part: SPAR — CRACKED (RT WING) · airframe 38,605 hrs · 37,129 cycles

RIGHT WING HOLE L CRACK INDICATED BY NDT INSP CRACK IS ASSESSED AS A CORNER CRACK IN THE FRM AT THE INTERFACE WITH REAR ANGLE FITTING AT 1 O'CLOCK POSITION HOLE L REWORKED UNTIL NO CRACK INDICATION IAW SRM 51-40-30. FINAL HOLE DIAMETER 0.624"/15.849 AS DETAILED ON JPF. HOLE NTD AND BOLT REPLACED WITH HLT344VF16-34 IAW SRM 51-40-20. HOLE L COVERED BY EA 6-5710-162973 PART 2 FOR FURTHER INSPECTION.

Part: FRAME — DAMAGED (ZONE 100) · airframe 38,605 hrs · 37,129 cycles

LEFT FRAME 47 REAR SPAR HOLE 'I' SHOWS EVIDENCE OF MECHANICAL DAMAGE AT 12 O'CLOCK THROUGH THE FULL BORE DEPTH. HOLE "I" REWORKED MECHANICAL DAMAGE REMOVED STARTING AT A BORE DIAMETER OF 0.531"/13.487MM TO 0.561"14.249MM IAW SRM 51-40-30 AND EA 6-5710-162973 PAGE 6.

Part: SKIN — DAMAGED (ZONE 500) · airframe 38,605 hrs · 37,129 cycles

LEFT WING LOWER SKIN HOLE 'S' SHOWS EVIDENCE OF MECHANICAL DAMAGE FROM STEEL BUSHES THROUGH THE FULL BORE DEPTH. THIS IS A PREVIOUSLY REWORKED HOLE. HOLE 'S' REWORKED UNTIL MECHANICAL DAMAGE REMOVED STARTING AT A BORE DIAMETER OF 0.751"/19.075MM TO FINAL DIAMETER OF 0.7825"/19.8755MM IAW SRM 51-40-30 AND EA 6-5710-162973, PAGE 5.

Part: FRAME — DAMAGED (ZONE 100) · airframe 38,605 hrs · 37,129 cycles

LEFT FRAME 47 REAR SPAR HOLE 'M' SHOWS EVIDENCE OF MECHANICAL DAMAGE AT 11 O'CLOCK THROUGH THE FULL BORE DEPTH. MECHANICAL DAMAGE REMOVED FROM HOLE M STARTING AT A BORE DIAMETER OF 0.5295"/13.449MM TO FINAL DIAMETER OF 0.561"/14.249 MM IAW SRM 51-40-30 AND EA 6-5710-162973, PAGE 7.

Part: ANGLE — CRACKED (ZONE 100) · airframe 38,605 hrs · 37,129 cycles

LEFT MLG BAY FWD CUTOUT ANGLE CRACKED, REF SRM 53-15-13 FIG 4 ITEM 40. REPLACED ANGLE WITH NEW ANGLE FABRICATED IAW DWG A538122522 AND FITTED IAW SRM 51-40-21.

Part: FRAME — CRACKED (ZONE 200) · airframe 38,605 hrs · 37,129 cycles

FR 51 RT BODY FRAME FOUND CRACKED AT S26R BOLT HOLE. FRAME REPLACED IAW SRM 51-40-21 AND EA 6-5315-162967.

Part: FRAME — DAMAGED (ZONE 200) · airframe 38,605 hrs · 37,129 cycles

RIGHT FRAME 48, BOLT HOLE 2 FOUND EXCEED STANDARD SIZE. REWORKED IAW EA 6-5315-162967.

Part: FRAME — CRACKED (ZONE 200) · airframe 38,605 hrs · 37,129 cycles

FRAME 48 FOUND CRACKED AT S26R. UPPER FRAME SECTION REPLACED IAW EA 6-5315-162967 AND SRM 51-40-21.

Part: FRAME — CRACKED (ZONE 200) · airframe 38,605 hrs · 37,129 cycles

FRAME 49 FOUND CRACKED, REWORKED AND SHOULDERED BUSHING FITTED IAW EA 6-5315-162967 AND SRM 51-40-21.

Part: FRAME — DAMAGED (ZONE 200) · airframe 38,605 hrs · 37,129 cycles

RT FRAME 51, BOLT HOLE 2 FOUND EXCEED STANDARD SIZE. BOLT HOLE REWORKED IAW EA 6-5315-162967.

Part: FRAME — CRACKED (ZONE 200) · airframe 38,605 hrs · 37,129 cycles

FR 51 BOLT HOLE 4 FOUND CRACKED AND BOLT HOLE 1-3. FOUND EXCEED STANDARD LT FRAME 51 HOLE 4 FOUND CRACKED AND HOLES 1,2 AND 3 FOUND TO EXCEED STANDARD SIZE HOLES. REWORKED IAW EA 6-5315-162967, STAGES 10 TO 34 REF.

Part: FRAME — DAMAGED (ZONE 200) · airframe 38,605 hrs · 37,129 cycles

RT FRAME 53, BOLT HOLE 3 FOUND EXCEED STANDARD SIZE. HOLE REWORKED IAW EA 6-5315-162967, STAGES 35-40 REF.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 38,605 hrs · 37,129 cycles

FRAME 79 S44R FOUND DAMAGED AT FASTENER HOLE, REPAIRED IAW SRM 53-10-13, FIG 202. REPAIR CLASSIFIED AS MAJOR.

Part: CROSSBEAM — DAMAGED · airframe 38,605 hrs · 37,129 cycles

AFT CARGO HOLD, ROLLER TRACK REPLACEMENT RT -Y1470 AT FR57 CROSSBEAM AND FRAME SUPPORT FITTING FOUND WITH EXTRA X2 HOLES AND CLOSE TO EXISTING STRUCTUAL FASTENERS DUE TO UNAUTHORIZED TRACK REPAIR. INVESTIGATE AND RECTIFY IAW RELEVANT MANUAL SRM. AFT CARGO HOLD FR57 RT CROSSBEAM AND FRAME SUPPORT FITTING FREEZE PLUG REPAIR IAW SRM 51-40-51 AND EA 6-5300-162970.

Part: SKIN — DELAMINATED (RT ELEVATOR) · airframe 38,605 hrs · 37,129 cycles

RT ELEVATOR TOP AND BOTTOM SKIN INBD AFT CORNER, DELAMINATING & PAINT CRACKING. REPAIRED IAW AE 6-5520-162959 , RAS 70566197/003/2012. MAJOR REPAIR CAT A.

Part: SKIN — DENTED (ZONE 100) · airframe 38,605 hrs · 37,129 cycles

IMPACT DAMAGE OBSERVED IN THE LOWER FUSELAGE SKIN POCKET FWD OF TAIL STEADY LOCATION FR 85 REPAIR C/OUT IAW SRM 53-10-12, FIG 225.

Part: INTERCOSTAL — CRACKED (ZONE 100) · airframe 38,605 hrs · 37,129 cycles

INTERCOSTAL AT FR46-47, STR 42L CRACKED. REMOVED, REPLACED AND FITTED IAW SRM 51-40-21, MINOR REPAIR TO SECONDARY STRUCTURE.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 38,605 hrs · 37,129 cycles

SKIN AFT OF FR 80/82 MISREPAIRED. REMOVED REMAINING DAMAGE. REPAIRED IAW EA 6-5319-162972 CLASSIFIED AS MAJOR

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 38,605 hrs · 37,129 cycles

SKIN BETWEEN FRAMES 30-31, STRINGERS 41- 42, MISREPAIRED. REPAIRED IAW SRM 53-10-12 FIG 225, SH1.

Part: STRINGER — MISREPAIRED · airframe 38,605 hrs · 37,129 cycles

AFT CARGO BAY STRINGER 52L MISREPAIRED FR 59-61. REPAIRED IAW SRM 53-10-14, FIG 201. REPAIR CLASSIFED AS A MAJOR

Part: FRAME — DENTED (ZONE 100) · airframe 38,605 hrs · 37,129 cycles

DENT FOUND ON FRAME AT FR 20A RT AFT FACE AND BETWEEN STR 40 TO 41, LOWER SECTION, DENT AT FR 20A RT AFT FACE BETWEEN STR 40 TO STR 41 FOUND ACCEPTABLE IAW EA 6-5300-157946 AND RAS 70566040/003/2012. JPF ATTACHED, SHEET 1, STAGES 1-3.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 38,605 hrs · 37,129 cycles

SKIN AT FR 77, STR 53-56, MISREPAIRED. REPAIRED IAW SRM 53-10-12, FIG 228, SH3.

Part: DOOR — CRACKED (STAB) · airframe 38,605 hrs · 37,129 cycles

STABILIZER BAY DOOR 313AL CRACKED REPAIR IAW EA6-5241-157940 AND SRM 51-71-11, PARA 4D.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,605 hrs · 37,129 cycles

AFT HOLD FLOOR SUPPORT BETWEEN FR63 AND FR64 SECOND FROM LT SIDE FOUND CORRODED AT ANCHOR NUT LOCATIONS. AFT HOLD SUPPORT BEAM AT FR63 AND FR64 SECOND FROM LT SIDE, REPLACED IAW SRM 51-40-21.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,605 hrs · 37,129 cycles

AFT HOLD FLOOR SUPPORT BETWEEN FR63 AND FR 64 LT FROM CENTER FOUND CORRODED. REPLACED IAW SRM 51-40-21.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 38,605 hrs · 37,129 cycles

UPPER DECK FLOOR SUPPORT AT Y730 AND BETWEEN FRAMES 11 TO 14 FOUND CORRODED. REPLACED IAW SRM 51-40-01 AND DWG A53612214.

Part: ROLLER TRACK — MISREPAIRED (ZONE 100) · airframe 38,605 hrs · 37,129 cycles

CARGO BAY FLOOR ROLLER TRACK NR 2 LT SPLICE MISREPAIRED. REPLACED IAW SRM 51-40-21, SRM 51-72-10 AND AMM 25-52-21-04-01 CLASSIFIED AS MAJOR.

Part: BULKHEAD — CORRODED (ZONE 100) · corrosion level 2 · airframe 38,605 hrs · 37,129 cycles

REAR PRESSURE BULKHEAD FOUND CORRODED. ANGLE REPLACED ON EA 6-5300-157937 AND IAW DWG R53970640.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 38,605 hrs · 37,129 cycles

SKIN FR 57.1-57.2 S35-37R MISREPAIRED. REPAIRED IAW SRM 53-10-12, PARA 9, FIG 228. REPAIR CLASSED AS MAJOR WITH CAT B

Part: RIB — CRACKED (RT WING) · airframe 37,778 hrs · 36,375 cycles

RT WING RIB 5 LOWER FLANGE CRACK EVIDENT AT HOLE LOCATION 47 10 MM IN LENGTH WITHIN SPOT FACE REPAIR CARRIED OUT IAW EA 6-57-10-150903. INTERIM REPAIR INSTALLED, RIB 5 TO BE REPLACED.

Part: RIB — CRACKED (LT WING) · airframe 37,778 hrs · 36,375 cycles

LT WING RIB 5 LOWER FLANGE CRACK EVIDENT AT HOLE LOCATION 54 12MM IN LENGTH WITHIN SPOT FACE REPAIR CARRIED OUT IAW EA 6-5710-150903. INTERIM REPAIR INSTALLED, RIB 5 TO BE REPLACED BY 42500 FC.

Part: RIB — CRACKED (ZONE 500) · airframe 37,778 hrs · 36,375 cycles

LT WING RIB 5 LOWER FLANGE CRACK EVIDENT AT HOLE LOCATION 47, 5 MM IN LENGTH WITHIN SPOT FACE. REPAIR CARRIED OUT IAW EA 6-5710-150903. INTERIM REPAIR INSTALLED, RIB 5 TO BE REPLACED.

Part: PANEL — DELAMINATED (RT WING) · airframe 36,290 hrs · 35,404 cycles

RT WING T/E NR 2 DEFECTOR PANEL RUBBED TAPE LOOSE AND PEELING REPAIRED IAW EA 6-5720-136631. REMOVED T/E NR 2 DEFLECTOR TO FOM. REMOVED DAMAGED FOIL. APPLIED NEW ALUMINUM FOIL. INSTALLED HARDWARE IAW EA 6-5720-136631, N/R N00389 FOR ORIGINAL EA N/R N01255 FOR THE APPLICATION OF THE WITNESS MARK.

Part: DEFLECTOR — DELAMINATED (RT WING) · airframe 36,290 hrs · 35,404 cycles

RT WING T/E COVE PANEL NR 4 LOWER SURFACE METAL TAPE PEELING/MISSING REPAIRED IAW EA 6-5720-136631. REMOVED PANEL TO FOM. REMOVED ALUMINUM FOIL AND HARDWARE. APPLIED NEW ALUMINUM FOIL AND INSTALLED HARDWARE IAW EA 6-5720-136631,"WINGS - WING FLAP HINGE DEFLECTOR PANELS NR 572 CB; 572 GB; 672 AB; 672 CB; 672 GB AND 672 LB". REINSTALLED AND CLOSED RT WING T/E COVE PANEL NR 4 IAW AMMN 27-54-42-4. N/R N00389 FOR ORIGINAL EA. N/R N01255 FOR THE APPLICATION OF THE WITNESS MARK.

Part: PANEL — DELAMINATED (RT WING) · airframe 36,290 hrs · 35,404 cycles

RT WING T/E NR1 DEFLECTOR PANEL RUBBED TAPE LOOSE AND PEELING REPAIRED IAW EA 6-5720-136631. R & R WS HARDWARE IAW SRM 51-40-00. REMOVED AND INSTALLED OF RT WING T/E NR 1 DEFLECTOR PANEL ACCOPMPLISHED IAW AMM 27-54-41-4. NR N01255 FOR THE APPLICATION OF THE WITNESS MARK.

Part: DEFLECTOR — DELAMINATED (ZONE 600) · airframe 36,290 hrs · 35,404 cycles

RT WING T/E COVE PANEL NR 3 LOWER SURFACE METAL TAPE PEELING/MISSING REPAIRED IAW EA 6-5720-136631. REMOVED AND REINSTALLED HARDWARE IAW SRM 51-40-00. N/R N00389 FOR ORIGINAL EA. N/R N01255 FOR THE APPLICATION OF THE WITNESS MARK.

Part: WEDGE — CRACKED (RT WING TE FLAP) · airframe 36,290 hrs · 35,404 cycles

RT WING INBD FLAP AT RIB 25A; TAIL IS CRACKED. REPAIRED RT WING INBD FLAP AT RIB 25A TAIL BY FABRICATING AND BONDING CORE, SKIN, DOUBLER AND BRACKET IAW EA 6-5750-136629 TITLE "WINGS - RT INBD FLAP T/E WEDGE AT RIB 25A".

Part: DOUBLER — CORRODED (ZONE 100) · corrosion level 2 · airframe 36,290 hrs · 35,404 cycles

AFT PIT DOUBLER AT FRAME 58-62; LBL 56 TO RBL 56 HAS CORROSION. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-17-12. FORMED NEW DOUBLER SECTION IAW SRM 53-17-12, FIG 208 AND DWG A53973332. LOCATED AND DRILLED DOUBLER SECTION IAW SRM 51-72-10 AND SRM 51-40-44. INSTALLED SURFACE PROTECTION IAW SRM 51-21-10 AND 51-23-10, PG 2. INSTALLED IAW SRM 53-17-12, FIG 208, PGS 237/ 238.

Part: LOCK — WORN (ZONE 800) · airframe 36,290 hrs · 35,404 cycles

BULK CARGO DOOR EXTERIOR HANDLE HAS EXCESSIVE PLAY. DISPLACED INTERNAL SKIN; REMOVED 3 EA WEBS AND REMOVED LOCKING MECHANISM IAW SRM 51-40-02, PARA 6 AND AMM 52-34-21-4. INSTALLED INTERNAL SKIN; INSTALLED 3 EA WEBS AND INSTALLED LOCKING MECHANISM IAW SRM 51-40-21, PARA'S 6; 7; 13 AND AMM 52-34-21-4. REMOVED PANEL 161 DF TO FOM AND INSTALLED PANEL 161 DF IAW AMM 53-10-35-4, PG 2, PARA C,D. ADJUSTED BULK CARGO DOOR AND SAFETIED ADJUSTMENT AND PERFORMED A DOOR WARNING TEST IAW AMM 52-34-11-5. TOOL T8346F & T05101-3.

Part: STRINGER — CORRODED (ZONE 200) · corrosion level 2 · airframe 36,290 hrs · 35,404 cycles

FRAME 58-62; LBL 56; STRINGER CORRODED. REMOVED STRINGER AT LBL 56 FROM FRAME 58 TO 62 & STR SPLICE AT FRAME 58 IAW SRM 53-10-14. RECEIVED NEW STRINGER, LOCATED AND DRILLED NEW STR SECTION IAW SRM 51-40-44 & SRM 53-10-14. FABBED SPLICE IAW SRM 53-10-14; FIG 210A; PGS 204A/ 240B. REMOVED CORROSION AT STRINGER LBL 56 IAW SRM 51-74-10 AND FOUND TO BE OUT OF LIMITS. ORIGINAL THICKNESS 0.172", MATERIAL REMOVED 0.044", MATERIAL REMAINING 0.128" IAW SRM 53-10-10; TABLE 102; PG 175. ALODINED STR AND SPLICE IAW SRM 51-21-10, 1. PRIMED STRINGER AND SPLICE IAW SRM 51-23-10; PG 2. PAINTED SPLICE IAW SRM 51-25-10. INSTALLED NEW STRINGER AND SPLICE IAW SRM 53-10-14; FIG 201A; PGS 204A/ 204B.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 36,290 hrs · 35,404 cycles

AFT PIT FRAME 59-62; THE STR AT RBL 56 HAS CORROSION. REMOVED STR AT RBL 56 FROM FRAME 58 TO 62 AND STR SPLICE AT FRAME 58 IAW SRM 53-10-14. REMOVED CORROSION ON STR AT RBL 56 IAW SRM 51-74-10 AND FOUND TO BE OUT OF LIMITS. ORIGINAL MATERIAL 0.172"; MATERIAL REMOVED 0.034"; MATERIAL REMAINING 0.138" IAW SRM 53-10-14; PGS 204A/ 204B. DRILLED AND LOCATED NEW STRINGER. FABBED SPLICE IAW SRM 53-10-14; FIG 201A; PGS 204A/ 204B. ALODINED SPLICE AND STRINGER IAW SRM 51-21-10; PG 1. PRIMED SPLICE AND STRINGER IAW SRM 51-23-10, PG 2. PAINTED SPLICE IAW 51-23-10; PG 5. INSTALLED NEW STRINGER AND SPLICE IAW SRM 53-10-14; FIG 201A; PGS 204A/ 204B.

Part: STRUT — DENTED (ZONE 700) · airframe 36,290 hrs · 35,404 cycles

NOSE LANDING GEAR STRUT HAS DENTED TUBING, FWD AND JUST ABOVE THE GLAND NUT. COMPLIED WITH EA NR 6-3200-136622 "LANDING GEAR - NOSE GEAR SPEED SENSING TRANSDUCER WIRE LOOP TUBE".

Part: SKIN — DAMAGED (ZONE 100) · airframe 36,290 hrs · 35,404 cycles

EXTERNAL FUSELAGE LOWER SKIN HAS 6 EA FASTENER HEADS SHEARED OFF; 2 EA BLIND RIVETS FROM FRAME 59 TO FRAME 60; STRINGER 53L TO STRINGER 54L. REMOVED DOUBLER AND INSTALLED NEW DOUBLER IAW SRM 53-17-12 FIG 208. REMOVED CLIPS; SPLICES; ANTENNAS BASE; DRAINS; ANTI-COLLISION LIGHT SUPPORT TO FOM IAW SRM 51-40-21, PARA'S 6 & 7. INSTALLED CLIPS; SPLICES; ANTENNAS BASE; DRAINS; ANTI-COLLISION LIGHT SUPPORT FOR FOM IAW SRM 51-40-21, PARA'S 6 & 7. AODINED AND PRIMED EXTERION SKIN IAW SRM 51-21-10, PGS 1 & 2. PAINTED SKIN IAW AMM 51-75-10-8. APPLIED CIC IAW AMM 51-22-00-0.

Part: HEAT EXCHANGER — TORN (RIGHT) · airframe 36,290 hrs · 35,404 cycles

RT HEAT EXCHANGER INBD ROD ATTACH FLANGE IS TORN OUT. REMOVED AND REINSTALLED HEAT EXCHANGER IAW AMM 21-51-32-1. WELDED ATTACH FLANGE IAW CMM 21-53-24, PARAGRAPH 6-D. LEAK CHECK GOOD IAW AMM 21-51-00-5. OPS CHECK GOOD IAW AMM 21-51-00-5.

Part: CHANNEL — CRACKED (ZONE 100) · airframe 36,290 hrs · 35,404 cycles

E/E COMPARTMENT TRANSPONDER RACK AFT INBD SUPPORT TEE IS CRACKED. REMOVED CHANNEL IAW SRM 51-40-21, PARA 5. REMOVED SUPPORT TEE FROM CHANNEL IAW SRM 51-40-21, PARA 6. FABBED TEE IAW DWG A92531500, ISSUE A. ALODINED IAW SRM 51-21-10, PG 1. PRIMED IAW SRM 51-23-10, PG 1. PAINTED IAW SRM 51-75-10, PG 1. INSTALLED SUPPORT TEE ONTO CHANNEL IAW SRM 51-40-21, PARA 6. INSTALLED CHANNEL IAW SRM 51-40-21, PARA 5.

Part: SUPPORT BRACKET — CORRODED (TAIL CONE) · corrosion level 2 · airframe 36,290 hrs · 35,404 cycles

TAIL CONE CENTERING FITTING SUPPORT BRACKET AT FRAME 91; FROM STR 21L TO STR 21R IS CORRODED. REMOVED TAIL CONE CENTERING SPIGOT BRACKETS IAW SRM 51-40-21, PARA 5. R & R TAIL CONE CENTERING CONSOLE, PO NR 675534.1 IAW SRM 51-40-21, PARA 6 AND 7. REINSTALLED TAIL CONE CENTERING SPIGOT BRACKETS IAW SRM 51-40-21, PARA 5.

Part: SUPPORT BRACKET — CORRODED (ZONE 100) · corrosion level 2 · airframe 36,290 hrs · 35,404 cycles

THE SUPPORT BRACKET INSIDE THE AFT CARGO LOADING CONTROL ACCESS PANEL HAS EXFOLIATED CORROSION; LOCATED AT THE FWD/UPPER CORNER. CORROSION EXCEEDS 50 PERCENT ON THE ANGLE, FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16, PG 6, TABLE 102, CODE "K". FABRICATED NEW ANGLE AND MATERIAL ID IAW DWG A5397511, PO NR 590646.1. ALODINED ANGLE IAW SRM 51-21-10, PG 1. PRIMER ANGLE IAW SRM 51-23-10, PG 2. PAINTED ANGLE IAW SRM 51-23-10, PG 2. INSTALLED FABRICATED ANGLE IAW SRM 51-40-21, PARA 3-B, PG 36.

Part: INSULATION — TORN (NR 1 PYLON) · airframe 36,290 hrs · 35,404 cycles

NR 1 PYLON ELBOW DUCT METAL INSULATION IS TORN AND DAMAGED. REPAIRED IAW EA 6-3611-136623.

Part: LATCH — CORRODED (NR 2 NACELLE) · airframe 36,290 hrs · 35,404 cycles

NR 2 ENGINE FAN COWL CENTER LATCH FITTING IS SEVERLY GOUGED. COMPLIED WITH EA 6-7110-136625.

Part: SKIN — DENTED (ZONE 100) · airframe 36,290 hrs · 35,404 cycles

EXTERNAL LOWER FUSELAGE SKIN DENTED BELOW THE RT FUSELAGE LIGHT; BS 1764, FRAME 26. CHECKED LIMITS IAW SRM 53-10-12, PARA 5-A (3) AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-12, FIG 110, DIA .109 A=4.35, B=.26, D=.037. MATERIAL THICKNESS 0.063. REMOVED DENTED DAMAGED AREA IAW SRM A300-600, 53-10-12, FIG 224, SHEET 4. EDGE SEALED DOUBLER IAW SRM 51-76-10. PAINTED DOUBLER IAW SRM 51-23-10.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 36,290 hrs · 35,404 cycles

MAIN CABIN SEAT TRACK AT BL 0 BETWEEN FRAMES 60 AND 61 IS WORN. WORN SCALLOPS OUT OF LIMITS IAW SRM 53-10-16. REMOVED DAMAGED SEAT TRACK SECTION FROM FRAME 58 TO FRAME 61 IAW SRM 53-10-16. MATERIAL ID IAW SRM 53-10-16, FIG 208, SHEET 2, PG 249. FABRICATED NEW SEAT TRACK SECTION IAW SRM 53-10-16. INSTALLED NEW SEAT TRACK SECTION FROM FRAME 58 TO FRAME 61 IAW SRM 53-10-16, BL 0.

Part: ANGLE — CRACKED (ZONE 100) · airframe 36,290 hrs · 35,404 cycles

E&E COMPARTMENT, LEFT SIDE AT FRAME 10, UPPER MCD FLOOR STRUCTURE HAS A CRACKED SUPPORT ANGLE. INSTALLED NEW ANGLE AND SHIM IAW SRM 51-40-21; PARA 7; SRM 51-70-00, PARA 2-B AND SRM 51-72-10, PARA 5, PG 2.

Part: SUPPORT — CRACKED (E/E BAY) · airframe 36,290 hrs · 35,404 cycles

AVIONICS COMPARTMENT TRANSPONDER FED RACK; AFT VERTICAL SUPPORT IS CRACKED AT FOOT OF FRAME 18. REMOVED CONNECTOR 2215VC & TERMINAL BLOCK 189VD IAW SRM 51-40-21, PARA 5. REMOVED VERTICAL SUPPORT IAW SRM 51-72-10, PARA 5A, PG 2. VERTICAL SUPPORT MAT ID IAW AIRBUS DWG 12A92531469, ISSUE "C". FABRICATED NEW VERTICAL SUPPORT IAW DWG 12A92531469, ISSUE "C". ALODINED VERTICAL SUPPORT IAW SRM 51-21-01, PG 1. PRIMED & PAINTED VERTICAL SUPPORT IAW SRM 51-23-10, PG 22. PART MARKED VERTICAL SUPPORT IAW GMM 7-0-1001, PARA 7-B. INSTALLED VERTICAL SUPPORT IAW SRM 51-72-10, PARA 6, PG2. REINSTALLED CONNECTOR 2215VC AND TERMINAL BLOCK 189VD IAW SRM 51-40-21. A/C PROGRAM IDENTIFICATION TEST GOOD REF AMM 34-52-00-5.

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 36,290 hrs · 35,404 cycles

MAIN CABIN FLOORBOARD BETWEEN FRAMES 55 AND 57 BROKEN. FABRICATED NEW FLOORBOARD 252 BF IAW DWG SRZ 25-005, REV "H".

Part: FLOORBOARD — PUNCTURED (MAIN CABIN) · airframe 36,290 hrs · 35,404 cycles

MAIN CABIN FLOORBOARD PUNCTURED BETWEEN FRAMES 22 AND 26. FABRICATED NEW FLOORBOARD 231 VF IAW DWG SRZ 25-005, REV "H".

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 36,290 hrs · 35,404 cycles

MAIN CABIN FLOOR PANEL 232VF I S BROKEN FABRICATED NEW FLOORBOARD 232 VF IAW DWG SRZ 25-005, REV "H".

Part: SUPPORT FITTING — CRACKED (CARGO DOOR HINGE) · airframe 36,290 hrs · 35,404 cycles

AFT CARGO COMPARTMENT BULK CARGO DOOR AFT HINGE SUPPORT CRACKED. REMOVED AND REINSTALLED BULK CARGO DOOR AFT HINGE ARM IAW AMM 52-34-12-4. R & R AFT HINGE SUPPORT FITTING IAW SRM 51-40-21, PARA'S 6 AND 7. FITTING PN A53973300200251, PO NR 675142.1 DOOR ADJUSTMENT C/W ON N00053 JPF STEPS 14 AND 15.

Part: SKIN — DAMAGED (BS 1923) · airframe 36,290 hrs · 35,404 cycles

LOWER RT EXTERNAL FUSELAGE AUXILIARY STATIC PORT HAS EVIDENCE OF BLENDING WITHIN CONTROL AREA BS 1923, FR29. COMPLIED WITH EA 6-5330-136619.

Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 36,290 hrs · 35,404 cycles

MAIN CABIN FLOOR PANEL IS CRACKED IN HALF (242 RJ). FABRICATED NEW FLOOR PANEL 242 RJ IAW FEDEX DWG SRZ 25-005, REV "H".

Part: SHAFT — PEELING (RUDDER ACTUATOR) · airframe 36,290 hrs · 35,404 cycles

RUDDER ACTUATOR VARIABLE STOP LEVER HINGE SHAFT PLATING PEELING AND CORRODED RT SIDE. REMOVED RUDDER VSU. REMOVED VSU LEVER ASSY SHAFT. BLENDED DAMAGE AND VERIFIED SHAFT DIMENSION AT 4.67 MM. APPLIED BRUSH CADMIUM PLATING AND ONE TOP COAT. REINSTALLED VSU LEVER ASSY SHAFT AND RUDDER VSU SYS. TEST OF RUDDER MECHANICAL CONTROLS AND OPS TEST OF RUDDER TRAVEL LIMITATION AT HIGH SPEED GOOD; 0.5MM GAP BETWEEN VSU DRIVE SHAFT AND ADDITIONAL STOPS GOOD IAW AMM 27-23-22-4; 27-21-00-5; 27-23-00-5; CMM 27-23-22; EA 6-2720-136620 "FLIGHT CONTROLS - RUDDER VARIABLE STOP LEVER" AND EA 6-2720-136637 "FLIGHT CONTROLS - RUDDER ACTUATOR VSU RIGGING".

Part: ATTACH FITTING — CRACKED (BS 1067) · airframe 36,290 hrs · 35,404 cycles

WASTE WATER SERVICE PANEL HOLD OPEN ROD OTBD ATTACH FITTING ON THE SERVICE DOOR IS CRACKED. REPLACED ATTACH FITTING IAW SRM 51-72-10, PAGE 2.

Part: CHANNEL — CRACKED (ZONE 100) · airframe 36,290 hrs · 35,404 cycles

AVIONICS COMPARTMENT BATTERY RACK CENTER HAT CHANNEL IS CRACKED AT FRAME 15C. REMOVED AND REINSTALLED BATTERIES IAW A300-600 AMM 24-31-11-4. ACFT BATTERIES OPS CHECKED GOOD IAW AMM 24-31-00-5. SET A/C CLOCKS IAW AMM 31-21-00. REMOVED AND REINSTALLED BATTERY RACK COVER SUPPORT IAW SRM 51-40-21, PARA 7, PG 5. REMOVED BATTERY RACK HAT CHANNEL IAW SRM 51-72-10, PARA 5. LOCATED AND DRILLED HAT CHANNEL P/N A9242053522200 IAW SRM 51-72-10, PARA 6-A. INSTALLED BATTERY RACK HAT CHANNEL IAW SRM 51-72-10, PARA 6.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 36,290 hrs · 35,404 cycles

MAIN CABIN FLOOR PANEL IS CRACKED AT FRAME 74; LBL 65 - LBL 82. FABRICATED NEW MAIN CABIN FLOOR PANEL AT FRAME 74; LBL 65 TO LBL 82 IAW DWG SRZ 25-005, REV "H".

Part: FLOORBOARD — BROKEN (MAIN CARGO DECK) · airframe 36,290 hrs · 35,404 cycles

MAIN CABIN CARGO COMPARTMENT FLOORBOARD IS BROKEN FROM FRAME 54.2 - FRAME 55; LBL 55 - LBL 72. FABRICATED NEW MAIN CABIN FLOORBOARD PANEL FROM FRAME 54.2 TO FRAME 55; LBL 55 TO LBL 72 IAW DWG SRZ 25-005, REV "H".

Part: SUPPORT — CRACKED (E/E BAY) · airframe 36,290 hrs · 35,404 cycles

AVIONICS COMPARTMENT LT AND RT SEAL SUPPORTS BELOW THE LADDER FT ARE CRACKED. REMOVED SEAL SUPPORTS (2EA) IAW SRM 51-72-10. ALODINED IAW SRM SRM 51-21-10. PRIMED IAW SRM 51-23-10. REMOVED PANELS TO INSTALL SUPPORTS IAW SRM 51-40-21. INSTALLED SEAL SUPPORTS IAW SRM 51-72-10. REINSTALLED PANELS (2EA) IAW SRM 51-40-21.

Part: FLOORBOARD — CRACKED (MAIN CARGO DECK) · airframe 36,290 hrs · 35,404 cycles

MAIN CABIN CARGO COMPARTMENT FLOORBOARD NR 241 GF IS CRACKED IN HALF. FABRICATED NEW MAIN CABIN FLOOR PANEL NR 241 GF IAW DWG SRZ 25-005, REV "H".

Part: FLOORBOARD — BROKEN (MAIN CABIN) · airframe 36,290 hrs · 35,404 cycles

MAIN CABIN FLOORBOARD IS BROKEN BETWEEN FRAME 62 AND FRAME 65. FABRICATED NEW MAIN CABIN FLOORBOARD BETWEEN FRAME 62 & 65 IAW DWG SRZ 25- 005, REV "H".

Part: FLOORBOARD — BROKEN (CARGO BAY) · airframe 36,290 hrs · 35,404 cycles

MAIN CARGO COMPARTMENT FLOOR BOARD 242 LK IS BROKEN FROM FRAME 53 - FRAME 54; RBL 76. FABRICATED NEW MAIN CABIN FLOORBOARD AT FRAME 53-54; RBL 76 IAW DWG SRZ 25- 005, REV "H".

Part: FLOORBOARD — BROKEN (MAIN CARGO DECK) · airframe 36,290 hrs · 35,404 cycles

MAIN CABIN CARGO COMPARTMENT FLOORBOARD HAS A BROKEN EDGE AT FRAME 68; LBL 50. FABRICATED NEW MAIN CABIN FLOORBOARD AT FRAME 68; LBL 50 IAW DWG SRZ 25-005, REV "H".

Part: AUTOTHROTTLE SYS — MALFUNCTIONED · airframe 34,701 hrs · 34,557 cycles

ON TAKEOFF ROLL (20 KTS AIRSPEED). PERFORMED RTO CHECKLIST IA QRH. MEL NON FLAGGED ITEM 22-30-01-C AUTO THROTTLE SYS RESET IN FLIGHT, WORKED FINE. PERFORMED AUTOTHROTTLE ADJUSTMENT AND TEST IAW AMM 22-30-00-5-02 ITEM "B". TEST PASSED SATISFACTORY ON GND. INTERROGATED AFS COMPUTER AND NO FAULTS RECORDED. NO HISTORY PER ATS DURING THE LAST 90 DAYS. OK FOR SVC. A/C DOWNGRADED TO CAT2 , NR 1 AND NR 2 AP'S CHECK 3A. (NO PARTS REMOVED OR REPLACED, BITE CK OK. 6 GOOD LEGS)

Part: WEB — BENT (ZONE 200) · airframe 33,436 hrs · 33,829 cycles

FUS FR 48,BETWEEN SEAT TRACKS 3L AND 4L, STIFFENER WEB 12" TO 24" BELOW FLOOR IS BENT. REMOVED AND REPLACED WEB IAW A300-600 SRM 51-40-21.

Part: WEB — BENT (ZONE 200) · airframe 33,436 hrs · 33,829 cycles

FUS FR 52,BETWEEN SEAT TRACKS 3L AND 4L,STIFFENER WEB 12" TO 24" BELOW FLOOR IS BENT, TOP I/B EDGE. REMOVED AND REPLACED WEB IAW A300-600 SRM 51-40-21.

Part: WEB — BENT (ZONE 200) · airframe 33,436 hrs · 33,829 cycles

FUS FR 50 BETWEEN SEAT TRACKS 3L AND 4L, STIFFENER WEB 12" TO 24" BELOW FLOOR BENT FABRICATED REPLACEMENT WEB IAW DRAWING A53832104. REMOVED AND REPLACED WEB IAW A300-600 SRM 51-40-21.

Part: SEAT TRACK — BENT (ZONE 200) · airframe 33,436 hrs · 33,829 cycles

LT TRACK Y1456 FR50, AFTER REMOVAL OF WEB, FOUND 1 LINK TRACK WITH BENT TAB ON I/B SIDE. REMOVED AND REPLACED SUPPORT LINK BRACKET, LT TRACK Y1456 FR50 IAW A300-600 SRM 51-41-21.

Part: SEAT TRACK — BENT (ZONE 200) · airframe 33,436 hrs · 33,829 cycles

LT TRACK Y1456 FR 51, AFTER REMOVAL OF WEB FOUND 1 LINK WITH BENT TAB ON I/B SIDE, REMOVED AND REPLACED SUPPORT LINK AT TRACK Y1456 FR 51 IAW A300-600 SRM 51-40-21.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 33,436 hrs · 33,829 cycles

FUS FR 53 SEAT TRACK 3L LOWER EDGE CRACKED, 1" WIDE REMOVED AND REPLACED SEAT TRACK 3L FROM FR 46 TO FR 54 IAW A300-600 SRM 51-40-21.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 33,436 hrs · 33,829 cycles

LOWER FUSELAGE FR 53 SEAT TRACK 2L, LOWER EDGE IS CRACKED, 1" WIDE REMOVED AND REPLACED SEAT TRACK 2L FR 46 TO FR 54 IAW A300-600 SRM 51-40-21.

Part: WEB — DAMAGED (ZONE 100) · airframe 33,436 hrs · 33,829 cycles

LWR FUSELAGE FR 49 BETWEEN SEAT TRACK 3L AND 4L 12" TO 24" BELOW FLOOR . THE STIFFENER WEB IS BENT AFT 1/4". REMOVED AND REPLACED WEB IAW A300-600 SRM 51-40-21.

Part: BRACKET — DAMAGED (ZONE 100) · airframe 33,436 hrs · 33,829 cycles

LWR FUSELAGE FR53 L SIDE OF CENTER 55" TRACK SUPPORT LINK BRACKET HAS THE I/B TAB ATTACH POINT FOR WEB IS BROKEN OFF. REMOVED AND REPLACED LINK IAW A300-600 SRM 51-40-21.

Part: SKIN — CRACKED (RT WING TE FLAP) · airframe 33,436 hrs · 33,829 cycles

AFTER REMOVAL OF RT WING CENTER FLAP CENTER UPPER RUB STRIP FOUND 1 EA CRACK 1 INCH LONG IN THE FLAP UPPER SKIN. REPAIRED UPPER SKIN OF RT CENTER FLAP IAW EA 6-5750-113403 AND TD FOK 302/2007 ISSUE A.

Part: WEB — DAMAGED (ZONE 100) · airframe 33,436 hrs · 33,829 cycles

LWR FUSELAGE FR 53 LEFT OF CENTER 18 TO 55" CARGO LOADING SYS SUPPORT WEB IS BENT ALONG THE INBD AND OTBD LWR EDGE. REMOVED AND REPLACED WEB IAW A30-600 SRM 51-40-21.

Part: WEB — DAMAGED (ZONE 100) · airframe 33,436 hrs · 33,829 cycles

LWR FUSELAGE FR 54 LEFT OF CENTER 33" TO 55" CARGO LOADING SYS SUPPORT WEB IS BENT ALONG THE I/B EDGE. REMOVED AND REPLACED LOADING SYS SUPPORT WEB IAW A300-600 SRM 51-40-21.

Part: SEAT TRACK — DAMAGED (ZONE 100) · airframe 33,436 hrs · 33,829 cycles

LWR FUSELAGE FR 54 18" LEFT OF CENTER, SEAT TRACK SUPPORT LINK IS BROKEN INTO TWO PIECES. REMOVED AND REPLACED TRACK SUPPORT LINK IAW A300-600 SRM 51-40-21.

Part: WEB — DAMAGED (ZONE 100) · airframe 33,436 hrs · 33,829 cycles

LWR FUSELAGE FR 51 BETWEEN TRACK 3L AND 4L, 12" TO 24" BELOW FLOOR. THE STIFFENER WEB IS BENT AFT 3/8". REMOVED AND REPLACED WEB IAW A300-600 SRM 51-40-21.

Part: BRACKET — DAMAGED (ZONE 100) · airframe 33,436 hrs · 33,829 cycles

LWR FUSELAGE FR 54 CENTER LINE SEAT TRACK SUPPORT LINK BRACKET IS BROKEN INTO TWO PIECES. REMOVED AND REPLACED SUPPORT LINK IAW A300-600 SRM 51-40-21.

Part: TRACK — BENT (ZONE 100) · airframe 33,436 hrs · 33,829 cycles

LT TRACK Y1456 FR 52 AFTER REMOVAL OF WEB FOUND 1 LINK TRACK WITH BENT TAB ON I/B SIDE. REMOVED AND REPLACED SUPPORT LINK BRACKET AT LT TRACK Y1456 FR 52 IAW A300-600 SRM 51-40-21.

Part: WEB — DAMAGED (ZONE 100) · airframe 33,436 hrs · 33,829 cycles

LWR FUSELAGE FR 53 BETWEEN SEAT TRACK 3L AND 4L 12" TO 24" BELOW FLOOR, STIFFENER WEB BENT AFT 1/2" ALONG THE TOP EDGE. REMOVED AND REPLACED WEB IAW A300-600 SRM 51-40-21.

Part: WEB — DAMAGED (ZONE 200) · airframe 33,436 hrs · 33,829 cycles

FOUND LWR FUSELAGE FR 49 BETWEEN SEAT TRACK 3L AND 4L, CARGO LOADING SYS SUPPORT WEB IS BENT ALONG THE O/B LWR EDGE. REMOVED AND REPLACED SUPPORT WEB AT FR 49 TRACK 3L THRU 4L IAW A300-600 SRM 51-40-21.

Part: WEB — DAMAGED (ZONE 100) · airframe 33,436 hrs · 33,829 cycles

FOUND LWR FUSELAGE FR 51 BETWEEN SEAT TRACK 3L AND 4L, CARGO LOADING SYS SUPPORT WEB IS BENT ALONG THE O/B LWR EDGE. REMOVED AND REPLACED WEB IAW A300-600 SRM 51-40-21.

Part: WEB — DAMAGED (ZONE 200) · airframe 33,436 hrs · 33,829 cycles

FOUND LWR FUSELAGE FR 50 BETWEEN SEAT TRACK 3L THRU 4L, CARGO LOADING SYS SUPPORT WEB IS BENT ALONG THE O/B LWR EDGE. REMOVED AND REPLACED LOADING SYS SUPPORT WEB AT FR 50 IAW A300-600 SRM 51-40-21.

Part: WEB — DAMAGED (ZONE 200) · airframe 33,436 hrs · 33,829 cycles

FOUND LWR FUSELAGE FR 52 BETWEEN SEAT TRACK 3L AND 4L, CARGO LOADING SYS SUPPORT WEB IS BENT ALONG THE O/B LWR EDGE. REMOVED AND REPLACED SUPPORT WEB AT FR 52 BETWEEN TRACK 3L AND 4L IAW A300-600 SRM 51-40-21.

Part: WEB — DAMAGED (ZONE 100) · airframe 33,436 hrs · 33,829 cycles

LT TRACK Y1456 FR 49 AFTER REMOVAL OF WEB FOUND 1 LINK TRACK WITH BENT TAB ON I/B SIDE. REMOVED AND REPLACED SUPPORT LINK IAW A300-600 SRM 51-40-21.

Part: WEB — DAMAGED (ZONE 100) · airframe 33,436 hrs · 33,829 cycles

LWR FUSELAGE FR 48 BETWEEN SEAT TRACK 3L THRU 4L THE CARGO LOADING SYS SUPPORT WEB IS BENT ALONG THE O/B EDGE. REMOVED AND REPLACED SUPPORT WEB IAW A300-600 SRM 51-40-21.

Part: TRACK — BENT (ZONE 200) · airframe 33,436 hrs · 33,829 cycles

LT TRACK I/1456 FR 48 AFTER REMOVAL OF WEB FOUND 1 LINK TRACK WITH BENT TAB ON I/B SIDE. REMOVED AND REPLACED SUPPORT LINK AT LT TRACK I/1456 FR 48 IAW A300-600 SRM 51-40-21.

Part: TRACK — MISREPAIRED · airframe 33,436 hrs · 33,829 cycles

PREVIOUS ANGLE REPAIR LOCATED ON AFT CARGO ROLLER TRACK NR 2 LT Y805 BETWEEN FRAMES 55 AND 56 HAS 2 EACH REPAIR ANGLES MEASURING 5.5 IN LONG, 1 EA. REPAIR SECTION MEASURING 9.7 IN LONG AND 1 EA DOUBLER ON BOTTOM SURFACE MEASURING 8.5 BY 6.3 IN. PREVIOUS REPAIR FOUND NOT TO BE IAW A300-600 SRM 53-10-15 FIG 203. REMOVED AND REPLACED REPAIR WITH CORRECT REPAIR IAW A300-600 SRM 53-10-15 FIG 202. THIS IS A REPAIR WITH NO AIRBUS PT NUMBER, REPAIR IDENTIFIED BY THE AGING AIRCRAFT INSPECTION PROGRAM.

Part: TRACK — MISREPAIRED · airframe 33,436 hrs · 33,829 cycles

PREVIOUS ANGLE REPAIR LOCATED ON AFT CARGO ROLLER TRACK NR 3 LT Y 1470 BETWEEN FRAMES 55 AND 56 HAS 2 EA. REPAIR ANGLES MEASURING 7.1 IN LONG , 1 EA. REPAIR SECTION MEASURING 7 IN LONG AND 1 EA. REPAIR DOUBLER ON BOTTOM SURFACE MEASURING 6.8 BY 6.3 IN. PREVIOUS REPAIR FOUND NOT TO BE IAW A300-600 SRM 53-10-15 PARA 5 PAGES 207-212 FIG 203. REMOVED AND REPLACED REPAIR WITH CORRECT REPAIR IAW A300-600 SRM 53-10-15 PARA 5 PAGES 207- 212 FIG 203. THIS IS A REPAIR WITH NO AIR BUS ISSUED PT NO. REPAIR IDENTIFIED BY THE AGING AIRCRAFT PROGRAM.

Part: TRACK — MISREPAIRED · airframe 33,436 hrs · 33,829 cycles

PREVIOUS ANGLE REPAIR LOCATED ON AFT CARGO ROLLER TRACK NR 3 RIGHT Y1470 BETWEEN FRAMES 55 AND 56 HAS 2 EACH ANGLES MEASURING 7.1" LONG, 1 EACH REPAIR SECTION MEASURING 7" LONG AND 1 EACH REPAIR DOUBLER ON BOTTOM SURFACE MEASURING 7.5" BY 6.3". PREVIOUS REPAIR FOUND NOT TO BE IAW A300-600 SRM 53-10-15 FIG 203. REMOVED AND REPLACED REPAIR WITH CORRECT REPAIR IAW A300-600 SRM 53-10-15 PARA 5 PAGES 207 THRU 212 FIG 203. THIS IS A REPAIR WITH NO AIRBUS ISSUED PART NUMBER. REPAIR INDENTIFIED BY THE AGING AIRCRAFT INSPECTION PROGRAM.

Part: ANGLE — MISREPAIRED (FUSELAGE) · airframe 33,436 hrs · 33,829 cycles

PREVIOUS ANGLE REPAIR LOCATED ON AFT CARGO ROLLER TRACK NR 3 RT Y1470 BETWEEN FRAMES 55 AND 56 HAS 2 EA ANGLES MEASURING 7.1" LONG, 1 EA REPAIR SECTION MEASURING 7" LONG AND 1 EA REPAIR DOUBLER ON BOTTOM SURFACE MEASURING 7.5" X 6.3". PREVIOUS REPAIR FOUND NOT TO BE IAW SRM 53-10-15, FIG 203. R & R REPAIR WITH CORRECT REPAIR IAW SRM 53-10-15, PARA 5, PAGES 207 THRU 212, FIG 203. THIS IS A REPAIR WITH NO ISSUED PN. REPAIR INDENTIFIED BY THE AGING ACFT INSP PROGRAM.

Part: ROLLER TRAY — MISREPAIRED (CARGO BAY) · airframe 33,436 hrs · 33,829 cycles

PREVIOUS ANGLE REPAIR LOCATED ON AFT CARGO ROLLER TRACK NR 1 RT -Y140 BETWEEN FRAME 57.3 AND 58 HAS 2 REPAIR ANGLES MEASURING 7.7" L , 1 REPAIR SECTION MEASURING 8.3" L AND 1 REPAIR DOUBLER ON BOTTOM SURFACE MEASURING 8.3" BY 6.3" PREVIOUS REPAIR FOUND NOT TO BE IAW A300-600 SRM 53-10-15 PARA 5 PAGE 207-212 FIG 203. REMOVED AND REPLACED REPAIR WITH CORRECT REPAIR IAW A300-600 SRM 53-10-15 PARA 5 FIG 203 PAGE 207-212. THIS IS A REPAIR WITH NO AIRBUS ISSUED PART NUMBER, REPAIR IDENTIFIED BY THE AGING AIRCRAFT INSPECTION PROGRAM.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 33,436 hrs · 33,829 cycles

PREVIOUS LONGERON "T" CAP REPAIR LOCATED IN BULK CARGO BETWEEN FRAMES 64 AND 65 UNDER FLOOR AT APPROX STRINGER 50 RT HAS 1 EACH REPAIR SECTION MEASURING 11" LONG AND 2 EACH REPAIR ANGLES MEASURING 10.5". PREVIOUS REPAIR FOUND NOT BE IAW A300-600 SRM 51-71-50 FIG 201. REMOVED AND REPLACED REPAIR WITH CORRECT REPAIR IAW A300-600 SRM 51-72-10. THIS IS A REPAIR WITH NO AIRBUS PART NUMBER. REPAIR IDENTIFIED BY AGING AIRCRAFT INSPECTION PROGRAM.

Part: TRACK — MISREPAIRED · airframe 33,436 hrs · 33,829 cycles

PREVIOUS ANGLE REPAIR LOCATED AT AFT CARGO ROLLER TRACK NR 1 LEFT Y140 BETWEEN FRAMES 57.3 AND 58 HAS 2 EA. REPAIR ANGLES MEASURING 7.4 IN LONG 1 EA. REPAIR SECTION MEASURING 8.2 IN LONG AND 1 EA. REPAIR DOUBLER ON BOTTOM SURFACE MEASURING 8.3 BY 6.3 IN. PREVIOUS REPAIR FOUND NOT TO BE IAW A300-600 SRM 53-10-15 PARA 5 PAGES 207-212 FIG 203. REMOVED AND REPLACED REPAIR WITH CORRECT REPAIR IAW A300-600 SRM 53-10-15 PARA 5 PAGES 207-212 FIG 203. THIS IS A REPAIR WITH NO AIRBUS ISSUED PART NUMBER , REPAIR IDENTIFIED BY THE AGING A/C INSP .

Part: TRACK — MISREPAIRED · airframe 33,436 hrs · 33,829 cycles

PREVIOUS ANGLE REPAIR LOCATED ON AFT CARGO ROLLER TRACK NR 3 RIGHT Y1470 BETWEEN FRAMES 56 AND 57 HAS 2 EACH REPAIR ANGLES MEASURING 7.1" LONG, 1 EACH. REPAIR SECTION MEASURING 13" LONG AND 1 EACH REPAIR DOUBLER ON BOTTOM SURFACE MEASURING 7" BY 6.3". PREVIOUS REPAIR FOUND NOT TO BE IAW A300-600 SRM 53-10-15 FIG 203. REMOVED AND REPLACED REPAIR WITH CORRECT REPAIR IAW A300-600 SRM 53-10-15 FIG. 202. THIS IS A REPAIR WITH NO AIRBUS ISSUED PART NUMBER. REPAIR IDENTIFIED BY THE AGING AIRCRAFT INSPECTION PROGRAM.

Part: TRACK — MISREPAIRED · airframe 33,436 hrs · 33,829 cycles

PREVIOUS ANGLE REPAIR LOCATED ON AFT CARGO ROLLER TRACK NR 3 RIGHT Y1470 BETWEEN FRAMES 57.3 ABD 58 HAS 2 EACH REPAIR ANGLES MEASURING 7.1" LONG, 1 EACH. REPAIR SECTION MEASURING 8.8" LONG AND 1 EACH REPAIR DOUBLER ON BOTTOM SURFACE MEASURING 7.3" BY 6.3". PREVIOUS REPAIR FOUND NOT TO BE IAW A300-600 SRM 53-10-15 PARA 5 PAGES 207 THRU 212 FIG 203. REMOVED AND REPLACED REPAIR WITH CORRECT REPAIR IAW A300-600 SRM 53-10-15 PARA 5 PAGES 207 THRU 212 FIG 203. THIS IS A REPAIR WITH NO AIRBUS PART NUMBER. REPAIR IDENTIFIED BY THE AGING AIRCRAFT INSPECTION PROGRAM.

Part: ANGLE — MISREPAIRED (FUSELAGE) · airframe 33,436 hrs · 33,829 cycles

PREVIOUS ANGLE REPAIR LOCATED ON AFT CARGO ROLLER TRACK NR 3 RT Y1470 BETWEEN FRAMES 57.3 ABD 58 HAS 2 EA REPAIR ANGLES MEASURING 7.1" LONG, 1 EA REPAIR SECTION MEASURING 8.8" LONG AND 1 EA REPAIR DOUBLER ON BOTTOM SURFACE MEASURING 7.3" X 6.3". PREVIOUS REPAIR FOUND NOT TO BE IAW SRM 53-10-15, PARA 5, PAGES 207 THRU 212 FIG 203. R & R REPAIR WITH CORRECT REPAIR IAW SRM 53-10-15 PARA 5, PAGES 207 THRU 212 FIG 203. THIS IS A REPAIR WITH NO MFG PN. REPAIR INDENTIFIED BY THE AGING ACFT INSP PROGRAM.

Part: TEE FITTING — MISREPAIRED (CARGO BAY) · airframe 33,436 hrs · 33,829 cycles

PREVIOUS TEE CAP REPAIR LOCATED IN BULK CARGO. PREVIOUS REPAIR FOUND NOT BE IAW SRM 51-71-50, FIG 201. R & R REPAIR WITH CORRECT REPAIR IAW SRM 51-72-10.

Part: CARGO TRACK — MISREPAIRED (FUSELAGE) · airframe 33,436 hrs · 33,829 cycles

PREVIOUS ANGLE REPAIR LOCATED ON AFT CARGO ROLLER TRACK NR 3 RT Y1470 BETWEEN FRAMES 56 AND 57 HAS 2 EA REPAIR ANGLES MEASURING 7.1" LONG, 1 EA REPAIR SEC MEASURING 13" LONG AND 1 EA REPAIR DOUBLER ON BOTTOM SURFACE MEASURING 7" X 6.3". PREVIOUS REPAIR FOUND NOT TO BE IAW SRM 53-10-15. FIG. 203. R & R REPAIR WITH CORRECT REPAIR IAW SRM 53-10-15, FIG 202.

Part: FRAME — MISREPAIRED (ZONE 100) · airframe 33,436 hrs · 33,829 cycles

PREVIOUS REPAIR LOCATED IN BULK CARGO ON FRAME 64 UNDER FLOOR BETWEEN STRINGER 46 AND 48 RT HAS 2 EACH REPAIR ANGLES ON THE AFT SIDE MEASURING 14.4" BY 2.9" AND 13.6" BY 2.2" PREVIOUS INSTALLED REPAIR WAS DETERMINED NOT TO BE IAW FEDEX EA6-5310-68347, DUE TO 15 EACH INCORRECT FASTENERS INSTALLED, BASED ON A VISUAL EVALUATION. REMOVED 15 EACH MS20470DD6 RIVETS, REAMED HOLES TO 1ST OVERSIZE AND INSTALLED 15 EACH LOCK FASTENER IAW A300-600 SRM 51-40-21 AND REF FEDEX EA6-5310-68347. REPAIR IS CLASSIFIED AS A MAJOR PER FED EX GMM 6-2-100.

Part: SKIN — MISREPAIRED (TE FLAP) · airframe 33,436 hrs · 33,829 cycles

PREVIOUS EXTERNAL REPAIR DOUBLER LOCATED ON LEFT WING INBOARD TRAILING EDGE LOWER SURFACE BETWEEN RIBS 11 AND 15 MEASURES 5.2 INCH BY 13.1 INCH. REMOVED AND REPLACED 5 EACH BLIND FASTENERS TO CORRECT REPAIR PER A300-600 SRM 51-40-21 AND FEDEX EA 6-5750-70315. REPAIR IS CLASSIFIED AS A MAJOR REPAIR PER FEDEX GMM 6-2-100.

Part: SKIN — MISREPAIRED (TE FLAP) · airframe 33,436 hrs · 33,829 cycles

PREVIOUS EXTERNAL REPAIR DOUBLER LOCATED ON LEFT WING INBOARD FLAP TRAILING EDGE LOWER SURFACE AT RIBS 9 AND 10 MEASURES 13.3 INCH BY 24 INCH. REMOVED AND REPLACED 3 EACH BLIND FASTENERS TO CORRECT THE REPAIR PER A300-600 SRM 51-40-21 AND REF FEDEX EA 6-5750-70315. THIS REPAIR IS CLASSIFIED AS A MAJOR PER FEDEX GMM 6-2-100.

Part: SKIN — MISREPAIRED (AILERONS) · airframe 33,436 hrs · 33,829 cycles

PREVIOUS EXTERNAL REPAIR DOUBLER ON LEFT WING AILERON LOWER TRAILING EDGE SKIN BETWEEN RIBS 1 TO 6 MEASURES 21 INCH BY 14.5 INCH AT THE AFT INBD EDGE. REMOVED AND REPLACED 3 BLIND FASTENERS TO CORRECT REPAIR PER A300-600 SRM 51-40-21 AND REFERENCE FEDEX EA 6-5761-70314 AND AIRBUS RAS/FOK/0651 2003 ISSUE A.

Part: INDICATOR — INACCURATE (NR 2 AIRSPEED) · airframe 30,277 hrs · 32,096 cycles

DURING TAKEOFF ROLL, NR 2 PRIMARY AIRSPEED INDICATOR CONTINUED TO INDICATE 30 KIAS WHILE NR 1 INDICATED 80 KIAS. TAKEOFF ABORTED AT 90 KIAS. ENT BY: 275418 RPT BY: 056042 FACT 25OCT05 06:18 ONT R AS PRECAUTIONARY USING DRY NITROGEN BLEW OUT NR 2 PITOT AND NO OBSTRUCTIONS WERE NOTED. REPLACED NR 2 ADC OPS NORMAL REF MM 34-11-34-4.

Part: FRAME — CRACKED (CABIN) · airframe 29,985 hrs · 31,940 cycles

MAIN CABIN AT FRAME 46 LT CRACKED APPROX 4 INCHES.

Part: FRAME — CRACKED (ZONE 200) · airframe 29,985 hrs · 31,940 cycles

MAIN CABIN RT FRAME 46 CRACKED. REMOVED AND REPLACED RT FRAME 46 AT STR 27 IAW A300-600 SRM 51-40-21 FIG 9.

Part: FRAME — CRACKED (ZONE 200) · airframe 29,985 hrs · 31,940 cycles

RIGHT MAIN CABIN FRAME 45 FOUND CRACKED. REMOVED AND REPLACED FRAME SECTION IAW A300-600 SRM 51-40-21 FIG 9, STR 22 TO STR 27.

Part: FITTING — CRACKED (LT WING TE FLAP) · airframe 29,985 hrs · 31,940 cycles

LT WING INBOARD FLAP OUTBOARD LEADING EDGE MOUNT FITTING CRACKED. (OPEN)

Part: PUMP — DAMAGED (ZONE 400) · airframe 28,059 hrs · 30,844 cycles

LOST GREEN SYS HYD FLUID AFTER FLAPS RETRACTED. NO HYDRAULIC OVERHEAT OCCURRED FOUND LINE BUSTED LT MLG UPLOCK. REMOVED & REPLACED LT MLG UPLOCK HOSE REF IPC 32-31-03-03 ITEM 30, NEEDS LEAK CHECK PAR 2C A300 MM 29-00-00-3. PUMP REMOVAL IN PROGRESS PER MM 29-11-32-4, A-300 MM-29-11-32-4. REMOVED AND REPLACED NR 2 ENG DRIVEN HYD PUMP PER A300- 600 M/M 29-11-32-4-01 NEEDS SERVICED AND LEAK CHECKED. REPLACED NR 1 GREEN SYS ENG DRIVEN HYD PUMP PER A300- 600 M/M 29-11-32-4-01. SERVICED GREEN SYS HYD FLUID. OPS & LEAK CHECK NORMAL. A/C OK FOR SERVICE.