N854GT

Part: CHANNEL — CRACKED (ZONE 300) · airframe 49,192 hrs · 8,154 cycles

EMP - LH HORIZONTAL STABILIZER TIP FAIRING T/E WEDGE U CHANNEL CRACK.(<P>EMP - LH HORIZONTAL STABILIZER TIP FAIRING T/E UPPER CLOSURE RIB REPLACED IAW RI-55-10-17553 REV A. NO FURTHER DEFECTS NOTED.</P>)

Part: STRIKER — CRACKED (ZONE 200) · airframe 49,192 hrs · 8,154 cycles

FWD OF BS 2360 STR 8R FOUND CRACK.(<P>FWD OF BS 2360 STR 8R CRACK REPAIRED IAW RI-53-61-17591 REV A. <SPAN>NO FURTHER DEFECTS NOTED.</SPAN></P>)

Part: PANEL — CRACKED (ZONE 500) · airframe 49,192 hrs · 8,154 cycles

LHW WS740 FIXED T/E PNL RIB FOUND CRACKED.(<P>LHW WS740 FIXED T/E PNL RIB CRACK REPAIRED IAW RI-57-24-17634 REV A.&NBSP;<SPAN>NO FURTHER DEFECTS NOTED.</SPAN></P>)

Part: STRINGER — CRACKED (ZONE 200) · airframe 49,192 hrs · 8,154 cycles

M/D - STA 860-880 S-10R STRINGER FOUND CRACK.(<P>M/D - STA 860-880 S-10R STRINGER CRACK REPAIRED IAW RI-53-21-17605 REV A.&NBSP;<SPAN>NO FURTHER DEFECTS NOTED.</SPAN></P>)

Part: STRIKER — CRACKED (ZONE 200) · airframe 49,192 hrs · 8,154 cycles

FWD OF BS 2360 STR 6R FOUND CRACKS.(<P>FWD OF BS 2360 STR 6R FOUND CRACKS REPAIRED IAW RI-53-61-17579 REV B. NO FURTHER DEFECTS NOTED.</P>)

Part: STRINGER — CRACKED (ZONE 200) · airframe 49,192 hrs · 8,154 cycles

M/D - STA 860-880 S-10L STRINGER FOUND CRACK.(<P>M/D - STA 860-880 S-10L STRINGER CRACK REPAIRED IAW RI-53-21-17609 REV A. <SPAN>NO FURTHER DEFECTS NOTED.</SPAN></P>)

Part: STRINGER — CRACKED (ZONE 20) · airframe 49,192 hrs · 8,154 cycles

2 EA CRACKS WERE FOUND ON STRINGER O/B SIDE APPROX 1/8" AND 11/16" AS MARKED AFT OF BS 2360 STR 2L.(<P>2 EA CRACKS FOUND ON STRINGER O/B SIDE APPROX 1/8" AND 11/16" AS MARKED AFT OF BS 2360 STR 2L WERE REPAIRED IAW RI-53-81-17607 REV A. NO FURTHER DEFECTS NOTED.</P>)

Part: SKIN — DAMAGED (NR 9 FLAP) · airframe 49,192 hrs · 8,154 cycles

#9 V/C FLAP LSA LAYER DAMAGED.(<P>PERFORMED REPAIR AT LSA LAYER DAMAGED AREA PER CMM 57-55-42 REPAIR 17-1 REV 33. NO FURTHER DEFECTS NOTED.</P>)

Part: STRINGER — CRACKED (ZONE 200) · airframe 49,192 hrs · 8,154 cycles

FWD OF BS 2360 STR 9R FOUND CRACK.(<P>FWD OF BS 2360 STR 9R CRACK REPAIRED IAW RI-53-61-17578 REV B. NO FURTHER DEFECTS NOTED.</P>)

Part: STRIKER — CRACKED (ZONE 200) · airframe 49,192 hrs · 8,154 cycles

AFT OF STA 2360 S4L FOUND CRACKED.(<P>AFT OF STA 2360 S4L CRACKED REPAIRED IAW RI-53-81-17594 REV B.&NBSP;<SPAN>NO FURTHER DEFECTS NOTED.</SPAN></P>)

Part: SKIN — DAMAGED (NR 8 FLAP) · airframe 49,192 hrs · 8,154 cycles

#8 V/C FLAP LSA LAYER DAMAGED.(<P>PERFORMED REPAIR AT #8 V/C FLAP LSA LAYER DAMAGED AREA PER CMM 57-55-42 REPAIR 17-1 REV 33. NO FURTHER DEFECTS NOTED.</P>)

Part: STRIKER — CRACKED (ZONE 200) · airframe 49,192 hrs · 8,154 cycles

FWD OF BS 2360 STR 1L FOUND CRACKS.(<P>FWD OF BS 2360 STR 1L CRACKS REPAIRED I.A.W RI-53-61-17598 REV A. <SPAN>NO FURTHER DEFECTS NOTED.</SPAN></P>)

Part: SKIN — CORRODED (NR 4 FLAP) · airframe 49,192 hrs · 8,154 cycles

#4 VC FLAP BULLNOSE FOUND EROSION.(<P>PERFORMED REPAIR AT EROSION AREA IAW&NBSP;<SPAN>SRM 51-70-04 REPAIR 5 REV 45. NO FURTHER DEFECTS NOTED.</SPAN></P>)

Part: STRINGER — CRACKED (ZONE 200) · airframe 49,192 hrs · 8,154 cycles

MD - STA 880-900 S-7L STRINGER FOUND CRACK.(<P>MD - STA 880-900 S-7L STRINGER CRACK REPAIRED IAW RI-53-20-17616 REV A.&NBSP;<SPAN>NO FURTHER DEFECTS NOTED.</SPAN></P>)

Part: SKIN — DAMAGED (NR 6 FLAP) · airframe 49,192 hrs · 8,154 cycles

#6 V/C FLAP LSA LAYER DAMAGED.(<P>PERFORMED REPAIR AT #6 V/C FLAP LSA LAYER DAMAGED AREA PER&NBSP;<SPAN>CMM 57-55-42 REPAIR 17-1 REV 33. NO FURTHER DEFECTS NOTED.</SPAN></P>)

Part: STRINGER — CRACKED (ZONE 200) · airframe 49,192 hrs · 8,154 cycles

AFT OF STA 2598, S6R FOUND CRACKED.(<P>AFT OF STA 2598, S6R CRACK REPAIRED IAW RI-53-81-17567 REV A.&NBSP;<SPAN>NO FURTHER DEFECTS NOTED.</SPAN></P>)

Part: STRINGER — CRACKED (ZONE 200) · airframe 49,192 hrs · 8,154 cycles

AFT OF STA 2360 S5L FOUND CRACKED.(<P>AFT OF STA 2360 S5L CRACK REPAIRED IAW RI-53-81-17623 REV A. NO FURTHER DEFECTS NOTED.</P>)

Part: STRINGER — CRACKED (ZONE 200) · airframe 49,192 hrs · 8,154 cycles

M/D - STA 2340-2360 S-21L STRINGER FOUND CRACK.(<P>M/D - STA 2340-2360 S-21L STRINGER CRACK REPAIRED IAW RI-53-61-17602 REV A.&NBSP;<SPAN>NO FURTHER DEFECTS NOTED.</SPAN></P>)

Part: STRINGER — CRACKED (ZONE 200) · airframe 49,192 hrs · 8,154 cycles

M/D - STA 1940-1960 S-9R STRINGER FOUND CRACK.(<P>M/D - STA 1940-1960 S-9R STRINGER CRACK REPAIRED IAW B747-8F SRM 53-60-03 REPAIR 4 ALTERNATIVE 2 REV 145. NO FURTHER DEFECTS NOTED.</P>)

Part: STRIKER — CRACKED (ZONE 200) · airframe 49,192 hrs · 8,154 cycles

M/D - STA 1940-1960 S-10L STRINGER FOUND CRACK.(<P>M/D - STA 1940-1960 S-10L STRINGER CRACK REPAIRED IAW RI-53-61-17629 REV A.&NBSP;<SPAN>NO FURTHER DEFECTS NOTED.</SPAN></P>)

Part: STRINGER — CRACKED (ZONE 200) · airframe 49,192 hrs · 8,154 cycles

AFT OF STA 2598, S5L FOUND CRACKED.(<P>AFT OF STA 2598, S5L CRACK REPAIRED IAW RI-53-81-17566 REV A. <SPAN>NO FURTHER DEFECTS NOTED.</SPAN></P>)

Part: STRINGER — CRACKED (ZONE 200) · airframe 49,192 hrs · 8,154 cycles

FWD OF BS 2360 STR 10L FOUND CRACK.(<P>FWD OF BS 2360 STR 10L CRACK REPAIRED IAW RI-53-61-17590 REV B. NO FURTHER DEFECTS NOTED.</P>)

Part: STRINGER — CRACKED (ZONE 200) · airframe 49,192 hrs · 8,154 cycles

M/D - STA 980+160 - 1000 S-12R STRINGER FOUND CRACK.(<P>M/D - STA 980+160 - 1000 S-12R STRINGER CRACK REPAIRED IAW RI-53-20-17599 REV A. NO FURTHER DEFECTS NOTED.</P>)

Part: STRINGER — CRACKED (ZONE 200) · airframe 49,192 hrs · 8,154 cycles

AFT OF STA 2598, S4L FOUND CRACKED.(<P>AFT OF STA 2598, S4L CRACK REPAIRED IAW RI-53-81-17626 REV A. <SPAN>NO FURTHER DEFECTS NOTED.</SPAN></P>)

Part: STRINGER — CRACKED (ZONE 200) · airframe 49,192 hrs · 8,154 cycles

FWD OF STA 2598 S6L FOUND CRACKED.(<P>FWD OF STA 2598 S6L CRACK REPAIRED IAW RI-53-81-17608 REV A.&NBSP;<SPAN>NO FURTHER DEFECTS NOTED.</SPAN></P>)

Part: STRINGER — CRACKED (ZONE 100) · airframe 49,192 hrs · 8,154 cycles

AFT OF STA 2598 S46R SUSPECT CRACKED.(<P>AFT OF STA 2598 S46R CRACK REPAIRED IAW RI-53-81-17627 REV A.&NBSP;<SPAN>NO FURTHER DEFECTS NOTED.</SPAN></P>)

Part: SKIN — DAMAGED (NR 18 FLAP) · airframe 49,192 hrs · 8,154 cycles

#18 V/C FLAP LSA LAYER DAMAGED.(<P>PERFORMED REPAIR AT #18 V/C FLAP LSA LAYER DAMAGED AREA PER CMM 57-55-42 REPAIR 17-1 REV 33. NO FURTHER DEFECTS NOTED.</P>)

Part: STRINGER — CRACKED (ZONE 200) · airframe 49,192 hrs · 8,154 cycles

FWD OF STA 2598 S3R FOUND CRACKED.(<P>FWD OF STA 2598 S3R CRACK REPAIRED IAW RI-53-81-17625 REV A.&NBSP;<SPAN>NO FURTHER DEFECTS NOTED.</SPAN></P>)

Part: PANEL — CRACKED (ZONE 500) · airframe 49,192 hrs · 8,154 cycles

LHW T/E LWR PNL (115U5464-1) FOUND CRACK AND DELAMINATION.(<P>PERFORMED REPAIR AT CRACK AND DELAMINATION AREA IAW RI-57-20-17583 REV A. NO FURTHER DEFECTS NOTED.</P>)

Part: STRINGER — CRACKED (ZONE 200) · airframe 49,192 hrs · 8,154 cycles

AFT OF STA 2598, S7R FOUND CRACKED.(<P>AFT OF STA 2598, S7R CRACK REPAIRED IAW RI-53-81-17569 REV A.&NBSP;<SPAN>NO FURTHER DEFECTS NOTED.</SPAN></P>)

Part: STRIKER — CRACKED (ZONE 200) · airframe 49,192 hrs · 8,154 cycles

FWD OF BS 2360 STR 6L FOUND CRACK.(<P>FWD OF BS 2360 STR 6L FOUND CRACK REPAIRED IAW RI-53-61-17576 REV B. NO FURTHER DEFECTS NOTED.</P>)

Part: STRINGER — CRACKED (ZONE 200) · airframe 49,192 hrs · 8,154 cycles

FWD OF STA 2598 S8L CRACKED.(<P>FWD OF STA 2598 S8L CRACK REPAIRED IAW RI-53-81-17573 REV A.&NBSP;<SPAN>NO FURTHER DEFECTS NOTED.</SPAN></P>)

Part: STRINGER — CRACKED (ZONE 200) · airframe 49,192 hrs · 8,154 cycles

M/D - STA 760-780 S-9L STRINGER FOUND CRACK.(<P>M/D - STA 760-780 S-9L STRINGER CRACK REPAIRED IAW RI-53-21-17628 REV A.&NBSP;<SPAN>NO FURTHER DEFECTS NOTED.</SPAN></P>)

Part: STRINGER — CRACKED (ZONE 200) · airframe 49,192 hrs · 8,154 cycles

FWD OF BS2360 STR 7L FOUND CRACKS.(<P>FWD OF BS2360 STR 7L CRACKS REPAIRED IAW RI-53-61-17577 REV A.&NBSP;<SPAN>NO FURTHER DEFECTS NOTED.</SPAN></P>)

Part: STRINGER — CRACKED (ZONE 200) · airframe 49,192 hrs · 8,154 cycles

FWD OF STA 2598 S5L FOUND CRACKED.(<P>FWD OF STA 2598 S5L CRACK REPAIRED IAW RI-53-81-17563 REV A.&NBSP;<SPAN>NO FURTHER DEFECTS NOTED.</SPAN></P>)

Part: STRINGER — CRACKED (ZONE 200) · airframe 49,192 hrs · 8,154 cycles

MAIN DECK STRINGER S7R STA 880-900 FOUND CRACK.(<P>MAIN DECK STRINGER S7R STA 880-900 CRACK REPAIRED IAW RI-53-21-17606 REV A.&NBSP;<SPAN>NO FURTHER DEFECTS NOTED.</SPAN></P>)

Part: STRINGER — CRACKED (ZONE 200) · airframe 49,192 hrs · 8,154 cycles

FWD OF BS 2360 STR 7R FOUND CRACKS.(<P>FWD OF BS 2360 STR 7R CRACKS REPAIRED IAW RI-53-61-17592 REV B.&NBSP;<SPAN>NO FURTHER DEFECTS NOTED.</SPAN></P>)

Part: STRINGER — CRACKED (ZONE 200) · airframe 49,192 hrs · 8,154 cycles

FWD OF STA 2598 S7R FOUND CRACKED(<P>FWD OF STA 2598 S7R CRACK REPAIRED IAW RI-53-81-17568 REV A.&NBSP;<SPAN>NO FURTHER DEFECTS NOTED.</SPAN></P>)

Part: STRINGER — CRACKED (ZONE 200) · airframe 49,192 hrs · 8,154 cycles

AFT OF STA 2598, S3L FOUND CRACKED.(<P>AFT OF STA 2598, S3L CRACK REPAIRED IAW RI-53-81-17593 REV A. NO FUTHER DEFECTS NOTED.</P>)

Part: STRINGER — CRACKED (ZONE 200) · airframe 49,192 hrs · 8,154 cycles

AFT OF STA 2360 S5R FOUND CRACKED.(<P>AFT OF STA 2360 S5R CRACK REPAIRED IAW RI-53-81-17597 REV A. <SPAN>NO FURTHER DEFECTS NOTED.</SPAN></P>)

Part: STRINGER — CRACKED (ZONE 200) · airframe 49,192 hrs · 8,154 cycles

M/D - STA 2340-2360 S-20R STRINGER FOUND CRACK.(<P>M/D - STA 2340-2360 S-20R STRINGER CRACK REPAIRED IAW RI-53-61-17604 REV A.&NBSP;<SPAN>NO FURTHER DEFECTS NOTED.</SPAN></P>)

Part: STRINGER — CRACKED (ZONE 200) · airframe 49,192 hrs · 8,154 cycles

M/D - STA 880-900 S-11R STRINGER FOUND CRACK.(<P>M/D - STA 880-900 S-11R STRINGER CRACK REPAIRED IAW RI-53-21-17600 REV A.&NBSP;<SPAN>NO FURTHER DEFECTS NOTED.</SPAN></P>)

Part: STRINGER — CRACKED (ZONE 200) · airframe 49,192 hrs · 8,154 cycles

AFT OF STA 2360 S7L FOUND CRACKED.(<P>AFT OF STA 2360 S7L CRACK REPAIRED IAW RI-53-81-17571 REV A. NO FURTHER DEFECTS NOTED.</P>)

Part: STRINGER — CRACKED (ZONE 200) · airframe 49,192 hrs · 8,154 cycles

M/D - STA 1140-1160 S-16R STRINGER FOUND CRACK.(<P>M/D - STA 1140-1160 S-16R STRINGER CRACK REPAIRED IAW RI-53-41-17638 REV A.&NBSP;<SPAN>NO FURTHER DEFECTS NOTED.</SPAN></P>)

Part: STRINGER — CRACKED (ZONE 200) · airframe 49,192 hrs · 8,154 cycles

M/D - STA 860-880 S-7R STRINGER FOUND CRACK.(<P>M/D - STA 860-880 S-7R STRINGER CRACK REPAIRED IAW RI-53-21-17606 REV A.&NBSP;<SPAN>NO FURTHER DEFECTS NOTED.</SPAN></P>)

Part: STRIKER — CRACKED (ZONE 200) · airframe 49,192 hrs · 8,154 cycles

FWD OF BS 2360 STR 2L FOUND CRACKS.(<P>FWD OF BS 2360 STR 2L CRACKS REPAIRED I.A.W RI-53-61-17633 REV A.&NBSP;<SPAN>NO FURTHER DEFECTS NOTED.</SPAN></P>)

Part: SKIN — CORRODED (NR 23 FLAP) · airframe 49,192 hrs · 8,154 cycles

# 23 VC FLAP BULLNOSE FOUND EROSION.(<P>PERFORMED REPAIR AT EROSION AREA IAW SRM 51-70-04 REPAIR 5 REV 45. NO FURTHER DEFECTS NOTED.</P>)

Part: CHANNEL — CRACKED (ZONE 300) · airframe 49,192 hrs · 8,154 cycles

EMP -RH HORIZONTAL STABILIZER TIP FAIRING T/E WEDGE U CHANNEL CRACKED.(<P>EMP - RH HORIZONTAL STABILIZER TIP FAIRING T/E UPPER CLOSURE RIB REPLACED IAW RI-55-10-17554 REV A. NO FURTHER DEFECTS NOTED.</P>)

Part: STRINGER — CRACKED (ZONE 200) · airframe 49,192 hrs · 8,154 cycles

M/D - STA 780-800 S-9L STRINGER FOUND CRACK.(<P>M/D - STA 780-800 S-9L STRINGER CRACK REPAIRED IAW RI-53-21-17628 REV A. <SPAN>NO FURTHER DEFECTS NOTED.</SPAN></P>)

Part: STRINGER — CRACKED (ZONE 200) · airframe 49,192 hrs · 8,154 cycles

AFT OF STA 2360 S24L FOUND CRACKED.(<P>AFT OF STA 2360 S24L CRACK REPAIRED IAW RI-53-81-17572 REV A. NO FURTHER DEFECTS NOTED.</P>)

Part: STRINGER — CRACKED (ZONE 200) · airframe 49,192 hrs · 8,154 cycles

AFT OF STA 2598 S24L SUSPECT CRACK.(<P>AFT OF STA 2598 S24L CRACK REPAIRED IAW RI-53-81-17596 REV A.&NBSP;<SPAN>NO FURTHER DEFECTS NOTED.</SPAN></P>)

Part: STRINGER — CRACKED (ZONE 200) · airframe 49,192 hrs · 8,154 cycles

FWD OF STA 2598 S1L FOUND CRACKED.(<P>FWD OF STA 2598 S1L CRACK REPAIRED IAW RI-53-81-17584 REV A.&NBSP;NO FURTHER DEFECTS NOTED.</P>)

Part: ATTACH FITTING — CRACKED (ZONE 500) · airframe 49,192 hrs · 8,154 cycles

LHW ILES 465.55 DIAGONAL STRUT ATT FTG FOUND CRACKED.(<P>LHW ILES 465.55 DIAGONAL STRUT ATT FTG CRACK REPAIRED IAW SRM 57-41-09-2R-2 REPAIR 2.&NBSP;<SPAN>NO FURTHER DEFECTS NOTED.</SPAN></P>)

Part: STRINGER — CRACKED (ZONE 200) · airframe 49,192 hrs · 8,154 cycles

AFT OF STA 2360 S21L FOUND CRACKED.(<P>AFT OF STA 2360 S21L CRACK REPAIRED IAW RI-53-81-17565 REV C. NO FURTHER DEFECTS NOTED.</P>)

Part: STRINGER — CRACKED (ZONE 200) · airframe 49,192 hrs · 8,154 cycles

AFT OF STA 2360 S14R FOUND CRACKED.(<P>AFT OF STA 2360 S14R CRACK REPAIRED IAW RI-53-81-17624 REV A. <SPAN>NO FURTHER DEFECTS NOTED.</SPAN></P>)

Part: STRINGER — CRACKED (ZONE 200) · airframe 49,192 hrs · 8,154 cycles

FWD OF STA 2598 S7L FOUND CRACKED.(<P>FWD OF STA 2598 S7L CRACK REPAIRED IAW RI-53-81-17580 REV A. NO FURTHER DEFECTS NOTED.</P>)

Part: STRIKER — CRACKED (ZONE 200) · airframe 49,192 hrs · 8,154 cycles

FWD OF BS2360 STR 1R FOUND CRACKS.(<P>FWD OF BS2360 STR 1R CRACKS REPAIRED IAW RI-53-61-17632 REV A.&NBSP;<SPAN>NO FURTHER DEFECTS NOTED.</SPAN></P>)

Part: STRIKER — CRACKED (ZONE 200) · airframe 49,192 hrs · 8,154 cycles

AFT OF STA 2598, S1L FOUND CRACKED.(<P>AFT OF STA 2598, S1L CRACK REPAIRED IAW RI-53-81-17587 REV A.&NBSP;<SPAN>NO FURTHER DEFECTS NOTED.</SPAN></P>)

Part: SKIN — DAMAGED (NR 19 FLAP) · airframe 49,192 hrs · 8,154 cycles

#19 V/C FLAP LSA LAYER DAMAGED.(<P>PERFORMED REPAIR AT #19 V/C FLAP LSA LAYER DAMAGED AREA PER CMM 57-55-42 REPAIR 17-1 REV 33. NO FURTHER DEFECTS NOTED.</P>)

Part: STRINGER — CRACKED (ZONE 200) · airframe 49,192 hrs · 8,154 cycles

AFT OF STA 2360 S2R FOUND CRACKED.(<P>AFT OF STA 2360 S2R CRACK REPAIRED IAW RI-53-81-17574 REV A. NO FURTHER DEFECTS NOTED.</P>)

Part: STRINGER — CRACKED (ZONE 200) · airframe 49,192 hrs · 8,154 cycles

AFT OF STA 2360 S6L FOUND CRACKED.(<P>AFT OF STA 2360 S6L CRACK REPAIRED IAW RI-53-81-17595 REV A. NO FURTHER DEFECTS NOTED.</P>)

Part: STRIKER — CRACKED (ZONE 100) · airframe 49,192 hrs · 8,154 cycles

AFT OF STA 2598 S49L SUSPECT CRACKED.(<P>AFT OF STA 2598 S49L CRACK REPAIRED IAW RI-53-81-17581 REV A. <SPAN>NO FURTHER DEFECTS NOTED.</SPAN></P>)

Part: STRINGER — CRACKED (ZONE 200) · airframe 49,192 hrs · 8,154 cycles

M/D - STA 1660-1680 S-9R STRINGER FOUND CRACK.(<P>M/D - STA 1660-1680 S-9R STRINGER CRACK REPAIRED IAW RI-53-60-17615 REV A. NO FURTHER DEFECTS NOTED.</P>)

Part: STRIKER — CRACKED (ZONE 200) · airframe 49,192 hrs · 8,154 cycles

FWD OF BS 2360 STR 2R FOUND CRACKS.(<P>FWD OF BS 2360 STR 2R CRACKS REPAIRED IAW RI-53-61-17601 REV A.&NBSP;<SPAN>NO FURTHER DEFECTS NOTED.</SPAN></P>)

Part: STRINGER — CRACKED (ZONE 200) · airframe 49,192 hrs · 8,154 cycles

FWD OF STA 2598 S6R FOUND CRACKED.(<P>FWD OF STA 2598 S6R CRACK REPAIRED IAW RI-53-81-17564 REV A.&NBSP;<SPAN>NO FURTHER DEFECTS NOTED.</SPAN></P>)

Part: STRINGER — CRACKED (ZONE 200) · airframe 49,192 hrs · 8,154 cycles

M/D - STA 860-880 S-8L STRINGER FOUND CRACK.(<P>M/D - STA 860-880 S-8L STRINGER CRACK REPAIRED IAW RI-53-21-17617 REV A.&NBSP;<SPAN>NO FURTHER DEFECTS NOTED.</SPAN></P>)

Part: STRINGER — CRACKED (ZONE 200) · airframe 49,192 hrs · 8,154 cycles

M/D - STA 2160-2180 S-11R STRINGER FOUND CRACK.(<P>M/D - STA 2160-2180 S-11R STRINGER CRACK REAPAIR IAW RI-53-61-17643 REV A.&NBSP;<SPAN>NO FURTHER DEFECTS NOTED.</SPAN></P>)

Part: SKIN — DAMAGED (NR 7 FLAP) · airframe 49,192 hrs · 8,154 cycles

#7 V/C FLAP LSA LAYER DAMAGED.(<P>PERFORMED REPAIR AT #7 V/C FLAP LSA LAYER DAMAGED AREA PER CMM 57-55-42 REPAIR 17-1 REV 33. NO FURTHER DEFECTS NOTED.</P>)

Part: STRINGER — CRACKED (ZONE 200) · airframe 49,192 hrs · 8,154 cycles

M/D - STA 860-880 S-11R STRINGER FOUND CRACK.(<P>MAIN DECK STRINGER S7R STA 880-900 CRACK REPAIRED IAW RI-53-21-17600 REV A.&NBSP;<SPAN>NO FURTHER DEFECTS NOTED.</SPAN></P>)

Part: STRINGER — CRACKED (ZONE 200) · airframe 49,192 hrs · 8,154 cycles

M/D - STA 840-860 S-9L STRINGER FOUND CRACK.(<P>M/D - STA 840-860 S-9L STRINGER CRACK REPAIRED IAW RI-53-21-17628 REV A.&NBSP;<SPAN>NO FURTHER DEFECTS NOTED.</SPAN></P>)

Part: STRINGER — CRACKED (ZONE 200) · airframe 49,192 hrs · 8,154 cycles

FWD OF BS 2360 STR 10R FOUND CRACK.(<P>FWD OF BS 2360 STR 10R CRACK REPAIRED IAW RI-53-61-17589 REV B.&NBSP;<SPAN>NO FURTHER DEFECTS NOTED.</SPAN></P>)

Part: STRIKER — CRACKED (ZONE 200) · airframe 49,192 hrs · 8,154 cycles

AFT OF STA 2598, S1R FOUND CRACKED.(<P>AFT OF STA 2598, S1R CRACK REPAIRED IAW RI-53-81-17585 REV A.&NBSP;<SPAN>NO FURTHER DEFECTS NOTED.</SPAN></P>)

Part: STRINGER — CRACKED (ZONE 200) · airframe 49,192 hrs · 8,154 cycles

M/D - STA 1940-1960 S-11L STRINGER FOUND CRACK.(<P>M/D - STA 1940-1960 S-11L STRINGER CRACK REPAIR IAW 747-8F SRM 53-60-03 REPAIR 4 ALTERNATIVE 2 &AMP; 747-8F SRM 53-00-03 REPAIR 7 ALTERNATIVE 2 &AMP; RI-53-61-17630 REV A.&NBSP;<SPAN>NO FURTHER DEFECTS NOTED.</SPAN></P>)

Part: STRINGER — CRACKED (ZONE 200) · airframe 49,192 hrs · 8,154 cycles

AFT OF STA 2598, S12L FOUND CRACKED.(<P>AFT OF STA 2598, S12L CRACK REPAIRED IAW RI-53-81-17603 REV B. <SPAN>NO FURTHER DEFECTS NOTED.</SPAN></P>)

Part: STRINGER — CRACKED (ZONE 200) · airframe 49,192 hrs · 8,154 cycles

AFT OF STA 2360 S20L FOUND CRACKED.(<P>AFT OF STA 2360 S20L CRACK REPAIRED IAW RI-53-81-17588 REV B. NO FURTHER DEFECTS NOTED.</P>)

Part: STRINGER — CRACKED (ZONE 200) · airframe 49,192 hrs · 8,154 cycles

M/D - STA 980+160 - 1000 S-12L STRINGER FOUND CRACK.(<P>M/D - STA 980+160 - 1000 S-12L STRINGER CRACK REPAIRED IAW RI-53-20-17611 REV A.&NBSP;<SPAN>NO FURTHER DEFECTS NOTED.</SPAN></P>)

Part: STRINGER — CRACKED (ZONE 200) · airframe 49,192 hrs · 8,154 cycles

M/D - STA 860-880 S-7L STRINGER FOUND CRACK.(<P>M/D - STA 860-880 S-7L STRINGER CRACK REPAIRED IAW RI-53-20-17616 REV A.&NBSP;<SPAN>NO FURTHER DEFECTS NOTED.</SPAN></P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,028 hrs · 6,828 cycles

EMP - APU COMPT RH FRAME CRACK FOUND AT STA 2696.78, HARNESS SUPPORT BRACKET AREA.(<P>EMP - APU COMPT RH FRAME P/N: 65B02763-8 WL 305 FRAME CRACK AREA REPAIRED IAW SRM 53-80-07-2R-1 REPAIR 1</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,028 hrs · 6,828 cycles

#9 VC FLAP  LSA LAYER IN POOR CONDITION(<P>PERFORMED LSA REPAIR AS PER CMM57-55-42 REPAIR 17-1</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,028 hrs · 6,828 cycles

R/H H.STAB (STAB BL 421.5) WEB CRACKED.(<P>R/H H.STAB (STAB BL 421.5) WEB CRACK AREA REPAIRED IAW SRM 55-10-09-2R-12 REPAIR 12.</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,028 hrs · 6,828 cycles

#18 VC FLAP  LSA LAYER IN POOR CONDITION(<P>PERFORMED LSA REPAIR AS PER CMM 57-55-42 REPAIR 17-1</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,028 hrs · 6,828 cycles

RHW L/E OLES 1450-1520 LWR FIXED PNLS SUPPORT CHANNEL FOUND CORROSION.(<P><SPAN>RHW L/E OLES 1450-1520 LWR FIXED PNLS SUP</SPAN>PORT CHANNEL CORROSION REMOVED AND REPROTECTED IAW SRM 57-10-02 AND SRM 51-20-01. CHECKED WITHIN SRM 57-41-13 ADL 1 FIG 101 LIMIT.</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,028 hrs · 6,828 cycles

R/H H.STAB (STAB BL 421.5) LWR CHORD CRACKED.(<P>R/H H.STAB (STAB BL 421.5) LOWER CHORD CRACK AREA REPAIRED IAW SRM 55-10-09-2R-12 REPAIR 12.</P>)

Part: STABILIZER — UNKNOWN (UNKNOWN) · airframe 40,028 hrs · 6,828 cycles

EMP RH H STAB STA 560 REAR SPAR STIFFENER CRACK(<P>RH HORIZONTAL STABILIZER REAR SPAR ATT ANGLE REPLACE IAW RI 55-00-16124 REV A</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,028 hrs · 6,828 cycles

FX - FUSELAGE SKIN STA 227 STR 22L FOUND RIVET BURN MARK.(<P>FX - STA 227 LH STR 22L 1EA RIVET BURN MARK REPAIRED IAW SRM 53-00-01-2R-9 REPAIR 9 PAR 5E.</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,028 hrs · 6,828 cycles

FX - NOSE CARGO DOOR EXIT SURFACE FOUND RIVET BURN MARK AT STA 220 LH S-14C TO STR 14D.(<P>FX - STA 220 LH STA 14C TO STR 14D NOSE CARGO DOOR EXIT SURFACE 1EA RIVET BURN MARK REPAIRED IAW SRM 53-00-01-2R-9 REPAIR 9 PAR 5E.</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,028 hrs · 6,828 cycles

LHW L/E CAVITY IFSS 465.55 SUPPORT RIB LOWER FLANGE BRACE SUPPORT FOUND FASTENER HOLE ELONGATED.(<P><SPAN>LHW L/E CAVITY IFSS 465.55 SUP</SPAN>PORT RIB LOWER FLANGE BRACE SUPPORT FASTENER HOLE ELONGATED AREA REPAIRED IAW RI-57-00-16123 REV.A</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,028 hrs · 6,828 cycles

FX - FUSELAGE SKIN STA 202.5 STR 22L FOUND RIVET BURN MARK.(<P>FX - STA 202.5 LH STR 22L 1EA RIVET BURN MARK REPAIRED IAW SRM 53-00-01-2R-9 REPAIR 9 PAR 5E.</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,028 hrs · 6,828 cycles

FX - NOSE CARGO DOOR EXIT SURFACE FOUND RIVET BURN MARK AT STA 254 LH S-14C.(<P><SPAN>FX - STA 254 LH STR-14C NOS</SPAN>E CARGO DOOR EXIT SURFACE 1EA RIVET BURN MARK REPAIRED IAW SRM 53-00-01-2R-9 REPAIR 9 PAR 5E.</P>)

Part: LAMP — UNKNOWN (UNKNOWN) · airframe 40,028 hrs · 6,828 cycles

EMERGENCY LIGHT INERTIA REEL LT FOUND INOP(<P>LAMP REPLACED AND OPERATION TEST NORMAL&NBSP;</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,028 hrs · 6,828 cycles

RHW L/E CAVITY ILE 440 SUPPORT RIB LOWER FLANGE BRACE SUPPORT FOUND CRACKED(<P>RHW L/E CAVITY ILES 442.84 RIB SUPPORT BEAM ATTACHMENT FITTING CRACK AREA REPAIRED IAW RI-57-41-16119 REV A</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,028 hrs · 6,828 cycles

FX - FUSELAGE SKIN STA 236 STR 22L TO STR 23L FOUND RIVET BURN MARK.(<P>FX - STA 236 LH STR 22L TO 23L 1EA RIVET BURN MARK REPAIRED IAW SRM 53-00-01-2R-9 REPAIR 9 PAR 5E.</P>)

Part: PANEL — DAMAGED · airframe 37,868 hrs · 6,488 cycles

MDDR 169109 - #2 ENG INBOARD PYLON PANEL 464 CBR MISSING/DAMAGE(<P>#2 ENG INBOARD PYLON PANEL 464 CBR P/N: 313U8660-11 DAMAGED AREA REPAIRED IAW RI-54-00-15813 REV.A</P>)

Part: STRINGER — CRACKED (BS 850-950) · airframe 31,777 hrs · 5,457 cycles

CRACK DAMAGES ON THE STRINGER S-9L BETWEEN STA 850 AND STA 950(<P>ACCOMPLISHED EI NO T2021A53M-351 REV 1. JOB COMPLETED AND CONDITION CHK NORMAL</P>)

Part: STRINGER — CRACKED (BS 740) · airframe 31,777 hrs · 5,457 cycles

REPAIR - CRACK DAMAGE ON THE STRINGER S-15R AT AFT SIDE OF STA 740(<P>REPAIR DAMAGE AREA IAW EI NO T2021A53M-380 REV 2. CONDITION CHK NORMAL AND JOB COMPLETED</P>)

Part: STRINGER — CRACKED (BS 1960) · airframe 31,777 hrs · 5,457 cycles

CRACK DAMAGE ON STRINGER S-18R, AT FWD SIDE OF STA 1960(<P>REPAIR STRINGER IAW EI NO T2021A53M-409 REV 1. CONDITION CK NORMAL AND JOB COMPLETED.</P>)

Part: STRINGER — CRACKED (BS 870-910) · airframe 31,777 hrs · 5,457 cycles

CRACK - STRINGER, FUSELAGE INTERNAL SKIN, STA 870 - STA 910.(<P>ACCOMPLISHED THE EI NO T2021A53M-352 REV 1. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)

Part: ACTUATOR — NO TEST (MLG) · airframe 31,777 hrs · 5,457 cycles

FOUND LH BLG ALTERNATE EXTENSION SYSTEM ELECTRICAL ACTUATOR FUNCTION TEST FAIL(<P>IAW AMM 32-35-01-004-001 REV 34 AND AMM 32-35-01-404-007 REV 34. REPLACED AND DO THE POST INSTALLATION TEST. RESULT WAS SATISFACTORY</P>)

Part: STRINGER — CRACKED (BS 2180) · airframe 31,777 hrs · 5,457 cycles

CRACK DAMAGE ON THE STRINGER S-19L OF STA 2180 OF AFT SIDE(<P>REMOVE AFFECTED FASTENER TO GET ACCESS IAW SRM 51-40-02 REV 32. ACCOMPLISHED EI NO T2021A53M-413 REV 2. REINSTALLED FASTENER IAW SRM 51-40-02 REV 33 AND DWG NO 146U2200 SHEET 167 REV -. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)

Part: STRINGER — CRACKED (BS 740) · airframe 31,777 hrs · 5,457 cycles

CRACK ON THE STRINGER S-14R OF STA 740 AFT SIDE(<P>REPAIR DAMAGED AREA IAW EI NO T2021A53M-376 REV 2. CONDITION CHECK NORMAL AND JOB COMPLETED.</P>)

Part: ACTUATOR — MALFUNCTIONED (RT MLG) · airframe 31,777 hrs · 5,457 cycles

FOUND RH WLG ALTERNATE EXTENSION ACTUATOR FUNCTION ABNORMAL(<P>IAW AMM 32-36-01/401 REV 34 REPLACED AND PERFORM OPERATION TEST. RESULT WAS NORMAL.</P>)

Part: STRINGER — CRACKED (BS 880-890) · airframe 31,777 hrs · 5,457 cycles

CRACK DAMAGES ON THE STRINGER S-11R BETWEEN STA 880 AND 890(<P>ACCOMPLISHED THE STRINGER REPAIR IAW EI NO 52021A53M-354 REV 1. CONDITION CHECK NORMAL AND JOB COMPLETED</P>)

Part: STRINGER — CRACKED (BS 1960) · airframe 31,777 hrs · 5,457 cycles

CRACK DAMAGE ON STRINGER S-15L AT FWD SIDE AND AFT SIDE OF STA 1960(<P>REMOVED AFFECTED FASTENER TO GET ACCESS IAW SRM 51-40-02 REV 32. ACCOMPLISHED EI NO T2021A53M-408 REV 1. REINSTALLED FASTENER IAW SRM 51-40-02 REV 32 AND DWG NO 146U1940 SHEET 206 REV - AND DWG NO 146U1980 SHEET 86 REV B. JOB COMPLETED AND CONDITION CHK NORMAL.</P>)

Part: STRINGER — CRACKED (BS 740) · airframe 31,777 hrs · 5,457 cycles

CRACK DAMAGE ON THE STRINGER S-17R OF STA 740 AFT SIDE(<P>ACCOMPLISHED THE JOB IAW EI NO T2021A53M-381 REV 2. JOB COMPLETED AND CONDITION CHK NORMAL</P>)

Part: STRINGER — CRACKED (BS 740) · airframe 31,777 hrs · 5,457 cycles

CRACK DAMAGE ON STRINGER S-23L, AT FWD SIDE OF STA 740.(<P>REMOVE AFFECTED FASTENERS TO GET ACCESS IAW SRM 51-40-02 REV 32. ACCOMPLISHED EI NO T2021A53M-382 REV 3. REINSTALLED FASTENERS IAW SRM 51-40-02 REV 33 AND DWG NO 142U0720 SHEET 68 REV -. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)

Part: STRINGER — CRACKED (BS 960-970 S7R) · airframe 31,777 hrs · 5,457 cycles

CRACK DAMAGES ON THE STRINGER S-7R BETWEEN STA 960 AND STA 970(<P>ACCOMPLISHED THE STRINGER REPAR IAW EI NO T2021A53M-348 REV 2 AND ATTACHING WITH WO 5541933 (070). CONDITION CHECK NORMAL AND JOB COMPLETED</P>)

Part: STRINGER — CRACKED (BS 880) · airframe 31,777 hrs · 5,457 cycles

CRACK - STRINGER, FUSELAGE INTERNAL SKIN, STA 880, S-8L(<P>ACCOMPLISHED THE EI NO T2021A53M-349 REV 1. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)

Part: STRINGER — CRACKED (BS 950-980 S9L) · airframe 31,777 hrs · 5,457 cycles

CRACK DAMAGE ON THE STRINGER S-9L BETWEEN STA 950 AND STA 980 + 20(<P>ACCOMPLISHED EI NO T2021A53M-351 REV 1 AND EI ATTACHED TO W/O NO 5541948 (072). JOB COMPLETED AND CONDITION CHECK NORMAL</P>)

Part: RIB — WORN (RT WING) · airframe 31,777 hrs · 5,457 cycles

RH WING INBD L/E CAVITY RIB WORN AT IFSS 401.01(<P>ACCOMPLISHED EI NO T2021A57M-407 REV 2. JOB COMPLETED AND CONDITION CHK NORMAL.</P>)

Part: STRINGER — CRACKED (BS 940-950) · airframe 31,777 hrs · 5,457 cycles

CRACK DAMAGE ON THE STRINGER S-8R BETWEEN STA 940 AND STA 950(<P>ACCOMPLISHED THE STRINGER REPAIR IAW EI NO T2021A53M-350 REV 1. CONDITION CHECK NORMAL AND JOB COMPLETED.</P>)

Part: STRINGER — CRACKED (BS 870-890 S7R) · airframe 31,777 hrs · 5,457 cycles

CRACK DAMAGES ON THE STRINGER S-7R BETWEEN STA 870 AND STA 890(<P>ACCOMPLISHED THE STRINGER REPAIR IAW EI NO T2021A-53M-348 REV 2. CONDITION CHECK NORMAL AND JOB COMPLETED.</P>)

Part: STRINGER — CRACKED (BS 870-890) · airframe 31,777 hrs · 5,457 cycles

CRACK - STRINGER, FUSELAGE INTERNAL SKIN, STA 882 S-7L.(<P>ACCOMPLISHED THE EI NO T2021A53M-347 REV 1. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)

Part: RIB — WORN (LT WING) · airframe 31,777 hrs · 5,457 cycles

LH WING INBD LE CAVITY RIB WORN AT IFSS 439.34.(<P>ACCOMPLISHED EI NO T2021A57M-415 REV 2. JOB COMPLETED AND CONDITION CHK NORMAL</P>)

Part: STRINGER — CRACKED (BS 2180) · airframe 31,777 hrs · 5,457 cycles

CRACK DAMAGE ON THE STRINGER S-13L OF STA 2180 AFT SIDE(<P>REMOVE AFFECTED FASTENERS TO GET ACCESS IAW SRM 51-40-02 REV 32. ACCOMPLISHED EI NO T2021A53N-412 REV 2. REINSTALLED FASTENERS IAW SRM 51-40-02 REV 32 AND DWG NO 146U3932 SHEET 10 REV -. JOB COMPLETED AND CONDITION CHECK NORMAL</P>)

Part: STRINGER — CRACKED (BS 870-880 S10R) · airframe 31,777 hrs · 5,457 cycles

CRACK DAMAGE ON THE STRINGER S-10R BETWEEN STA 870 AND STA 880(<P>ACCOMPLISHED THE STRINGER REPAIR IAW EI NO T2021A53M-353 REV 1. CONDITION CHECK NORMAL AND JOB COMPLETED</P>)

Part: STRINGER — CRACKED (BS 2180) · airframe 31,777 hrs · 5,457 cycles

CRACK DAMAGE ON THE STRINGER S-20L OF STA 2180 AFT SIDE(<P>REMOVED AFFECTED FASTENER TO GET ACCESS IAW SRM 51-40-02 REV 32. ACCOMPLISHED EI NO T2021A53M-414 REV 1. REINSTALLED FASTENER IAW SRM 51-40-02 REV 32. AND DWG NO 146U2200 SHEET 166 REV -. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)

Part: SKIN — GOUGED (BS 2575 S49-51L) · airframe 31,777 hrs · 5,457 cycles

GOUGE ON THE EXTERNAL SIDE OF SKIN NEAR STA 2575 BETWEEN S-49L AND S-51L(<P>REPAIR DAMAGE AREA IAW SRM 53-00-01-2R-1 FIG 208. REV 32. AND DWG NO 148U3260 SHEET 1 REV 0. JOB COMPLETED AND CONDITION CHK NORMAL.</P>)

Part: STRINGER — CRACKED (BS 1960) · airframe 31,777 hrs · 5,457 cycles

CRACK DAMAGE ON STRINGER S-20R, AT FWD SIDE OF STA 1900(<P>REPAIR STRINGER IAW EI NO T2021A53M-410 REV 1. COND CHK NORMAL AND JOB COMPLETED.</P>)

Part: STRINGER — CRACKED (BS 2180) · airframe 31,777 hrs · 5,457 cycles

CRACK DAMAGE ON STRINGER S-10R OF STA 2180 AFT SIDE(<P>ACCOMPLISH EI NO T2021A53M-411 REV 2 AND DWG NO 146U2181 SHEET 389 REV - AND DWG NO 146U1312 SHEET 113 REV - AND DWG NO 146U3481 SHEET 47 REV -. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)

Part: SENSOR — FAILED (LT BLG) · airframe 29,031 hrs · 4,993 cycles

ON DEPARTURE "GEAR TILT" EICAS CAUTION. NON NORMAL CHECK LIST ACTIONED. "GEAR TILT" STATUS MSG. FOUND CMC MSG 32723. IFIM / 32-31-00-810-821 PERFORMED. LT BODY GEAR TRUCK TILT SENSOR REMOVED AND REPLACED AS PER AMM 32-61-12-402-009, 32-61-12-002-001. PSEU / TEST PASSED. DISCREPANCY- FOUND LT BODY GEAR TRUCK TILT ACTUATOR HYD SUPPLY LINE BROKEN AND FOUND SMALL LEAKAGE. CORRECTIVE ACTION- LT BODY GEAR TRUCK TILT ACTUATOR HYD SUPPLY LINE REMOVED AND REPLACED AS PER 20-11-18-204-008. HYD LEAK CHECK AND TRUCK TILT ACTUATOR BLEED / PERFORMED AS PER AMM 32-13-15-404-010.

Part: CHANNEL — CRACKED (LT HORIZ STAB) · airframe 23,409 hrs · 4,041 cycles

LT HORIZONTAL STABILIZER T/E BOND ASSY CHANNEL CRACK.(<P>LT HORIZONTAL STABILIZER T/E BOND ASSY. CHANNEL REPAIRED IAW RI-55-10-13343 REV.A<BR /></P>)

Part: FITTING — CHAFED (TE FLAP) · airframe 23,469 hrs · 4,050 cycles

LT WING I/B FLAP O/B ROLLER GUIDE FITTING FOUND CHAFING MARK.(<P>LHW FIXED T/E WBL 448.7 DEFLECTION TRACK CHAFING AREAS REPAIRED IAW RI-57-20-13351 REV.B.</P>)

Part: RIB — NOT REPORTED (LT HORIZ STAB) · airframe 23,409 hrs · 4,041 cycles

LT HORIZONTAL STABILIZER RIB TIME LIMITED REPAIR CONVERSION REPAIR(<P>LT HORIZONTAL STABILIZER CLOSURE RIB REPAIRED IAW RI-55-10-13346 REV.A<BR /></P>)

Part: LUG — CRACKED (NR 3 PYLON) · airframe 23,409 hrs · 4,041 cycles

NR 3 PYLON I/B NACELLE COVER VAPOR BARRIER O/B LUG FOUND CRACKED(<P>NR 3 PYLON I/B NACELLE COVER VAPOR BARRIER O/B LUG REPAIRED IAW RI-57-41-13342 REV.A</P>)

Part: FITTING — CHAFED (TE FLAP) · airframe 23,469 hrs · 4,050 cycles

RT WING I/B FLAP O/B ROLLER GUIDE FITTING FOUND CHAFFING MARK.(<P>RHW FIXED T/E WBL 448.7 DEFLECTION TRACK CHAFING AREAS REPAIRED IAW RI-57-20-13351 REV.B</P>)

Part: FRAME — DAMAGED (NR 4 PLYON) · airframe 14,716 hrs · 2,571 cycles

NR 4 PYLON FOUND HEAT DAMAGED ON AFT FAIRING NR 1 FRAMES. REPAIRED IAW R1-54-00-116REV A.

Part: SUPPORT — BROKEN (BS 1480) · airframe 14,716 hrs · 2,517 cycles

AFT CARGO BS 1480 LBL 6 CEILING SUPPORT FOUND BROKEN. THE CELING SUPPORT WAS REPAIRED IAW R1-25-22-11680 REV A.

Part: FLOOR PANEL — DEFORMED (BS 600-640) · airframe 14,716 hrs · 2,571 cycles

FWD CARGO BAY BALL MAT PANEL BS 600-640 FOUND DEFORMED. REPAIRED IAW EO 4825A103</P>)

Part: STRUCTURE — DAMAGED (RT WING) · airframe 14,716 hrs · 2,571 cycles

RT WING TIP OTBD AFT EDGE CORNER FOUND BURNED. REPAIRED IAW RI-57-30-11689 REV A.

Part: SKIN — DAMAGED (BS 200) · airframe 14,716 hrs · 2,571 cycles

BS 200 STRINGERS 24A TO 26R SKIN ONE FASTENER HOLE FOUND LIGHTNING STRIKE. INSTALLED A FREEZE PLUG REPAIR IAW R1-52-10-11688 REV A.

Part: CHANNEL — CRACKED (RT WING MLG WW) · airframe 14,716 hrs · 2,571 cycles

RT WING T/E CAVITY WS 500 MLG UPPER CHANNEL FOUND CRACKED. REPAIRED IAW RI-57-22-11684 REV A.

Part: CHANNEL — CRACKED (LT WING) · airframe 14,716 hrs · 2,571 cycles

LT WING T/E WS 500 MLG UPPER CHANNEL FOUND CRACKED. REPAIRED IAW RI-57-22-11683 REV A.

Part: SUPPORT BRACKET — CRACKED (NR 2 PYLON) · airframe 14,716 hrs · 2,571 cycles

NR 2 PYLON AFT VAPOR BARRIER TOP PANEL OTBD SUPPORT BRACKET FOUND CRACK. NR 2 PYLON AFT VAPOR BARRIER OTBD LUG REPAIRED IAW RI-57-41-11687 REV A.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 14,243 hrs · 2,508 cycles

REJECTED TAKEOFF. MASTER WARNING CONFIGURATION STAB LOW SPEED. PROBLEM CAUSED BY FLT CONTROL SYS MESSAGE. PERFOMED LCE L AND LCE R GROUND TEST IAW AMM 27-09-01 AND FOUND ALL SATISFACTORY.

Part: ACCESS DOOR — MISSING (AC SYSTEM) · airframe 10,565 hrs · 1,894 cycles

LEFT SIDE AIR CONDITIONING ACCESS DOOR, DOOR MISSING. R & R DOOR 191NL IAW MM 52-48-01.

Part: FRAME — BROKEN (FUSELAGE) · airframe 6,827 hrs · 1,288 cycles

BROKEN CONDITION ON THE STATION 1600 LOWER FRAME UPPER CAP NEAR RBL 9. REPAIR DAMAGE IAW EI NO T2015A53B044.

Part: FMC — MALFUNCTIONED (COCKPIT) · airframe 2,732 hrs · 472 cycles

EICAS MESSAGE, FMC RUNWAY DIS, DISPLAYED DURING TAKEOFF ROLL. RESET FMC LT & FMC RT IAW 34-51-00.

Part: WARNING MESSAGE — ILLUMINATED (FMC)

LOW SPEED REJECT (40-50KTS) DUE TO EICAS MESSAGE "FMC RUNWAY DIS" CONFIRMED POSITION THEN NORMAL TAKE OFF,

Part: ENGINE — DAMAGED (NR 2) · airframe 2,357 hrs · 400 cycles

NR 2 ENGINE, REQUIRES REPLACEMENT DUE TO HIGH PRESSURE COMPRESSOR ROTOR DAMAGED BEYOND SERVICEABLE LIMITS. REPLACED NR 2 ENGINE IAW AMM 71-00-00 AND REMOVAL AND INSTALLATION LIST 1039.

Part: ENGINE — POWER LOSS · airframe 2,332 hrs · 396 cycles

UNCOMMANDED ROLLBACK OF NR 2 AND NR 4 ENGINES IN ICE CONDITIONS, ENG X THRUST, MASTER CAUTION. ENGINES RETURNED TO NORMAL AFTER EXITING ICE CRYSTALS, NOTIFIED MCC, INSPECTED ENGINES IAW FIM 73-21-00 STEP 1 THROUGH 9, NFF, OK FOR CONTINUED SERVICE.