N856FT

Part: LIGHT — INOP (UPPER DECK DOME)

EMERGENCY LIGHT IN UPPER DECK DOME INOP. REPLACED EMERGENCY LIGHT ASSY AND CKECKED OK PER MM 35-51-00.

Part: LIGHT — INOP (PAX DOOR)

EMERGENCY EXIT LIGHT INOP AT DOOR SLIDE AREA. REPLACED EMERGENCY LIGHT MODULE AT UPPER DOOR OVERHEAD LOCATION. OPS CHECK NORMAL PER MM 35-51-00.

Part: CONNECTOR — LOOSE (COCKPIT)

EMERGENCY LIGHTING DOES NOT WORK. CLEANED AND RESEATED CANNON PLUG ON EMERGENCY PANEL SYSTEM. OPS NORMAL PER MM 33-51-00.

Part: FAIRING — DAMAGED (NR 4 ENGINE)

NR 4 ENGINE DOG HOUSE FAIRING TORN/DAMAGED. REPAIRED TO SRM 51-40-02.

Part: BULKHEAD — DAMAGED (NR 4 PYLON)

NR 4 PYLON INTERNAL AT BULKHEAD LINE PASS THROUGH ELONGATED. REPAIRED PER SRM 54-10-03 AND MM 20-11-05.

Part: RIB — CRACKED (NR 2 ENG COWL)

NR 2 ENGINE INBOARD POWER COWL RIB CRACKED. REPAIRED PER SRM 51-30-02 AND 51-10-01.

Part: ANGLE — CRACKED (NR 1 ENG COWL)

NR 1 ENGINE INBOARD CORE COWL MOST AFT RIB ASSY HAS CRACKED ANGLE. REPAIRED PER SRM 51-10-01 AND 51-30-01.

Part: COWL — LOOSE (NR 2 ENGINE)

NR 2 ENGINE CORE COWL 3RD LATCH AREA HAS LOOSE FASTENERS. REPAIRED PER SRM 51-30-02.

Part: FAIRING — DELAMINATED (NR 3 PYLON)

NR 3 PYLON V FAIRING DELAMINATED. REPAIRED PER SRM 51-30-07.

Part: PANEL — DELAMINATED (LT WING)

LEFT WING UPPER SURFACE PANEL DELAMINATED INBD 2ND FROM ROOT AREA. REPAIRED PER SRM 51-40-15.

Part: COWL — LOOSE (NR 1 ENGINE)

NR 1 ENGINE OUTBOARD CORE COWL TOP AFT CORNER LOOSE FASTENERS. REPAIRED PER SRM 51-30-02.

Part: SKIN — DELAMINATED (AIR COND DOOR)

NR 3 AIR CONDITIONING BAY DOOR DELAMINATED. REPAIRED PER SRM 51-24-11 AND 51-40-15.

Part: FAIRING — DELAMINATED (AIR COND DOOR)

NR 3 PACK EXIT DOOR FAIRING PANEL DELAMINATED. REPAIRED PER SRM 51-40-15.

Part: COWL — DAMAGE (NR 2 ENGINE)

NR 2 ENGINE INBOARD POWER COWL LOWER CORNER SKIN DAMAGED. REPAIRED PER SRM 54-30-03 AND 51-10-02.

Part: SKIN — DELAMINATED (LT TE FLAP)

LEFT OUTBOARD TRAILING EDGE AFT FLAP LOWER SURFACE 4 FOOT DELAMINATION. REPAIRED PER SRM 51-40-07.

Part: SKIN — DELAMINATED (NR 4 SPOILER)

NR 4 SPOILER UPPER SURFACE DELAMINATED. REMOVED AND REPLACED SPOILER PANEL PER MM 27-61-02.

Part: FASTENER — MISSING (AIR COND DOOR)

PANEL 191NL MISSING FASTENERS. REPAIRED PER SRM 51-30-02.

Part: PANEL — DELAMINATED (RT WING)

RIGHT WING UPPER SURFACE FIXED TRAILING EDGE PANEL DELAMINATED. REPAIRED PER SRM 51-40-15.

Part: COWL — CHAFED (NR 2 ENGINE)

NR 2 ENGINE INBD CORE COWL PREVIOUS REPAIR CHAFFED THROUGH. REPAIRED PER SRM 54-30-03.

Part: SKIN — DELAMINATED (LT MLG DOOR)

LEFT WING GEAR DOOR CORNER DELAMINATED. REPAIRED PER SRM 51-40-09.

Part: FAIRING — DELAMINATED (NR 4 PYLON)

NR 4 PYLON V FAIRING DELAMINATED. REMOVED AND REPLACED FAIRING SRM 51-10-01 AND 51-30-02.

Part: HINGE — CORROSION (RT MLG DOOR)

RIGHT CENTER GEAR DOOR HINGE LIGHT SURFACE CORROSION. REPAIRED BY SRM 51-10-02 AND 51-10-06.

Part: COWL — CRACKED (NR 1 ENGINE)

NR 1 ENGINE OUTBD CORE COWL MOST AFT LATCH HOUSING CRACKED AND DAMAGED. REPAIRED PER SRM 51-30-02.

Part: STINGER — LOOSE (NR 1 ENGINE)

NR 1 ENGINE STINGER ASSY LOOSE AND MISSING FASTENERS. REPAIRED PER SRM 51-30-02.

Part: SKIN — DELAMINATED (RT MLG DOOR)

RIGHT WING GEAR DOOR 5 INCH DELAMINATED. REPAIRED PER SRM 51-40-09.

Part: PANEL — DELAMINATED (RT WING)

RIGHT WING UPPER SURFACE TRAILING EDGE PANEL DELAMINATED. REPAIRED PER SRM 51-40-15 AND 51-24-11.

Part: EXHAUST SLEEVE — LOOSE (NR 3 ENGINE)

NR 3 ENGINE EXHAUST SLEEVE A 1 O'CLOCK POSITION LOOSE FASTENERS. REPAIRED PER SRM 51-30-02.

Part: PANEL — DELAMINATION (LT WING)

LEFT WING UPPER SURFACE FWD INBOARD TRAILING EDGE PANEL DELAMINATED. REPAIRED PER SRM 51-40-09.

Part: BATTERY PACK — DISCHARGED (CABIN)

UPPER DECK EMERGENCY LIGHTS WILL NOT GO OUT WITH POWER OFF POSTION. REMOVED AND REPLACED UPPER DECK EMERGENCY LIGHTING BATTERY PACK PER MM 33-51-00.

Part: PRESS XMTR — INOPERATIVE (NR 4 HYD SYST)

NR 4 HYD PRESS PEGGED AT 4,000 PSI, FOLLOWED BY A LOW QTY ANNUNCIATOR AND DECREASING HYD QTY. HYD TEMP REMAINED NORMAL PRIOR TO AND FOLLOWING ABNORMAL PROCEDURES IN AOM. REPLACED NR 4 HYD PRESS TRANSMITTER IAW MM 29-31-01. OPS AND LEAK CHECK NORMAL. SYSTEM PRESS FOUND NORMAL PER MM 29-11-00.

Part: HINGE — CRACKED (LT MLG DOOR)

LT WING GEAR DOOR HINGE FWD POSITION FAILURE, FOUND AFTER BLOCK-IN. FOUND NO OTHER DAMAGE. REMOVED AND REPLACED FWD HINGE PER MM 32-12-01.

Part: SKIN — CORROSION (LT WING)

LEVEL 1 CORROSION, ON LT WING UPPER SURFACE AFT OF FRONT SPAR. BLENDED AND TREATED PER SRM 51-10-01.

Part: CHANNEL — CRACKED (NR 3 PYLON)

NR 3 PYLON SKIRT BEAM AREA HYD PRESS FILTER MODULE UPPER SUPPORT CHANEL CRACKED. REPLACED CHANNEL PER SRM 51-10-01.

Part: SEAT TRACK — CORRODED (BS 1780)

LEVEL 1 CORROSION ON SEAT TRACK FLANGE AT BS 1780 TO 1800, LBL 75. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01.

Part: RAIL — CRACKED (NR 3 ENGINE)

NR 3 ENG TEC R-RAIL AT 10 O'CLOCK POSITION HAS CRACKED RADIAL LIGHTING HOLE. WELDED AND STRESS RELIEVED PER PWA MM 72-53-01 NR 22.

Part: SEAT TRACK — BROKEN (BS 2099)

SEAT TRACK BROKEN AT BS 2099, LBL 66. REPLACED SEAT TRACK PER BAC SRM 51-10-01.

Part: FRAME — CRACKED (RT HORIZ STAB)

CRACKED INTERNAL FRAMES (2) AT PANEL 341BR ON RIGHT HORIZONTAL STABILIZER. REPAIRED FRAMES PER BAC SRM 55-10-06.

Part: SKIN — CRACKED (LT INBD ELEV)

CRACK ON AFT INBOARD CORNER OF LEFT INBOARD ELEVATOR. FIBERGLASS REPAIR ACCOMPLISHED PER BAC SRM 51-40-15.

Part: STIFFENER — CRACKED (WS 669.5)

RIGHT WING STRINGER 22 WINT STA 669.5 VERTICAL STIFFENER CRACKED AT UPPER NR 1 FASTENER HOLE. REPLACED STIFFENER PER SRM 51-10-01.

Part: BRACE — CRACKED (LT WING)

LEFT WING L/E RIB TO FRONT SPAR LWR CHORD TUBE BRACE FWD END CRACKED. REPLACED BRACE PER MM 20-51-01.

Part: FORGING — CORRODED (BS 1560)

LEVEL 1 CORROSION ON LEFT MAIN DECK WINDOW FRAME FORGING FORWARD EDGE AT BS 1560. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01.

Part: SEAT TRACK — CORRODED (BS 1860)

LEVEL 1 CORROSION ON SEAT TRACK FLANGE AT BS 1860 TO 1880, LBL 96. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01.

Part: SEAT TRACK — CORRODED (BS 1885)

LEVEL 1 CORROSION ON SEAT TRACK FLANGE AT BS 1885, RBL 11. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01.

Part: STRINGER — CORRODED (BS 1617)

LEVEL 1 CORROSION ON STRINGER 22L AT BS 1617. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-02.

Part: FRAME — CRACKED (BS 2685)

APU COMPARTMENT BS 2685 RIGHT WL 306 FRAME CRACKED. STOP DRILLED AND REPAIRED PER SRM 51-10-01 AND 51-40-03 FIG 2.

Part: SKIN — CORRODED (WS 1525-1545)

LEVEL 1 CORROSION RT UPPER WING SURFACE BETWEEN FRONT AND REAR SPAR STRINGER 1 TO 25 WING STA 1525 1545. BLENDED AND TREATED PER SRM 51-10-01.

Part: SKIN — CORRODED (RT WING)

LEVEL 1 CORROSION ON RIGHT WING UPPER SURFACE FORWARD OF INBOARD AILERON. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-02 AND BAC OHM 20-10-03.

Part: SKIN — CORROSION (RT WING)

LEVEL 1 CORROSION, RT WING UPPER SURFACE ALONG MIDSPAR AREA ON SKIN. BLENDED AND TREATED PER BAC SRM 51-10-01.

Part: CHANNEL — CRACKED (NR 3 PYLON)

NR 3 PYLON THROTTLE PUSH PULL CABLE ATTACH CHANNEL ADJACENT TO ANTI-ICE DUCT IS CRACKED. REPAIRED PER SRM 51-40-03 FIG 3.

Part: SPAR WEB — CORROSION (CENTER TANK)

CENTER TANK REAR SPAR WEB FOUND CORROSION AT LT OVERRIDE JETTISON PUMP BONDING JUMPER ATTACH AREA. BLENDED AND TREATED PER SRM 51-10-01.

Part: SKIN — CORROSION (LT WING)

LEVEL 1 CORROSION, LT WING UPPER SURFACE ALONG FRONT SPAR SPOTS OF CORROSION AROUND FASTENER HEADS ALONG FRONT SPAR. BLENDED AND TREATED PER SRM 51-10-01.

Part: LADDER — CRACKED (COCKPIT)

MAIN DECK TO UPPER DECK CREW LADDER BOTTOM STEP CRACKED BOTH SIDES, NR 3 STEP CRACKED RT SIDE, NR 4 STEP CRACKED LT SIDE. REPAIRED LADDER STEPS PER SRM 51-40-02 FIG 1.

Part: STIFFENER — CRACKED (BS 42)

UPPER DECK FLOORBEAM STIFFENER CRACKED AT RBS 440, RBL 42. REPAIRED STIFFENER PER BAC SRM 51-10-01.

Part: FRAME — CRACKED (BS 2060)

FRAME AT BS 2060 STRINGER 15 FOUND CRACKED. REPAIRED PER REPAIR SCHEME 53-60-33628.

Part: SEAT TRACK — CORRODED (BS 1920)

LEVEL 1 CORROSION ON SEAT TRACK AT BS 1920 TO 2040, LBL 11. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01.

Part: SKIN — CORROSION (LT WING)

LEVEL 1 CORROSION, LT WING UPPER SURFACE AT REAR SPAR. BLENDED AND TREATED PER SRM 51-10-01.

Part: GATE — CRACKED (L1 DOOR)

L1 DOOR UPPER GATE CRACKED AT AREA 2 LOCATION. REPLACED GATE PER MM 51-11-01.

Part: SEAT TRACK — CRACKED (BS 700)

SEAT TRACK CRACKED AT BS 700, LBL 29. REPAIRED SEAT TRACK PER BAC SRM 53-10-05.

Part: RAIL — CRACK (NR 3 ENGINE)

NR 3 ENG TEC S-RAIL AT 1:30 POSITION HAS A RACE TRACK SLOT O/D CRACK. WELDED AND RELIEVED PER PWA MM 72-53-01 NR 22.

Part: FRAME — CRACKED (R 2 DOOR)

R2 DOOR AFT UPPER CORNER OF FRAME IS CRACKED. REPAIRED FRAME PER SRM 52-10-02 FIG 10.

Part: RIB — CRACKED (NR 2 MAIN TANK)

NR 2 MAIN TANK LOWER REP STIFFENER CRACKED RIB. ALSO, WEB UNDER STIFFENER CRACKED. REPLACED STIFFENER AND REPAIRED WEB PER SRM 51-10-01 AND 57-10-05 FIG 2.

Part: CHANNEL — CRACKED (NR 16 LE FLAP)

RT WING NR 16 L/E FLAP PANEL UPPER O/B HINGE ATTACH CHANEL CRACKED. REPAIRED CHANEL PER SRM 51-10-01 PG 18.

Part: WEB — CRACKED (INBD AILERON)

CRACKED INBOARD AILERON OUTBOARD WEB. REPAIRED PER BAC SRM 51-40-02.

Part: RIB — CRACKED (NR 14 LE FLAP)

NR 14 L/E FLAP PANEL I/B WEB LOWER RADIUS CRACKED. REPLACED FLAP SUPPORT RIB PER SRM 51-10-01.

Part: SKIN — CRACKED (L1 DOOR)

L1 DOOR LOWER HINGE CUTOUT CRACKED ADJACENT TO SEAL RETAINER. REPAIRED PER SRM 53-10-02 FIG 12.

Part: REVEAL — CRACKED (L4 DOOR)

L4 DOOR FWD CUTOUT UPPER CORNER REVEAL CRACKED 2 PLACES. REPAIRED PER HAECO REPAIR SCHEME R-53-61-33667.

Part: STIFFENER — CRACKED (RT MLG WW)

RT BLG WHEEL WELL AFT BULKHEAD BS 1480 BULKHEAD STIFFENER ADJACENT TO OLEO STRUT STOWAGE FAIRING IS CRACKED. ALSO, WEB UNDER STIFFENER IS CRACKED. REPLACED STIFFENER AND REPAIRED WEB PER SRM 51-10-01 AND 51-40-02.

Part: TENSION TIE — CRACKED (BS 920)

CRACKED TENSION TIE AT BS 920, S 8 AND 9. REPAIRED TENSION PER SB 747 53-2371.

Part: SEAT TRACK — CRACKED (BS 517)

SEAT TRACK FLANGE CRACKED AT BS 517 TO 523, LBL 33. REPLACED SEAT TRACK PER BAC SRM 51-10-01.

Part: TRUNNION — CORROSION (RT MLG)

LEVEL 1 CORROSION, FOUND ON RT I/B BODY GEAR TRUNNION AND TRUNNION CAP. TRUNNION BORE MACHINED NDT OK AND BUSHING CUT PER BOEING SRM 53-10-08 ITEM 1-24.

Part: SKIN — CORROSION (RT WING)

LEVEL 1 CORROSION, RT WING UPPER SURFACE ALONG FRONT SPAR. BLENDED AND TREATED PER BAC SRM 51-10-01.

Part: STRINGER — CRACKED (BS 1575)

STRINGER 16R END CRACKED AT BS 1575. REPAIRED STRINGER PER BAC SRM 53-10-03.

Part: ATTACH PLATES — CRACKED (RT HORIZ STAB)

CRACKED INTERNAL ATTACH PLATES AND FRAMES (12) AT PANEL 341BR ON RIGHT HORIZONTAL STABILIZER. REPAIRED PARTS PER BAC SRM 55-10-06.

Part: SEAT TRACK — CORRODED (BS 1500)

LEVEL 1 CORROSION ON SEAT TRACK CROWN FLANGE AT BS 1500 TO 1520, LBL 11. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01.

Part: SKIN — CHAFED (NR 4 PYLON)

NR 4 PYLON HAS DEEP CHAFE MARKS AT UPPER EXTERNAL SKIN CROWN AREA. REPAIRED PER REPAIR SCOPE (HAECO) BLENDED O/B DEEP NDT NO CRACKS, INSTALLED REPAIR PER RS 54-51-33635.

Part: FRAME — CRACKED (BS 2674)

APU COMPT LEFT BS 2674 WL 310 FRAME CRACKED AND DAMAGED. STOP DRILLED AND REPAIRED AREA CRACKED PER SRM 51-10-01 AND 51-40-03 FIG 2.

Part: SEAT TRACK — CRACKED (BS 5601)

SEAT TRACK CRACKED AT BS 560, LBL 11. REPLACED SEAT TRACK PER BAC SRM 51-10-01.

Part: TRUNNION — CORROSION (LT MLG)

LEVEL 1 CORROSION, FOUND LT I/B BODY GEAR TRUNNION AND TRUNNION CAP. TRUNNION BORE MACHINED NDT OK BUSHING CUT TRUNNION CAP. REPLACED PER BOEING SRM 53-10-08 ITEM 1-24.

Part: TIE CLIP — CRACKED (BS 2180)

STRINGER TIE CLIP AT BS 2180 STRINGER 12 FOUND CRACKED. REPLACED CLIP PER SRM 51-10-01.

Part: STRINGER — CORRODED (BS 1605)

LEVEL 1 CORROSION AT FUSELAGE LEFT STRINGER 20 AT BS 1605. BLENDED AND TREATED PER SRM 51-10-01.

Part: TIE BRACKET — CRACKED (BS 2220)

CRACKED STRINGER 21R FRAME TIE BRACKET AT BS 2220. REPLACED BRACKET PER BAC SRM 51-10-01.

Part: SKIN — CORRODED (LT WING)

LEVEL 1 CORROSION ON LT WING LOWER SURFACE SKIN 70 INCHES AFT OF FRONT SPAR BEHIND NR 1 PYLON. REMOVED HI-LOKS BLENDED SHOT PEENED AND TREATED AND INSTALLED HI-LOKS PER SRM 51-10-02 AND 51-10-01 AND OHM 20-10-03.

Part: WEB — CRACKED (NR 16 LE FLAP)

NR 16 L/E FLAP O/B WEB UPPER RADIUS IS CRACKED. STOP DRILLED AND REPAIRED O/B SUPPORT PER SRM 51-40-03.

Part: SEAT TRACK — CORRODED (BS 480)

LEVEL 1 CORROSION ON SEAT TRACK FLANGE AT BS 480, RBL 43. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01.

Part: WEB — CRACKED (MAIN DECK)

MAIN DECK RT O/B FLOOR SUPPROT HORIZONTAL WEB FOUND CRACKED. REPAIRED PER SRM 51-40-02 FIG 1.

Part: FRAME — CRACKED (LT HORIZ STAB)

CRACKED INTERNAL FRAMES AND ATTACH PLATES (6) AT PANEL 341CL ON LEFT HORIZONTAL STABILIZER. REPAIRED FRAMES AND PLATES PER BAC SRM 55-10-06.

Part: ANGLE — CORRODED (BS 1582)

CORROSION ON FLOOR SUPPORT ANGLE AT BS 1582, RBL 116. REPLACED SUPPORT ANGLE PER BAC SRM 51-40-04.

Part: SEAT TRACK — CORROSION (BS 1920-2040)

LEVEL 2 CORROSION, ON MAIN DECK SEAT TRACK FLANGE BS 1920-2040. REPLACED TRACK PER SRM 53-10-01.

Part: CHANNEL — CRACKED (NR 4 PYLON)

NR 4 PYLON SKIRT BEAM AREA HYD PRESS FILTER SUPPORT CHANNELS CRACKED. REPLACED CHANNELS PER SRM 51-10-01.

Part: PANEL — DELAMINATED (LT TE AFT FLAP)

LT I/B AFT FLAP LOWER CENTER STRESS PANEL DELAMINATED AT CENTER AREA. REPLACED STRESS PANEL PER SRM 51-10-01.

Part: PANEL — CRACKED (NR 3 SPOILER)

NR 3 SPOILER PANEL AT ROD END ATTACH FITTING FILLET AREA IS CRACKED. REPLACED SPOILER PANEL PER MM 27-61-02.

Part: SEAT TRACK — CORRODED (BS 1820)

LEVEL 1 CORROSION ON SEAT TRACK FLANGE AT BS 1820 TO 1840, LBL 11. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01.

Part: TIE CLIP — CRACKED (BS 1335)

CRACKED STRINGER 15R TIE CLIP AT BS 1335. REPLACED STRINGER TIE CLIP PER BAC SRM 51-10-01.

Part: SEAT TRACK — CORRODED (BS 2135)

LEVEL 1 CORROSION ON SEAT TRACK LOWER SURFACE AT BS 2135, LBL 11. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01.

Part: SKIN — CORRODED (RT WING)

LEVEL 1 CORROSION ON RT WING UPPER SURFACE BETWEEN MID AND REAR SPARS WS 550, 915, 1215, 1470. BLENDED AND TREATED PER SRM 51-10-01.

Part: SKIN — CORROSION (RT WING)

LEVEL 1 CORROSION, FOUND ON RT WING UPPER SURFACE REAR SPAR AREA. BLENDED AND SHOT PEENED AND TREATED PER SRM 51-10-01.

Part: SEAT TRACK — CORRODED (BS 560)

LEVEL 1 CORROSION ON SEAT TRACK AT BS 560 TO 580, RBL 8. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01.

Part: RETAINER — CRACKED (L1 DOOR)

R1 DOOR LOWER HINGE CUTOUT AREA ADJACENT TO PRES SEAL RETAINER IS CRACKED. REPAIRED PER SRM 51-10-02 FIG 12.

Part: SPLICE — CORROSION (HORIZ STAB)

LEVEL 1 CORROSION FOUND ON LWR AFT SPLICE PLATES LT AND RT HOLE SPLICE PLATE. FOUND 2 EA LOOSE BOLTS. AFTER REMOVAL OF BOLTS FOUND CRACK IN SPLICE PLATE. REMOVED AND TREATED CORROSION DRILLED OVERSIZED BORE ON HOLE WITH CRACK, NDT, SHOT PEENED AND REINSTALLED FASTENERS SRM 51-10-01 BOEING TELEX PAO HKG 98-0058RE.

Part: STRINGER — CRACKED (BS 2184)

STRINGER 14L END CRACKED AT BS 2184. REPLACED STRINGER PER BAC SRM 51-40-01.

Part: SEAT TRACK — CORRODED (BS 2250)

LEVEL 1 CORROSION ON SEAT TRACK FLANGE AT BS 2250 TO 2260, LBL 11. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01.

Part: SKIN — CORRODED (BS 1741)

LEVEL 1 CORROSION FOUND ON SKIN LAP AT FUSELAGE RIGHT BS 1741 TO 2100 STRINGER 12. BLENDED AND TREATED PER SRM 51-10-01.

Part: FRAME — CRACKED (BS 1920)

CRACKED SIDEWALL FRAME AT BS 1920, S 13R. REPAIRED FRAME PER BAC SRM 53-10-04.

Part: DOUBLER — CRACKED (NR 8 SPOILER)

NR 8 SPOILER ROD END FITTING DOUBLER CRACKED AT FASTENER HOLES. REPLACED NR 8 SPOILER PER MM 27-61-01.

Part: BRACKET — CRACKED (NR 14 LE FLAP)

NR 14 LE FLAP BULNOSE FAIRING MOST I/B AND MOST O/B ATTACH ARM TO FLAP PANEL BRACKETS ARE CRACKED. REPLACED BRACKETS PER SRM 51-10-01.

Part: PANEL — CRACKED (NR 10 SPOILER)

NR 10 SPOILER PANEL AT ROD END FITTING FILLET AREA CRACKED. REPLACED SPOILER PANEL PER SRM 27-61-02.

Part: BRACKET — CRACKED (BS 2674)

APU COMPT BS 2674 LEFT WL 310 INTER FRAME SUPPORT BRACKET CRACKED. REPLACED BRACKET PER SRM 51-10-01.

Part: FRAME — CRACKED (BS 2040)

FRAME I/B FLANGE CRACKED AT FUSELAGE RIGHT BS 2040 STRINGER 15. REPAIRED PER REPAIR SCHEME 53-60-33627 AND BOEING TELEX.

Part: BRACKET — CRACKED (NR 13 LE FLAP)

NR 13 L/E FLAP BULLNOSE MOST I/B ATTACH ARM BRACKET ON FLAP PANEL IS CRACKED. REPLACED BRACKET PER SRM 51-10-01.

Part: CHANNEL — CRACKED (LT MLG DOOR)

LT BLG O/B STRUT DOOR CRACKED UNDER FWD STOP FITTING. CRACKED CHANNEL REPLACED PER SRM 51-10-01.

Part: SEAT TRACK — CORRODED (BS 1900)

LEVEL 1 CORROSION IN SEAT TRACK FLANGE AT BS 1900 TO 1905, LBL 11. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01.

Part: SEAT TRACK — CORROSION (MAIN DECK)

LEVEL 1 CORROSION, FOUND ON MAIN DECK SEAT TRACK AT BS 1900 BL 11. BLENDED AND TREATED PER BOEING SRM 53-10-01.

Part: RAIL — CRACKED (NR 3 ENGINE)

NR 3 ENG TEC S-RAIL AT 11:45 POSITION HAS A CLEVIS PIN HOLE CRACK. REMOVED ENG MOUNT, WELDED AND RELIEVED AND REINSTALLED MOUNT PER PWA MM 72-53-01 NR 22.

Part: LONGERON — CORRODED (BS 1582)

LEVEL 1 CORROSION ON LONGERON AT LEFT BS 1583. REMOVED CORROSION AND TREATED PER BAC SRM 53-10-01.

Part: SKIN — CORROSION (WS 540-830)

LEVEL 1 CORROSION RIGHT WING UPPER SURFACE BETWEEN FRONT AND MID SPARS STR 14 TO 30 WING STA 540 TO 830. BLENDED AND TREATED PER SRM 51-10-01.

Part: TIE CLIP — CRACKED (BS 2220)

STRINGER TIE CLIP CRACKED AT FUSELAGE BS 2220 STRINGER 22L. REPLACED CLIP PER SRM 51-10-01.

Part: BRACKET — CRACKED (NR 15 LE FLAP)

NR 15 L/E FLAP BULLNOSE ATTACH ARM BRACKET MOST I/B IS CRACKED. REPLACED ARM BRACKET PER SRM 51-10-01.

Part: SKIN — CORRODED (BS 720-740)

LEVEL 1 CORROSION ON FUSELAGE SKIN AT BS 720 TO 740, STR 0. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01.

Part: SEAT TRACK — CORRODED (BS 1760)

LEVEL 1 CORROSION ON SEAT TRACK CROWN FLANGE AT BS 1760 TO 1880, LBL 76. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01.

Part: FLOORBEAM — CORRODED (BS 1780)

LEVEL 1 CORROSION ON MAIN DECK FLOORBEAM UPPER CHORD SURFACE AT BS 1780, LBL 10 TO RBL 10. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01.

Part: SEAT TRACK — CORRODED (BS 1900)

LEVEL 1 CORROSION ON SEAT TRACK FLANGE AT BS 1900 TO 1920, LBL 33. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01.

Part: SEAT TRACK — CORRODED (BS 1875)

LEVEL 1 CORROSION ON SEAT TRACK FLANGE AT BS 1875 TO 1880, LBL 11. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01.

Part: SKIN — CORROSION (LT WING)

LEVEL 1 CORROSION ON LT WING UPPER SURFACE ALONG FRONT SPAR SKIN AT FASTENER HEADS. BLENDED AND TREATED PER SRM 51-10-01.

Part: SKIN — CRACKED (RT WING)

CRACKED AND CHAFED RIGHT WING LOWER LEADING EDGE SKIN. REPAIRED PER BAC SRM 57-30-04.

Part: SUPPORT — CRACKED (BS 960)

FUSELAGE LEFT BS 960 LBL 10 RBL10 FUSE FDW BODY FAIRING SUPPORT FRAME FOUND CRACKED AND CORRODED. REPAIRED FRAME PER SRM 53-50-04 FIG 2.

Part: RAIL — CRACKED (NR 3 ENGINE)

NR 3 ENG TEC S-RAIL AT 1:30 AND 10 O'CLOCK POSITION HAS 2 EA RACETRACK SLOT O/D CRACKS. WELDED AND RELIEVED PER PWA MM 72-53-01 NR 22.

Part: WEB — CRACKED (NR 13 LE FLAP)

NR 13 L/E FLAP PANEL I/B WEB UPPER RADIUS CRACKED. REPAIRED PER SRM 51-40-03 FIG 3.

Part: BRACKET — CRACKED (BS 1840)

FUSELAGE BS 1840 TO 1860 BL 30 PDU SUPPORT ATTACH BRACKET CRACKED. REPAIRED BRACKET PER SRM 51-10-01.

Part: FORGING — CORRODED (BS 1620)

LEVEL 1 CORROSION ON LEFT MAIN DECK WINDOW FRAME FORGING FORWARD EDGE AT BS 1620. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01.

Part: SUPPORT — CRACKED (BS 1620)

FUSELAGE BS 1620 BL 50 TO 57 RIGHT BODY FAIRING SUPPORT FRAME CRACKED. FRAME REPAIRED PER SRM 53-50-04 FIG 2.

Part: TIE — CRACKED (BS 1080)

CRACKED FRAME TIE AT BS 1080, S 3R TO 4R. REPLACED FRAME TIE PER BAC SRM 51-10-01.

Part: FRAME — CRACKED (BS 2080)

FRAME AT BS 2080 STR 25 FOUND CRACKED. REPAIRED PER REPAIR SCHEME 53-60-33629.

Part: ANGLE — CRACKED (RT WING)

RT WING T/E ACCESS PANEL 672 EB INBOARD SUPPORT FRAME AFT MOUNTING ANGLE CRACKED. SUPPORT ANGLE REPAIRED PER SRM 51-10-01.

Part: SEAT TRACK — CORRODED (BS 1800)

LEVEL 1 CORROSION ON SEAT TRACK FLANGE AT BS 1800 TO 1810, LBL 11. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01.

Part: FORGING — CORRODED (FUSELAGE)

LEVEL 1 CORROSION FOUND ON FUSELAGE WINDOW FORGING. CORROSION BLENDED AND TREATED. REMAINING THICKNESS .081 INCHES DEEP PER SRM 51-10-01.

Part: SKIN — CORROSION (LT WING)

LEVEL 1 CORROSION, FOUND LT WING LOWER SKIN 62 INCHES AFT OF FRONT SPAR. BLENDED AND TREATED PER BOEING SRM 51-10-01.

Part: SEAT TRACK — CORRODED (BS 1515)

LEVEL 1 CORROSION ON SEAT TRACK FLANGE AT BS 1515, LBL 11. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01.

Part: FLOORBEAM — CORRODED (BS 1580)

LEVEL 1 CORROSION ON MAIN DECK FLOORBEAM TOP CHORD AT BS 1580, RBL 8 TO RBL 11. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01.

Part: SEAT TRACK — CORRODED (BS 1910)

LEVEL 1 CORROSION ON SEAT TRACK FLANGE AT BS 1910, LBL 11. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01.

Part: SEAT TRACK — CRACKED (BS 5131)

SEAT TRACK CRACKED AT BS 513 TO 516, LBL 11. REPLACED SEAT TRACK PER BAC SRM 51-10-01.

Part: BULKHEAD — CRACKED (NR 2 PYLON)

NR 2 PYLON BULKHEAD RT TOP CORNER FILLET PLATE FASTENER HOLES 2 EA CRACKED. DOUBLER REPAIRED PER REPAIR SCHEME 54-51-33638 AND SB.

Part: RAIL — CRACKED (NR 4 ENGINE)

NR 4 ENG TEC R-RAIL AT 11 O'CLOCK POSITION PREVIOUS WELD AT LIGHTING HOLE SLOT INNER RADIUS CRACKED. WELDED AND NORMALIZED PER PWA MM 72-53-01 NR 22.

Part: CHORD — CRACKED (LT WING)

LT WING LOWER CHORD FASTENER HOLE CRACK ON WEB AT 4 O'CLOCK POSITION. REPAIRED HOLE TO OVERSIZED TO .562 NDT NO CRACK FOUND PER HAECO RS 57-21-33654.

Part: FRAME — CRACKED (BS 880)

FRAME CRACKED AT STRINGER CUTOUT DOUBLER. REPAIRED PER REPAIR SCHEME RS 53-22-33668 REF BOEING TELEX NR PAO HKG 98-0036RE.

Part: FRAME — CRACKED (BS 1760)

FRAME I/B FLANGE CRACKED AT FUSELAGE RIGHT BS 1760 STRINGER 15. REPAIRED PER REPAIR SCHEME 53-60-33626 AND BOEING TELEX.

Part: SKIN — CORRODED (BS 2000-2120)

LEVEL 1 CORROSION FOUND ON LAP SEAM FUSELAGE LEFT AT BS 2000 TO 2120. BLENDED AND TREATED PER SRM 51-10-01.

Part: SEAT TRACK — CORRODED (BS 1657)

LEVEL 1 CORROSION ON SEAT TRACK FLANGE AT BS 1657 TO 1660, RBL 95. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01.

Part: SHEAR TIE — CRACKED (BS 880)

FRAME SHEAR TIE CRACKED AT BS 880 LEFT STRINGERS 10 TO 11. REPAIRED PER REPAIR SCHEME 53-22-33669 AND BOEING TELEX.

Part: WEB — CRACKED (NR 16 LE FLAP)

NR 16 L/E FLAP O/B WEB UPPER RADIUS CRACKED. STOP DRILLED AND REPAIRED PER SRM 51-40-03 FIG 1.

Part: CHANNEL — CRACKED (LT MLG DOOR)

FWD HINGE SUPPORT CHANEL CRACKED LT BODY O/B STRUT DOOR. SUPPORT CHANEL REPAIRED PER SRM 51-40-03 FIG 4.

Part: LINK — CRACKED (NR 6 TE FLAP)

NR 6 CANOE FAIRING PIVOTING LINK I/B SURFACE LWR SECTION IS CRACKED. REPLACED LINK ASSY PER MM 27-51-26.

Part: SKIN — CORROSION (LT WING)

LEVEL 1 CORROSION, ON LT WING UPPER SURFACE BETWEEN FRONT AND MIDSPAR. BLENDED AND TREATED PER BAC 51-10-01.

Part: FORGING — CORROSION (BS 1600-1620)

LEVEL 1 CORROSION, FOUND ON WINDOW FORGING FWD EDGE BS 1600-1620. BLENDED AND TREATED PER BOEING TELEX PAO-HKG-98-0042RE 23/01/98.

Part: FORGING — CORROSION (WINDOW BS 1580)

LEVEL 1 CORROSION, FOUND ON WINDOW FORGING FWD EDGE BS 1580-1600. BLENDED AND TREATED PER BOEING TELEX PAO-HKG-98-0042RE 23/1/98.

Part: SKIN — CORROSION (LT WING)

LEVEL 1 CORROSION, FOUND LOWER SKIN 38 INCHES AFT OF FRONT SPAR STRINGER 10. BLENDED AND TREATED PER BOEING SRM 57-30-01.

Part: STRINGER — CRACKED (BS 740)

STRINGER 23 AT BS 740 CRACKED. REPLACED STRINGER PER SRM 51-10-01.

Part: COWL — DAMAGED (NR 4 ENGINE)

DAMAGE TO NR 4 ENGINE NOSE COWL AT 9 O'CLOCK POSITION. REPAIRED PER SRM 51-70-00.

Part: PLATE — CRACKED (NR 4 PYLON)

2 INCH CRACK ON NR 4PYLON, OUTBD SIDE ABOVE AND FWD OF HALF MOON PLATE. REPAIRED PER MA 5430-06:01.

Part: SHAFT — SHEARED (NLG DOOR)

SHEARED NOSE LANDING GEAR DOOR GROUND OPERATING HANDLE SHAFT. REPLACED SHAFT PER BOEING MAINTENANCE MANUAL 32-34-07 OPERATIONAL CHECK NORMAL.

Part: ENGINE — FLAMED OUT (NR 2)

AFTER TAKEOFF APPROXIMATELY 400 FT AGL, NR 2 ENGINE FLAMED OUT. ENACTED INFLIGHT RESTART PROCEDURES. ENGINE RESTARTED NORMALLY AND RETURNED TO BFM AND LANDED UNEVENTFULLY. CHECKED PT3 AND PS3 WATER TRAPS AND FOUND CLEAN PER M/M 75-31-01 AND CHECKED FUEL CONTROL MAIN FILTER AND FOUND CLEAN, IAW M/M 73-21-01. LEAK CHECKED GOOD, FOUND ENGINE OK FOR CONTINUED SERVICE.

Part: FITTING — CRACKED (LT MLG)

CRACKS AND LEVEL 2 CORROSION ON OUTBOARD END FITTING OF LEFT WING LANDING GEAR SUPPORT BEAM PER ULTRASONIC INSPECTION. REPLACED END FITTING PER BAC MM 57-15-01.

Part: PANEL — DELAMINATED (LT SPOILER)

DELAMINATION ON LEFT WING NR 2 SPOILER. REPLACED SPOILER PANEL PER BAC MM 27-61-02.

Part: FRAME — CRACKED (NR 3 PYLON)

CRACK ON RIGHT SIDE OF NR 3 PYLON INTERIOR FRAME. REPLACED FRAME PER BAC SRM 51-10-01.

Part: SKIN — CRACKED (BS 2460)

CRACK ON SKIN ON RIGHT SECTION 48 AT STA 2460, APPROXIMATELY STRINGER 8. REMOVED DAMAGE, CONFIRMED NO CRACK USING HIGH FREQUENCY EDDY CURRENT PER BAC SRM 51-00-02, FABRICATED REPLACEMENT AND INSTALLED PER BAC SRM 53-30-03, 51-30-02 AND 51-24-11.

Part: PANEL — DELAMINATED (NR 3 PYLON)

DELAMINATION ON PANEL NR 474AR ON NR 3 PYLON. REPAIRED DELAMINATION PER BAC SRM 51-40-06.

Part: FLANGE — CRACKED (NR 1 ENGINE)

CRACK ON NR 1 ENGINE TURBINE EXHAUST CASE S-FLANGE AT 1:30 O'CLOCK. WELD REPAIR AND STRESS RELIEF PER PWA MM 72-53-01.

Part: EXHAUST CONE — CRACKED (NR 2 ENGINE)

CRACKED NR 2 ENGINE EXHAUST PLUG END CAP. WELD REPAIRED PER BAC MM 78-11-04 AND INSPECTED PER BAC SOPM 20-20-02.

Part: PANEL — DELAMINATED (NR 4 PYLON)

DELAMINATION ON PANEL NR 484AR ON NR 4 PYLON. REPAIRED DELAMINATION PER BAC SRM 51-40-06.

Part: FLANGE — CRACKED (NR 4 ENGINE)

CRACK ON NR 4 ENGINE TURBINE EXHAUST CASE FLANGE (RAIL) AT 7 O'CLOCK. WELD REPAIR AND STRESS RELIEF PER PWA MM 72-53-01.

Part: FUSE PIN — CORRODED (NR 4 PYLON)

LEVEL 2 CORROSION ON NR 4 PYLON OUTBOARD FUSE PIN INSERT. REPLACED FUSE PIN PER BAC MM 54-10-03.

Part: PANEL — CRACKED (NR 2 PYLON)

CRACK ON PANEL NR 462EL ON NR 2 PYLON. FABRICATED AND INSTALL REPLACEMENT PANEL PER BAC SRM 51-30-02.

Part: PANEL — DELAMINATION (NR 2 PYLON)

DELAMINATION OF INNER SKIN ON ACCESS PANEL NR 462AL ON NR 2 PYLON. REPLACED INNER SKIN AND PANEL CORE PER BAC SRM 51-40-06.

Part: FLANGE — CRACKED (NR 2 ENGINE)

CRACK ON NR 2 ENGINE TURBINE EXHAUST CASE R-FLANGE AT 2 O'CLOCK. WELD REPAIR AND STRESS RELIEF PER PWA MM 72-53-01.

Part: FLANGE — CRACKED (NR 2 ENGINE)

CRACK ON NR 2 ENGINE TURBINE EXHAUST CASE R-FLANGE AT 6:30 O'CLOCK. WELD REPAIR AND STRESS RELIEF PER PWA MM 72-53-01.

Part: PANEL — PUNCTURED (NR 3 PYLON)

TWO PUNCTURES ON NR 3 PYLON PANEL NR 474AR. POTTED CORE AND APPLIED DOUBLER PER BAC SRM 51-40-06.

Part: SUPPORT — CRACKED (BS 1780-1810)

CRACKED RIGHT SIDEWALL SUPPORT AT STATION 1780 TO 1810 IN LOWER AFT CARGO COMPARTMENT. FABRICATED AND INSTALLED NEW SUPPORT PER BAC SRM 51-30-02.

Part: PANEL — DELAMINATED (LT WING)

DELAMINATED UPPER TRAILING EDGE PANEL ON LEFT WING INBOARD. REPAIRED WITH FIBERGLASS FILLERS AND OVERLAYS PER BAC SRM 51-40-09, SEALED AND APPLIED CONDUCTIVE COATING PER BAC SRM 51-40-11.

Part: FLANGE — CRACKED (NR 2 ENGINE)

CRACK ON NR 2 ENGINE TURBINE EXHAUST CASE S-FLANGE AT 2 O'CLOCK. WELD REPAIR AND STRESS RELIEF PER PWA MM 72-53-01.

Part: SKIN — CRACKED (RT TE FOREFLAP)

CRACKED RIGHT OUTBOARD FOREFLAP LEADING EDGE. REPAIRED USING FIBERGLASS FILLERS AND OVERLAYS PER BAC SRM 51-40-09.

Part: PANEL — DELAMINATED (NR 2 PYLON)

DELAMINATED PANEL NR 464AR ON NR 2 PYLON. POTTED AND SEALED DAMAGED AREA PER BAC SRM 51-40-06.

Part: FAIRING — GOUGED (NR 8 FLAP TRACK)

GOUGED NR 8 FLAP TRACK FAIRING (CANOE) ON RIGHT WING. REPAIRED USING FIBERGLASS OVERLAYS PER BAC SRM 51-40-09.

Part: CLIP — CRACKED (NR 2 PYLON)

CRACKED ATTACH CLIP FORWARD OF DIAGONAL LINK ON NR 2 PYLON. REPLACED DAMAGED ATTACH CLIP PER BAC SRM 51-10-01.

Part: SKIN — CHAFED (LT TE FORE FLAP)

CHAFING THROUGH LEADING EDGE OF LEFT OUTBOARD FORE FLAP. FIBERGLASS REPAIR MADE PER BAC SRM 51-40-06.

Part: SKIN — DELAMINATED (LT HORIZ STAB)

DELAMINATION ON THE LEFT HORIZONTAL STABILIZER TRAILING EDGE ADJACENT TO THE NAVIGATION LIGHT. REMOVED DELAMINATION, POTTED CORE AND INSTALLED AND BONDED FIBERGLASS OVERLAYS PER BAC SRM 51-40-14.

Part: ACCESS PANEL — CRACKED (LT WING)

CRACKS AROUND TWO FASTENER HOLES ON AILERON POWER PACKAGE ACCESS PANEL ON LEFT WING. REPAIRED PANEL PER BAC SRM 51-10-02.

Part: PANEL — PUNCTURED (NR 4 PYLON)

PUNCTURE ON PANEL NR 484 ON NR 4 PYLON. REPAIRED PUNCTURE PER BAC SRM 51-40-06.

Part: SKIN — CORROSION (RT WING)

LEVEL 1 CORROSION ON RIGHT WING UPPER SKIN AT FRONT SPAR APPROXIMATELY 9 FEET INBOARD OF WING TIP. BLENDED OUT CORROSION PER BAC SRM 57-30-01, MATERIAL REMOVED WITHIN SRM LIMITS.

Part: PANEL — PUNCTURED (NR 3 PYLON)

PUNCTURE ON PANEL NR 474AL ON NR 3 PYLON. POTTED CORE AND APPLIED A DOUBLER PER BAC SRM 51-40-06.

Part: FRAME — CRACKED (NR 3 PYLON)

CRACK ON LEFT SIDE OF NR 3 PYLON INTERIOR FRAME. REPLACED FRAME PER BAC SRM 51-10-01.

Part: FLANGE — CRACKED (NR 1 ENGINE)

CRACK ON NR 1 ENGINE TURBINE EXHAUST CASE R-FLANGE AT 6:00 O'CLOCK. WELD REPAIR AND STRESS RELIEF PER PWA MM 72-53-01.

Part: PANEL — DELAMINATED (RT WING)

DELAMINATION ON RIGHT WING LEADING EDGE PANEL BETWEEN ENGINES 3 AND 4. REMOVED DAMAGE AND REPAIRED WITH FIBERGLASS OVERLAYS PER BAC SRM 51-40-09.

Part: EXHAUST NOZZLE — TORN (NR 3 ENGINE)

NR 3 ENGINE LEFT UPPER EXHAUST NOZZLE OUTER SKIN HAS AN AREA APPROXIMATELY 6 BY 12 MISSING, RIVETS PULLED THROUGH SKIN AND SKIN TORN. REPAIRED PER BOEING SRM 54-30-03 FIG 11.

Part: OIL CAP — COCKED (NR 1 ENGINE)

OIL LOSS CAUSED NUMBER 1 ENGINE SHUT DOWN 2 HOURS 20 MINUTES AFTER TAKEOFF WHEN PILOTS CAUTION PANEL OIL PRESSURE WARNING LIGHT ILLUMINATED AND INDICATED PRESSURE FLUCUATING BETWEEN 30 AND 35 PSI. FOUND OIL LOSS DUE TO TANK FILLER CAP COCKED ON FILLER NECK AND NOT SEALING. PERFORMED ENGINE INSPECTION PER BAC MM 72-00-00, RESERVICED ENGINE OIL SYSTEM PER BAC MM 12-13-03, REPLACED O-RING ON FILLER CAP PER BAC MM 79-11-04, REINSTALLED CAP AND PERFORMED LEAK CHECK.

Part: TREAD — LOST (NR 11 TIRE)

AFTER TAKEOFF, RIGHT BODY GEAR DOOR OPEN LIGHT ON IN PRIMARY AND ALTERNATE. RETURNED TO HKG. FOUND NR 11 TIRE TREAD PEELED OFF, THE RIGHT BODY GEAR DOOR RELEASE HANDLE LOWER CABLE BROKEN, OUTBOARD TRAILING EDGE FLAP TORQUE TUBE BENT AND BS 1540 RIB LOWER AREA CRACKED. REPAIRED CRACKED RIB PER BOEING SRM 51-40-09, REPLACED DAMAGE SHAFT PER M/M 27-51-04. REPLACED TIRE PER BOEING M/M 32-45-01.

Part: COWL — DELAMINATED (NR 3 ENGINE)

NR 3 ENGINE OUTBOARD FAN COWL INSIDE HAS DELAMINATED AREA. REMOVED DAMAGE AND BONDED NEW CORE AND METAL REPAIR PER BOEING SRM 51-40-06.

Part: ACCESS PANEL — DELAMINATED (VERT STAB)

DELAMINATED ACCESS PANEL ON VERTICAL STABILIZER LOWER. REPAIRED PER BOEING SRM 51-40-06.

Part: COWL — DELAMINATED (NR 4 ENGINE)

NR 4 ENGINE OUTBOARD FAN COWL HAS 2 DELAMINATE AREAS. REPAIRED PER BOEING SRM 51-40-06.

Part: DOUBLER — CORRODED (LT MLG WW)

LEVEL 2 CORROSION ON REPAIR DOUBLER LEFT WHEEL WELL FORWARD VERTICAL SUPPORT. REMOVED AND FABRICATED NEW SUPPORT ANGLE IAW BOEING SRM 51-30-02.

Part: SKIN — CORRODED (BS 436)

LEVEL 2, LWR FX SKIN BULGED APPROX STA 436 BL R-4 FASTENER MISSING HEADS. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER AND FILLER IAW BOEING SRM 51-30-3 AND 51-30-02 AND TREATED AREA IAW 51-10-6.

Part: PANEL — DELAMINATED (RT WING LE)

PANEL DELAMINATED RHW LEADING EDGE TOP I/B OF NR 3 PYLON. REPAIRED AREA WITH FIBERGLASS FILLERS AND OVERLAYS, BONDED PER BOEING SRM 51-40-9.

Part: COWL — DELAMINATED (NR 3 ENGINE)

NR 3 ENGINE INBOARD FAN COWL INSIDE SURFACE HAS DELAMINATED AREA. FABRICATED DOUBLER AND REPAIRED IAW BOEING SRM 51-40-06.

Part: FLANGE — CRACKED (NR 4 PYLON)

NR 4 PYLON I/B SIDE AFT LWR ACCESS DOOR FLANGE CRACKED. BLENDED AREA TO REMOVE CRACK CONDITION IAW BOEING SRM 54-10-03 AND HFEC INSP IAW NDT PT-6 51-00-00 FIG 4.

Part: DOOR — DAMAGED (NR 2 PYLON)

NR 2 PYLON OUTBOARD SAIL PLANE DOOR INSIDE SURFACE HAS PUNCTURE. REMOVED DAMAGED AREA AND HOT BONDED NEW DOUBLER IN PLACE IAW BOEING SRM 51-40-06.

Part: COWL — DELAMINATED (NR 4 ENGINE)

NR 4 ENGINE INBOARD FAN COWL HAS 2 DELAMINATED AREA ON OUTSIDE SKIN. REPAIRED PER BOEING SRM 51-40-06 AND PAINTED IAW BOEING SRM 51-24-11.

Part: PANEL — CRACKED (LT WING)

CRACKED AND DELAMINATED PANEL LEFT WING TRAILING EDGE FORWARD OF INBOARD AILERON ON TOP OF WING. REPAIRED PER 51-40-15 AND 51-24-11.

Part: FAIRING — DELAMINATED (BS 1000)

RIGHT BODY FAIRING AT BS 1000 BY CENTER WING SUMP PLUG PANEL DELAMINATED. REPAIRED PER BOEING SRM 51-40-07.

Part: COWL PANELS — DAMAGED (NR 4 ENGINE)

NR 4 ENGINE NOSE COWL PANELS DAMAGED AT THE 11 TO 1 O'CLOCK POSITION. REPAIRED PANELS PER BOEING SRM 51-40-06.

Part: FRAME — CRACKED (BS 1480)

CRACKED LOWER CHORD BETWEEN NUT PLATES BS 1480 TO LBL 48. REPAIRED PER BOEING SRM 53-50-04.

Part: FRAME — CRACKED (BS 1536)

CRACKED LOWER CHORD BY NUT PLATE NEAR BS 1536 TO LBL 60. REPAIRED PER BOEING SRM 53-50-04.

Part: PRECOOLER — CRACKED (NR 3 ENGINE)

NR 3 PRECOOLER CRACKED. WELDED PER BAC 5975.

Part: PANEL — DELAMINATION (RT WING)

RIGHT WING, DELAMINATED UPPER L/E PANEL AFT NR 18 L/E. REPAIRED PER BOEING SRM 51-40-12.

Part: SKIN — CRACKED (BS 540)

BS 540 STR 9R EXTERIOR SKIN CRACKED AND AREA DISBONDED. REPAIRED PER BOEING SRM 53-30-03.

Part: PANEL — CRACKED (LT HORIZ STAB)

LEFT HORIZONTAL, TRAILING EDGED CRACKED AND NUMEROUS LOOSE FASTENERS BY POSITION LIGHT. REPAIRED PER BOEING SRM 51-40-09 AND 12-09-06.

Part: CASE — CRACKED (ENGINE)

NR 3 ENG 'S' RAIL CRACKED AT 60 DEG POSITION ON TURBINE EXHAUST CASE TEC. REPAIRED WELDED AND STRESS RELIEVED PER MM 72-53-01 CASE CYCLE 6A.

Part: FRAME — CRACKED (BS 880)

BS 880 AT STR 38L FRAME CRACKED FWD CARGO. REPAIRED PER BOEING SRM 53-10-04.

Part: BATTERY PACK — DISCHARGED (CABIN)

CREW SERVICE DOOR EMERGENCY LIGHTS INOPERABLE. REPLACED PER MM 33-51-00.

Part: PANEL — DAMAGED (RT WING)

RT WING L/E PANEL DAMAGED AFT OF NR 18 L/E FLAP. REPAIRED PER BOEING SRM 51-40-06.

Part: FRAME — CRACKED (BS 1820)

BS 1820 FRAME CRACKED AT STR 40L. REPAIRED PER BOEING SRM 53-10-04.

Part: SKIN — DAMAGE (RT TE FLAP)

RT I/B FLAP UPPER STRESS PANEL OF AFT FLAP AT I/B END HAS A TEAR. REPAIRED PER BOEING SRM 51-40-06.

Part: RIVETS — LOOSE (EXHAUST SLEEVE)

LOOSE RIVETS NR 1 ENG LT SIDE EXHAUST SLEEVE AT 270 POSITION. REPAIRED PER BOEING SRM 51-30-02.

Part: INLET FAN CASE — WORN (NR 4 ENGINE)

SEVERE VIBRATION ON CLIMB OUT OF HNL. REPLACED INLET FAN CASE AND 2 MATCHED SETS OF BLADES PER BOEING MAINTENANCE MANUAL 72-31-04 AND 72-31-02.

Part: ROLLER TRAY — CRACKED (BS 1800)

CRACK AFT CARGO BS 1800 LBL 34 WL 118 ROLLER TRAY ATTACHMENT TO WEB CHORD. REPAIRED PER BOEING SRM 53-10-04.

Part: BRACKET — CRACKED (CABIN)

CRACK IN UPPER DECK LADDER LOWER RAIL BRACKET. REPLACED BRACKET PER BOEING SRM 51-10-01.

Part: PUMP — FAILED (NR 4 HYD SYST)

ON TAXI OUT, NR 4 HYDRAULIC SYSTEM AIR DRIVEN PUMP INOPERATIVE IN AUTO OR CONTINUOUS. FOUND HYDRAULIC PUMP FAILED. REPLACED HYDRAULIC PUMP PER BOEING MAINTENANCE MANUAL 29-11-17.

Part: AIR DRIVE UNIT — INOPERATIVE (NR 4 ENGINE)

ON TAXI OUT, NR 4 HYDRAULIC SYSTEM AIR DRIVEN PUMP INOPERATIVE IN AUTO OR CONTINUOUS. CHECKED OIL LEVEL, LUBED CONTROL VALVE, RESET ADP PER MAINTENANCE MANUAL 29-11-08 AND OPERATIONAL CHECK OK PER MAINTENANCE MANUAL 29-11-00.

Part: PT2 SENSOR — CONTAMINATED (NR 4 ENGINE)

NR 4 ENGINE HAD NO THRUST LEVER RESPONSE WHEN AIRCRAFT READY FOR TAKEOFF. CHECKED ENGINE CONTROL LINKAGE, ALL CHECKED GOOD. CHECKED PS4 LINE CHECKS GOOD. CHECKED PT2 SENSOR AND LINE CHECKED GOOD. APPLIED HEAT PER MAINTENANCE MANUAL 71-00-00 PAGE 262, RAN ENGINE AND LEAK CHECK AND RUN UP ALL CHECKED GOOD PER MAINTENANCE MANUAL 71-00-00. SUSPECT DE-ICING FLUID GOT INTO PT2 SENSOR.

Part: BRACKET — CRACKED (RT MLG DOOR)

CRACKED BRACKET RIGHT WING LANDING GEAR STRUT DOOR AFT BRACKET. REMOVED FABRICATED AND INSTALLED BRACKET PER BOEING SRM 51-10-01 AND 51-30-02.

Part: FITTING — CRACKED (CARGO DOOR)

CRACKED AFT CARGO DOOR LIFT ACTUATOR MOUNT FITTING .75 INCH CRACK OUT OF NR 7 BOLT HOLE. REPAIRED PER POLAR AIR CARGO MAINTENANCE AUTHORIZATION 5310-17:01.

Part: ANGLE — CRACKED (NR 4 ENGINE COWL)

THREE CRACKED ANGLES NR 4 ENGINE INBOARD CORE COWL UPPER INNER ANGLES. FABRICATED AND INSTALLED ANGLES PER BOEING SRM 51-10-01 AND 51-30-02.

Part: SKIN — CRACKED (EMPENAGE)

SEVERAL SKIN CRACKS BETWEEN RIVETS ON LEFT SIDE OF TAILCONE EXTERIOR ABOVE APU EXHAUST DUCT. REMOVED AND REPLACED SKIN SECTION PER BOEING SRM 51-10-01 AND 51-30-02.

Part: FAIRING — CRACKED (NR 4 ENGINE)

CRACKED AND BENT NR 4 ENGINE FORWARD FAIRING RIGHT HAND FORWARD CORNER. REPAIRED PER BOEING SRM 51-40-02.

Part: BREATHER TUBE — CRACKED (NR 2 ENGINE)

CRACKED BREATHER TUBE DUCT ON NR 2 ENGINE INBOARD CORE COWL. WELD REPAIRED PER BAC 5975.

Part: PANEL — DELAMINATED (RT WING)

DELAMINATED PANEL RIGHT WING UPPER LEADING EDGE JUST INBOARD OF NR 3 ENGINE. REPAIRED PER BOEING SRM 51-40-09.

Part: SKIN — DELAMINATED (NR 2 LE FLAP)

SKIN SEPARATING ON LEFT WING INBOARD FLAP LEFT TOP CORNER INBOARD SIDE. REPAIRED PER BOEING SRM 51-40-15.

Part: PANEL — DELAMINATED (RT WING)

DELAMINATED PANEL RIGHT WING UPPER GAP PANEL AT NR 3 PYLON. REPAIRED PER BOEING SRM 51-40-09.

Part: DOOR STOP — CRACKED (LANDING GEAR)

CRACKED DOOR STOP ON LOWER BODY GEAR ADJUSTMENT TO SIDE BRACE. REPLACED STOP PER BOEING MAINTENANCE MANUAL 32-14-00.

Part: BRACKET — BROKEN (NR 11 LE FLAP)

LEFT WING LEADING EDGE FLAP NR 11 HAS BROKEN BRACKET ON CONNECTION ROD FROM BULLNOSE TO SLAT. REMOVED AND REPLACED BRACKET PER BOEING SRM 51-10-01.

Part: ACTUATOR — LEAKING (NR 1 SPOILER)

NR 3 HYDRAULIC SYSTEM FLUID LOSS. AIRCRAFT RETURNED TO MIAMI. ON GROUND FOUND LEAKING NR 1 SPOILER ACTUATOR LEAKING, CRACKED ACTUATOR END CAP. REPLACED PER BOEING MAINTENANCE MANUAL.

Part: COOLING SHROUD — BROKEN (NR 2 ENGINE)

COOLING SHROUD BROKEN ON NR 2 ENGINE GENERATOR. REPLACED NR 2 ENGINE GENERATOR COOLING SHROUD PER BAC MM 75-21-02.

Part: BLEED VLV PLATE — BROKEN (NR 3 ENGINE)

PLATE FOR LOCKOUT OF NR 3 ENGINE HIGH STAGE BLEED VALVE BROKEN. REPLACED BROKEN LOCKOUT PLATE PER BAC MM 36-11-05.

Part: LIGHT — INOPERATIVE (CABIN)

INOPERATIVE EMERGENCY LIGHT ON UPPER DECK CEILING. REPLACED EMERGENCY LIGHT ASSEMBLY PER BAC MM 33-51-06.

Part: SKIN — GOUGED (NR 1 PYLON)

DEEP GOUGE IN NR 1 PYLON CAPSKIN BETWEEN NAC 193 AND 210. REPAIRED PER POLAR AIR CARGO MAINTENANCE AUTHORIZATION 5430-01:01.

Part: PLATE — CORRODED (BS 2240)

CORROSION AT MAIN DECK TIE DOWN PLATE UPPER SURFACE AT STA 2240 LBL3. CORROSION REMOVED AS PER BAC SRM 51-10-01 AND RE-PROTECTED PER SRM 51-10-02.

Part: BEARING — DAMAGED (L5 DOOR)

DAMAGED BEARING AT THE BODY TORQUE TUBE CAM PLATE ON L5 DOOR. REPLACED CAM PLATE BEARING AND CK'D DOOR RIG PER BAC MM 53-10-03 FIG 6 AND HAECO REPAIR SCHEME R-53-00-32968.

Part: SKIN — PUNCTURED (LT ELEV)

SMALL PUNCH (HOLE) ON UPPER LEFT INBD ELEVATOR SURFACE. FIBERGLASS REPAIR PER BAC SRM 51-40-15.

Part: FLOOR BEAM — CORRODED (BS 2240)

LEVEL 1 CORROSION ON MAIN DECK RT OTBD FLOOR BEAM STA 2240. CORROSION REMOVED AND RE-PROTECTED PER BAC SRM 51-10-01 AND SRM 51-1-02.

Part: SKIN — DELAMINATED (RT TE MID FLAP)

DELAMINATED RIGHT WING INBOARD MID FLAP LOWER SKIN ADJACENT TO THE INBOARD FLAP TRACK. REPAIRED PER BOEING SRM 51-40-15.

Part: TENSION TIE — DENTED (BS 900)

DENT ON FWD SIDE OF TENSION TIE AT MAIN DECK STA 900 RBL 60 APPROX S10L. REPAIRED TENSION TIE PER BAC SRM 51-40-03 FIG 1.

Part: SUPPORT — CORRODED (BS 400)

CORROSION AT FWD LOWER CARGO SUPPORT BEAM EDGE AT STA 400 LT/RT S44 TO 46. CORROSION REMOVED AND RE-PROTECTED PER BAC SRM 51-10-01 AND SRM 51-10-02.

Part: FASTENER — MISSING (FRONT SPAR)

MISSING FASTENER AT FSSI 950 COMMON TO WING FRONT SPAR CHORD. RIVET REPLACED PER BAC SRM 51-30-02.

Part: DOOR FRAME — DENTED (CARGO DR CUTOUT)

DENT IN SIDE CARGO DOOR CUTOUT FRAME INBOARD ATTACH METAL STRAP BS 1940 APPROX S11L. METAL STRAP REPLACED PER BAC SRM 51-10-01 PG 8.

Part: FAIRING — DAMAGED (LT TE FLAP)

DAMAGED NR 1 FLAP TRACK FORWARD FIXED FAIRING EXTERNAL SURFACE. REPAIRED PER BAC SRM 51-40-15.

Part: SKIN — DAMAGED (RT TE AFT FLAP)

DAMAGED SKIN ON RIGHT WING INBOARD AFT FLAP LOWER SURFACE ADJACENT TO NR 6 FLAP TRACK. REPAIRED PER BOEING SRM 51-40-15.

Part: SUPPORT — CORRODED (BS 1500-1520)

LEVEL 1 CORROSION MAIN DECK LEFT MOST OUTBOARD LONGITUDIINAL FLOOR SUPPORT UPPER AND LOWER SURFACE BS 1500 TO 1520. REMOVED CORROSION AND TREATED PER BOEING SRM 51-10-01 AND 51-10-02.

Part: TENSION TIE — CRACKED (BS 800)

CRACK TO RT OTBD END OF TENSION TIE AT MAIN DECK STA 800 APPROX S11R. REPAIRED TENSION TIE PER HAECO DESIGN DEVIATION ORDER HX135017 AND IAI SB 747-53-2371.

Part: SCUFF PLATE — CRACKED (R1 DOOR CUTOUT)

CRACK ON R1 DOOR SCUFF PLATE CORNER AREA. WELD REPAIR ACCOMPLISHED PER HAECO STANDARD PRACTICE 70-310-003.

Part: SUPPORT — CORRODED (BS 2060-2190)

CORROSION ON RT OTBD MAIN DECK FLOOR SUPPORT BETWEEN STA 2060 AND 2190. CORROSION REPAIR PER BAC SRM 51-40-03. (REF HAECO NR'S 5256 AND 5257).

Part: SUPPORT — CORROSION (BS 1720-1730)

CORROSION ON MAIN DECK RT OTBD LONG FLOOR SUPPORT UPPER SURFACE BETWEEN STA 1720 AND STA 1730. CORROSION REMOVED AND RE-PROTECTED PER BAC SRM 51-10-01 AND 51-10-02.

Part: ACOUSTIC PANEL — DEBONDED (NR 3 ENG COWL)

DEBONDING AT NR 3 NOSE COWL 11 O'CLOCK POSITION ACOUSTIC PANEL. REPAIRED PER BAC SRM 54-30-03 FIG 29.

Part: SEAT TRACK — CORRODED (BS 2182)

LEVEL 1 CORROSION AT MAIN DECK TIE DOWN (SEAT) TRACK STA 2182 LBL 98. CORROSION REMOVED AND RE-PROTECTED PER BAC SRM 51-10-01 AND SRM 51-10-02.

Part: SKIN — CRACKED (RT TE AFT FLAP)

CRACKED SKIN ON RIGHT WING INBOARD AFT FLAP LOWER SURFACE. REPAIRED PER BOEING SRM 51-40-06.

Part: PANEL — CRACKED (LT WING)

CRACKED PANEL NR 573AB. REPAIRED PER BOEING SRM 51-40-15.

Part: STIFFENER — CRACKED (WS 670)

CRACK AT OTBD FRONT SPAR VERTICAL RIB STIFFENER IN NR 3 MAIN TANK AT WS 670. TEMP REPAIR, STOP DRILLED CRACK AND INSTALLED A REPAIR STRAP PER HAECO REPAIR SCHEME R-57-21-32967 AND BOEING FAX APPROVAL.

Part: FLOOR BEAM — CORRODED (BS 2360)

LEVEL 1 CORROSION ON RT OTBD MAIN DECK FLOOR BEAM UPPER CHORD AT STA 2360. REMOVED CORROSION PER BAC SRM 51-10-01 AND RE-PROTECTED PER SRM 51-10-02.

Part: BOLT — SHEARED (WS 590)

SHEARED BOLT AT APPROX WS 590 LWR ATTACH FOR STRINGER 7 IN NR 3 MAIN TANK. REPLACED BOLT.

Part: SEAT TRACK — CORRODED (BS 2200-2220)

CORROSION AT MAIN DECK TIE DOWN (SEAT) TRACK INBD FLANGE FROM STA 2200 TO STA 2220 LBL11. CORROSION REMOVED AND RE-PROTECTED PER BAC SRM 51-10-01 AND 51-10-02.

Part: FITTING — CRACKED (BS 1720)

CRACK AT S19R END FITTING, BS 1720. REPLACED END FITTING PER BAC SRM 51-10-01 PG 18.

Part: PANEL — CORRODED (FUSELAGE)

LEVEL 1 CORROSION KEEL BEAM ACCESS PANEL 193P INNER SURFACE SEVERAL PLACES. REMOVED CORROSION AND TREATED PER BOEING SRM 51-10-01 AND 51-10-02.

Part: BEARING — DAMAGED (L2 DOOR)

DAMAGED UPPER BEARING AT L2 DOOR TORQUE TUBE LWR HINGE. BEARING REPLACED AND DOOR RIG CK'D PER BAC MM 52-11-01.

Part: BEARING — DAMAGED (R1 DOOR)

BEARING PROTRUDING AT R1 DOOR TORQUE TUBE LWR GUIDE ARM. LWR GUIDE ARM BEARING REPLACED AND DOOR RIG CK'D PER BAC MM 52-11-01.

Part: SKIN — CORRODED (BS 1480)

LEVEL 1 CORROSION FUSELAGE SKIN BS 1480 AT STRINGER S46L AND S47L. REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.

Part: FLOOR BEAM — CORRODED (BS 1660)

LEVEL 1 CORROSION MAIN DECK BS 1660 FLOOR BEAM UPPER CHORD AT RBL 100 RIGHT END REINFORCING PLATE. REMOVED CORROSION AND TREATED PER BOEING SRM 51-10-01 AND 51-10-02.

Part: STRINGER — CRACKED (BS 1000-1020)

CRACKED STRINGER S6R BETWEEN BS 1000 AND 1020. REPAIRED PER HAECO REPAIR SCHEME 53-00-32968 REFERENCE BOEING FAX PAO-HKG-96-0001TE, 0003RE,0006RE.

Part: BRACKET — CRACKED (BS 960)

CRACK AT UPPER FRAME ATTACH ANGLE AT STA 960 S7R APPROX .6250 INCH LONG. REPLACED FRAME ATTACH BRACKET PER BAC SRM 51-10-10 PG 18.

Part: SKIN — CORRODED (BS 840-850)

LEVEL 1 CORROSION ON BELLY SKIN AND BODY FAIRING SUPPORT STRUCTURE BS 840 AND 850. REMOVED CORROSION AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.

Part: SUPPORT — CRACKED (BS 987)

LEVEL 2 CORROSION/CRACK ON BODY FAIRING SUPPORT BS 987 LBL 10 TO RBL 60. REPLACED SUPPORT PER BOEING SRM 51-10-01.

Part: THRESHOLD — CRACKED (R5 DOOR)

CRACK IN THRESHOLD R5 DOOR FORWARD LOWER CORNER. REPAIRED PER BOEING SRM 51-30-02.

Part: NOSE COWL — DENTED (NR 4 ENGINE)

DENT IN NR 4 ENGINE NOSE COWL 9 O'CLOCK POSITION. REPAIRED PER BOEING SRM 51-40-06 PARA 2L.

Part: TIE DOWN TRACK — CORRODED (BS 1670)

LEVEL 1 CORROSION MAIN DECK BS 1670 RBL 98 TIE DOWN TRACK OUTBOARD FLANGE. REMOVED CORROSION AND TREATED PER BOEING SRM 51-10-01 AND 51-10-02.

Part: FRAME — CRACKED (L5 DOOR)

CRACK AT AFT LWR CORNER AREA LWR AFT LATCH ROLLER OF L5 DOOR INTERIOR FACE. CRACK REPAIRED PER BAC SRM 51-40-02 FIG 1.

Part: FLOOR PLATE — CORRODED (BS 1980-2040)

LEVEL 1 CORROSION AFT BULK CARGO DOOR SILL ENTRY FLOOR PLATE UNDER SCUFF PLATE UPPER SURFACE AT BS 1980 TO 2040. CORROSION REMOVED AND TREATED PER BOEING SRM 51-10-01 AND 51-10-02.

Part: THRESHOLD — CRACKED (L5 DOOR)

CRACK AT FWD LWR CORNER THRESHOLD ON L5 DOOR. WELD REPAIR MADE TO THRESHOLD PER BAC5975 HAECO TECHNICAL ASSISTANCE REQUISITION 059055 AND INSTALLED PER BAC SRM 51-30-02.

Part: FLOOR BEAM — CORROSION (BS 800)

LEVEL 1 CORROSION MAIN DECK BS 800 FLOOR BEAM RIGHT END REINFORCING PLATE IN BOTH UPPER AND LOWER SURFACE. REMOVED CORROSION AND REPROTECTED AREA PER BOEING 51-10-01 AND 51-10-02.

Part: KEEL BEAM — CORRODED (BS 1350)

LEVEL 1 CORROSION KEEL BEAM BOX EXTERIOR LOWER SURFACE AT BS 1350 LBL 10 TO RBL 10. REMOVED CORROSION AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.

Part: TENSION TIE — CRACKED (BS 900)

CRACK AT MAIN DECK LEFT OTBD END TENSION TIE STA 900 APPROX S11L. TENSION TIE REPAIRED PER SB 747-53-2371 FIG 3 AND HAECO DESIGN DEVIATION ORDER HX135017.

Part: SUPPORT — CORRODED (BS 1660-1720)

LEVEL 1 CORROSION MAIN DECK BS 1660 TO BS 1720 RIGHT MOST OUTBOARD LONGITUDINGAL FLOOR SUPPORT UPPER SURFACE. CORROSION REMOVED AND TREATED PER BOEING SRM 51-10-01 AND 51-10-02.

Part: SUPPORT — CORROSION (BS 770-800)

LEVEL 1 CORROSION RIGHT MOST OUTBOARD LONGITUDINAL FLOOR SUPPORT UPPER SURFACE BETWEEN BS 770 AND BS 800. REPLACED FLOOR SUPPORT PER BOEING SRM 51-10-01 PG 18.

Part: BRACKET — CRACKED (BS 2020)

CRACKED BULK CARGO FLOOR PANEL SUPPORT ATTACH BRACKET AT BS 2020 RBL 55. REPAIRED PER BOEING SRM 51-40-05.

Part: SUPPORT — CORRODED (BS 880)

LEVEL 2 CORROSION BODY FAIRING SUPPORT SURFACE BS 880 LBL 25 TO RBL 25. REPAIRED PER BOEING SRM 53-50-04.

Part: FLOOR BEAM — CORRODED (BS 2200)

LEVEL 1 CORROSION TO MAIN DECK FLOOR BEAM UPPER CHORD STA 2200 BETWEEN LBL 87 AND LBL 98. REMOVED CORROSION AND RE-PROTECTED PER BAC SRM 51-10-01 AND 51-10-02.

Part: BEARING — DAMAGED (R1 DOOR)

DAMAGED LWR BEARING AT R1 DOOR BODY TORQUE TUBE. REPLACED BEARING AND CK'D DOOR RIG PER BAC MM 52-10-01.

Part: SUPPORT — CORRODED (BS 2350)

LEVEL 1 CORROSION ON LATERAL FLOOR SUPPORT AT MAIN DECK STA 2350 BETWEEN RBL 10 AND RBL 40. REMOVED CORROSION PER BAC SRM 51-10-01 AND RE-PROTECTED PER BAC SRM 51-10-02.

Part: FAIRING — DAMAGED (NR 6 FLAP TRACK)

DAMAGE AT NR 6 FLAP TRACK FORWARD FIXED FAIRING EXTERNAL SURFACE. REPAIRED PER BOEING SRM 51-40-15.

Part: DOUBLER — CRACKED (R4 DOOR CUTOUT)

CRACK AT INTERIOR DOUBLER IN LWR LATCH FITTING AREA OF FWD LWR R4 DOOR CUTOUT. REPAIRED DOUBLER PER BAC SRM 53-10-04 FIG 84.

Part: SCUFF PLATE — CORROSION (L3 DOOR CUTOUT)

LEVEL 1 CORROSION ON EXTERNAL SKIN AT L3 DOOR SCUFF PLATE. CORROSION REMOVED AND AREA RETREATED PER BAC SRM 51-10-01.

Part: BEARING — DAMAGED (L4 DOOR)

DAMAGED BEARINGS AT L4 TORQUE TUBE GUIDE ARM. REPLACED BEARINGS AND CK'D RIG OF DOOR PER BAC MM 52-11-01.

Part: SUPPORT — BROKEN (BS 1940-1960)

BROKEN AFT CARGO SLOPE PANEL SUPPORT AT BS 1940 TO 1960. REPLACED SLOPE PANEL SUPPORT PER BOEING SRM 51-10-01.

Part: STRINGER — DEFORMED (BS 360-380)

STRINGER 40 DEFORMED FWD CARGO COMP RT STA 360 TO STA 380. REFORMED STRINGER PER BAC SRM 51-40-01 AND HFEC CK OK.

Part: ANGLE — CRACKED (BS 1340)

DIAGONAL SUPPORT CRACKED AT L3 DOOR AFT CUTOUT BS 1340 APPROX S21L. REPLACED SUPPORT ANGLE PER BAC SRM 51-10-01 PG 18.

Part: SKIN — CORROSION (HORIZ STAB LE)

LEVEL 1 MINOR SURFACE CORROSION ON LEFT HORIZ STAB LEADING EDGE STA 200. SURFACE CORROSION REMOVED AND AREA REPROTECTED PER BAC MM 51-21-03 AND BAC SRM 51-10-02.

Part: FLOOR BEAM — CORROSION (BS 1660)

LEVEL 1 CORROSION MAIN DECK BS 1660 FLOOR BEAM LEFT END REINFORCING PLATE AT SCREW HOLE AREA. REMOVED CORROSION PER BOEING SRM 51-10-01 AND 51-10-02.

Part: REVEAL — CRACKED (R4 DOOR)

CRACK AT FWD REVEAL UPPER HINGE AREA OF R4 DOOR CUTOUT. CUTOUT REVEAL REPAIRED PER BAC SRM 51-40-03.

Part: FAIRING — DAMAGED (NE 3 FLAP TRACK)

DAMAGE NR 3 FLAP TRACK FORWARD FIXED FAIRING EXTERNAL SURFACE. REPAIRED PER BOEING SRM 51-40-15.

Part: SUPPORT — CORRODED (BS 2200-2220)

LEVEL 1 CORROSION AT MAIN DECK LEFT OTBD LONGITUDINAL FLOOR SUPPORT STA 2200 TO STA 2220. REMOVED CORROSION AND RE-PROTECTED PER BAC SRM 51-10-01 AND 51-10-02.

Part: STRINGER — CRACKED (BS 1460-1480)

CRACKED STRINGER S2R BETWEEN BS 1480 AND 1460. REPAIRED PER HAECO REPAIR SCHEME 53-00-32968 REFERENCE BOEING FAX PAO-HKG-0001TE, 003RE, 0006RE.

Part: FAIRING — DAMAGED (NR 4 FLAP TRACK)

DAMAGE AT NR 4 FLAP TRACK FORWARD FIXED FAIRING EXTERNAL SURFACE. REPAIRED PER BOEING SRM 51-40-15.

Part: SEAT TRACK — CORRODED (BS 640-645)

LEVEL 1 CORROSION MAIN DECK RBL 98 SEAT TRACK OUTBOARD FLANGE BETWEEN BS 640 AND 645. REMOVED CORROSION AND TREATED PER BOEING SRM 51-10-01 AND 51-10-02.

Part: BRACKET — CRACKED (BS 1773)

CRACKED AFT CARGO TIE DOWN TRACK ATTACH BRACKET AT BS 1773 RBL 30. REPAIRED PER BOEING SRM 51-10-01.

Part: SUPPORT — CORRODED (BS 520-560)

LEVEL 1 CORROSION RIGHT MOST OUTBOARD LONGITUDINAL FLOOR SUPPORT LOWER SURFACE BS 520 TO BS 560. REMOVED CORROSION AND TREATED PER BOEING SRM 51-10-01 AND 51-10-02.

Part: REVEAL — CRACKED (L4 DOOR CUTOUT)

CRACK AT BS 1670 BETWEEN S17 TO 18L, L4 DOOR CUTOUT FWD UPPER CORNER REVEAL. TRIMMED REVEAL TO REMOVE CRACK PER BAC SRM 53-10-01 FIG 1.

Part: PANEL — DEBONDED (NR 4 ENGINE)

DEBONDED PANEL NR 4 ENGINE NOSE COWL 6 O'CLOCK POSITION. REPAIRED PER BOEING SRM 54-30-03 FIG 28.

Part: KEEL BEAM — CORRODED (BS 1220)

LEVEL 1 CORROSION KEEL BEAM BOX LOWER EXTERIOR SURFACE BS 1220 TO 1230. CORROSION REMOVED AND REPROTECTED AS PER BOEING SRM 51-10-01 AND 02.

Part: SCUFF PLATE — CRACKED (CARGO DOOR)

DAMAGED AFT SCUFF PLATE AT BULK CARGO DOOR. WELD REPAIR MADE PER BAC SRM 51-30-02.

Part: BEARING — DAMAGED (R2 DOOR)

DAMAGED UPPER BEARING AT R2 DOOR TORQUE TUBE LWR HINGE. BEARING REPLACED AND DOOR RIG CK'D PER BAC MM 52-11-01.

Part: NOSE COWL — DEBONDED (NR 1 ENGINE)

DEBONDED PANEL NR 1 ENGINE NOSE COWL TOP PANEL 12 O'CLOCK POSITION. REPAIRED PANEL PER BOEING SRM 54-30-03.

Part: BEARING — DAMAGED (R1 DOOR)

DAMAGED LOWER BEARING AT UPPER HINGE ON R1 DOOR TORQUE TUBE. UPPER HINGE BEARING REPLACED AND DOOR RIG CK'D PER BAC MM 52-11-01.

Part: DOOR — CORRODED (EMPENANGE)

LEVEL 1 CORROSION APU BATTERY COMPARTMENT DOOR INNER SURFACE. REMOVED CORROSION PER BOEING SRM 51-10-01 WITHIN LIMITS PER 52-00-02, TREATED PER 51-10-02.

Part: SUPPORT — CORRODED (BS 1440)

CORROSION MAIN DECK BS 1440 LATERAL FLOOR SUPPORT AT LBL 75 TO 97. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.

Part: FRAME — CRACKED (L5 DOOR CUTOUT)

CRACK AT MID REVEAL AREA OF L5 DOOR CUTOUT AT APPROX S19 TO 20L. CUTOUT REVEAL REPAIRED PER BAC SRM 51-10-01 AND DOOR RIG CK'D PER BAC MM 52-11-01.

Part: SKIN — DETACHED (R1 DOOR)

EXTERIOR SKIN DETACHED ON R1 DOOR AT LOWER HINGE AREA. REFORMED SKIN PER BAC SRM 51-40-1.

Part: STRINGER — CRACKED (BS 1000-1020)

CRACK STRINGER 1R BETWEEN BS 1000 AND 1020. REPAIRED STRINGER AS PER HAECO REPAIR SCHEME 53-00-32968 REFERENCE BOEING FAX PAO-HKG-96-0001TE, 0003RE, 0006RE.

Part: SHEAR TIE — CRACKED (BS 2300)

CRACK AT FRAME ATTACH SHEAR TIE AT R5 DOOR CUTOUT BS 2300, BETWEEN S18 TO 9R. SHEAR TIE REPAIRED PER BAC SRM 53-10-04 FIG 3.

Part: NOSE COWL — DENTED (NR 1 ENGINE)

DENT IN NR 1 ENGINE NOSE COWL 7 O'CLOCK POSITION. METAL FILLER REPAIRED AS PER BOEING SRM 51-40-06 PARA 2L.

Part: LONGERON — CORRODED (BS 980-990)

LEVEL 1 CORROSION LONGERON OUTBOARD SURFACE AT BS 980 TO 990 S50R TO S51R. REMOVED CORROSION PER BOEING SRM 51-10-01 AND 51-10-02.

Part: FRAME — CRACKED (L5 DOOR CUTOUT)

CRACK AT FRAME ATTACH SHEAR TIE OF L5 DOOR CUTOUT AT BS 2300 A18-19L. SHEAR TIE REPAIRED PER BAC SRM 53-10-04 FIG 3.

Part: SKIN — CORRODED (BS 1240-1260)

LEVEL 1 CORROSION ON FUSELAGE SKIN BETWEEN S8R AND S9R BS 1240 TO 1260. REMOVED CORROSION AND TREATED PER BOEING SRM 51-10-01 AND 51-10-02.

Part: FRAME — CRACKED (R4 DOOR)

CRACK AT R4 DOOR FWD FRAME UPPER CORNER. TRIMMED FRAME TO REMOVE CRACK PER BAC SRM 52-00-01 FIG 1.

Part: FLOOR BEAM — CORRODED (BS 860)

LEVEL 2 CORROSION BS 860 FLOOR BEAM RIGHT END REFORCING FLOOR SUPPORT AT SCREW HOLES. FABRICATED AND REPLACED FLOOR SUPPORT PER BOEING SRM 51-10-01 PAGE 18.

Part: FRAME — CRACKED (R4 DOOR CUTOUT)

CRACK AT FWD FRAME UPPER CORNER OF R4 DOOR CUTOUT. TRIMMED FRAME TO REMOVE CRACK PER BAC SRM 53-10-01.

Part: BEARING — DAMAGED (R4 DOOR)

DAMAGED LWR BEARING AT R4 DOOR TORQUE TUBE UPPER HINGE. REPLACED BEARING AND CK'D DOOR RIG PER BAC MM 52-11-01.

Part: FLOOR SUPPORT — CORRODED (BS 863)

LEVEL 1 CORROSION MAIN DECK BS 863 RIGHT OUTBOARD LONGITUDINAL FLOOR SUPPORT UPPER SURFACE. REMOVED CORROSION AND TREATED PER BOEING SRM 51-10-01 AND 51-10-02.

Part: TE SKIN — CRACKED (LT TE FORE FLAP)

CRACK LEFT WING INBOARD FORE FLAP TRAILING EDGE AT APPROXIMATELY NR 3 FLAP TRACK POSITION. REPAIRED PER BOEING SRM 51-40-15.

Part: BEARING — DAMAGED (L4 DOOR)

DAMAGED BEARING AT L4 DOOR TORQUE TUBE MID SUPPORT. BEARING REPLACED AND DOOR RIG CK'D PER BAC MM 52-11-01.

Part: FLOOR BEAM — CORRODED (BS 980)

LEVEL 1 CORROSION MAIN DECK FLOOR BEAM UPPER CHORD LOWER SURFACE BS 980 RBL 110. REMOVED CORROSION AND TREATED PER BOEING SRM 51-10-01 AND 51-10-02.

Part: FAIRING — DAMAGED (RT TE FLAP)

DAMAGED NR 8 FLAP TRACK FORWARD FIXED FAIRING EXTERIOR SURFACE. REPAIRED PER BOEING SRM 51-40-15.

Part: FRAME — CORRODED (BS 2368)

LEVEL 1 CORROSION FRAME 2638 AT WL 219 LBL 12 TO RBL 12. REMOVED CORROSION PER BOEING SRM 51-10-01 WITHIN LIMITS PER 53-10-02, TREATED PER 51-10-02.

Part: FLOOR SUPPORT — CRACKED (BS 782)

CRACK AT SCREW HOLE BS 782 MOST OUTBOARD FLOOR SUPPORT. REPAIRED PER BOEING SRM 51-40-04.

Part: TIE DOWN TRACK — CORRODED (BS 862)

LEVEL 1 COROSION BS 862, RBL 98 TIE DOWN TRACK OUTBOARD. REMOVED CORROSION AND TREATED PER BOEING SRM 51-10-01 AND 51-10-02.

Part: FAIRING — DAMAGED (NR 5 FLAP TRACK)

DAMAGE AT NR 5 FLAP TRACK FORWARD FIXED FAIRING AT EXTERNAL SURFACE. REPAIRED PER BOEING SRM 51-40-15.

Part: FAIRING — DELAMINATED (NR 6 TE FLAP)

DELAMINATION, EROSION AND PAINT CHIPPING NR 6 FLAP TRACK MOVABLE FAIRING. REPAIRED PER BOEING SRM 51-40-15.

Part: FLOOR PLATE — CORRODED (BS 1850)

LEVEL 1 CORROSION AFT CARGO FLOOR PLATE UPPER SURFACE BS 1850 RBL 7 TO RBL 14. REMOVED CORROSION AND TREATED PER BOEING SRM 51-10-01 AND 51-10-02.

Part: FLOOR BEAM — CORRODED (BS 1720)

LEVEL 1 CORROSION MAIN DECK BS 1720 FLOOR BEAM UPPER CHORD UPPER SURFACE. CORROSION REMOVED AND TREATED PER BOEING SRM 51-10-01 AND 51-10-02.

Part: STRINGER — CRACKED (BS 1980)

CRACK AT STRINGER 3L STA 1980. REPAIRED STRINGER 3L CRACK PER BAC SRM.

Part: STRINGER — CRACKED (WS 670)

CRACK AT WING STA 670 FORWARD UPPER STRINGER CAP IN NR 2 MAIN TANK. REPAIRED IAW SB 57-2273 FIG'S 7 AND 9 AND HAECO TECH ASSISTANCE REQUISITION 058029.

Part: FAIRING — DAMAGED (LT TE FLAP)

DAMAGED LEFT WING NR 2 FLAP TRACK FORWARD FIXED FAIRING EXTERNAL SURFACE. REPAIRED PER BOEING SRM 51-40-15.

Part: SUPPORT — CORRODED (BS 1280)

LEVEL 1 CORROSION KEEL BEAM PANEL SUPPORT AT BS 1280 LBL 10 TO RBL 10. REMOVED CORROSION AND TREATED PER BOEING SRM 51-10-01 AND 51-10-02.

Part: SUPPORT — CORRODED (BS 827)

LEVEL 2 CORROSION BS 827 LEFT MOST OUTBOARD LONGITUDINAL FLOOR SUPPORT. REPLACED FLOOR SUPPORT PER BOEING SRM 51-10-01 PAGE 18.

Part: DOOR — DAMAGED (LT/RT MLG STRUT)

DAMAGE EXTERNAL AREA OF BOTH WING LANDING GEAR STRUT DOORS. REPAIRED PER BOEING SRM 51-40-15.

Part: SKIN — CRACKED (RT TE FORE FLAP)

CRACK RIGHT WING OUTBOARD FORE FLAP LEADING EDGE SKIN. REPAIRED PER BOEING SRM 51-40-15.

Part: SUPPORT — CORRODED (BS 2280-2300)

LEVEL 2 CORROSION TO RT OTBD MAIN DECK FLOOR SUPPORT AT STA 2280 TO 2300. REPLACED FLOOR SUPPORT PER BAC SRM 51-10-01 PG 18.

Part: ROLLER TRAY — CRACKED (CARGO COMPT)

CRACKED ANGLE AREA ON ROLLER TRAY. REPAIRED PER BOEING SRM 51-40-03.

Part: FAIRING — DAMAGED (RT TE FLAP)

DAMAGED NR 7 FLAP TRACK FORWARD FIXED FAIRING EXTERNAL SURFACE. REPAIRED PER BOEING SRM 52-40-15.

Part: TENSION TIE — CRACKED (BS 780)

CRACK AT MAIN DECK LEFT OTBD END OF TENSION TIE AT STA 780 APPROX S11L. REPAIRED TENSION TIE PER SB 747-53-2371 AND HAECO DESIGN DEVIATION ORDER HX135017.

Part: TENSION TIE — CRACKED (BS 800)

CRACK AT MAIN DECK LEFT OTBD END OF TENSION TIE AT STA 800 APPROX S11L. REPAIRED TENSION TIE PER SB 747-53-2371 AND HAECO DESIGN DEVIATION ORDER HX135017.

Part: FLOOR — CORRODED (BS 2160-2200)

LEVEL 1 CORROSION LEFT OTBD MAIN DECK FLOOR WEB UPPER SURFACE BS 2160 TO BS 2200. REMOVED CORROSION AND RE-PROTECTED PER BAC SRM 51-01-01.

Part: FASTENERS — SHEARED (WS 660)

TWO SHEARED RIVETS (FASTENERS) AT FRONT SPAR LOWER CHORD AT APPROX WS 660 IN NR 3 MAIN TANK. REPLACED FASTENERS PER BAC SRM 51-30-02.

Part: BEARING — DAMAGED (L4 DOOR)

DAMAGED LWR BEARING AT L4 TORQUE TUBE UPPER HINGE. REPLACED UPPER HINGE BEARING AND CK'D RIG OF DOOR PER BAC MM 52-11-01.

Part: THRESHOLD — CRACKED (R5 DOOR)

CRACK AT AFT LWR CORNER THRESHOLD OF R5 DOOR. REPLACED CORNER THRESHOLD PER BAC SRM 51-10-01.

Part: FASTENER — SHEARED (LT/RT WING)

INSPECTION PER AD 95-02-15 SB 57A2266, FOUND 49 SHEARED FASTENERS AT RIGHT WING FRONT SPAR FS 575.81 TO 684.18, AND 36 SHEARED FASTENERS AT LEFT WING FRONT SPAR FS 575.81 TO 668.18. PERFORMED HFEC INSPECTION, NO CRACKS FOUND. MODIFIED AND INSTALLED FASTENERS PER SB 57A2266.