N857FT

Part: SKIN — HOLE (LT TE FOFEFLAP)

LEFT WING OUTBOARD POSITION FORE FLAP LEADING EDGE HAS HOLE IN PREVIOUS REPAIR. REPAIRED DAMAGED AREA PER SRM 51-40-09.

Part: SPOILER — HOLE (NR 12 SPOILER)

RIGHT WING NR 12 SPOILER HAS SMALL HOLE IN TOP SIDE SURFACE. CLEANED, POTTED DAMAGED AREA AND REPAIRED PER SRM 51-40-06.

Part: LINER — CRACKED (APU EXHAUST)

APU EXHAUST INNER LINER HAD 12 INCH CRACK. REMOVED AND REPLACED EXHAUST LINER PER MM 49-81-03.

Part: COWL — HOLE (NR 3 ENGINE)

NR 3 ENGINE OUTBOARD CORE COWL HAS HOLE IN SKIN AND TEMPORARY FASTENER INSTALLED. FABRICATED DOUBLER AND INSTALLED PER SRM 54-30-03.

Part: FAIRING — DAMAGED (NR 4 ENGINE)

NR 4 ENGINE FWD FAIRING HAS A HOLE WORN THRU STRUCTURE. FABRICATED DOUBLER AND INSTALLED PER SRM 54-30-03.

Part: FRAME — CRACKED (RT TE MIDFLAP)

RT I/B MIDFLAP INBOARD MOST FRAME CRACKED. STOPPED DRILLED CRACK AND FABRICATED DOUBLER AND TREATED, PRIMED AND INSTALLED IAW SRM 51-40-03.

Part: LONGERON — DAMAGE (BS 1900)

STA 1900 LONGERON 19R TO 26R FRAME HAS SERVERAL GOUGES ON I/B LIP. REPAIRED FRAME IAW SRM 51-40-03.

Part: FRAME — DAMAGED (BS 2060)

FRAME AT STA 2060 HAS SEVERAL GOUGES FROM GILL LINER SUBSTRUCTURE AT LONGERON 14R TO 21R. REPAIRED FRAME IAW SRM 51-10-03. INSTALLED DOUBLER IAW SRM 51-30-02.

Part: FRAME — DAMAGED (BS 1780)

FRAME AT STA 1780 RIGHT SIDE HAS DEEP GOUGE CAUSED FROM GILL LINER SUBSTRUCTURE AT LONGERON 21R. BLENDED GOUGE AT FRAME IAW SRM 51-10-01. INSTALLED DOUBLER REPAIR IAW SRM 51-10-01.

Part: STRINGER — CRACKED (BS 2330)

STA 2330 LONGERON 14R IS CRACKED. REMOVED CRACKED STRINGER AND SPLICE. FABRICATED, TREATED, PRIMED AND REINSTALLED STRINGER AND SPLICE IAW SRM 53-10-03 FIG 4 AND 54-30-02.

Part: FAIRING — DAMAGED (NR 3 TE FLAP)

NR 3 FLAP CANOE TRAILING EDGE DAMAGED. REMOVED DAMAGED AREA AND APPLIED FIBERGLASS LAY UP OF 3 PLY SKINS IAW SRM 51-40-15.

Part: LONGERON — CRACKED (BS 2330)

STA 2330 LONGERON 17R IS CRACKED. REMOVED CRACKED STRINGERS AND SPLICE. FABRICATED, TREATED, PRIMED AND REINSTALLED STRINGER AND SPLICE IAW SRM 53-30-02 FIG 4 AND 51-30-02.

Part: SKIN — PUNCTURED (LT AILERON)

HOLE IN LOWER SURFACE OF LEFT INBOARD AILERON. CLEANED AREA, REMOVED DAMAGED MATERIAL, AND REPAIRED WITH FIBERGLASS OVERLAYS IAW SRM 51-40-06.

Part: SKIN — DAMAGED (RT TE MIDFLAP)

RT I/B MIDFLAP HAS DEEP GOUGE AT LEADING EDGE I/B CARRIAGE CUT OUT. REWORKED GOUGES IAW SRM 57-50-01. TREATED AND PRIMED IAW SRM 51-10-02.

Part: FITTING — DAMAGED (RT TE MIDFLAP)

RT I/B MIDFLAP AFT SUPPORT FITTING GOUGED. REMOVED AND REPLACED RT O/B MIDFLAP AFT SUPPORT FITTING IAW SB 747-27-2280.

Part: ANGLE — CRACKED (BS 1480)

L ANGLE BELOW SPLICE FITTING AT RIGHT BODY GEAR WHEEL WELL STA 1480 CRACKED. REMOVED AND REPLACED L ANGLE IAW SRM 51-10-01 AND 51-30-02.

Part: SKIN — CORROSION (FUSELAGE)

LEVEL 1 CORROSION, FOUND UNDER BOTH ATC ANTENNAS. REMOVED CORROSION IAW SRM 51-10-06.

Part: PIN — CORRODED (RT TE FLAP)

RIGHT WING NR 7 SPINDLE AFT BOGIE O/B SUPPORT PIN CORRODED. REPLACED O/B SUPPORT PIN ON NR 7 SPINDLE AFT BOGIE IAW 747 OHM 27-51-75.

Part: SKIN — DELAMINATED (RT MLG DOOR)

RIGHT FLYING DOOR LOWER SECTION HAS SPOTS OF DELAMINATION ON ITS INNER SURFACE AT DENT LOCATION. SANDED AND REMOVED DAMAGED AREA AND REPAIRED IAW SRM 51-40-09.

Part: ANTENNA — CORROSION (NR1 & NR2 ATC)

NR 1 AND NR 2 ATC ANTENNAS HAVE SURFACE CORROSION. REPLACED BOTH NR 1 AND NR 2 ATC ANTENNAS. OPS CHECKED GOOD IAW 3450-01-01.

Part: FAIRING — DAMAGED (NR 2 TE FLAP)

NR 2 FLAP FAIRING CANOE HAS HOLE DAMAGE INSIDE. APPLIED FIBERGLASS OVERLAYS AND REPAIRED IAW SRM 51-40-15.

Part: SKIN — DAMAGED (LT TE MIDFLAP)

LEFT INBOARD MIDFLAP HAS HOLE IN UPPER SURFACE JUST AFT OF INBOARD CARRIAGE. REMOVED DAMAGED SKIN AND REPAIRED WITH FIBERGLASS DOUBLERS IAW SRM 51-40-09.

Part: SKIN — DAMAGED (NR 2 TE FLAP)

NR 2 LEFT AFT FLAP TRAILING EDGE DAMAGED. REPAIRED DAMAGE AT AFT T/E FLAP IAW SRM 51-40-09.

Part: COWLING — DAMAGED (NR 4 ENGINE)

NR 4 ENG INBOARD T/R TRAILING EDGE AT 8 O'CLOCK POSITION SKIN DAMAGED AND PEELING IN THREE AREAS. REPAIRED SKIN ROUTED SMALL CRACK AND REBONDED SKIN IAW 51-40-05.

Part: SUPPORT — CORRODED (CABIN)

LEVEL 1 CORROSION FOUND UNDER F/E SEAT FLOOR PANEL SUPPORT BEAM. REMOVED SURFACE CORROSION ON SUPPORT BEAM AND TREATED IAW SRM 51-10-06.

Part: SUPPORT — CORRODED (BS 340)

LEVEL 1 CORROSION AT SUPPORT CHANNEL FOR DRAIN PAN AT BS 340. CORROSION REMOVED FROM SUPPORT CHANNEL AT STA 340 IAW SRM 51-10-01.

Part: SKIN — CRACKED (NR 3 ENG COWL)

NR 3 ENG O/B FAN COWL CRACK ON UPPER FWD AND AFT HINGE CUTOUT. BLENDED OUT CRACKED AREA AROUND FORWARD HINGE. CRACK WITHIN SRM LIMITS PER SRM 51-40-06 FIG 2. REPAIRED PER SRM 51-40-06.

Part: FLOORBEAM — CORRODED (BS 600)

LEVEL 1 CORROSION FOUND ON BOTTOM OF FLOORBEAM BS 600. REMOVED SURFACE CORROSION IAW SRM 51-10-01.

Part: DOOR — CORRODED (LT MLG)

LEVEL 1 CORROSION LEFT FLYING DOOR LOWER SECTION ALONG LOWER EDGE OF ITS INNER SURFACE AROUND BOLD HEADS. REMOVED AND REPLACED FASTENERS AND CLEANED AREAS IAW SRM 51-30-02.

Part: SKIN — CORROSION (RT MLG DOOR)

RT BODY MLG BOTH INBOARD AND OUTBOARD STRUT DOOR ASSEMBLIES HAVE MANY SPOTS WITH LOST FINISH AND SURFACE CORROSION. REMOVED MINOR SURFACE CORROSION IAW SRM 51-10-01. TREATED AND PRIMED IAW SRM 51-10-02.

Part: SKIN — CORROSION (LT MLG DOOR)

LEFT BODY MLG INBD AND OTBD STRUT DOOR ASSEMBILES HAVE MANY SPOTS WITH LOST FINISH AND SURFACE CORROSION. REMOVED MINOR SURFACE CORROSION IAW SRM 51-10-01. TREATED AND PRIMED IAW SRM 51-10-02.

Part: COWL — DENTED (NR 2 ENGINE)

NUMBER 2 ENGINE NOSE COWL SKIN DENTED AT 0630 POSITION. REPAIRED NOSE COWL PANEL AT 0630 POSITION PER SRM 51-40-07.

Part: TRANSMITTER — INOPERATIVE (NR 2 ENGINE EPR)

NR 2 ENGINE WOULD NOT MAKE TAKEOFF THRUST. TEMP 912 DEGREES 1:08 EPR. ABORTED TAKEOFF. REMOVED AND REPLACED EPR TRANSMITTER REF MM 77-11-00. REMOVED AND REPLACED T7 LINE AS PRECAUTION REF MM 77-12-00. REQ OPS CHECK. OPS CHECK SATISFACTORY PER MM 77-00-00.

Part: BRAKE — DAMAGED (NR 11-15 WHEEL)

WHILE PARKED ON GATE, NR 9, NR 11, AND NR 15, MAIN WHEELS COLLAPSED DUE TO BRAKE OVERHEAT. ON WHEEL CHANGE, NR 11 AND NR 15 BRAKE UNITS WERE FOUND DAMAGED AND WERE REPLACED.

Part: FITTING — GOUGED (LT AILERON)

LEFT I/B AILERON I/B PRIMARY HINGE WING FITTING LT SIDE IS GOUGED BY RETAINER BOLT HOLE AREA. BLENDED GOUGE LESS THAN 10 PERCENT MATERIAL LOSS PER SRM 57-50-01.

Part: ENGINE — MALFUNCTIONED (NR 2)

VIBRATION ON TAKEOFF. RETARDED AND ADVANCED NR 2 ENG THROTTLE. VIBRATION FOLLOWED THROTTLE MOVEMENT. A/C PACKS WERE OFF. REMOVED AND REPLACED NR 2 ENGINE PER MM 71-00-00. OPS CHECK, LEAK CHECK ALL NORMAL ON ENG RUN-UP PER MM 71-00-00.

Part: KEEL BEAM — DAMAGED (BS 1380)

SHEET METAL DAMAGE TO LOWER KEEL BEAM AREA AND LOWER WEB AT STA 1380 RT BODY WHEEL WELL. REPAIRED DAMAGED SECTION BY CUTTING OUT DAMAGE AND FABRICATION FILLERS, DOUBLERS AND TRIPLERS AND REPLACING PER PAC MA NR 5310-24:10.

Part: ACCUMULATOR — FAILED (BS 1380)

BRAKE ACCUMULATOR LOWER CAP BROKEN OFF COMPLETELY. REMOVED AND REPAIRED BRAKE ACCUMULATOR PER MM 32-41-09. PRECHARGED ACCUMULATOR PER MM 12-15-09. SYSTEM TESTS NORMAL PER MM 32-41-00.

Part: KEEL BEAM — DAMAGED (BS 1380)

SHEET METAL DAMAGE TO UPPER KEEL BEAM WEB AT STATION 1380 IN THE RIGHT BODY WHEEL WELL. REPAIRED DAMAGED SECTION BY CUTTING DOUBLERS AND TRIPLERS PER PAC MA 5310-24:01.

Part: ACCUMULATOR — RUPTURED (NR 4 HYD SYST)

DURING APPROACH, AFTER GEAR DOWN LOST NR 4 HYD SYSTEM, 0 BRAKE PRESSURE ON GUAGE. HYD BRAKE ACCUMULATOR RUPTURED, DAMAGE TRIM AIR DUCT, APU FUEL DRAIN LINE, HYD LINE DAMAGE.

Part: FRAME — CRACKED (BS 540)

BS 540 S26L FRAME CRACKED. REPAIRED FRAME PER RS53-22-33687 BOEING.

Part: FLAP — CORROSION (NR 7 TE FLAP)

LEVEL 1 CORROSION AT LEADING EDGE FRONT SPAR WS 972 NR 7 FLAP. REPAIRED CORROSION PER SRM 51-10-01.

Part: SEAT TRACK — CORROSION (BS 920)

LEVEL 1 CORROSION ON SEAT TRACK STA 920 RBL 97R. REPAIRED CORROSION PER SRM 53-10-05.

Part: STIFFENER — CORROSION (BS 1350)

LEVEL 1 CORROSION ON RT WING GEAR STA 1350 STIFFENER. REPAIRED CORROSION PER SRM 51-10-01.

Part: SUPPORT — CRACKED (BS 2705)

APU VERTICAL SUPPORT TUBE AT BS 2705 WL 364 HAS CRACK. REPLACED PER SRM 51-10-01.

Part: SEAT TRACK — WORN (BS 2260)

SEAT TRACK BS 2260 BL 33 DEEPLY WORN. REPLACED SEAT TRACK PER SRM 53-10-05.

Part: COWL — CORROSION (NR 4 PYLON)

NR 4 ENG NOSE COWL SKIN SURFACE CORROSION. REMOVED SURFACE CORROSION AND REPROTECTED PER SRM 51-10-01 AND 51-10-02.

Part: TIE DOWN — CORRODED (BS 2300)

LEVEL 1 CORROSION AT TIE DOWN FITTING SUPPORT FUSELAGE BS 2300 BL 22. REMOVED CORROSION AND REPROTECTED PER SRM 51-10-01 AND 51-10-02.

Part: REVEAL — CRACKED (R1 DOOR)

R-1 DOOR FWD REVEAL PANEL CRACKED. REPAIRED PER SRM 51-40-03 FIG 3.

Part: SUPPORT — CRACKED (CABIN)

LEVEL 1 CORROSION MAIN DECK FLOOR SUPPORT BL 22 TO 24. REPAIRED CORROSION PER SRM 51-40-04.

Part: FASTENERS — CORRODED (NR 3 PYLON)

LEVEL 1 CORROSION ON NR 3 PYLON AFT STRUT DIAG BRACE AFT END LARGE HI-LOK HEADS. SURFACE CORROSION REMOVED PER SRM 51-10-01.

Part: COWL — DELAMINATED (NR 3 ENGINE)

PANEL 474BL DELAMINATED TOP LT CORNER OF NR 3 ENGING COWL. HOT BOND REPAIR PER SRM 51-40-06 FIG 17.

Part: BASE — CORRODED (NR 1 DME ANTENNA)

NR 1 DME ANT BASE CORRODED. CORROSION REMOVED AND REPROTECTED PER SRM 51-01-01 AND 51-10-02.

Part: REVEAL — CRACKED (L4 DOORWAY)

L4 DOOR CUTOUT LWR REVEAL CRACKED. REMOVED CRACKED AREA PER SRM 51-10-01.

Part: DOOR — CORROSION (LT MLG)

LT BODY GEAR DOOR CORRODED. REMOVED CORROSION PER SRM 51-10-01 AND 51-10-02.

Part: SUPPORT — CRACKED (BS 2060)

FLOOR SUPPORT CHANNEL CRACKED AT BS 2060 BL 22. REPAIRED SUPPORT CHANNEL PER SRM 51-40-03 FIG 2.

Part: TIE DOWN TRACK — CORRODED (BS 1120-1170)

LEVEL 1 CORROSION ON MAIN DECK TIE DOWN TRACK AT BS 1120 TO 1170 BL R11. REMOVED CORROSION AND REPROTECTED PER SRM 51-10-01 AND 51-10-02.

Part: WEB — CRACKED (BS 2120)

WEB AT BS 2120 TO 2140 STR 28R TO 29R CRACKED. REPAIRED WEB PER SRM 51-40-02 AND 51-40-03.

Part: TENSION TIE — CRACKED (BS 820)

TENSION TIE CRACKED AT BS 820 WL 300. TENSION TIE REPAIRED PER SB 53-2371 FIG 3.

Part: FLOORBEAM — CORROSION (BS 980)

LEVEL 1 CORROSION ON FLOORBEAM UPPER CHORD AT FUSELAGE BS 980 L2 TO R2. CORROSION REMOVED AND REPROTECTED PER SRM 51-10-01 AND 51-10-02.

Part: FLOOR PANEL — CORROSION (BS 520)

LEVEL 1 CORROSION AT FLOOR PANEL FUSELAGE BODY STATION 520 TO 540 BL 8. CORROSION REMOVED AND PANEL REPLACED AND REPROTECTED PER SRM 51-01-01 AND 51-10-02.

Part: SUPPORT — CORRODED (BS 1220)

LEVEL 1 CORROSION AT FLOOR SUPPORT FUSELAGE BS 1220 BL 85 TO 97. CORROSION REMOVED AND REPROTECTED PER SRM 51-01-01 AND 51-10-02.

Part: CLIP — DAMAGED (BS 1480)

RT BODY GEAR CLIP DAMAGED STA 1480 ABOVE ANTI-SKID MODULE. REMOVED AND REPLACED CLIP PER MM 20-51-01.

Part: FRAME — CRACKED (BS 860)

FRAME CRACKED AT BS 860 L 25. REPAIRED FRAME PER BACRS 53-22-33686.

Part: SUPPORT — CRACKED (BS 1487)

FUSELAGE SUPPORT FORGING CRACKED AT BS 1487. REPLACED FITTING PER SRM 51-10-01.

Part: SEAT TRACK — CORROSION (BS 520-530)

LEVEL 1 CORROSION ON SEAT TRACK BS 520 TO 530 BL L47. CORROSION REMOVED TRACK REPLACED AND REPROTECTED PER SRM 51-10-01, 53-10-01, 51-10-02.

Part: SKIN — DAMAGED (APU COMPT AREA)

APU COMPT RT DOOR RECESS CUTOUT ENLARGED. REPAIRED CUTOUT PER SRM 52-40-02 FIG 1.

Part: COWL — DELAMINATED (NR 4 ENGINE)

NR 4 RT SIDE FAN COWL DELAMINATED. REPAIRED BY HOT BOND REPAIR PER SRM 51-40-06 FIG 17A.

Part: TENSION TIE — CRACKED (BS 880)

TENSION TIE CRACKED AT FUSELAGE BS 880 WL 300. REPAIRED PER SB 53-2371 FIG 3.

Part: TIE DOWN — CORROSION (BS 980)

LEVEL 1 CORROSION ON TIE DOW AT FUSELAGE BS 980 BL L11. CORROSION REMOVED AND REPROTECTED PER SRM 51-10-01 AND 51-10-02.

Part: SKIN — CORROSION (RT WING)

SURFACE CORROSION ON UPPER SPAR SKIN RT WING. CORROSION REMOVED AND REPROTECTED PER SRM 51-10-01 AND 51-10-03.

Part: TIE DOWN — CORRODED (BS 2180)

LEVEL 1 CORROSION AT TIE DOWN FUSELAGE BS 2180 BL 30. REMOVED CORROSION AND REPROTECTED PER SRM 51-10-01 AND 51-10-02.

Part: SUPPORT — CORROSION (BS 1100)

LEVEL 1 CORROSION AT FLOOR SUPPORT AT FUSELAGE BS 1100 R80 TO R97. CORROSION REMOVED AND REPROTECTED PER SRM 51-10-01 AND 51-10-02.

Part: SUPPORT — CORRODED (BS 2310)

LEVEL 1 CORROSION AT FLOOR SUPPORT FUSELAGE BS 2310 BL 25 TO 33. CORROSION REMOVED AND REPROTECTED PER SRM 51-01-01 AND 51-10-02.

Part: FASTENERS — CORRODED (NR 3 PYLON)

ANCHOR NUTS SURFACE CORROSION ON NR 3 PYLON NAC STA 379 TO 417. CORROSION REMOVED AND RETREATED PER SRM 51-01-01 AND 51-10-02.

Part: BRACKET — BROKEN (BS 1380/1400)

FUSELAGE SUPPORT BRACKET BS 1380/1400 BROKEN. SUPPORT BRACKET REPLACED PER SRM 51-10-01.

Part: TENSION TIE — CRACKED (BS 840)

TENSION TIE CRACKED AT BS 840 WL 300. TENSION TIE REPAIRED PER SRM 53-23-71.

Part: SEAT TRACK — CORRODED (BS 1110)

LEVEL 1 CORROSION ON SEAT TRACK FLANGE AT BS 1110 BL 98. CORROSION REMOVED, REPAIRED AND REPROTECTED PER SRM 51-10-01, 53-10-01 AND 51-10-02.

Part: SKIN — CORROSION (LT WING)

LT WING UPPER SKIN FRT SPAR EXT CORRODED. CORROSION REMOVED AND REPROTECTED PER SRM 51-10-01 AND SRM 51-10-02.

Part: SUPPORT — CORRODED (BS 2279)

LEVEL 1 CORROSION AT FLOOR SUPPORT BS 2279 TO 2200 L41. CORROSION REMOVED AND REPROTECTED PER SRM 51-10-01 AND 51-10-02.

Part: PANEL — DELAMINATED (LT WING)

LT WING INBD PANEL ABOVE LANDING LIGHT DELAMINATED. FIBERGLASS REPAIRED PER SRM 51-40-12.

Part: SEAT TRACK — CORROSION (BS 498)

LEVEL 1 CORROSION ON SEAT TRACK BS 498 TO 500 LBL 99L. REPAIRED CORROSION PER SRM 51-10-01.

Part: TIE DOWN — CORROSION (BS 1000)

LEVEL 1 CORROSION ON TIE DOWN AT FUSELAGE BS 1000 BL R97. CORROSION REMOVED AND REPROTECTED PER SRM 51-01-01 AND 51-10-02.

Part: SEAT TRACK — CORROSION (BS 520)

LEVEL 1 CORROSION ON UPPER DECK SEAT TRACK AT BS 520 BL 9. CORROSION REMOVED, REPAIRED AND REPROTECTED PER SRM 51-10-01, 51-10-02 AND 53-10-05.

Part: CHANNEL — CRACKED (CARGO COMPT)

FWD CARGO FLOOR SUPPORT CHANNEL CRACKED. SUPPORT REPAIRED PER SRM 51-10-01.

Part: SKIN — HOLE (NR 4 PYLON)

NR 4 PYLON RT HYD DOOR NR 484AR HAS HOLE. HOT BOND REPAIRED HOLE PER SRM 51-40-06.

Part: TENSION TIE — CRACKED (BS 860)

TENSION TIE CRACKED AT BS 860 WL 300. TENSION TIE REPAIRED PER SB 53-2371 FIG 3.

Part: COWL — DELAMINATED (NR 4 ENGINE)

NR 4 ENGINE RT COWL DELAMINATED. REPAIRED COWL BY HOT BOND PER SRM 51-40-06 FIG 17A.

Part: ANCHOR NUTS — CORROSION (BS 1220)

LEVEL 1 CORROSION AT FLOOR SUPPORT ANCHOR NUTS. CORROSION REMOVED AND REPROTECTED PER SRM 51-10-01 AND 51-10-02.

Part: TENSION TIE — CRACKED (BS 780)

TENSION TIE CRACKED. TENSION TIE REPAIRED PER SB 53-2371 FIG 5.

Part: PANEL — DELAMINATED (PYLON)

PANEL 484AL ON PYLON SKIN WORN AND DELAMINATED. HOT BOND REPAIRED PER SRM 51-40-06.

Part: SEAT TRACK — BROKEN (BS 2150)

MAIN DECK SEAT TRACK BROKEN AT BS 2150 TO 2230. SEAT TRACK REPAIRED PER SRM 53-10-08.

Part: COWL — DELAMINATED (NR 4 ENGINE)

NR 4 FAN COWL DELAMINATED. HOT BOND REPAIR PER SRM 51-20-06 FIG 17A.

Part: REVEAL — CRACKED (L5 DOOR)

L-5 DOOR UPPER REVEAL CRACKED. REVEAL REPAIRED PER SRM 53-10-04 FIG 9.

Part: FLOOR PANEL — DAMAGED (CARGO COMPT)

FWD CARGO COMPARTMENT BS 570/600 FLOOR PANEL DAMAGED. REPAIRED DAMAGE PER SRM 51-40-02.

Part: WEB — CRACKED (BS 570)

FWD CARGO COMPARTMENT BS 570 SUPPORT WEB CRACKED. REPLACED PER SRM 51-10-01.

Part: SEAT TRACK — CRACKED (BS 2250)

BS 2250 LBL 11 SEAT TRACK WEB CRACKED. REPAIRED SEAT TRACK PER SRM 51-40-02.

Part: SPLICE — CRACKED (BS 1350)

MAIN DECK BS 1350 STR 13L SPLICE FITTING CRACKED. REPLACED FITTING PER SRM 51-10-01.

Part: FLOOR PANEL — DAMAGED (BS 520/600)

UPPER DECK BS 520/600 RPL 9/27 FLOOR PANEL DAMAGE. REPLACED FLOOR PANEL PER SRM 53-21-02.

Part: FAIRING — CRACKED (NR 4 PYLON)

NR 4 PYLON, V FAIRING LEFT FWD CRACKED. REPAIRED FAIRING PER SRM 51-40-03.

Part: PLATE — DAMAGED (NR 2 PYLON)

DAMAGE ON NR 2 PYLON DUCT REAR LOWER PLATE. REPLACED PER SRM 51-10-01.

Part: FASTENERS — MISSING (BS 570-600)

FWD CARGO COMPT BS 570/600 FLOOR PANEL MISSING FASTENERS. REMOVED AND REPLACED FASTENERS PER SRM 51-30-02.

Part: ANGLE — CRACKED (BS 400)

FWD E/E COMP BS 400 ANGLE CRACKED. REPLACED PER SRM 51-10-01.

Part: ANGLE — BROKEN (BS 1900-1920)

AFT CARGO COMPARTMENT BS 1900/1920 SUPPORT ANGLE BROKEN. REPLACED PER SRM 51-10-01.

Part: FASTENERS — LOOSE (NR 4 PYLON)

NR 4 PYLON INSIDE STRUT AT STA 221.9 LOOSE FASTENERS. REMOVED AND REPLACED FASTENERS PER SRM 51-30-02.

Part: PANEL — CRACKED (BS 1480)

LT BODY GEAR STA 1480 PANEL CRACKED. REPAIRED CRACK PER SRM 51-40-15.

Part: ANGLE — CRACKED (BS 320)

NLG BS 320, 2 CRACKED ANGLES. REMOVED AND REPLACED PER SRM 51-10-01.

Part: TIE STRAP — CRACKED (BS 1940/1980)

BULK CRGO BS 1940/1980 S40L TIE STRAPS DAMAGED AND CRACKED. REPLACED TIE STRAPS PER SRM 51-10-01.

Part: BRACKET — CRACKED (NR 1 PYLON)

NR 1 PYLON FILTER MOUNT BRACKED CRACKED, 2 EA. REPLACED PER SRM 51-40-03.

Part: CHANNEL — BROKEN (BS 560)

BS 560 FWD CARGO RT SIDE CHANNEL BROKEN. REPAIRED PER SRM 51-40-02.

Part: SHEAR TIE — CRACKED (BS 1780)

AFT CARGO COMPARTMENT STA 1780 S47L SHEAR TIE CRACKED. REPAIRED PER 53-10-04.

Part: SKIN — DELAMINATED (RT TE FOREFLAP)

RT WING INBD OF NR 7 FLAP TRACK FOREFLAP DELAMINATED. REPAIRED FOREFLAP DELAMINATION PER SRM 51-40-15.

Part: FLOOR PANEL — DAMAGED (BS 1450-1460)

MAIN DECK BS 1450 TO 1460 FLOOR PANEL DAMAGED. REPAIRED PER SRM 53-21-02.

Part: SKIN — DENTED (BS 1980)

FUSELAGE SKIN DENTED AT BS 1980 S47R TO S51R. REPAIRED SKIN PER SRM 51-40-01 AND SRM 51-10-02.

Part: SEAT TRACK — CORROSION (BS 2190)

LEVEL 1 CORROSION ON MAIN DECK BS 2190 LBL 11 SEAT TRACK. REPLACED TRACK PER SRM 53-10-05 FIG 14.

Part: SEAT TRACK — CORRODED (BS 520)

LEVEL 1 CORROSION ON UPPER DECK SEAT TRACK BS 502 THRU 530 LBL 9. REMOVED CORROSION PER SRM 51-10-01 AND TRACK REPAIRED PER SRM 51-10-05.

Part: PANEL — DELAMINATED (LT WING)

LT T/E PANEL 572AB DELAMINATED. REPAIRED PANEL PER SRM 51-40-15.

Part: FLOORBEAM — CORROSION (BS 980)

LEVEL 1 CORROSION MAIN DECK FLOORBEAM AT STA 980 RBL 70. REPAIRED PER 51-40-04 FIG 1.

Part: NUT PLATE — DAMAGED (VERT STAB)

TWELVE DAMAGED NUT PLATE ON VERTICAL FIN. REMOVED AND REPLACED PER SRM 51-30-02.

Part: FASTENERS — MISSING (NR 3 PYLON)

NR 3 PYLON AFT FIXED FAIRING 4 ANCHOR NUTS MISSING. REPLACED FASTENERS PER SRM 51-10-01.

Part: DOOR — CRACKED (BS 1840-1860)

BS1840 TO 1860 DRIP SHROUD ACCESS DOOR CRACKED. REPLACED PER SRM 51-10-01.

Part: DOOR — DEFORMED (NR 1 PYLON)

NR 1 PYLON RT TRAILING EDGE DOOR DEFORMED. REPAIRED PER SRM 51-10-01.

Part: SEAT TRACK — CORROSION (BS 920)

LEVEL 1 CORROSION ON MAIN DECK SEAT TRACK BS 920 RBL 97R. CORROSION REMOVED AND REPAIRED PER SRM 53-10-05 FIG 14.

Part: PLATE — DAMAGED (RT WING)

RT WING T/E ACCESS PANEL 691DB DAMAGED ANCHOR NUTS. REMOVED AND REPLACED PER SRM 51-10-01.

Part: STRAP — CRACKED (NR 1 PYLON)

NR 1 PYLON INTERNAL STRAP CRACKED AT STA 207. REPLACED PER SRM 51-10-01.

Part: PANEL — DAMAGED (LT WING)

LT WING FUELING PANEL DAMAGED LATCH. REMOVED AND REPLACED PER SRM 52-49-09.

Part: PANEL — DAMAGED (RT WING)

RT WING PANEL 672DB DAMAGED ANCHOR NUTS. REMOVED AND REPLACED PER SRM 51-10-01.

Part: NUT PLATE — DAMAGED (NR 3 STRUT)

NR 3 AFT ENGINE STRUT L/R 4 DAMAGED NUT PLATES. REMOVED AND REPLACED PER SRM 51-30-02.

Part: DRIVE ROD — BROKEN (RT TE FLAP)

AFTER HARD LANDING, EXTERIOR INSPECTION FOUND RIGHT INBOARD FLAP NOT FULL UP. FOUND DRIVE RODS FOR THE AFT CANOE ASSEMBLY BROKEN AT THE NR 5 AND NR 6 POSITIONS. DRIVE RODS REPLACED PER BOEING M/M 27-51-01. NR 6 CANOE WAS FOUND WITH A HOLE. REPLACED PER BOEING M/M 27-51-26. NR 5 CANOE WAS FOUND DAMAGED. REPAIRED PER BOEING SRM 51-40-09. ON RETRACTION OF FLAPS THE INBOARD AILERON WAS CONTACTED AT THE AFT END. REPLACED AILERON PER BOEING M/M 27-11-01. RETRACTION ALSO DAMAGED THE NR 3 AFT FLAP REPAIRED PER BOEING SRM 51-40-06, 51-40-07 AND 51-40-09. COMPLIED WITH HARD LANDING INSPECTION PHASE 1 PER BOEING M/M 05-51-05. NO ADDITIONAL DISCREPANCIES FOUND.

Part: LINE — CRACKED (NR 4 PYLON)

NR 4 HYDRAULIC SYSTEM FLUID LOSS TO 1.6 GALLONS. FOUND CRACKED PRESSURE LINE IN NR 4 PYLON. REPLACED LINE, ENGINE DRIVEN PUMP CASE DRAIN AND PRESSURE FILTERS PER BOEING MAINTENANCE MANUAL 29-11-23, 29-11-05, AND 29-11-18.

Part: SKIN — DELAMINATION (NR 8 SPOILER)

RT WING NR 8 SPOILER LWR SURFACE HAS AREA OF DELAMINATION. REMOVED DISBONDED SKIN AND DAMAGED CORE. BONDED NEW CORE FILLER AND DOUBLERS IAW SRM 51-40-06.

Part: ACTUATOR — LEAKING (RT MLG TILT)

NR 4 HYDRAULIC SYSTEM FLUID LOSS TO 1.6 GALLONS. DECLARED EMERGENCY TO PROVIDE TIME FOR ABNORMAL PROCEDURES. EMERGENCY TERMINATED AFTER LANDING ALL SYSTEMS FUNCTIONED NORMAL. FOUND RIGHT WING POSITIONING ACTUATOR LEAKING. REPLACED PER BOEING M/M 32-11-20.

Part: FAIRING — WORN (NR 7 FIXED CANOE)

NR 7 FIXED FAIRING CANOE NEEDS COMPOSIT REPAIR. REPAIRED FIXED FAIRING BY USING FIBERGLASS OVERLAYS IAW SRM 51-40-15.

Part: SKIN — DELAMINATED (NR 3 SPOILER)

LT WING NR 3 SPOILER UPPER SKIN DELAMINATION. REMOVED AND REPLACED NR 3 SPOILER PER MM 27-61-02.

Part: SKIN — DELAMINATION (RT TE MIDFLAP)

R/W O/B T/E MIDFLAP LOWER SIDE DELAMINATION. REPAIRED IAW SRM 51-40-09.

Part: SKIN — DAMAGED (NR 11 SPOILER)

NR 11 SPOILER UPPER SKIN IN NEED OF REPAIR. REPAIRED IAW SRM 51-40-06.

Part: SEAT TRACK — CRACKED (BS 1780)

SEAT TRACK CRACKED AT BS 1780 AT RBL 50. REPAIRED IAW SRM 53-10-05 FIG 5.

Part: ANGLE — CRACKED (BS 1310)

ANGLE CRACKED BOTTOM OF KEEL BEAM APPROX STA 1310. REMOVED AND REPLACED ANGLE BOTTOM OF KEEL BEAM STA 1310 IAW SRM 51-30-02 AND 51-10-01.

Part: ANGLE — CORROSION (BS 1360)

LEVEL 1 CORROSION ON PANEL SUPPORT ANGLE BRACKET KEEL BEAM AREA STA 1360. REMOVED T- EXTRUSION AND ANGLE BRACKET AND REPLACED WITH NEW FABRICATED ANGEL IAW SRM 51-30-02.

Part: PANEL — CORRODED (NR 12 SPOILER)

LEVEL 1 CORROSION ON #12 SPOILE PANEL UPPER SERVICE - LITE CORROSION. REMOVED CORROSION PER SRM 51-10-01.

Part: RIVET — FAILED (BS 1300)

KEEL BEAM AREA, BS 1300 RIVET HEAD POPPED OFF. REMOVED AND REPLACED FASTENER IAW SRM 51-30-02.

Part: FAN BLADE — CRACK (NR 3 ENGINE)

NR 3 ENGINE, NR 5 FAN BLADE HAS A CRACK AT L/E. REMOVED CRACK BY BLENDING IAW MM 72-31-02.

Part: FLOORBEAM — CRACKED (BS 1800)

AFT PIT STA 1800 FLOORBEAM FLANGE CRACKED AT RT END APPROX RBL 50. REMOVED AND REPLACED FLOORBEAM IAW SRM 51-10-01. FABRICATED NEW FLOORBEAM IAW SRM 51-30-02.

Part: INERTIAL NAV SYS — FAILED (NR 1)

NR 1 INS FAILED. THIS A/C EQUIPED WITH ONLY 2 INS SYSTEMS. A/C RETURNED TO AMS. REPLACED NR 1 INU IAW MM 34-41-07. NIL MALFUNCTION CODES FINE ALIGNMENT C/W.

Part: SEAL — MISINSTALLED (NR 1 ENGINE)

ENGINE SHUT DOWN AT 21,000 FEET DUE TO LOSS OF NR 1 ENGINE OIL QUANTITY AND LOSS OF OIL PRESSURE WITH INCREASE IN OIL TEMPERATURE OF APPROXIMATELY 25 DEGREES. FOUND NR 1 ENGINE DRIVEN PUMP DEACTIVATED WITH KIT. DRIVE SEAL LINE IN CASE NOT PROPERLY REMOVED AND CAPPED. REPLACED ENGINE DRIVEN PUMP PER BOEING MAINTENANCE MANUAL 29-22-05. PER 72-00-00 CHECKED OIL SCREENS AND CHIP DETECTORS. RESERVICED WITH OIL LEAK CHECK GOOD. NO DISCREPANCIES NOTED, ENGINE RETURNED TO SERVICE.

Part: HYD LINE — HOLE (NR 1 PYLON)

LOST NR 1 HYDRAULIC SYSTEM QUANTITY ON APPROACH. FOUND HOLE ON NR 1 AIR DRIVEN HYDRAULIC PUMP PRESSURE LINE REPLACED LINE AND LEAK CHECKED PRE BOEING M/M 29-11-00. DEACTIVATED NR 1 ENGINE DRIVEN PUMP PER MEL 29-1 DUE TO PUMP OPERATED WITH SUPPLY TO OFF POSITION.

Part: CANOE — HOLE (TE FLAPS)

HOLE IN NR 2 CANOE FWD RT SIDE. SANDED DOWN AREA, FILLED HOLE WITH AERODYNAMIC FILLER, SANDED DOWN AND APPLIED FIBERGLASS OVERLAY AS PER SRM 51-40-07.

Part: MOUNTING RING — CORRODED (FUSELAGE)

CORRODED AND BUCKLED MOUNTING RING, LOW RANGE ALT. BLENDED OUT CORROSION AND REWORKED MOUNTING RING.

Part: PANEL — CRACKED (LT MLG DOOR)

CRACKS AND OBLONG HOLES ON LEFT WING GEAR DOOR CLOSEOUT PANEL. FABRICATED AND INSTALLED LEFT WING GEAR DOOR CLOSEOUT PANEL PER BAC SRM 51-10-02.

Part: TRACK — CRACKED (LT TE MIDFLAP)

CRACK AT FORWARD END OUTBOARD FLANGE OF MIDFLAP TO FOREFLAP OUTBOARD TRACK ON LEFT OUTBOARD FLAP ASSEMBLY. BLENDED OUT DAMAGED AREA PER BAC OHM 57-52-55 AND MM 27-51-04 AND PERFORMED HIGH FREQUENCY EDDY CURRENT INSPECTION PER BAC NDTM PART 6, NO FURTHER CRACKS.

Part: FITTING — CRACKED (RT TE FOREFLAP)

CRACKED ATTACH FITTING ON RIGHT OUTBOARD FOREFLAP INBOARD CARRIAGE. REPLACED ATTACH FITTING PER BAC MM 27-51-05.

Part: CASE RAIL — CRACKED (NR 1 ENGINE)

CRACK AT 10 O'CLOCK ON NR 1 ENGINE TURBINE EXHAUST CASE R-RAIL. WELD REPAIR AND STRESS RELIEF IAW PWA ENGINE MM 72-53-01, REPAIR 14.

Part: TR SLEEVE — DAMAGED (NR 4 ENGINE)

DAMAGE ON TRAILING EDGE INBOARD LOWER SIDE OF NR 4 ENGINE FAN THRUST REVERSER SLEEVE. REPAIRED DAMAGE ON NR 4 ENGINE FAN SLEEVE PER BAC SRM 54-30-03.

Part: SKIN — GOUGED (FUSELAGE)

PUNCTURED AND GOUGED FUSELAGE SKIN AT AFT CENTERLINE INBOARD OF TAIL JACK POINT. REMOVED DAMAGED SKIN, PERFORMED HIGH FREQUENCY EDDY CURRENT INSPECTION PER BAC NDTM PART 6, NO CRACKS. INSTALLED NEW SKIN WITH DOUBLER AND TREATED PER BAC SRM 53-30-03 AND 51-10-02.

Part: CASE RAIL — CRACKED (NR 2 ENGINE)

CRACK ON TURBINE EXHAUST CASE R-RAIL APPROX 10 O'CLOCK ON NR 2 ENGINE. WELD REPAIRED AND STRESS RELIEVED PER PWA ENGINE MANUAL 72-53-01, REPAIR 14.

Part: CASE RAIL — CRACKED (NR 3 ENGINE)

CRACK ON TURBINE EXHAUST CASE S-RAIL APPROX 1700 O'CLOCK ON NR 3 ENGINE. WELD REPAIRED AND STRESS RELIEVED PER PWA ENGINE MANUAL 72-53-01, REPAIR 14.

Part: FITTING — CRACKED (LT MLG BEAM)

CORROSION CRACKING FOUND DURING NDT INSPECTION ON LEFT WING GEAR WALKING BEAM END FITTING. REPLACED LEFT WING GEAR WALKING BEAM END FITTING PER BAC MM 57-15-01.

Part: FAIRING — CRACKED (FUSELAGE)

CRACKED RIGHT FUSELAGE WING TO BODY FAIRING AFT OF BODY GEAR. FIBERGLASS REPAIR APPLIED PER BAC SRM 51-40-09.

Part: DOOR — DELAMINATED (APU INLET)

DELAMINATION ON APU INLET DOOR. REPLACED APU INLET DOOR PER BAC MM 49-15-03.

Part: DOORS — CHAFED (LT MLG)

CHAFING AND TEAR DAMAGE ON LEFT WING GEAR WHEEL WELL DOORS AT AFT ENDS. DAMAGED PARTS REMOVED AND REPLACED PER BAC SRM 51-10-03 AND 51-30-02.

Part: DUCT — CRACKED (NR 2 ENGINE)

CRACKED STARTER PNEUMATIC DUCT ON NR 2 ENGINE. REPLACED DUCT PER BAC MM 36-11-01.

Part: FAIRING — CRACKED (FUSELAGE)

CRACK ON LEFT FUSELAGE BODY FAIRING ABOVE BODY GEAR. REMOVED CRACK AND APPLIED FIBERGLASS FILLERS AND DOUBLERS PER BAC SRM 51-40-15.

Part: PRECOOLER — CRACKED (NR 4 ENGINE)

CRACKED INTERNAL BRACKET ON NR 4 ENGINE PRECOOLER. REPLACED NR 4 ENGINE PRECOOLER PER BAC MM 36-12-01.

Part: FAIRING — CRACKED (FUSELAGE)

DELAMINATED AND CRACKED LEFT FUSELAGE BODY TO WING FAIRING FORWARD OF WING GEAR. REPAIRED FAIRING WITH FIBERGLASS OVERLAYS PER BAC SRM 51-40-15.

Part: FUEL CONTROL — FAILED (NR 4 ENGINE)

NR 4 ENGINE, AFTER POWER SET AND STABLE (1.12 EPR) TAKEOFF ROLL WAS STARTED, WHILE CONTINUING TO SET TAKEOFF POWER, NR 4 ENGINE FLAMED OUT AND TAKEOFF WAS ABORTED. REPLACED FUEL CONTROL UNIT AS PER M/M 73-21-01. REPLACED FUEL PUMP PRECAUTIONARY PER M/M 73-11-01, REPLACED TT2 SENSOR PER M/M 73-21-04 AND TESTED PER M/M 71-00-00 TEST 3, FOUND OK.

Part: ENGINE — OVER TEMP (NR 1)

AFTER ENGINE START FOR TAXI, NR 1 ENGINE SHUT DOWN DUE TO HIGH EGT (NOTE TAIL WIND), DIGITAL RECORDING EGT INDICATOR SHOWS 1100 DEGREES FOR 64 SEC. BORESCOPE INSPECTED COMBUSTION SECTION AND TURBINE SECTIONS PER BOEING M/M 72-00-00. FOUND FUEL NOZZLES, HPT STAGE 1 NGV, 1ST STAGE BLADES, 2ND STAGE BLADES, 3RD STAGE BLADES AND 4TH STAGE BLADES ALL SATISFACTORY. OVER TEMPERATURE VISUAL INSPECTION PER 72-00-00 AND 71-00-00 SATISFACTORY. RUN CHECK AT TAKEOFF POWER EPR 1.45 CHECKED NORMAL PER M/M 71-00-00. REPLACED ENGINE FUEL CONDITION ACTUATOR PRECAUTIONARY PER M/M 76-11-04. ENGINE RELEASED WITH 100 HOUR TIME LIMIT. ENGINE TO BE CHANGED.

Part: WING TIP — CORRODED (RT WING)

LEVEL 1 CORROSION RT WING TIP, UPPER SKIN PANEL IS CORRODED AND DELAMINATED. FABED AND INSTALLED NEW PANEL PER BOEING SRM 51-30-02.

Part: COWL — DELAMINATED (NR 3 ENGINE)

NR 3 ENG O/B FAN COWL DELAMINATED AND DENTED AT 5:00 POSITION. REPAIRED PER BOEING SRM 51-40-06.

Part: SKIN — CRACKED (L 1 DOOR)

L-1 EXTERNAL DOOR SKIN CRACKED AT LOWER FWD CORNER. STOP DRILLED AND FABED REPAIR PER BOEING SRM 52-00-03.

Part: DUCT — CRACKED (NR 3 ENGINE)

NR 3 ENG COMPENSATOR DUCT CRACKED. REMOVED AND REPLACED DUCT PER BOEING SRM 36-11-16.

Part: TIP — DAMAGED (LT HORIZ STAB)

LT HORIZ STAB TIP UPPER T/E METAL TORN. REPAIRED PER BOEING SRM 51-30-02.

Part: EXHAUST SLEEVE — DAMAGED (NR 3 ENGINE)

NR 3 ENG EXHAUST SLEEVE EXTERNAL SKIN TORN BACK ON RT SIDE. REPAIRED PER BOEING SRM 54-34-03.

Part: SKIN — DAMAGED (LT TE MID FLAP)

LT WING I/B MID FLAP L/E TORN AT I/B END. HOT BOND REPAIR PER BOEING SRM 51-40-12.

Part: COWL — CRACKED (NR 1 ENGINE)

NR 1 ENG LT CORE COWL CSD DOOR FRAME IS CRACKED AND GOUGED. FABED DOUBLER AND REPAIRED PER BOEING SRM 51-30-02, 51-10-02.

Part: COWL — DAMAGED (NR 2 ENGINE)

NR 2 I/B CORE COWL AFT TOP CORNER HAS TORN METAL. REPAIRED PER BOEING SRM 51-30-02, 51-10-01.

Part: COWL — CRACKED (NR 4 ENGINE)

NR 4 O/B CORE COWL FWD BOTTOM ALIGNMENT PIN PUSHED BACK AND STRUCTURE CRACKED. REPAIRED PER SRM 51-40-02, 51-30-02.

Part: BRACKET — CRACKED (NR 3 ENGINE)

NR 3 ENG PRECOOLER LT FWD TOP ATTACH BRACKET CRACKED. REMOVED AND REPLACED BRACKET PER MM 70-50-00.

Part: SUPPORT ROD — BROKEN (LT WING)

LT WING FLYING PANEL O/B SUPPORT ROD SHEARED AT LOWER END. REMOVED AND REPLACED ROD ASSY, RIGGED PANEL PER MM 57-22-02.

Part: COWL — CHAFED (NR 2 ENGINE)

NR 2 O/B CORE COWL STIFFENER CHAFING AGAINST PRECOOLER BRACKET. REMOVED AND REPLACED STIFFENER PER BOEING SRM 51-30-02.

Part: STOP PAD — BROKEN (LT MLG DOOR)

LT BODY GEAR DOOR HAS BROKEN STOP PAD BRACKET. REMOVED AND REPLACED STOP PAD BRACKET PER BOEING SRM 51-30-02.

Part: SPAR — CORRODED (LT WING)

LEVEL 1 LT WING L/E SPAR LOWER CHORD CAP HAS LIGHT CORROSION. REMOVED CORROSION WITHIN LIMITS. ALODINED AND PRIMED PER BOEING SRM 57-30-01.

Part: R/S RAIL — CRACKED (NR 1 ENGINE)

NR 1 ENG R AND S RAIL AT 6:00 POSITION HAS RADIAL LIGHTENING HOLE CRACKS. WELDED AND STRESS RELIEVED PER MM 72-53-01.

Part: COWL — CHAFED (NR 1 ENGINE)

NR 1 ENG O/B CORE COWL STIFFENER CHAFED THROUGH. REMOVED AND REPLACED STIFFENER PER BOEING SRM 51-30-02.

Part: BRACKET — CRACKED (NR 3 LE FLAP)

NR 3 L/E DEVICE PDU BRACKET MOUNT ANGLE CRACKED. REPAIRED PER BOEING SRM 51-30-02.

Part: BRACE — DAMAGED (LT/RT PYLON)

NR 2 ENG DIAGONAL BRACE CHAFED FWD END BOTH LT AND RT SIDES. INSPECTED AREA PER SRM 54-40-01 FOUND TO BE WITHIN LIMITS PER ZONE 2, BLENDED AREA PER SRM 54-40-01 C/W EDDY CURRENT INSP NDT MM 51-00-00 OK FOR SERVICE, SHOT PEENED, TREATED AND PAINTED PER SRM 51-40-01.

Part: CADC — FAILED (NR 2)

IN CRUISE AT FLIGHT LEVEL 350, CAPTIAN AND FIRST OFFICER ALTITUDE DIFFERENCE GRADUALLY INCREASED FROM 100 FOOT TO 500 FOOT WITH CAPTAINS ALTIMETER HIGH. REPLACED NR 2 CADC PER BOEING M/M 34-12-01, OPERATIONAL CHECK AND LEAK CHECK NORMAL PER 34-11-00.

Part: ACM — CONTAMINATED (NR 1 PACK)

SMOKE FILLED THE COCKPIT AT TOP OF DESCENT. TURNED AIR CONDITIONING PACKS OFF AND CLOSED ENGINE BLEED AIR VALVES WITH NO EFFECT. SMOKE CLEARED BEFORE LANDING. PERFORMED MAINTENANCE CHECK OF AIR CONDITIONING SYSTEM AND FOUND NR 1 WATER SEPARATOR CONTAMINATED. DEACTIVATED NR 1 A/C PACK AND REACTIVATED NR 2 PACK.

Part: AXLE — FAILED (LT MLG)

FINAL REPORT, AXLE FAILED, SHEARED DURING TRANSIT FUELING AT THE LEFT WING GEAR RIGHT FRONT POSITION NR 2 MAIN. REPLACED THE LEFT WING GEAR TRUCK AND AXLE ASSEMBLY PER BAC MM 32-11-11.

Part: PACK — OIL CONTAMINATED (NR 2)

OIL SMOKE IN THE COCKPIT DURING CRUISE FLIGHT. SOURCE IDENTIFIED AS NR 2 A/C PACK, DEACTIVATED PACK.

Part: EXHAUST PLUG — TORN (NR 4 ENGINE)

NR 4 ENGINE EXHAUST PLUG INTERIOR TORN AND PEELED BACK. REMOVED AND REPLACED PLUG PER BOEING MAINTENANCE MANUAL 78-11-04.

Part: CASCADE VANE — BROKEN (NR 3 ENGINE)

NR 3 ENGINE RIGHT THRUST REVERSER CASCADE VANE AT 4 O'CLOCK POSITION HAS BROKEN VANE. REPAIRED PER BOEING MAINTENANCE MANUAL 78-31-07.

Part: EXHAUST CASE — CRACKED (NR 1 ENGINE)

NR 1 ENGINE S-RAIL AT 6:00 O'CLOCK POSITION HAS A HORIZONTAL CRACK. REPAIRED PER BOEING MAINTENANCE MANUAL 72-53-01.

Part: BRACKET — CRACKED (RT MLG WW)

RIGHT WING GEAR WHEEL WELL BRACKET CRACKED ABOVE WING GEAR DOWN LOCK CYLINDER. REPAIRED PER SRM 51-10-01.

Part: SKIN — CRACKED (NR 2 PYLON)

NR 2 PYLON INBOARD SIDE CRACK IN PREVIOUS REPAIR. BLENDED OUT CRACK PER BOEING SRM 53-30-01, TREATED AND PAINTED PER 51-10-02.

Part: EXHAUST CASE — CRACKED (NR 1 ENGINE)

NR 1 ENGINE R-RAIL AT THE SIX-THIRTY POSITION HAS A HORIZONTAL CRACK. REPAIRED PER BOEING MAINTENANCE MANUAL 72-53-01.

Part: CASCADE VANE — CRACKED (NR 3 ENGINE)

NR 3 ENGINE 4TH CASCADE OUTBOARD SIDE CRACKED. REPAIRED PER BOEING MAINTENANCE MANUAL 78-31-07.

Part: EXHAUST CASE — CRACKED (NR 1 ENGINE)

NR 1 ENGINE S-RAIL AT 12 O'CLOCK POSITION HAS A VERTICAL CRACK. OK FOR 1,000 HOUR REINSPECTION PER BOEING MAINTENANCE MANUAL 72-53-02.

Part: EXHAUST PLUG — DELAMINATED (NR 1 ENGINE)

NR 1 ENGINE EXHAUST PLUG INTERIOR IS DELAMINATED. REMOVED AND REPLACED PER BOEING MAINTENANCE MANUAL 78-11-04.

Part: RIVET — CRACKED (NR 3 PYLON)

CRACKED RIVET ON LOWER SLOT SEAL (NACELLE STATION 180 WATER LINE 124) RIGHT SIDE NR 3 PYLON. REPLACED RIVET PER BOEING SRM 51-30-02.

Part: ENGINE — MALFUNCTIONED (NR 3)

AFTER ENGINE START NR 3 ENGINE OIL QUANTITY DROPPED, OIL PRESSURE LOW AT IDLE POWER, NO OIL OVER TEMP. REMOVED FILTER AND FOUND CARBON DEPOSITS. CLEANED, REINSTALLED, DRAINED OIL, RESERVICED, INSPECTED N2 TACK SHAFT FOR PLAY AND NONE FOUND. PERFORMED ENGINE RUN, ALL PARAMETERS GOOD REFERENCE M/M 71-00-44. THOUGH NEXT FLIGHT NO FURTHER PROBLEMS ENGINE CHANGED PRECAUTIONARY.

Part: ENGINE — MALFUNCTIONED (NR 3)

WHEN THROTTLES REDUCED FOR DESCENT, OIL QUANTITY DROPPED TO ZERO AND PRESSURE DROPPED TO 30 PSI OIL PRESSURE STAYED ABOVE 20 PSI REST OF FLIGHT, AFTER ENGINE SHUT DOWN IAW ALTERNATE PROCEDURES. AFTER SHUT DOWN OIL QUANTITY CAME BACK TO 4.2 GALLONS. RESTARTED OIL PRESSURE OK 44 PSI, THEN OIL QUANTITY DROPPED TO 1 GALLON PRESSURE FLUCTUATED 34 TO 39 PSI. MOTORED ENGINE OIL TANK SERVICED WITH 2 QUARTS OF OIL, CHECKED OIL FILTER, NO CONTAMINATION. CHECKED CHIP DETECTORS, NO CONTAMINATION. REPLACED OIL PRESSURE TRANSMITTER PRECAUTIONARY PER M/M 79-31-00. RUNUP AND ALL PARAMETERS NORMAL PER M/ M 71-00-00. POLAR REPLACED ENGINE LATER DUE TO REPEAT OF PROBLEM.

Part: SKIN — DAMAGED (BS 2598)

DAMAGED SKIN ON AFT FUSELAGE AT BS 2598 FROM S26R TO S42R. REPAIRED PER POLAR AIR MAINTENANCE AUTHORIZATION 5330-12:01.

Part: OVERHEAT SENSOR — MALFUNCTIONED (NR 1 PYLON)

AIR TURNBACK DUE LEFT WING L/E OVERHEAT LIGHT ILLUMINATED DURING CLIMB. LIGHT EXTINGUISHED BY REDUCING THRUST NUMBER 1 ENGINE WITH PYLON VALVE CLOSED. NO PNEUMATIC LEAKS FOUND IN NR 1, NR 2 PYLON OR LEFT WING MANIFOLD. FOUND NR 1 PYLON OVERHEAT DETECTOR INTERMITTENTLY SHORTING. DEACTIVATED PER DISPATCH DEVIATIONS MANUAL. REFERENCE SERVICE BULLETIN 747-26-2066.

Part: FAN BLADES — DAMAGED (NR 1 ENGINE)

DAMAGED NR 1 ENGINE FAN BLADES DUE TO BIRD STRIKE. REPLACED OUT OF LIMIT BLADES AND BLENDED OTHER DAMAGED FAN BLADES PER BAC MM 72-31-02.

Part: RUB STRIP — MISSING (NR1 ENG FAN CASE)

MISSING NR 1 ENGINE FAN CASE RUB STRIP SECTIONS DUE TO BIRD STRIKE. REPAIRED PER BAC MM 72-31-04.

Part: FAN EXH STATORS — DAMAGED (NR 1 ENGINE)

DAMAGED NR 1 ENGINE FAN EXHAUST STATORS DUE TO BIRD STRIKE. REPAIRED PER BAC MM 72-31-05.

Part: NOSE COWL LINER — DELAMINATED (NR 1 ENGINE)

DELAMINATED AND DAMAGED NR 1 ENGINE NOSE COWL ACCOUSTICAL INNER LINER DUE TO BIRD STRIKE. REMOVED AND REPLACED NOSE COWL PER BAC MM 71-11-01.

Part: SHEAR TIE — CRACKED (BS 1000)

CRACKED SHEAR TIE ON TIE DOWN TRACK BS 1000 WL 195 RBL 75. REPLACED PART PER BOEING SRM 51-10-03 PART MANUFACTURED PER DRAWING 64-53-1096.

Part: SHEAR TIE — CRACKED (BS 1000)

CRACKED SHEAR TIE ON TIE DOWN TRACK BS 1000 WL 195 LBL 57. REPLACED PART PER BOEING SRM 51-10-03 PART MANUFACTURED PER DRAWING 64-53-1096.

Part: SHEAR TIE — CRACKED (BS 1000)

CRACKED SHEAR TIE ON TIE DOWN TRACK BS 1000 WL 195 RBL 57. REPLACED PART PER BOEING SRM 51-10-03 PART MANUFACTURED PER DRAWING 64-53-1096.

Part: SPAR WEB — CRACKED (FSS 668)

CRACKED LEFT WING FRONT SPAR WEB FS 668 TO 697. REPAIRED IN ACCORDANCE WITH BOEING DRAWING 112U8040.

Part: SPAR WEB — CRACKED (FSS 680)

CRACKED RIGHT WING FRONT SPAR WEB FS 668 TO 697. REPAIRED IN ACCORDANCE WITH BOEING DRAWING 112U8040.

Part: PRESS DECK — CORRODED (BS 1416)

LEVEL 1 CORROSION FASTENER HEAD BS 1416 RBL 127 ON PRESSURE DECK WEB. CORROSION REMOVED PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, REPROTECTED PER 51-10-02.

Part: PANEL — CORRODED (RT WING)

BOOST PUMP CUTOUT AT PANEL LOCATION 645CB HAS LEVEL ONE SURFACE CORROSION. CORROSION REMOVED IAW SRM 51-10-07, FOUND WITHIN LIMITS IAW SRM 57-30-03. REPROTECTED AFTER INSPECTION CLEARANCE IAW SRM 51-10-02.

Part: SKIN — CORRODED (BS 1352)

LEVEL 1 CORROSION RIGHT BODY GEAR WHEEL WELL PRESSURE WEB SKIN BS 1352 RBL 84 ABOVE ANTI-SKID MODULE. CORROSION REMOVED PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, REPROTECTED PER 51-10-02.

Part: SPAR CHORD — CORRODED (CENTER TANK)

FOUND FRONT SPAR LOWER CHORD CORRODED IN CENTER TANK DRY BAY AT RBL 120. CORROSION REMOVED IAW SRM 51-10-01 AND FOUND WITHIN LIMITS IAW SRM 57-10-01. REPROTECTED AFTER INSPECTION CLEARANCE IAW SRM 51-10-02.

Part: SKIN — CORRODED (RT WING)

LEVEL 1 CORROSION AT RIGHT WING BOOST PUMP CUTOUT WBL 383. CORROSION REMOVED PER BOEING SRM 51-10-01, WITHIN LIMITS PER 57-30-03, REPROTECTED PER 51-10-02.

Part: SPAR — CORRODED (WING)

CORROSION ON LOWER CHORD OF FRONT SPAR IN CENTER TANK DRY BAY RBL 77. CORROSION REMOVED PER BAC SRM 51-10-01 AND AREA REPROTECTED PER BAC SRM 51-10-02.

Part: SPAR — CORRODED (CENTER WING)

LEVEL 1 CORROSION ON FRONT SPAR LOWER CHORD IN CENTER TANK DRY BAY AT LBL77. REMOVED CORROSION IAW BOEING SRM 51-10-01 WITHIN LIMITS PER 53-10-01 PROTECTED PER 51-10-01.

Part: SPAR — CORRODED (CENTER WING)

LEVEL 1 CORROSION CENTER WING FRONT SPAR UPPER CHORD DRY BAY FROM RBL 90 TO RBL 115. CORROSION REMOVED PER BOEING SRM 51-10-01, WITHIN LIMITS PER 57-10-01, REPROTECTED PER 51-10-02.

Part: KEEL BEAM — CORRODED (BS 1007)

LEVEL 1 CORROSION KEEL BEAM BOX RIGHT UPPER CHORD AT BS 1007 WL 115. REMOVED CORROSION PER BOEING SRM 51-10-01 WITHIN LIMITS PER BOEING SRM 53-30-10 AND TREATED PER BOEING SRM 51-10-02.

Part: SPAR CHORD — CORRODED (CENTER TANK)

FRONT SPAR LOWER CHORD FOUND CORRODED IN CENTER TANK DRY BAY RBL 77. LEVEL ONE CORROSION REMOVED AND FOUND WITHIN LIMITS IAW SRM 57-10-01. TREATED AND PRIMED IAW SRM 57-20-01.

Part: KEEL BEAM — CORRODED (BS 1005)

LEVEL 1 CORROSION BS 1005 WL 100 RIGHT KEEL BEAM BOW. REMOVED CORROSION PER BOEING SRM 51-10-01 WITHIN LIMITS PER BOEING SRM 53-30-10 AND TREATED PER BOEING SRM 51-10-02.

Part: STRINGER — CORRODED (CENTER WING)

LEVEL 1 CORROSION CENTER WING DRY BAY UPPER SKIN STRINGER 32C AT RBL 75. REMOVED CORROSION PER BOEING SRM 51-10-01 WITHIN LIMITS PER 53-10-01 PROTECTED PER 51-10-02.

Part: STRINGER — CORRODED (CENTER WING)

LEVEL 1 CORROSION CENTER WING DRY BAY UPPER SKIN STRINGER S29C AT RBL 90. REMOVED CORROSION PER BOEING SRM 51-10-01 WITHIN LIMITS PER 53-10-01, REPROTECTED PER 51-10-02.

Part: STRINGER — CORRODED (CENTER WING)

LEVEL 1 CORROSION CENTER TANK DRY-BAY UPPER SKIN STRINGER S30C AT BBL 0 TO RBL 10. REMOVED CORROSION PER BOEING SRM 51-10-01 WITHIN LIMITS PER 53-10-01 PROTECTED PER 51-10-02.

Part: SKIN — CORRODED (CENTER WING)

LEVEL 1 CORROSION CENTER WING DRY BAY UPPER SKIN AT STRINGER 33C RBL 108 WL 190. REMOVED CORROSION PER BOEING SRM 51-10-01 WITHIN LIMITS PER 53-10-01 PROTECTED PER 51-10-02.

Part: SKIN — CORRODED (CENTER WING)

LEVEL 1 CORROSION CENTER WING DRY BAY UPPER SKIN AT STRINGER 29C AT LBL 75. REMOVED CORROSION PER BOEING SRM 51-10-01 WITHIN LIMITS PER 53-10-01 PROTECTED PER 51-10-02.

Part: SKIN — CORRODED (CENTER WING)

LEVEL 1 CORROSION CENTER WING DRY BAY UPPER SKIN STRINGER 33C LBL 108 WL 190. REMOVED CORROSION PER BOEING SRM 51-10-01 WITHIN LIMITS PER 53-10-01 PROTECTED PER 51-10-02.

Part: STRINGER — CORRODED (CENTER WING)

LEVEL 1 CORROSION ON CENTER WING DRY BAY UPPER SKIN STRINGER 30C AT RBL 55 TO RBL 95. REMOVED CORROSION PER BOEING SRM 51-10-01 WITHIN LIMITS PER 53-10-01, REPROTECTED PER 51-10-02.

Part: SKIN — CORRODED (CENTER WING)

LEVEL 1 CORROSION CENTER WING DRY BAY UPPER SKIN AT STRINGER S32C ON LOWER FLANGE FROM RBL 84 TO 59. REMOVED CORROSION PER BOEING SRM 51-10-01 WITHIN LIMITS PER 53-10-01, REPROTECTED PER 51-10-02.

Part: SPAR — CORRODED (CENTER WING)

LEVEL 1 CORROSION FRONT SPAR UPPER CHORD IN CENTER TANK DRY BAY FROM LBL 105 TO 115. REMOVED CORROSION PER BOEING SRM 51-10-01 WITHIN LIMITS PER 53-10-01, REPROTECTED PER 51-10-02.

Part: SKIN — CORRODED (CENTER WING)

LEVEL 1 CORROSION CENTER WING DRY BAY UPPER SKIN AT STRINGER 31C AT LBL 30 TO LBL 75. REMOVED CORROSION PER BOEING SRM 51-10-01 WITHIN LIMITS PER 53-10-01 PROTECTED PER 51-10-02.

Part: FLOOR BEAM — CORRODED (BS 460)

LEVEL 1 CORROSION UPPER DECK FLOOR BEAM LOWER T-SECTION OF FALSE BEAM JUST OUTBOARD OF CIRCULAR STAIR CUTOUT STR 460 RBL 0 TO RBL 30. CORROSION REMOVED PER BOEING SRM 51-10-01 WITHIN LIMITS AND PROTECTED PER 51-10-02.

Part: FLOOR BEAM — CORRODED (BS 440)

LEVEL 1 CORROSION ON UPPER DECK FLOOR BEAM LOWER-T BS 440 RBL 50. REMOVED CORROSION PER BOEING SRM 51-10-01 WITHIN LIMITS PER 53-10-01 PROTECTED PER 51-10-02.

Part: BULKHEAD — CORRODED (BS 1350)

LEVEL 1 CORROSION AT 1350 BULKHEAD LBL 118 WL 168 WHERE HYDRAULIC LINES PASS THROUGH BULKHEAD. CORROSION REMOVED PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, REPROTECTED PER 51-10-02.

Part: SKIN — CORRODED (BS 780)

LEVEL 1 CORROSION ON EXTERNAL SURFACE OF SKIN PANEL BS 780 BBL 0 AROUND RIVET HEADS. REMOVED CORROSION PER BOEING SRM 51-10-01 WITHIN LIMITS PER 53-10-01 PROTECTED PER 51-10-02.

Part: SKIN — CORRODED (BS 760)

LEVEL 1 CORROSION ON EXTERNAL SURFACE OF SKIN PANEL BS 760 BBL 0 TO BBL 12R AROUND RIVET HEADS. REMOVED CORROSION PER BOEING SRM 51-10-01 WITHIN LIMITS PER 53-10-01 PROTECTED PER 51-10-02.

Part: COUPLING — LOOSE (NR 2 PYLON)

DURING MAINTENANCE, FOUND FUEL LEAK INBOARD NR 2 PYLON. INSPECTED DRY BAY AREA ABOVE NR 2 PYLON PER MM 28-11-00. FOUND FUEL FEED MANIFOLD COUPLING LOOSE AT SPAR. TIGHTENED AND SECURED COUPLING, PRESSURE CHECK GOOD.

Part: CHIP DETECTOR — BROKEN (NR 3 ENGINE)

FOUND NR 3 ENGINE ANGLE GEARBOX CHIP DETECTOR BROKEN. REPLACED CHIP DETECTOR IAW MM 72-61-01.

Part: DOOR CUTOUT — CORRODED (CARGO COMPT)

INSPECTION OF THE AFT CARGO DOOR CUTOUT REVEALED LEVEL 2 CORROSION AT THE AFT LOWER CORNER. REMOVED EXISTING FASTENERS AND SKIN, FABRICATED FILLER AND DOUBLER, INSTALLED REPAIR PARTS IAW POLAR AIR CARGO MAINTENANCE AUTHORIZATION 5330-08:01. PERFORMED HFEC INSPECTION TO ASSURE STRUCTURE CORROSION AND DAMAGE FREE IAW SRM 51-10-01.

Part: CHANNEL — CRACKED (RT MLG DOOR)

FOUND RIGHT HAND BODY GEAR FLYING DOOR AFT ATTACH HINGE AND BOLTS LOOSE AND STRUCTURE CRACKED. REMOVED DOOR, FABBED NEW CHANNEL, INSTALLED IAW SRM 51-30-02.

Part: ACCESS PANEL — DAMAGED (FUSELAGE)

FOUND HOLE IN FUSELAGE ACCESS PANEL FORWARD OF RIGHT HAND PACK LOUVER DOOR. REMOVED DAMAGED AREA, POTTED SAME AND APPLIED DOUBLERS IAW SRM 51-40-02.

Part: SKIN — CORRODED (BS 1840)

LOWER FUSELAGE SKIN BULGED WITH TWO FASTENERS POPPED, STA 1840 AT STR 44. REMOVED AND CLEANED LEVEL TWO CORROSION FROM SKIN AND SURROUNDING STRUCTURE IAW SRM 51-10-06. REPAIRED IAW SRM 53-30-03.

Part: DUCT CLAMP — BROKEN (NR 1 ENGINE)

NR 1 ENGINE STARTER PNEUMATIC DUCT HAS A BROKEN 'V' BAND CLAMP AT STARTER. REMOVED AND REPLACED 'V' CLAMP AT STARTER IAW MM 36-11-01.

Part: FAIRING — MISSING TIP (NR 3 PYLON)

NUMBER 3 ENGINE FORWARD FAIRING LEADING EDGE TIP IS MISSING. REPLACED MISSING TIP IAW MM 54-51-01.

Part: FRAME — CRACKED (NR 2 ENGINE COWL)

NR 2 ENGINE INBOARD CORE COWL LOWER FRAME CRACKED AND TORN AT NR 5 LATCH U-BOLT, GUIDE PIN PUSHED BACK. REMOVED AND REPLACED SECTION OF FRAME IAW SRM 51-10-01 AND 51-10-02.

Part: DOOR CUTOUT — CORRODED (BULK CARGO DOOR)

INSPECTION OF BULK CARGO DOOR CUTOUT REVEALED EVIDENCE OF LEVEL 2 CORROSION AT AFT LOWER CORNER. REMOVED EXISTING DOUBLER AND SKIN, FABRICATED FILLER AND TRIPLER, INSTALLED SAME, ALL IAW POLAR AIR CARGO MAINTENANCE AUTHORIZATION 5330-07:01. PERFORMED HFEC INSPECTION TO ASSURE STRUCTURE CORROSION AND DAMAGE FREE IAW SRM 51-10-01.

Part: ACCESS PANEL — DELAMINATED (RT WING)

FOUND LOWER RIGHT WING ACCESS PANEL DELAMINATED JUST OUTBOARD OF NR 5 FLAP TRACK FAIRING. REMOVED DAMAGED AREA AND APPLIED FIBERGLASS OVERLAYS IAW SRM 51-40-15.

Part: FLOOR PANEL — DAMAGED (AFT CARGO COMPT)

FOUND AFT CARGO COMPARTMENT RIGHT HAND WALKWAY HAS A HOLE JUST FWD OF ENTRY DOOR. REPAIRED HOLE IN CARGO FLOOR IAW SRM 51-40-02.

Part: SHIELD — BROKEN (AFT CARGO DOOR)

FOUND AFT CARGO DOOR AFT FIBERGLASS SHIELD FOR PRESSURE DOOR BROKEN AWAY. INSTALLED NEW SHIELD IAW MM 52-34-00.

Part: SKIN — LOOSE (LT TE MIDFLAP)

LEFT WING INBOARD FLAP MID FLAP FIBERGLASS PEELING LOOSE ON LOWER SURFACE AT FRONT SPAR APPROX 2 FEET FROM INBOARD END. REMOVED DAMAGED AREA, POTTED SAME AND APPLIED FIBERGLASS OVERLAYS IAW SRM 51-40-09.

Part: PRECOOLER — CRACKED (NR 2 ENGINE)

FOUND NR 2 ENGINE PRECOOLER CRACKED AT FORWARD LOWER INBOARD CORNER. REMOVED WELD REPAIR IAW BAC 5975, USING 34755 TIG ROD AND REPLACED SAME. LEAK CHECKED ENGINE IAW MM 36-21-01.

Part: SUPPORT — BROKEN (CARGO COMPT)

AFT CARGO COMPARTMENT LEFT SIDE FORWARD FRAME SUPPORTS ARE BROKEN AWAY FROM FRAME ON ANGLED SIDEWALL. REMOVED AND REPLACED TENSION STRAP SUPPORTS IAW SRM 51-30-03.

Part: SKIN — CORRODED (BS 1960)

LOWER FUSELAGE SKIN BULGED AND SEVERAL PULLED RIVETS FS 1960 BETWEEN S-42R AND 43R. REMOVED LEVEL TWO CORROSION IAW SRM 51-10-01. REPAIRED FUSELAGE SRM 53-30-03.

Part: SKIN — LOOSE (LT TE MIDFLAP)

LEFT WING INBOARD FLAP MIDFLAP LOWER SURFACE HAS FILLER PULLING LOOSE INBOARD OF INBOARD CANOE. REMOVED DAMAGED AREA, POTTED SAME AND APPLIED FIBERGLASS OVERLAYS IAW SRM 51-40-09.

Part: FAIRING — MISSING (RT PACK DOOR)

RIGHT HAND PACK LOUVER DOOR ACCESS PANEL SECTION OF FAIRING MISSING AT FORWARD INBOARD END OF DOOR. INSTALLED NEW FAIRING IAW SRM 51-30-02.

Part: FLOOR PANEL — PUNCTURED (CARGO COMPT)

FOUND HOLE IN BULK CARGO PIT AT FORWARD RIGHT HAND END. REPAIRED HOLE IN FLOOR IAW SRM 51-40-02.

Part: RAIL SUPPORT — TORN (BS 560)

FOUND FORWARD CARGO COMPARTMENT SIDE RAIL SUPPORT TORN AT STA 560. REMOVED AND REPLACED SUPPORT IAW SRM 51-30-02 AND 51-10-01.

Part: LINING — DAMAGED (CARGO COMPT)

BULK CARGO INTERIOR CORNER DAMAGED AT FORWARD LOWER SIDE OF OPENING. REPAIRED DOOR CORNER IAW SRM 51-40-09.

Part: PANEL — ERODED (LT WING L/E)

FOUND TOP OF LEFT WING ERODED ALONG LEADING EDGE OF FIBERGLASS PANELS, SEVERAL AREAS AT LEADING EDGE OF WING. REPAIRED LEADING EDGE IAW SRM 51-40-15.

Part: ROLLER TRAY — CRACKED (BS 1800)

AT APPROX STA 1800 FOUND 2 ROLLER TRAYS CRACKED, RBL 30 AND RBL 48. REMOVED AND REPLACED CRACKED TRAYS IAW SRM 51-30-02.

Part: PS4 LINE — LOOSE (NR 1 ENGINE)

AFTER AIRCRAFT WAS PUSHED OFF BLOCKS, UNABLE TO START NR 1 ENGINE, HANGING WITH NO ACCELERATION. INSPECTED AND FOUND BURNER PRESSURE SENSE PS4 LINE LOOSE AT FCU. TIGHTENED SAME, ENGINE START AND OPERATION NORMAL IAW MM 71-00-00.

Part: FUEL CONTROL — INOPERATIVE (NR 4 ENGINE)

ON TAXI FOR DEPARTURE, NR 4 ENGINE FLAMED OUT. ACFT RETURNED TO GATE. REMOVED AND REPLACED FUEL CONTROL IAW MM 73-21-01. REMOVED AND REPLACED FUEL PUMP IAW MM 73-11-01. FUEL PUMP PART NR 705300, SERIAL NR 2027, TSI 2541.

Part: O-RING — DAMAGED (NR 3 ENGINE)

ON DEPARTURE CLIMB-OUT PASSING 15,000 FEET, NR 3 ENGINE OIL PRESSURE LIGHT BEGAN FLICKERING. OIL PRESS WAS AT 50 PSI PLUS OR MINUS 10 PSI AND DECREASING. OIL QUANTITY INDICATED 1.2 GALLONS. WHEN OIL PRESSURE DECREASED TO 35 PSI, ENGINE WAS SHUT DOWN. ACCOMPLISHED ONE ENGINE INOP DESCENT, APPROACH AND LANDING. APPROACH AND LANDING WERE NORMAL. NO DAMAGE NOTED TO AIRCRAFT ON INSPECTION AFTER LANDING. FOUND EDP SHAFT O-RING SEAL DAMAGED. REMOVED AND REPLACED SAME IAW MM 29-11-05. WINDMILL INSPECTION COMPLETED PER 72-00-00, IDLE POWER LEAK CHECK GOOD. ENGINE RUNUP PER 71-00-00.

Part: SKIN — CRACKED (NR 2 PYLON)

DURING SCHEDULED ENGINE CHANGE, FOUND NUMEROUS CRACKS IN NR 2 PYLON BOTTOM PLATE. REPAIRED PER SRM 54-10-03, FIG. 3.

Part: WARNING LIGHT — INOPERATIVE (FE PANEL)

RETURNED TO BLOCKS DUE TO ADP AND EDP LOW PRESSURE WARNING LIGHTS AND ADP RUN LIGHTS INOP AT FEO PANEL AFTER ENGINE START. CYCLED BETWEEN APU AND ENGINE GENERATORS AND LIGHTS OPERATED NORMALLY.

Part: SKIN — DAMAGED (BS 1800-1810)

GROUND DAMAGE AFT FUSELAGE AT STA 1800 TO 1810 STR 34R TO 35R SHOWS DENT AND .75 INCH CRACK BETWEEN AFT CARGO DOOR AND DOOR CONTROL SWITCH. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER PER SRM 53-30-03. PRESSURIZED, LEAK CHECK OK.

Part: SEAT TRACK — CRACKED (COPILOT SEAT)

FOUND CO-PILOT'S AFT OUTBOARD SEAT TRACK CRACKED AT AFT END. MAINTENANCE CARRYOVER ITEM 857016, TRACK TO BE REPLACED IAW MM 25-11-01.

Part: SEAT TRACK — CRACKED (COPILOT SEAT)

FOUND CO-PILOT'S OUTBOARD FORWARD SEAT TRACK CRACKED AT AFT END. TRANSFERRED TO MAINTENANCE CARRYOVER ITEM 857016, TRACK TO BE REPLACED IAW MM 25-11-01.

Part: COMPRESSOR — STALLED (NR 3 ENGINE)

HKG - UPON APPLYING MAX TAKEOFF POWER, NR 3 ENGINE COMPRESSOR STALLED AT 1.40 EPR. HEARD A LOUD BANG, EGT PEGGED MAX TEMP INDICATOR POINTER AT BOTTOM OF GAUGE 1,100 DEGREES. ABORTED TAKEOFF AT APPROXIMATELY 5 KNOTS, RETARDED ENGINE TO IDLE, SHUTDOWN ENGINE IAW ENGINE STALL CHECKLIST. EGT EXCEEDED 915 DEGREES FOR APPROX 3 SECONDS. BORESCOPED ENGINE, NO DAMAGE FOUND. PRECAUTIONARY REPLACED TT2 SENSOR, PERFORMED FULL POWER RUNUP, ALL INDICATIONS NORMAL. ENGINE NOW 80 HOUR LIMITED.

Part: R RAIL — CRACKED (NR 4 ENGINE)

NR 4 ENGINE R-RAIL IS CRACKED AT FIVE THIRTY POSITION. REPAIRED RAIL IAW MM 72-53-01.

Part: DOOR — CRACKED (NLG)

NOSE LANDING GEAR SERVICE PANEL DOOR CRACKED. REPAIRED DAMAGE AND REINSTALLED IAW 52-40-00.

Part: CORNER — TORN (NR 1 ENGINE)

NR 3 ENGINE INBOARD COWL OUTBOARD FORWARD TOP CORNER ON REPAIR TORN. REMOVED DAMAGED REPAIR, REPAIRED TORN DOUBLER IAW SRM 54-30-02. INSTALLED DOUBLER IAW SRM 51-10-01 AND 54-30-02.

Part: LATCH — CRACKED (NR 1 ENGINE)

NR 1 ENGINE LEFT HAND CORE COWL THIRD LATCH FROM LEADING EDGE HAS CRACKED REPAIR. FABRICATED AND INSTALLED DOUBLER IAW SRM 54-30-01.

Part: SKIRT FAIRING — CRACKED (NR 2 PYLON)

NR 2 ENG OUTBOARD SKIRT FAIRING AFT PANEL CRACKED. REMOVED DAMAGED PANEL AND ADJACENT SPLICE IAW SRM 51-10-01. FABRICATED AND INSTALLED NEW PARTS IAW SRM 51-10-01

Part: SKIRT FAIRING — CRACKED (NR 2 PYLON)

NR 1 ENGINE SKIRT FAIRING AT DRAIN TUBE CUTOUT HOLE AREA CRACKED. BLENDED DAMAGE IAW SRM 51-10-01.

Part: FAIRING — CRACKED (FS 1000)

FOUND CRACK IN FUSELAGE FAIRING PANEL BETWEEN A/C BAYS AT FORWARD ADF PANEL, APPROX STA 1000. STOP DRILLED CRACK IAW SRM 51-10-01. HFEC INSPECTED AND DETERMINED CRACK ENDS AT STOP DRILL IAW MM 51-00-00.

Part: CLIP — BROKEN (NR 1 ENGINE)

NR 1 ENGINE LEFT HAND CORE COWL HAS BROKEN FRAME SUPPORT CLIP AT PRE-COOLER EXHAUST CUTOUT. FABRICATED NEW SUPPORT CLIP AND INSTALLED IAW SRM 51-10-01.

Part: FRAME — CRACKED (NR 1 ENGINE)

NR 1 ENGINE LT CORE COWL HAS CRACKED FRAME LOWER SURFACE. REMOVED DAMAGED AREA, REPAIRED IAW SRM 54-14-03. REINSTALLED REPAIRED AREA IAW SRM 54-14-03.

Part: FIRESHIELD — DELAMINATED (NR 1 ENGINE)

NR 1 ENGINE RT CORE COWL UPPER FAIRING LOWER SKIN DELAMINATED. REMOVED DAMAGED FIRESHIELD, FABRICATED NEW COUPLER AND INSTALLED IAW SRM 54-30-03.

Part: ANGLE — CRACKED (NR 2 ENGINE)

NR 2 ENGINE INBOARD CORE COWL FORWARD LOCK LATCH CUTOUT ANGLE CRACKED. INSTALLED NEW DOUBLER AND ANGLE IAW SRM 51-30-02.

Part: EXHAUST FUNNEL — CRACKED (NR 2 ENGINE)

NR 2 ENGINE OUTBOARD CORE COWL INNER EXHAUST FUNNEL CRACKED. REPAIRED IAW BAC59-75 PER STEP 4 AND 5.

Part: SKIRT FAIRING — CRACKED (NR 2 PYLON)

NR 1 ENGINE OUTBOARD SKIRT FAIRING FORWARD PANEL CRACKED WITH 2 EACH FASTENERS MISSING. REMOVED DAMAGED PANEL IAW SRM 51-10-01, FABRICATED AND INSTALLED NEW PANEL IAW 51-10-01.

Part: PANEL — MALFUNCTIONED (VHF 1/2)

WHILE IN POSITION AND HOLDING FOR TAKEOFF, EXPERIENCED FAILURE OF VHF NR 1 AND VHF NR 2. DISCONNECTED ELECTRONICS BAY AUDIO SELECTOR PANEL PLACARDED AND DISPATCHED.

Part: GEAR BOX — FROZEN (NR 4 ENGINE)

A/C PUSHED OUT FOR ENGINE START, NR 4 ENGINE WOULD NOT START. FOUND THAT GEAR BOX WOULD NOT TURN. ENGINE REPLACED.

Part: ENGINE — FAILED (NR 4)

ON CLIMBOUT FROM HKG PASSING THROUGH FL 230, NR 4 ENGINE SURGED WITH EGT GOING TO 940 C, ALL PARAMATERS INDICATED FAILED ENGINE. SECURED ENGINE AS PER EMERGENCY CHECK LIST. ON GROUND INSPECTION FOUND METAL IN TAIL PIPE. ENGINE REPLACED.

Part: GASKET — WORN (NR 4 ENGINE)

PRECAUTIONARY SHUTDOWN DUE TO DECREASING OIL PRESSURE, DROPPED BELOW 30 PSI WITH INCREASED BREATHER TEMPERATURE, ENGINE OIL PRESSURE LOW LIGHT ON WINDMILL TIME 1 PLUS 20 OIL PRESSURE ALWAYS 10 TO 15 PSI. FOUND OIL LEAK AT NR 1 AND NR 2 OIL BREATHER LINE. REPLACED GASKET, LEAK CHECK OK.

Part: SUPPORT — CORRODED (BS 1800)

CORROSION UNDER NUTPLATE AFT LOWER CARGO STA 1800 TO STA 1810, FLOOR SUPPORT CHANNEL AT RBL 30. REMOVED, FABRICATED, AND INSTALLED FLOOR SUPPORT CHANNEL PER BOEING SRM 51-10-01, 51-12-00, AND 51-30-02.

Part: FLOOR BEAM — DAMAGED (BS 1780)

BS 1780 LOWER AFT CARGO FLOOR BEAM CAP IS DAMAGED (TORN) AT LBL 30. REPLACED SECTION OF CAP ANGLE PER BOEING SRM 51-10-01, 51-12-00, AND 51-30-02.

Part: BUSHING — WORN (LT MLG DOOR)

LEFT MAIN WING LANDING GEAR LOWER DOOR FORWARD HINGE BADLY WORN. REMOVED AND REPLACED BUSHINGS PER BOEING MAINTENANCE MANUAL 32-12-00.

Part: ANGLE — CORRODED (BS 1820)

CORROSION AT AFT LOWER CARGO FLOOR SUPPORT ANGLE UNDER NUT PLATE BS 1820, RBL 30. REMOVED AND REPLACED FLOOR SUPPORT ANGLE PER BOEING SRM 51-10-01, 51-12-00, 51-30-02.

Part: SUPPORT — BROKEN (BS 1800)

FLOOR SUPPORT CHANNEL BROKEN AT AFT LOWER CARGO COMPARTMENT BS 1800, LBL 30. REMOVED, FABRICATED, AND INSTALLED SUPPORT CHANNEL PER BOEING SRM 51-10-01, 51-12-00, 51-30-02.

Part: BUSHINGS — WORN (RT MLG DOOR)

RIGHT BODY GEAR OUTBOARD DOOR ACTUATOR UPPER ATTACH BUSHING BADLY WORN. REPLACED BUSHINGS PER OVERHAUL MANUAL 20-50-03. INSTALLED ACTUATOR PER MAINTENACE MANUAL 32-33-27.

Part: RIVETS — LOOSE (NR 1 ENG EXHAUST)

NR 1 ENGINE EXHAUST SLEEVE HAS PULLED THROUGH, LOOSE AND MISSING FASTENERS ON THE TRAILING EDGE FROM 10 O'CLOCK TO 2 O'CLOCK POSTION. REMOVED AND REPLACED FASTENERS PER BOEING SRM 51-30-02.

Part: FLOOR BEAM — TORN (BS 1780)

BS 1780 LBL 30 FLOOR SUPORT WEB IS TORN ABOUT 6 INCHES BELOW FLOOR BEAM AFT CARGO COMPARTMENT. REPAIRED PER BOEING SRM 51-40-02.

Part: RIVETS — LOOSE (RT MLG DOOR)

RIGHT BODY GEAR INBOARD DOOR INNER SKIN LOOSE AT 2 ROWS OF FASTENERS. REMOVED AND REPLACED FASTENERS PER BOEING SRM 51-30-02.

Part: FLOOR BEAM — CRACKED (BS 1800)

BS 1800, RBL 50, FLOOR BEAM CAP ANGLE IS CRACKED ON FORWARD SIDE OUTBOARD END AFT LOWER CARGO. REPLACED SECTION OF FLOOR BEAM CAP PER BOEING SRM 51-10-01, P 18, 51-12-00, AND 5130-02.

Part: LADDER — CRACKED (CREW ENTRY)

CREW ENTRY LADDER, TOP RUNG CRACKED LEFT AND RIGHT SIDES. WELD REPAIRED PER BOEING SRM 51-30-02.

Part: SEAL LAND — BENT (FWD CARGO DOOR)

FORWARD CARGO BAY DOOR FORWARD SEAL LAND 10 INCHES AND 30 INCHES UP FROM INBOARD BOTTOM CORNER IS BENT. STRAIGHTENED PER BOEING SRM 51-40-03.

Part: FLOOR — DAMAGED (BS 1820)

ONE INCH HOLE IN AFT CARGO COMPARTMENT AT BS 1820 TO BS 1780, LBL 30. REPAIRED PER BOEING SRM 51-40-02 AND SRM 51-30-02.

Part: STRAP — CRACKED (NR 3L DOOR)

CRACK WITH STOP DRILL HOLE ON STRAP ON INTERNAL STRUCTURE REAR FRAME AT NR 3 LEFT ENTRY DOOR. REPAIRED PER BOEING SRM 51-40-03 AND 51-30-02.

Part: SHUT OFF VALVE — FAILED (NR 2 HYD SYSTEM)

NR 2 STABILIZER TRIM HYDRAULIC CONTROL CIRCUIT BREAKER POPPED. REMOVED AND REPLACED SYSTEM NR 2 HYDRAULIC SHUTOFF VALVE ACTUATOR ON STABILIZER TRIM HYDRAULIC MODULE.

Part: FUEL LINE — LEAKING (NR 2 PYLON)

JFK - DURING WALK-AROUND INSPECTION, FUEL WAS FOUND LEAKING FROM INBD SIDE OF NR 2 PYLON ABOVE ENGINE. REMOVED L/E GAP COVER PANEL. FOUND FUEL FEED TUBE LEAKING DUE TO A HOLE CHAFED IN TUBE BY THE PNEUMATIC DUCT CLAMP. REMOVED TUBE AND ACCOMPLISHED A TEMPORARY REPAIR IAW MM 20-11-05. LINE REINSTALLED AND PRESSURE CHECKED IAW 28-22-00. LINE WILL BE REPLACED WITHIN 250 HOURS PER MM. PNEUMATIC DUCT CLAMP HAD ROTATED AGAINST FUEL TUBE BECAUSE ANTI-ROTATION SPRINGS WERE MISSING FROM CLAMP. FCD ISSUED TO CHECK OTHER PYLONS FOR SIMILAR CONDITION.