N850FT

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 83,615 hrs · 20,774 cycles

DELAMINATION FOUND ON L/WING INBOARD T/E FLAP AFT FLAP UPPER SURFACE WBL-236. REPAIRED PER SRM 51-40-26.

Part: STRUCTURE — CRACKED (MLG DOOR) · airframe 83,615 hrs · 20,774 cycles

CRACK FOUND ON RBJ - I/B W/W DOOR INBOARD EDGE. REPAIRED PER SRM 51-10-01 & 51-30-02.

Part: SKIN — CORRODED (NR 7 SPOILER) · airframe 83,615 hrs · 20,774 cycles

LEVEL 1 CORROSION FOUND ON NR 7 SPOILER. BOND REPAIR PER SRM 51-40-06.

Part: SKIN — DELAMINATED (NR 1 SPOILER) · airframe 83,615 hrs · 20,774 cycles

DELAMINATION FOUND ON NR 1 SPOILER. REPAIRED PER SRM 51-40-06.

Part: WIRE — BROKEN (CABIN) · airframe 83,238 hrs · 20,691 cycles

RIGHT UPPER DECK EMERGENCY LIGHT ADJACENT TO CREW EXIT LIGHT INOP. REPAIRED BROKEN WIRE. OPS CHECK GOOD IAW 20-10-13.

Part: SKIN — PUNCTURED (FUSELAGE) · airframe 83,173 hrs · 20,674 cycles

A/C DAMAGED BY GROUND HANDLER AT STA 1780, LT SIDE WL 130 BS 1788 STRINGER 35 LEFT TO STRINGER 36 LEFT EXTERIOR SKIN PUNCTURED. REMOVED AFT CARGO LINER AT BS 1780, REMOVED DAMAGED SKIN, INSTALLED DOUBLER PER SRM 53-30-03 FIG 1, INSTALLED AFT CARGO LINER.

Part: LIGHT — WILL NOT TEST (CABIN)

ON GROUND, N1 LIGHT IN FORWARD P-2 PANEL WILL NOT TEST. TROUBLESHOOTING CARRIED OUT PER PAC WDM 77-12-11 AND WDM 33-11-01. COMPONENTS CHECKED AND REFITTED. DEFECT SELF-RECTIFIED. OPS CHECK SATISFACTORY. (X)

Part: ACTUATOR — FAILED (WING GEAR) · airframe 82,981 hrs · 20,630 cycles

LT WING GEAR ALT ROTARY ACTUATOR (MOTOR) FAILED FUNCTIONAL CHECK. LT WING ROTARY ACTUATOR (ALT) REPLACED PER MM 32-35-01.

Part: FRAME — CRACKED (FUSELAGE) · airframe 82,981 hrs · 20,630 cycles

STA 940 FRAME CRACKED AROUND STRINGER 34R AND VERTICAL POST. FRAME REPAIRED PER SRM 53-10-04 FIG 52.

Part: SKIN — DAMAGED (LT WING) · airframe 82,981 hrs · 20,630 cycles

LEFT WING FIXED T/E UPPER PANEL REMOVED DUE TO WATER CONTAMINATION. REPAIRED AND REPLACED PER SRM 51-40-12, 51-40-09 & 57-22-01.

Part: SEAT TRACK — CRACKED (BS 735)

SEAT TRACK INTERCOSTAL FOUND CRACKED, BS 735 BL 25L. REMOVED AND REPLACED INTERCOSTAL PER SRM 51-10-01.

Part: SUPPORT — CRACKED (BS 1970-1980)

BULK CARGO FLOOR SUPPORT FOUND CRACKED BL 35L, BS 1970 TO 1980. REPAIRED AS PER SRM 51-40-03 FIGURE 1.

Part: ANGLE — CRACKED (BS 805)

FRAME SUPPORT ANGLE FOUND CRACKED, BS 805L, WL 199.5. REMOVED AND REPLACED ANGLE AS PER SRM 51-10-01 AND 51-30-02.

Part: STRINGER — CORRODED (BS 1955-1963)

LEVEL 2 CORROSION FOUND IN BULK CARGO COMPARTMENT BS 1955-1963L BL 5-7 STR 51. REPLACED AND SPLICED STRINGER PER SRM 51-10-01 PG 18 AND SRWS914578.

Part: FRAME — CRACKED (BS 1840)

FRAME FOUND CRACKED AT BS 1840, STR 12R. REPAIRED PER SRM 53-10-04 FIGURE 1.

Part: STRINGER — CRACKED (BS 2178)

STRINGER FOUND CRACKED, MAIN DECK FUSELAGE, BS 2178 STR 2R. REPAIRED PER HAECO REPAIR SCHEME 53-61-33872 AND SRWS 914638.

Part: FRAME — CRACKED (BS 1670)

FRAME SUPPORT WEB FOUND CRACKED, MAIN DECK FUSELAGE BS 1670, STR 17-19R. REPAIRED PER HAECO REPAIR SCHEME 53-61-33872.

Part: ANGLE — CRACKED (BS 805)

FRAME SUPPORT ANGLE FOUND CRACKED, BS 805R, WL 199.5. REMOVED AND REPLACED ANGLE AS PER SRM 51-10-01 AND 51-30-02.

Part: KEEL BEAM — CORRODED (BS 990-1000)

LEVEL ONE CORROSION FOUND ON RIGHT KEEL BEAM CHORD, BS 990-1000 BL 9R. REPAIRED PER HAECO REPAIR SCHEME AND BOEING TELEX PAO-HKG-98-0198RE.

Part: TIE — CORRODED (BS 860)

LEVEL ONE CORROSION FOUND BELOW FLOOR SHEAR FITTING TIE, BS 860, BL L47 - R47. CORROSION REMOVED AND AREA REPAIRED IAW SRM 53-10-04 FIG 3A.

Part: FRAME — CRACKED (BS 1680)

FRAME SUPPORT WEB FOUND CRACKED, MAIN DECK FUSELAGE BS 1680, STR 23-24R. REPAIRED PER SRM 53-10-04 FIGURE 84 AND HAECO REPAIR SRWS 914630.

Part: FRAME — CRACKED (BS 1860)

FRAME FOUND DEEPLY CHAFED AND CRACKED, BS 1860 STR 12R. FRAME REPAIRED PER SRM 53-10-04 FIGURE 1.

Part: STRINGER — CORRODED (BS 1955-1963)

LEVEL TWO CORROSION FOUND ON STRINGER 51, BS 1955 TO 1963, BL 5 - 7L. REPLACED AND SPLICED STRINGER AS PER SRM 51-10-01 PAGE 18.

Part: SUPPORT — CRACKED (BS 1980)

BULK CARGO FLOOR SUPPORT FOUND CRACKED BL 60L, BS 1980. REPAIRED AS PER SRM 51-40-03 FIGURE 1.

Part: SKIN — CORRODED (BS 1600-2060)

LEVEL ONE CORROSION FOUND AT LAP SEAM, BS 1600 TO 2060, STR 12L. BLENDED AREA, AREA REPROTECTED AS PER SRM 51-10-01.

Part: INTERCOSTAL — CRACKED (BS 2350)

LEVEL ONE CORROSION AND CRACKS FOUND AT HAT SECTION BOX INTERCOSTALS, BS 2350, LBL 11 - RBL 11. CORROSION REMOVED, INTERCOSTALS REPAIRED AND REPLACES IAW SRM 53-10-01 AND 51-10-01.

Part: STRINGER — CRACKED (BS 2178)

STRINGER FOUND CRACKED, MAIN DECK FUSELAGE BS 2178, STR 3R. REPAIRED PER HAECO REPAIR SCHEME 53-61-33872 AND SRWS 914637.

Part: FRAME — CRACKED (BS 1760)

FRAME FOUND CRACKED AND DEFORMED AT INBOARD CHORD, BS 1760 STRINGER 10-11R. REPAIRED PER SRM 53-10-04 FIGURE 1.

Part: KEEL BEAM — CORRODED (BS 990-1000)

LEVEL ONE CORROSION FOUND AT KEEL BEAM FORWARD LEFT HAND INNER CHORD, BS 990 TO 1000, BL 8L. BLENDED AREA AND AREA REPROTECTED PER SRM 53-10-01 AND 51-10-01.

Part: CLIP — CRACKED (BS 260)

NOSE LANDING GEAR PRESSURE DECK TO FLOORBEAM, TWO EACH CLIPS FOUND CRACKED, BS 260, LBL 12 AND 24. REMOVED AND REPLACED CLIPS PER SRM 51-10-01 PAGE 18.

Part: FRAME — CRACKED (FUSELAGE)

FRAME SUPPORT WEB FOUND CRACKED, MAIN DECK FUSELAGE STRINGER 17-19L. REPAIRED PER HAECO REPAIR SCHEME 53-61-33872.

Part: FRAME — CRACKED (BS 600)

FRAME RADIUS FOUND CRACKED BS 600, STR 19L. FRAME REPAIRED AS PER HAECO REPAIR SCHEME 53-22-33837.

Part: STRINGER — CRACKED (BS 255)

STRINGER FOUND CRACKED ON SPLICE, BS 255 STRINGER 39L. SPLICE REMOVED AND REPLACED AS PER SRM 51-10-01 PAGE 18.

Part: STRAP — CRACKED (NR 2 DOORWAY)

DOOR FRAME INNER CHORD STRAP FOUND CRACKED, NR 2 MAIN DECK DOOR, STRINGER 18L. REPAIRED PER HAECO REPAIR SCHEME 53-21-338 AND SRWS 914646.

Part: SKIN — CHAFED (NR 4 PYLON)

NUMBER FOUR PYLON OUTBOARD SKIRT FOUND CHAFED ON INSIDE SURFACE. REPAIRED PER SRM 54-30-03 FIGURE 35 AND 36.

Part: SUPPORT — CRACKED (BS 2063)

BULK CARGO FLOOR SUPPORT FOUND CRACKED BL 50L, BS 2063. REPAIRED AS PER SRM 51-40-03 FIGURE 1.

Part: SHEAR TIE — CRACKED (BS 2320)

SHEAR TIE FOUND CRACKED BS 2320, STR 18 TO 19R. REPAIRED AS PER SRM 51-10-04 FIGURE 4.

Part: PANEL — DELAMINATED (RT WING)

STRESS PANEL NR 688JT FOUND DELAMINATED. HOT BOND REPAIRED AS PER SRM 51-40-06 FIGURE 17A.

Part: SEAT TRACK — CRACKED (BS 570)

SEAT TRACK INTERCOSTAL SUPPORT FOUND CRACKED BS 570, BL 32R. REMOVED AND REPLACED AS PER SRM 51-10-01.

Part: SUPPORT — CRACKED (BS 2000)

BULK CARGO FLOOR SUPPORT FOUND CRACKED BL 40R, BS 2000. REPAIRED AS PER SRM 51-40-03 FIGURE 1.

Part: FRAME — CRACKED (L3 DOORWAY)

FORWARD FRAME UPPER HINGE CUTOUT CRACKED, MAIN DECK L3 DOOR. REPAIRED AS PER HAECO REPAIR ORDER R52-11-33839.

Part: SUPPORT — CRACKED (BS1935-1940)

BULK CARGO FLOOR SUPPORT FOUND CRACKED BL 20R, BS 1935 TO 1940. REPAIRED AS PER SRM 51-40-03 FIGURE 2.

Part: FLANGE — CRACKED (NR 2 ENGINE)

FOUND RADIAL OD LIGHTENING HOLE CRACK, R FLANGE AT 10:00 POSITION. WELD REPAIRED PER MM 72-53-01 REPAIR 22.

Part: INTERCOSTAL — BROKEN (BS 610-615)

FLOOR PANEL INTERCOSTAL SUPPORTS (TWO EACH) FOUND BROKEN, FWD CARGO COMPARTMENT BS 610-615, BL 40L. REPLACED SUPPORTS AS PER SRM 51-10-01.

Part: ANGLE — CRACKED (COCKPIT DOORWAY)

HINGE SUPPORT FOUND CRACKED AT DOOR ATTACH AREA, COCKPIT ESCAPE HATCH. REPLACED HINGE SUPPORT ANGLE PER MM 52-21-00.

Part: SHEAR TIE — CRACKED (BS 2160)

SHEAR TIE FOUND CRACKED BS 2160, STR 21-22R. REMOVED AND REPLACED TIE AS PER SRM 51-10-01 PAGE 18.

Part: SHEAR TIE — CORRODED (BS 1680)

LEVEL ONE CORROSION FOUND ON AFT CARGO COMPARTMENT SHEAR TIE, BS 1680, STR 50-51R. REPAIRED AS PER SRM 53-10-03 FIGURE 3.

Part: WEB — CRACKED (BS 2230)

FRAME SUPPORT WEB FOUND CRACKED BS 2230, STR 174. STOP DRILLED, NDT INSPECTED AND REPAIRED AS PER SRM 51-10-04 FIGURE 71.

Part: INTERCOSTAL — CRACKED (BS 420-440)

FRAME INTERCOSTAL FOUND CRACKED BS 420 TO 440, STR 8-9R. REMOVED AND REPLACED AS PER SRM 51-10-01 PAGE 18.

Part: FAIRING — DELAMINATED (BS 850)

LEFT FUSELAGE BODY FAIRING AT STA 850 IS DELAMINATED. REPAIRED PANEL PER SRM 51-40-07.

Part: FAIRING — DELAMINATED (LT WING ROOT)

LEFT HAND UNDERWING ROOT PANEL DELAMINATED. REMOVED PANEL AND REPAIRED PANEL AND INSTALLED PER SRM 51-40-09.

Part: FAIRING — DELAMINATED (BS 900)

LEFT FUSELAGE BODY FAIRING AT STA 900 IS DELAMINATED. REPAIRED PANEL PER SRM 51-40-07.

Part: SKIN — DAMAGED (RT TE FLAP)

RIGHT OUTBOARD FLAP, MID FLAP LOWER SKIN JUST OUTBOARD OF JACK SCREW HAS A HOLE IN THE SKIN. REMOVED, SANDED DAMAGED AREA, PREPARED FOR BONDING, POTTED DAMAGED .5 INCH DIA APPLIED 3 PLY FIBERGLASS LAY-UP IAW SRM 51-40-09.

Part: SKIN — LOOSE (NR 3 PYLON)

#3 ENGINE PYLON EXTERNAL SKIN OUTBOARD LOWER HALF SKIRT PANEL HAS NUMEROUS LOOSE AND WORKING FASTENERS. REMOVED AND REPLACED FASTENERS PER 51-10-01.

Part: SILL — DAMAGED (CARGO DOORWAY)

INNER MAIN CARGO DOOR SILL PROTECTOR DAMAGED. REMOVED AND REPLACED SILL PROTECTOR PER SRM 51-30-02.

Part: WATER SEPARATOR — CRACKED (NR 2)

NR 2 WATER SEPARATOR DELAMINATED AND CRACKED. REMOVED AND REPLACED NR 2 WATER SEPARATOR PER MM 21-51-05.

Part: ISOLATION VALVE — INOPERATIVE (LEFT)

LOW DUCT PRESS ON LEFT WING DURING START. ISOLATION VALVE DOES NOT CLOSE. REMOVE AND REPLACED ISOLATION VALVE. OPS CHECK GOOD IAW MM 36-11-07.

Part: PANEL — CRACKED (LT TE FLAP)

LT WING OUTBD FLAP COVE LIP PANEL CRACKED. REPAIRED AND APPLIED FIBERGLASS OVERLAY PER SRM 51-40-09.

Part: DOOR — DELAMINATED (LT MLG)

LT WING GEAR FLYING DOOR DELAMINATED OUTER AFT CORNER. REPAIRED BY CUTTING OUT DAMAGE AND INSTALLING NEW FIBERGLASS OVERLAYS PER SRM 51-40-06.

Part: SKIN — DELAMINATED (NR 6 SPOILER)

NR 6 SPOILER INBD EDGE SEPARATED AND HAS 2 AREAS OF DELAMINATION. REPAIRED WITH FIBERGLASS AND BONDED PER SRM 51-40-06.

Part: SKIN — CRACKED (FUSELAGE)

NR 3 INBD C/C TOP SIDE AFT END EXTERIOR SKIN CRACKED. REPAIRED PER SRM 54-10-03.

Part: SKIN — MISREPAIRED (NR 3 SPOILER)

NR 3 SPOILER HAS POSSIBLE INCORRECT REPAIR TO UPPER SURFACE. REPAIRED IN ACCORDANCE WITH SRM 51-40-06.

Part: PANEL — DELAMINATED (LT WING)

LT WING UPPER TRAILING EDGE, FIXED PANEL DELAMINATED FWD OF SPOILER NR 5. SANDED AREA, REMOVED DAMAGED OUTER PANEL INST FIBERGLASS FILLER AND OVERLAY, BONDED PER SRM 51-40-15.

Part: SILL — CORROSION (CARGO DOORWAY)

AFT CARGO DOOR SERRATED PLATE 3, 4, 5 AND 8 HAS CORROSION ON DOOR SILL AREA. REMOVED CORROSION PER SRM 51-10-01.

Part: PANEL — DELAMINATION (LT WING)

LT WING TOP FIXED PANEL IN FRONT OF SPOILER NR 5 OUTER HINGE PANEL DELAMINATION. CUT OUT DAMAGED AREA. REMOVED WATER CONTAMINATION AND APPLIED FIBERGLASS OVERLAY PER SRM 51-40-15.

Part: PANEL — CRACKED (RT TE FLAP)

RT WING OUTBD FLAP COVE LIP PANEL HAS CRACK. REMOVED DAMAGE AREA, POTTED CRACKED HONEYCOMB, APPLIED FIBERGLASS FILLER AND OVERLAY PER SRM 51-40-15.

Part: FAIRING — CRACKED (BS 1460-1520)

FUSELAGE LT BODY FAIRING STA 1460-1520 JUST AFT LT BODY WHEEL WELL CRACKED AT 2 PLACES. REMOVED AND REPAIRED PANEL PER SRM 51-40-15.

Part: INTERCOSTAL — CRACKED (BS 1590)

AFT CARGO COMPARTMENT APPROX STA 1590 LBL 30 SUB FLOOR INTERCOSTAL BENT AND CRACKED. INSTALLED NEW FABRICATED INTERCOSTAL WEB ASSY.

Part: SKIN — DELAMINATED (LT WING SPOILER)

NR 5 SPOILER PANEL DELAMINATED. REPLACED SPOILER PANEL PER BOEING M/M 27-62-01.

Part: TIRE — FAILED (LT MLG)

ON TAKEOFF ROLL, 2 LEFT AFT BODY GEAR TIRES FAILED. REPLACED 2 FAILED TIRE AND WHEEL ASSEMBLIES AND OPPOSITE PAIR OF TIRE AND WHEEL ASSEMBLIES PER M/M 32-45-01. REPLACED NR 7 BRAKE PRECAUTIONARY PER M/M 32-41-15. PERFORMED CONDITIONAL INSPECTION PER M/M 05-51-34. REPLACED ANTI-SKID MODULE PRECAUTIONARY PER M/M 32-42-02. ADDITIONAL DAMAGE TO BODY GEAR DOOR CONNECTING ROD, LEFT BODY GEAR OUTBOARD DOOR HINGE, LEFT BODY GEAR DOOR CONNECTING ROD, LEFT BODY GEAR WIRING HARNESS, FLAP TORQUE TUBE, LEFT BODY GEAR HYDRAULIC LINES, AND FLAP HYDRAULIC RETURN LINE. REPLACED PER M/M.

Part: PRECOOLER — CRACKED (NR 3 ENGINE)

CRACK IN NR 3 ENG PRE-COOLER, AFT OF HIGH STAGE BLEED CONNECTION. WELDED CRACK IAW PW 72-53-01.

Part: FAIRING — DAMAGE (RT TE FLAP)

DAMAGE TO RT WING NR 8 FAIRING CANOE O/B SIDE. REPAIRED PER MAE EA 47-5720-15-A0299.

Part: PANEL — CRACKED (RT WING TE)

CRACK ON RIGHT WING LOWER TRAILING EDGE PANEL OUT BOARD OF INBOARD SPOILER. STOP DRILLED CRACK AND APPLIED FIBERGLASS OVERLAYS PER BOEING 51-40-09.

Part: SUPPORT — DAMAGED (CARGO COMPT)

DAMAGED CEILING SUPPORT STRUCTURE IN THE BULK CARGO COMPARTMENT. FABRICATED AND INSTALLED CEILING SUPPORT STRUCTURE PER BOEING SRM 51-40-10 AND 51-10-01.

Part: SKIN — DELAMINATED (RT TE MIDFLAP)

DELAMINATED PREVIOUS REPAIR ON RIGHT OUTBOARD MID FLAP. POTTED CORE AND APPLIED FIBERGLASS OVERLAYS PER BOEING SRM 51-40-09.

Part: REFUEL PANEL — DELAMINATED (LT WING)

DELAMINATED PREVIOUS REPAIR AT ATTACH POINT FOR LEFT WING INBOARD REFUEL PANEL. REPAIRED PER BOEING SRM 51-40-09.

Part: PANEL — CRACKED (LT WING)

CRACK ON PREVIOUS REPAIR ON LEFT WING UPPER PANEL. REPAIRED BY POTTING CORE AND APPLYING FIBERGLASS OVERLAYS PER BOEING SRM 51-40-09.

Part: BRACKET — CORRODED (RT WING TE)

LEVEL 1 CORROSION ON RIGHT WING TRAILING EDGE SUPPORT ROD ATTACH BRACKET ON OUTBOARD END OF FALSE SPAR. REMOVED CORROSION AND TREATED PER BOEING SRM 51-10-01.

Part: BRACE — BROKEN (RT WING L/E)

BROKEN RIGHT WING LEADING EDGE SUPPORT BRACE. FABRICATED AND REPLACED SUPPORT BRACE PER BOEING SRM 57-21-00.

Part: SKIN — SPLIT (RT AILERON)

SPLIT ON RIGHT OUTBOARD AILERON TRAILING EDGE. REPAIRED USING POTTING AND FIBERGLASS OVERLAYS PER BOEING SRM 51-40-09.

Part: COWL FAIRING — CRACKED (NR 3 ENGINE)

CRACK IN NR 3 ENGINE FAN COWL ATTACH (SADDLE) FAIRING AND CHAFE ANGLE. FABRICATED AND REPLACED FAIRING SKIN AND CHAFE ANGLE PER BOEING SRM 51-30-02.

Part: CLIP — CRACKED (NR 3 PYLON)

CRACK ON NR 3 PYLON UPPER CLIP NEAR WING LEADING EDGE. FABRICATED AND INSTALLED CLIP PER BOEING SRM 51-30-02.

Part: CLOSEOUT PANEL — CRACKED (L1 DOORWAY)

CRACK IN FIBERGLASS CLOSE OUT PANEL FOR FUSELAGE SKIN AT UPPER FORWARD CORNER - L1 DOOR FRAME. REPAIRED WITH FIBERGLASS OVERLAYS PER BOEING SRM 51-40-09.

Part: FLANGE — CRACKED (NR 3 ENGINE)

CRACK ON Q-FLANGE OF NR 3 ENGINE TURBINE EXHAUST CASE AT 1:30 O'CLOCK. WELD REPAIR MADE PER BOEING PROCESS 5975. INSPECTED WELD PER BOEING SOPM 20-20-02.

Part: SKIN — DENTED (LT WING LE)

DENT IN LEFT WING LEADING EDGE INBOARD OF INBOARD LANDING LIGHT. VISUAL INSPECTION AND HIGH FREQUENCY EDDY CURRENT CONFIRMED NO CRACK. DENT FOUND TO BE WITHIN ALLOWABLE LIMITS PER BOEING SRM 57-30-01.

Part: WING TIP — DAMAGE (RT WING)

DAMAGED OUTBOARD AFT CORNER ON THE RIGHT WING TIP. REMOVED DAMAGE AND REPAIRED PER BOEING SRM 51-40-09.

Part: FORMER — GOUGED (NR 3 PY;ON)

GOUGED NR 3 PYLON FORWARD LOWER FORMER. BLENDED OUT GOUGE PER BOEING SRM 54-10-01.

Part: FORMER — GOUGED (NR 3 PYLON)

GOUGED NR 3 PYLON FORMER FORWARD OF PYLON VALVE. BLENDED OUT GOUGE PER BOEING SRM 51-10-06.

Part: TIRE — FAILED (LT MLG)

ABORTED TAKEOFF DUE TO APPARENT TIRE FAILURE. FOUND NR 5 AND NR 6 TIRES FAILED. REPLACED NR 5 , NR 6, NR 7 AND NR 8 TIRE AND WHEEL ASSEMBLIES PER BOEING M/M 32-45-01. COMPLIED WITH CONDITIONAL INSPECTION PER M/M 5-51-25. SERVICED MLG STRUTS PER M/M 32-10-00 LEFT WLG STRUT LOW. FOUND LEFT BODY GEAR SHOCK STRUT OUTBOARD DOOR LINKAGE ROD DAMAGED, REPLACED PER M/M 32-14-06. PERFORMED BRAKE RELEASE CHECK PER M/M 32-40-00, ALL CHECKED GOOD.

Part: ALTIMETER — STICKING (RT COCKPIT)

ON DESCENT, FIRST OFFICER'S ALTIMETER STICKING FOR APPROXIMATELY 500 FT. REMOVED AND REPLACED ALTIMETER PER BOEING M/M 34-13-04 AND OPERATIONAL CHECKED PER M/M 34-17-04.

Part: PANEL — DAMAGED (RT WING)

DAMAGED RIGHT WING ROOT LEADING EDGE PANEL. REPAIRED WITH FIBERGLASS OVERLAYS PER BAC SRM 51-40-09.

Part: FIRE BOTTLE — CRACKED (NR 1 ENGINE)

CRACKED MOUNTING LUG ON NR 1 ENGINE RIGHT FIRE BOTTLE. REPLACED NR 1 ENGINE RIGHT FIRE BOTTLE PER BAC MM 26-21-03.

Part: SKIN — PUNCTURED (LT TE FOREFLAP)

PUNCTURE IN LOWER SURFACE OF LEFT INBOARD FORE FLAP. REPAIRED WITH FIBERGLASS OVERLAY PER BAC 51-40-15.

Part: DOOR — DELAMINATED (RT MLG)

DELAMINATION OF PREVIOUS REPAIR ON RIGHT WING GEAR STRUT DOOR. REPAIRED PER BAC SRM 51-40-06.

Part: PANEL — DAMAGED (NR 3 SPOILER)

DAMAGED ON NR 3 SPOILER PANEL. REPAIRED WITH FILLER AND DOUBLER PER BAC SRM 51-40-06.

Part: ANGLE — CORRODED (RT LAVATORY)

LEVEL 2 CORROSION ON LOWER T-ANGLE AROUND LAV PAN AT RIGHT BL 40. FABRICATED AND INSTALLED NEW T-ANGLE PER BAC SRM 51-40-04.

Part: DOOR — DELAMINATED (RT MLG)

DELAMINATION ON RIGHT WING GEAR FLYING DOOR. REPAIRED PER BAC SRM 51-40-06.

Part: PANEL — CRACKED (WS 807)

CRACK ON BOTTOM OF RIGHT WING LEADING EDGE PANEL AT WS 807. REPAIRED PER BAC SRM 51-40-09.

Part: TRUNNION — CORRODED (LT MLG)

LEVEL 1 CORROSION ON THE LEFT BODY GEAR TRUNNION. REMOVED LIGHT SURFACE CORROSION PER BAC OHM 32-00-05.

Part: PANEL — CORRODED (BS 1241)

LEVEL 1 CORROSION ON INBOARD FUSELAGE PANEL FORWARD OF RIGHT WING GEAR. REMOVED CORROSION AND RETREATED PANEL PER BAC SRM 51-10-06 AND 51-10-02.

Part: FAIRING — DELAMINATED (NR 194FR)

DELAMINATION ON RIGHT AFT FAIRING PANEL 194FR. REPAIRED PER BAC SRM 51-40-09.

Part: PANEL — DELAMINATED (RT WING)

DELAMINATION ON RIGHT WING PANEL 621FT. REPAIRED PER BAC SRM 51-40-12.

Part: FAIRING — DELAMINATED (NR 194DR)

DELAMINATION ON RIGHT AFT FAIRING PANEL 194DR. REPAIRED PER BAC SRM 51-40-09.

Part: HINGE PANEL — CORRODED (NLG DOOR)

BULGED HINGE PANEL ON LEFT NOSE LANDING GEAR STRUT DOOR AFT INBOARD CORNER. FOUND LOOSE FASTENERS AND LEVEL 1 CORROSION. REMOVED CORROSION, RETREATED AND CLOSED PER BAC SRM 51-10-01, 51-10-02 AND 51-30-00.

Part: SKIN — CORRODED (BS 1963)

BULGED SKIN AT BS 1963, BL 26. LAP SEAM OPENED, FOUND ONLY LEVEL 1 SURFACE CORROSION. REMOVED CORROSION, RETREATED AND CLOSED PER BAC SRM 51-10-01 AND 51-10-02.

Part: BRACE — DAMAGED (NR 1 PYLON)

NR 1 PYLON I/B DIAGONAL BRACE CHAFED FWD END. INSP AREA PER BOEING SRM 54-40-01 ZONE 3 FOUND TO BE WITHIN LIMITS, EDDY CURRENT C/W, NO CRACKS FOUND PER NDT 54-40-07 PART 6. BLENDED OUT AREA, FLAT PEENED AREA, TREATED AND PAINTED PER BOEING SRM 51-10-01 AND 54-40-01.

Part: BRACKET — DAMAGED (NR 4 PYLON)

NR 4 PYLON RT SIDE DIAGONAL BRACE CHAFE MARK FROM 1ST STUD BRACKET. INSP AREA FOUND OK FOR SERVICE PER BOEING SRM 54-40-01, ZONE 3 EDDY CURRENT C/W PER NDT 54-40-04 PART 6, NO CRACKS NOTED. BLENDED OUT AREA, FLAT PEENED AREA, TREATED AND PAINTED AS PER BOEING SRM 51-10-01 AND 54-40-01.

Part: BRACE — DAMAGED (NR 1 PYLON)

NR 1 PYLON O/B DIAGONAL BRACE CHAFED FWD END. INSP AREA PER BOEING SRM 54-40-01 ZONE 3 TO BE WITHIN LIMITS, EDDY CURRENT C/W, NO CRACKS FOUND PER NDT 50-40-07 PART 6. BLENDED OUT AREA, FLAT PEENED AREA, TREATED AND PAINTED AS PER BOEING SRM 51-10-01 AND 54-40-01.

Part: TRANSFER VALVE — LEAKING (RUDDER)

ON CLIMBOUT, NR 3 HYDRAULIC QUANTITY WENT TO 0. SYSTEM SHUTDOWN AS PER ABNORMAL CHECK LIST. FOUND UPPER RUDDER TRANSFER VALVE LEAKING FROM VALVE ITSELF. REPLACED VALVE ASSEMBLY, LEAK CHECKED AND OPERATIONAL CHECKED PER 27-21-16.

Part: CADC — MALFUNCTIONED (E/E COMPT)

NUMBER 1 AND NUMBER 3 INS TAS AND WIND DIRECTION BLANK AND/OR FLASHING MANY DIFFERENT TRUE AIR SPEEDS AND WIND DIRECTION AND SPEEDS. NUMBER 1 INS WOULD NOT NAVIGATE CORRECTLY. NUMBER 2 INS ERROR RATE 5 MILES PER HOUR. REPLACED NR 1 CADC PER MAINTENANCE MANUAL 34-12-01 BITE TEST/FUNCTIONAL CHECKED PER 34-12-00. REPLACED NUMBER 2 INU PER MAINTENANCE MANUAL 34-41-03, OPERATIONAL CHECK PER 34-41-00.

Part: PANEL — DELAMINATED (LT TE FOREFLAP)

DELAMINATED PANEL LEFT WING INBOARD TRAILING EDGE FORE FLAP. REPLACED PANEL PER BOEING SRM 51-10-01.

Part: SKIN — CORRODED (WS 1437-1453)

LEVEL 1 CORROSION AND NON-STANDARD REPAIRS ON LOWER WING LEADING EDGE SKIN PANEL AT WS 1437.25 AND 1453.35. REPAIRED PER BOEING SRM 57-30-30.

Part: SPAR WEB — CORRODED (WS 1237-1246.35)

LEVEL 1 CORROSION LEFT WING FRONT SPAR WEB BETWEEN WS 1237.05 AND 1246.35 JUST ABOVE LOWER CHORD. CORROSION REMOVED AND FOUND WITHIN LIMITS PER BOEING SRM 57-10-01.

Part: SPAR — CORROSION (WS 938.45-964.56)

LEVEL 1 CORROSION ON LEFT WING FRONT SPAR BETWEEN WS 938.45 AND 964.56 BESIDE VERTICAL STIFFENER. BLENDED CORROSION FOUND WITHIN LIMITS PER BOEING SRM 57-10-01 FIG. 1.

Part: LINK FITTING — CORRODED (RT TE FLAP)

LEVEL 1 CORROSION RIGHT INBOARD FLAP INBOARD SPINDLE NR 5 AFT LINK FITTING BOLT HOLES CORRODED. REPAIRED PER BOEING TELEX 32-9430.

Part: SPAR — CORRODED (WS 732.5)

LEVEL 1 CORROSION LEFT WING FRONT SPAR MID-SECTION ON WEB BY VERTICAL STIFFENER LES 732.56. BLENDED CORROSION FOUND WITHIN LIMITS PER BOEING SRM 57-10-01 FIG. 1.

Part: SPAR — CORRODED (WS 728.56-802.5)

LEVEL 1 CORROSION ON LEFT WING FRONT SPAR WEB BETWEEN WS 782.56 AND 802.5 AT THE TOP CHORD. BLENDED CORROSION FOUND WITHIN LIMITS PER BOEING SRM 57-10-01 FIG. 1.

Part: SKIN — CORRODED (WS 1357-1402)

LEVEL 1 CORROSION LEFT WING LOWER SKIN UPPER SURFACE AT WS 1357, 1373, 1385 1393 AND 1402. CORROSION REMOVED AND FOUND WITHIN LIMITS PER BOEING SRM 57-30-01.

Part: SKIN — CORRODED (LT WING)

LEVEL 1 CORROSION ON LEFT WING UPPER SKIN BELOW FIBERGLASS STRIP BETWEEN LEADING EDGE STRUCTURE AND SKIN IN THE FOLLOWING AREAS, BETWEEN WS 1246.35 AND 1267.65, OUTBOARD OF WS 1293.15, BETWEEN 1318.65 AND 1339.75, AND BETWEEN WS 1349.29 AND 1365.25. BLENDED CORROSION FOUND WITHIN LIMITS PER BOEING SRM 57-30-01 FIG. 1.

Part: FAIRING FRAME — CORRODED (BS 1480)

LEVEL 2 CORROSION, ON AFT BELLY FAIRING FRAME AT CENTER LINE JUST AFT OF KEEL BEAM AT BS 1480. FAIRING FRAME REMOVED, MANUFACTURED AND REINSTALLED AS PER SAMPLE BOEING SRM 53-50-04.

Part: INTERCOSTAL — CORRODED (BS 510)

LEVEL 1 CORROSION FOUND ON INTERCOSTAL AT BS 510 LBL 30 ON UPPER CHORD. REMOVED CORROSION WITHIN LIMITS PER BOEING SRM 51-10-01.

Part: SKIN — DAMAGED (FUSELAGE)

AT FS 2412, FORWARD OF STABILIZER JACK SCREW ACCESS DOOR, SKIN DISPLAYS EVIDENCE OF BULGING AROUND FASTENER HEADS. FUSELAGE SKIN EXTERNAL REPAIR DONE IAW BOEING SRM 53-30-03.

Part: SKIN — CORRODED (RT WING)

LEVEL 1 CORROSION RIGHT WING UPPER SKIN OUTBOARD OF INBOARD FIXED TRAILING EDGE PANEL. BLENDED OUT CORROSION PER BOEING SRM 51-10-01.

Part: SKIN — CORRODED (RT WING)

LEVEL 1 CORROSION ON RIGHT WING UPPER SKIN OUTBOARD OF INBOARD FIXED TRAILING EDGE PANEL AT PREVIOUSLY BLENDED OUT AREA. BLENDED OUT PER BOEING SRM 51-10-01 WITHIN LIMITS.

Part: KEEL BEAM — CORRODED (BS 1241-1480)

LEVEL 1 CORROSION, ON KEEL BEAM BS 1241 TO 1480, 4 LOCATIONS. BLENDED AREAS FOUND WITHIN LIMITS AND RETREATED PER BOEING SRM 51-10-01 AND 51-10-02.

Part: BRACKET — CORRODED (BS 1320)

LEVEL 2 CORROSION, HINGE BRACKET BS 1320 KEEL BEAM AREA RIGHT SIDE. REPLACED HINGE BRACKET PER BOEING SRM 53-10-22 FIG 17.

Part: INTERCOSTAL — CORRODED (BS 1468)

LEVEL 2 CORROSION, LATERAL INTERCOSTAL BEAM BS 1468 KEEL BEAM AREA. REPLACED PART PER BOEING SRM 51-30-02.

Part: KEEL BEAM — CORRODED (BS 1241-1480)

LEVEL 1 CORROSION FOUND ON KEEL BEAM AREA BETWEEN STA 1241 TO STA 1480, 4 LOCATIONS. STA 1270 LT, STA 1340, STA 1420 AND STA 1440. AREAS BLENDED, CLEANED, ALODINED AND PRIMERED. FOUND WITHIN LIMITS AS PER BOEING SRM 53-10-01.

Part: SKIN — CORRODED (WS 1312-1556)

LEVEL 1 CORROSION ON RIGHT WING LOWER SKIN JUST FORWARD OF FRONT SPAR AT WING WS 1312, 1556, 1440 AND 1504. BLENDED CORROSION FOUND WITHIN LIMITS PER BOEING SRM 57-30-01 FIG. 2.

Part: SKIN — CORRODED (RT TE FOREFLAP)

LEVEL 1 CORROSION, RIGHT INBOARD TRAILING EDGE FLAP FOREFLAP LOWER SURFACE. BLENDED OUT CORROSION AND REPAIRED DELAMINATED AREAS PER BOEING SRM 51-40-09.

Part: BLANKING PLATE — MIS INSTALLED (NR 3 ENG)

LOSS OF OIL FROM NR 3 ENGINE ON CLIMB. ENGINE SHUT DOWN DUMPED FUEL AND RETURNED TO ANC. FOUND BLANKING PLATE FOR NR 3 ENGINE DRIVEN PUMP PER MEL NOT INSTALLED PROPERLY. CORRECTLY INSTALLED BLANKING PLATE PER DISPATCH DEVIATION GUIDE 29-110-05 PAGE 201 PARAGRAPH 3. IDLE RUN LEAK CHECK OK.

Part: CONTROL ROD — BROKEN (CARGO DOOR)

MAIN DECK CARGO DOOR WOULD NOT CLOSE NORMALLY AFTER CARGO LOADING. FOUND FORWARD PULL IN HOOK CONTROL ROD BROKEN. REPLACED ROD PER M/M 52-32-00.

Part: TIRES — FLAT (NR 2/4)

ON WALKAROUND CHECK, FOUND NR 2 AND NR 4 TIRES FLAT. REPLACED NR 1, 2, 3 AND 4 TIRES PER MAINTENANCE MANUAL 32-45-01. COMPLETED BRAKE ANTI-SKID OPERATIONAL CHECK PER M/M 32-42-00, ALL CHECKS SATISFACTORY.

Part: SLEEVE — DENTED (NR 1 ENGINE)

DEEP LONG DENT NR 1 ENGINE FAN REVERSER SLEEVE AT 7 O'CLOCK POSITION. REPAIRED PER POLAR AIR CARGO MA 7830-01:01 AND BOEING SRM 51-40-06 PARA 3 AND 51-24-11.

Part: BRACKET — CORRODED (KEEL BEAM)

LEVEL 2 CORROSION KEEL BEAM ACCESS PANELS 191HH AND 191KK 6 INNER ATTACHMENTS BRACKETS. FABRICATED AND REPLACED BRACKETS PER BOEING SRM 51-10-01.

Part: BRACKET — CRACKED (NR 4 TE FLAP)

BROKEN FORWARD CANOE HANGER BRACKET ON NR 4 FLAP TRACK. REPLACED BRACKET PER BAC MM 27-51-26.

Part: BRACKET — BROKEN (NR 4 TE FLAP)

THREE BROKEN HANGER BRACKETS FOR NR 4 FLAP TRACK CANOE FAIRING. REPLACED BRACKETS PER BAC MM 27-51-26.

Part: SKIN — DELAMINATED (LT ELEVATOR)

DELAMINATED OUTBOARD TRAILING EDGE CORNER OF LEFT INBOARD ELEVATOR. REPAIRED WITH FIBERGLASS OVERLAYS PER BAC SRM 51-40-09 AND REPAINTED PER BAC SRM 51-24-11.

Part: RIB — CRACKED (NR 4 ENG COWL)

CRACKED AFT UPPER RIB AND BRACKET ON NR 4 ENGINE OUTBOARD COWL. FABRICATED AND INSTALLED NEW RIB AND BRACKET PER BAC SRM 51-10-01.

Part: KEEL BEAM — CORRODED (FUSELAGE)

LEVEL 1 CORROSION KEEL BEAM PANELS 191GG, 191HH, 191JJ AND 191KK. CLEANED CORROSION ON PANELS 191HH AND 191KK SRM 51-10-01 AND REPLACED 191GG AND 191JJ FOR CONVENIENCE PER SRM 51-10-01 AND 51-10-02.

Part: FITTING — CRACKED (L1 DOOR)

CRACKED LOWER L-1 DOOR LOWER TORQUE TUBE PIVOT HINGE BEARING FITTING. REPLACED FITTING PER BOEING SRM 51-30-03.

Part: SKIN — DAMAGED (NR 3 ENG COWL)

DAMAGED SKIN ON BOTH AFT CORNERS OF NR 3 ENGINE INBOARD FAN COWL. FABRICATED AND INSTALLED FILLER AND DOUBLERS PER BAC SRM 51-40-06.

Part: SKIN — DELAMINATED (RT ELEVATOR)

DELAMINATED SKIN ON RIGHT ELEVATOR INBOARD CORNER OF LOWER TRAILING EDGE. REPAIRED WITH FIBERGLASS OVERLAYS PER BAC SRM 51-40-09 AND REPAINTED PER BAC SRM 51-24-11.

Part: SKIN — DAMAGED (NR 4 ENG COWL)

DAMAGED LOWER AFT CORNER SKIN ON NR 4 ENGINE OUTBOARD FAN COWL. FABRICATED AND INSTALLED FILLER AND DOUBLER PER BAC SRM 51-40-06.

Part: CUTOUT — CRACKED (NR 3 ENG COWL)

CRACKED PRECOOLER DOOR CUTOUT ON NR 3 ENGINE INBOARD COWL. FABRICATED AND INSTALLED NEW PART PER BAC SRM 51-10-02.

Part: FITTING — BROKEN (FWD CARGO BAY)

BROKEN SIDE RAIL ATTACH FITTING IN FORWARD CARGO BAY ADJACENT TO DOOR. REPLACED RAIL ATTACH FITTING PER BAC MM 25-54-25.

Part: FLANGE — CRACKED (NR 3 ENG COWL)

CRACKED UPPER FORWARD FLANGE ON NR 3 ENGINE INBOARD COWL. FABRICATED AND INSTALLED NEW FLANGE PER BAC SRM 51-10-01.

Part: SKIN — DELAMINATED (LT ELEVATOR)

DELAMINATION ON LEFT INBOARD ELEVATOR LOWER SKIN. REPAIRED WITH FIBERGLASS OVERLAYS PER BAC SRM 51-40-09 AND REPAINTED PER BAC SRM 51-24-11.

Part: SKIN — CORRODED (RT MLG DOOR)

LEVEL 1 CORROSION ON RIGHT BODY GEAR INBOARD GEAR DOOR SKIN. REMOVED CORROSION PER BAC SRM 51-10-01 AND REPROTECTED PER BAC SRM 51-10-02.

Part: SKIN — WORN (NR 2 ENG COWL)

WORN LOWER OUTER SKIN ON NR 2 ENGINE FAN COWL. FABRICATED AND INSTALLED DOUBLER PER BAC SRM 51-40-06.

Part: ANGLE — CRACKED (NR 1 ENGINE COWL)

CRACK AND DEFORMATION ON NR 1 CORE COWL HAT SECTION ANGLE. STOP DRILLED AND REPAIRED PER BAC SRM 51-40-01.

Part: ANGLE — CRACKED (NR 2 ENG COWL)

CRACKED NR 2 ENGINE OUTBOARD CORE COWL ANGLE AT PRECOOLER DOORS. FABRICATED AND INSTALLED NEW ANGLE PER BAC SRM 51-10-02.

Part: ANGLE — CRACKED (NR 2 ENGINE)

CRACKED SKIRT FAIRING ANGLE ON NR 2 ENGINE. REPAIRED PER BAC SRM 51-30-02.

Part: SKIN — WORN (NR 2 ENG COWL)

WORN OUTER UPPER SKIN ON NR 2 ENGINE FAN COWL. FABRICATED AND INSTALLED DOUBLER PER BAC SRM 51-40-06.

Part: SKIN — CORRODED (BS 1800)

LEVEL 1 CORROSION ON SKIN AROUND ANTENNA AT BS 1800. REMOVED CORROSION PER BAC SRM 51-10-01 AND REPROTECTED PER BAC SRM 51-10-02.

Part: STRAPS — CORRODED (NLG WW)

LEVEL 1 CORROSION ON NOSE LANDING GEAR WHEEL WELL UPPER PRESSURE WEB STRAPS. REMOVED CORROSION PER BAC SRM 51-10-01 AND REPROTECTED PER BAC SRM 51-10-02.

Part: PANEL — CRACKED (LT WING)

CRACKED AND DELAMINATED PANEL OUTBOARD OF NR 5 SPOILER ON UPPER LEFT WING. REPAIRED WITH FIBERGLASS OVERLAYS PER BAC SRM 51-40-09 AND REPAINTED PER BAC SRM 51-24-11.

Part: SKIN — CORRODED (RT MLG DOOR)

LEVEL 1 CORROSION ON RIGHT BODY GEAR INBOARD GEAR DOOR TRAILING EDGE SKIN. REMOVED CORROSION PER BAC SRM 51-10-01 AND REPROTECTED PER BAC SRM 51-10-02.

Part: SKIN — WORN (NR 1 ENG COWL)

WORN INBOARD TRAILING EDGE SKIN ON NR 1 ENGINE FAN COWL. FABRICATED AND INSTALLED FILLER AND DOUBLER PER BAC SRM 51-40-06.

Part: RADOME — DELAMINATED (FWD FUSELAGE)

DELAMINATED AREAS ON RADOME. REPAIRED PER BAC SRM 51-40-09 AND REPAINTED PER BAC SRM 51-24-11.

Part: SKIN — CRACKED (RT ELEVATOR)

CRACK ON RIGHT INBOARD ELEVATOR OUTBOARD TRAILING EDGE LOWER CORNER. REPAIRED WITH FIBERGLASS OVERLAYS PER BAC SRM 51-40-09 AND REPAINTED PER BAC SRM 51-24-11.

Part: DEFLECTOR — BROKEN (BS 2360)

BROKEN AIR FLOW DEFLECTOR ON AFT FUSELAGE DRAIN AT BS 2360 RBL 4. REPLACED PER BAC SRM 51-10-01.

Part: BALL MAT TRAY — DAMAGED (FWD CARGO BAY)

DAMAGED BALL MAT TRAY IN FORWARD LOWER CARGO BAY. REPLACED BALL MAT TRAY WITH FABRICATED TRAY PER BAC SRM 51-10-01.

Part: LINE — WORN (NR 3 HYD SYST)

LOSS OF HYDRAULIC FLUID NR 3 HYDRAULIC SYSTEM AFTER TAKEOFF. SYSTEM DEPRESSURIZED AND STABILIZED AT 1.3 GALLONS. ALL SYSTEMS WORKED NORMAL ON APPROACH TO JFK. FOUND HYDRAULIC LINE WORN THROUGH ON NR 3 PYLON IN THE GAP COVER AREA. REPLACED LINE LEAK CHECKED OK PER MAINTENANCE MANUAL 29-11-00 PAGE 602.

Part: BRACKET — BROKEN (APU FIRE LOOP)

TWO BROKEN ATTACH BRACKETS FOR APU FIRE LOOP ON APU DOOR. REPAIRED PER BAC SRM 51-10-01.

Part: FAIRING — CRACKED (NR 3 PYLON)

CRACKED TIP ON NR 3 PYLON AFT FAIRING ABOVE STRINGER. REPAIRED PER BAC SRM 51-10-01.

Part: COVER, HINGE — DAMAGED (PACK DOOR)

DAMAGED HINGE COVERS AT 3 POSITIONS ON AIR CONDITIONING PACK DOORS. REPAIRED PER BAC SRM 51-10-01.

Part: DOUBLER — CRACKED (NR 3 PYLON)

CRACKED DOUBLER ON NR 3 PYLON SLOT SEAL FAIRING. REPAIRED PER BAC SRM 54-30-03 FIG 6.

Part: LIGHT — INOPERATIVE (CABIN)

INOPERATIVE EMERGENCY LIGHT ASSEMBLY ON UPPER DECK. REPLACED EMERGENCY LIGHT AND BATTERY PACK ASSEMBLY PER BAC MM 33-51-00.

Part: RIB — CRACKED (APU COMPT)

CRACKED RIB IN APU COMPARTMENT IN STRUCTURE FOR HOLDING AFT APU REMOVAL FISH POLE AND CRACKED BOLT HOLE. PARTS TO BE REPLACED WITHIN 50 CYCLE OPERATION WITH APU REMOVED APPROVED BY BOEING. REPLACED SUPPORT RIB ASSEMBLY PER BOEING SRM 51-10-01.

Part: NOSE COWL — DEFORMED (NR 2 ENGINE)

NR 2 ENGINE NOSE COWL OUTER SKIN FROM 1 TO 3 O'CLOCK POSITION SKIN BULGING FROM SEALANT AND MISSING SCREW. REPLACED EXTERIOR SKIN IAW BOEING SRM 51-30-02.

Part: SEAT MECHANISM — WORN (COCKPIT)

F/E SEAT TRACK HAS WORN HOLES, HORIZONTAL LATCH WILL NOT LATCH SECURELY. REPLACED SEAT ASSY PER MM 25-11-02.

Part: NOSE COWL — DENTED (NR 4 ENGINE)

DENT AT 6 O'CLOCK POSITION NR 4 ENGINE NOSE COWL. REPAIRED PER BOEING SRM 54-30-03.

Part: HINGE — CORRODED (ACM DOOR)

LEVEL 1 CORROSION ON NR 3 AIR CYCLING MACHINE ACCESS DOOR. REPLACED HINGE PER BOEING MAINTENANCE MANUAL 52-48-01.

Part: TIRE — FAILED (NR 5/6)

DURING INITIAL APPROACH TO JFK, ATC NOTIFIED OF RUBBER SECTIONS FOUND ON RUNWAY AT LCK. AFTER LANDING, FOUND CAP MISSING ON NR 6 TIRE AND NR 5 TIRE THERMALLY DEFLATED AFTER TAXI. REPLACED NR 5 AND NR 6 TIRE ASSEMBLIES PER BOEING MAINTENANCE MANUAL 32-45-01. PERFORMED BURST INSPECTION PER BOEING MM 05-51-25. BLED NRS 5, 6, 7, 8 BRAKES PER BOEING MM 32-41-00 PRECAUTIONARY.

Part: PANEL — DENTED (FUSELAGE)

WING TO FUSELAGE PANEL 193F HAS AREA IN CENTER OF PANEL WITH NUMEROUS DENTS, FOUND ON BLOWN TIRE INSPECTION. REPLACED PANEL PER BOEING SRM 51-10-01.

Part: BRACKET — BENT (LT MLG)

BENT LEFT BODY GEAR LOWER DRAG STRUT SEGMENT BRACKET FOR BUNGEE, FOUND ON BLOWN TIRE INSPECTION. REPLACED BRACKET PER BOEING SRM 51-10-01.

Part: OVERHEAT LOOP — CRIMPED (LT MLG WW)

CRIMPED OVER HEAT LOOP LEFT BODY GEAR WHEEL WELL PRESSURE DECK INBOARD, FOUND ON BLOWN TIRE INSPECTION. REPLACED LOOP AND TESTED PER BOEING MAINT MANUAL 26-17-02.

Part: PANEL — DAMAGED (FUSELAGE)

DAMAGED PANEL NR 193B ADF PANEL 16.5 BY 18.5 AREA, FOUND ON BLOWN TIRE INSPECTION. REPLACED PANEL PER BOEING SRM 51-10-01.

Part: PANEL — PUNCTURED (FUSELAGE)

WING TO FUSELAGE PANEL 193D HAS 2 AREAS OF DAMAGE 1 AFT CENTER 32 BY 31.25, THE OTHER FORWARD LOWER 8 BY 2.5, FOUND ON BLOWN TIRE INSPECTION. REPLACED PANEL PER BOEING SRM 51-10-01.

Part: BRACKET — BROKEN (LT MLG)

SUPPORT BRACKETS BROKEN FOR LEFT BODY GEAR PRIORITY VALVE, FOUND ON BLOWN TIRE INSPECTION. REMOVED FABRICATED AND REPLACED BRACKETS PER BOEING SRM 51-10-01.

Part: BUNGEE — DAMAGED (LT MLG)

DAMAGED BUNGEE ON LEFT BODY LANDING GEAR, FOUND ON BLOWN TIRE INSPECTION. REPLACED BUNGEE PER BOEING MAINT MANUAL 32-33-16.

Part: ACTUATOR ROD — BROKEN (LT MLG DOOR)

BROKEN ACTUATOR ROD FOR THE LEFT BODY GEAR INBOARD DOOR, FOUND ON BLOWN TIRE INSPECTION. REPLACED ROD PER BOEING MAINT MANUAL 32-14-05.

Part: TORQUE TUBE — BENT (LT MLG)

OUTBOARD FLAP DRIVE TORQUE TUBE BENT, WHIP GUARD BENT AND WHIP GUARD BRACKET BENT, BLOWN TIRE DAMAGE. REPLACED TORQUE TUBE WHIP GUARD AND BRACKET RIGGED FLAPS PER BOEING M/M 27-51-20.

Part: SUPPORT — DAMAGED (BS 1480-1500)

DAMAGED FAIRING SUPPORT STRUCTURE BL 0 FROM 1480 TO 1500, FOUND ON BLOWN TIRE INSPECTION. REPLACED SUPPORT STRUCTURE PER BOEING SRM 51-10-01.

Part: PANEL — DAMAGED (FUSELAGE)

PANEL NR 193C HAS 2 AREAS OF DAMAGE, ONE IN THE CENTER OF PANEL 20 INCH CRACK, THE OTHER A 6 BY 7 HOLE, FOUND ON BLOWN TIRE INSPECTION. REPLACED PANEL PER BOEING SRM 51-10-01.

Part: FITTING — BROKEN (LT MLG ACT)

BROKEN LEFT BODY GEAR INBOARD DOOR ACTUATOR FITTING, FOUND ON BLOWN TIRE INSPECTION. REPLACED FITTING PER BOEING SRM 51-10-01.

Part: PANEL — DAMAGED (BS 1480)

DAMAGED VERTICAL HONEYCOMB PANEL BS 1480 LEFT BODY GEAR WHEEL WELL, FOUND ON BLOWN TIRE INSPECTION. REPLACED PANEL PER BOEING SRM 51-10-01.

Part: LONGERON BOX WEB — DENTED (LT MLG WW)

DAMAGED WEB AND STRINGER LEFT BODY GEAR WHEEL WELL LONGERON BOX BS 1460 AFT OF BRACKET FOR OVERWING SLIDE BOTTLE, NOT INSTALLED. FOUND ON BLOWN TIRE INSPECTION. REPAIRED PER BOEING SRM 51-40-02 AND 51-10-01.

Part: SUPPORT — DENTED (BS 1480)

DAMAGED FAIRING SUPPORT STRUCTURE FOR THE LEFT HAND WING TO BODY FAIRING BS 1480, FOUND ON BLOWN TIRE INSPECTION. REPLACED SUPPORT STRUCTURE PER BOEING SRM 51-10-01.

Part: FAIRING SUPPORT — CRACKED (BS 1540)

BENT FAIRING SUPPORT LEFT WING TO BODY FAIRING BS 1540, FOUND ON BLOWN TIRE INSPECTION. REPAIRED PER BOEING SRM 53-50-04, EDDY CURRENT INSPECTION REVEALED NO CRACKS.

Part: FITTING — BROKEN (BS 1480)

BROKEN FITTING FOR LONGERON BOX SUPPORT ROD LEFT BODY GEAR WHEEL WELL BS 1480, FOUND ON BLOWN TIRE INSPECTION. REMOVED FABRICATED AND INSTALLED FITTING PER BOEING SRM 51-10-01.

Part: STIFFENER — BENT (BS 1362)

BENT PRESSURE DECK STIFFENERS BENT LEFT BODY GEAR WHEEL WELL BS 1362 ABOVE VERTICAL TIRE GUARD, FOUND ON BLOWN TIRE INSPECTION. REPAIRED PER MA 53:40-01:01.

Part: PRESSURE DECK — PUNCTURED (BS 1355)

PUNTURE IN PRESSURE DECK, BENT STIFFENER AND GOUGED SPLICE PLATE LEFT BODY GEAR WHEEL WELL BS 1355 LBL 127.75, FOUND ON BLOWN TIRE INSPECTION. REPAIRED PER MA A5340-02:01.

Part: TIRE GUARD — DENTED (LT MLG)

LEFT BODY GEAR WHEEL WELL VERTICAL TIRE GUARD UPPER WEB DAMAGED. FOUND ON BLOWN TIRE INSPECTION. REMOVED FABRICATED AND REPLACED PER BOEING SRM 51-40-00.

Part: ANGLE — BENT (LT MLG)

LEFT BODY GEAR HYDRAULIC BULKHEAD OUTBOARD SUPPORT ANGLE BENT FOUND DURING BLOWN TIRE INSPECTION. REMOVED FABRICATED AND INSTALLED PER BOEING SRM 51-10-01.

Part: COWL LOWER RAIL — CRACKED (NR 3 ENGINE)

NR 3 ENGINE INBOARD CORE COWL LOWER RAIL CRACKED IN 3 PLACES. REMOVED, FABRICATED AND INSTALLED LOWER RAIL PER BOEING SRM 51-10-01 AND SRM 51-30-02.

Part: EXHAUST SLEEVE — PIECE MISSING (NR 2 ENGINE)

DURING B-CHECK, FOUND NR 2 ENGINE EXHAUST SLEEVE, LEFT SIDE, MANY FASTENERS LOOSE AND MISSING, LOWER RIGHT LEADING EDGE SKIN PIECE MISSING, REMOVED AND REPLACED FASTENERS, INSTALLED DOUBLERS PER BOEING SRM 54-30-03 AND SRM 51-10-01.

Part: HINGE — CRACKED (RT MLG DOOR)

RIGHT WING GEAR INBOARD DOOR FORWARD HINGE IS CRACKED. REPLACED HINGE PER BOEING MAINTENANCE MANUAL 32-12-03.

Part: SKIN — DELAMINATED (LT ELEVATOR)

DURING B-CHECK, FOUND LEFT INBOARD ELEVATOR, INBOARD AFT CORNER DELAMINATED. REPAIRED PER BOEING SRM 51-40-15.

Part: FAIRINGS — DELAMINATED (FLAP TRACKS)

NRS 1, 2, 3, 5, AND 8 FLAP TRACK FIXED FAIRINGS HAVE SEVERAL AREAS OF EROSION AND DELAMINATION. REPAIRED PER BOEING SRM 51-40-12.

Part: KEEL BEAM — CORRODED (BS 1000)

DURING B-CHECK, FOUND LEVEL 1 CORROSION ON RIGHT SIDE OF THE KEEL BEAM BS 1000. REMOVED AND TREATED CORROSION WITHIN LIMITS PER BOEING SRM 51-10-01.

Part: EXHAUST DUCT — CRACKED (APU)

CRACK IN THE APU EXHAUST DUCT AT 12:00 O'CLOCK POSITION. WELDED CRACK PER BAC 5975.

Part: SLIDE BAR — WORN THROUGH (RIGHT)

DURING B-CHECK, FOUND RIGHT BODY GEAR OUTBOARD DOOR SLIDE BAR FORWARD UPPER FLANGE WORN THROUGH. FABRICATED AND INSTALLED NEW FLANGE CHANNEL PER BOEING SRM 51-10-01.

Part: EXHAUST CASE — CRACKED (NR 2 ENGINE)

DURING B-CHECK, FOUND NR 2 ENGINE R-RAIL HAS 2 CRACKS AT THE 5:30 AND 7:00 O'CLOCK POSITIONS. WELDED, STRESS RELIEVED, AND SHOT PEENED PER MAINTENANCE MANUAL 72-53-01, AND SRM 51-10-07.

Part: EXHAUST CASE — CRACKED (NR 3 ENGINE)

DURING B-CHECK, FOUND NR 3 ENGINE R-RAIL HAS 2 CRACKS AT THE 6:00 AND 7:OO O'CLOCK POSITIONS. WELDED, STRESS RELIEVED, AND SHOT PEENED PER MAINTENANCE MANUAL 72-53-01 AND SRM 51-10-07.

Part: BUSHING — MIGRATED (RT MLG)

DURING B-CHECK, FOUND RIGHT BODY GEAR TRUNNION BUSHING MIGRATED BEYOND .050 INCH LIMIT (.075 INCH). RESEATED BODY GEAR TRUNNION BUSHING PER BOEING MAINTENANCE MANUAL 32-13-01.

Part: SKIN — CRACKED (NR 1 PYLON)

DURING B-CHECK, FOUND NR 1 PYLON SKIN CRACKED ON INBOARD SIDE AFT OF LOWER SLOT SEAL. REPAIRED PER BOEING SRM 54-30-03.

Part: SKIN — CRACKED (NR 2 PYLON)

DURING B-CHECK, FOUND NR 2 ENGINE PYLON INBOARD AFT LOWER SKIN IS CRACKED AND FASTENERS FORWARD OF CRACK ARE WORKED LOOSE. FABRICATED AND INSTALLED REPAIR DOUBLER PER BOEING SRM'S 51-30-02, 54-30-03, AND 54-50-03.

Part: COWL — TORN (NR 4 ENGINE)

DURING B-CHECK, FOUND NR 4 ENGINE OUTBOARD CORE COWL FORWARD UPPER CORNER TORN AND LOOSE FASTENERS ON OUTER SKIN. REPAIRED PER BOEING SRM 51-30-02.

Part: TIRE — BLOWN (NR 2/3 MLG)

NR 2 AND 3 MAIN TIRES FOUND BLOWN ON ARRIVAL. NR 1 MAIN TIRE HAD FLAT SPOT AND THERMAL RELIEF AT BLOCKS. NR 4 MAIN TIRE HAD FLAT SPOT BUT RETAINED AIR. REMOVED AND REPLACED NR 1, 2, 3, 4 WHEEL ASSEMBLIES IAW MM 32-45-01. REMOVED AND REPLACED NR 4 BRAKE ASSEMBLY DUE TO BROKEN DISC FOUND WHEN WHEEL ASSEMBLY REMOVED, IAW MM 32-41-15. COMPLIED WITH BLOWN TIRE INSPECTION PER MM 5-51-34, ANTI-SKID BITE CHECKS NORMAL.

Part: AIR DRIVEN PUMP — PRESS FLUX (NR 1 ENGINE)

ON TAXI OUT, NR 1 ADP INOP, PRESSURE FLUCTUATION 0 TO 2500 PSI, RETURNED TO BLOCKS. CLEANED FILTERS, RESET OVERSPEED SWITCH AND LUBED REGULATOR SHUTOFF VALVE AND OPERATIONAL CHECK GOOD IAW MM 29-11-05.

Part: WIRE — SHORTED (TE FLAPS)

EXPERIENCED FLAP FAILURE/ASYMMETRY LOCKOUT ON CLIMBOUT. RETRACTED T/E FLAPS USING ALTERNATE SYSTEM, DIVERTED TO BIRMINGHAM DUE TO ATLANTA WEATHER. TROUBLESHOT SYSTEM, FOUND LOCKOUT PROBLEMS STOPPED WHEN MODE 'S' RELAY CB PULLED. REPAIRED SHORTED WIRE FOUND NEAR P54 PANEL, RELAY 4R914, OPS CHECK NORMAL PER MM 27-58-00.

Part: WINDSHIELD — CRACKED (RT COCKPIT)

FIRST OFFICER'S WINDSHIELD CRACKED ON TAXI OUT. REMOVED AND REPLACED WINDSHIELD IAW MM 56-11-01.

Part: ACTUATOR FITTING — SHEARED BOLTS (AFT CARGO DOOR)

LOWER AFT CARGO DOOR AFT LIFT ACTUATOR MOUNTING BOLTS SHEARED. REMOVED AND REPLACED AFT ROTARY ACTUATOR IAW MM 52-34-03. FOUND AFT ROTARY ACTUATOR CASTING CRACKED AFT SIDE, 5.5 INCH LONG BY .5 INCH WIDE. REMOVED AND REPLACED CRACKED CASTING IAW SRM 51-10-01. REMOVED AND REPLACED CRACKED WIRING HARNESS SUPPORT BRACKET, AFT CARGO DOOR, STA 1800 RIGHT SIDE IAW SRM 51-10-01. REMOVED AND REPLACED DAMAGED FRAME AT BS 1900 IAW SRM 51-10-01. REPAIRED AFT ROTARY ACTUATOR SUPPORT FITTING IAW SRM 51-10-01. REMOVED AND REPLACED FWD ROTARY ACTUATOR AS PRECAUTIONARY IAW MM 52-34-03.

Part: SUPPORT BEAM — CORRODED (PANEL 191M)

FOUND FAIRING SUPPORT BEAM EXFOLIATED FWD END OF PANEL 191M. REMOVED DAMAGED AREA, FABRICATED REPAIR ANGLE AND INSTALLED IAW SRM 51-40-03.

Part: HEAT DUCT — CRACKED (BS 1480)

FOUND CRACKED WELD AT AFT CARGO STATION 1480 HEAT DUCT. REPAIRED IAW OHM 36-10-04.

Part: PANEL — CRACKED (HORIZ STAB)

FOUND SMALL CRACKS ON THE HORIZONTAL STABILIZER, RT T/E UNDER STATIC DISCHARGE BASE THIRD FROM OUTSIDE. REPAIRED IAW SRM 51-40-15.

Part: SKIN — CORRODED (BS 2484-2658)

FOUND LEVEL ONE CORROSION ON FUSELAGE SKIN BETWEEN STA 2484 TO 2658 WL 366.50 RT SIDE. REMOVED CORROSION AND TREATED IAW SRM 51-10-01.

Part: PANEL — CORRODED (HORIZ STAB)

FOUND LEVEL ONE CORROSION AT RT HORIZONTAL STABILIZER TIP, AROUND STATIC DISCHARGE BASE SECOND FROM THE FRONT SIDE. CORROSION REMOVED AND AREA REPROTECTED IAW SRM 51-10-01.

Part: ACTUATOR — FAILED (RT AILERON)

DURING FLIGHT CONTROL CHECK, RT OUTBOARD AILERON DID NOT MOVE. GATE TURN BACK. AIRCRAFT DISPATCHED TO SJU FOR LOCKOUT ACTUATOR CHANGE DUE TO STRIKE AT CAY. AILERON LOCKOUT ACTUATOR REPLACED IAW MM 27-11-16.

Part: TURBINE — FAILED (NR 1 ENGINE)

WITH POWER STABLE AT 1.36 EPR AND NO THROTTLE MOVEMENT AT 26,000 FT CLIMBING TO 29,000 FT, NR 1 ENGINE APPEARED TO SURGE AND COMPRESSOR STALLED WITH A RAPID RISE IN EGT, 975 FOR 5 TO 6 SECONDS UNTIL THROTTLE WAS RETARDED. ENGINE WAS COOLED FOR 5 MINUTES AND SHUTDOWN. ENGINE WAS RESTARTED, WOULD NOT PRODUCE FULL POWER WITHOUT GOING INTO CAUTION RANGE. PROCEEDED WITH REDUCED POWER TO JNB. FOUND METAL IN TAIL PIPE, ENGINE TO BE REPLACED.

Part: NET — NOT SECURED (CARGO COMPT)

FELT YAW ON CLIMBOUT AT 5,500 FEET, ALL ENGINE INDICATIONS NORMAL AND NO FLUID LOSS OBSERVED. FLIGHT ENGINEER WAS SENT BACK TO CARGO DECK AFTER LEVEL OFF, OBSERVED BANGING SOUNDS OUTSIDE CARGO DOOR. RETURNED TO ORD, FOUND SECTION OF CARGO NET HANGING OUTSIDE MAIN CARGO DOOR FLAPPING IN THE WIND.

Part: CHECK VALVE — FAILED (NR 3 HYD ADP)

DURING CONTROL CHECK ON TAXI OUT, NR 3 HYDRAULIC PRESS LIGHT ILLUMINATED WITH SUBSEQUENT LOSS OF TOTAL SYSTEM QUANTITY. DEPRESSURIZED SYSTEM AND RETURNED TO BLOCKS. FOUND NR 3 HYDRAULIC CHECK VALVE FAILED, VALVE CRACKED AT THREADS. REMOVED REMAINING THREADED SECTION, INSPECTED MODULE THREADS, INSTALLED NEW CHECK VALVE. LEAK AND OP CHECK NORMAL PER MM 29-11-40.

Part: HF COUPLER — FAILED (NR 2)

DUE TO RAPID INCREASE IN CABIN ALTITUDE WHEN NR 2 HF SYSTEM KEYED, PASSENGER MASKS DEPLOYED AND OXYGEN ACTIVATED. REPLACED HF COUPLER, STOWED ALL MASKS AND RESET 02 FLOW CONTROL.

Part: ACTUATOR — FAILED (RT AILERON)

OFF BLOCKS ON FLIGHT CONTROL CHECK RIGHT OUTBOARD AILERON LOCKED OUT WITH FLAPS DOWN. REPLACED AILERON LOCK-OUT ACTUATOR.

Part: AILERON CONTROLS — LOCKED OUT (RIGHT)

DURING DEPARTURE, RIGHT OUTBOARD AILERON WAS LOCKED OUT. RETURNED TO BLOCKS, RECYCLED FLAPS AND OPERATION NORMAL.

Part: ENGINE — FLAMED-OUT (NR 4)

DURING LEVEL OFF FL 370, THE NR 4 ENGINE FLAMED-OUT. RESTART AT FL 190, ENGINE OPERATED NORMAL FOR REMAINDER OF FLIGHT. TROUBLESHOOTING PER MAINTENANCE MANUAL 71-00-42 PG 118. ALL ITEMS FOUND NORMAL, AIRCRAFT RELEASED.

Part: ENGINE — FLAME-OUT (NR 1)

DURING CRUISE FL 370, NR 1 ENGINE FLAMED-OUT, ENGINE SHUTDOWN PROCEDURE ACCOMPLISHED. DESCENDED TO FL 350 IN FLIGHT START PER AOM ENGINE PERFORMANCE NORMAL. CHECKED ENGINE INTAKE AND EXHAUST, FUEL PUMP PRESSURE CHECKED, CONDITION MOTOR CHECKED, AND WATER CONTAMINATION CHECKED PER MAINTENANCE MANUAL 71-00-42. ALL CHECKED GOOD AIRCRAFT RELEASED.

Part: LE RIB — CRACKED (RT WING)

CRACKED LEADING EDGE RIB AT SUPPORT FOR GROUP 3 LEADING EDGE PDU INTERCOSTAL INBOARD END, BS 938.45 WS 294. REPAIRED PER BOEING TELEX 32-9430 PAO-SIN-95-0006RE, RI-PA57-018.

Part: SKIN — PUNCTURE (NR 3 TE FLAP)

PUNCTURE LEFT WING INBOARD MIDFLAP LOWER SURFACE OUTBOARD OF NR 3 FLAP TRACK. REPAIRED PER BOEING SRM 51-40-09.

Part: SPAR CHORD — CORRODED (LT WING)

CORROSION AT LES 777 LEFT WING LEADING EDGE CAVITY LOWER FRONT SPAR CHORD. REMOVED CORROSION PER BOEING SRM 51-10-01 WITHIN LIMITS PER 51-10-01.

Part: LE SKIN — PUNCTURED (NR 4 FOREFLAP)

PUNCTURE LEFT WING INBOARD FOREFLAP LEADING EDGE AT NR 4 FLAP TRACK. REPAIRED PER BOEING SRM 51-40-09.

Part: FAIRING MOUNT — CRACKED (NR 2 PYLON)

PYLON NR 2 INBOARD SIDE FAIRING MOUNT IS CRACKED. REPAIRED PER BOEING SRM 54-10-00.

Part: COMPRESSOR — STALLED (NR 3 ENGINE)

NR 3 ENGINE EXPERIENCED AUDIBLE STALL AT TOP OF DESCENT INTO ANC. N1 AND N2 INDICATORS DROPPED WITH STEADY RISE IN EGT SHUTDOWN ENGINE AT 750 DEGREES. RELIGHT OF ENGINE NORMAL ENGINE PERFORMED NORMAL FOR THE REST OF FLIGHT. INSPECTED ENGINE PER MAINTENANCE MANUAL NO ITEMS FOUND OUT OF LIMITS, AIRCRAFT RELEASED.

Part: ENGINE — FAILED (NR 3)

DURING POST EVC, FUEL PUMP AND FUEL CONTROL CHANGE RUNUP ENGINE STALLED AT 1.41 EPR WITH RAPID EGT RISE, ENGINE SHUTDOWN. GROUND REPORTED FIRE IN TAIL PIPE. MOTORED ENGINE, FIRE PUT OUT. FOUND METAL IN TAIL PIPE. ENGINE TO BE CHANGED

Part: CONTROL CABLE — BROKEN (LT MLG WW)

DURING POST FLIGHT INSPECTION, FOUND LEFT BODY GEAR DOOR GROUND RELEASE CABLE BROKEN. REPLACED CABLE.

Part: ENGINE — FAILED (NR 3)

DURING CLIMBOUT FROM SEA, PASSING 10,000 FEET ALTITUDE, NR 3 ENGINE OIL PRESSURE WENT O, NR 3 ENGINE OIL PRESSURE LIGHT AND NR 3 ENGINE FILTER BYPASS LIGHT ILLUMINATED. SHUTDOWN ENGINE IAW IN FLIGHT ENGINE CHECK LIST. ON GROUND RUN, OIL RUNNING FROM ENGINE NR 3 BEARING VENT TUBE AND METAL IN ENGINE OIL FILTER. ENGINE TO BE REPLACED.

Part: RETRACT MECH — LACK OF LUBE (LANDING GEAR)

AFTER TAKEOFF LEFT AND RIGHT WING LANDING GEAR WOULD NOT RETRACT. DUMPED FUEL, RETURNED TO MIA. LUBRICATED LANDING GEAR, CHECKED ALL RIGGING. FUNCTIONAL CHECKED GOOD, RETURNED TO SERVICE.

Part: DOOR — CRACKED (NLG)

CRACK ON AFT INBOARD CORNER OF AFT LEFT NOSE GEAR DOOR. INSTALLED REPAIR PER BOEING SRM 51-40-03 PAGE 9-12.

Part: COVER — CRACKED (NLG STEERING)

SMALL CRACK IN COVER AT LEFT INSPECTION HOLE ON NOSE GEAR STEERING CABLE COVER. BLENDED SMALL CRACK PER BOEING SRM 51-10-01.

Part: DOOR — CRACKED (NLG)

CRACK IN AFT INBOARD CORNER OF AFT RIGHT NOSE GEAR DOOR. INSTALLED REPAIR AS PER BOEING SRM 51-40-03 PAGE 9-12.

Part: RIVET — SHEARED (NLG DOOR)

RIVET HEAD SHEARED ON AFT STRIKER PLATE FOR AFT LEFT NOSE GEAR DOOR, INBD CORNER. REPLACED RIVET AS PER BOEING SRM 51-30-02.

Part: SKIN — WORN (NLG DOOR)

NOTCH WORN INTO OUTER SKIN AT RIGHT AFT NOSE GEAR DOOR, AFT HINGE CUTOUT. REPAIRED PER BOEING SRM 51-10-01 PAGE 20.