N831FT

Part: ACCUMULATOR — FAILED (BRAKE)

NR 1 AND NR 4 HYDRAULIC SYSTEM PRESSURE AND QUANTITY WENT TO ZERO DURING PUSHBACK. FOUND BRAKE SURGE ACCUMULATOR FAILED, REPLACED SAME IAW MM 32-41-22. SERVICED SYSTEM IAW MM 12-15-11, REPLENISHED HYDRAULIC FLUID, LEAK CHECK GOOD

Part: PANEL — DELAMINATED (RT WING LE)

FOUND RIGHT HAND WING UPPER LEADING EDGE PANEL DELAMINATED WITH SECTION MISSING JUST OUTBOARD OF NR 3 ENGINE PYLON. REPAIRED PANEL PER SRM 51-40-14.

Part: STRUCTURE — CRACKED (NLG WW)

FOUND NOSE LANDING GEAR ACTUATOR UPPER SUPPORT STRUCTURE CRACKED AT LOWER INBOARD FLANGE AREA JUST AFT OF WEB. BLENDED OUT CRACKED AREA PER EA PAO-LAX-95-0041RE.

Part: PANEL — TORN (TE MIDFLAP)

FOUND PANEL TORN AT LEFT WING INBOARD MIDFLAP BETWEEN NR 3 AND NR 4 FLAP TRACK FAIRINGS. REPAIRED PANEL PER SRM 51-40-04.

Part: SKIN — CRACKED (BS 2710)

FOUND 4 INCH CRACK IN FUSELAGE SKIN AT STA 2710, ABOVE LEFT ELEVATOR. REPAIRED PER SRM 53-30-03.

Part: BOLT — CORRODED (CARGO DOOR)

FOUND RUST ON BOLT AND HOLE AT NR 3 LATCH LOWER ATTACH POINT FOR AFT CARGO DOOR. REMOVED CORROSION PER SRM 51-10-01, TREATED AND PRIMED PER SRM 51-10-02.

Part: SKIN — CRACKED (BS 2650)

FOUND 2 INCH CRACK IN FUSELAGE SKIN AT STATION 2650 ABOVE LEFT ELEVATOR. REPAIRED PER SRM 53-30-03.

Part: SKIN — DAMAGED (LT ELEVATOR)

FOUND HOLE IN LEFT INBOARD ELEVATOR UPPER SURFACE WITH HONEYCOMB EXPOSED. REPAIRED PER SRM 51-40-15.

Part: FIRE LIGHT — ILLUMINATED (APU)

DURING PREFLIGHT CHECK, FOUND APU FIRE HANDLE HAD LIGHTS ON WITH NO BELL. FEO PULLED THE FIRE HANDLE, LIGHT REMAINED ON, FEO FIRED THE FIRE BOTTLE AND LIGHT WENT OUT. APU PLACED ON DMI NOT TO BE USED. REPLACED BOTTLE AND SQUIB PER MM 26-22-01. APU OPS DURING RUN OK, UNABLE TO DUPLICATE ON GROUND. RETURNED TO SERVICE.

Part: T2 TURBINE BLADE — FAILED (NR 1 ENGINE)

NR 1 ENGINE FL 19,000 COMPRESSOR STALL WITH EGT RISE, PRECAUTIONARY ENGINE SHUTDOWN. FOUND TWO FAILED T2 TURBINE BLADES. ENGINE TO BE REPLACED PER POLAR WORK CARDS.

Part: LIMITER SPRING — BROKEN (LT CONTROL WHEEL)

FIRST OFFICER'S CONTROL WHEEL HAS 2 DEGREES PLAY BEFORE GETTING ANY AILERON MOVEMENT. CAPTAIN'S CONTROL WHEEL OK. FOUND AILERON CONTROL LOAD LIMITER TORSION SPRING BROKEN. REMOVED AND REPLACED LOAD LIMITER PER BOEING MAINTENANCE MANUAL 27-11-05.

Part: ENGINE — MALFUNCTIONED (NR 1)

NR 1 ENGINE AUTO DECELERATION WITHOUT THROTTLE MOVEMENT, SLOW ENGINE RESPONSE 40 MINUTES INTO FLIGHT, PRECAUTIONARY SHUT DOWN. RESTARTED ENGINE IN-FLIGHT, ALL NORMAL AFTER RESTART. INSPECTED TAIL PIPE AND BLEEDS FOR FOD, PULLED 8TH STAGE CHECK VALVE AND DUCT INSPECTED FOR BLADE DAMAGE, INSPECTED 8TH STAGE CHECK VALVE AND DUCT, CHECKED THE SUMP OF THE FUEL CONTROL FOR WATER, CHECKED BURNER SENSE LINE, C/W DECAY CHECK OF PRECOOLER, CHECKED CHIP DETECTORS, NO DEFECTS FOUND, GROUND RUN OK.

Part: STRINGER — CRACKED (BS 1778)

S34L CRACKED IN RADIUS, BS 1778 AT OLD SET MARK. REPLACED STRINGER.

Part: FITTING — CRACKED (BS 1480)

LEFT BODY LANDING GEAR RETRACT ACTUATOR UPPER FITTING CRACKED, BS 1480 BULKHEAD. REPLACED FITTING.

Part: LIGHTS — SMOKING (FLIGHT DECK)

ACRID TYPE SMELL NOTED INITIALLY DURING CLIMB THRU FL 280, 3 MINUTES LATER OBSERVED FAINT SMOKE FROM LEFT GLARESHIELD. TURNED OFF ALL INTSTRUMENT BACK GROUND LIGHTS SMOKE AND ODOR STOPPED, TURNED LIGHTS ON 1 AT A TIME SMOKE AND ODOR DID NOT RETURN. MAINTENANCE AT ORD INSPECTED BEHIND GLARESHIELD, UNABLE TO LOCATE ANY UNITS OVERHEATED.

Part: FRAME — CORRODED (BS 1060)

CORROSION AT BS 1060 FRAME UNDER RIGHT FAIRING. CORROSION REMOVED PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01.

Part: BRACKET — CORROSION (NR 14 LE FLAP)

CORROSION ON U-CHANNEL FAIRING ON HINGE BRACKET, INBOARD HINGE OF NR 14 LEADING EDGE FLAP. MANUFACTURED BRACKET PER BOEING SRM 51-20-01, INSTALLED PER 51-30-02.

Part: RIB — CRACKED (WS 850)

CRACK ON LEFT WING LEADING CAVITY WS 850 FORGED RIB AT THE AFT UPPER LEFT SIDE CHORD. MANUFACTURED REINFORCEMENT PER BOEING SRM 57-20-03, INSTALLED PER BOEING SRM 51-30-02.

Part: RIB — CRACKED (WS 960)

CRACKED FORGE RIB LEFT WING LEADING EDGE CAVITY WS 960 AFT RIGHT SIDE UPPER CHORD. MANUFACTURED REINFORCEMENT PER BOEING SRM 57-20-03, INSTALLED PER SRM 51-30-02.

Part: SKIN — CRACKED (NR 4L DOOR)

CRACK IN SKIN AT NR 4L DOOR LOWER HINGE CUTOUT. REPAIRED BY BLEND OUT, WITHIN LIMITS PER BOEING SRM 52-00-02.

Part: PRESSURE DECK — CORRODED (BS 1280-1400)

CORROSION ON PRESSURE DECK WEBS RBL 11 BETWEEN BS 1280 AND 1400 RBL 33 BS 1300 TO 1400. MANUFACTURED AND INSTALLED REINFORCEMENT PER BOEING SRM 53-10-07 FIG 2 DETAIL 2.

Part: RIB — CRACKED (WS 800)

CRACKED FORGED RIB LEFT WING LEADING EDGE CAVITY WS 800. (2 CRACKS ON AFT UPPER LEFT SIDE CHORD). MANUFACTURED REINFORCEMENT PER BOEING SRM 57-20-03 INSTALLED PER BOEING SRM 51-30-02.

Part: SKIN — CORRODED (BS 1820-1840)

SWELLING ON EXTERNAL SKIN BETWEEN BS 1820 AND 1840 AT S47R. REMOVED FASTENERS FROM SWELLED AREA, REMOVED CORROSION FROM SKIN PER SRM 51-10-01, WITHIN LIMITS PER 53-10-01, INSTALLED FASTENER PER SRM 53-10-01.

Part: INTERCOSTAL — CRACKED (BS 500-520)

CRACKS ON INTERCOSTAL AT S30R BETWEEN BS 500 AND 520. MANUFACTURED NEW INTERCOSTAL PER BOEING SRM 53-10-21, INSTALLED PER 51-30-02.

Part: SKIN — CORRODED (BS 1800-1820)

SWELLING ON EXTERNAL SKIN BETWEEN BS 1800 AND 1820 AT S50L. REMOVED CORROSION PER BOEING SRM 51-10-01.

Part: RIB — CRACKED (WS 930)

CRACKED UPPER LEFT CHORD ON FORGE RIB AT WS 930 LEFT WING LEADING EDGE CAVITY. MANUFACTURED REINFORCEMENT PER BOEING SRM 57-20-03, INSTALLED PER SRM 51-30-02.

Part: STRINGER — CORRODED (CABIN)

CORROSION IN JOINT S6R TO RIGHT SIDE. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02.

Part: FITTING — CORRODED (BS 1920)

CORROSION IN CONNECTING FITTING TO BS 1920 RIGHT SIDE S40R TO S41R. INSTALLED NEW FITTING PER BOEING SRM 51-30-02.

Part: Z-ANGLE — CORRODED (BS 1240)

CORROSION ON SUPPORT-Z AT BS 1240 BETWEEN LBL 40 AND LBL 80. REMOVED CORROSION PER BOEING SRM 51-10-01.

Part: SKIN — TORN (BS 2598)

SKIN TORN AND PARTLY SEPARATED AT BS 2598 ABOVE STABILIZER FAIRING. REPAIRED PER IAI ENGINEERING ORDER MF-MAN B47-53-83977.

Part: POST — CRACKED (BS 440)

CRACK IN LOWER POST NEAR ATC INSTRUMENT BS 440 BETWEEN S40R AND S41R. REPAIRED PER BOEING SRM 51-40-03.

Part: SKIN — CRACKED (BS 400)

NOSE WHEEL WELL BS 400 LEFT AND RIGHT CORNERS CRACKED. REPAIRED PER SB 53-2305.

Part: BRACKETS — CRACKED (RT MLG DOOR)

TWO CRACKED BRACKETS, RIGHT WING GEAR LOWER SHOCK STRUT DOOR. MANUFACTURED AND INSTALLED BRACKETS PER BOEING SRM 51-20-01 AND 51-30-02.

Part: BRACKET — BROKEN (BS 1260)

BRACKET RIGHT WING WHEEL WELL AT CEILING BS 1260 INBOARD SIDE HYDRAULIC LINE CLAMP. MANUFACTURED AND INSTALLED PER BOEING SRM 51-20-01 AND 51-30-02.

Part: ANGLE — CORRODED (BS 1920-1960)

CORROSION ON THE FLOOR PROFILE ANGLE BETWEEN BS 1920 AND 1960, LEFT AND RIGHT SIDES AT BL 55. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01.

Part: RETAINER — CORRODED (RT MLG DOOR)

CORRODED DOOR SEAL RETAINER RIGHT BODY GEAR SHOCK STRUT DOOR. REPLACED SEAL, INSTALLED PER BOEING SRM 51-30-02.

Part: ANGLE — CORRODED (RT MLG DOOR)

CORROSION ON RIGHT BODY GEAR SIDE STRUT INBOARD DOOR UPPER ANGLE. MANUFACTURED NEW ANGLE INSTALLED PER BOEING SRM 51-30-02.

Part: SKIN — CORRODED (LT MLG DOOR)

CORROSION UNDER SEAL RETAINER LEFT BODY GEAR WHEEL INBOARD DOOR AFT WEB. INSTALLED NEW WEB SKIN AND FASTENERS PER BOEING SRM 51-30-02.

Part: ANGLE — CORRODED (LT MLG DOOR)

CORROSION ON LEFT BODY GEAR SIDE STRUT INBOARD DOOR UPPER ANGLE. REPLACED ANGLE AND INSTALLED PER BOEING SRM 51-30-02.

Part: SKIN — CRACKED (LT MLG DOOR)

CRACKS ON INNER SKIN LEFT BODY GEAR WHEEL WELL INBOARD DOOR. INSTALLED NEW SKIN AND FASTENERS PER BOEING SRM 51-30-02.

Part: STIFFENER — BROKEN (BS 2240-2280)

BROKEN STIFFENERS, 2 BETWEEN BS 2240 AND 2280 LBL 33 AND 56. MANUFACTURED NEW STIFFENERS PER BOEING SRM 51-40-03.

Part: ANGLE — CRACKED (BS 540-560)

CRACK IN FLOOR ANGLE BETWEEN BS 540 AND 560 LBL 122. REPAIRED PER BOEING SRM 51-40-04.

Part: SHEAR TIE — DAMAGED (BS 520-540)

DAMAGED SHEAR TIE BETWEEN BS 520 AND 540 LBL 65. REPAIRED PER BOEING SRM 51-40-02.

Part: SUPPORT — MISSING (BS 740)

MISSING RISER SUPPORT UPPER DECK BS 740 LEFT SIDE ON FRAME WL 360. INSTALLED RISER PER BOEING SRM 53-10-21 AND 51-30-02.

Part: FLOOR PANEL — DAMAGED (COCKPIT)

DAMAGE AND SURFACE CORROSION ON PANEL BETWEEN CAPTAINS SEAT RAILS. MANUFACTURED REPLACEMENT PANEL PER BOEING SRM 51-20-01 AND 51-30-02.

Part: STRINGER — CRACKED (BS 480)

CRACK IN S38R AT BS 480. REPAIRED PER BOEING SRM 53-10-03 FIG 3.

Part: WEB — CORRODED (BS 1920)

CORROSION ON UPPER CHORD WEB AT BS 1920 RBL 55. REPLACED STRAP INSTALLED PER BOEING SRM 51-30-02.

Part: EYE BOLTS — CORRODED (NR 1 PYLON)

PYLON SKIRT NR 1 SUPPORT ROD EYE BOLTS CORRODED. INSTALLED NEW ROD PER BOEING M/M 20-50-01.

Part: FITTING — CRACKED (BS 1820)

CRACK ON FITTING AT BS 1820 S40R. REPLACED FITTING, INSTALLED PER BOEING SRM 51-30-02.

Part: BRACKET — CRACKED (NR 1 PYLON)

CRACKED BRACKET NR 1 PYLON NS 253 INTERNAL ON LEFT WALL. MANUFACTURED NEW BRACKETS PER BOEING SRM 54-10-02.

Part: COWLING — DAMAGED (NR 3 ENGINE)

DAMAGE ON NR 3 ENGINE LEFT FAN COWL EXTERIOR SKIN. REPAIRED PER BOEING SRM 54-30-03.

Part: BULKHEAD — CORRODED (BS 1000)

CORROSION UNDER BOLTS BS 1000 LEFT SIDE. SURFACE CORROSION REWORKED AND TREATED PER BOEING SRM 51-10-02, WITHIN LIMITS.

Part: SKIN — CORRODED (CARGO DR CUTOUT)

SURFACE CORROSION ON HI-LOCK HEADS, ON EXTERNAL SKIN MAIN SIDE CARGO DOOR CUTOUT. REMOVED CORROSION PER BOEING SRM 51-10-01.

Part: CHORD — CRACKED (NLG WW)

CRACK ON CHORD RIGHT SIDE NOSE WHEEL CORNER. REPAIRED PER BOEING DRAWING 141U1098 (SB 53-2272).

Part: TURBINE CASE — CRACKED (NR 2 ENGINE)

ENGINE NR 2 S-FLANGE AT 2 O'CLOCK IS CRACKED IN TWO PLACES ONE ON THE OD AND ONE FROM RAIL TO CASE OF TURBINE. REPAIRED PER 72-53-01

Part: SKIN — SEPARATED (LT TE AFT FLAP)

LEFT WING OUTBOARD FLAP UPPER SURFACE 2 POINTS OF SEPARATION. REPAIRED PER BOEING SRM 51-40-06.

Part: ANGLE — CORRODED (BS 1240-1260)

CORROSION ON SUPPORT ANGLE FOR FLOOR, BETWEEN BS 1240 AND 1260 LBL 100. REPLACED ANGLE PER BOEING SRM.

Part: SKIN — CRACKED (CARGO DR CUTOUT)

CRACK ON AFT BULK CARGO DOOR CUTOUT, AT INTERNAL LOWER FORWARD CORNER. REPAIRED PER BOEING SRM 51-40-10.

Part: COWLING — CORRODED (NR 3 ENGINE)

SURFACE CORROSION AND LOOSE RIVETS ON NR 3 ENGINE COWLING, RIGHT EXTERIOR SURFACE SKIN. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS. REPLACED LOOSE RIVETS.

Part: SPOILER — CRACKED (RT WING)

CRACK AT SKIN NEAR PCU FITTING ON NR 7 SPOILER RIGHT WING. REPAIRED PER BOEING SRM 51-40-06.

Part: COWLING — CORRODED (NR 3 ENGINE)

SURFACE CORROSION ON NR 3 ENGINE RIGHT COWLING INTERIOR SURFACE SKIN. REMOVED CORROSION PER BOEING SRM 51-10-01.

Part: EXHAUST BELLOW — CRACKED (APU)

APU EXHAUST BELLOW BENT AND CRACKED. REPLACED BELLOW.

Part: BRACKET — BROKEN (NR 3 ENGINE)

BROKEN HOLDING BRACKET FOR SUPPORT ROD NR 3 ENGINE LEFT COWLING. MANUFACTURED BRACKET PER BOEING SRM 51-20-02, INSTALLED PER 51-30-02.

Part: SKIN — CORRODED (BS 1000)

CORROSION FUSELAGE SKIN EXTERNAL AND INTERIOR, BS 1000 BETWEEN S38L AND S40L. REPAIRED PER EO B747-53-84022-A40-010.

Part: SKIN — CRACKED (BS 520)

CRACK AROUND FASTENER AT BS 520 S43R. REPAIRED PER BOEING SRM 53-30-03 FIG 47 SHEET 3.

Part: ANGLE — CRACKED (VERT STAB)

CRACK ON VERTICAL STABILIZER AT STA 232.5 LEFT ANGLE ON NUTPLATE STRIP. REPAIRED PER BOEING SRM 51-40-04.

Part: SKIN — CORRODED (RT WING)

SURFACE CORROSION ON LOWER RIGHT WING SKIN BETWEEN WBS 254 AND 614. REMOVED CORROSION PER BOEING SRM 57-10-01.

Part: FITTING — PLUGGED HOLE (BS 1740)

BS 1740 S4L ON THE LOWER FORWARD FITTING THAT CONNECTS THE INTERCOSTAL TO THE FRAME ON LEFT SIDE OF THE T-CHORD HAS 2 PLUG HOLES 1.8750 INCHES IN DISTANCE AND SECOND .3750 INCH IN DISTANCE FROM EXISTING HILOCK. INSTALLED STRAP PER IAI E.O. MF-MAN-B47-53-84008.

Part: WEB — CRACKED (BS 1245)

CRACK IN WEB AT BS 1245 RBL 108 RIGHT WING GEAR WHEEL WELL. REPAIRED PER BOEING SRM 53-10-07 FIG 16.

Part: SKIN — CORRODED (BS 1319)

SURFACE CORROSION IN LEFT WING GEAR WHEEL WELL AT BS 1319 LEFT SIDE. REPAIRED PER BOEING SRM 51-40-04 FIG 3.

Part: HINGE — CORRODED (FWD CARGO DOOR)

CORROSION LOWER CARGO DOOR EXTERNAL UPPER HINGE SEGMENTS. REMOVED CORROSION PER BOEING SRM 51-10-01, 51-10-02.

Part: SKIN — CORRODED (FWD CARGO DOOR)

CORROSION ON FORWARD CARGO DOOR HINGE OUTER SIDE. REMOVED CORROSION PER BOEING SRM 51-10-01 TREATED PER 51-10-02.

Part: BULKHEAD — CORRODED (BS 1350)

SURFACE CORROSION ON LEFT BS 1350 BULKHEAD, AT BL 76 LOWER CHORD. REWORKED PER BOEING SB 53-23-10 AND SRM 51-10-02.

Part: SKIN — CORRODED (WS 294-614)

SURFACE CORROSION ON LOWER SKIN LEFT WING BETWEEN WS 294 AND 614. REMOVED AND TREATED PER BOEING SRM 51-10-01, WITHIN LIMITS PER 57-10-01.

Part: PANEL — BROKEN (RT MLG DOOR)

BROKEN FIBERGLASS ON RIGHT WING GEAR LOWER SHOCK STRUT DOOR AT AFT SIDE. REPAIRED PER BOEING SRM 51-40-09.

Part: WEB — CRACKED (LT MLG DOOR)

CRACK ON LEFT BODY GEAR SIDE STRUT INBOARD DOOR LOWER WEB. REPAIRED PER BOEING SRM 51-40-01.

Part: ANGLE — BROKEN (WING TO BODY)

BROKEN BRACKET NEAR RIGHT BODY GEAR OUTBOARD SHOCK STRUT DOOR BRACKET SUPPORTS BODY TO WING FAIRING. MANUFACTURED NEW BRACKET PER BOEING SRM 51-40-02, INSTALLED PER 51-30-02.

Part: INTERCOSTAL — BROKEN (BS 440-460)

BROKEN INTERCOSTAL MAIN DECK BETWEEN FLOORBEAMS BS 440 AND 460 APPROXIMATLY RBL 50. REPLACED INTERCOSTAL INSTALLED PER BOEING SRM 51-30-02.

Part: SKIN — CRACKED (BS 740-760)

CRACKS IN FUSELAGE SKIN BETWEEN BS 740 AND 760 S26R. REPAIRED PER BOEING SRM 53-30-03 FIG 1.

Part: WEB — CRACKED (BS 1241)

CRACK ON PRESSURE DECK WEB BS 1241 RBL 106. TRIMMED AREA TO REMOVE CRACK PER BOEING SRM 53-10-07 FIG 16 DETAIL 2.

Part: BLKHD STRINGERS — CRACKED (BS 400)

TWO CRACKS AT FORWARD BS 400 BULKHEAD STRINGER S44L AND S44R, AT CORNER AFT O WHEEL WELL AND CRACK AT BS 400 AROUND FASTENER. REPAIRED PER BOEING SB 53-23-05 AND SRM 53-30-03 FIG 35.

Part: BRACKET — CORRODED (BS 1241)

SHEARED HI-LOC DUE TO CORRODED BRACKET AT BS 1241 RBL 106. REPLACED BRACKET AND FASTENER PER BOEING SRM 51-20-01 AND 51-30-02.

Part: COWLING — CRACKED (APU)

APU RIGHT COWLING FORWARD EDGE CRACKED AND 2 RIVETS SHEARED. REPAIRED PER BOEING SRM 51-10-01 AND 51-30-02.

Part: ANGLE — BROKEN (NR 3 PYLON)

BROKEN INTERNAL FRAME ANGLE CORNER NR 3 PYLON NS 270. REPAIRED PER BOEING SRM 54-10-02.

Part: SUPPORT — CORRODED (BS 2000)

CORROSION IN U-SUPPORT, SUPPORTING THE FAIRINGS IN THE UPPER SIDE BS 2000 RBL 87. REPAIRED PER BOEING SRM 51-40-03.

Part: SKIN — CORRODED (BS 1940)

SWELLING ON EXTERNAL SKIN AT BS 1940 S47R. REWORKED AND TREATED PER BOEING SRM 51-10-02, WITHIN LIMITS, INSTALLED FASTENERS PER 51-30-02.

Part: ANGLE — CORRODED (BS 1320-1350)

CORROSION ON SUPPORT ANGLE FOR FLOOR MAIN DECK WL 178 LEFT SIDE BETWEEN BS 1320 AND 1350. REPLACED SUPPORT ANGLE, INSTALLED PER BOEING SRM 51-30-02.

Part: ANGLE — CRACKED (WS 630)

RIGHT WING LEADING EDGE CAVITY WS 630 RIB TO LEADING EDGE CONNECTION ANGLE IS CRACKED. REPLACED ANGLE MANUFACTURED PER BOEING SRM 51-20-02, INSTALLED 51-30-02.

Part: SKIN — CORRODED (BS 1940)

SWELLING AND PROTRUDING RIVETS IN FUSELAGE SKIN, AT BS 1940 BETWEEN S47L AND S51L. REWORKED AREA AND TREATED PER BOEING SRM 51-10-02, WITHIN LIMITS, INSTALLED PER 51-30-02.

Part: SKIN — CORROSION (BS 1800-1860)

SWELLING IN FUSELAGE SKIN RIGHT SIDE BETWEEN BS 1860 AND 1800 S47R. SWELLING AREA REWORKED AND TREATED PER BOEING SRM 51-10-02, WITHIN LIMITS, INSTALLED PER 51-30-02.

Part: CHORD — CORRODED (BS 1350)

CORROSION ON LOWER FLANGE OF THE LOWER CHORD LANDING GEAR BEAM, AT BS 1350 LEFT AND RIGHT. REWORKED PER BOEING SB 53-2310 WITHIN LIMITS.

Part: COWLING — CRACKED (NR 3 ENGINE)

CRACK ON FORWARD EDGE NR 3 ENGINE RIGHT COWLING EXTERIOR SURFACE SKIN. REPAIRED PER BOEING SRM 54-30-03.

Part: SKIN — CORROSION (BS 1789-1800)

SWELLING IN FUSELAGE SKIN BETWEEN BS 1780 AND 1800 AT S49R. AREA REWORKED AND TREATED PER BOEING SRM 51-10-02, WITHING LIMITS, INSTALLED FASTENERS PER 51-30-01.

Part: BRACKET — BROKEN (WS 1168)

BROKEN BRACKET RIGHT WING LEADING EDGE CAVITY WS 1168. MANUFACTURED PART PER BOEING SRM 51-20-02, INSTALLED PER 51-30-02.

Part: COWL FRAME — CRACKED (NR 4 ENGINE)

CRACKED FRAME 3RD HOOK NR 4 ENGINE RIGHT MAIN COWL UPPER. REPAIRED PER BOEING SRM 54-30-03.

Part: CLIPS — CORRODED (BS 2060-2080)

CORRODED FASTENERS AND CLIPS AT MAIN DECK WINDOWS BETWEEN BS 2060 AND 2080. REPLACED CLIPS AND FASTENERS PER BOEING MAINT MANUAL 56-21-01.

Part: COWLING — CORRODED (NR 2 ENGINE)

SURFACE CORROSION ON INTERIOR SURFACE SKIN OF NR 2 ENGINE RIGHT COWLING. REMOVED CORROSION PER BOEING SRM 51-10-01.

Part: COWLING — CORRODED (NR 3 ENGINE)

SURFACE CORROSION ON NR 3 ENGINE LEFT COWLING INTERIOR. REMOVED CORROSION PER BOEING SRM 51-10-01.

Part: DOOR — CRACKED (LT MLG)

CRACK LEFT WING LANDING GEAR UPPER HALF DOOR FWD SIDE EDGE. REPAIRED PER BOEING SRM 51-40-03.

Part: COWL — CRACKED (NR 2 ENGINE)

CRACK WITH STOP HOLE ON EXTERIOR SURFACE O, NR 2 LEFT COWLING, UNDER CSD OIL FILL PANEL. REPAIRED PER BOEING SRM 51-40-02.

Part: COWLING — CORRODED (NR 2 ENGINE)

SURFACE CORROSION ON RIVET HEADS AND SHEARED RIVETS ON THE EXTERIOR SURFACE OF NR 2 LEFT COWLING. REPLACED RIVETS PER BOEING SRM 51-30-02.

Part: FITTING — CRACKED (1240)

CRACKS ON S3L, BS 1240 FWD SIDE. REPLACED FITTING PER BOEING SRM 51-30-02.

Part: FIITING — CORRODED (BS 1240)

CRACKS AND CORROSION ON FITTINGS TO S1L AND S1R, BS 1240. REPLACED FITTINGS INSTALLED PER BOEING SRM 51-30-02.

Part: BRACKET — CRACKED (APU COMPT)

CRACKED APU AFT MOUNT SUPPORT ROD MOUNTING BRACKET IS CRACKED BOTH SIDES. REPAIRED PER BOEING SRM 51-20-02.

Part: SEAL GROOVE — CRACKED (CARGO DOOR)

MAIN SIDE CARGO DOOR FWD INTERIOR SIDE PRESSURE SEAL GROOVE IS DAMAGED AND CRACKED IN 2 PLACES. REPAIRED PER BOEING SRM 51-40-01.

Part: T-CHORD — DOUBLE DRILLED (BS 1950-2000)

BETWEEN BS 1950 AND BS 2000 ON S4L ON T-CHORD, FOUND DOUBLE HOLES AND OVAL HOLES. REPAIRED PER IAI E.O. MF-MAN-B47-53-83972.

Part: T-CHORD — DOUBLE DRILLED (BS 1700-1750)

BETWEEN BS 1700 AND BS 1750 AT S4L ON THE T-CHORD, FOUND DOUBLE HOLES AND OVAL HOLES. T-CHORD REPLACED WITH NEW PART PER E. O. MF-MAN-B47-53-83972.

Part: WEB — CRACKED (BS 1394)

CRACK RIGHT BODY GEAR WHEEL WELL BS 1394 OUTBOARD WALL INNER BOX CAVITY WEB. REPAIRED PER BOEING SRM 51-40-02.

Part: SKIN — CORRODED (BS 1372)

SURFACE CORROSION RIGHT BODY GEAR WHEELWELL BS 1372 OUTBOARD WHEELWELL INNER BOX CAVITY REPAIRED PER IAI E.O. MF-MAN-B47-53-8400.

Part: WEB — CRACKED (BS 1480)

CRACK IN THE SUPPORTING WEB NR 294C BS 1480 RIGHT. REPAIRED PER 51-40-09.

Part: STUB FRAME — CRACKED (BS 1394)

CRACKS ON DOUBLER AND STUB FRAME AT BS 1394 BETWEEN RBL 98 AND RBL 125. INSTALLED DOUBLER PER BOING SRM 53-10-22.

Part: FITTING — CORRODED (RT LE FLAP)

CORROSION IN BOTH HINGES FITTING SIDES RIGHT WING KRUGER LEADING EDGE FLAP NR 15. MANUFACTURED PLATE SUPPORT PER 51-20-01, INSTALLED PER 51-30-02.

Part: PANEL — SEPARATED (BS 1200)

SEPARATION ON AIR CONDITIONING BAY PANEL, BS 1200 LEFT PANEL ADJACENT TO WING ROOT. REPAIRED PER BOEING SRM 51-40-09.

Part: PANEL — SEPARATED (RT INBD TE FLAP)

SEPARATION, RIGHT WING INBOARD AFT FLAP OUTBOARD CORNER. REPAIRED PER BOEING SRM 51-40-09.

Part: FITTING — CRACKED (BS 434)

CRACKED FITTING PN 65B07922-4, AT NR 1R DOOR BS 434 BETWEEN S23R AND S24R. REPLACED PART, INSTALLED PER BOEING SRM 51-30-02.

Part: TIE CLIP — CORRODED (BS 1160)

CORROSION IN TIE CLIP AT FRAME BS 1160 AT S4R. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01.

Part: SKIN — DELAMINATED (RT TE FOREFLAP)

DELAMINATION RIGHT INBOARD FOREFLAP LOWER SURFACE NEAR INBOARD LINK, MID LINK AND INBOARD ARM. REPAIRED PER BOEING SRM 51-40-06.

Part: SEAL — CRACKED (RT MLG DOOR)

CRACK IN RIGHT BODY GEAR SHOCK STRUT OUTBOARD DOOR LOWER EDGE. INSTALLED NEW SEAL AND FASTENERS.

Part: PANEL — DELAMINATED (RT TE FLAP)

HONEY COMB SEPARATION AND DRILLED HOLES AT INTERNAL SIDE RIGHT WING OUTBOARD AFT FLAP UPPER PANEL. REPAIRED PER BOEING SRM 51-40 06.

Part: SKIN — CORRODED (RT MLG DOOR)

SURFACE CORROSION ON RIGHT BODY GEAR SHOCK STRUT INBOARD DOOR. REMOVED CORROSION PER BOEING SRM 51-10-01.

Part: DOOR — CRACKED (RT MLG)

RIGHT BODY GEAR SHOCK STRUT INBOARD DOOR AFT SIDE HAS 6 IN CRACK AND 2 DAMAGED AREAS. REPLACED SEAL, RIB AND ANGLE, INSTALLED PER SRM 51-30-02.

Part: FRAME — CRACKED (NR 5R DOOR)

CRACK ON FORWARD FRAME LOWER STOP FITTING AREA ENTRY DOOR NR 5. REPAIRED PER BOEING SRM 51-40-02 FIG 1.

Part: BOLTS — CORRODED (BS 100)

CORROSION AROUND BOLTS AT BS 100 LBL 6. CORROSION REMOVED PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01.

Part: DOOR — DAMAGED (LT MLG)

DAMAGE LEFT BODY GEAR INBOARD SIDE STRUT DOOR AFT SIDE AFT UPPER CORNER. REPAIRED PER BOEING SRM 52-80-02.

Part: DOOR — CRACKED (LT MLG)

LEFT BODY INBOARD SIDE STRUT DOOR AFT LOWER CORNER CRACKED AND PARTIALLY TORN. REPAIRED PER BOEING SRM 52-80-02.

Part: DOOR — DAMAGED (LT MLG)

LEFT BODY GEAR INBOARD DOOR AFT SIDE UPPER AREA DAMGED. REPAIRED PER BOEING SRM 52-80-02.

Part: STRINGER — CORRODED (BS 520)

CORROSION ON EDGE S30R AT BS 520. REPAIRED PER BOEING SRM 53-10-03.

Part: STRINGER — CORRODED (BS 980-1000)

CORROSION ON S35L BETWEEN BS 980 AND 1000. REPAIRED PER BOEING SRM 53-10-03.

Part: BULKHEAD — CRACKED (BS 2360)

CRACK .25 INCH IN LENGTH ON BS 2360, BULKHEAD SKIN BY S46R. REPAIRED PER BOEING SRM 53-10-04, SB 53-2275 AND 53-10-04.

Part: STRINGER — CORRODED (BS 1200)

CORROSION IN S4L, AT BS 1200. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01.

Part: STRINGER — CRACKED (BS 2368)

CRACK ON SIDE OF S46L BS 2368. REPAIRED PER BOEING SRM 53-10-03 FIG 2.

Part: BLKHD PANEL — PATCH PEELING (BS 1241)

FIBERGLASS PANEL PATCH IS PEELING OFF ON BS 1241 LOWER CANTED BULKHEAD. REPAIRED PER BOEING SRM 51-40-09.

Part: SKIN — CORRODED (LT MLG)

BULGES ALONG SEAM LEFT BODY GEAR WHEEL WELL INBOARD DOOR EXTERNAL SKIN. REMOVED RIVETS, REMOVED CORROSION PER BOEING SRM 51-10-01, TREATED PER 51-10-02, INSTALLED PER SRM 51-30-01.

Part: DOOR — CRACKED (RT MLG)

CRACKED HOLE AND POPPED RIVET RIGHT BODY GEAR GEAR SHOCK STRUT INBOARD DOOR NEAR CAUTION DECAL. REPAIRED PER BOEING SRM 52-80-02.

Part: STRINGER — CORRODED (BS 740-760)

CORROSION IN S43R BETWEEN BS 740 AND 760. REPAIRED PER 53-10-03 FIG 1.

Part: PANEL — CRACKED (LT MLG)

LEFT BODY GEAR SIDE STRUT DOOR UPPER INSPECTION PANEL ABOVE ROD FITTING CRACKED. REPLACED PANEL INSTALLED PER BOEING SRM 51-30-02.

Part: BRACKET — DEFORMED (BS 1600-1620)

DEFORMED BRACKET IN CONNECTION TO ANGLE SUPPORT FLOOR PANEL BETWEEN BS 1600 AND 1620 WL 198. REPAIRED PER BOEING SRM 51-40-01.

Part: BRACKET — CRACKED (NR 2 PYLON)

2 CRACKS ON NR 2 PYLON SKIRT FORWARD MOUNTING BRACKET. FABRICATED NEW BRACKET PER BOEING SRM 54-50-02.

Part: SKIN — DELAMINATED (LT WING)

INNER SKIN DELAMINATION AT OUTBOARD BAY UNDER PANEL LEFT WING OUTBOARD MIN FLAP. REPAIRED PER BOEING SRM 51-40-06.

Part: STRINGER — CORRODED (BS 1200)

CORROSION IN S4R AT BS 1200. REMOVED AND TREATED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER BOEING SRM 53-10-01.

Part: DOOR — CRACKED (RT MLG)

SMALL CRACK ON AFT INNER EDGE RIGHT BODY GEAR SHOCK STRUT INBOARD DOOR. REPLACED PART.

Part: FLOOR — CORRODED (BS 1280-1490)

CORROSION ON FLOOR BS 1280 TO 1300 LBL 7 TO 14 AND BS 1416 TO 1419 LBL 2 TO 14. REPAIRED PER BOEING SRM 53-10-07.

Part: ANGLE — BROKEN (BS 980)

BROKEN ANGLE ON BS 980 NEAR S43L. REPAIRED PER BOEING SRM 51-30-02.

Part: DOOR — CRACKED (RT MLG)

CRACK RIGHT BODY GEAR SHOCK STRUT INBOARD DOOR FORWARD EXTERNAL SKIN NEAR FIRST HINGE. REPAIRED PER 52-80-02 FIG 1.

Part: SKIN — CRACKED (LT MLG DOOR)

SMALL CRACK AT AFT END CORNER LEFT BODY GEAR WHEEL WELL INBOARD DOOR SKIN. INSTALLED NEW DOOR SKIN PER SRM 51-30-02.

Part: STIFFENER — CRACKED (LT WING)

CRACK IN THE LEFT SIDE TRAILING EDGE STIFFENER, SEAL RIB ASSY LOWER, SRM 57-20-02 FIG 2 INTE 1. REPAIRED PER SRM 51-40-04.

Part: CHORD — CRACKED (NR 4 PYLON)

EDDY CURRENT INSPECTION PER SB 54-2159, FOUND CRACK IN NR 4 PYLON HORIZONTAL CHORD LEFT SIDE. REAMED HOLE, INSTALLED FREEZE PLUG PER BOEING SB 54-2159, CRACK CLEANED UP.

Part: SKIN — CRACKED (DOOR 1 L)

CRACK IN 1L DOOR LOWER HINGE CUTOUT SKIN, LOWER FORWARD CORNER. REPAIRED PER BOEING SRM 52-00-02.

Part: SKIN — DAMAGED (LT MLG DOOR)

DAMAGED LEFT BODY GEAR WHEEL WELL INBOARD DOOR INNER SKIN OUTBOARD SIDE NEAR DOOR ROD FITTING. INSTALLED NEW DOOR SKIN.

Part: SUPPORT — CORRODED (BS 1240)

CORROSION ON Z-SUPPORT AT BS 1240 BETWEEN LBL 40 AND LBL 80. CORROSION REMOVED PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01.

Part: STRINGER — CORRODED (BS 1120)

CORROSION IN S3R AT FRAME BS 1120. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01.

Part: TIE CLIP — CORRODED (BS 1200)

CORROSION IN TIE CLIP AT S2L, AT FRAME BS 1200. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01.

Part: INTERCOSTAL — CRACKED (BS 600)

CRACKED INTERCOSTAL BS 600 S26R. REPAIRED PER BOEING SRM 51-40-02.

Part: STRINGER — CORRODED (BS 1980)

LIGHT SURFACE CORROSION ON S5R AT BS 1980. REMOVED CORROSION PER BOEING SRM 51-01-01, WITHIN LIMITS PER 53-10-01.

Part: ANGLE — CRACKED (LT MLG WW)

SIDE ANGLE CRACKED AT MIDDLE AREA. REPLACED PARTS 65B11442-907, 65B11442-17 AND 65B13398-5.

Part: RIB — CRACKED (WS 950)

CRACK ON LEFT WING LEADING CAVITY WS 950 FORGED RIB AFT UPPER CHORD. REPAIRED PER BOEING SRM 57-20-03.

Part: WEB — CRACKED (WS 620)

CRACK AT AFT AUXILIARY SPAR WEB AT WS 620 AT LOWER SIDE OF STIFFENER. MANUFACTURED NEW PART PER BOEING SRM 57-20-02.

Part: WEB — CRACKED (BS 700)

CRACKS FORWARD CARGO BS 700 BETWEEN RBL 45 AND RBL 58 ON WEB. REPAIRED PER BOEING SRM 51-40-02.

Part: STRINGER — CORRODED (BS 1960)

CORROSION ON S45R BS 1960 RIGHT SIDE LOWER. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01.

Part: DOOR — DAMAGED (NLG)

DAMAGED FORWARD NOSE GEAR RIGHT DOOR LOWER EDGE. REPAIRED PER SRM 52-80-02.

Part: SKIN — DAMAGED (RT MLG DOOR)

DAMAGE TO CORNER SKIN RIGHT BODY GEAR SHOCK STRUT INBOARD DOOR AFT UPPER END. REPAIRED PER BOEING SRM 52-80-02 FIG 1.

Part: ANGLES — OVAL HOLES (FUSELAGE)

OVAL HOLES FOUND ON 2 ANGLES AND 2 WEBS WHILE MODIFYING PER SB 53-2272 DRAWING 62400003 SHEET 91A. REPLACED PARTS, INSTALLED PER DRAWING 62400003 SHEET 91A.

Part: FLOOR — TORN (BS 1660-1680)

TEAR IN FLOOR SKIN BETWEEN BS 1660 AND 1680 LBL 25. MANUFACTURED NEW PART PER BOEING SRM 51-40-02.

Part: FAIRING — MISSING (RT WING)

FIBERGLASS MISSING ON RIGHT WING REAR TRAIILING EDGE, WS UPPER FAIRING LOWER SURFACE AT UPPER FIXED FAIRING. REPAIRED PER BOEING SRM 51-40-09.

Part: STIFFENER — CRACKED (NR 2R DOOR)

CRACKED STIFFENER AT AFT SIDE MAIN DECK ENTRY DOOR 2R CUTOUT LOWER. REPAIRED PER BOEING SRM 51-40-03.

Part: BRACKET — CRACKED (NR 2 PYLON)

CRACKED BRACKET NR 2 PYLON SKIRT RETURN MODULE MOUNTING BRACKET LEFT SIDE. MANUFACTURED NEW PART PER SRM 54-12-02, INSTALLED PER 51-30-02.

Part: BRACKET — BROKEN (LT WING TE)

BROKEN SUPPORT BRACKET LEFT WING TRAILING EDGE. MANUFACTURED AND REPLACED BRACKET PER BOEING SRM 51-20-01.

Part: BULKHEAD — CORRODED (BS 1000)

CORROSION ON BS 1000 BETWEEN S45L AND S47R. CORROSION REMOVED PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01.

Part: SKIN — CUT (LT MLG DOOR)

LEFT WING LANDING GEAR INBOARD DOOR HAS A CUT ON INNER SKIN SURFACE. REPAIRED PER BOEING SRM 52-80-02-1.

Part: WEB — MISDRILLED (BS 1420)

OVAL HOLE IN THE WEB AT BS 1420 LBL 33. REPAIRED PER BOEING SB 53-2224.

Part: STRINGER — CORRODED (BS 1480)

CORROSION ON S41L BS 1480. REPAIRED PER BOEING SRM 53-10-03.

Part: PRESSURE PAN — DELAMINATED (FUSELAGE)

DELAMINATION ON APU PRESSURE PAN. REPAIRED PER BOEING SRM 51-40-09.

Part: MOUNT BRACKET — BROKEN (NR 3 SKIRT)

NR 3 SKIRT FORWARD MOUNTING BRACKET IS BROKEN. INSTALLED NEW FITTING PER BOEING SRM 51-30-02.

Part: FLANGE — CORRODED (BS 1920)

CORROSION FOUND IN THE UPPER FLANGE AT BS 1920 ABOVE S42L. REPAIRED PER BOEING SRM 53-10-28 AND SRM 51-30-02.

Part: CLIP — CORRODED (BS 1880)

CORROSION ON CLIP BS 1880 S13R. REMOVED CORROSION PER SRM 51-10-01.

Part: SEAT TRACK — BROKEN (BS 1500)

BROKEN SEAT BS 1500 LBL 75. REPLACED SEAT TRACK PER BOEING SRM 53-10-05.

Part: PANEL — DELAMINATED (LT WING)

DELAMINATION ON LEFT WING OUTBOARD PANEL. REPAIRED PER BOEING SRM 51-40-06.

Part: STRINGER — CORRODED (BS 1220)

CORROSION IN S4L AT BS 1220 UNDER TIE CLIP. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01.

Part: DOOR — CRACKED (NLG)

CRACKED AND SHEARED RIVET RIGHT NOSE GEAR STRUT DOOR. REPAIRED PER BOEING SRM 51-40-03 FIG 1.

Part: STRINGER — CORRODED (BS 2040)

SURFACE CORROSION IN S7L AT BS 2040. REMOVED PER BOEING SRM 51-10-01.

Part: SKIN — HOLE (NR 2 AFT FLAP)

HOLE IN LEFT AFT INBOARD FLAP AT LEADING EDGE NEXT TO OUTBOARD LINK. REPAIRED PER BOEING SRM 51-40-09.

Part: ANGLE — BROKEN (BS 1287)

ANGLE BROKEN AT BS 1287 UNDER BEAM RBL 112. REPLACED ANGLE PER BOEING SRM 51-40-02.

Part: SUPPORT — CRACKED (BS 580)

CRACK ON CEILING SUPPORT AT BS 580 RBL 75. REPAIRED PER BOEING SRM 51-40-03.

Part: FLOOR PANEL — DAMAGED (AFT CARGO)

AFT CARGO LEFT FORWARD FLOOR PANEL IS DAMAGED IN SEVERAL PLACES. REPAIRED PER BOEING SRM 51-40-02, FIG. 1.

Part: SILL — DAMAGED (CARGO DOOR)

DAMAGED DOOR SILL ON BULK CARGO FORWARD SIDE. REPAIR PER BOEING SRM 51-40-03.

Part: RETAINERS — CORRODED (BS 1090)

CORROSION ON ANGLE ON DOOR BS 1090 LEFT SIDE. REPLACED SEAL RETAINER FASTENERS. INSTALLED PER BOEING SRM 51-30-02.

Part: LE PANEL — DENTED (VERT STAB)

FOUR DENTS ON VERTICAL FIN LEADING EDGE PANEL. BLENDED OUT DAMAGE PER BOEING SRM 51-10-01.

Part: STRINGER — OPEN HOLES (BS 1980/1960)

S46L HAS OPEN HOLES BETWEEN BS 1980 AND 1960. INSTALLED FASTENERS PER BOEING SRM 51-30-02.

Part: HINGE — CORRODED (AFT CARGO DOOR)

CORROSION IN THE LOWER AFT CARGO DOOR HINGE SEGMENTS. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER SRM 53-10-01.

Part: SEAT TRACK — CORRODED (BS 2140-2200)

CORROSION IN SEAT TRACK BETWEEN BS 2140 AND 2200 AND LBL 98. REMOVED THE CORROSION PER BOEING SRM 51-10-01.

Part: WEB — OIL CAN (BS 2280)

OIL CAN IN THE WEB AT BS 2280 RIGHT ABOVE S36R AND S38R. REPAIRED PER BOEING SRM 53-10-04.

Part: STRAP — BROKEN (BS 747-760)

BROKEN STRAP BETWEEN BS 747 AND 760 ABOVE S36L. MANUFACTURED NEW STRAP PER BOEING SRM 53-10-21 AND 51-30-02.

Part: INTERCOSTAL — TORN (BS 860-880)

TEAR ON INTERCOSTAL AND A DENT ON ANGLE ABOVE INTERCOSTAL AT S34R BETWEEN BS 860 AND 880. REPAIRED PER BOEING SRM 51-40-02 FIG 1.

Part: SKIN — SEPARATED (RT WING TIP)

SKIN IS SEPARTATED ON RIGHT WING TIP LOWER SURFACE NEAR BASE OF HF ANTENNA. REPAIRED PER BOEING SRM 51-40-09.

Part: FLOORBEAM — CORRODED (BS 460)

CORROSION IN FLOORBEAM CAP BS 460 RBL 85. REPAIRED PER BOEING SRM 51-40-04.

Part: FRAME — CRACKED (NR 2 PYLON)

CRACKS ON BOTH SIDES OF LEFT SIDE OF AFT ENGINE MOUNT FRAME NS 222 ON NR 2 NACELLE. REPLACED DOUBLERS PER BOEING SRM 54-30-03 FIG 36.

Part: BRACKET — CRACKED (BS 1475)

CRACK IN BRACKET S28R BS 1475. REPAIRED PER BOEING SRM 51-40-03 FIG 4.

Part: STRINGER — CORRODED (BS 1420)

SURFACE CORROSION ON S9L BS 1420. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01.

Part: CLIP — CORRODED (BS 208)

SURFACE CORROSION IN TIE CLIP STRINGER S6R BS 2080. REMOVED CORROSION PER BOEING SRM 51-10-01.

Part: TE STRIP — GAPPED (NR 1 FLAP)

LEFT OUTBOARD MID-FLAP TRAILING EDGE STRIP IS GAPPED ALONG THE FLAP. REPAIRED PER BOEING SRM 51-40-09.

Part: ANGLE — CRACKED (BS 2000)

CRACK IN SUPPORT ANGLE FOR FLOOR PANEL BS 2000 RBL 15. REPAIRED PER BOEING SRM 51-40-03.

Part: STRINGER — CORRODED (BS 1900)

CORROSION IN S46L NEAR BS 1900. REPAIRED PER BOEING SRM 51-10-01 WITHIN LIMITS PER 53-10-01.

Part: BEAM — CORRODED (BS 2020)

CORROSION IN UPPER CHORD BEAM BS 2020 RBL 15. CORROSION REMOVED PER SRM 51-10-01 WITHIN LIMITS PER 53-10-01.

Part: STRIP — CRACKED (HORIZ STAB TE)

RIGHT STABILIZER TRAILING EDGE STRIP CRACKED BETWEEN NAV LIGHT AND ELEVATOR. REPAIRED PER BOEING SRM 51-40-04.

Part: ANGLE — BROKEN (BS 2040)

BROKEN SUPPORT ANGLE FOR FLOOR PANEL BS 2040 RBL 25. REPAIRED PER BOEING SRM 51-40-02.

Part: STRINGER — CORRODED (BS 1960)

CORROSION IN STRINGER S45L AT BS 1960. REMOVED CORROSION PER BOEING SRM 51-10-01 WITHIN LIMITS PER 53-10-01.

Part: SKIN — CORRODED (BS 940-980)

CORROSION IN SKIN BETWEEN BS 940 AND 980 AT S39R. REMOVED CORROSION PER BOEING SRM 51-10-01.

Part: FITTING — CORRODED (BS 2360)

CORROSION MAIN DECK AT BS 2360 S18L. FOUND CORROSION IN FITTING ATTACH FASTENERS TO THE WEB. REPLACED FITTING PER BOEING SRM 51-30-02.

Part: ANGLE — CRACKED (BS 1940)

CRACK IN SUPPORT ANGLE FOR FLOOR PANEL AT BS 1940 LBL 45. REPAIRED PER SRM 51-40-03 AND SRM 53-10-23.

Part: SKIN — DAMAGED (BS 2160)

TEAR AND DAMAGE IN BULK CARGO WALL AT BS 2160. REPAIRED PER BOEING SRM 51-40-02 FIG 4.

Part: SEAT TRACK — CORRODED (BS 620)

CORROSION IN SEAT TRACK LBL 11.33 AT BS 620. REMOVED CORROSION PER BOEING SRM 51-10-01.

Part: SKIN — DELAMINATED (NR 2 MID FLAP)

DELAMINATIONS ON LEFT INBOARD MID-FLAP UPPER SKIN SECOND ROW MOST OUTBOARD PANEL. REPAIRED PER BOEING SRM 51-40-06.

Part: SEAT TRACK — CORRODED (BS 1780-1900)

CORROSION IN TRACK RBL 45 TO RBL 25 AND LBL 25 BETWEEN BS 1900 AND BS 1780. REPAIRED PER BOEING SRM 53-10-05.

Part: BRACKET — BROKEN (FWD CARGO)

WATER TANK AIR FILTER MOUNTING BRACKET BROKEN. MANUFACTURED NEW BRACKET PER BOEING SRM 51-20-02 AND SRM 51-30-02.

Part: SPLICE — CORRODED (BS 1480)

CORROSION IN SPLICE FITTING BS 1480 S41L. REPAIRED PER BOEING SRM 53-10-23 AND SRM 51-30-02.

Part: RIB — CRACKED (WS 1042)

CRACK RIGHT WING LEADING EDGE CAVITY WS 1042, FORGED RIB UPPER CHORD FOUND WITH HFEC. REPAIRED PER BOEING SB 747-57-2116, FIG 6.

Part: CLIP — CRACKED (BS 1740)

MAIN DECK BS 1740 S16R HAS A CLIP WITH CRACK. FABRICATED NEW CLIP PER BOEING SRM 53-10-02 AND INSTALLED PER SRM 51-30-02.

Part: FASTENERS — CORRODED (BS 2360)

MAIN DECK BS 2360 IN S14R, S14L, S15L, S15R, S18R, S19R, S20R, S21R HAS CORRODED FASTENERS, REPLACED FASTENERS PER BOEING SRM 51-30-02.

Part: SKIN — CORRODED (BS 1000-1240)

CORROSION ON SHEET METAL PANELS UNDER HINGE DOORS LEFT AND RIGHT SIDES BETWEEN BS 1000 AND BS 1240. REMOVED CORROSION PER BOEING SRM 51-10-01 WITHIN LIMITS PER 53-10-01.

Part: FRAME — TEAR (BS 600)

TEAR AROUND NUTPLATE HOLE BS 600 RBL 98. REPAIRED PER BOEING SRM 51-40-03.

Part: RIBS — CRACKED (NR 1 FLAP)

LEFT OUTBOARD MID-FLAP 2 RIBS NEXT TO INBOARD FORE FLAP TRACK CRACKED. MANUFACTURED 2 RIBS PER BOEING SRM 57-10-02. INSTALLED PER 51-30-02.

Part: SKIN — DAMAGED (NR 1 FLAP)

SKIN DAMAGE LEFT OUTBOARD MID-FLAP LEADING EDGE UPPER SURFACE. REPAIRED PER BOEING SRM 51-40-09.

Part: ANGLE — CRACKED (BS 2060)

CRACK IN SUPPORT ANGLE FLOOR PANEL RBL 22 AT BS 2060. REPAIRED PER BOEING SRM 51-40-03, FIG 2.

Part: ANGLE — CRACKED (BS 2100)

CRACK IN SUPPORT ANGLE CARGO FLOOR PANEL BS 2100 RBL 75. REPAIRED PER BOEING SRM 51-40-03.

Part: STRINGER — CORRODED (BS 2240)

CORROSION IN S42L BETWEEN BS 2240-2260. CORROSION REMOVED PER BOEING SRM 51-10-01.

Part: INTERCOSTAL — CORRODED (BS 2280/2300)

CORROSION IN INTERCOSTAL NEAR S33L BETWEEN BS 2280 AND BS 2300. CORROSION REMOVED PER BOEING SRM 51-10-01.

Part: BLKHD SKIN — CORRODED (BS 2360)

CORROSION IN SKIN AT PRESSURE BULKHEAD BS 2360 S46L - S48L. CORROSION REMOVED PER BOEING SRM 51-10-01 WITHIN LIMITS PER 53-10-01.

Part: FLANGE — CORRODED (BS 2240)

CORROSION IN LOWER FLANGE AT BS 2240 AT CONNECTION TO SKIN BETWEEN S44L - W46L (LEVEL 2). REPAIRED PER SRM 53-10-23.

Part: INTERCOSTAL — CRACKED (BS 960-980)

CRACK IN INTERCOSTAL BETWEEN BS 960-980 (FLOOR BEAM) AT BRL 73. REPAIRED PER BOEING SRM 51-40-02.

Part: LE SKIN — DELAMINATED (NR 2 FORE FLAP)

LEFT WING INBOARD FORE FLAP LEADING EDGE HAS DELAMINATION AT LEADING EDGE CENTER AREA. REPAIRED PER BOEING SRM 51-40-06.

Part: PANEL — DELAMINATED (HORIZ STAB)

RIGHT STABILIZER UPPER SURFACE HAS DELAMINATION ON PANEL JUST AHEAD OF OUTBOARD ELEVATOR. PANEL REPLACED.

Part: ROD — DISCONNECTED (FSS 1100)

RIGHT WING FSS 1100 LEADING EDGE CAVITY SUPPORTING ROD FROM RIB TO LOWER SURFACE FAIRING IS DISCONNECTED FROM BRACKET. REPAIRED PER BOEING SRM 57-10-02 AND SRM 51-30-02.

Part: FLOOR PANEL — DAMAGED (BS 720-760)

DAMAGED FLOOR PANELS FORWARD CARGO LEFT SIDE AT BS 720-760. MANUFACTURED NEW PART PER BOEING SRM 53-10-02.

Part: DOOR SILL — CORRODED (BS 2235)

CORROSION AND MISSING 2 RIVETS AT BS 2235 S22L ON SILL OF DOOR 5L. CORROSION CLEANED AND TREATED PER BOEING SRM 51-10-01. FOUND WITHIN LIMITS PER BOEING SRM 53-10-01.

Part: ANGLE — CRACKED (BS 2040/2080)

CRACK IN SUPPORT ANGLE FLOOR PANEL BETWEEN BS 2040 AND BS 2080 LBL 50. REPAIRED PER BOEING SRM 51-40-03.

Part: STRAP — CORRODED (BS 680)

CORROSION ON STRAP AT BOTTOM OF MAIN DECK FLOOR BEAM BS 680 BETWEEN RBL 57 AND RBL 98. CORROSION REMOVED PER BOEING SRM 51-10-01 WITHIN LIMITS PER 53-10-01.

Part: ANGLE — CRACKED (BS 1920/2120)

DENTS AND CRACKS IN SUPPORT ANGLE FOR PANEL BETWEEN BS 2120 AND BS 1920 LBL 30. MANUFACTURED AND REPLACED PER BOEING SRM 51-30-02 AND SRM 53-10-23.

Part: SUPPORT — CRACKED (BS 600-640)

DENTS AND CRACK ON CEILING SUPPORT BETWEEN BS 600 AND BS 640, RBL 98. REPAIRED PER BOEING SRM 51-40-03.

Part: ANGLE — CORROSION (BS 1340)

CORROSION ON SUPPORT ANGLE FOR FLOOR PANEL BS 1340 RBL 22. CORROSION REMOVED PER BOEING SRM 51-10-01 WITHIN LIMITS PER 53-10-01.

Part: SUPPORT — CORRODED (BS 970)

CORROSION ON CEILING SUPPORT BS 970. MANUFACTURED NEW SUPPORT PER BOEING SRM 53-10-21. INSTALLED PER BOEING SRM 51-30-02.

Part: ANGLE — CRACKED (BS 2000)

CRACK IN SUPPORT ANGLE FOR FLOOR PANEL BS 2000 RBL 15 AND RBL 75. REPAIRED PER BOEING SRM 51-40-03.

Part: ANGLE — CRACKED (BS 2000-2020)

CRACK IN SUPPORT ANGLE FOR FLOOR PANEL RBL 25 BETWEEN BS 2000 AND BS 2020. REPAIRED PER BOEING SRM 51-40-03.

Part: SUPPORT — CORRODED (BS 660-680)

CORROSION ON CEILING SUPPORT AT BS 660-680 AND RBL 57-75. CORROSION REMOVED PER BOEING SRM 51-10-01.

Part: STRUCTURE — DAMAGED (BS 1760-1780)

CRACK AND BEND IN FLOOR RIB, GOUGE, AND HIT IN FLOOR COVER SHEET METAL BETWEEN BS 1760 AND BS 1780, RBL 25 AND RBL 45. REPAIRED PER BOEING SRM 51-40-03.

Part: ANGLE — CRACKED (BS 2040)

CORROSION AND CRACK IN SUPPORT ANGLE FLOOR PANEL BS 2040 RBL 20 TO RBL 40. REPAIRED PER BOEING SRM 51-40-03, FIG 2.

Part: STRUCTURE — DAMAGED (BS 1780-1800)

CRACK AND DENTS IN THE FLOOR COVER SHEET METAL BETWEEN BS 1780 AND BS 1800, LBL 45 AND LBL 35. REPAIRED PER BOEING SRM 53-10-23.

Part: FLOOR BEAM — CORRODED (BS 2280)

CORROSION IN THE WEB AT BS 2280 UNDER UPPER CHORD FLOOR BEAM AT WL 188 RBL 33 TO LBL 33. CORROSION REMOVED PER BOEING SRM 51-10-01.

Part: FLOOR BEAM — CRACKED (BS 1820)

CRACK IN UPPER CHORD AT FLOOR BEAM BS 1820 AT RBL 15. REPAIRED PER BOEING SRM 51-40-04, FIG 1.

Part: ANGLE — CORRODED (BS 2340)

CORROSION IN ANGLE AT LOWER SIDE AREA AT WEB BS 2340 NEAR S48R. CORROSION REMOVED PER BOEING SRM 51-10-01.

Part: CHORD — DAMAGED (BS 1820)

EXISTING REPAIR UNACCEPTABLE, UPPER CHORD BS 1820 ABOVE S42L. REPLACED REPAIR WITH REPAIR PER BOEING SRM 53-40-03, FIG. 3.

Part: FLANGE — CORRODED (BS 2260)

CORROSION ON LOWER FLANGE BS 2260 AT CONNECTION TO SKIN BETWEEN S50L AND S51L. CORROSION REMOVED PER BOEING SRM 51-10-01.

Part: FITTING — CRACKED (BS 1840-1860)

CRACK AND CORROSION IN FLOOR FITTING AT FLOOR COVER BETWEEN BS 1840 AND BS 1860. REPLACED FITTING PER BOEING SRM 51-30-02.

Part: FLANGE — CORRODED (BS 2200)

CORROSION IN LOWER FLANGE AT BS 2200 AT CONNECTION SKIN AT S44L TO S48L. REMOVED CORROSION PER BOEING SRM 51-10-01.

Part: SKIN — CORRODED (BS 1860-1920)

CORROSION IN CENTER COVER SHEET METAL BETWEEN BS 1860 TO BS 1920. REPLACED COVER PER BOEING SRM 51-10-23 AND SRM 51-30-02.

Part: TE SKIN — DAMAGED (NR 2 FORE FLAP)

LEFT WING INBOARD FORE FLAP AT UPPER SURFACE OF TRAILING EDGE PATCHES REQUIRE UPGRADE. REPAIRED PER BOEING SRM 51-40-09.

Part: LE SKIN — DAMAGED (NR 1 FORE FLAP)

LEFT OUTBOARD FORE FLAP DAMAGE TO LEADING EDGE SKIN NEXT TO INBOARD FITTING. REPAIRED PER BOEING SRM 51-40-09.

Part: TENSION TIE — CRACKED (BS 780)

CRACK IN TENSION TIE AT BS 780 LBL 85. CRACK AROUND 1 HOLE ONLY. REPAIRED PER BOEING SRM 51-40-03 AND SRM 51-30-02.

Part: RIB — CRACKED (FSS 1385)

RIGHT WING LEADING EDGE CAVITY FSS 1385 FORGED RIB RIGHT AND LEFT SIDES OF UPPER CHORD CRACKED. REPLACED RIB INSTALLED PER BOEING SRM 51-30-02.

Part: HINGE — BROKEN (NR 3 PYLON)

BROKEN HINGE AND LOOSE RIVETS ON BLOW OUT PANEL AT NR 3 RIGHT PYLON FAIRING DOOR. REPAIRED PER BOEING SRM 51-30-02.

Part: SKIN — CORRODED (WING CENTER SEC)

CORROSION IN THE UPPER SKIN (CEILING) AND STRINGERS AND ANGLE BETWEEN FRONT SPAR TO STR 28C IN DRY BAY (INTERNAL) CENTER-SECTION. REMOVED CORROSION FROM UPPER SKIN PER BOEING SRM 51-10-01 WITHIN LIMITS PER SRM 53-10-01. TREATED PER 51-10-02.

Part: ANGLE — CRACKED (BS 2020)

CRACK IN EXISTING REPAIR ON SUPPORT ANGLE FOR FLOOR PANEL BS 2020 RBL 10 TO RBL 7.5. MANUFACTURED NEW SUPPORT PER BOEING SRM 53-10-23 AND SRM 53-10-01.

Part: ANGLE — BROKEN (BS 1970)

BROKEN EXISTING REPAIR SUPPORT ANGLE FOR FLOOR PANEL BS 1970 RBL 22. REPAIRED PER BOEING SRM 51-40-03.

Part: ANGLE — CRACKED (BS 2000)

CRACK IN SUPPORT ANGLE FOR FLOOR PANEL BS 2000 RBL 45. REPAIRED PER BOEING SRM 51-40-03.

Part: SKIN — DENTED (NR 2 MID FLAP)

THREE LARGE DENTS LEFT INBOARD MID-FLAP INBOARD OF INBOARD CARRIAGE LOWER SURFACE. REPAIRED PER BOEING SRM 51-40-06.

Part: PROFILE FIBER — MISSING (NR 3 TE FLAP)

RIGHT WING INBOARD FLAP INBOARD PROFILE FIBER IS MISSING. REPAIRED PER BOEING SRM 51-40-09.

Part: FLOOR BEAM — BENT (BS 1760)

BEND IN UPPER CHORD AT FLOOR BEAM AT BS 1760 AT LBL 30. REPAIRED PER BOEING SRM 51-40-01 AND SRM 51-10-01.

Part: ROLLER TRAY — CORRODED (BS 1780-1820)

CORROSION IN ROLLER TRAY LBL 35 BETWEEN BS 1780 AND BS 1820. REPAIRED PER BOEING SRM 53-10-06.

Part: ANGLE — CORRODED (BS 1920-1960)

CORROSION IN SUPPORT ANGLE FOR FLOOR PANEL BETWEEN BS 1920 AND BS 1960, RBL 7.5 AND RBL 15. REPAIRED PER BOEING SRM 53-10-23 AND SRM 51-30-02.

Part: FAIRING DOOR — CORRODED (NR 2 PYLON)

CORROSION AND SMALL CRACK ON LOWER EDGE NR 2 PYLON FAIRING EXTERIOR SURFACE SKIN. REMOVED CORROSION AND CRACK PER BOEING SRM 51-10-01.

Part: FLOOR — CORRODED (BS 1660-1760)

CORROSION IN FLOOR COVER SHEET METAL BETWEEN BS 1660 AND 1760 AT RBL 40. REPLACED SKIN PANEL PER BOEING SRM 53-10-23.

Part: STRINGER — CORRODED (BS 680-700)

CORROSION AND DENTS ON S47L AND S47R BETWEEN BS 680 AND 700. CORROSION REMOVED AND DENTS STRAIGHTENED PER BOEING SRM 51-10-01.

Part: ANGLE — CORRODED (NR 4L DOOR)

CORROSION ON ANGLE AND BROKEN ANCHOR NUT DOOR NR 4L LOWER SCRUFF. REPLACED ANGLE PER BOEING SRM 51-40-03.

Part: FLOORBEAM — BENT (BS 1520)

BEND IN UPPER CHORD AT FLOORBEAM BS 1520 AT LBL 25. STRAIGHTENED PER BOEING SRM 51-40-01 AND 51-10-01.

Part: RIB — BROKEN (FWD CARGO)

BROKEN RIB BETWEEN BS 960 AND 980 BETWEEN RBL 24.75 AND RBL 45.5. REPAIRED PER BOEING SRM 53-10-21.

Part: STRINGER — CRACKED (BS 680-700)

CRACK ON S46L BETWEEN BS 680 AND 700. CRACK REPAIRED PER BOEING SRM 53-10-03 FIG 1.

Part: RIB — TORN (BS 700)

TEAR ON BS 700 RBL 8. REPAIRED PER BOEING SRM 51-40-02.

Part: INTERCOSTAL — BENT (BS 765)

BEND ON INTERCOSTAL AT BS 765, BETWEEN LBL 22.75 AND LBL 45.5. REPAIRED PER BOEING SRM 51-40-03.

Part: STRINGER — CORRODED (BS 1000)

CORROSION ON S37L BS 1000. REPAIRED PER BOEING SRM 53-10-03 AND 51-30-02.

Part: STOP — CORRODED (3L DOOR)

CORROSION 3L DOOR STOP 5. REMOVED CORROSION PER BOEING SRM 51-10-01.

Part: INTERCOSTAL — CORRODED (BS 420)

CORROSION ON INTERCOSTAL BS 420 S30R. REMOVED CORROSION PER BOEING SRM 51-10-01.

Part: SEAT TRACK — CORRODED (BS 2240)

CORROSION IN SEAT TRACK AT BS 2240 LBL 33. REMOVED THE CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS SRM 53-10-01.

Part: INTERCOSTAL — DENTED (BS 570)

DENT ON INTERCOSTAL BS 570 BETWEEN LBL 45 AND RBL 45. REPAIRED PER BOEING SRM 51-40-03 FIG 1.

Part: STRAP — MISINSTALLED (BS 840)

REPAIR NOT PER CURRENT SRM ON STRAP AT BS 840 LT. REPLACED PER BOEING SRM 53-10-21.

Part: FITTING — CORRODED (BS 660)

CORROSION ON FITTING BS 660 AT RBL 30. CORROSION REMOVED PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01.

Part: STRINGER — CORRODED (BS 940/960)

CORROSION IN S36R BETWEEN BS 940 AND 960. CORROSION REMOVED PER BOEING SRM 51-10-01.

Part: STRINGER — CORRODED (BS 820/840)

CORROSION IN S44L BETWEEN BS 820 AND 840. CORROSION REMOVED PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01.

Part: ANGLE — CRACKED (CARGO DOOR)

CRACKED ANGLE BULK CARGO DOOR INTERNAL AT AFT LOWER CORNER. REPAIRED PER BOEING SRM 51-40-03.

Part: LAP SPLICE — CORRODED (AFT PRESS BLKHD)

TWO INDICATIONS (LFEC) OF CRACKS OR CORROSION ON AFT PRESSURE BULKHEAD LAP SPLICE. REMOVED CORROSION BETWEEN LAP PER BOEING SRM 51-10-01.

Part: BRACKET — CORRODED (BS 1285)

CORROSION ON BRACKET CONNECTING INTERCOSTAL TO FRAME BS 1285 S26L WL 198. REPAIRED PER BOEING SRM 51-10-01.

Part: DOOR — CRACKED (NLG)

CRACKS AND DENTS ON LEFT NOSE GEAR STRUT DOOR. REPAIRED PER BOEING SRM 51-30-02.

Part: ANGLE — CORRODED (BS 2200-2220)

CORROSION IN ANGLE AT BS 2220 TO 2200 S26L WL 198. REMOVED THE CORROSION PER BOEING SRM 51-10-01.

Part: PANEL — SEPARATION (NR 1 TE MIDFLAP)

NR 1 MIDFLAP LEADING EDGE PANEL HAS SEPARATION. REPAIRED PER BOEING SRM 51-40-06.

Part: MOUNT BRACKET — BROKEN (NR 2 SKIRT)

NR 2 SKIRT FORWARD MOUNTING BRACKET IS BROKEN. INSTALLED NEW FITTING PER BOEING SRM 51-30-02.

Part: SKIN — BENT (CREW SERV DOOR)

CREW SERVICE DOOR AFT LOWER CORNER OUTER SKIN BENT. REPAIRED PER BOEING SRM 51-40-01.

Part: DOOR — DENTED (NLG)

TWO DENTS IN THE RIGHT NOSE GEAR DOOR. REPAIRED PER BOEING SRM 52-80-02.

Part: BRACKET — BROKEN (CREW SERV DOOR)

CREW SERVICE DOOR FORWARD BOTTOM SIDE SUPPORT STOP BRACKET BROKEN. REPLACED BRACKET PER BOEING OVERHAUL MANUAL 52-13-11.

Part: SUPPORT — CRACKED (BS 1394)

CRACK IN FAIRING SUPPORT AT FUSELAGE RIGHT SIDE AT BS 1394 AREA ABOVE WING. REPLACED SUPPORT PER BOEING SRM 51-40-03.

Part: FITTING — CORRODED (FS 1394)

CRACK AND CORROSION IN LONGERON FITTING AT BS 1394, BEFORE WING SLIDE COMPARTMENT ABOVE WING. REMOVED CRACK AND CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01.

Part: BLKHD FITTING — CORRODED (BS 2340-2360)

CORROSION IN FITTING BETWEEN BS 2340 AND 2360 S24L AT ATTACH PRESSURE BULKHEAD. CORROSION REMOVED AND TREATED PER BOEING SRM 51-10-01.

Part: SKIN — CRACKED (NR 1 PYLON)

CRACK ON NR 1 PYLON SKIRT NEAR TO RIGHT AFT HYDRAULIC RESERVOIR MOUNTING BOLT. REPAIRED PER BOEING SRM 54-12-02 AND 51-30-02.

Part: PANEL — DELAMINATED (LT WING)

WING PANEL HAS DELAMINATIONS DENTS AND MISSING EDGE. REPAIRED PER BOEING SRM 51-40-06 AND 51-40-09.

Part: SEAT TRACK — CORRODED (BS 1320)

SURFACE CORROSION ON SEAT TRACK RBL 33 BETWEEN BS 1320 AND 1480. CORROSION REMOVED PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02.

Part: HINGE — CRACKED (NR 2 PYLON)

CRACK ON BLOWOUT PANEL HINGE NR PYLON LEFT SIDE. REPLACED HINGE PER BOEING SRM 51-30-02.

Part: SKIN — CRACKED (BS 1680-1720)

CRACK IN THE FUSELAGE SKIN LEFT SIDE BETWEEN BS 1680 AND 1720 AT S40L LAP JOINT. REPAIRED PER BOEING SRM 53-30-03.

Part: FLOOR — CRACKED (BS 765)

CRACK ON FLOOR AND BEND ON INTERCOSTAL AT BS 765 RBL 24.75 AND RBL 45.5. REPAIRED PER BOEING SRM 53-10-21.

Part: FLOOR PANEL — TORN (BS 1660)

TEAR ON FLOOR PANEL BS 1660 TO 1680 ABOVE S40R. REPAIRED PER BOEING SRM 51-40-02.

Part: SUPPORT FTG — CRACKED (WS 669.5)

CRACK IN RIB SUPPORT FITTING UPPER CHORD AND ANGLE UPPER CHORD LEFT WING WS 669.5. REPAIRED PER BOEING SB 57-2273.

Part: FLOOR PANEL — BROKEN (BS 700)

BROKEN FLOOR PANEL BS 700 FORWARD CARGO RIGHT SIDE. MANUFACTURED NEW PART PER BOEING SRM 53-10-21. INSTALLED PER BOEING SRM 51-30-02.

Part: SKIN — CORRODED (BS 1740)

CORROSION IN SKIN PANEL AND STRINGER S41L NEAR BS 1740. REPAIRED PER BOEING SRM 53-10-03 AND 51-10-01, STRINGER REPAIR AND SKIN BLENDED WITHIN LIMITS.

Part: ROLLER TRAY — CORRODED (BS 1740-1760)

CRACK AND CORROSION IN ROLLER TRAY RBL 35 TO 38 AND LBL 5.5 BETWEEN BS 1740 AND 1760. REPAIRED PER BOEING SRM 53-10-06 AND 51-10-01.

Part: CHORD — DENTED (BS 840)

DENTS ON UPPER CHORD BETWEEN RBL 45.5 AND LBL 45.5 BS 840. STRAIGHTENED AND SMOOTHED PER BOEING SRM 53-10-01.

Part: PANEL — DAMAGED (BS 780)

DAMAGE ON PLUG PANEL BS 780 ABOVE S46R. REPLACED PANEL PER SRM 53-10-21 AND 51-30-02.

Part: CHORD — DAMAGED (BS 780)

DAMAGE ON UPPER CHORD AT THE BL0 BS 780. DAMAGE BLENDED OUT PER BOEING SRM 51-10-01 WITHIN LIMITS PER 53-10-01.

Part: BRACKET — CORRODED (BS 800)

CORROSION IN BRACKET BS 800 S47L. CORROSION REMOVED PER BOEING SRM 51-10-01 WITHIN LIMITS PER 53-10-01.

Part: SUPPORTS — CORRODED (BS 540-560)

CORROSION ON 2 SUPPORTS AT BL0 BETWEEN BS 540 AND 560. REPAIRED PER BOEING SRM 51-40-03.

Part: ANGLE — CRACKED (BS 640-660)

CRACK AND CORROSION ON ANGLE BETWEEN BS 640 AND 660, BETWEEN RBL 30 AND RBL 45. REPAIRED PER BOEING SRM 51-40-04.

Part: WEB — DAMAGED (BS 1520)

TEAR IN THE WEB BS 1520 BOTTOM TO UPPER CHORD ABOE S48L AND S49L. REPAIRED PER BOEING SRM 51-40-02.

Part: CLIP — CORRODED (BS 1920)

CORROSION ON CLIP BS 1920 S14R. CORROSION REMOVED PER BOEING SRM 51-10-01.

Part: INTERCOSTAL — CORRODED (BS 480-500)

CORROSION ON INTERCOSTAL BS 480 TO 500 S30R. CORROSION REMOVED PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01.

Part: SEAT TRACK — GOUGED (BS 2140)

GOUGES IN SEAT TRACK BS 2140 RBL 11. REPLACED SEAT TRACK PER IAI EO MF-MAN-B47-53-83975.

Part: ANGLE — BROKEN (BS 540)

BROKEN ANGLE ON BS 540 BETWEEN S39R AND S40R. MANUFACTURED NEW ANGLE PER BOEING SRM 51-10-21 AND 51-30-02.

Part: STRINGER — TORN (BS 760)

TEAR ON S35R BS 760. REPAIRED PER BOEING SRM 53-10-03 FIG 1.

Part: FLOORBEAM — DAMAGED (BS 620-640)

TEAR ON UPPER FLOORBEAM IN CARGO COMPARTMENT BETWEEN BS 620 AND 640 NEAR CENTER. REPAIRED PER BOEING SRM 51-40-02 FIG 1.

Part: SKIN — CRACKED (NR 2 PYLON)

CRACK NR 2 PYLON OUTER SKIN NS 221. REPAIRED PER IAI EO MAN-747-54-83978.

Part: HINGE — CORRODED (R2 DOOR)

CORROSION IN R2 DOOR LOWER HINGE. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01.

Part: FITTING — CORRODED (LT WING)

CORROSION UNDER FITTING AT WBL 584. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 57-10-01.

Part: BRACKET — CORRODED (BS 2230)

CORROSION BS 2230 AT BRACKET FROM FRAME TO INTERCOSTAL S26L WL 198. MANUFACTURED NEW PART PER BOEING SRM 51-40-03.

Part: INTERCOSTAL — DAMAGED (BS 1900-1920)

TEAR AND CORROSION ON INTERCOSTAL BETWEEN FRAME BS 1900 AND 1920, BETWEEN LBL 7.5 AND LBL 375. REPAIRED PER BOEING SRM 51-40-02.

Part: FITTING — CORRODED (RT WING)

CORROSION UNDER FITTINGS AT WBL 584 AND 743 RIGHT WING ON LOWER SURFACE SKIN. CORROSION REMOVED PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01.

Part: BRACKETS — BROKEN (BS 1900-1920)

TWO BROKEN BRACKETS ATTACHED TO INTERCOSTAL BETWEEN FRAME BS 1900 AND 1920 LBL 25. REPLACED PER BOEING SRM 51-10-23 AND 51-30-02.

Part: BRACKET — BROKEN (BS 1900-1920)

BROKEN BRACKET ATTACHING INTERCOSTAL BETWEEN BS 1900 AND 1920 BL 0. REPAIRED PER BOEING 51-40-04.

Part: STRINGER — CORRODED (BS 855-860)

CORROSION S26R BS 855 TO 860. CORROSION REMOVED PER BOEING SRM 51-10-01.

Part: ANGLE — WORN (NR 3 PYLON)

ANGLE WORN AND MISSING FASTENERS IN NR 3 PYLON SKIRT RIGHT FORWARD SIDE. REPAIRED PER BOEING SRM 51-40-01 AND 51-30-02.

Part: LONGERON — CORRODED (OVERWING)

SURFACE CORROSION AT OVERWING LONGERON LEFT AND RIGHT SIDES. CORROSION REMOVED PER BOEING SRM 51-10-01, TREATED PER 51-10-02.

Part: BRACKET — CRACKED (CARGO COMPT)

CRACK IN MAIN CARGO DOOR MANUAL HAND PUMP AFT MOUNTING BRACKET. REPAIRED PER BOEING SRM 51-40-04 AND 51-30-02.

Part: PANELS — DELAMINATED (WINGS)

DELAMINATIONS, DENTS AND EDGE DAMAGE ON WING PANELS 672AB, 672CB, 577ET AND 677FT. REPAIRED PER BOEING SRM 51-40-06 AND 51-40-09.

Part: SKIN — WORN (NR 4 PYLON)

WORN METAL IN RIGHT AFT SIDE NR 4 PYLON SKIRT. REPAIRED PER BOEING SRM 54-10-02 AND 51-30-02.

Part: SKIN — CRACKED (FUSELAGE)

CRACKED SKIN AT NOSE WHEEL WELL DOOR HINGE CUTOUT RIGHT DOOR FWD HINGE. REPAIRED PER BOEING SRM 53-10-20 AND 51-30-02.

Part: ANGLE — CRACKED (BS 1800-1820)

CRACK ON ANGLE BS 1800 TO 1820 RBL 45 AFT CARGO COMPARTMENT. REPAIRED PER BOEING SRM 53-10-23, 51-30-02 AND 53-11-25.

Part: WEB — CORRODED (BS 1300/1310)

CORROSION ON THE WEB BETWEEN BS 1300 AND 1310 LBL 33. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02.

Part: SEAT TRACK — OVAL HOLE (MAIN DECK)

OVAL HOLE AT SEAT TRACK TO WEB ATTACHMENT. REPAIRED PER BOEING SB 53-2224, OVERSIZE FASTENER.

Part: SEAT TRACK — DAMAGED (BS 1910/1890)

DAMAGE ON SEAT TRACK AT RBL 25 BETWEEN BS 1910 AND 1890. REPAIRED PER BOEING SRM 53-10-05.

Part: SKIN — CORRODED (BS 880-900)

CORROSION IN SKIN BETWEEN BS 900 AND 880 S39R. REMOVED PER BOEING SRM 51-10-01.

Part: TEAR STRAP — CORRODED (BS 1160)

CORROSION IN TEAR STRAP BETWEEN S6R AND S7R AT BS 1160. CORROSION REMOVED PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01.

Part: STRINGER — CORRODED (BS 1080)

CORROSION IN S5L AND TEAR STRAP AT BS 1080. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01.

Part: FLOORBEAM — CORRODED (BS 500)

CORROSION AND SHEARED RIVET IN LOWER CABIN FLOORBEAM BS 500 RBL 45. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01.

Part: PANEL — DELAMINATED (LT WING)

TOP OF LEFT WING DELAMINATED PANEL. REPAIRED PER BOEING SRM 51-40-06.

Part: BRACKET — DAMAGED (NR 1 PYLON)

DAMAGE FWD SKIRT MOUTNING BRACKET NR 1 PYLON. INSTALLED NEW FITTING PER 51-30-02.

Part: CLIP — CORRODED (BS 204)

SURFACE CORROSION ON TIE CLIP S4R BS 2040. REMOVED CORROSION PER BOEING SRM 51-10-01.

Part: FITTING — BROKEN (LT WING)

BROKEN MOUNT FITTING ON UPPER RIGHT WING PANEL AT LEFT WING NR 4 TRACK FWD MOUNT. MANUFACTURED NEW PANEL PER BOEING SRM 57-10-02, INSTALLED PER 51-30-02.

Part: CLIP — CORRODED (BS 1620)

CORROSION IN TIE CLIP AT S6L BS 1620. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01.

Part: STRINGER — CORRODED (BS 880-900)

CORROSION IN S38R BS 880 TO 900. REMOVED CORROSION PER BOEING SRM 51-10-01.

Part: SKIN — CORRODED (BS 760-780)

CORROSION IN SKIN BETWEEN BS 760 AND 780 S39L. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01.

Part: STRINGERS — CORRODED (BS 820-840)

CORROSION IN STRINGERS S39L AND S40L BETWEEN BS 820 AND 840. CORROSION REMOVED PER BOEING SRM 51-10-01.

Part: SKIN — CORRODED (BS 840-860)

CORROSION IN SKIN BETWEEN BS 840 AND 860. CORROSION REMOVED PER BOEING SRM 51-10-01.

Part: FAIRING — BROKEN (WS 680)

LOWER FAIRING BROKEN AT WS 680 RIGHT WING REAR SPAR. REPAIRED PER BOEING SRM 51-40-09.

Part: RIB — CRACKED (RT WING)

CRACKS FOUND AT RIGHT WING LEADING EDGE CAVITY FS 800 AND 762 ON RIB UPPER CHORD. REPAIRED PER BOEING SB 57-2116 FIG 6.

Part: STRINGER — CORRODED (BS 1200)

CORROSION IN S4L AT BS 1200 UNDER TIE CLIP. REMOVED THE CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01.

Part: STRINGER — CORRODED (BS 1060)

CORROSION IN S5L BS 1060. CORROSION REMOVED PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01.

Part: HF TUNER BASE — CRACKED (RIGHT WING)

HF TUNER BASE CRACKED RIGHT WING TIP. REPLACED PER BOEING SRM 51-30-02.

Part: FAIRING — HOLE (WS 1240)

HOLE IN FAIRING FIBER GLASS RIGHT WING LOWER SURFACE WS 1240. REPAIRED PER BOEING SRM 51-40-09.

Part: PANEL — DELAMINATED (RT WING)

DELAMINATED WING PANEL RIGHT WING. REPAIRED PER BOEING SRM 51-40-06.

Part: PANEL — DELAMINATED (RT WING)

DELAMINATION AND TRAILING EDGE MISSING ON RIGHT WING.

Part: STRINGER — CORRODED (BS 1560)

CORROSION IN S4R BS 1560. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01.

Part: SKIN — CORRODED (BS 780-800)

CORROSION IN SKIN BETWEEN BS 780 AND 800 AT S39R. CORROSION REMOVED PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01.

Part: STRINGER — CORRODED (BS 840-860)

CORROSION S39R BETWEEN BS 840 AND 860. REMOVED PER BOEING SRM 51-10-01.

Part: BRACKET — ELONGATED HOLE (NR 3 PYLON)

CORROSION ON PNEUMATIC DUCT ATTACH BRACKET ON NR 3 NACELLE FIRE WALL NS 195 LEFT SIDE. ALSO, ELONGATED BOLT HOLE AND BADLY CHAFED. REPAIRED PER BOEING SRM 54-10-02. REPLACED FOR ELONGATED HOLE, NOT A LEVEL 2.

Part: STRINGER — CORRODED (BS 1000)

CORROSION IN S40L BS 1000. REPAIRED STRINGER PER BOEING SRM 53-10-03 AND 51-30-02.

Part: PANEL — DELAMINATED (LT WING)

DELAMINATION ON WING PANEL LEFT WING. REPAIRED PER BOEING SRM 51-40-06.

Part: PANEL — DELAMINATED (LT WING)

DELAMINATION AND TRAILING EDGE MISSING LEFT WING. REPAIRED PER BOEING SRM 51-40-06.

Part: STRINGER — CORRODED (BS 520)

CORROSION IN S40R BS 520. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01.

Part: CLIP — CORRODED (BS 540)

CORROSION IN CLIP S39R BS 540. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01.

Part: SKIN — CORRODED (BS 820-940)

CORROSION IN SKIN BETWEEN BS 820 AND 840 AT S39R. CORROSION REMOVED PER BOEING SRM 51-10-01.

Part: MOUNT BRIDGE — CRACKED (BS 2716.6)

CRACK PAST STOP DRILL JUST AHEAD OF AFT APU MOUNT BRIDGE CONNECTION RIGHT AND LEFT SIDE AT BS 2716.6. REPAIRED PER BOEING SRM 51-20-01 AND 51-30-02.

Part: SKIN — CRACKED (NR 2 PYLON)

CRACK ON LOWER EDGE NR 2 PYLON RIGHT SIDE DOOR FAIRING EXTERIOR SURFACE SKIN. REPAIRED PER BOEING SRM 51-30-02.

Part: SKIN — CORRODED (BS 540-560)

CORROSION IN SKIN BETWEEN BS 540 AND 560 S39L. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 51-10-02.

Part: SKIN — CORRODED (BS 780-800)

CORROSION IN SKIN BETWEEN BS 780 AND 800 S39L. CORROSION REMOVED PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01.

Part: SKIN — CORRODED (BS 500-520)

CORROSION IN SKIN BETWEEN BS 500 AND 520 S39L. CORROSION REMOVED PER BOEING SRM 51-10-01.

Part: SKIN — CORRODED (BS 1500-1580)

CORROSION ON SKIN FROM BS 1500 TO 1580 BETWEEN S18R AND S20R. CORROSION REMOVED PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01.

Part: STRINGER — CORRODED (BS 1000)

CORROSION IN S6L JOINT TO FRAME BS 1000. CORROSION REMOVED PER BOEING SRM 51-10-01, NEW FASTENERS INSTALLED PER 51-30-02.

Part: SKIN — CORRODED (BS 1480-1920)

SURFACE CORROSION ON SKIN BETWEEN BS 1480 AND 1920, S39L AND S39R. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-1.

Part: SKIN — SWELLING (LT WING)

SWELLING OF WING PANEL UPPER WING AT INBOARD HINGE NR 5 SPOILER. REPAIRED PER BOEING SRM 51-40-09.

Part: SKIN — CORRODED (LT WING)

SURFACE CORROSION ON LOWER SKIN AT BOOST PUMP ACCESS, LEFT WING. CORROSION REMOVED PER BOEING SRM 51-10-01, WITHIN LIMITS PER 57-30-01.

Part: FLOORBEAM — CORRODED (BS 500)

CORROSION IN LOWER CAP FLOORBEAM BETWEEN RBL 11 AND LBL 11 BS 500. REPAIRED PER BOEING SRM 51-40-04.

Part: FLOORBEAM — GOUGED (BS 140)

GOUGE ON WEB FLOORBEAM BS 140 RBL 15. REPAIRED PER BOEING SRM 51-40-02.

Part: TE SKIN — DELAMINATED (RT ELEVATOR)

SMALL DELAMINATIONS ON RIGHT INBOARD ELEVATOR AT TRAILING EDGES INBOARD AND OUTBOARD EDGES. REPAIRED PER BOEING SRM 51-40-09.

Part: BRACKET — CRACKED (NR 4 PYLON)

CRACKED FORWARD SKIRT MOUTNING BRACKET NR 4 PYLON. REPLACED FITTING PER BOEING SRM 51-30-02.

Part: BRACKET — CRACKED (WS 1110)

CRACKED RIGHT WING TRAILING EDGE FAIRING ANCHOR NUT BRACKET AT WS 1110. REPAIRED PER BOEING SRM 51-30-02 NEW ANGLES.

Part: BRACKET — CRACKED (BS 1940)

CRACK IN SUPPORT ANGLE FLOOR PANEL LBL 7.5 BETWEEN BS 1940-2060. REPAIRED PER BOEING SRM 51-30-02, SRM 53-10-23.

Part: SUPPORT — CRACKED (BS 560)

CRACK AND CORROSION ON CEILING SUPPORT BS 560 RBL 75-98. MANUFACTURED NEW SUPPORT PER BOEING SRM 53-10-21. INSTALLED PER 51-30-02.

Part: FASTENERS — MISSING (BS 2300)

MAIN DECK BETWEEN S17L AND S18L HAS 5 MISSING FASTENERS ON BS 2300. INSTALLED MISSING FASTENERS PER BOEING SRM 51-30-02.

Part: OMEGA — BROKEN (BS 2000)

BULK CARGO NR 2 OMEGA FOR RIGHT BS 2000 IS BROKEN. PERFORMED REPAIR PER BOEING SRM 51-40-03.

Part: ROLLER TRAYS — BROKEN (AFT CARGO)

AFT CARGO 2 ROLLER TRAYS FROM RIGHT SIDE ARE BROKEN ON AFT POINT. REPAIR PERFORMED PER BOEING SRM 53-10-06, FIG 1.

Part: SUPPORT — CORRODED (BS 1350/1480)

CORROSION ON PANEL SUPPORT BETWEEN BS 1350 AND BS 1480 BETWEEN LBL 16.5 AND RBL 16.5. REMOVED CORROSION PER BOEING SRM 51-10-01 WITHIN LIMITS PER BOEING SRM 53-10-01.

Part: ROLLER TRAY — BROKEN (BS 660)

ROLLER TRAY BROKEN SECOND FROM RIGHT SIDE BS 660 FORWARD CARGO PIT. REPAIRED PER BOEING SRM 53-10-06, FIG. 1.

Part: STIFFENER — BROKEN (NR 3 NOSE COWL)

ENGINE NR 3 FAN NOSE COWL AFT BULKHEAD AT 3 O'CLOCK, FOUND BROKEN PIECE IN STIFFNER. TRIMMED AND TREATED PER SRM 51-10-01. MATERIAL IS WITHIN LIMITS PER BOEING SRM 54-12-01.

Part: CLIP — CRACKED (BS 1780)

CRACKED CLIP MAIN RIGHT SIDE BS 1780 S16R. FABRICATED NEW CLIP PER BOEING SRM 51-30-02.

Part: ATTACH ANGLE — DAMAGED (BS 820-840)

DAMAGE IN MAIN DECK FLOOR ATTACH ANGLE BETWEEN BS 820-840 AT LBL 105. CLEANED AND SMOOTHED DAMAGE PER BOEING SRM 51-10-01.

Part: ANGLE — CORRODED (BS 2160)

CORROSION ON SUPPORT ANGLE FLOOR PANEL BS 2160 BETWEEN RBL 40 AND LBL 53. CORROSION REMOVED PER BOEING SRM 51-10-01 WITHIN THE LIMITS PER 53-10-01.

Part: SKIN — CRACKED (NR 2L DOOR)

NR 2L ENTRY DOOR HAS 2 CRACKS, ONE IN INNER SKIN AND ONE IN OUTER SKIN. CRACKS WERE TRIMMED PER BOEING 51-10-01 WITHIN LIMITS PER 53-10-01.

Part: FLANGE — CORRODED (BS 2180)

CORROSION ON LOWER FLANGE OF BS 2180 ON UPPER SURFACE BETWEEN S44L AND S48L. REMOVED CORROSION PER BOEING SRM 51-10-01.

Part: ANGLE — CRACKED (BS 1940-2040)

CRACK IN FLOOR SUPPORT ANGLE RBL 37.5 BS 1940-2040. REPAIRED AS PER BOEING SRM 51-40-03.

Part: SPAR — CORROSION (BS 1000)

CORROSION IN THE UPPER SPAR AT BS 1000 BETWEEN LBL 30 TO RBL 120 IN DRY-BAY (INTERNAL) CENTER SECTION RIGHT. REMOVED CORROSION PER BOEING SRM 51-10-01. TREATED PER 51-10-02 WITHIN LIMITS PER 53-10-01.

Part: ANGLE — CRACKED (BS 2080-2100)

CRACK IN SUPPORT ANGLE FLOOR PANEL RBL 30 BETWEEN BS 2080-2100. REPAIRED PER BOEING SRM 51-40-03.

Part: FRAME — CRACKED (BS 640)

CRACK IN STA 640 LEFT SIDE BETWEEN S17L AND S18L. REPAIRED PER IAI MF-MAN-B47-53-83987.

Part: INTERCOSTAL — DENTED (BS 2140-2160)

DENT IN INTERCOSTAL AT S31R BETWEEN BS 2140-2160. REPAIRED PER BOEING SRM 51-40-01.

Part: ANGLE — CRACKED (BS 2000)

CRACK IN SUPPORT ANGLE FOR FLOOR PANEL AT BS 2000 LBL 22. REPAIRED PER BOEING SRM 53-10-03 AND SRM 5130-02.

Part: ANGLE — CORRODED (BS 2280-2360)

CORROSION IN FLOOR OMEGAS AND ANGLE BRACKET BETWEEN BS 2280-2360 LBL 0 TO RBL 70. REMOVED CORROSION PER BOEING SRM 51-10-01 WITHIN LIMITS PER 53-10-01.

Part: ANGLE — CRACKED (AFT CARGO)

CRACK IN SUPPORT ANGLE FOR FLOOR PANEL BETWEEN BS 1920 AND BS 2080 LBL 37. REPAIRED PER SRM 51-40-03.

Part: ANGLE — CORRODED (BS 2280-2360)

CORROSION IN CONNECTION FLOOR ANGLE BETWEEN BS 2280-2360 AT S26L. REMOVED THE CORROSION PER BOEING SRM 51-10-01.

Part: SPLICE — CORRODED (BS 1960)

CORROSION IN S47R SPLICE AT BS 1960. REPLACED SPLICE FITTING PER BOEING SRM 53-10-03.

Part: STRINGER — CORRODED (BS 2000)

CORROSION IN BS 2000 AT S33L. REMOVED CORROSION PER BOEING SRM 51-10-01.

Part: STRINGER — CORRODED (BS 1960)

CORROSION IN S44R BS 1960. CORROSION REMOVED PER BOEING SRM 51-10-01 WITHIN LIMITS PER 53-10-01.

Part: STRINGER — CORRODED (BS 2300)

CORROSION IN S49L NEAR BS 2300. CORROSION REMOVED PER BOEING SRM 51-10-01.

Part: ANGLE — CORRODED (BS 1920-1940)

CORROSION AND DENT IN SUPPORT ANGLE FOR FLOOR PANEL BETWEEN BS 1920 AND BS 1940 BL 0. CORROSION REMOVED AND DENT SMOOTHED PER BOEING SRM 51-10-01 WITHIN LIMITS PER 53-10-01.

Part: WEB — CORRODED (BS 2300)

CORROSION IN WEB AT BS 2300 ABOVE S45L TO S46L. CORROSION REMOVED PER BOEING SRM 51-10-01.

Part: ANGLE — DENTED (BS 1320)

DENT ON SUPPORT ANGLE FOR FLOOR PANEL BS 1320 RBL 5. STRAIGHTENED AND SMOOTHED PER BOEING SRM 51-10-01 WITHIN LIMITS PER 53-10-01.

Part: ANGLES — CORRODED (BS 2320/2340)

CORROSION IN ANGLES AT WEB BS 2320 AND BS 2340 ABOVE S45L AND S46L. INSTALLED NEW ANGLES PER BOEING SRM 53-10-23.

Part: ANGLE — CORRODED (BS 1960)

CRACK IN SUPPORT ANGLE FOR FLOOR PANEL AT BS 1960 RBL 15. REPAIRED PER BOEING SRM 51-40-03.

Part: BULKHEAD — CORRODED (BS 2360)

CORROSION IN BS 2360 BETWEEN S50R TO S50L. CORROSION REMOVED PER BOEING SRM 51-50-01.

Part: BEAM — CORRODED (BS 2040)

CORROSION IN UPPER CHORD BEAM BS 2040 BETWEEN RBL 7 AND RBL 15. CORROSION REMOVED PER BOEING SRM 51-10-01 WITHIN LIMITS PER 53-10-01.

Part: SKIN — CORRODED (BS 1000)

CORROSION IN THE WALL AT BS 1000 AT RBL 9, RBL 10 AREA IN DRY-BAY (INTERNAL) CENTER SECTION RIGHT. REMOVED CORROSION PER BOEING SRM 51-10-01. TREATED AND PAINTED PER 51-10-02 WITHIN LIMITS PER 53-10-01.

Part: WEAR STRIP — MISSING (NR 2 FORE FLAP)

LEFT WING INBOARD FORE FLAP INBOARD SIDE MOVABLE SURFACE WEAR STRIP MISSING. REPAIRED PER BOEING SRM 51-40-09.

Part: DOOR — DAMAGED (RT MLG)

RIGHT WING LANDING GEAR WHEELWELL INBOARD DOOR FORWARD LOWER CORNER IS DAMAGED. REPAIRED PER SRM 51-40-03, FIG. 1.

Part: SKIN — CORRODED (BS 1900-1920)

CORROSION IN SKIN BETWEEN BS 1900 AND BS 1920 NEAR S45R. REMOVED CORROSION PER BOEING SRM 51-10-01 WITHIN LIMITS PER 53-10-01.

Part: WEB — CORRODED (BS 1960-1980)

CORROSION IN WEB BETWEEN BS 1960 AND BS 1980 UNDER SUPPORT ANGLE FOR FLOOR PANEL RBL 45. REPAIRED PER BOEING SRM 53-10-23 AND SRM 51-30-02.

Part: ANGLE — CRACKED (BS 2000-2020)

CRACK IN SUPPORT ANGLE FOR FLOOR PANEL BETWEEN BS 2000 AND BS 2020 RBL 5 AND RBL 53. REPAIRED PER BOEING SRM 51-40-03.

Part: FAIRING DOOR — CHAFED (NR 4 PYLON)

NR 4 STRUT LEFT FAIRING DOOR INTERNAL LOWER CHORD SKIN IS GOUGED AND CHAFED BADLY. REPAIRED PER BOEING SRM 51-10-01, 53-50-00, AND 51-10-02.

Part: ANGLE — CRACKED (BS 2040)

CRACK IN SUPPORT ANGLE FOR FLOOR PANEL BS 2040 BL 0. REPAIRED PER BOEING SRM 51-40-03.

Part: WEAR STRIP — BROKEN (NR 2 FORE FLAP)

LEFT WING INBOARD FORE FLAP INBOARD FIBERGLASS STRIP BROKEN. MANUFACTURED NEW STRIP PER BOEING SRM 57-10-02 AND SRM 51-30-02.

Part: DOUBLER — GOUGED (NR 1 PYLON)

DEEP SKIN GOUGE LEFT SIDE NS 240 NR 1 PYLON. REPLACED DOUBLER PER BOEING SRM 51-30-02.

Part: ANGLES — CRACKED (NR 3L DOOR)

CRACKED AND BROKEN STRAP ANGLES THAT ATTACH TRIM PANELS NR 3 LEFT ENTRY DOOR. REPLACED ANGLES PER BOEING SRM 52-10-02.

Part: INTERCOSTAL — CORRODED (BS 1430-1480)

CORROSION ON SKIN FITTINGS AND INTERCOSTAL BETWEEN BS 1430 AND BS 1480 BETWEEN LBL 16 AND RBL 16. MANUFACTURED AND INSTALLED REINFORCING BRACKET PER BOEING SRM 53-10-22.

Part: STRUCTURE — DAMAGED (DOOR CUT OUT)

DAMAGE ON CUT-OUT INTERNAL STRUCTURE ABOVE NR 3L ENTRY DOOR. DAMAGE SMOOTHED AND TREATED ACCORDING TO BOEING SRM 51-10-01.

Part: BRACKET — DAMAGED (BS 1242)

DAMAGE ON BRACKET AT BS 1242, LBL 50. REPAIRED PER BOEING SRM 51-40-02.

Part: ANGLES — CORRODED (BS 1300-1350)

CORROSION ON LOWER SKIN ANGLES ON INTERCOSTAL BETWEEN BS 1300 AND BS 1350 BETWEEN LBL 16 AND RBL 16 (LEVEL 2). MANUAFACTURED AND INSTALLED REINFORCEMENT ANGLES PER BOEING SRM 53-10-22.

Part: KEEL BEAM — CORRODED (RIGHT)

SURFACE CORROSION ON UPPER SIDE OF KEEL BEAM BOX, RIGHT BODY GEAR WHEEL WELL, LEVEL 1. REMOVED CORROSION PER BOEING SRM 51-10-01.

Part: ANGLE — CORRODED (BS 1240)

CORROSION ON ANGLE AT THE BULKHEAD BS 1240, LBL 50. CORROSION REMOVED PER BOEING SRM 51-10-01 WITHIN LIMITS PER SRM 53-10-01 (LEVEL 1).

Part: BULKHEAD — BENT (NR 1 PYLON)

NR 1 PYLON BULKHEAD LOWER SIDE BADLY BENT NS 180. REPAIRED PER BOEING SRM 51-10-02 AND 51-30-02.

Part: FAIRING — DAMAGED (NR 1 PYLON)

HOLE ON UNDER WING AT TRAILING EDGE FAIRING RIGHT SIDE NR 1 PYLON. REPAIRED PER 51-40-02.

Part: TE FIBER — DETERIORATED (NR 25 LE FLAP)

RIGHT WING NR 25 LEADING EDGE FLAP VARIABLE CAMBER TRAILING EDGE FIBER IS DETERIORATED. REPAIRED PER BOEING SRM 51-40-09.

Part: SKIN — DENTED (BS 1700-1720)

DENT WITH SCRATCH IN FUSELAGE SKIN LEFT SIDE BETWEEN BS 1700 AND 1720, BETWEEN S37L AND S38L. STRAIGHTENED DENT AND BLENDED PER BOEING SRM 51-10-01.

Part: RIB — DAMAGED (RT INBD AILERON)

TEAR IN LIGHTENING HOLE RIGHT INBOARD AILERON NEAR INBOARD HINGE. REPAIRED PER BOEING SRM 57-20-01.

Part: FAIRING — DAMAGED (RT WING)

RIGHT WING LEADING EDGE FAIRING WS 630 EDGE IS DAMAGED AND FIBERGLASS AROUND FASTENER HEADS ARE PEELING. REPAIRED PER BOEING SRM 51-40-09.

Part: SUPPORT — CORRODED (FS 1000-1240)

CORROSION ON FAIRING SUPPORT AND AROUND ACCESS FOR AIR CONDITIONING BETWEEN BS 1000 AND 1240, BETWEEN LBL 16 AND LBL 90, LEVEL 1. CORROSION REMOVED PER BOEING SRM 51-10-01.

Part: SUPPORT — CORRODED (BS 1050)

CORROSION ON SUPPORT BRACKET BS 1050 RIGHT SIDE, LEVEL 1. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER BOEING SRM 53-10-01.

Part: SKIN — TEAR (BS 1470)

TEAR ON SHEET METAL AT BS 1470 LBL 15. REPAIRED PER BOEING SRM 52-10-02.

Part: FAIRING — DELAMINATED (FUSELAGE)

DELAMINATION ON FAIRING PANEL NR 192E. REPAIRED PER BOEING SRM 51-40-09.

Part: FITTING — CORRODED (BS 1350)

CORROSION BS 1350 RT UPPER CORNER FITTING RIGHT BODY GEAR WHEEL WELL. CORROSION REMOVED PER BOEING SRM 51-10-01.

Part: SKIN — BULGED (FS 1720-1740)

BULGE IN FUSELAGE SKIN LEFT SIDE BETWEEN BS 1720 AND 1740 AT S32L. REMOVED THE RIVET AND CLEANED PER BOEING SRM 51-10-01. INSTALLED NEW RIVET PER BOEING SRM 51-30-02.

Part: SKIN — DENTED (FS 2240)

DENT AND SCRATCHES IN FUSELAGE SKIN RIGHT SIDE AT BS 2240 UNDER NR 5R DOOR. BLENDED OUT SCRATCHES PER BOEING SRM 51-10-01, DENT WITHIN LIMITS PER BOEING SRM 53-10-1.

Part: SKIN — CORROSION (FS 1800-1820)

SURFACE CORROSION IN THE FUSELAGE SKIN BETWEEN BS 1800 TO BS 1820 AND BETWEEN S46R AND S46R. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER BOEING SRM 53-10-01.

Part: SKIN — DENTED (FS 720-740)

DENT IN FUSELAGE SKIN LEFT SIDE BETWEEN BS 720 AND 740, BETWEEN S27L AND S28L. SMOOTHED DENT PER BOEING SRM 51-40-01, WITHIN LIMITS PER 53-10-01.

Part: BEARING — MIRGATED (NR 7 FLAP TRACK)

BEARING HAS ROTATION AND MIGRATED RIGHT WING, NR 7 FLAP TRACK UNDER WING FORWARD LUG MOUNT. REPAIRED ACCORDING TO BOEING SERVICE BULLETIN 747-57-2262.

Part: ANGLE — CRACKED (WS 600)

TWO ANGLE BRACKETS ARE CRACKED RIGHT WING TRAILING EDGE WS 600, UNDER NR 7 SPOILER PCU. MANUFACTURED NEW ANGLES PER BOEING SRM 57-20-02, INSTALLED PER BOEING SRM 51-30-02.

Part: SUPPORT — CRACKED (BS 1030)

CRACK ON FAIRING SUPPORT AT BS 1030 RBL 120. REPAIRED PER BOEING SRM 51-40-03.

Part: SUPPORT — CORRODED (BS 1240)

CORROSION ON FAIRING SUPPORT AT BS 1240 LEFT SIDE. CORROSION REMOVED PER BOEING SRM 51-10-01.

Part: SKIN — CRACKED (NR 1 PYLON)

A .25 INCH CRACK AT NS 222 AND .5 INCH CRACK AT NS 236. DISCOVERED AFTER REMOVAL OF DOUBLER NR 1 PYLON. REPAIRED PER BOEING SRM 54-30-03 PAGE 113.

Part: FAIRING — DELAMINATED (FUSELAGE)

DENTS AND DELAMINATION ON FAIRING PANELS NR 292C, 294A, 291D, 5L AND 6L. REPAIRED PER BOEING SRM 51-40-09.

Part: TRACK FITTING — MIGRATED (NR 3 TE FLAP)

MIGRATION ON NR 3 FLAP TRACK UNDER WING FITTING. REPAIRED PER BOEING SERVICE BULLETIN 57-2262.

Part: FAIRING — DENTED (NR 192C)

NR 192C FAIRING PANEL DENTED ON INNER AND OUTER PANELS. REPAIRED PER BOEING SRM 51-40-09.

Part: PANEL — DELAMINATED (NR 192A)

PANEL NR 192A DELAMINATED. REPAIRED PER BOEING 51-40-09.

Part: FAIRING — DENTED (NR 2 RT)

NR 2 RIGHT FORWARD FAIRING PANEL DENTED. REPAIRED PER SRM 51-40-09.

Part: FAIRING — DELAMINATED (NR 1 LT)

NR 1 LEFT LOWER FAIRING PANEL DENTS AND DAMAGED. REPAIRED PER SRM 51-40-09.

Part: TRACK FITTING — MIGRATED (NR 1 TE FLAP)

MIGRATION ON NR 1 TRAILING EDGE FLAP TRACK UNDER WING FITTING. REPAIRED ACCORDING TO BOEING SB 57-2262.

Part: FAIRING — DENTED (NR 6 RT)

NR 6 RIGHT UPPER FAIRING PANEL DELAMINATED AND DENTED. REPAIRED PER BOEING SRM 51-40-09.

Part: FAIRING — DENTED (NR 3 LT)

NR 3 LEFT FAIRING PANEL DELAMINATIONS AND DENTS. REPAIRED PER BOEING SRM 51-40-09.

Part: FAIRING — DELAMINATED (NR 3 RT)

NR 3 RIGHT FAIRING PANEL HAS HOLES AND DELAMINATIONS. REPAIRED PER BOEING SRM 51-40-09.

Part: SKIN — CORRODED (FS 1580-1740)

CORROSION IN FUSELAGE SKIN LEFT SIDE BETWEEN BS 1580 AND 1740 AT S12L, LEVEL 1. CORROSION REMOVED PER BOEING SRM 51-10-01, FOUND WITHIN LIMITS PER BOEING SRM 53-10-01.

Part: SKIN — CORRODED (FS 820-860)

CORROSION ON FUSELAGE SKIN BETWEEN BS 820 TO 860 BETWEEN S45L AND S45R, LEVEL 1. CORROSION REMOVED AS PER BOEING SRM 51-10-01.

Part: SUPPORTS — CORRODED (FS 920-960)

CORROSION ON FAIRING SUPPORTS BS 920 TO 960 AND 100 S40R TO S47R, LEVEL 1. CORROSION REMOVED PER BOEING SRM 51-10-01.

Part: BEARING — MIGRATED (NR 8 FLAP TRACK)

RIGHT WING FLAP TRACK NR 8 FORWARD MOUNT LUG BEARING HAS MIGRATED. REPAIRED PER BOEING SB 747-57-2262, FITTING INSTALLED PER BOEING SB 747-57-2238.

Part: FAIRING — CRACKED (RT WING)

CRACK RIGHT REAR SPAR LOWER TRAILING EDGE FAIRING AT WS 740. REPAIRED PER BOEING SRM 51-40-09.

Part: FAIRINGS — DENTED (TE FLAPS)

DELAMINATIONS AND DENTS ON FLAP FIXED FAIRINGS AT TRACKS NR 2, 3, 7, 8. REPAIRED PER BOEING SRM 51-40-09.

Part: FAIRING — DAMAGED (FUSELAGE)

HOLES IN INNER SIDE OF FAIRING PANEL NR 191C. REPAIRED PER BOEING SRM 51-40-09.

Part: FAIRING — CRACKED (FUSELAGE)

DENTS AND CRACKS ON FAIRING PANEL 191P. REPAIRED PER BOEING SRM 51-40-09.

Part: RIB — CRACKED (NR 3 PYLON)

CRACK WITH STOP HOLE ON INNER RIB SIDE AT NS 222 NR 3 PYLON. REPAIRED PER BOEING SRM 54-10-03.

Part: SKIN — CORRODED (FS 1265-1280)

SURFACE CORROSION IN FUSELAGE SKIN LEFT SIDE BETWEEN BS 1265 AND 1280 UNDER DOOR NR 3L S26L, LEVEL 1. CORROSION REMOVED PER BOEING SRM 51-10-01.

Part: SKIN — CORRODED (BS 2360)

CORROSION IN THE FUSELAGE SKIN AT BS 2360, LEFT SIDE BETWEEN S4L AND S9L, LEVEL 1. CORROSION REMOVED AND TREATED PER BOEING SRM 53-10-01.

Part: DOOR PANEL — DELAMINATED (FUSELAGE)

NR 2 HEAT EXCHANGER EXIT DOOR PANEL (AFT OF LOWER) HAS DELAMINATION. REPAIRED PER BOEING SRM 51-40-09.

Part: SUPPORT — CORRODED (FS 820-860)

CORROSION ON FAIRING SUPPORT BETWEEN S43R AND S47R STA 820 AND 860, LEVEL 1. REMOVED CORROSION PER SRM 51-10-01.

Part: SUPPORT — CORRODED (FUSELAGE)

CORROSION ON RIGHT FAIRING SUPPORT FROM STA 800 TO 840 AND 880 TO 920, LEVEL 1. REMOVED CORROSION PER BOEING SRM 51-10-01.

Part: PANEL — DAMAGED (LT WING)

FIBERGLASS DAMAGED AROUND THE EDGES OF DOOR HINGE PANEL 573CB. REPAIRED PER BOEING SRM 51-40-09.

Part: ANGLE — CORRODED (FS 800-880)

CORROSION ON ANGLE ABOVE AIR CONDITIONING CHANNEL BETWEEN STA 800 AND 880 RIGHT. CORROSION REMOVED PER BOEING SRM 51-10-01.

Part: HINGE — CORRODED (CARGO DOOR)

CORROSION IN FWD AND AFT CARGO DOOR HINGES, LEVEL 1. REMOVED CORROSION PER BOEING SRM 51-10-01 AND TREATED PER 51-10-02.

Part: FAIRING — DAMAGED (NR 1 RT)

NR 1 RIGHT LOWER FAIRING PANEL HOLES ON INNER AND OUTER SIDES. REPAIRED PER BOEING SRM 51-40-09.

Part: SKIN — CRACKED (BS 1000)

CRACK FUSELAGE SKIN BS 1000 S43L. REPAIRED AS PER BOEING SRM 53-30-03 FIG 11.

Part: PANEL — SEPARATED (RT WING)

RIGHT WING TRAILING EDGE UPPER SURFACE NEAR OUTBOARD AILERON INBOARD SIDE HAS FIBERGLASS SEPARATION. REPAIRED ACCORDING TO BOEING SRM 51-40-09.

Part: WALL — DAMAGED (BS 1100)

TEAR IN WALL AT BS 1100 RBL 98. REPAIRED PER BOEING SRM 53-40-02.

Part: RIVETS — LOOSE (BS 1480)

LOOSE RIVETS AT STA 1480 LBL 75. RIVETS CHANGED PER BOEING SRM 51-30-02, 52-10-02.

Part: SUPPORT — CRACKED (BS 1240)

CRACK ON FAIRING SUPPORT BS 1240 LBL 125. REPAIRED PER BOEING SRM 51-40-03.

Part: DOOR — CORRODED (BS 1050)

CORROSION ON DOOR AT BS 1050 NEAR HINGE RIGHT SIDE, LEVEL 1. CORROSION REMOVED PER BOEING SRM 51-10-01.

Part: RAIN CHANNEL — SHEARED (BS 1265)

SHEARED RIVET AND 1 BLIND FASTENER IN RAIN CHANNEL BS 1265 AT S15R. INSTALLED NEW RIVETS PER BOEING SRM 51-30-02.

Part: FAIRING — DELAMINATED (FUSELAGE)

DELAMINATIONS ON NR 9 LEFT FAIRING PANEL. REPAIRED PER BOEING SRM 51-40-09.

Part: ANGLE — BROKEN (BS 1287)

BROKEN ANGLE SUPPORT FOR HYD TUBE AT STA 1287 IN THE RIGHT WING GEAR WHEEL WELL. MANUFACTURED NEW ANGLE PER BOEING SRM 57-10-02.

Part: FAIRING — DENTED (LOWER FUSELAGE)

DELAMINATION AND DENTS, FAIRING PANELS NR 191H, 191E, AND 191F. REPAIRED PER BOEING SRM 51-40-09.

Part: FAIRINGS — DENTED (LOWER FUSELAGE)

FAIRING PANELS NR 1 RT AND 292C DENTED. REPAIRED PER BOEING SRM 51-40-09.

Part: SKIN — LOOSE RIVETS (WS 630 LE)

LOOSE RIVETS AND 1 MISSING RIVET ON WING LEADING EDGE SKIN WS 630 ABOVE NACELLE NR 3. REPLACED RIVETS PER BOEING SRM 51-30-02.

Part: BLKHD ANGLE — CORRODED (BS 1240)

CORROSION Z-ANGLE, ON THE BULKHEAD BS 1240 RIGHT SIDE, LEVEL 1. CORROSION REMOVED PER SRM 51-10-01 AND 51-10-02.

Part: SKIN — CHAFED (NR 1 PYLON)

CHAFED SKIN AT NR 1 NACELLE STRUT TOP SKIN AT NS 222. SMOOTHED OUT SKIN, WITHIN LIMITS PER BOEING SRM 54-10-01.

Part: SPLICE STRAP — CRACKED (BS 1241)

CRACKS IN AFT HOLES OF THE BS 1241 SPLICE STRAP LEFT AND RIGHT SIDE. REPLACED STRAPS PER BOEING SERVICE BULLETIN 747-53-2283.

Part: SKIN — CORRODED (FS 1600-1620)

CORROSION IN FUSELAGE SKIN, RIGHT SIDE BETWEEN BS 1600 AND 1620 S12R, LEVEL 1. CORROSION REMOVED PER BOEING SRM 51-10-01, WITHIN LIMITS PER BOEING SRM 53-10-01.

Part: RAIN CHANNEL — DENTED (BS 860)

DENT IN RAIN CHANNEL AT FUSELAGE LEFT SIDE ABOVE L2 DOOR AT BS 860. BLENDED OUT DENT PER BOEING SRM 51-30-02.

Part: SKIN — CORROSION (FS 2360)

SURFACE CORROSION IN FUSELAGE SKIN RIGHT SIDE BS 2360 BETWEEN S22R AND S25R, LEVEL 1. CORROSION REMOVED PER BOEING SRM 51-10-01, WITHIN LIMITS PER BOEING SRM 53-10-01.

Part: HINGE — GROOVED (RT INBD AILERON)

GROOVE AT RIGHT WING INBOARD AILERON LOWER OUTBOARD HINGE LEADING EDGE. DAMAGE CLEANED UP WITHIN LIMITS PER BOEING SRM 57-20-01, TREATED PER SRM 51-10-01.

Part: SKIN — DENTED (FS 2280-2360)

DENT AND CHAFING IN FUSELAGE SKIN LEFT SIDE BETWEEN BS 2280 AND 2360 BETWEEN S21L AND S23L. DENT STRAIGHTENED AND SMOOTHED PER BOEING SRM 51-40-01 AND WITHIN LIMITS PER BOEING SRM 53-10-01.

Part: SUPPORT — CORRODED (FS 800)

CORROSION ON OMEGA SUPPORT AT STA 800 BETWEEN S38 AND S39, LEVEL 1. REMOVED CORROSION PER BOEING SRM 51-10-01.

Part: SKIN — CORRODED (BS 2360)

CORROSION IN FUSELAGE SKIN AT STA 2360 BETWEEN S4R AND S7R, LEVEL 1. CORROSION REMOVED PER BOEING SRM 51-10-01.

Part: SEAT TRACK — BROKEN (BS 260)

SEAT TRACK IS BROKEN AT STA 260 LBL 60. INSTALLED NEW SEAT TRACK PER BOEING SRM 53-10-05.

Part: BRACKET — BROKEN (NR 3 PYLON)

BROKEN BRACKET THAT ATTACHES FUEL FEED LINE ON NR 3 PYLON CLOSURE SPAR APPROXIMATELY NS 236. FABRICATED NEW BRACKET PER SRM 54-30-02.

Part: SPAR — CHAFED (NR 3 PYLON)

CHAFING ON INSIDE OF LOWER SPAR FROM NS 180 TO NS 236, NR 3 PYLON. REPLACED WEAR STRAPS PER BOEING SRM 51-30-02.

Part: FAIRING — DENTED (FUSELAGE)

SMALL HOLES DENTS AND DELAMINATION ON NR 2 LEFT FAIRING PANEL. REPAIRED PER BOEING SRM 51-40-09.

Part: DOOR — BENT (LT MLG)

LEFT BODY GEAR UPPER DOOR HAS BENT EDGE. DAMAGE TRIMMED AND REPAIRED PER BOEING SRM 51-40-03.

Part: SKIN — DENTED (BS 2200)

DEEP HIT IN THE FUSELAGE SKIN RIGHT SIDE AT BS 2200 S3R. BLENDED OUT DAMAGE IN THE SKIN PER BOEING SRM 51-10-01, DENT IS WITHIN LIMITS PER BOEING SRM 53-10-01.

Part: SUPPORT — CORRODED (FS 980)

CORROSION ON FAIRING SUPPORT BS 980 BETWEEN S40L AND S47L, LEVEL 1. REMOVED CORROSION AS PER SRM 51-10-01.

Part: ANGLE — CORRODED (FWD CARGO DOOR)

CORROSION IN ANGLE BRACKET AT CUTOUT FOR THE FORWARD CARGO DOOR. REPAIRED ANGLE BRACKET PER BOEING SRM 51-40-03.

Part: ANGLE — CORRODED (FS 860-920)

CORROSION ON Z-ANGLE, BETWEEN BS 860 AND 920 S47L AND S47R, LEVEL 1. CORROSION REMOVED PER BOEING SRM 51-10-01.

Part: ANGLES — CRACKED (BS 260)

CRACKED ANGLES ON NOSE WHEEL WELL CEILING STA 260 WL 180 RBL 10 AND LBL 10. NEW ANGLES MANUFACTURED PER BOEING SRM 51-40-03.

Part: FAIRING SUPPORT — CORRODED (FS 800-920)

CORROSION ON FAIRING SUPPORT FROM SIDE STA 800 TO 920 RIGHT SIDE, LEVEL 1. CORROSION REMOVED PER SRM 51-10-01.

Part: ANGLE — CRACKED (NR 3 PYLON)

CRACK ON ANGLE ON NR 3 PYLON CLOSURE SPAR RIGHT INSIDE, APPROXIMATELY NS 215 TO 290. FABRICATED NEW ANGLE AS PER SRM 54-10-02, INSTALLED PER SRM 51-30-02.

Part: DOOR — BROKEN (LEFT WING)

LONG HINGE DOOR UNDER LEFT INBOARD AILERON WALKING BEAM AND MAIN ACTUATOR IS BROKEN. REPAIRED PER BOEING SRM 51-40-09.

Part: FAIRING — DENTED (FUSELAGE)

DENTS NR 5 RIGHT AFT FAIRING PANEL. REPAIRED PER BOEING SRM 51-40-09.

Part: CHORD — CRACKED (NR 2 RT WINDOW)

CREW WINDOW NR 2 RIGHT, FOUND CRACK IN UPPER CHORD INBOARD SIDE AT BS 320. REMOVED AND REPLACED CHORD PER BOEING SRM 51-30-02.

Part: PANEL — DENTED (BS 980-1000)

DENT ON THE CORNER PANEL BETWEEN BS 980 AND 1000 RIGHT SIDE NEAR THE CENTER LINE. REPAIRED PER BOEING SRM 51-40-09.

Part: PANEL — CRACKED (LT WING)

SMALL SURFACE CRACKS AND HOLES OVER INBD SURFACE OF LEFT WING TRAILING EDGE FIXED LOWER PANEL, UNDER NR 4 GROUND SPOILER. REPAIRED PER BOEING SRM 51-40-09.

Part: PANEL — CRACKED (LEFT WING)

CRACKS AND HOLES ON INBOARD SURFACE OF HINGE PANEL NR 591CB. LEFT WING LEADING EDGE CAVITY. REPAIRED PER BOEING SRM 51-40-09.

Part: FUEL DOOR — DAMAGED (LT WING)

PART OF FIBER ON INBOARD SURFACE OF INBOARD FUELING BAY DOOR IS PEELING OFF ON LEFT WING. REPAIRED PER BOEING SRM 51-40-09.

Part: PANEL — PEELED (RT WING LE)

RIGHT WING INTERIOR OF LEADING EDGE CAVITY LOWER SURFACE PANEL 611DB INBOARD SIDE PART OF HONEYCOMB COVER IS MISSING. REPAIRED PER BOEING SRM 51-40-09.

Part: FAIRING — DELAMINATED (NR 2 LT)

NR 2 LEFT FAIRING PANEL HAS DELAMINATION AND HOLES. REPAIRED PER BOEING SRM 51-40-09.

Part: FAIRING — DENTED (NR 2 RT)

NR 2 RIGHT FAIRING PANEL DELAMINATIONS AND DENTS. REPAIRED PER BOEING SRM 51-40-09.

Part: FAIRING — DELAMINATED (NR 4 LT)

NR 4 LEFT FAIRING PANEL DENTED AND DELAMINATED. REPAIRED PER BOEING SRM 51-40-09.

Part: FAIRING — DENTED (NR 6 RT)

NR 6 RIGHT LOWER FAIRING PANEL DELAMINATED AND DENTED. REPAIRED PER BOEING SRM 51-40-09.

Part: PANEL — DELAMINATED (NR 192B)

PANEL NR 192B DENTED AND DELAMINATED. REPAIRED PER BOEING SRM 51-40-09.

Part: FAIRING — DELAMINATED (NR 10)

NR 10 FAIRING PANEL DENTED AND DELAMINATED. REPAIRED PER BOEING SRM 51-40-09.

Part: FAIRING — DENTED (NR 1 RT)

NR 1 RIGHT FAIRING PANEL HAS DENTS AND HOLES. REPAIRED PER BOEING SRM 51-40-09.

Part: FITTING — CRACKED (WS 956)

CRACK ON SUPPORT ROD BASE, ON LOWER FIXED PANEL ON RIGHT WING LEADING EDGE CAVITY WS 956, UNDER NR 8 PDU. INSTALLED NEW FITTING PER BOEING SRM 51-30-02.

Part: PANEL — DELAMINATED (NR 192)

PANEL NR 192 DENTED AND DELAMINATED. REPAIRED PER BOEING SRM 51-40-09.

Part: SUPPORT — CORRODED (BS 1620-1660)

CORROSION ON OMEGA SUPPORT BETWEEN STA 1620 AND 1660. CORROSION REMOVED AS PER BOEING SRM 51-10-01, FOUND WITHIN LIMITS PER BOEING SRM 53-10-01.

Part: FAIRING — DENTED (NR 1 RT)

NR 1 RIGHT LOWER FAIRING PANEL DELAMINATED AND DENTED. REPAIRED PER BOEING SRM 51-40-09.

Part: RIB — CRACKED (RT WING)

RIGHT WING LEADING EDGE CAVITY F.S.S. 1200 ON FORGED RIB AFT END OF UPPER CHORD CRACKED. REPAIRED AS PER BOEING SERVICE BULLETIN 57-2116.

Part: SUPPORT — CORRODED (FUSELAGE)

CORROSION ON FWD FAIRING OMEGA SUPPORT AND ANGLE BETWEEN STA 840 TO 880 AND 920 TO 960, LEVEL 1. CORROSION REMOVED PER BOEING SRM 51-10-01.

Part: FRAME — DAMAGED (NR 5L DOOR)

NR 5 LEFT DOOR FORWARD FRAME DAMAGED INBOARD OF BOTH LOWER STOP FITTINGS. REWORKED DAMAGED AREA PER BOEING SRM 51-10-02.

Part: ANGLE — CRACKED (NR 3 PYLON)

CRACK AND DAMAGE ON ANGLE THAT ATTACHES FAIRING TO WING RIGHT ADJACENT TO UPPER LINK FITTING NS 222 NR 3 PYLON. REPLACED ANGLE PER BOEING SRM 54-10-02.

Part: BRACKET — CORROSION (FUSELAGE)

CORROSION ON OMEGA BRACKET, LEVEL 1. REMOVED PER BOEING SRM 51-10-01.

Part: BUSHING — MIGRATED (NR 4/6 TE FLAPS)

CLEVIS BUSHINGS MIGRATED ON NR 4 AND NR 6 TRAILING EDGE FOREFLAP SEQUENCE CARRIAGES. PERFORMED SERVICE BULLETIN 747-57-2166 FIG 1 ITEMS 2 THROUGH 4.

Part: BRACKET — WORN (HINGE DOOR)

BRACKET UNDER HINGE DOOR NR 573CB IS WORN OUT. MANUFACTURED NEW PART PER BOEING SRM 57-10-02 AND INSTALLED PER BOEING SRM 51-30-02.

Part: SUPPORT — CORRODED (FS 920)

CORROSION ON FAIRING SUPPORT BS 920 BETWEEN S40R AND S47R, LEVEL 1. REMOVED CORROSION PER BOEING SRM 51-10-01.

Part: LE SKIN — TORN (LT AILERON)

TEAR ON LEADING EDGE SKIN LOWER SURFACE ON LEFT INBOARD AILERON IS TORN. REPLACED SKIN PER BOEING SRM 51-30-02.

Part: STRAP — BENT (NR 2 PYLON)

NR 2 PYLON STRAP VENT ON LOWER SPAR AT NS. 180. NEW STRAP FABRICATED PER SRM 54-30-03, INSTALLED PER SRM 51-30-02.

Part: FAIRING — CRACKED (NR 2 PYLON)

NR 2 PYLON HAS CRACK WITH STOP HOLE ON LOWER SAIL BOAT AT NS. 286. DAMAGED SECTION REMOVED FROM SAIL BOAT, FOUND WITHIN LIMITS PER SRM 54-10-01.

Part: RIB — CRACKED (WS 1322)

RIGHT WING LEADING EDGE CAVITY FS 1322 FORGED RIB AFT UPPER CHORD END IS CRACKED. REPAIRED PER BOEING SB 57-2116 FIGURE 6.

Part: RIB — CRACKED (WS 790)

RIGHT WING LEADING EDGE FLAP NR 18 CAVITY WS 790 FORGED RIB LEFT UPPER STIFFENER AND CHORD ARE CRACKED. REPAIRED PER BOEING SERVICE BULLETIN 57-2116 AND BOEING SRM 51-30-02.

Part: BLOW OUT PANEL — DAMAGED (NR 2 PYLON)

NR 2 PYLON DAMAGE ON CUT-OUT ON BLOW OUT PANEL AT NS. 180. INSTALLED DOUBLER PER BOEING SRM 54-10-02 AND 51-30-02.

Part: PANEL — CORROSION (NR 2 PYLON)

SURFACE CORROSION ON SCREW HEADS AND RIVETS NR 2 PYLON FAIRING TO WING LEFT SIDE, ALSO LOOSE RIVETS. REPLACED LOOSE RIVETS PER BOEING SRM 51-30-02 AND CLEANED SURFACE CORROSION PER BOEING SRM 51-10-01.

Part: SKIN — CORRODED (WS 782-1084)

FOUND CORROSION ON RIGHT WING SKIN AND AROUND FASTENERS BETWEEN WS. 782 TO 1084 AT REAR SPAR. REMOVED CORROSION PER BOEING SRM 51-10-01, FOUND WITHIN LIMITS PER BOEING SRM 53-10-01.

Part: SKIN — CORRODED (WS 528-724)

FOUND CORROSION ON RIGHT WING UPPER SKIN AND AROUND FASTENERS BETWEEN WS 528 AND 724 AT THE REAR SPAR. REMOVED CORROSION PER BOEING SRM 51-10-01 FOUND WITHIN LIMITS PER BOEING SRM 53-10-01.

Part: SKIN — CORRODED (LT WING)

CORROSION ON LEFT WING UPPER SKIN BETWEEN MID AND REAR SPAR AT WBL 724. REMOVED CORROSION PER BOEING SRM 51-10-01, AREA IS WITHIN LIMITS PER BOEING SRM 57-20-01.

Part: SPAR — CHAFING (NS 180-236)

CHAFING ON BOTH SIDES LOWER SPAR FROM INSIDE NS. 180 TO NS. 236. FABRICATED NE STRAPS AS PER BOEING SRM 54-10-02, INSTALLED PER SRM 51-30-02.

Part: STRAP — DAMAGED (NR 2 PYLON)

NR 2 PYLON RIGHT SIDE FORWARD LOWER STRAP IS DAMAGED AT NS. 128. NEW STRAP FABRICATED AS PER SRM 54-10-02 AND INSTALLED AS PER SRM 51-30-02.

Part: DOOR PANEL — DELAMINATED (FUSELAGE)

NR 3 HEAT EXCHANGER EXIT DOOR PANEL (AFT OF LOUVERS) DELAMINATED. REPAIRED PER BOEING SRM 51-40-09.

Part: PANEL — PEELING (LT WING)

THE MICARTA STRIP ON LEFT WING TRAILING EDGE LOWER SURFACE OF TOP FIXED PANEL, NEST TO NR 1 SPOILER IS PEELING OFF. REPAIRED PER BOEING SRM 51-40-09.

Part: SAIL BOAT — DAMAGED (NR 3 PYLON)

DAMAGE ON LOWER SAIL BOAT NS 301 NR 3 PYLON. REPAIRED PER BOEING SRM 51-30-02.

Part: SKIN — DAMAGED (LT LE FLAPS)

TOP EDGES OF EACH LEFT WING LEADING EDGE FLAP NR 1 TO NR 10 ARE DAMAGED. REPAIRED PER BOEING SRM 51-40-09.

Part: SKIN — CORRODED (WS 323/586)

RIGHT WING UPPER SKIN CORROSION ON SKIN AND AROUND FASTENERS BETWEEN WS 323 AND WS 586 AT THE MID SPAR. REMOVED CORROSION PER BOEING SRM 51-10-01 AND FOUND WITHIN LIMITS PER BOEING SRM 53-10-01.

Part: PANEL — DENTED (NR 2 PYLON)

NR 2 DAMAGE (DENT) AND RIVET IS PENETRATING SKIN ON RIGHT FAIRING PYLON TO WING. DENT HAS BEEN REMOVED AND RIVET REPLACED AS PER BOEING SRM 51-30-02.

Part: SKIN — LOOSE (NR 3 PYLON)

LOOSE RIVETS ON NR 3 PYLON LEFT SURFACE SKIN. REPLACED RIVETS PER SRM 51-30-02.

Part: SKIN — WORN (LT WING)

EXPOSED FIBER ON LEFT WING LEADING EDGE LOWER EXTERNAL SKIN, UNDER LANDING LIGHT. REPAIRED PER BOEING SRM 51-40-09.

Part: DOOR PANEL — DELAMINATED (FUSELAGE)

NR 1 HEAT EXCHANGER EXIT DOOR PANEL (AFT OF LOUVERS) DELAMAINATED. REPAIRED PER BOEING SRM 51-40-09.

Part: SPAR — DAMAGED (NR 3 PYLON)

DAMAGE ON LOWER SPAR STRAP NS 222 FIREWALL NR 3 PYLON. REPAIRED PER BOEING SRM 54-30-03 FIG 35.

Part: SKIN — PEELING (WS 1100-1250)

RIGHT WING UPPER SURFACE WS 1100 TO 1250 FIBER PEELING OFF. REPAIRED PER BOEING SRM 51-40-09.

Part: TENSION TIE — CRACKED (FS 760)

UPPER DECK TENSION TIE AT STA. 760 LEFT AND RIGHT, FOUND CRACKED. MODIFIED PER BOEING SERVICE BULLETIN 53-2088.

Part: MID FLAP — DAMAGED (LT TE MID FLAP)

LEFT INBOARD TRAILING EDGE MID FLAP HAS 2 AREAS DAMAGED. REPAIRED PER BOEING SRM 51-40-09.

Part: SKIN — CRACKED (NR 3 PYLON)

CRACK WITH STOP DRILLED ENDS ON NR 3 PYLON LEFT SURFACE SKIN AT LOWER SPAR APPROXIMATELY NS 255. REPLACED SKIN PANEL.

Part: SKIN — DAMAGED (NR 3 PYLON)

DAMAGE ON LOWER SPAR LEFT SURFACE SKIN APPROXIMATELY NS 230 NR 3 PYLON. REPAIRED PER BOEING SRM 54-30-03.

Part: SKIN — LOOSE (NR 3 PYLON)

LOOSE RIVETS ON RIGHT EXTERIOR SURFACE SKIN ON NR 3 PYLON. REPLACED RIVETS PER BOEING SRM 51-30-02.

Part: ANGLE — BROKEN (FS 400)

NOSE LANDING GEAR WHEELWELL BS 400 LEFT SIDE ANGLE BRACKET IS BROKEN. MANUFACTURED NEW ANGLE BRACKET FROM 7075-T6 0.50 INCH MATERIAL PER BOEING SRM 53-10-20 AND INSTALLED PER BOEING SRM 51-30-02.

Part: SKIN — CORRODED (WS 724-972)

FOUND CORROSION ON RIGHT WING UPPER SKIN AND AROUND FASTENERS BETWEEN WS 724 AND WS 972 AT THE MID SPAR AREA. REMOVED CORROSION PER SRM 51-10-01 AND FOUND WITHIN LIMITS PER SRM 53-10-01.

Part: SKIN — CORRODED (WS 586)

FOUND CORROSION ON RIGHT WING UPPER SKIN AND AROUND FASTENERS BETWEEN MID AND REAR SPAR AT THE WS. 586 AREA. REMOVED CORROSION PER BOEING SRM 51-10-01, AREA WITHIN LIMITS PER BOEING SRM 57-20-01.

Part: SKIN — CORRODED (LT WING)

CORROSION 3 POINTS ON LEFT WING UPPER SKIN BETWEEN WBL 832 AND 907 AT THE MID SPAR. CLEANED PER BOEING SRM 51-10-01 AND FOUND WITHIN LIMITS PER BOEING SRM 57-20-01.

Part: SKIN — CORRODED (LT WING)

CORROSION ON 3 POINTS ON LEFT WING UPPER SKIN BETWEEN MID AND AFT SPARS BETWEEN WBL. 586 AND 617 (LEVEL 1). CORROSION REMOVED PER BOEING SRM 51-10-01 AND FOUND WITHIN LIMITS PER BOEING SRM 57-20-01.

Part: TENSION TIES — CRACKED (FUSELAGE)

UPPER DECK TENSION TIE AT STA. 780, 800, 820, 860, 880, 900, 920, 940 LH AND RH, FOUND CRACKS. REPAIRED PER BOEING SERVICE BULLETIN 53-2371.

Part: SKIN — CRACKED (NR 2 PYLON)

CRACK ON NR 2 PYLON EXTERNAL SKIN ON RIGHT FORWARD LOWER SPAR EDGE. NEW STRAP FABRICATED PER BOEING SRM 54-10-02, INSTALLED PER BOEING SRM 51-30-02.

Part: SKIN — CORRODED (BS 1480-1680)

CORROSION ON SKIN BETWEEN STR 40 TO 50 AND BETWEEN STA 1480 TO 1680 LT AND RT. REMOVED AS PER BOEING SRM 51-10-01.

Part: SUPPORT — CORROSION (BS 1480-1620)

CORROSION ON SUPPORT FAIRING AT THE CENTER LINE BETWEEN STATION 1480 TO 1620. CORROSION REMOVED PER BOEING SRM 51-10-01.

Part: SEAT TRACK — CORRODED (BS 620-640)

UPPER DECK SEAT TRACK CORRODED AT LBL 22 BETWEEN STA 620 TO 640. REMOVED CORROSION AS PER BOEING SRM 51-10-01.

Part: SEAT TRACK — CORRODED (FS 530-540)

UPPER DECK SEAT TRACK LBL 6O BETWEEN STA. 530 TO 540 CORRODED. REMOVED CORROSION PER SRM 51-10-01 WITHIN LIMITS.

Part: SKIN — CORRODED (BS 1660)

CORROSION ON FITTING SUPPORT FAIRING AT STA 1660 STR 49 AREA. REPAIRED PER BOEING SRM 51-40-04.

Part: SUPPORT — CORRODED (BS 1580)

CORROSION ON SUPPORT FAIRING STA 1580 BETWEEN STR 28 TO 50 RT AND LT. CORROSION REMOVED PER SRM 51-10-01.

Part: SUPPORT — CORRODED (BS 1540)

CORROSION ON SUPPORT FAIRING STA 1540 BETWEEN STR 25 TO 50. CORROSION REMOVED AS PER BOEING SRM 51-10-01.

Part: ANGLE — CRACKED (BS 580)

UPPER DECK FLOORBEAM CHORD AT STA 580 RBL 45, FOUND CRACKED ANGLE. INSTALLED NEW ANGLE PER BOEING SRM 51-10-00.

Part: FAIRING — DELAMINATED (NR 5)

NR 5 FAIRING PANEL DELAMINATED ON OUTER SIDE. REPAIRED PER BOEING SRM 51-40-09.

Part: FAIRING — CORROSION (BS 1620)

CORROSION ON AFT FAIRING AT STA 1620 STRINGER 47 AREA. CORROSION REMOVED PER BOEING SRM 51-10-01.

Part: TE FIBER — DETERIORATED (NR 21 LE FLAP)

RIGHT WING LEADING EDGE FLAP NR 21 VARIABLE CAMBER TRAINING EDGE FIBER IS DETERIORATED. REPAIRED PER BOEING SRM 51-40-09.

Part: FASTENERS — CORRODED (LT WING)

CORROSION AROUND FASTENERS AT WBL 862 AND 1056 AT THE MID SPAR. CLEANED CORROSION AS PER BOEING SRM 51-10-01.

Part: SUPPORT — DENTED (BS 1620-1660)

DENT ON OMEGA SUPPORT BETWEEN STA 1620 TO 1660 STR 40 AREA. REPAIRED AS PER BOEING SRM 51-40-04.

Part: SKIN REPAIR — PEELING (LT TE MID FLAP)

LEFT WING INBOARD MID FLAP LOWER SKIN HAS FIBERGLASS REPAIR PEELING OFF. REPAIRED PER BOEING SRM 51-40-09.

Part: SKIN — CORRODED (BS 1480-1680)

CORROSION ON FUSELAGE SKIN AT THE CENTER LINE BETWEEN S50L AND S50R BETWEEN STA 1480 AND 1680. CORROSION REMOVED AS PER BOEING SRM 51-10-10.

Part: SKIN — CORRODED (WS 724-972)

FOUND CORROSION ON RIGHT WING UPPER SKIN AND AROUND FASTENERS BETWEEN WBS 724 AND WS 972 AT THE FRONT SPAR AREA. CORROSION REMOVED PER BOEING SRM 51-10-01 AND FOUND WITHIN LIMITS PER BOEING SRM 53-10-01.

Part: SKIN — DELAMINATING (LT ET FLAP)

LEFT WING OUTBOARD FLAP AFT FLAP HAS LARGE REPAIR DELAMINATING. REPAIRED PER BOEING SRM 51-40-09.

Part: EXHAUST — CRACKED (APU)

APU EXHAUST AFT END AT 12 O'CLOCK IS CRACKED. TRIMMED AND SMOOTHED THE CRACK PER BOEING SRM 51-10-01.

Part: COVER — DELAMINATED (WS 1120)

RIGHT WING LEADING EDGE WS. 1120 FIBER COVER ABOVE PYLON NR 4 COMING OFF. REPAIRED PER BOEING SRM 51-40-09.

Part: ARM — CORRODED (NLG)

NOSE LANDING GEAR ARM CONNECTED TO LANDING GEAR ACTUATOR IS CORRODED ON FORWARD SIDE. CORROSION REMOVED AND TREATED PER BOEING SRM 51-10-01.

Part: SUPPORT — CORRODED (BS 1660)

CORROSION ON SUPPORT FAIRING STA 1660 BETWEEN STR 33 TO 46 LT AND RT. REPAIRED AS PER BOEING SRM 51-10-01.

Part: AFT FLAP — DAMAGED (LT TE FLAP)

LEFT WING OUTBOARD FLAP AFT FLAP HAS LARGE REPAIR REQUIRING UPGRADE. REPAIRED PER BOEING SRM 51-40-09.

Part: STRINGER — CORRODED (BS 1740-1750)

DURING BASE LINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION STRINGER 41 BS 1740 TO 1750.

Part: TE SKIN — DAMAGED (AFT TE FLAP)

FOUND LEFT OUTBOARD TRAILING EDGE AFT FLAP OUTBOARD TRAILING EDGE DAMAGED. REPAIRED ACCORDING TO BOEING SRM 51-40-09.

Part: TRUNNION — CRACKED (RT MLG)

DURING INSPECTION PER AD 90-06-18 R1, FOUND CRACK INDICATION ON RIGHT WING LANDING GEAR TRUNNION JOURNAL OUTBOARD BOLT HOLE. REPAIRED BY REAMING HOLE PER BOEING M/M 32-11-47 AND INSTALLING BUSHING PER BOEING MM 32-11-49.