N840AL

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,608 hrs · 68,014 cycles

DURING SCHEDULED MX FOUND A 2 INCH FUSELAGE SKIN CRACK ON THE LT SIDE BS 787 STRINGER 19L.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,311 hrs · 67,390 cycles

DURING SCHEDULED MX FOUND A 4 INCH FUSELAGE SKIN CRACK ON THE RT SIDE BS 344 STRINGER 15R.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,311 hrs · 67,390 cycles

DURING SCHEDULED MX FOUND A 3 INCH FUSELAGE SKIN CRACK ON THE LT SIDE BS 727B STRINGER 18L.

Part: SPAR — CORRODED (LT WING) · airframe 64,799 hrs · 66,271 cycles

LT WING L/E SPAR AT STA 278 HAS CORROSION AROUND FASTENER HOLES. INSTALLED REPAIR IAW DWG 57-14014-1 AND FAA 8110-3, APPROVAL.

Part: DOOR FRAME — GOUGED (BS 348) · airframe 64,799 hrs · 64,271 cycles

GOUGE IN LOWER BS 348 DOOR FRAME STRINGER 16L. INSTALLED NEW FRAME IAW SRM 53-10-2, FIG 1 AND DRG 65-54961-1, SH 1.

Part: FLOORBEAM — CORRODED (BS 807) · airframe 64,799 hrs · 66,271 cycles

CORROSION ON UPPER FLANGE CABIN FLOORBEAM, BS 807 BETWEEN LBL 45 AND RBL 45. INSTALLED REPAIR IAW DWG 53-14034-1 WITH 8110-3 APPROVAL.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 64,799 hrs · 66,271 cycles

INBD LT FLAP WB 96 HAS DENT IN L/E UPPER SURFACE. INSTALLED REPAIR IAW SRM 57-50-4 & 51-30-2.

Part: SEAT TRACK — CORRODED (BS 540-580) · airframe 64,799 hrs · 66,271 cycles

CORROSION ON BOTH FLANGES OF CABIN SEAT TRACK BS 540 - 580. INSTALLED A REPAIR IAW DWG 57-14029 WITH 8110-3 APPROVAL.

Part: SPAR — CORRODED (LT WING) · airframe 64,799 hrs · 66,271 cycles

LT WING L/E CAVITY LOWER SPAR HAS CORROSION AROUND FASTENER HOLES. INSTALLED REPAIR IAW DWG 57-14015-1 WITH 8110-3 APPROVAL.

Part: NUT PLATE — DAMAGED (HORIZONTAL STAB) · airframe 64,799 hrs · 66,271 cycles

LT & RT HORIZONTAL STAB HINGE FITTINGS HAVE QUESTIONAL CLEARANCE. R & R NUTPLATES IAW DWG 55-14054-1 WITH 8110-3, APPROVAL.

Part: SKIN — DAMAGED (RT WING TE FLAP) · airframe 64,799 hrs · 66,271 cycles

RIGHT INBD MIDFLAP HAS AREAS OF CORROSION UPPER SURFACE AND PUNCTURE IN SKIN. REMOVED CORROSION IAW SRM 51-10-06. FABRICATED AND INSTALLED REPAIR TO SKIN IAW SRM 51-30-2.

Part: FLOORBEAM — CORRODED (BS 727B) · airframe 64,799 hrs · 66,271 cycles

CORROSION ON UPPER FLANGE OF CABIN FLOORBEAM AT STA 727B BETWEEN LBL 24-RBL 45. INSTALLED A REPAIR IAW DWG 53-14028-1 WITH 8110-3, APPROVAL.

Part: SKIN — DENTED (FUSELAGE) · airframe 64,799 hrs · 66,271 cycles

SEVERAL DENTS JUST FWD AT TAIL JACK POINT. FABRICATED REPAIR PARTS IAW SRM 53-30-3, PG 357-359 AND INSTALLED IAW SRM 51-30-2.

Part: BULKHEAD — DAMAGED (AFT) · airframe 64,799 hrs · 66,271 cycles

AFT PRESSURE BULKHEAD AFT SIDE PAN & COVER AREA CHAFED. REMOVED DAMAGE GORE WEB AND PREVIOUS REPAIR IAW SRM 51-30-2, PG 32 AND SR1-2020138697 INSTRUCTIONS. HFEC EDDY CURRENT HOLES AND SURROUNDING AREA.INSTALLED REPAIR IAW SRM 53-10-11, PG 119-127, DWG 53-14025 AND FAA FORM 8110-9 APPROVAL.

Part: SPAR — CORRODED (LT WING) · airframe 66,271 hrs · 64,799 cycles

LT WING L/E CAVITY LOWER SPAR AT LWS 567 HAS CORROSION. CORRISON WAS OUT OF LIMITS. INSTALLED REPAIR IAW DWG 57-14014-1.

Part: SPAR — CORRODED (LT WING) · airframe 66,271 hrs · 64,799 cycles

LEFT WING L/E CAVITY FWD LOWER SPAR AT LWS 476 HAS CORROSION. AREA OF CORROSION WAS OUT OF LIMITS. INSTALLED REPAIR IAW DWG 57-14015-1 WITH APPROVAL IAW 8110-3.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 66,271 hrs · 64,799 cycles

INBD LT FLAP WB 117.10 L/E DENTED IN UPPER SURFACE. REMOVED DAMAGED AREA AND INSTALLED REPAIR IAW SRM 57-50-4, FIG 4.

Part: SUPPORT CHANNEL — CORRODED (BS 727-887) · airframe 66,271 hrs · 64,799 cycles

LT CARGO BAY SIDEWALL SUPPORT CHANNEL HAS NUMEROUS AREAS OF CORROSION LBL 22 BETWEEN BS 727 - 887. REPAIRED IAW SRM 53-10-13, FIG 1.

Part: SEAT TRACK — CORRODED (BS 476-480) · airframe 66,271 hrs · 64,799 cycles

SEAT TRACK FLANGE HAS CORROSION AT BS 476-480. INSTALLED THE SEAT TRACK REPAIR IAW SRM 51-30-05, FIG 7.

Part: SUPPORT FITTING — CORRODED (BS 1144) · airframe 66,271 hrs · 64,799 cycles

FITTING CORRODED LT SIDE APU BAY, BS 1144. AFT LATCH SUPPORT, FABRICATED AND INSTALLED LATCH SUPPORT FITTING IAW SRM 51-30-2.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 66,271 hrs · 64,799 cycles

FLOOR SUPPORT CHANNEL CORRODED. FABRICATED AND INSTALLED NEW FLOOR SUPPORT IAW SRM 51-20-1 FIG 7 & 51-30-2.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 66,271 hrs · 64,799 cycles

FLOOR SUPPORT CHANNEL CORRODED. FABRICATED AND INSTALLED NEW FLOOR SUPPORT IAW SRM 51-20-1, FIG 7 AND 51-30-2.

Part: FLOORBEAM — CORRODED (BS 887) · airframe 66,271 hrs · 64,799 cycles

FLOORBEAM UPPER SURFACE HAS CORROSION AT BS 887, BL 0 TO RBL 45. FLOORBEAM REPAIRED IAW SRM 53-10-9, FIG 7.

Part: FRAME — CORRODED (BS 500B) · airframe 66,271 hrs · 64,799 cycles

FWD CARGO BAY BS 500B, S26R HAS CORROSION UNDER FRAME LIP. INSTALLED FRAME REPAIR IAW SRM 53-10-4.

Part: STRINGER — CORRODED (BS 440-500A) · airframe 66,271 hrs · 64,799 cycles

STRINGER 27L HAS AREAS OF CORROSION IN FWD CARGO BAY BETWEEN BS 440 - 500A. INSTALLED STRINGER REPAIR IAW SRM 53-10-3, FIG 1, SHT 7, DETAIL VI.

Part: SUPPORT CHANNEL — CORRODED (BS 380-520) · airframe 66,271 hrs · 64,799 cycles

CORROSION UNDER AND AROUND NUTPLATES ON BOTTOM OF LT SIDEWALL SUPPORT CHANNEL FWD CARGO BAY AT BS 380 AND 520, LBL 23. INSTALLED SUPPORT CHANNEL AND SPLICE IAW SRM 53-10-13.

Part: SKIN — CORRODED (RT WING TE FLAP) · airframe 66,271 hrs · 64,799 cycles

RIGHT OTBD AFT FLAP HAS CORROSION ON UPPER L/E STARTING APPROX 144 INCHES FROM INBD EDGE OF PART. REMOVED DAMAGED AREA OF SKIN AND INSTALLED A REPAIR IAW SRM 57-50-4, FIG 5, NOTE 1.

Part: STIFFENER — CRACKED (VERTICAL STAB) · airframe 66,271 hrs · 64,799 cycles

VERTICAL STABILIZER FRONT SPAR AFT SURFACE AT VSS 200 RT HAS A CRACKED STIFFNER. FABRICATED AND INSTALLED STIFFNER IAW SRM 51-30-5 & 51-30-2.

Part: INTERCOSTAL — CRACKED (BS 460-480) · airframe 66,271 hrs · 64,799 cycles

FWD PIT INTERCOSTAL CRACKED, BS 460-480, S25-26L. CUTOUT DAMAGED AREA AND INSTALLED REPAIR IAW SRM 737-51-40-3, PG 1.

Part: SHEAR TIE — CORRODED (BS 767) · airframe 66,271 hrs · 64,799 cycles

SHEAR TIE CORRODED IN AFT CARGO BAY BILGE BS 767, LBL 10-12. REPLACED SHEAR TIE IAW SRM 51-30-2..

Part: SEAT TRACK — CORRODED (BS 480) · airframe 66,271 hrs · 64,799 cycles

CABIN SEAT TRACK CROWN HAS CORROSION AT BS 480+10, RBL 25. SEAT TRACK REPAIRED IAW SRM 53-10-5, FIG 8.

Part: SEAT TRACK — BROKEN (BS 360) · airframe 66,271 hrs · 64,799 cycles

CABIN SEAT TRACK CROWN IS BROKEN, BOTH SIDES AT BS 360+14 LBL 23. INSTALLED SEAT TRACK REPAIR IAW SRM 53-10-5.

Part: SEAT TRACK — CORRODED (BS 986) · airframe 66,271 hrs · 64,799 cycles

CABIN SEAT TRACK FLANGE HAS CORROSION AT BS 986+2 RBL 17. INSTALLED SEAT TRACK REPAIR IAW SRM 53-10-5.

Part: SUPPORT CHANNEL — CORRODED (BS 493-520C) · airframe 66,271 hrs · 64,799 cycles

CORROSION ON BOTTOM OF RT SIDEWALL SUPPORT CHANNEL IN FWD CARGO BAY BS 493 TO 520C, RBL 23. FABRICATED AND INSTALLED REPAIR SUPPORT CHANNEL IAW SRM 51-30-01, FIG 7 & 51-30-2.

Part: INTERCOSTAL — CORRODED (BS 500B-520) · airframe 66,271 hrs · 64,799 cycles

INTERCOSTAL CORRODED IN FWD CARGO BAY BETWEEN BS 500B AND 520. FABRICATED INTERCOSTAL AND INSTALLED IAW SRM 51-20-1, FIG 3/6 AND 51-30-2, PARA 4.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 66,271 hrs · 64,799 cycles

FWD CARGOBAY UNDER FLOOR SUPPORT RT DOOR THRESHOLD AT AFT DOOR FRAME HAS CORROSION. CLEANED AREA AND FOUND NUTPLATE CHANNEL CORRODED. R & R CHANNEL IAW SRM 51-40-4 PG 18 & 19 AND 51-30-2.

Part: STRINGER — CORRODED (BS 380) · airframe 66,271 hrs · 64,799 cycles

STRINGER 27L CORRODED IN FWD CARGO BAY BS 380. REMOVED SECTION OF CORRODED STRINGER. FABRICATED, LOCATED AND DRILLED NEW SECTION IAW SRM 53-10-3, FIG 1. INSTALLED REPAIR PARTS IAW SRM 53-10-3.

Part: FAIRING — DENTED (THRUST REVERSER) · airframe 66,271 hrs · 64,799 cycles

NR 1 ENGINE INBD THRUST REVERSER ACTUATOR FAIRING HAS A DENT. REMOVED DAMAGED AREA, AND INSTALLED A REPAIR IAW SRM 51-40-2, FIG 1, 51-40-2.

Part: SEAT TRACK — CORRODED (BS 741-751) · airframe 66,271 hrs · 64,799 cycles

CORROSION ON SEAT TRACK, RBL 25 FROM BS 741-751. REMOVED DAMAGED AREAS OF SEAT TRACK IAW SRM 53-10-5, FIG 8. INSTALLED SECTION OF SEAT TRACK IAW SRM 51-30-2.

Part: SKIN — DENTED (HORIZONTAL STAB) · airframe 66,271 hrs · 64,799 cycles

LT HORIZONAL SKIN DENT AT LT SIDE STAB STA 111, 15" OF FRONT SPAR. REMOVED DAMAGED SKIN IAW SRM 55-10-3, FIG 8. INSTALLED REPAIR IAW SRM 55-10-3, FIG 8.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 66,271 hrs · 64,799 cycles

LEFT HORIZONTAL STAB RIB LOWER ANGLE CRACKED STA 111, 15" FROM FRONT SPAR. REMOVED RIB WEB AND SECTION LOWER CHORD, FABRICATED REPAIR AND INSTALLED IAW SRM 55-10-3, FIG 8 AND 51-30-2.

Part: CHANNEL — CRACKED (CARGO BAY) · airframe 66,271 hrs · 64,799 cycles

FWD CARGO BAY HAT CHANNEL DOUBLER FOR VHF ANTENNA IS CRACKED. REMOVED HAT CHANNEL, FABRICATED NEW CHANNEL AND REINSTALLED NEW SECTION IAW SRM 51-30-2.

Part: SILL — CORRODED (BS 907) · airframe 66,271 hrs · 64,799 cycles

CABIN BELOW FLOOR SUPPORTS HAS CORROSION ON UPPER SURFACE BS 907+6, RBL 60. REMOVED CORRODED AREAS AND REPAIRED MOPSILL IAW SRM 51-30-2 AND 51-40-3.

Part: SEAT TRACK — DAMAGED (BS 480) · airframe 66,271 hrs · 64,799 cycles

SEAT TRACK CROWN DAMAGED AT BS 480+12 LBL 6L. CUT AND REMOVED DAMAGED AREA IAW SRM 53-10-05, FIG 9 AND INSTALLED REPAIR IAW SRM 51-30-02.

Part: FLOORBEAM — CORRODED (BS 616) · airframe 66,271 hrs · 64,799 cycles

FLOORBEAM UPPER SURFACE HAS CORROSION AT BS 616 BL 0-LBL 26. REPAIRED IAW SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 400-460) · airframe 66,271 hrs · 64,799 cycles

SEAT TRACK FLANGE HAS CORROSION AROUND FASTENER HOLES UPPER & LOWER SURFACES BS 400 TO 460, RBL 62. INSTALLED REPAIR IAW SRM 53-10-5.

Part: INTERCOSTAL — CORRODED (BS 500A-500B) · airframe 66,271 hrs · 64,799 cycles

INTERCOSTAL CORRODED, FWD CARGO BAY LBL 24.5 BETWEEN BS 500B AND 500A. INSTALLED NEW INTERCOSTAL IAW SRM 51-30-2.

Part: FRAME — CRACKED (CARGO DOOR) · airframe 64,105 hrs · 64,695 cycles

CARGO DOOR HAS 1.2500" CRACK ON Z-FRAME. REPAIR IS A TYPICAL FORMED SECTION REPAIR FROM SRM.

Part: STRUCTURE — CRACKED (SERVICE DOOR) · airframe 64,105 hrs · 64,695 cycles

1.7500" CRACK FOUND ON FWD SERVICE DOOR, BS 328.

Part: INTERCOSTAL — CRACKED (DOOR FRAME) · airframe 64,105 hrs · 64,695 cycles

CRACK FOUND ON INTERCOSTAL INSIDE OF FWD SERVICE DOOR FRAME BS 332.

Part: DOOR FRAME — CRACKED (SERVICE DOORWAY) · airframe 64,105 hrs · 64,695 cycles

CRACK FOUND ON FWD SERVICE DOOR DOOR FRAME B.S. 332.

Part: SKIN — CRACKED (BS 787 S18L) · airframe 63,650 hrs · 63,715 cycles

DURING SERVICE CHECK, FOUND A 2 INCH SKIN CRACK ON THE LT SIDE AFT OF THE T/E WING TO BODY FAIRING BS 787, STRINGER 18L. REPAIRED IAW SRM 53-30-3, FIG 48, DETAIL XI, PROCEDURE IV & VII.

Part: SKIN — CRACKED (BS 827 S19L) · airframe 63,650 hrs · 63,715 cycles

DURING SERVICE CHECK, FOUND A 3 INCH SKIN CRACK ON THE LT SIDE AFT OF THE T/E WING TO BODY FAIRING BS 827, STRINGER 19L. REPAIRED IAW SRM 53-30-3, FIG 48, DETAIL XI, PROCEDURE IV & VII.

Part: PLUG — FAILED (LT MLG ACTUATOR) · airframe 63,430 hrs · 63,240 cycles

AFTER TAKEOFF, BOTH HYDRAULIC A LOW PRESSURE LIGHTS ILLUMINATED THEN EXTINGUISHED. HYDRAULIC PRESSURE NORMAL BUT HYDRAULIC QUANTITY AT ZERO. DECLARED EMERGENCY AND RETURNED DEPARTURE. INSPECTED ACFT AND FOUND PLUG FROM LT MLG ACTUATOR DAMAGED. R & R PLUG.

Part: SKIN — CORRODED (BS 1016) · corrosion level 2 · airframe 62,796 hrs · 61,886 cycles

EXFOLIATION CORROSION AT STA 1016 AT STRINGER 26R TO 27R IN AREA OF OUTER WASTE DRAIN PAN. REMOVED CORROSION, AFTER REMOVAL OF CORROSION IT WAS DETERMIND THAT THERE WAS EXCESSIVE MATERIAL LOSS, WHICH DETERMIND THE AREA TO BE OUT OF LIMITS. AFTER EVALUATION IS WAS DETERMIND THAT THE REPAIR WAS NOT A STANDARD SRM REPAIR. CONTACTED ENGINEERING FIRM FLIGHT VEHICLE CONSULTING (FVC). A REPAIR SCHEME WAS DEVELOPED AND SUBMITTED. A REPAIR EO WAS PROVIDED AND THE ACFT WAS REPAIRED IAW WITH FLIGHT VEHICLE CONSULTING EO 53-12090-1.

Part: STRINGER SPLICE — CORRODED (BS 1016) · corrosion level 2 · airframe 62,796 hrs · 61,886 cycles

CORROSION AT FUSELAGE BULKHEAD BS 1016 AT STRINGER 25R. REMOVED CORROSION, AFTER CORROSION REMOVAL, AREA FOUND TO BE OUT OF LIMITS AT STRINGER 25R FROM STA 1016 TO 1026. FABRICATED REPAIR SPLICE AND INSTALLED REPAIR COMPOENENTS IAW SRM.

Part: FLOOR SUPPORT — CORRODED (BS 663) · corrosion level 2 · airframe 62,796 hrs · 61,886 cycles

CORROSION ON FLOOR SUPPORT AT STA 663 NEAR RBL 45. REMOVED CORROSION FROM FOUND SUPPORT, CORROSION FOUND TO BE OUT OF LIMITS. R & R FLOOR SUPPORT IAW CURRENT SRM.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 62,796 hrs · 61,886 cycles

CORROSION RT WING UPPER SURFACE UNDER WING WALKWAY PAINT AT WING STA 765.9 AT WBL 92.5. BLENDED CORROSION, AFTER CORROSION REMOVAL IT WAS DETERMIND THE MATERIAL LOSS WAS OUT OF LIMITS. AFTER REVIEWING THE CURRENT SRM IT WAS DETERMIND THERE WAS NOT REPAIR IN THE SRM. THE DISCREPANCY WAS REFERED TO A DER, FLIGHT VEHICLES CONSULTING. A REPAIR SCHEME WAS DEVELOPED AND PROVIDED. ALL REPAIRS WERE ACCOMPLISHED UNDER THE INSTRUCTIONS PROVIDED BY THE EO FROM FLIGHT VEHICLES CONSULTING ON EO 57-12102-1.

Part: FLOORBEAM — CORRODED (BS 767) · corrosion level 2 · airframe 62,796 hrs · 61,886 cycles

CORROSION ON FLOORBEAM AT BS 767 AT RBL 45. REMOVED CORROSION, AFTER CORROSION REMOVAL, DAMAGE FOUND TO BE OUT OF LIMITS. REMOVED CORRODED FLOORBEAM, AND FABRICATED REPAIR STRAPS AND INSTALLED STRAPS IAW CURRENT SRM.

Part: RIB — CRACKED (NR 2 NACELLE) · airframe 62,796 hrs · 61,886 cycles

NR 2 ENGINE FIXED FAN COWL HAS CRACKED RIB. REMOVED CRACKED RIB AND FABRICATED REPAIR PARTS AND INSTALLED REPAIR PARTS IAW CURRENT SRM.

Part: FRAME — CRACKED (BS 380) · corrosion level 2 · airframe 62,796 hrs · 61,886 cycles

CRACK AT INTERNAL FRAME, STRINGER 5R BODY STATION 380. REMOVED 2 EA STRINGER CLIPS 5R AT BODY STATION 380, REMOVED DAMAGED INTERIOR FRAME, FABRICATED REPAIR PARTS AND INSTALLED ALL REPAIR PARTS IAW SRM.

Part: FLOORBEAM — CORRODED (BS 706) · corrosion level 2 · airframe 62,796 hrs · 61,886 cycles

CORROSION ON FLOORBEAMS AT BS 706 AT RBL 45. REMOVED CORROSION FROM FLOORBEAM BS 706. CORROSION FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR PARTS FOR FLOORBEAM AND INSTALLED ALL REPAIR PARTS IAW CURRENT SRM.

Part: ACCESS PANEL — CORRODED (ZONE 500) · corrosion level 2 · airframe 62,796 hrs · 61,886 cycles

CORROSION AT LT WING FWD LOWER SPAR AT ACCESS PANEL MATING SURFACE FROM WBL 227.0 TO WBL 522.0. REMOVE ALL CORROSION FROM PANEL MATING SURFACE. MATERIAL LOSS FOUND TO OUT OF LIMITS AT WBL 291.82 AND WBL 314.76. DAMAGE FOUND TO BE OUTSIDE OF THE PARAMETER OUTLINED IN SRM. A REPAIR SCHEME WAS DEVELOPED AND PROVIDED. ALL REPAIR PARTS AND INSTALLATION WAS PERFORMED AS OUTLINED DWG 57-12094-1. AREAS THAT WERE WITH-IN LIMITS WERE TREATED AND PRIMED IAW INSTRUCTIONS OUTLINED IN CURRENT SRM.

Part: RIB — CRACKED (L/E FLAP) · airframe 62,796 hrs · 61,886 cycles

LEFT FORE FLAP WBL 355 INBD SIDE OF RIB HAS A CRACK IN FITTING. R & R IAW SRM.

Part: RIB — CORRODED (LT MLG DOOR) · corrosion level 2 · airframe 62,796 hrs · 61,886 cycles

CORROSION ON AFT RIB OF LT MLG INNER DOOR. FOUND RIB ON INNER DOOR FOR LT MLG CORROSION BEYOND LIMITS. R & R RIB IAW SRM.

Part: SKIN — CORRODED (ZONE 500) · corrosion level 2 · airframe 62,796 hrs · 61,886 cycles

CORROSION ON TOP OF LT WING UNDER WALKWAY PAINT. BLENDED CORROSION, AFTER CORROSION REMOVAL FROM WING SKIN, MATERIAL LOSS FOUND TO BE OUT OF LIMITS. REPAIR REQUIREMENTS FOUND TO BE OUTSIDE OF STANDARD SRM REPAIR. FABRICATED REPAIR PARTS AND INSTALLED ALL REPAIR PARTS AS OUTLINED BY EO 57-12101-1.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 62,796 hrs · 61,886 cycles

CORROSION ON FLOORBEAM AT STA 312 AT RBL 12. REMOVED CORROSION, FLOORBEAM FOUND TO BE OUT OF LIMITS. CUT OUT TEE CAP EXTRUSION, FABRICATED REPAIR PARTS AND INSTALLED REPAIR PARTS IAW SRM.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 62,796 hrs · 61,886 cycles

CORROSION AT BS 1004, AT STRINGER 27L. CUT OUT CORRODED SECTION OF STRINGER. FABRICATED REPAIR PARTS AND INSTALLED REPAIR PARTS IAW SRM.

Part: STRINGER SPLICE — CRACKED (ZONE 100) · airframe 62,796 hrs · 61,886 cycles

STRINGER SPLICE CRACKED AT S4L AT BS 908. REMOVED CRACKED STRINGER SPLICE, FABRICATED REPAIR PARTS AND INSTALLED REPAIR PARTS IAW SRM.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 62,796 hrs · 61,886 cycles

CORROSION ON SEAT TRACK AT STA 540 TO 578 AT LBL 24.75. REMOVED CORROSION, SEAT TRACK FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR PARTS AND INSTALLED IAW SRM.

Part: RETAINER SEAL — CORRODED (NR 5 SLAT) · corrosion level 2 · airframe 62,796 hrs · 61,886 cycles

CORROSION ON RT NR 5 L/E SLAT LOWER SEAL RETAINER. REMOVED CORROSION, SEAL RETAINER FOUND TO BE OUT OF LIMITS. FABRICATED NEW SEAL REATINER AND INSTALLED IAW WITH CURRENT SRM.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 62,796 hrs · 61,886 cycles

CORROSION ON FLOORBEAM AT BS 727B AND RBL 24. REMOVED CORROSION, FLOORBEAM FOUND TO BE OUT OF LIMITS, FABRICATED REPAIR STRAP AND INSTALLED ALL REPAIR PARTS IAW SRM.

Part: FLOORBEAM — CORRODED (BS 540) · corrosion level 2 · airframe 62,796 hrs · 61,886 cycles

CORROSION ON FLOORBEAM AT BS 540 AND LBL 24. REMOVED CORROSION, FLOOR SUPPORT FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR STRAP AND INSTALLED REPAIR PARTS IAW SRM.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 62,796 hrs · 61,886 cycles

CORROSION ON SEAT TRACK AT STATION 540 AND RBL 64. AFTER CORROSION REMOVAL, SEAT TRACK FOUND TO BE OUT OF LIMITS. REPLACED SEAT TRACK IAW SRM.

Part: RUB STRIP — GOUGED (LT WING) · airframe 62,796 hrs · 61,886 cycles

LT INBD ENGINE TO WING FLAP SUPPORT FITTING RUB STRIP IS GOUGED. REMOVED RUB STRIP, FABRICATED REPAIR STRIP AND INSTALLED STRIP IAW SRM.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 62,796 hrs · 61,886 cycles

CORROSION ON FLOORBEAM AT BS 967 AND RBL 12. CORROSION FOUND TO BE OUT OF LIMITS. PERFORMED A SPLICE REPAIR TO THE FLOORBEAM IAW CURRENT SRM.

Part: RETAINER SEAL — CORRODED (ZONE 500) · corrosion level 2 · airframe 62,796 hrs · 61,886 cycles

CORROSION ON NR 2 L/E SLAT LOWER RUB SEAL RETAINER OTBD OF SLAT ACTUATOR ATTACH POINT. REMOVED CORRODED SEAL RETAINER, FABRICATED REPAIR PARTS AND INSTALLED SEAL RETAINER IAW SRM.

Part: SEAT TRACK — CORRODED (BS 663-747) · corrosion level 2 · airframe 62,796 hrs · 61,886 cycles

CORROSION ON SEAT TRACK AT BS 663 TO 747 AT RBL 24.75. R & R SEAT TRACK IAW SRM.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 62,796 hrs · 61,886 cycles

CORROSION ON FLOORBEAM AT STA 727 AND RBL 24 TO 36. REMOVED CORROSION, FLOORBEAM FOUND TO BE OUT OF LIMITS, FABRICATED REPAIR STRAP AND INSTALLED IAW CURRENT SRM.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 62,796 hrs · 61,886 cycles

CORROSION ON FLOORBEAM CAP AT STA 727B AND APPROX LBL 40. AFTER CORROSION REMOVAL FLOORBEAM FOUND TO BE OUT OF LIMITS. FABRICATED A REPAIR STRAP AND INSTALLED IAW CURRENT SRM.

Part: ANGLE — CRACKED (ZONE 100) · airframe 62,796 hrs · 61,886 cycles

AFT CARGO BAY LEFT TRANSITION PANEL ANGLE CRACKED BETWEEN STATION 907 AND 927. REMOVED CRACKED ANGLE AND FABRICATED REPLACE PARTS IAW SRM.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 62,796 hrs · 61,886 cycles

CORROSION ON SEAT TRACK AT STA 663 TO 727 AND LBL 62. REMOVED CORROSION, SEAT TRACK BECAME OUT OF LIMITS. R & R SEAT TRACK IAW SRM.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 62,796 hrs · 61,886 cycles

CORROSION ON SEAT TRACK AT BS 616 RBL 46. CORROSION FOUND TO BE OUT OF LIMITS, R & R SEAT TRACK IAW SRM.

Part: BRACKET — CRACKED (ZONE 500) · airframe 62,796 hrs · 61,886 cycles

LEFT INBD MID FLAP - OTBD CARRIAGE ASSY PULLEY SUPPORT BRACKET CRACKED. R & R PULLEY SUPPORT BRACKET IAW WITH MM 27-51-21.

Part: SPAR — CORRODED (RT WING) · corrosion level 2 · airframe 62,796 hrs · 61,886 cycles

CORROSION AT LOWER RT WING L/E FWD SPAR AT WBL 227.0 TO WBL 522.0. REMOVED CORROSION, FABRICATED 2 REPAIR STRAPS AND INSTALLED IAW CURRENT SRM.

Part: SKIN — CORRODED (WING) · airframe 62,796 hrs · 61,886 cycles

CORROSION ON INTERNAL SKIN AND LONGERON BETWEEN WING STA 557.0 AND WBL 583.0. REMOVED CORROSION, ALODINE, AND PRIMED STRUCTURE IAW CURRENT SRM.

Part: SKIN — CORRODED (ZONE 500) · corrosion level 2 · airframe 62,796 hrs · 61,886 cycles

CORROSION ON LEFT WING INTERNAL SURFACE AND LONGERON BETWEEN WING STA 557.0 AND WBL 583.0. REMOVED CORROSION, ALODINE AND PRIMED IAW CURRENT SRM.

Part: SKIN — CORRODED (ZONE 600) · corrosion level 2 · airframe 62,796 hrs · 61,886 cycles

CORROSION ON INTERNAL SKIN AND LONGERON BETWEEN WING STA 557.0 AND WBL 583.0. REMOVED CORROSION, MATERIAL LOSS WITHIN LIMITS. ALODINED AND PRIMED STRUCTURE IAW CURRENT SRM.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 62,796 hrs · 61,886 cycles

CORROSION AT AFT FUSELAGE BULKHEAD AT BS 1016, STRINGER 17L. CUT OUT DAMAGED STRINGER 17L FROM 1016 TO 1026 TO ACCESS STRINGER TIE FITTING. FABRICATED REPAIR PART AND INSTALLED IAW SRM.

Part: SKIN — CRACKED (BS 360 S14R) · airframe 62,297 hrs · 60,891 cycles

DURING SERVICE CHECK FOUND A 2.5" CRACK ON THE RT SIDE FUSELAGE AT BS 360+4, BELOW STRINGER 14R. THE CRACK WAS REPAIRED IAW ENGINEERING CHANGE ORDER 3824, SB 737-53A1177 REV 6 & SRM 53-30-03, FIGURE 48.

Part: SKIN — CRACKED (BS 807) · airframe 62,270 hrs · 60,832 cycles

DURING SERVICE CHECK, FOUND A 4" FUSELAGE SKIN CRACK ON THE LT SIDE AFT OF THE T/E WING TO BODY FAIRING BS807+3 STRINGER 18L. THE CRACK WAS REPAIRED IAW SRM 53-30-3, FIGURE 48, DETAIL XI.

Part: FAIRING — DAMAGED (LT WING) · airframe 62,130 hrs · 60,549 cycles

AFT LT PYLON FAIRING ASSY-WING TO NACELLE STRUCTURE DAMAGED. REPLACED NR1 ENGINE TO WING AFT FAIRING IAW AMM 54-51-32. NO MAJOR REPAIR REQUIRED. THE ACFT WAS RETURNED TO SERVICE.

Part: LOCK — LACK OF LUBE (MLG) · airframe 61,418 hrs · 59,070 cycles

LANDING GEAR LEVER WILL NOT MOVE UP AFTER TAKEOFF. CLEANED AND LUBED LANDING GEAR LOCK MECHANISM. OPS CK OK IAW AMM 32-31-31. ACFT RETURNED TO SERVICE.

Part: CONNECTOR — DAMAGED (TE FLAP SYSTEM) · airframe 61,125 hrs · 58,459 cycles

NON-ETOPS CARGO FLIGHT 551. DURING LANDING, WHEN THE CREW LOWERED THE FLAPS, THERE WAS A FLAP ASYMMETRY INDICATION AT FLAPS 1. THE CREW FOLLOWED QRH PROCEDURES AND DECLARED AN EMERGENCY. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND PIN 50 ON CONNECTOR D4283J BENT CAUSING AN INTERMITTENT FALSE INDICATION. THE PIN WAS REPLACED IN ACCORDANCE WITH SOPM 20-11-02. FLAP OPERATIONAL CHECK SATISFACTORY PER BOEING AMM 27-58-01. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CLAMP — DISLODGED (CABIN PRESSURE) · airframe 61,000 hrs · 58,189 cycles

ON DESCENT, AT ABOUT FL 240, THE CREW EXPERIENCED THE ALTITUDE WARNING HORN SOUND. CREW CHECKED THE CABIN ALTITUDE, CANCELLED THE HORN, DONNED OXYGEN MASKS, AND ESTABLISHED COMMUNICATION. CREW DECLARED AN EMERGENCY AND CONTINUED AN EMERGENCY DECENT TO BELOW FL 140. CREW FOLLOWED UP WITH THE CABIN ALTITUDE WARNING AND THE EMERGENCY DESCENT CHECKLIST. CREW REMOVED MASKS BELOW FL 100 AND CANCELLED THE EMERGENCY. CREW PROCEEDED TO LAND WITHOUT FURTHER INCIDENT. FOUND FLEXIBLE PRESSURE SEAL CLAMP DISLODGED. MX RE-SECURED CLAMP. GROUND LEAK CHECK SATISFACTORY IAW MM 05-51-91. REPLACED PRESSURE CONTROLLER IAW MM 21-31-21. GROUND LEAK CHECK SATISFACTORY IAW MM 305-51-91. REPLACED NR1 ENGINE PRESSURE REGULATOR IAW MM 21-11-31. GROUND LEAK CHECK SATISFACTORY IAW MM 05-51-91.

Part: FIRE LOOP — FAILED (NR 1 NACELLE) · airframe 60,995 hrs · 58,179 cycles

NON-ETOPS CARGO FLT 14. CREW NOTED THE NR 1 ENGINE OVERHEAT LIGHT ILLUMINATED. CREW FOLLOWED QRH PROCEDURES AND SHUT DOWN THE NR 1 ENGINE. CREW LANDED WITHOUT FURTHER INCIDENT. REPLACED NR 1 ENGINE UPPER OVERHEAT LOOP IN ACCORDANCE WITH MM 26-11-11. OPS CHECK GOOD ON ENGINE RUN.

Part: ELEMENT — FALSE ACTIVATION (NR 1 NACELLE) · airframe 60,993 hrs · 58,176 cycles

CREW NOTED THE NR1 ENGINE OVERHEAT LIGHT ILLUMINATED. CREW FOLLOWED QRH PROCEDURES AND SHUTDOWN THE NR 1 ENGINE. CREW LANDED WITHOUT FURTHER INCIDENT. MX REPLACED THE NR1 ENGINE LOWER FIRE DETECTION SENSING ELEMENT IAW AMM 26-11-11, AND OPS CHECK WAS SATISFACTORY. THE ACFT WAS RETURNED TO SERVICE.

Part: SKIN — CRACKED (BS 308 S18R) · airframe 65,574 hrs · 65,398 cycles

LOWER FUSELAGE, SKIN CRACKED AT BS 308 BELOW STRINGER 18RT. THE CRACK REQUIRES A MAJOR REPAIR.

Part: INDICATOR — FAILED (NR 1 TANK) · airframe 60,711 hrs · 57,586 cycles

MX FERRY FLIGHT. AFTER TAKEOFF THE CREW NOTED THE LOSS OF FUEL INDICATION FOR THE NR 1 FUEL TANK. THE CREW RETURNED TO DEPARTURE. MX R & R THE NR 1 TANK FUEL QUANTITY INDICATOR IAW AMM 28-41-61.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,711 hrs · 57,586 cycles

LOWER EXTERNAL FUSELAGE AT BS 907 BETWEEN STRINGER 25RT AND STRINGER 26RT WITH SKIN BULGED.

Part: TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 60,711 hrs · 57,586 cycles

LOWER FUSELAGE FWD CARGO COMPARTMENT AT BS 440, LBL 24, WL 208 TRACK LOWER FLANGE WITH CORROSION.

Part: STRAP — CORRODED (LT MLG WW) · corrosion level 2 · airframe 60,711 hrs · 57,586 cycles

LEFT MAIN WHEEL WELL CEILING STRAP WITH CORROSION AT BS 703, LBL 50, WL 200.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 60,711 hrs · 57,586 cycles

UPPER FUSELAGE MAIN CARGO CABIN, CARGO TRACK AT BL 0, BETWEEN BS 460 AND BS 500B+8.5 WITH CORROSION.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,711 hrs · 57,586 cycles

LOWER FUSELAGE, AFT CARGO COMPARTMENT AT BS 865.5 STRINGER 27RT WITH CORROSION.

Part: FRAME — CRACKED (ZONE 200) · airframe 60,711 hrs · 57,586 cycles

UPPER FUSELAGE MAIN CARGO CABIN AT BS 986.5 BETWEEN STR 2L AND 3L, FUSELAGE FRAME WITH CRACK.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 60,711 hrs · 57,586 cycles

LOWER FUSELAGE E&E COMPARTMENT FROM BS 344 TO BS 360 STR 25LT WITH CORROSION.

Part: BEAM — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 60,711 hrs · 57,586 cycles

EMPENNAGE RT HORIZONTAL STABILIZER UPPER T/E BEAM WITH CORROSION AT ELEV STA 94.27, 213.32.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 60,711 hrs · 57,586 cycles

LOWER FUSELAGE AFT SECTION AT BS 977 STR 20LT WITH CORROSION.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,711 hrs · 57,586 cycles

LOWER FUSELAGE AFT CARGO COMPARTMENT AT BS 727A FROM STR 25L TO STR 27R FRAME WITH CORROSION.

Part: SKIN — GOUGED (ZONE 100) · airframe 60,711 hrs · 57,586 cycles

LOWER AFT FUSELAGE INTERNAL SECTION AT BS 1003 BETWEEN STRINGERS 20 AND 21 RT FUSELAGE SKIN WITH GOUGE.

Part: SKIN — BULGED (RT WING) · airframe 60,711 hrs · 57,586 cycles

RT WING TRAILING EDGE SECTION NR 6 FLAP TRACK FAIRING O/B LATERAL STEEL STRAP WITH BULGED SKIN AND WEAR.

Part: HINGE PIN — CORRODED (ZONE 300) · corrosion level 2 · airframe 60,711 hrs · 57,586 cycles

((EE4Y)) HORIZONTAL STABILIZER PIVOT HINGE IAW ECO 3472 PART II. (W/O Y10122, SUB JOB 2, ITEM 94).

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 60,711 hrs · 57,586 cycles

((EE4Y)) LOWER FUSELAGE CARGO COMPARTMENT AT BS 865.5, STR 27R WITH CORROSION. (W/O Y10122, SUB JOB 1, ITEM 229).

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 60,711 hrs · 57,586 cycles

((EE4Y)) LOWER FUSELAGE FWD CARGO COMPARTMENT BS 500A, BTWN LBL 25 AND RBL 25 FLOORBEAM UPPER CHORD WITH CORROSION. (W/O Y10122, SUB JOB 1, ITEM 208).

Part: BEAR STRAP — CRACKED (ZONE 100) · airframe 60,711 hrs · 57,586 cycles

((EE4Y)) LOWER FUSELAGE AFT CARGO COMPARTMENT BS 844 BETWEEN STRINGERS 23 & 24RH, BEAR STRAP DOUBLER WITH CRACK. (W/O Y10122, SUB JOB 1, ITEM 230).

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 60,711 hrs · 57,586 cycles

((EE4Y)) UPPER FUSELAGE PAX CABIN FLOORBEAM UPPER SKIN WITH CORROSION BETWEEN STA 480-520, LBL 45-65. (W/O Y10122, SUB JOB 2, ITEM 144).

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 60,711 hrs · 57,586 cycles

((EE4Y)) LOWER FUSELAGE AFT CARGO COMPARTMENT BS 727B BETWEEN RBL 25 AND LBL 25 FLOORBEAM UPPER CHORD UPPER SURFACE WITH CORROSION. (W/O Y10122, SUB JOB 1, ITEM 212).

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 60,711 hrs · 57,586 cycles

((EE4Y)) LOWER FUSELAGE FWD CARGO COMPARTMENT AT BS 500A, RBL 25, WL 207 FLOORBEAM UPPER FLANGE LOWER FACE WITH CORROSION. (W/O Y10122, SUB JOB 1, ITEM 1736).

Part: STRINGER — CORRODED (BS 892 S26R) · corrosion level 2 · airframe 60,711 hrs · 57,586 cycles

((EE4Y)) LOWER FUSELAGE AFT CARGO COMPARTMENT BS 892, STRINGER 26RT WITH CORROSION. (W/O Y10122, SUB JOB 1, ITEM 210).

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 60,711 hrs · 57,586 cycles

((EE4Y)) UPPER FUSELAGE PAX CABIN FLOORBEAM WITH CORROSION AT STA 500A BETWEEN LBL 25 & LBL 40. (W/O Y10122, SUB JOB 2, ITEM 145).

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 60,711 hrs · 57,586 cycles

((EE4Y)) LOWER FUSELAGE FWD CARGO COMPARTMENT AT BS 500B, LBL 39, WL 200 FLOORBEAM LOWER FLANGE WITH CORROSION. (W/O Y10122, SUB JOB 1, ITEM 170).

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 60,711 hrs · 57,586 cycles

((EE4Y)) LOWER FUSELAGE E & E COMPARTMENT FROM BS 352 TO BS 360, STR 22 LT WITH CORROSION. (W/O Y10122, SUB JOB 1, ITEM 177).

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 60,711 hrs · 57,586 cycles

((EE4Y)) UPPER FUSELAGE MAIN CABIN FLOORBEAM UPPER CHORD AT B STA 947.6 BETWEEN BL 0 TO LBL 45 WITH CORROSION AT SEVERAL PLACES. (W/O Y10122, SUB JOB 2, ITEM 142).

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 60,711 hrs · 57,586 cycles

((EE4Y)) LOWER FUSELAGE MAIN CARGO COMPARTMENT FLOORBEAM WITH CORROSION AT LOWER FLANGE AT BS 460 WL 200 AT LBL 42. W/O Y10122, SUB JOB 1, ITEM 204).

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 60,711 hrs · 57,586 cycles

((EE4Y)) LOWER FUSELAGE FWD CARGO COMPARTMENT AT BS 500, LBL 22, WL 200 FLOORBEAM LOWER FLANGE WITH CORROSION. (W/O Y10122, SUB JOB 1, ITEM 169).

Part: WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 60,711 hrs · 57,586 cycles

((EE4Y)) UPPER FUSELAGE PAX CABIN FLOOR WEB WITH CORROSION BETWEEN STA 420 & 440, LBL 40 TO LBL 65. (W/O Y10122, SUB JOB 2, ITEM 154).

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 60,711 hrs · 57,586 cycles

((EE4Y)) LOWER FUSELAGE FWD CARGO COMPARTMENT BS 500B AT LBL 55 FLOORBEAM UPPER CHORD LOWER SURFACE WITH CORROSION. (W/O Y10122, SUB JOB 1, ITEM 214).

Part: SUPPORT — CRACKED (ZONE 100) · airframe 60,711 hrs · 57,586 cycles

((EE4Y)) LOWER FUSELAGE AFT CARGO COMPARTMENT AT BS 794 BETWEEN STR 22R AND STR 23R SUPPORT WITH CRACK. (W/O Y10122, SUB JOB 1, ITEM 227).

Part: INTERCOSTAL — CRACKED (ZONE 100) · airframe 60,711 hrs · 57,586 cycles

((EE4Y)) LOWER FUSELAGE AFT CARGO COMPARTMENT AT BS 817 BETWEEN STR 24R AND 25R INTERCOSTAL WITH CRACK. (W/O Y10122, SUB JOB 1, ITEM 228).

Part: STIFFENER — CRACKED (ZONE 100) · airframe 60,711 hrs · 57,586 cycles

((EE4Y)) LOWER FUSELAGE FWD CARGO COMPARTMENT AT BS 500B BL STIFFENER WITH CRACK. (W/O Y10122, SUB JOB 1, ITEM 216).

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 60,711 hrs · 57,586 cycles

((EE4Y)) LOWER FUSELAGE AFT CARGO COMPARTMENT AT BS 860, RBL 3 CARGO FLOORBEAM WITH CORROSION. ( W/O Y10122, SUB JOB 1, ITEM 220).

Part: VERTICAL BEAM — CRACKED (ZONE 100) · airframe 60,711 hrs · 57,586 cycles

((EE4Y)) LOWER FUSELAGE AFT CARGO COMPARTMENT BS 727+4 LBL 17, WL 156 BULKHEAD VERTICAL BEAM FLANGE WITH CORROSION. (W/O Y10122, SUB JOB 1, ITEM 207).

Part: PAN — CRACKED (ZONE 200) · airframe 60,711 hrs · 57,586 cycles

((EE4Y)) PAX CABIN MAIN CARGO DOOR LOWER PAN AT STA 475 AND STA 405 WITH CRACK. (W/O Y10122, SUB JOB 2, ITEM 135).

Part: STRINGER — CRACKED (ZONE 200) · airframe 60,711 hrs · 57,586 cycles

((EE4Y)) MAIN CARGO CABIN AT BS 500B+3 AND BS 500B+13,5 AT SCANNING LIGHT AREA STRINGER 16 RT WITH CRACK. (W/O Y10122, SUB JOB 2, ITEM 134).

Part: SKIN — CRACKED (CARGO DOOR) · airframe 60,711 hrs · 57,586 cycles

((EE4Y)) UPPER FUSELAGE MAIN CARGO DOOR, AT BS 460 LOWER FRAME SKIN WITH CRACK. (W/O Y10122, SUB JOB 2, ITEM 116).

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 60,711 hrs · 57,586 cycles

((EE4Y)) LOWER FUSELAGE AFT CARGO COMPARTMENT FLOORBEAM AT BS 847 FROM RBL 30 TO RBL 55 FLOORBEAM LOWER CHORD WITH CORROSION. (W/O Y10122, SUB JOB 1, ITEM 94).

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 60,711 hrs · 57,586 cycles

((EE4Y)) LOWER FUSELAGE AFT CARGO COMPARTMENT AT BSTA 867 FROM RBL 60 TO LBL 60 FLOORBEAM LOWER CHORD WITH CORROSION. (W/O Y10122, SUB JOB 1, ITEM 112).

Part: CARGO TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 60,711 hrs · 57,586 cycles

((EE4Y)) LOWER FUSELAGE AFT CARGO COMPARTMENT FROM BSTA 716 TO 727B CARGO TRACK WITH CORROSION. (W/O Y10122, SUB JOB 1, ITEM 77).

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 60,711 hrs · 57,586 cycles

((EE4Y)) LOWER FUSELAGE AFT CARGO COMPARTMENT AT BSTA 1006, STR 20L, FRAME WITH CORROSION. (W/O Y10122, SUB JOB 1, ITEM 136).

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 60,711 hrs · 57,586 cycles

((EE4Y)) LOWER FUSELAGE FWD CARGO COMPARTMENT FROM BS 460 TO BS 520, BL 0, WL 200 FLOOR SUPPORT UPPER AND LOWER FLANGE WITH CORROSION. (W/O Y10122, SUB JOB 1, ITEM 174).

Part: INTERCOSTAL — CRACKED (ZONE 200) · airframe 60,711 hrs · 57,586 cycles

((EE4Y)) UPPER FUSELAGE CARGO CABIN BS 294.5 INTERCOSTAL CARCKED AT STRINGER 12 LT. (WO Y10122, SUB JOB 2, ITEM 97).

Part: INTERCOSTAL — CRACKED (ZONE 200) · airframe 60,711 hrs · 57,586 cycles

((EE4Y)) UPPER FUSELAGE CARGO CABIN BS 294.5 INTERCOSTAL CRACKED AT STRINGER 11 LT. (WO Y10122, SUB JOS 2, ITEM 97).

Part: HINGE PIN — CORRODED (ZONE 300) · corrosion level 2 · airframe 60,711 hrs · 57,586 cycles

DURING THE ACCOMPLISHMENT OF ECO 3472R4, RELATED TO AD 2004-19-10 (SB737-55A1077) WAS FOUND THE HORIZONTAL STABILIZER PIVOT HINGE INNER PIN WITH CORROSION ON ITS SHANK. ( WO Y10122, SUB JOB 9, ITEM 24).

Part: INTERCOSTAL — CRACKED (ZONE 200) · airframe 60,711 hrs · 57,586 cycles

((EE4Y)) UPPER FUSELAGE CARGO CABIN BS 294.5 STR, 8 LT INTERCOSTAL WITH CRACK. (WO Y10122, SUB JOB 2, ITEM 96).

Part: ANGLE — CORRODED (ZONE 500) · corrosion level 2 · airframe 60,711 hrs · 57,586 cycles

((EE4Y)) LT WING NR 2 SLAT OTBD MAIN TRACK AREA LOWER ANGLE WITH CORROSION. (W/O Y10122, SUB JOB 5, ITEM 18).

Part: SPAR — CORRODED (LWS 460) · corrosion level 2 · airframe 60,711 hrs · 57,586 cycles

((EE4Y)) LT WING FRONT SPAR LOWER CHORD FLANGE WITH CORROSION AT W STA 460. (WO Y10122, SUB JOB 5, ITEM 1).

Part: SPAR — CORRODED (ZONE 500) · corrosion level 2 · airframe 60,711 hrs · 57,586 cycles

((EE4Y)) LT WING FRONT SPAR LOWER CHORD FLANGE WITH CORROSION AT W STA 602. (W/O Y10122, SUB JOB 5, ITEM 3).

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 60,711 hrs · 57,586 cycles

((EE4Y)) LOWER FUSELAGE FWD CARGO COMPARTMENT AT BS 500A, BL 50R, WL 200 FLOORBEAM LOWER FLANGE WITH CORROSION. (W/O Y10122, SUB JOB 1, ITEM 68).

Part: STRAP — CORRODED (ZONE 200) · corrosion level 2 · airframe 60,711 hrs · 57,586 cycles

((EE4Y)) UPPER FUSELAGE PAX CABIN FROM BSTA 340 TO BSTA 310 BL 45L FLOOR STRAP WITH CORROSION. (W/O Y10122, SUB JOB 2, ITEM 105).

Part: STRINGER CLIP — CRACKED (ZONE 200) · airframe 60,711 hrs · 57,586 cycles

((EE4Y)) UPPER FUSELAGE MAIN CARGO CABIN AT B/S 616 STR 3L STRINGER TIE CLIP WITH CRACK. (W/O Y10122, SUB JOB 2, ITEM 66).

Part: SPAR — CORRODED (ZONE 500) · corrosion level 2 · airframe 60,711 hrs · 57,586 cycles

((EE4Y)) LT WING FRONT SPAR LOWER CHORD FLANGE WITH CORROSION AT W STA 520. (W/O Y10122, SUB JOB 5, ITEM 1).

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 60,711 hrs · 57,586 cycles

((EE4Y)) LOWER FUSELAGE AFT CRAGO COMPARTMENT AT BSTA 787 FROM BL 0 TO BL 60L FLOORBEAM LOWER CHORD WITH CORROSION. (W/O Y10122, SUB JOB 1, ITEM 82).

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 60,711 hrs · 57,586 cycles

((EE4Y)) UPPER FUSELAGE MAIN CARGO CABIN AT B/S 1016 FLOORBEAM UPPER FLANGE WITH CORROSION FROM BL 45R TO BL 45L. (W/O Y10122, SUB JOB 2, ITEM 98).

Part: SKIN — DENTED (ZONE 200) · airframe 60,711 hrs · 57,586 cycles

((EE4Y) UPPER EXTERNAL FUSELAGE AT B/S 959.5 BETWEEN STRINGER 4R AND 5R SKIN WITH DENT. (W/O Y10122, SUB JOB 2, ITEM 59).

Part: SKIN — BULGED (ZONE 100) · airframe 60,711 hrs · 57,586 cycles

((EE4Y)) LOWER EXTERNAL FUSELAGE AT STRINGER 26L B/S 874.5 WITH BULDGED SKIN. (WORK ORDER Y10122, SUB JOB 1, ITEM 5).

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 60,711 hrs · 57,586 cycles

((EE4Y)) LOWER FUSELAGE AFT CARGO COMPARTMENT AT BSTA 877 STR 26L WITH CORROSION. (W/O Y10122, SUB JOB 1, ITEM 117).

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 60,711 hrs · 57,586 cycles

((EE4Y)) LOWER FUSELAGE AFT CARGO COMPARTMENT AT BSTA 887 BL 30L TO BL 60L FLOOR BEAM UPPER CHORD WITH CORROSION. (W/O Y10122, SUB JOB 1, ITEM 125).

Part: STRINGER CLIP — CRACKED (ZONE 200) · airframe 60,711 hrs · 57,586 cycles

((EE4Y)) UPPER FUSELAGE MAIN CARGO CABIN AT B/S 767 STR 5R, STRINGER TIE CLIP WITH CRACK. W/O Y10122, SUB JOB 2, ITEM 72.

Part: STRINGER CLIP — CRACKED (ZONE 200) · airframe 60,711 hrs · 57,586 cycles

((EE4Y)) UPPER FUSELAGE MAIN CARGO CABIN AT B/S 787 STR 5R, STRINGER TIE CLIP WITH CRACK. W/O Y10122, SUB JOB 2, ITEM 73.

Part: STRINGER CLIP — CRACKED (ZONE 100) · airframe 60,711 hrs · 57,586 cycles

((EE4Y) LOWER FUSELAGE AFT CARGO COMPARTMENT BSTA 727A STR 25L WITH CLIP CRACKED. (W/O Y10122, SUB JOB 1, ITEM 71).

Part: STRINGER CLIP — CRACKED (ZONE 200) · airframe 60,711 hrs · 57,586 cycles

((EE4Y)) UPPER FUSELAGE MAIN CARGO CABIN AT B/S 747 STR 5L, STRINGER TIE CLIP WITH CRACK. WORK ORDER Y10122, SUB JOB 2, ITEM 71.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 60,711 hrs · 57,586 cycles

UPPER FUSELAGE MAIN CARGO CABIN AT B/S 986.5 FLOORBEAM UPPER CHORD WITH CORROSION BETWEEN LBL 16 AND RBL 45. (W/O Y10122, SUB JOB 2, ITEM 100).

Part: STRINGER CLIP — CRACKED (ZONE 200) · airframe 60,711 hrs · 57,586 cycles

((EE4Y)) UPPER FUSELAGE MAIN CARGO CABIN AT B/S 727B STR 7R, STRINGER TIE CLIP WITH CRACK. WORK ORDER Y10122, SUB JOB 2, ITEM 70.

Part: STRINGER CLIP — CRACKED (ZONE 200) · airframe 60,711 hrs · 57,586 cycles

((EE4Y)) UPPER FUSELAGE MAIN CARGO CABIN AT B/S 787 STR 6R, STRINGER TIE CLIP WITH CRACKED. W/O Y10122, SUB JOB 2, ITEM 73.

Part: SKIN — CRACKED (ZONE 600) · airframe 60,711 hrs · 57,586 cycles

((EE4Y)) RT WING FRONT SPAR SECTION, LEADING EDGE SKIN WITH CRACK AT WBL STA 280.76. ( W/O Y10122, SUB JOB 6, ITEM 16).

Part: STRINGER CLIP — CRACKED (ZONE 200) · airframe 60,711 hrs · 57,586 cycles

((EE4Y)) UPPER FUSELAGE MAIN CARGO CABIN AT B/S 747 STR 8L, STRINGER TIE CLIP WITH CRACK. W/O Y10122, SUB JOB 2, ITEM 71.

Part: STRINGER CLIP — CRACKED (ZONE 200) · airframe 60,711 hrs · 57,586 cycles

((EE4Y) UPPER FUSELAGE MAIN CARGO CABIN AT B/S 727B STR 5R, STRINGER TIE CLIP WITH CRACK. W/O Y10122, SUB JOB 2, ITEM 70.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 60,711 hrs · 57,586 cycles

((EE4Y)) UPPER FUSELAGE PAX AT BSTA 328 BL 30L FLOOR ANGLE WITH CRACK. (W/O Y10122, SUB JOB 2, ITEM 107).

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 60,711 hrs · 57,586 cycles

UPPER FUSELAGE PAX CABIN AT BSTA 294 FLOORBEAM UPPER FLANGE WITH CORROSION BETWEEN BL 12R TO BL 55R. ( W/O Y10122, SUB JOB 2, ITEM 111).

Part: STRINGER CLIP — CRACKED (ZONE 200) · airframe 60,711 hrs · 57,586 cycles

((EE4Y)) UPPER FUSELAGE MAIN CARGO CABIN AT B/S 767 STR 6L, STRINGER TIE CLIP WITH CRACK. W/O Y10122, SUB JOB 2, ITEM 72.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 60,711 hrs · 57,586 cycles

((EE4Y)) UPPER FUSELAGE PAX CABIN AT BSTA 328 BL 35R FLOOR ANGLE WITH CRACK. (W/O Y10122, SUB JOB 2, ITEM 112).

Part: SKIN — CRACKED (ZONE 500) · airframe 60,711 hrs · 57,586 cycles

LT WING L/E SKIN WITH CRACK AT WBL 384. (W/O Y10122, SUB JOB 5, ITEM 9).

Part: SUPPORT — CRACKED (ZONE 100) · airframe 60,711 hrs · 57,586 cycles

((EE4Y)) LOWER FUSELAGE AFT CARGO DOOR CUT-OUT AT BSTA 793 FROM STR 22R TO 25R STOP FITTING INNER SUPPORT CRACKED. (WORK ORDER Y10122, SUB JOB 1, ITEM 84).

Part: STRINGER CLIP — CRACKED (ZONE 200) · airframe 60,711 hrs · 57,586 cycles

((EE4Y)) UPPER FUSELAGE MAIN CARGO CABIN AT B/S 747 STR 5R, STRINGER TIE CLIP WITH CRACK. W/O Y10122, SUB JOB 2, ITEM 71.

Part: CHANNEL — CRACKED (BS 874) · airframe 60,711 hrs · 57,586 cycles

((EE4Y)) LOWER FUSELAGE AFT CARGO COMPARTMENT AT BSTA 847 STR 19R CHANNEL CRACKED. (W/O Y10122, SUB JOB 1, ITEM 135).

Part: SKIN — CRACKED (ZONE 100) · airframe 60,711 hrs · 57,586 cycles

((EE4Y)) LOWER FUSELAGE FWD CARGO COMPARTMENT DOOR INNER SKIN AT BS 440 BETWEEN BEAM 2,3 WITH CRACK. (W/O Y10122, SUB JOB 1, ITEM 67).

Part: STRINGER CLIP — CRACKED (ZONE 200) · airframe 60,711 hrs · 57,586 cycles

((EE4Y)) UPPER FUSELAGE MAIN CARGO CABIN AT B/S 787 STR 3R, STRINGER TIE CLIP WITH CRACK. W/O Y10122, SUB JOB 2, ITEM 73.

Part: CROSSBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 60,711 hrs · 57,586 cycles

((EE4Y)) UPPER FUSELAGE MAIN CARGO CABIN AT BL 0 BETWEEN B/ 986.5 AND B/S 1006, CROSS BEAM UPPER CHORD WITH CORROSION. (W/O Y10122, SUB JOB 2, ITEM 102).

Part: SKIN — CRACKED (CARGO DOOR) · airframe 60,711 hrs · 57,586 cycles

((EE4Y)) LOWER FUSELAGE AFT CARGO COMPARTMENT DOOR INNER SKIN CRACKED. (W/O Y 10122, SUB JOB 1, ITEM 95).

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 60,711 hrs · 57,586 cycles

((EE4Y)) UPPER FUSELAGE PAX CABIN AT BSTA 328 BETWEEN BL 12R TO BL 55R, FLOOR BEAM UPPER FLANGE WITH CORROSION. (W/O Y10122, SUB JOB 2, ITEM 109).

Part: SKIN — CRACKED (ZONE 600) · airframe 60,711 hrs · 57,586 cycles

((EE4Y)) RT WING FRONT SPAR SECTION LEADING EDGE SKIN WITH CRACK AT WBL 405. (WORK ORDER Y10122, SUB JOB 6, ITEM 12).

Part: SKIN — CRACKED (ZONE 200) · airframe 60,711 hrs · 57,586 cycles

((EE4Y)) EXTERNAL UPPER FUSELAGE AT B/S 533 STR 16R FUSELAGE SKIN WITH CRACK. (W/O Y10122, SUB JOB 2, ITEM 115).

Part: STRINGER CLIP — CRACKED (ZONE 200) · airframe 60,711 hrs · 57,586 cycles

((EE4Y)) UPPER FUSELAGE MAIN CARGO CABIN AT B/S 727A STR 7R STRINGER TIE CLIP WITH CRACK. WO Y10122, SUB JOB 2, ITEM 69.

Part: STRINGER CLIP — CRACKED (BS 440 S3R) · airframe 60,711 hrs · 57,586 cycles

((EE4Y)) UPPER FUSELAGE MAIN CARGO CABIN AT B/S 440 STR 3, STRINGER TIE CLIPS WITH CRACKS.

Part: STRINGER CLIP — CRACKED (ZONE 200) · airframe 60,711 hrs · 57,586 cycles

((EE4Y)) UPPER FUSELAGE MAIN CARGO CABIN B/S 440 STR 10R, STRINGER TIE CLIP WITH CRACK.

Part: STRINGER CLIP — CRACKED (ZONE 200) · airframe 60,711 hrs · 57,586 cycles

((EE4Y)) UPPER FUSELAGE MAIN CARGO CABIN AT B/S 685 STR 4R STRINGER TIE CLIP WITH CRACK. WORK ORDER Y10122, SUB JOB 2, ITEM 67.

Part: STRINGER CLIP — CRACKED (ZONE 200) · airframe 60,711 hrs · 57,586 cycles

((EE4Y)) UPPER FUSELAGE MAIN CARGO CABIN AT B/S 616 STR 3R STRINGER TIE CLIP WITH CRACK. W/O Y10122, SUB JOB 2, ITEM 66.

Part: ATTACH FITTING — CORRODED (BS 867 FRAME) · corrosion level 3 · airframe 60,711 hrs · 57,586 cycles

((EE4Y)) LOWER FUSELAGE AFT CARGO COMPARTMENT AT BSTA 867 LSTR 20 CLIP WITH CORROSION.

Part: STRINGER CLIP — CRACKED (ZONE 200) · airframe 60,711 hrs · 57,586 cycles

((EE4Y)) UPPER FUSELAGE MAIN CARGO CABIN AT B/S 440 STR 4R, STRINGER TIE CLIP WITH CRACK.

Part: ATTACH FITTING — CORRODED (BS 867 FRAME) · corrosion level 2 · airframe 60,711 hrs · 57,586 cycles

((EE4Y)) LOWER FUSELAGE AFT CARGO COMPARTMENT AT BS 867, S26L CLIP WITH CORROSION.

Part: STRINGER CLIP — CRACKED (ZONE 200) · airframe 60,711 hrs · 57,586 cycles

((EE4Y)) UPPER FUSALAGE MAIN CARGO CABIN AT B/S 420 STR 5R, STRINGER TIE CLIPS WITH CRACK.

Part: STRINGER CLIP — CRACKED (BS 400 S10R) · airframe 60,711 hrs · 57,586 cycles

((EE4Y)) UPPER FUSELAGE MAIN CARGO CABIN AL B/S 400 STR 10R, STRINGER TIE CLIP WITH CRACK.

Part: STRINGER CLIP — CRACKED (BS 400 S4R) · airframe 60,711 hrs · 57,586 cycles

((EE4Y)) UPPER FUSELAGE MAIN CARGO CABIN AT B/S 400 STR 4R AND STR 10R STRINGER TIE CLIPS WITH CRACK.

Part: ATTACH FITTING — CRACKED (BS 727A FRAME) · airframe 60,711 hrs · 57,586 cycles

((EE4Y)) LOWER FUSELAGE AFT CARGO COMPARTMENT AT BS 727A, S25L WITH CRACK.

Part: STRINGER CLIP — CRACKED (BS 420) · airframe 60,711 hrs · 57,586 cycles

((EE4Y)) UPPER FUSELAGE MAIN CARGO CABIN AT B/S 420 STR 10, STRINGER TIE CLIP WITH CRACK.

Part: STRINGER CLIP — CRACKED (ZONE 200) · airframe 60,711 hrs · 57,586 cycles

((EE4Y)) UPPER FUSELAGE MAIN CARGO CABIN AT B/S 706 STR 10L STRINGER TIE CLIP CRACK. WORK ORDER Y10122, SUB JOB 2, ITEM 68.

Part: STRINGER CLIP — CRACKED (ZONE 200) · airframe 60,711 hrs · 57,586 cycles

((EE4Y)) UPPER FUSELAGE MAIN CARGO CABIN AT B/S 460 STR 4R STRINGER TIE CLIP WITH CRACK. WORK ORDER Y10122, SUBJOB 2, ITEM 65.

Part: STRINGER — CRACKED (ZONE 300) · airframe 60,711 hrs · 57,586 cycles

EMPENNAGE TAIL COMPARTMENT FWD CORNER OF THE HORIZ STABILIZER CUTOUT AT THE UPPER HORIZ BEAM STRINGER S-5A RT CRACKED FROM BS 1138 TO BS 1142.

Part: INTERCOSTAL — CRACKED (ZONE 200) · airframe 60,711 hrs · 57,586 cycles

((EE4Y)) UPPER FUSELAGE CARGO CABIN B/S 360 STR 14 LT INTERCOSTAL WEB CRACKED.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 60,711 hrs · 57,586 cycles

LWR FUSELAGE AFT CARGO COMPARTMENT AT B STA 767, STR 20L WITH CORROSION.

Part: SKIN — DELAMINATED (ZONE 100) · airframe 60,711 hrs · 57,586 cycles

((EE4Y)) LOWER FUSELAGE LT AIR CONDITIONING BAY DOOR INNER SKIN DELAMINATED AT STA 138.

Part: SKIN — CANNING (ZONE 100) · airframe 60,711 hrs · 57,586 cycles

((EE4Y)) LOWER EXTERNAL FUSELAGE AT B/S 360.5 BETWEEN STRINGERS 22R AND 23R SKIN WITH OIL CAN.

Part: SUPPORT ANGLE — CRACKED (ZONE 100) · airframe 60,711 hrs · 57,586 cycles

((EE4Y)) LOWER FUSELAGE AT B/S 535.5 WL 144 LBL 45, WING TO BODY SUPPORT ANGLE WITH CRACK.

Part: DUCT — CRACKED (ZONE 100) · airframe 60,711 hrs · 57,586 cycles

LOWER FUSELAGE LT AIR CONDITIONING BAY, PRIMARY HEAT EXCHANGER EXHAUST DUCT CRACKED.

Part: INTERCOSTAL — CRACKED (ZONE 200) · airframe 60,711 hrs · 57,586 cycles

((EE4Y)) UPPER FUSELAGE CARGO CABIN B/S 294.5 STRINGER 8 LT INTERCOSTAL ANGLE CRACKED.

Part: INTERCOSTAL — CRACKED (ZONE 200) · airframe 60,711 hrs · 57,586 cycles

((EE4Y)) UPPER FUSELAGE CARGO CABIN B/S 294.5 INTERCOSTALS CRACKED (2EA) AT STRINGER 11 AND 12 LT.

Part: CONNECTOR — BROKEN (POWER SUPPLY) · airframe 60,711 hrs · 57,586 cycles

LOWER FUSELAGE FWD CARGO COMPARTMENT BATTERY POWER SUPPLY GROUND CONNECTION BROKEN.

Part: SKIN — CRACKED (BS 306 S18R) · airframe 60,711 hrs · 57,586 cycles

LOWER EXTERNAL FUSELAGE AT BS 306 STRINGER 18R SKIN WITH CRACK.

Part: LINE — OBSTRUCTED (PITOT/STATIC SYS) · airframe 60,593 hrs · 57,357 cycles

NON-ETOPS CARGO FLIGHT 28 HNL-OGG. ON TAKEOFF ROLL, CREW NOTED THE CAPTAIN’S AIRSPEED INDICATOR WAS INOP. CREW ABORTED TAKEOFF AT 80 KNOTS AND RETURNED TO THE CARGO RAMP WITHOUT FURTHER INCIDENT. MAINTENANCE FLUSHED OUT CAPT PITOT STATIC LINE AND REMOVED DEBRIS FROM CAPT PITOT TUBE. OPERATION AND LEAK CHECK SATISFACTORY PER AMM 34-12-0. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — CRACKED (BS 540) · airframe 60,433 hrs · 57,031 cycles

DURING SCHEDULED 2B CK INSP A 3 CIRCUMFERENTIAL CRACK AT BS 540 BETWEEN S-0 AND S-1L WAS DISCOVERED. CONFIRMED WITH EDDY CURRENT INSP. MX ACTION CUTOUT DAMAGE CRACK, USE A .50" RADIUS CUT AT CORNERS, MAINTAINED 2DMINIMUM EDGE DISTANCE, LAY-OUT DOUBLER AND TRIPLER, LAY-OUT 3 AND 4 FASTENER ROWS BEYOND ALL SIDES OF CUTOUT, INSPECTED ALL FASTENER HOLES BY HFEC METHOD NO DEFECTS NOTED AND INSTALLED REPAIR DOUBLER AND TRIPLER ASSY IAW SRM 53-30-3 FIG. 48 DETAIL XXII.

Part: DOOR FRAME — CRACKED (BS 492.4) · airframe 60,128 hrs · 56,388 cycles

DURING SCHEDULED INSP A 2 INCH CRACK WAS DISCOVERED AT BS 492.4, S-24R FWD CARGO DOOR AFT FRAME LWR DOOR STOP WEB IAW (AD 2005-07-19) INSP AFT AND FWD CARGO DOOR STRUCTURE CUT-OUTS. R & R FWD CARGO DOOR AFT FRAME ASSY. IAW ECO 3512 R3. ACFT RETURNED TO SERVICE.

Part: PROBE — OBSTRUCTED (NR 2 PT2) · airframe 59,923 hrs · 55,949 cycles

ON TAKEOFF ROLL, HAD HIGH EPR FOR 2 ENG. ALL OTHER INDICATIONS MATCHED NR 1 ENGINE. ABORTED TAKEOFF "UNEVENTFUL" AND RETURNED TO RAMP. MX FOUND BUG IN THE NR 2 ENG PT2 PROBE. CLEARED PROBE; OPS CHECK OK. ACFT RETURNED TO SERVICE.

Part: SMOKE DETECTOR — DEFECTIVE (AFT CARGO PIT)

WHILE PARKED ON RAMP POST ARRIVAL WITH GROUND POWER ENGAGED AND ENGINE SHUTDOWN, THE AFT CARGO SMOKE WARNING LIGHT ON THE FIRE DETECTION/PROTECTION CENTER CONSOLE PANEL, MASTER FILE WARNING AND BELL ILLUMINATED / SOUNDED. REPLACED AFT CARGO SMOKE DETECTOR IAW AMM 26-16-11. OPS CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,922 hrs · 53,777 cycles

APPROX 3 INCH CRACK DISCOVERED AT BS 533 TO BS 536 STR 16R. REPAIRED IAW SRM 53-30-3 FIG 48 DETAIL IX.

Part: ROD END — DISCONNECTED (SQUAT SWITCH) · airframe 58,890 hrs · 53,707 cycles

FLT 912, LIH-HNL: LANDING GEAR LEVER WOULD NOT GO TO THE UP POSITION AFTER TAKEOFF. ALL SIX GEAR INDICATOR LIGHTS WERE ILLUMINATED. DECLARED EMERGENCY, CONTINUED TO HNL AND LANDED WITHOUT INCIDENT. MAINTENANCE: RECONNECTED THE SQUAT SWITCH CABLE ROD END. OPS CHECK, GEAR SWING, AND EMERGENCY GEAR SWING OK. RIG CHECK OKAY REF 27-62-51. AIRCRAFT RETURNED TO SERVICE.

Part: WARNING LIGHT — FALSE ACTIVATION (OVERHEAT) · airframe 58,778 hrs · 53,507 cycles

FLT 320, HNL-OAK: LT WING-BODY OVERHEAT LIGHT ILLUMINATED IN FLIGHT DURING CRUISE AT ABOUT FL350. LIGHT WENT OUT AFTER. ACCOMPLISHED QRH PROCEDURES AND RETURNED TO HNL. INSPECTED AIR CONDITIONING BAY DUCTS, LEADING FLAP DUCTS AND OVERWING DUCTS. NO LEAKS DETECTED. ALSO PERFORMED HIGH POWER RUN; SYSTEM CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (A)

Part: ACTUATOR — INOPERATIVE (LT MLG LOCK) · airframe 5,864,136 hrs · 53,202 cycles

FLIGHT 916 LIH-HNL. ON APPROACH CREW SELECTED GEAR DOWN AND NOTED INDICATION FOR LEFT MAIN GEAR NOT LOCKED. CREW PULLED MANUAL RELEASE HANDLE AND GOT ALL 3 GEARS DOWN AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED LEFT MAIN GEAR LOCK ACTUATOR IAW AMM 32-32-51 PG 401-403. THE AIRCRAFT WAS RETURNED TO SERVICE. (A)

Part: ACTUATOR — INOPERATIVE (LT MLG LOCK) · airframe 5,864,136 hrs · 53,202 cycles

FLIGHT 916 LIH-HNL. ON APPROACH CREW SELECTED GEAR DOWN AND NOTED INDICATION FOR LEFT MAIN GEAR NOT LOCKED. CREW PULLED MANUAL RELEASE HANDLE AND GOT ALL 3 GEARS DOWN AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED LEFT MAIN GEAR LOCK ACTUATOR IAW AMM 32-32-51 PG 401-403. THE AIRCRAFT WAS RETURNED TO SERVICE. (A)

Part: SEAL — OUT OF ADJUST (CARGO DOOR) · airframe 58,262 hrs · 52,316 cycles

CARGO FLIGHT 940 HNL-KOA - DURING CLIMB, THE CREW NOTED A LOUD AIR NOISE COMING FROM THE MAIN CARGO DOOR INDICATING AN INCOMPLETE SEAL ON THE DOOR. THE CREW RETURNED TO HNL WITHOUT FURTHER INCIDENT. MAINTENANCE ADJUSTED THE MAIN CARGO DOOR PRESSURE SEAL AND PRESSURE CHECKED THE AIRCRAFT PER AMM 21-00-05. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (E/E BAY DOOR) · airframe 57,727 hrs · 50,991 cycles

NON-ETOPS CARGO FLIGHT 909 HNL-LIH - DURING CLIMB, THE CREW NOTED THAT THE PRESSURE CONTROL PANEL SHOWED AUTO FAIL AND THE AIRCRAFT WAS NOT PRESSURIZING. THE CREW ATTEMPTED TO SWITCH TO STANDBY CONTROL AND WERE STILL UNABLE TO PRESSURIZE THE CABIN. THE CREW RETURNED TO HNL WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE ELECTRONIC EQUIPMENT BAY DOOR UNLATCHED AND OPEN. MAINTENANCE ALSO FOUND A DAMAGED WIRE ON THE DOOR OPEN SWITCH INDICATOR CIRCUIT. THIS PREVENTED DOOR OPEN ANNUNCIATION ON THE FLIGHT DECK. THE AIRCRAFT WAS PRESSURE CHECKED WITH THE DOOR CLOSED AND RETURNED TO SERVICE UNDER MEL 52-3 FOR THE INOPERATIVE DOOR INDICATION. MAINTENANCE LATER REPAIRED THE BROKEN SWITCH WIRE AND FUNCTION CHECKED THE INDICATION PER MM 52-71-31 AND REMOVED MEL 52-3. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SENSOR — OUT OF ADJUST (LT MLG) · airframe 57,698 hrs · 50,911 cycles

NON-ETOPS FLIGHT 913 HNL-LIH, ON APPROACH TO LIH, THE CREW PLACED THE LANDING GEAR HANDLE TO THE DOWN POSITION AND NOTED THAT THE LEFT MAIN LANDING GEAR INDICATION FAILED TO SHOW DOWN AND LOCKED. THE CREW DECLARED AN EMERGENCY AND ELECTED TO RETURN TO HNL. ON APPROACH TO HNL, WHEN THE LANDING GEAR WAS LOWERED AGAIN, ALL THREE LANDING GEAR INDICATED DOWN AND LOCKED. THE CREW LANDED IN HNL WITHOUT FURTHER INCIDENT. MAINTENANCE ADJUSTED THE LEFT DOWN LOCK SENSOR PER AMM 32-61-31 AND COMPLETED A LANDING GEAR SWING TEST WITH ALL CHECKS SATISFACTORY. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SWITCH — FAILED (P5 PANEL) · airframe 58,041 hrs · 51,768 cycles

NON-ETOPS CARGO FLIGHT 945 KOA-HNL - DURING CLIMB, THE LEFT DC BUSS LOST POWER. THE CREW STARTED THE APU TO REESTABLISH ELECTRICAL LOAD TO THE LEFT HAND DC BUSS. THE AIRCRAFT LANDED IN KOA WITHOUT FURTHER INCIDENT. MAINTENANCE PLACED THE NR 1 GENERATOR ON MEL 24-1-1 AND RETURNED THE AIRCRAFT TO SERVICE. MAINTENANCE REMOVED AND REPLACED THE GENERATOR CONTROL SWITCH AND REMOVED MEL 24-1-1.