N779AS

Part: CABLE — BROKEN (NR 2 ENGINE) · airframe 67,836 hrs · 38,777 cycles

DURING TAXI NR 2 ENGINE N1 AND N2 BEGAN UNCOMMANDED ROLLBACK, EGT CONTINUED TO CLIMB. ABOUT 840 DEGREES NR 2 GENERATOR CUT OFF. PLACING NR 2 START LEVER TO CUTOFF HALTED EGT RISE. ACFT GROUNDED. PERFORMED EIS BIT TEST, NO DEFECTS NOTED. VERIFIED FROM CREW MAX EGT 835 DEGREES NR 2 ENGINE PRIOR TO SHUTDOWN. IAW AMM 31-42-00. PERFORMED ENGINE FUEL FEED VALVE CHECK FOR NR 2 ENGINE, VALVE LEVER MOVED NORMAL, INSPECTED NR 2 ENGINE FOR FOD ON INTAKE AND EXHAUST, NO DEFECT NOTED. CONFIRMED ENGINE ROLLBACK AT ENGINE RUN. FOUND VSV FEEDBACK CABLE BROKEN AT VSV ATTACH ROD END. R & R VSV FEEDBACK CABLE REF AMM 75-31-02. ADJUSTED VSV FEEDBACK CABLE, REF AMM 75-31-02, PERFORMED ACCEL/DECEL CHECK REF AMM 71-00-00, TEST NR 8. OPS CHECKS GOOD.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 67,814 hrs · 38,765 cycles

MULTIPLE INSERTS CORRODED ON FLOOR PANEL BY THE L-1 DOOR. ACFT GROUNDED. MFG NEW FLOOR PANEL IAW EA 400-53EA-16240.

Part: STOP PIN — CHAFED (BS 794) · airframe 66,326 hrs · 37,704 cycles

AFT CARGO DOOR STOP PIN FITTING ON LOWER FWD SIDE IS HEAVILY CHAFED. ACFT GROUNDED. R & R AFT CARGO LOWER FWD DOOR STOP PIN FITTING IAW SRM 51-40-02-0G-0, PARA 7D.

Part: SKIN — CRACKED (BS 947-972) · airframe 66,326 hrs · 37,704 cycles

R2 DOOR CUTOUT IS CRACKED AT FWD LWR CORNER IN BEARSTRAP MARKED IN RED. ACFT GROUNDED. REPAIRED R2 DOOR CUTOUT FWD LOWER CORNER IAW SRM 53-00-01-2R-32. REPAIR 32.

Part: SKIN — CRACKED (BS 947-972) · airframe 66,326 hrs · 37,704 cycles

L2 DOOR CUTOUT IS CRACKED AT FWD LOWER CORNER IN BEARSTRAP MARKED IN RED. ACFT GROUNDED. REPAIRED L2 DOOR CUTOUT FWD LOWER CORNER IAW SRM 53-00-01-2R-32, REPAIR 32, THIS REPAIR IS A CATEGORY B REPAIR, REQUIRES INSPECTION WITH THRESHOLD OF 66,000 AND INTERVAL OF 24,000 FLT CYCLES. CURRENT ACFT CYCLES IS 37,704. NOTE: CAT B INFORMATION BEING TRACKED IN FILEMAKER PRO. RTOWELL 74711.

Part: SKIN — CHAFED (LT WING FLAP) · airframe 66,326 hrs · 37,704 cycles

LEFT OTBD FOREFLAP INBD L/E CHAFED. ACFT GROUNDED. R & R L/E SKIN IAW SRM 57-53-01-01-2 AND 51-40-02-0G-0.

Part: FILLER — CORRODED (BS 986) · corrosion level 2 · airframe 66,326 hrs · 37,704 cycles

AFT WASTE WATER DRAIN MAST FWD FILLER IS CORRODED. ACFT GROUNDED. REMOVED FILLER FABRICATED NEW FILLER AND INSTALLED IAW EA 1AD20122314-400-53-10.

Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 65,441 hrs · 37,175 cycles

EMERGENCY LIGHT EXIT LOCATOR SIGN AT L-1 DOOR HAS BROKEN LENS AND SEVERAL BROKEN LAMPS. ACFT GROUNDED. RELAMPED, REPLACED LENS, AND TESTED IAW MM 33-51-81-962-011. OPS NORMAL.

Part: FITTING — CRACKED (SEAL DEPRESSOR) · airframe 65,411 hrs · 37,159 cycles

L2 DOOR FWD FRAME LOWER DEPRESSOR FITTING IS CRACKED. ACFT GROUNDED. DISPLACED L2 FWD SIDEWALL PANEL IAW AMM 25 21 25 004 001, R & R SEAL DEPRESSOR FITTING IAW SRM 51-40-02-0G-0, REINSTALLED L2 FWD SIDEWALL PANEL IAW AMM 25-21-25-404-010.

Part: LAMP — FAILED (EMERGENCY LIGHT) · airframe 63,770 hrs · 36,170 cycles

INTERIOR EMERGENCY LIGHTS FOUND ABOVE SEAT 9DEF TO BE INOPERATIVE. ACFT GROUNDED. R & R EMERGENCY AISLE LIGHT LAMP AT 9 DEF, OPS CHECKED GOOD IAW AMM 33-51-21-962-001.

Part: DOUBLER — CORRODED (TAILSKID) · corrosion level 2 · airframe 63,160 hrs · 35,803 cycles

RIGHT FUSELAGE FWD OF BS 1088 AT TAILSKID DOUBLER HAS CORROSION. R & R TAILSKID DOUBLER IAW SRM 51-40-02-0G-0.

Part: SIGN — DAMAGED (EMERGENCY LIGHT) · airframe 61,702 hrs · 34,902 cycles

EMERGENCY LIGHT EXIT LOCATOR SIGN ADJACENT TO L1 DOOR HAS BROKEN LENS AND SEVERAL BROKEN LAMPS. ACFT GROUNDED. REPLACED LAMPS, REPLACED LENS, AND TESTED IAW MM 33-51-81-962-011. OPS NORMAL.

Part: DOOR — OUT OF ADJUST (L1) · airframe 61,011 hrs · 34,477 cycles

L1 DOOR IS HARD TO CLOSE AND SOMETIMES BINDS. PERFORMED VERTICAL ADJUSTMENT OF L-1 DOOR IAW AMM 52-11-00-705-007, 3, H. ADJUSTED HORIZONTAL CONTROL ROD ADJUSTMENT IAW AMM 52-11-00-705-007, 3, J, 4. PERFORMED GUIDE ARM ADJUSTMENT IAW AMM 52-11-705-00, 3, G. OPS CHECK NORMAL IAW AMM 52-11-705-00.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 60,979 hrs · 34,463 cycles

EMERGENCY LIGHT EXIT LOCATOR SIGN ON NR 1 GALLEY ADJACENT TO R-1 DOOR HAS BROKEN LENS. ACFT GROUNDED. REPLACED LENS AND TESTED IAW MM 33-51-11-962-002. OPS NORMAL.

Part: LENS — UNSECURE (EMERGENCY LIGHT) · airframe 60,948 hrs · 34,449 cycles

EXIT LIGHT COVER IN FORWARD GALLEY FELL OFF. FOUND R1 DOOR FWD. EMERGENCY LIGHT ASSY BROKEN, REMOVED ENTIRE LIGHT ASSY & REINSTALLED A NEW ASSY AFTER CORRECTLY ROUTING LIGHTING WIRES BEHIND GALLEY PANELS. OPS CHECKED GOOD.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 59,967 hrs · 33,873 cycles

LT WING L/E INBD WEB ABOVE ACCESS PANEL 6308 IS CRACKED. REMOVED CRACKED SPAR SUPPORT ANGLE FABRICATED NEW ANGLE AND INSTALLED IAW DWG 69-38865 AND SRM-51-40-02.

Part: SIGN — LOOSE (CABIN) · airframe 57,833 hrs · 32,571 cycles

LEFT "EXIT SIGN" OVER EMERGENCY EXITS CAME LOOSE. INSPECTED LT OVERWING ACCESS PANEL "SIGN". SECURED AND VERIFIED SECURE. OK FOR SVC.

Part: HANDLE — LACK OF LUBE (L1 DOOR) · airframe 57,760 hrs · 32,533 cycles

L1 DOOR HANDLE IS HARD TO OPEN AND CLOSE. LUBED FWD ENTRY DOOR PER AMM 12 25 21. OPS NORMAL.

Part: LIGHT — LOOSE (CABIN)

EMERGENCY LIGHTING STRIP IS LOOSE UNDER SEAT 24D AND HAS BECAME A TRIPPING HAZARD. REMOVED & REPLACED DAMAGED EMERGENCY TRACK STRIP IAW 33 51 91 P/N S68191 1 BATCH 1171677.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,850 hrs · 31,990 cycles

FRAME CRACKED AT PSU ATTACH BRACKAT AT FS 400 BETWEEN STRINGER 8R + 9R. ACCOMPLISHED FRAME REPAIR IAW EA 20062609 400 53 123.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,850 hrs · 31,990 cycles

SHEAR TIE AT STA 767 BETWEEN STR 27L AND 26L CORRODED. REMOVED CORROSION OUT OF LIMITS. FABRICATED TREATED APPLIED FINISH AND INSTALLED REPAIR PARTS IAW B737 400 SRM 53 00 07.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,850 hrs · 31,990 cycles

STRINGER CLIP AT STA 520 STR 8R IS CRACKED. REPLACED STRINGER CLIP IAW B737 400 SRM 51 40 02.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,850 hrs · 31,990 cycles

STRINGER CLIP AT STA 727A STR 6R IS CRACKED. REPLACED STR CLIP IAW B737 400 SRM 51 40 02.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,850 hrs · 31,990 cycles

FRAME 767 SHEAR TIE BETWEEN STR 26R AND 25R CORRODED. REMOVED CORROSION OUT OF LIMITS. FABRICATED TREATED APPLIED FINISH AND INSTALLED REPAIR PARTS IAW B737 400 SRM 53 00 07.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,850 hrs · 31,990 cycles

AFT CARGO COMPARTMENT SHEAR TIE CORRODED AT STA 847 BETWEEN STR 27L AND 27R. REMOVED CORROSION OUT OF LIMITS. FABRICATED TREATED APPLIED FINISH AND INSTALLED REPAIR PARTS IAW B737 400 SRM 53 00 07.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,850 hrs · 31,990 cycles

FRAME AT STA 787 SHEAR TIE DOUBLER BETWEEN STR 25R AND 26R IS CORRODED. REMOVED CORROSION OUT OF LIMITS. FABRICATED TREATED APPLIED FINISH AND INSTALLED REPAIR PARTS IAW B737 400 SRM 53 00 07.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,850 hrs · 31,990 cycles

FRAME 787 SHEAR TIE DOUBLER BETWEENS TR 25L AND 26L CORRODED. REMOVED CORROSION OUT OF LIMITS. FABRICATED TREATED APPLIED FINISH AND INSTALLED REPAIR PARTS IAW B737 400 SRM 53 00 07.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,850 hrs · 31,990 cycles

AFT CARGO COMPARTMENT FS 907 FRAME AFT LOWER LEG CORRODED BETWEEN S27L TO S27R. REPLACED NEW FAIL SAFE IAW B737 400 SRM 51 40 02 SRM 52 60 07 SRM 51 40 05 MM 51 21 41 327 032 MM 51 21 00 001.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,850 hrs · 31,990 cycles

AFT CARGO COMPARTMENT FS 927 FRAME AFT LOWER LEG CORRODED BETWEEN S 26L AND S 27L. REPLACED NEW FAIL SAFE IAW B737 400 SRM 51 40 02 SRM 53 60 07 SRM 51 40 05 MM 51 21 41 377 032 MM 51 21 00 001.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,850 hrs · 31,990 cycles

FRAME 767 SHEAR TIE BETWEEN STR 26R AND 27R IS CORRODED. REMOVED CORROSION OUT OF LIMITS. FABRICATED TREATED APPLIED FINISH AND INSTALLED REPAIR PARTS IAW B737 400 SRM 53 00 07.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,850 hrs · 31,990 cycles

FORWARD CARGO SHEAR TIE AT STA 500F BETWEEN STR 27L AND 26L CORRODED. REMOVED CORROSION OUT OF LIMITS. FABRICATED TREATED APPLIED FINISH AND INSTALLED REPAIR PARTS IAW B737 400 SRM 53 00 07.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,850 hrs · 31,990 cycles

FORWARD CARGO SHEAR TIE AT STA 500D BETWEEN STR 28L AND 28R CORRODED. REMOVED CORROSION OUT OF LIMITS. FABRICATED TREATED APPLIED FINISH AND INSTALLED REPAIR PARTS IAW B737 400 SRM 53 00 07.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,850 hrs · 31,990 cycles

FORWARD CARGO SHEAT TIE AT STA 500B BETWEEN STR 26L AND 27L IS CORRODED. REMOVED CORROSION OUF OF LIMITS. FABRICATED TREATED APPLIED FINISH AND INSTALLED REPAIR PARTS IAW B737 400 SRM 53 00 07.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,850 hrs · 31,990 cycles

FORWARD CARGO SHEAR TIE AT STA 500D BETWEEN STA 28R AND 27R CORRODED. REMOVED CORROSION OUT OF LIMITS. FABRICATED TREATED APPLIED FINISH AND INSTALLED REPAIR PARTS IAW B737 400 SRM 53 00 07.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,850 hrs · 31,990 cycles

FORWARD CARGO SHEAR TIE AT STA 500F BETWEEN STR 28L AND 27L CORRODED. REMOVED CORROSION OUT OF LIMITS. FABRICATED TREATED APPLIED FINISH AND INSTALLED REPAIR PARTS IAW B737 400 SRM 53 00 07.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,850 hrs · 31,990 cycles

CABIN FRAME CRACKED AT FS 440 BETWEEN STRINGER 8L AND 9L. ACOMPLISHED FRAME REPAIR IAW EA AD 20062609 400 53 123.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,850 hrs · 31,990 cycles

FORWARD CARGO SHEAR TIE AT STA 500D BETWEEN STR 28L AND 27L CORRODED. REMOVED CORROSION OUT OF LIMITS. FABRICATED TREATED APPLIED FINISH AND INSTALLED REPAIR PARTS IAW B737 400 SRM 53 00 07.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,850 hrs · 31,990 cycles

FORWARD CARGO TIEDOWN FITTING AND FLOOR SUPOPRT ANGLE FORWARD OF STA 500G BETWEEN STR 26L AND 27L CORRODED. REMOVED CORROSION OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR PARTS IAW B737 400 SRM 53 00 53.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,850 hrs · 31,990 cycles

FORWARD CARGO SHEAR TIE AT STA 500A BETWEEN STR 28L AND 28R IS CORRODED. REMOVED CORROSION OUT OF LIMITS. FABRICATED TREATED APPLIED FINISH AND INSTALLED REPAIR PARTS IAW B737 400 SRM 53 00 07.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,850 hrs · 31,990 cycles

FORWARD CARGO SHEAR TIE AT STA 500D BETWEEN STR 25R AND 24R CORRODED. REMOVED CORROSION OUT OF LIMITS. FABRICATED TREATED APPLIED FINISH AND INSTALLED REPAIR PARTS IAW B737 400 SRM 53 00 07.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,850 hrs · 31,990 cycles

FORWARD CARGO SHEAR TIE AT FS 520 BETWEEN STR 28L AND 28R CORRODED. REMOVED CORROSION OUT OF LIMITS. FABRICATED TREATED APPLIED FINISH AND INSTALLED REPAIR PARTS IAW B737 400 SRM 53 00 07.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,850 hrs · 31,990 cycles

FORWARD CARGO SHEAR TIE AT STA 500G BETWEEN STR 28R AND 27R CORRODED. REMOVED CORROSION OUT OF LIMIT. FABRICATED TREATED APPLIED FINISH AND INSTALLED REPAIR PARTS IAW B737 400 SRM 53 00 07.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 56,850 hrs · 31,990 cycles

SEAT TRACK GOUGED BEYOND LIMITS STA 767 857 LBL 49.45. CUT OUT DAMAGED SECTION AND REPLACED SEAT TRACK IAW B737 400 SRM 53 00 52 FIG 201.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 56,850 hrs · 31,990 cycles

SEAT TRACK AT LBL 45 FS 727+6.45 727B HAS SEVERAL SPOTS OF BARE METAL. BLENDED DAMAGED AREAS FOUND TO BE OUT OF LIMITS IAW B737 400 SRM 53 00 52 DETAIL V PG 105. INSTALLED NEW SEAT TRACK IAW B737 400 MM 20 50 11 912 002 FIG 203 PG 1.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 56,850 hrs · 31,990 cycles

SEAT TRACK GOUGED BEYOND LIMITS STA 737 757 LBL 24.75. CUT OUT DAMAGED SECTION INSTALLED SEAT TRACK REPAIR IAW B737 400 SRM 53 00 52 FIG 201.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,850 hrs · 31,990 cycles

FLOORBEAM AT STA 328 BL 0 OUTBOARD TO SERVICE DOOR HAS AREAS OF CORROSION. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW B737 400 SRM 53 10 51. REPAIRED FLOORBEAM IAW B737 400 SRM 53 10 51 FIG 201 REPAIR 5.

Part: SHEAR WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,850 hrs · 31,990 cycles

CABIN SHEER WEB CORRODED AT STRINGER 17L BETWEEN FS 500F 500G. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. FABRICATED NEW SHEAR WEB AND INSTALLED IAW B737 400 SRM 53 30 13 FIG 101 51 30 01 FIG 7 AND 51 40 02.

Part: WEB — DAMAGED (FUSELAGE) · corrosion level 2 · airframe 56,850 hrs · 31,990 cycles

LT FLOOR WEB AT FS 986 IS CRACKED AND CORRODED. REMOVED CRACKED LT FLOOR WEB IAW B737 400 SRM 51 40 02. FABRICATED NEW SHEAR WEB IAW B737 400 SRM 51 40 05. INSTALLED NEW WEB IAW B737 400 SRM 51 40 02.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,850 hrs · 31,990 cycles

PASSENGER CABIN L1 DOOR INTERCHORD (MOP SILL) CORRODED AT STA 312 TO STA 344 UPPER FLANGE. REPLACED INTERCHORD IAW B737 400 SRM 51 40 02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,850 hrs · 31,990 cycles

FRAME CRACKED AT PSU MOUNT BRACKET AT FS 747 BETWEEN STRINGERS 8R + 9R. ACCOMPLISHED FRAME REPAIR IAW EA AD20062609 400 53 123.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,850 hrs · 31,990 cycles

R1 DOOR MPSILL/INNER CHORD IS CORRODED. REPLACED R1 DOOR MOPSILL/INNER CHORD IAW B737 400 SRM 51 40 02.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 56,850 hrs · 31,990 cycles

STRINGER (12 R) CRACKED AT FS 291. REPLACED STRINGER IAW EA 400 53EA 06151.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,850 hrs · 31,990 cycles

FOUND CRACKED AT PSU MOUNT BRACKET FS 480 BETWEEN STRINGERS 8R + 9R. ACCOMPLISHED FRAME REPAIR IAW EA AD20062609 400 53 123.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 56,850 hrs · 31,990 cycles

STRINGER 13R CRACKED AT FS 291. REPLACED STRINGER IAW ASA EA 400 53EA 06151.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,850 hrs · 31,990 cycles

FRAME CRACKED AT PSU MOUNT BRACKET BETWEEN 8R+9R. ACCOMPLISHED FRAME REAPIR IAW EA AD 20062609 100 52 123.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,850 hrs · 31,990 cycles

STRINGER CLIP AT STA 277 STR 12L IS CRACKED. REPLACED STRINGER CLIP IAW B737 400 SRM 51 40 02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,850 hrs · 31,990 cycles

CABIN FRAME CRACKED AT PSU ATTACH BRACKET AT FS 400 BETWEEN STRINGER 8L + 9L. ACCOMLISHED FRAME REPAIR IAW EA 20062609 400 53 123.

Part: GUIDE ARM — OUT OF ADJUST (L1 DOOR) · airframe 56,086 hrs · 31,514 cycles

FORWARD ENTRY DOOR L1 WILL NOT CLOSE. THE FLAP ON THE TOP IS NOT GOING INTO PLACE PROPERLY. FOUND AFT LATCH ROLLERS NOT ENGAGING LATCH FITTINGS DUE TO AFT DOOR EDGE LAGGING FORWARD EDGE. ADJUSTED GUIDE ARM IAW B737 400 AMM 52 11 00.

Part: PLATE — LOOSE (SERVICE DOOR) · airframe 55,844 hrs · 31,405 cycles

R1 (FORWARD GALLEY SERVICE DOOR) HARD TO CLOSE FOUND UPPER HINGE LOWER CAM PLATE ATTACH BOLTS LOOSE. TIGHTEN BOLTS. DOOR OPS CHECKS OK PER B737 400 AMM 52 41 00 705 001 1.

Part: JAM-NUT — LOOSE (ENTRY DOOR) · airframe 54,795 hrs · 30,858 cycles

FORWARD ENTRY DOOR L1 HARD TO CLOSE. FOUND GUIDE ARM JAM NUT LOOSE. REPLACED L1 DOOR GUIDE ARM PER MM 52 11 21.

Part: SKIN — CRACKED (LT WING) · airframe 53,055 hrs · 29,806 cycles

LEFT WING L/E SKIN CRACKED AT I/B CORNER OF NR 1 K-FLAP O/B SPRING DOOR CUTOUT. REPAIRED L/E SKIN AT I/B CORNER OF NR 1 K-FLAP O/B SPRING DOOR CUTOUT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,055 hrs · 29,806 cycles

FUSELAGE SKIN HAS A CRACK IN SKIN BS 727D STR 10L.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 53,055 hrs · 29,806 cycles

STRINGER 8L INTERCOSTAL WEB AFT ATTACH CLIP IS CRACKED AT RIVET HOLE AT BS 360.

Part: DOOR FRAME — CRACKED (CARGO BAY) · airframe 53,055 hrs · 29,806 cycles

FWD CARGO DOORWAY FWD FRAME IS CRACKED AT 25R LOWER DOOR STOP. REMOVED CRACKED FRAME AND INSTALLED NEW FRAME.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 53,055 hrs · 29,806 cycles

STRINGER 11L INTERCOSTAL WEB AFT ATTACH CLIP IS CRACKED AT RADIUS AT BS 360. REMOVED CRACKED CLIP INSTALLED NEW CLIP.

Part: PAN — CRACKED (ENTRY DOOR) · airframe 53,055 hrs · 29,806 cycles

AFT ENTRY DOOR LINER LOWER ATTACH PAN IS CRACKED. REMOVED AND REPLACED DOOR LINER LOWER ATTACH PAN PER AMM 52-13-61.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 53,055 hrs · 29,806 cycles

STRINGER 11L INTERCOSTAL WEB AFT ATTACH CLIP IS CRACKED AT RADIUS AT BS 360.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 53,055 hrs · 29,806 cycles

STRINGER 8L INTERCOSTAL WEB AFT ATTACH CLIP IS CRACKED AT RIVET HOLE AT BS 360. REMOVED CRACKED CLIP INSTALLED NEW CLIP.

Part: SKIN — PUNCTURED (FOREFLAP) · airframe 49,921 hrs · 27,944 cycles

LT INBD FORE FLAP LOWER SURFACE PUNCTURED. REMOVED DAMAGED AREA FABRICATED FILLER AND DOUBLER INSTALLED IAW SRM 51 70 10.

Part: SKIN — PUNCTURED (MIDFLAP) · airframe 49,921 hrs · 27,944 cycles

RT IB MID FLAP TRAILING EDGE WEDGE HAS A PUNCTURE IB OF 2ND TRACK. REMOVED EXISTING DOUBLER FABBED REPAIR PARTS AND BONDED REPAIR IAW B737 400 SRM 51 70 10.

Part: SKIN — DENTED (FUSELAGE) · airframe 49,921 hrs · 27,944 cycles

RT EXTERNAL FUSELAGE DENTED AT STA 236 BELOW AND AFT OF EXTERNAL POWER DOOR. REMOVED DAMAGED AREA FABBED REPAIR PARTS INSTALLED THE REPAIR IAW AAR EA 13108 AND ASA EA 400 53 EA 00454.

Part: SKIN — DENTED (MIDFLAP) · airframe 49,921 hrs · 27,944 cycles

LT INBD MID FLAP T/E WEDGE LOWER SURFACE HAS MULTIPLE SHARP DENTS AT INBD CORNER AT PREVIOUS REPAIR. REMOVED PREVIOUS REPAIR FABBED REPAIR PARTS AND BONDED IAW SRM51 70 10.

Part: SKIN — DAMAGED (DOOR) · airframe 49,921 hrs · 27,944 cycles

LT DOOR UPPER AFT CORNER CURLED BACK. REMOVED DAMAGED AREA FABRICATED FILLER AND DOUBLER INSTALLED IAW SRM 52-00-01.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,921 hrs · 27,944 cycles

FUSELAGE SKIN CRACKED AFT OF STA 303 BELOW LT DOOR UPPER HINGE REMOVED DAMAGED SKIN. FABRICATED INSTALLED REPLACEMENT GAP COVER IAW SRM 51 40 02.

Part: SKIN — PUNCTURED (RUDDER) · airframe 49,921 hrs · 27,944 cycles

RUDDER PUNCTURED RT SIDE APPROX. 16" FROM 88" FROM LOWER EDGE. PREPPED PUNCTURED AREA AND REPAIRED AREA IAW B737 400 SRM 51 70 03 REP 2.

Part: SKIN — DELAMINATED (MIDFLAP) · airframe 49,921 hrs · 27,944 cycles

LT IB MID FLAP T/E WEDGE IS DELAMINATED UPPER SURFACE CENTER. REMOVED DAMAGED AREA FABRICATED REPAIR PARTS BONDED REPAIR IAW SRM 51 70 10 REP 4.

Part: SKIN — DENTED (NR 3 SPOILER) · airframe 49,921 hrs · 27,944 cycles

NR 3 SPOILER UPPER SKIN HAS A CLUSTER OF DENTS 1.8 IN FWD OF T/E. REMOVED DAMAGED AREA FABRICATED FILLER AND DOUBLER BONDED REPAIR IAW SRM 51 70 10.

Part: SKIN — DENTED (FOREFLAP) · airframe 49,921 hrs · 27,944 cycles

LT IB FORE FLAP UPPER SURFACE DENTED. REMOVED DAMAGED AREA FABRICATED FILLER AND DOUBLER BONDED REPAIR IAW SRM 51 70 10.

Part: SKIN — DENTED (NR 2 SPOILER) · airframe 49,921 hrs · 27,944 cycles

NR 2 SPOILER UPPER SKIN IS DENTED. PREPPED DAMAGED AREA FABRICATED DOUBLER AND BONDED REPAIR IAW SRM 51 70 10 REPAIR 2.

Part: SKIN — CHAFED (FOREFLAP) · airframe 49,921 hrs · 27,944 cycles

LT OB FORE FLAP IB LEADING EDGE IS CHAFED. REMOVED DAMAGED AREA FABRICATED HEAT TREATED AND INSTALLED REPLACEMENT SKIN IAW SOPM 20 50 01.

Part: SKIN — CHAFED (MIDFLAP) · airframe 49,921 hrs · 27,944 cycles

RT OTBD MID FLAP CHAFED ABOVE NR 7 FLAP TRACK FAIRING. REMOVED DAMAGED AREA FABRICATED REPAIR PARTS AND BONDED REPAIR IAW SRM 51 70 10.

Part: SKIN — DENTED (NR 3 SPOILER) · airframe 49,921 hrs · 27,944 cycles

LT NR 3 SPOILER UPPER SKIN DENTED .45 INCH DIAMETER AND .004 DEEP A/Y=112. REMOVED DAMAGED AREA FABRICATED AND INSTALLED DOUBLER IAW SRM 51 70 10.

Part: DOUBLER — PUNCTURED (MIDFLAP) · airframe 49,921 hrs · 27,944 cycles

LT INBD MID FLAP LOWER SURFACE PREVIOUS REPAIR DOUBLER PUNCTURED. REMOVED DAMAGED AREA FABRICATED FILLER AND DOUBLER INSTALLED IAW SRM 51 70 10.

Part: SKIN — DENTED (FOREFLAP) · airframe 49,921 hrs · 27,944 cycles

LT IB FORE FLAP LOWER SURFACE HAS A CLUSTER OF 20 DENTS BEHIND NR 2 TIRE. REMOVED DAMAGED AREA FABRICATED FILLER AND DOUBLER BONDED REPAIR IAW SRM 51 70 10.

Part: SKIN — DENTED (HORIZ STAB) · airframe 49,921 hrs · 27,944 cycles

RT HORIZ STAB AT STA 92.7 HAS 2 DENTS ON THE LEADING EDGE. REMOVED PREVIOUS REPAIR FABRICATED FILLER AND DOUBLER INSTALLED IAW SRM 55 10 01.

Part: SKIN — DENTED (HORIZ STAB) · airframe 49,921 hrs · 27,944 cycles

RT HORIZ STAB AT STA101 HAS A DENTS ON THE LEADING EDGE. REMOVED PREVIOUS REPAIR FABRICATED FILLER AND DOUBLER INSTALLED IAW SRM 55 10 01.

Part: SKIN — DENTED (CARGO DOOR) · airframe 34,063 hrs · 18,628 cycles

AFT CARGO DOOR DENTS WITH SCRATCHES AND DENTS WITH CREASES IN 3 AREAS. REMOVED AFT CARGO DOOR EXTERNAL SKIN. FABRICATED LOCATED DRILLED AND INSTALLED A REPLACEMENT SKIN IAW B737 400 SRM 52 30 01 FIG 201.

Part: LATCH — MISINSTALLED (L2 DOOR SLIDE) · airframe 46,378 hrs · 25,967 cycles

FLIGHT ATTENDANT UNABLE TO ARM L2 DOOR. FOUND LATCH ASSY INSTALLED INCORRECTLY. PROPERLY INSTALLED LATCH ASSY. (REF MM25 61 35 PG 209 & MM SUPP 25 61 35)

Part: SKIN — DENTED (FUSELAGE) · airframe 45,829 hrs · 25,689 cycles

DENT IN FUSELAGE SKIN. REPAIRED IAW EA 5330 02224 AND SRM 53-00-01 REPAIR 31 DETAIL 9.

Part: A/C PACK — LEAKING (A/C BAY) · airframe 44,344 hrs · 24,849 cycles

SMOKE IN CABIN ON TAKEOFF OUT OF ADQ. REMOVED AND REPLACED LEFT PACK ACM PER AMM 21-51-11. OPS AND LEAK CHECK GOOD.

Part: SKIN — DENTED (BS 492) · airframe 42,548 hrs · 23,758 cycles

FUSELAGE SKIN DENTED ATR AFT SIDE OF FWD DOOR CUTOUT. REPAIRED DENT PER EA 5330 02181.

Part: RETAINER — CORRODED (OVERWING EXIT) · airframe 42,548 hrs · 23,758 cycles

CORROSION IN RIGHT AFT OVERWING EXIT LWR SEAL RETAINER. REMOVED AND REPLACED LWR SEAL RETAINER PER SRM 51-40-02.

Part: FLOORBEAM — CORRODED (BS 360) · corrosion level 2 · airframe 42,548 hrs · 23,758 cycles

FLOORBEAM CORRODED. REPAIRED PER EA 5310 02651.

Part: DOOR FRAME — CORRODED (BS 794) · corrosion level 2 · airframe 42,548 hrs · 23,758 cycles

AFT CARGO BAY DOORWAY FRAME CORRODED. REMOVED AND REPLACED FRAME PER SRM 51-40-02 AND DWG 65 47959.

Part: FRAME — CRACKED (BS 303) · airframe 42,548 hrs · 23,758 cycles

FRAME CRACKED AT STOP PAD FITTING. REPAIRED FRAME PER EA 5310 02653 AND ER 06 2544.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,548 hrs · 23,758 cycles

FOUND CRACKED FRAME WEB. REMOVED AND REPLACED FRAME PER SRM 51 40 02.

Part: SKIN — LIGHTNING STRIKE (BS 268-273) · airframe 42,548 hrs · 23,758 cycles

PER EA 5330 1981 PERMINATE REPAIR REQUIRED TO LOCATION STATED ON LOGPAGE 5916421 W I 24 MONTHS OF THIS ENTRY DATE. REPAIRED PER EA 5330 02126.

Part: SKIN — DENTED (FUSELAGE) · airframe 42,548 hrs · 23,758 cycles

FOUND DENT IN FUSELAGE SKIN. REPAIRED PER EA 533 02125.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,548 hrs · 23,758 cycles

CORROSION ON UPPER FLANGE OF 986.5 FLOORBEAM. REPAIRED IAW EA 5310 02652.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,548 hrs · 23,758 cycles

FLOORBEAM CORRODED. REPAIRED IAW SRM 53 10 51.

Part: SKIN — LIGHTNING STRIKE (FUSELAGE) · airframe 42,548 hrs · 23,758 cycles

LIGHTING STRIKES ON SKIN AT CAPT'S NR 3 WINDOW LWR AFT CORNER. REPAIRED LIGHTING STRIKES ON SKIN AT CAPT'S NR 3 WINDOW CUT OUT LWR AFT CORNER.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 42,548 hrs · 23,758 cycles

ELONGATED HOLES IN FRAME FLANGE. CUT OUT AND REMOVED 1.1 X .90 DAMAGED AREA ON FRAME UPPER FLANGE. FABRICATED AND INSTALLED REPAIR IAW SRM 51 70 11.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,548 hrs · 23,758 cycles

SKIN DOUBLER CORRODED. REMOVED AND REPLACED IAW SRM 51 40 02.

Part: SHEAR TIE — CORRODED (BS 747) · corrosion level 2

FOUND CORROSION ON SHEAR TIE. REPAIRED PER SRM 53 00 07.

Part: FRAME — CRACKED (BS 793) · airframe 42,548 hrs · 23,758 cycles

FOUND CRACK IN FRAME STRAP. REMOVED AND REPLACED FRAME STRAP PER SRM 51 40 02.

Part: FLOORBEAM — CORRODED (BS 344) · corrosion level 2 · airframe 42,548 hrs · 23,758 cycles

FOUND CORROSION ON FLOORBEAM. REPAIRED PER ER 06 2584 AND EA 5310 02649.

Part: FRAME — CRACKED (BS 380) · airframe 42,548 hrs · 23,758 cycles

FOUND CRACK IN FRAME. REPAIRED PER SRM 53 00 07.

Part: FRAME — CORRODED (BS 500E) · corrosion level 2 · airframe 42,548 hrs · 23,758 cycles

FOUND CORROSION ON FRAME. REPAIRED PER SRM 53 00 07.

Part: SILL — CORRODED (BS 913-1016) · corrosion level 2 · airframe 42,548 hrs · 23,758 cycles

FOUND CORROSION ON LT CREASE BEAM MOP SILL. REMOVED AND REPLACED MOPSILL PER SRM 51 40 02.

Part: FRAME — CRACKED (BS 360) · airframe 42,548 hrs · 23,758 cycles

CRACK IN FRAME FASTENER. REPAIRED FRAME PER SRM 53 00 07.

Part: FAILSAFE — CORRODED (BS 787) · airframe 42,548 hrs · 23,758 cycles

FOUND CORROSION ON FAIL/SAFE. REPAIRED PER SRM 51 70 11.

Part: FAILSAFE — CORRODED (BS 793) · airframe 42,548 hrs · 23,758 cycles

FOUND CORROSION ON FAIL/SAFE ANGLE. REPLACED PART PER SRM 51 40 02 AND DWG 65 47959.

Part: FRAME — PUNCTURED (BS 787) · airframe 42,548 hrs · 23,758 cycles

FOUND UPPER FRAME FLANGE PUNCTURED. CUT OUT DAMAGE AND INSTALLED REPAIR PER SRM 51 70 11.

Part: SHEAR TIE — CORRODED (BS 787) · corrosion level 2 · airframe 42,548 hrs · 23,758 cycles

FOUND CORROSION ON SHEAR TIE. CUT OUT DAMAGE AND INSTALLED REPAIR PER SRM 53 00 07.

Part: SHEAR TIE — CORRODED (BS 887) · corrosion level 2 · airframe 42,548 hrs · 23,758 cycles

FOUND CORROSION ON SHEAR TIE. CUT OUT AND INSTALLED REPAIR PER SRM 53 60 07.

Part: FRAME — CRACKED (BS 480) · airframe 42,548 hrs · 23,758 cycles

FOUND CRACK IN FRAME. REMOVED DAMAGE IN FRAME FABRICATED REPAIR PARTS AND INSTALLED PER SRM 53 00 07.

Part: SHEAR TIE — CORRODED (BS 500) · corrosion level 2 · airframe 42,548 hrs · 23,758 cycles

FOUND CORROSION ON AFT SIDE OF SHEAR TIE. REPLACED SHEAR TIE PER SRM 51 40 02.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,548 hrs · 23,758 cycles

CORROSION ON SHEAR TIE. REPAIRED PER SRM 53 00 07 REPAIR 3.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,548 hrs · 23,758 cycles

CORROSION ON SHEAR TIE. FABRICATED AND INSTALLED SHEAR TIE PER SRM 53 00 07.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,548 hrs · 23,758 cycles

SHEAR TIE CORRODED. REMOVED DAMAGED SHEAR TIE FABRICATED REPAIR PARTS AND INSTALLED PER SRM 53 00 07.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,548 hrs · 23,758 cycles

CORROSION ON SHEAR TIE. BLENDED FOUND OUT OF LIMITS REMOVED DAMAGE FABRICATED NEW SHEAR TIE AND INSTALLED PER SRM 53 00 07.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,548 hrs · 23,758 cycles

STRINGER CLIP CORRODED. REMOVED CORROSION FOUND OUT OF LIMITS REPLACED STRINGER CLIP PER SRM 53 00 07 AND 51 40 02.

Part: ANGLE — TOOL DAMAGE (CARGO DOOR) · airframe 42,548 hrs · 23,758 cycles

FWD CARGO DOOR HAS TOOLING MARKS ON FWD INBD L ANGLE LOCATED AT DOOR DAMPNER MOUNT FITTING. BLENDED DAMAGE FOUND OUT OF LIMITS FABRICATED AND INSTALLED NEW L ANGLE PER SRM 51 30 01.

Part: SILL — CORRODED (CORRODED) · corrosion level 2 · airframe 42,548 hrs · 23,758 cycles

CORROSION ON RT CREASE BEAM MOPSILL. REMOVED AND REPLACED CREASE BEAM MOPSILL PER SRM 51-40-02.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,548 hrs · 23,758 cycles

CORROSION ON SHEAR TIE. REPAIRED PER SRM 53 00 07.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,548 hrs · 23,758 cycles

CORROSION ON MOPSILL. REMOVED AND REPLACED PER SRM 51 40 02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,548 hrs · 23,758 cycles

WHILE WORKING FOUND BSTA 360 FLOORBEAM CORRODED AROUND NUT PLATES. REPAIRED FLOORBEAM IAW SRM 53-00-51.

Part: STRAP — CORRODED (FUSELAGE) · airframe 42,548 hrs · 23,758 cycles

CORROSION ON REINFORCEMENT STRAP. REMOVED AND REPLACED STRAP PER SRM 51 40 02.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,548 hrs · 23,758 cycles

CORROSION ON SHEAR TIE. FABRICATED AND INSTALLED SHEAR TIE PER SRM 53 00 07.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,548 hrs · 23,758 cycles

CORROSION ON SHEAR TIE. FABRICATED AND INSTALLED SHEAR TIE PER SRM 53-00-07.

Part: SHEAR TIE — CORRODED (BS 520) · corrosion level 2 · airframe 42,548 hrs · 23,758 cycles

FOUND CORROSION ON FWD SIDE OF SHEAR TIE. REMOVED AND REPLACED SHEAR TIE PER SRM 53 00 07.

Part: DOUBLER — CORRODED (BS 794) · airframe 42,548 hrs · 23,758 cycles

WHILE WORKING FOUND CORROSION ON INTERNAL DOUBLER AT BSTA 794. REMOVED AND REPLACED INTERNAL DOUBLER PER SRM 53 00 04.

Part: FRAME — DENTED (BS 500D) · airframe 42,548 hrs · 23,758 cycles

FOUND FWD CARGO COMPARTMENT UPPER FLANGE DENTED. REPAIRED FRAME PER SRM 51 70 11.

Part: SILL — CORRODED (BS 306) · corrosion level 2 · airframe 42,548 hrs · 23,758 cycles

FOUND CORROSION ON L 1 MOPSILL CORRODED UPPER AND LOWER SURFACES. REMOVED AND REPLACED MOPSILL L 1.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 42,548 hrs · 23,758 cycles

FOUND CORROSION ON FWD ENTRY DOOR SUB THRESHOLD "U" AND "Z" CHANNELS UPPER AND LOWER SURFACES. REMOVED AND REPLACED "U" AND "Z" CHANNELS PER SRM 51 40 02.

Part: SHEAR TIE — CORRODED (BS 500F) · corrosion level 2 · airframe 42,548 hrs · 23,758 cycles

FOUND CORROSION ON FWD SIDE OF FRAME. REMOVED AND REPLACED SHEAR TIE PER SRM 53 00 07.

Part: TEE FITTING — CORRODED (BS 1185-1195) · airframe 42,548 hrs · 23,758 cycles

APU COMPT CORROSION ON TEE FITTING AT AFT APU AIR INLET CUTOUT. REPLACED T CHORD AT AFT APU AIR INLET PER SRM 51 40 02.

Part: TEE FITTING — CORRODED (BS 1124-1131) · airframe 42,548 hrs · 23,758 cycles

APU COMPARTMENT CORROSION ON TEE FITTING AT FWD APU AIR INLET CUTOUT. REMOVED AND REPLACED T CHORD AT FWD APU AIR INLET CUTOUT PER SRM 51 40 02.

Part: STRINGER — CORRODED (BS 1117-1127) · airframe 42,548 hrs · 23,758 cycles

WHILE WORKING FOUND RT LOWER APU TORQUE BOX STRINGER CORRODED. REMOVED AND REPLACED RT LOWER APU TORQUE BOX STRINGER PER SRM 51 40 02.

Part: TEE FITTING — CORRODED (BS 1114) · airframe 42,548 hrs · 23,758 cycles

WHILE WORKING FOUND RT UPPER APU TORQUE BOX STRINGER CORRODED. REMOVED AND REPLACED RT UPPER APU TORQUE BOX STRINGER PER SRM 51 40 02.

Part: FRAME — DENTED (500E S23-24R) · airframe 42,548 hrs · 23,758 cycles

FOUND FWD CARGO COMP FRAME UPPER FLANGE IS DENTED. CUT OUT DAMAGED SECTION OF FRAME 2" BY 6.2" FROM ORIGINAL THICKNESS OF .050". INSTALLED REPAIR PARTS AND REFINISHED PER SRM 53 00 07.

Part: ARM — WORN (L1 DOOR) · airframe 41,190 hrs · 23,079 cycles

L1 DOOR DOES NOT CLOSE PROPERLY. HANDLE DOES NOT FULLY LATCH DOWN WHEN CLOSING DOOR, HANDLE JAMS. FOUND L1 DOOR FWD LOWER ROLLER ARM GOUGED. GOUGE CAUSED BY WORN UPPER AND LWR HINGE ARMS MAKING DOOR SAG AND ROLLER ARM IMPACT GUIDE PLATE.

Part: WEDGE — DENTED (TE FLAP)

RT IB MID FLAP T/E WEDGE 7420R HAS SEVERAL DINGS. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLERS AND DOUBLERS IAW SRM. (K)

Part: SKIN — PUNCTURED (TE FLAP)

RT IB FORE FLAP LWR SKIN PUNCTURED. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLERS AND DOUBLERS IAW SRM. (K)

Part: SKIN — DENTED (LT TE FLAP)

LT IB FORE FLAP DENTED, DELAMINATED ON LOWER SKIN AT CENTER TRACK. REMOVED DAMAGE, FABRICATED AND INSTALLED SKIN SECTION AND DOUBLER IAW SRM. (K)

Part: FRAME — CRACKED (FUSELAGE)

FRAME AT BSTA 500, RBL 1, WL 154 CRACKED. REPAIRED FRAME IAW SRM. (K)

Part: WEB — CORRODED (FUSELAGE)

AFT PIT DOOR-SILL WEB CORRODED. REMOVED CORRODED WEB, LOCATED AND INSTALLED NEW WEB IAW SRM. (K)

Part: STRINGER — CORRODED (FUSELAGE)

STRINGER 28L IS CORRODED AT BSTA 500G. REMOVED DAMAGED SECTION OF STR 28L, FABRICATED AND INSTALLED REPAIR PIECES IAW SRM. (K)

Part: SHEAR TIE — CORRODED (FUSELAGE)

SHEAR TIE AND FRAME AT 747 BL0, RBL 5, IS CORRODED. REMOVED DAMAGED SECTION OF SHEAR TIE AND FRAME, FABRICATED AND INSTALLED REPAIR PIECES IAW SRM. (K)

Part: SHEAR TIE — CORRODED (FUSELAGE)

SHEAR TIE AT FRAME 727C BL 0 IS CORRODED. REMOVED DAMAGED SECTION OF SHEAR TIE, FABRICATED AND INSTALLED REPAIR PIECES IAW SRM. (K)

Part: SHEAR TIE — CORRODED (FUSELAGE)

SHEAR TIE AT FRAME 747C, RBL 12 IS CORRODED. REMOVED DAMAGED SECTION OF SHEAR TIE, FABRICATED AND INSTALLED REPAIR PIECES IAW SRM. (K)

Part: SHEAR TIE — CORRODED (FUSELAGE)

SHEAR TIE AT BSTA 807, BL0, CORRODED. REMOVED CORRODED REPAIR PART, FABRICATED AND NSTALLED REPAIR PIECES IAW SRM. (K)

Part: WIRE — DAMAGED (CABIN)

SEA - DURING LINE CHECK, FOUND EMERGENCY TRACK LIGHT WIRING DAMAGE AT ROW 2-7 AND INOPERATIVE. REPLACED LIGHT ASSEMBLY, OPERATIONAL CHECK GOOD. (M)

Part: SKIN — PUNCTURED (L/E FLAP)

PAE - DURING SI CHECK, FOUND RIGHT INBOARD FORE FLAP LOWER SKIN IS PUNCTURED 19 INCHES FROM INBOARD END AND 9 INCHES FROM TRAILING EDGE. REPAIRED IAW SRM 51-70-10. (M)

Part: CARGO TRACK — DAMAGED (FUSELAGE)

PAE - DURING SI CHECK, FOUND AFT CARGO BAY FLOOR TRACK AT BS 750 TO BS 756, WL 150 AND BL 3 LEFT AND RIGHT DAMAGED. REPAIRED IAW ASA EA 5320-01378. REF ASAA010057. (M)

Part: CARGO TRACK — DAMAGED (FUSELAGE)

PAE - DURING SI CHECK, FOUND AFT CARGO BAY FLOOR TRACK AT BS 750 TO BS 756, WL 150 AND BL 3 LEFT AND RIGHT DAMAGED. REPAIRED IAW ASA EA 5320-01378. (M)

Part: STRINGER CLIP — BENT (FUSELAGE)

PAE - DURING SI CHECK, FOUND AFT CARGO BAY STRINGER CLIP AT STRINGER RT, WL 158, BL 27 LEFT AND BS 727F IS BENT. REPLACED IAW SRM. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

PAE - DURING SI CHECK, FOUND FLOORBEAM CORRODED SEVERAL PLACED NEAR NUT PLATE HOLES AT BS 986.5, RBL 5-43, AND WL208, LEVEL 1. REPAIRED IAW SRM AND ASA EA5310-01928. (M)

Part: SILL — CORRODED (FUSELAGE)

PAE - DURING SI CHECK, FOUND CORROSION ON MOPSILL AT BS 344-350, LBL 56 AND WL 208. REMOVED AND REPLACE PER SRM 51-40-05. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

PAE - DURING SI CHECK, FOUND FLOORBEAM CORRODED AT BS 1016, LBL 29 AND WL 208. REPAIRED IAW SRM AND ASA EA 5310-01925. (M)

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2

PAE - DURING SI CHECK, FOUND CORROSION ON MOPSILL AT BS 325, LBL 56 AND WL 208, LEVEL 2. REMOVED AND REPLACED PER SRM 51-40-05. (M)

Part: SUPPORT FITTING — CORRODED (FUSELAGE)

PAE - DURING SI CHECK, FOUND CORROSION ON GIRT BAR SUPPORT FITTING AT BS 312, WL 208, LBL 55. REPLACED IAW WITH SRM. (M)

Part: SUPPORT FITTING — CORRODED (FUSELAGE) · corrosion level 2

PAE - DURING SI CHECK, FOUND GIRT BAR SUPPORT FITTING CORRODED AT BS 344, WL 208 AND LBL 56 (LEVEL II). REPLACED IAW SRM. (M)

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2

PAE - DURING SI CHECK, FOUND CORROSION ON MOPSILL AT BS 943-998, LBL 52 AND WL 208 (LEVEL II) REPLACED IAW SRM. (M)

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2

PAE - DURING SI CHECK, FOUND CORROSION ON MOPSILL AT BS 334, WL 208 AND RBL 57 , LEVEL II. REPLACED IAW SRM. (M)

Part: DOUBLER — CRACKED (FUSELAGE)

PAE - DURING SI CHECK, FOUND EXTERNAL POWER CUT OUT INTERNAL SKIN DOUBLER IS CRACKED AT TWO LOCATIONS FORWARD LOWER CORNER AT STATION 228 AND RBL 30 AND WL 175 TO 185. REPAIRED IAW EA 5330-01514. (M)

Part: FRAME — CRACKED (FUSELAGE)

PAE - DURING SI CHECK, FOUND SIDE CHORD ON LEFT AND RIGHT SIDE AT BS 178 AND WL 207 CRACKED. REPAIR PENDING. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

PAE - DURING SI CHECK, FOUND CORROSION ON FLOORBEAM AT BS 947, RT BL 4 AND WL 208, LEVEL II. REPAIRED PER SRM 53-00-51. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2

PAE - DURING SI CHECK, FOUND CORROSION ON FLOORBEAM NUT PLATE HOLES AT BS 986.5 LBL 2 TO 43 AND WL 208, LEVEL 2. REPAIR PENDING. (M)

Part: LAMP — INOPERATIVE (ROW 16,19) · airframe 24,186 hrs · 13,996 cycles

SEA-DURING LINE CHECK, FOUND EMERGENCY TRACK LIGHTING INOPERATIVE AT ROWS 16, 19. REMOVED AND REPLACED LIGHTS AND WIRING ASSEMBLIES, OPS CHECKED NORMAL.

Part: LIGHT — DISCONNECTED (ROW 6 - 7)

PDX DURING SERVICE INSPECTION FOUND EMERERGENCY TRACK LIGHTS INOP AT ROW 6-7, (WIRE DISCONNECTED). RECONNECTED TRACK LIGHTS, OPERATION CHECKED NORMAL, NO DEFECTS NOTED.

Part: BEARING — LACK OF LUBE (PAX DOOR)

SEA - PRIOR TO FLIGHT 7264 - THE L1 DOOR WAS FOUND TO BE HARD TO CLOSE. LUBRICATED HINGE BEARINGS AND DOOR OPERATED NORMALLY. (M)

Part: WINDOW — MALFUNCTIONED (COCKPIT)

SEA - PRIOR TO FLIGHT 84, THE FIRST OFFICERS SLIDING WINDOW WOULD NOT CLOSE. LUBRICATED SLIDING WINDOW AND WINDOW OPERATED NORMALLY. (M)

Part: WIRE — BROKEN (ROW 3 - 7)

SAN - PRIOR TO FLIGHT 521, THE EMERGENCY EXIT TRACK LIGHTS AT ROWS 3-7 WERE FOUND TO BE INOPERATIVE. CONTRACT MAINTENANCE REPAIRED BROKEN WIRE AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

PDX - DURING MAINTENANCE CHECK, THREE EMERGENCY EXIT FLOOR TRACK LIGHTS AT AFT OVERWING EXIT WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRING/LIGHTS AND LIGHTS OPERATED NORMALLY. (M)

Part: CONTROL PANEL — SMOKE (RT GCU) · corrosion level 3 · airframe 20,956 hrs · 12,217 cycles

PDX - FLT 603 - DURING FLIGHT, THE NR 2 GENERATOR BUS OFF LIGHT ILLUMINATED WITH ASSOCIATED SYSTEM LIGHTS. ODOR OF ELECTRICAL SMOKE WAS NOTED, THEN DISSIPATED. SMOKE WAS NOTED COMING FROM THE GCU. REMOVED POWER FROM NR 2 GEN BUS AND SMOKE CEASED. THE AIRCRAFT LANDED IN PDX WITHOUT INCIDENT. PDX MAINTENANCE REPLACED THE RT GCU WITH THE APU GCU. FAULTY GCU NOW POSITIONED IN THE APU GCU RACK AND WAS RELEASED PER MEL 24-2. PDX MAINT RAN ENGINES AND BOTH LEFT AND RIGHT GCU''S OPERATED NORMALLY. THE APU GCU WAS SUBSEQUENTLY REPLACED AND THE MEL WAS CLEARED. (X)

Part: SNUBBER — FAILED (L-1 DOOR)

SEA - FLT 399 - L-1 DOOR DIFFICULT TO CLOSE. REPLACED L-1 DOOR SNUBBER ASSEMBLY AND DOOR OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

PDX - DURING MAINTENANCE CHECK, THREE EMERGENCY EXIT FLOOR TRACK LIGHTS AT THE AFT OVERWING EXIT WERE FOUND TO BE INOPERATIVE. RECONNECTED LIGHTS/WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: SIGN — MISSING (LT AFT DOOR)

ANC - FLT 94 - THE LEFT AFT DOOR LOWER 'EXIT' SIGN WAS FOUND TO BE MISSING. REPLACED 'EXIT' SIGN. (M)

Part: LIGHT — INOPERATIVE (CABIN)

SEA - PRIOR TO FLT 138, ONE RED EMERGENCY EXIT FLOOR TRACK LIGHT ASSEMBLY WAS FOUND MISSING AT AFT EXIT AND WIRES WERE FOUND TO BE STICKING OUT OF TRACK. REPLACED AFT TWO LIGHT ASSEMBLIES AND SECURED. LIGHTS OPERATED NORMALLY. (M)

Part: TRACK — CORRODED (BS 803-809)

SEA - DURING C-CHECK, MINOR SURFACE CORROSION WAS FOUND AT TWO LOCATIONS ON THE UPPER SURFACE ON THE OUTBOARD FLANGE OF THE TIE DOWN TRACK IN THE AFT CARGO COMPARTMENT. REPAIRED PER EA 5360-01015. (M)

Part: SKIN — PUNCTURED (BS 1064)

SEA - DURING C-CHECK, A PUNCTURE WAS FOUND IN THE FUSELAGE SKIN AT FS 1064 AND STRINGER 24. REPAIRED PER EA 5330-01311 AND BOEING TELEX ASA-SEA-98-00012RR. (M)

Part: SKIN — PEELING (LT ELEVATOR)

SEA - DURING C-CHECK, A SMALL SECTION OF THE OUTER CARBON LAYER WAS FOUND PEELING ON THE LEFT ELEVATOR LOWER SURFACE NEXT TO THE 3RD HINGE CUTOUT FROM INBOARD END. REPAIRED PER EA 5520-01051 AND BOEING TELEX ASA-SEA-98-0010RR. (M)

Part: BRACKET — WORN (BS 729.35)

SEA - DURING C-CHECK, EXCESSIVE WEAR WAS FOUND AROUND FASTENER HOLE ON THE LEFT MLG FAIRING BRACKET AT STATION 729.35. REPAIRED PER EA 5320-01333. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, 3 EACH EMERGENCY EXIT FLOOR TRACK LIGHTS AT AFT OVERWING EXIT AND AFT 6 EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED WIRING AT BOTH LOCATIONS AND LIGHTS OPERATED NORMALLY. (X)

Part: BATTERY — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROWS 22 THROUGH 24. REPLACED BATTERY AND LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROWS 22 THROUGH 26. REPLACED BATTERY AND LIGHTS OPERATED NORMALLY. (M)

Part: ARM GUIDE — MALFUNCTION (L1 DOOR)

SEA - FLT 72 - L1 DOOR DIFFICULT TO CLOSE. REPLACED ARM ASSEMBLY GUIDE AND DOOR OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE AFT 2 EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, BOTH THE FORWARD AND AFT EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED BOTH FORWARD AND AFT WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: LIGHT — DEFECTIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE L-1 EMERGENCY EXIT IDENTIFIER WAS FOUND TO HAVE ONE LAMP OUT AND A BROKEN LENS. REPLACED LIGHT ASSEMBLY AND OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE FROM ROW 26 AFT. RECONNECTED TRACK WIRING AT ROW 26 AND LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY PACK — DEFECTIVE (CABIN)

SFO - DURING MAINTENANCE CHECK, THE AFT 6 EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. REPLACED BATTERY CHARGER AND BATTERY PACK, LIGHTS OPERATED NORMALLY. REFERENCE ASAA9540105.

Part: BATTERY CHARGER — DEFECTIVE (CABIN)

SFO - DURING MAINTENANCE CHECK, THE AFT 6 EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. REPLACED BATTERY CHARGER AND BATTERY PACK, LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, ALL EMERGENCY LIGHTS AFT OF ROW 25 WERE FOUND INOPERATIVE. REPLACED AFT BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

JNU - DURING MAINTENANCE CHECK, THE LEFT AFT EMERGENCY LIGHTS BATTERY PACK WAS FOUND INOPERATIVE. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (X)

Part: L1 DOOR — LACK OF LUBE (FWD CABIN)

ANC - PILOT REPORT - FORWARD ENTRY DOOR DIFFICULT TO CLOSE AND MAKES CREAKING NOISE DURING LAST FEW INCHES UNTIL CLOSED. MAINTENANCE GREASED, VISUALLY INSPECTED AND OPS CHECKED OKAY. (X)

Part: EEL BATT CHARGER — MALFUNCTIONED (CABIN)

SEA - SEVERAL EMERGENCY LIGHTS IN AFT CABIN CAME ON FOR A FEW SECONDS, THEN WENT OFF FOR A FEW SECONDS. THIS HAPPENED THREE TIMES. MAINTENANCE REPLACED BOTH AFT CABIN BATTERY PACKS. (M)

Part: HINGES — LACK OF LUBE (L1 DOOR)

SEA - FLT 489 - CREW REPORTED, L1 DOOR HARD TO CLOSE AND MAKES BINDING NOISE. LUBED DOOR HINGES AND GUST LOCK, DOOR OPERATED NORMALLY. (W)

Part: GALLEY DOOR — LACK OF LUBE (FWD CABIN)

JNU - CHECK, R1 FWD DOOR DOOR DIFFICULT TO OPEN. MAINTENANCE LUBED HINGES AND CAM ROLLER BEARINGS. (W)