N660SW

Part: SKIN — CRACKED (FUSELAGE) · airframe 89,988 hrs · 67,850 cycles

SKIN CRACKED, BETWEEN BS 297 TO 298, STRINGER 18R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 89,988 hrs · 67,850 cycles

SKIN CRACKED, BETWEEN BS 847+6 - 847+6.75, STRINGER 20L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 89,988 hrs · 67,850 cycles

SKIN CRACKED, BETWEEN BS 460+5 - 460+6, STRINGER 16R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 89,988 hrs · 67,850 cycles

FUSELAGE SKIN CRACKED, BETWEEN BS 877+15.5 TO 887+16.0, STRINGER 20R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 89,988 hrs · 67,850 cycles

SKIN CRACKED, BETWEEN BS 294.5+11.75 - 294.5+12.50, STRINGER 18R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 89,988 hrs · 67,850 cycles

SKIN CRACKED, BETWEEN BS 360+13.75" TO 360+14.25, STRINGER 19R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 89,988 hrs · 67,850 cycles

SKIN CRACKED AT BS 764, STRINGER 22R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 89,988 hrs · 67,850 cycles

SKIN CRACKED, BETWEEN BS 887+15.5 - 887+16.0, STRINGER 20R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 89,988 hrs · 67,850 cycles

SKIN CRACKED, BETWEEN BS 847+6 TO 846+7, STRINGER 20L. REPAIRED SKIN IAW WO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 89,988 hrs · 67,850 cycles

SKIN CRACKED AT BS 500+5, STRINGER 16R. REPAIRED SKIN IAW EA.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 89,988 hrs · 67,850 cycles

STRINGER SPLICE CRACKED AT BS 360, STRINGER 6R. REPAIRED SPLICE IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 89,988 hrs · 67,850 cycles

SKIN CRACKED AT BS 480+13, STRINGER 16L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 89,988 hrs · 67,850 cycles

SKIN CRACKED AT BS 908-1, BETWEEN STRINGER 6L - 7L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 89,988 hrs · 67,850 cycles

SKIN CRACKED, BETWEEN BS 400+17 - 400+18, STRINGER 1L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 89,988 hrs · 67,850 cycles

SKIN CRACKED AT BS 360+15, STRINGER 8L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 89,988 hrs · 67,850 cycles

SKIN CRACKED AT BS 360, STRINGER 6R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 89,988 hrs · 67,850 cycles

SKIN CRACKED AT BS 360+1, BETWEEN STRINGER 5R - 6R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 89,988 hrs · 67,850 cycles

SKIN CRACKED AT BS 500+14, STRINGER 8R. REPAIRED SKIN IAW EA.

Part: LENS — CRACKED (CABIN) · airframe 89,372 hrs · 67,393 cycles

FORWARD ENTRY DOOR, CABIN EMER LIGHT LENS CRACKED. R & R LIGHT ASSEMBLY IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 87,722 hrs · 66,195 cycles

FUSELAGE SKIN CRACKED AT BS 500B, BETWEEN STRINGER 15R TO 18R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 87,722 hrs · 66,195 cycles

FUSELAGE SKIN CRACKED AT BS 500+3, STRINGER 18R. REPAIRED SKIN IAW EA.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 87,722 hrs · 66,195 cycles

R2 DOOR EMER EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.

Part: ATTACH ANGLE — CRACKED (FLAP FAIRING) · airframe 87,712 hrs · 66,185 cycles

LEFT WING NR 3 FLAP TRACK FAIRING AFT OF FIRE BOX PANEL, OTBD ATTACH ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 87,712 hrs · 66,185 cycles

AFT CARGO COMPARTMENT SCUFF PLATE CRACKED ON UPPER SURFACE. REPAIRED SCUFF PLATE IAW EA.

Part: LIGHT — BROKEN (CABIN) · airframe 87,712 hrs · 66,185 cycles

R1 DOOR FWD EMER EXIT LIGHT BROKEN. R & R LIGHT IAW AMM.

Part: SPINDLE — CORRODED (TE FLAP) · airframe 87,712 hrs · 66,185 cycles

RIGHT WING TE OTBD FLAP, CARRIAGE SPINDLE CORRODED. R & R SPINDLE IAW MT.

Part: BEAM — CRACKED (FUSELAGE) · airframe 87,712 hrs · 66,185 cycles

RIGHT STUB BEAM LOWER CHORD CRACKED AT BS 639 FRAME. REPAIRED CHORD IAW EA.

Part: STRAP — BROKEN (FUSELAGE) · airframe 87,712 hrs · 66,185 cycles

FLOORBEAM STRAP BROKEN AT BS 328, BL 0. REPAIRED STRAP IAW SRM & DWG.

Part: FITTING — CRACKED (L1 DOOR) · airframe 87,712 hrs · 66,185 cycles

L1 DOOR ANGLE BRACKET CLIP CRACKED AT BS 294.5, STRINGER 10L. R & R CLIP IAW SRM & DWG.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 87,712 hrs · 66,185 cycles

LEFT CREASE BEAM WEB CRACKED BETWEEN BS 616 TO 639. R & R WEB IAW SRM & MM.

Part: SKIN — CRACKED (LE SLAT) · airframe 87,712 hrs · 66,185 cycles

LEFT WING NR 1 SLAT SKIN TOP SURFACE FROM LE & INBD END CRACKED AT FASTENER. REPAIRED SLAT SKIN IAW EA.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 87,712 hrs · 66,185 cycles

LEFT STUB BEAM CREASE BEAM WEB AT CRACKED BS 639. REPAIRED WEB IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 87,712 hrs · 66,185 cycles

FRAME OTBD CHORD FWD FLANGE CRACKED AT BS 727, STRINGER 18A, BOTH LOWER FASTENER LT & HOLES. REPAIRED CHORD IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 87,712 hrs · 66,185 cycles

FRAME OTBD CHORD FWD FLANGE CRACKED AT BS 727, STRINGER 18A AFT LOWER FASTENER RT HOLE. REPAIRED CHORD IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 87,189 hrs · 65,813 cycles

FUSELAGE SKIN CRACKED AT BS 440 + 12 STRINGER 16R. REPAIRED SKIN IAW SRM.

Part: SKIN — CHAFED (TE FLAP) · airframe 87,189 hrs · 65,813 cycles

LEFT WING INBD FORE FLAP CHAFED ON INBD UPPER SURFACE. REPAIRED FORE FLAP IAW SRM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 87,189 hrs · 65,813 cycles

L2 DOOR EMER EXIT SIGN INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 87,189 hrs · 65,813 cycles

FRAME CRACKED AT BS 727C STRINGER 25L. REPAIRED FRAME IAW EA .

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 87,189 hrs · 65,813 cycles

RIGHT MAIN WW PRESS DECK CRACKED AT BS 664, RBL 43. REPAIRED DECK IAW SRM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 87,189 hrs · 65,813 cycles

LEFT OVERWING EMER EXIT SIGN INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 86,272 hrs · 65,134 cycles

FUSELAGE SKIN CRACKED AT AFT CARGO DOOR AFT UPPER CORNER CUT OUT, STATION 848, BETWEEN STRINGERS 18R & 19R. REPAIRED SKIN IAW EA.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 85,924 hrs · 64,897 cycles

LEFT WING INBD TE AFT FLAP DELAMINATED ON LOWER SURFACE. R & R AFT FLAP IAW AMM.

Part: CABLE — MISROUTED (R2 DOOR) · airframe 85,139 hrs · 64,338 cycles

R2 DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE IAW MM.

Part: SKIN — CRACKED (LE SLAT) · airframe 84,715 hrs · 64,032 cycles

RT WING NR 4 SLAT INBD LOWER EDGE SKIN CRACKED. R & R NR 4 SLAT IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 84,715 hrs · 64,032 cycles

FUSELAGE SKIN CRACKED AT STATION 583, STRINGER 10L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 84,715 hrs · 64,032 cycles

FUSELAGE SKIN CRACKED AT STATION 500D+5, STRINGER 8R. REPAIRED SKIN IAW EA.

Part: PANEL — CRACKED (FUSELAGE) · airframe 84,715 hrs · 64,032 cycles

RT FUSELAGE FWD WING TO BODY AT LOWER EDGE CRACKED ON PANEL 3479R. REPAIRED PANEL IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 84,715 hrs · 64,032 cycles

FUSELAGE SKIN CRACKED AT STATION 500B+6, STRINGER 15L. REPAIRED SKIN IAW EA.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 84,642 hrs · 63,979 cycles

EMERGENCY LIGHT INOPERATIVE AFT OF LT HAND LOWER AFT WING TO BODY FAIRING. RELAMPED LIGHT IAW MM.

Part: LENS — MISSING (CABIN) · airframe 83,224 hrs · 62,905 cycles

R2 DOOR LOWER EMERGENCY EXIT LIGHT LENS MISSING. REMOVED AND REPLACED LENS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 82,960 hrs · 62,712 cycles

RIGHT EMERGENCY OVERWING LIGHTS INOP. RELAMPED LIGHTS IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 82,726 hrs · 62,538 cycles

FUSELAGE SKIN AT BS 480+16 CRACKED AT STR 17R. REPAIRED SKIN PER SRM AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 82,726 hrs · 62,538 cycles

FUSELAGE SKIN CRACKED AT STR 16R, BS 480 + 4". REPAIRED SKIN PER EA AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 82,726 hrs · 62,538 cycles

FUSELAGE SKIN CRACKED AT STR 16R CRACKED, BS 500D + 4". REPAIRED SKIN PER EA.

Part: LIGHT — LOOSE (CABIN) · airframe 82,696 hrs · 62,517 cycles

CEILING EMERGENCY EXIT LIGHT NOT SECURED, MID-CABIN. RE-SECURED CEILING EMERGENCY EXIT, MID-CABIN IAW M/M.

Part: O-RING — FAULTY (HYDRAULIC SYS) · airframe 82,518 hrs · 62,397 cycles

DIVERSION -- A HYDRAULIC SYSTEM LEAK. REPLACE O-RING ON NR 1 ENGINE PRESSURE LINE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 82,394 hrs · 62,305 cycles

EMERGENCY LIGHT INOP LOCATED AT BS 727 EXTERNAL FUSELAGE RIGHT SIDE. REMOVED & REPLACED EMERGENCY LIGHT LOCATED AT BS 727 EXTERNAL FUSELAGE RIGHT SIDE AS PER AMM 33-51-22-962-001 & PERFORMED TEST IS OK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 82,394 hrs · 62,305 cycles

EMERGENCY EXIT LIGHT IN BULL NOSE INOP AT ROW 13 ABC. REMOVED AND REPLACED EMERGENCY EXIT LIGHT AT ROW 13 ABC IAW AMM 33-51-42-962-001, AND PERFORMED TEST IS OK.

Part: STRUCTURE — CRACKED (LE SLAT) · airframe 82,394 hrs · 62,305 cycles

CRACK IN I/B SLAT CAN OF SLAT NR 1. REPLACED I/B SLAT CAN OF SLAT NR 1 IAW DRAWING 65-45320 AND SRM B737-300 51-10-02 PARAGRAPH 8.

Part: STIFFENER — CRACKED (NR 2 PYLON) · airframe 82,394 hrs · 62,305 cycles

CRACK ON STIFFENER LOCATED ON AFT STRUT FAIRING ENGINE NR 2. REPLACED STIFFENER LOCATED ON AFT STRUT FAIRING ENGINE NR 2 IAW SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CORROSION ON STRINGER SPLICE LOC BETWEEN BS 360 AND STR 26R E/E COMPARTMENT. REPLACED STRINGER SPLICE AND FASTENERS LOCATED BS 360 AND STR 26R E/E COMPARTMENT IAW B737-300 SRM 51-10-02, ITEM 8 AND SRM 51-40-02 AND DRAWING

Part: STRINGER — CRACKED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CRACK ON STRINGER 24R FASTENERS HOLE LOCATED BETWEEN BS 887 TO BS 907 AFT CARGO COMPARTMENT 3EA LOCATION. REPAIRED STRINGER SECTION PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

STRINGER CORRODED BETWEEN BS 360 TO BS 380, STR 26R. REMOVED AND REPLACED STRINGER IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CRACK ON WEB LOCATED BETWEEEN BS 400 TO BS 420 AND STR 26L FWD CARGO COMPARTMENT. REPLACED WEB LOCATED BETWEEN BS 400 TO BS 420 AND STR 26L FWD CARGO COMPARTMENT IAW SRM B737-300 51-10-02 ITEM 8 SRM B737-300 51-40-02 AND DRAWING #69-41473.

Part: WEB — CRACKED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CRACK ON WEB LOCATED BETWEEN BETWEEN BS 460 TO BS 480 AND STR 26L FWD CARGO COMPARTMENT. REPLACED WEB LOCATED BETWEEN BS 460 TO BS 480 AND S-26L FWD CARGO COMPARTMENT IAW SRM B737-300 51-10-02 ITEM 8 SRM B737-300 51-40-02 AND DRAWING 69-41473.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CRACK ON ANGLE BSTA 927 STR 20R AFT CARGO COMP. PERFORMED REPAIR ON ANGLE LOCATED BETWEEN BS 907+16" TO BS 947.5, STR 20R AFT CARGO COMPARTMENT IAW SRM B737-300, 51-70-11.

Part: SKIN — CRACKED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

SKIN CRACKED AT BS 887+13.5, STR 25R. REPAIRED SKIN IAW SRM.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CORROSION ON BS 1016 BULKHEAD DOME WEBS LOCATED BETWEEN LBL 3 AND RBL 3 AT WL 189. PERFORMED REPAIR ON BS 1016 BULKHEAD DOME WEB LOC BETWEEN RBL 7 TO LBL 7 WL 189 IAW ACO#7360-53 AND DWG 65C28106.

Part: STRINGER — CRACKED (RT WING) · airframe 82,394 hrs · 62,305 cycles

CRACK ON STRINGER 8 UPPER SURFACE AND WS 479.00 FUEL TANK RT/WING L=1.5" APPROX (S-8R). PERFORMED REPAIR ON STRINGER 8 UPPER PANEL STRINGER LOCATED WS 479.00 IAW EA 1-357-7804 REV 0 AND EO AEM-HC57-297/12 RO.

Part: FLAP — DELAMINATED (LT WING) · airframe 82,394 hrs · 62,305 cycles

DELAMINATION ON LEFT FORE FLAP O/B (OUTBOARD AREA). REPAIRED LEFT FORE FLAP O/B (OUTBOARD AREA) IAW B737-300 SRM 51-40-10-2R-0.

Part: BRACKET — CRACKED (FLAP FAIRING) · airframe 82,394 hrs · 62,305 cycles

RIGHT WING NR 6 FLAP TRACK FAIRING BRACKET CRACKED. REMOVED AND REPLACED BRACKET IAW SRM AND DRAWING.

Part: SKIN — CRACKED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

SKIN CRACKED AT BS 907+14, STR 25R. REPLACED SKIN IAW SRM AND DRAWING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

FRAME WEB CRACKED AT BS 440, STR 16R. REMOVED AND REPLACED WEB IAW EO AND EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

FRAME CRACKED AT BS 947.5, STR 19R. REMOVED AND REPLACED FRAME IAW EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CRACK ON TIE CLIP LOCATED AT BS 663.75 AND STR 10L IN PAX CABIN. REPLACED TIE CLIP LOCATED AT BS 663.75 AND STR 10L IN PAX CABIN IAW SRM B737-300 51-10-02-0G-0 PAGE 8, PARAGRAPH 8 AND SRM 51-40-02 AND DRAWING 65-46541.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CORROSION ON STRINGER 28R BETWEEN BS 294.5 AND BS 312 E/E COMPARTMENT. REPLACED STRINGER 28R BETWEEN BS 294.5 AND BS 312 E/E COMPARTMENT IAW B737-300 SRM 51-10-02 B737-300 SRM 51-40-02 AND DRAWING 65-45800.

Part: ROLLER — WORN (TE FLAP) · airframe 82,394 hrs · 62,305 cycles

WEAR ON ROLLER LOC INTERNAL AREA OF FORE FLAP TRACK OF MIDFLAP O/B LEFT (6E/A). REPLACED ROLLER LOC INTERNAL AREA OF FORE FLAP TRACK OF MID FLAP O/B LEFT (6E/A) IAW SOPM 20-50-03 AND HARDWARE

Part: SKIN — CRACKED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CRACK ON EXTERNAL SKIN AT BS 927+15 AND STR 21R LOWER LOBE FUSELAGE. REPLACED SKIN IAW SRM AND DRAWING.

Part: SKIN — CRACKED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CRACK ON EXTERNAL SKIN AT BS 927+14 AND STR 22R LOWER LOBE FUSELAGE. REPLACED SKIN IAW SRM AND DRAWING.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CRACK ON TIE CLIP AT THE PAX CABIN STRUCTURE BS 706 STR 10R. REMOVED AND REPLACED TIE CLIP IAW SRM AND DRAWING.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CRACK ON TIE CLIP AT THE PAX CABIN STRUCTURE BS 706 STRINGER 1. REPLACED TIE CLIP AT THE PAX CABIN STRUCTURE BS 706 STRINGER 1 IAW SRM B737-300 51-10-02 ITEM 8 AND INSTALLED FASTENERS IAW SRM B737-300 51-40-02 AND DRAWING 65-49902.

Part: SKIN — CRACKED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CRACK ON EXTERNAL SKIN FUSELAGE AT BS 967+4 AND ABOVE STR 23L. REPAIRED SKIN IAW EA AND EO.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CRACK ON ATTACH CLIP COMMON TO THE BS 348.2 FRAME AND S-15L. REPLACED ATTACH CLIP COMMON TO THE BS 348.2 FRAME AND S-15L IAW B737-300 SRM 51-10-02-0G-0 ITEM 8 B737-300 SRM 51-40-02-0G-0 AND DRAWING 65-17685

Part: FITTING — CRACKED (HORIZ STAB) · airframe 82,394 hrs · 62,305 cycles

CRACK ON FITTING LOCATED BS 1118 LBL 10 HORIZONTAL STABILIZER CENTER SECTION UPPER POSITION. REPLACED FITTING LOCATED BS 1118 LBL 10 HORIZONTAL STABILIZER CENTER SECTION UPPER POSITION IAW SRM B737-300 51-40-02 AND DWG 65-47598.

Part: SUPPORT ANGLE — CRACKED (LT PYLON) · airframe 82,394 hrs · 62,305 cycles

CRACK ON SUPPORT ANGLE LOC ON AFT POSITION PYLON STRUT I/B SIDE ENGINE 1. REPLACED SUPPORT ANGLE LOC ON AFT POSITION PYLON STRUT I/B SIDE ENGINE 1 IAW B737-300 SRM 51-10-02 ITEM 8 PAGE 8 DWG #313A1380 AND SRM B737-300 51-40-02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CRACK ON FRAME WEB AT BS 727C AT STR 14R. REPAIRED WEB IAW EA AND EO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CRACK ON RADIAL WEB SPLICE HIDDEN ROW OF FASTENERS AT BULKHEAD BS 1016 STR 15R. REPAIRED WEB IAW EA AND EO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CRACK ON RADIAL WEB SPLICE HIDDEN ROW OF FASTENERS AT BULKHEAD BS 1016 STR 15R. REPAIRED WEB IAW EA AND EO.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CORROSION ON STRINGER 23R BETWEEN BS 259.7 AND BS 294.5 NOSE COMPARTMENT. REPAIRED STRINGER 23R BETWEEN BS 294.5+2" TO BS 294.5+15" IAW B737-300 SRM 53-00-03-2R, REPAIR 1, DETAIL VI.

Part: FRAME — CRACKED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CRACK ON FRAME AT BSTA 320 STR E/E COMPARTMENT. REPLACED FRAME AT BS 320 STR 18L/20L E/E COMPARTMENT IAW SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CRACK ON RADIAL WEB SPLICE HIDDEN ROW OF FASTENERS AT BULKHEAD BS 1016 BL 0. REPAIR WEB IAW EA AND EO.

Part: FRAME — CORRODED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CORROSION ON FRAME BETWEEN S-27L AND S-26L AT BS 360 E/E COMPARTMENT. PERFORMED REPAIR ON FRAME LOCATED BETWEEN S-27L AND S-26L AT BS 360 E/E COMPARTMENT IAW SRM B737-300 53-00-07 REPAIR 7 DETAIL II TABLE 1.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CORROSION ON STRINGER 26L BETWEEN BS 344 AND BS 351.2+4" E/E COMPARTMENT. REPAIRED STRINGER 26L BETWEEN BS 330 TO BS 360 IAW SRM B737-300 53-00-03-2R-1 REPAIR 1 DETAIL VII.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CRACK ON RADIAL WEB SPLICE HIDDEN ROW OF FASTENERS AT BULKHEAD BS 1016 STR 15R. REPAIRED WEB IAW EA AND EO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CRACK ON RADIAL WEB SPLICE HIDDEN ROW OF FASTENERS AT BULKHEAD BS 1016 BL 0. REPAIRED WEB IAW EA AND EO.

Part: WEB — CRACKED (NLG WW) · airframe 82,394 hrs · 62,305 cycles

CRACK AT RIGHT SIDE OF THE NLG W/W AROUND FASTENER HEAD AT WL 169.1 AND BS 233.7+1. REPAIRED WEB IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CRACK ON TIE CLIP LOCATED BS 827 AT STR 16R IN AFT PAX CABIN. REPLACED TIE CLIP LOCATED BS 827 AT STR 16R IN AFT PAX CABIN IAW B737-300 SRM 51-40-02, SRM 51-10-02 ITEM 8 AND DWG 65-46552.

Part: FITTING — CRACKED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CRACK ON CLIP LOCATED BS 767 AT STR 16R IN AFT PAX CABIN. REPLACED TIE LOCATED BS 767 AT STR 16R IN AFT PAX CABIN IAW B737-300 SRM 51-40-02 SRM 51-10-02 ITEM 8 AND DWG 65-46549.

Part: FRAME — CORRODED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CORROSION ON FRAME LOCATED BETWEEN S-27R AND S-28R AT BS 380 E/E COMPARTMENT. PERFORMED REPAIR ON FRAME LOCATED BETWEEN S-27R AND S-28R AT BS 380 E/E COMPARTMENT IAW SRM B737-300, 53-00-07 REPAIR 4 DETAIL II.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CRACK ON RADIAL WEB SPLICE HIDDEN ROW OF FASTENERS AT BULKHEAD BS 1016 STR 15R. REPAIRED WEB IAW EA AND EO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CRACK ON RADIAL WEB SPLICE HIDDEN ROW OF FASTENERS AT BULKHEAD BS 1016 STR 15R. REPAIRED WEB IAW EA.

Part: COMPOUND — CRACKED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CRACK ON LEVELING COMPOUND LOC BETWEEN BS 203.8 AND BS 227.8 LOWER LOBE FUSELAGE. REPLACED LEVELING COMPOUND LOC BETWEEN BS 203.8 AND BS 227.8 LOWER LOBE FUSELAGE IAW B737-300 AMM 51-41-11-538-009.

Part: SKIN — CRACKED (RT WING) · airframe 82,394 hrs · 62,305 cycles

CRACK ON EXTERNAL SKIN AT LEADING RIGHT WING WBL 254.00. REPAIRED EXTERNAL SKIN AT LEADING EDGE R/T WING WBL 254.00 IAW B737-300 SRM 51-70-16-0G-0.

Part: BOLT — WORN (LE SLAT) · airframe 82,394 hrs · 62,305 cycles

WEAR ON BOLT OF SUPPORT FITTING OF THE SLAT ACTUATOR NR 4. REMOVED AND REPLACED BOLT OF SUPPORT FITTING OF THE SLAT ACTUATOR NR 4 AS PER AMM 27-81-41-404-056 STEP 3E(7)(A) THRU 3E(7)(C).

Part: STRINGER — CORRODED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CORROSION ON STRINGER 28R BETWEEN BS 360 AND BS 380 E/E COMPARTMENT. REPAIRED STRINGER 28R BETWEEN BS 360 TO BS 400 IAW B737-300 SRM 53-00-03 REPAIR 1 FIGURE 201 SHEET 8 DETAIL VII.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CRACK ON RADIAL WEB SPLICE HIDDEN ROW OF FASTENERS AT BULKHEAD BS 1016 BL 0. REPAIRED SPLICE IAW EA AND EO.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CORROSION ON STRINGER 24L BETWEEN BS 294.5 AND BS 312 E/E COMPARTMENT. REPAIRED STRINGER 24L BETWEEN BS 294.5 TO BS 325 E/E COMPARTMENT IAW SRM B737-300 53-00-03-2R-1 REPAIR 1 DETAIL VI.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CORROSION ON STRINGER 25R BETWEEN BS 312 AND BS 328 E/E COMPARTMENT. REPAIRED STRINGER 25R BETWEEN BS 312 TO BS 328 E/E COMPARTMENT IAW SRM B737-300 53-00-03-2R-1 REPAIR 1 DETAIL V.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

A CRACK ON SPLICE STRINGER LOCATED AT BS 360 AND STRINGER 4L IN PAX CABIN. REPLACED SPLICE STRINGER LOCATED AT BS 360 AND S-4L IN PAX CABIN IAW EA N.1-353-21257 REV 0 AND EO N.AEM-HC53-553/12 R0

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

F-38A CRACK ON SPLICE STR AT BS 360 AND STR 7L IN PAX CABIN. REPLACED SPLICE IAW SRM AND EO.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CRACK SUPPORT ANGLE AT BS 320 BETWEEN S20L AND 21L IN E/E COMPARTMENT. REPLACED ANGLE IAW SRM AND DRAWING.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CRACK ON SUPPORT ANGLE OF J 10-BOX LOCATED AT BS 380 AND LEVEL OF S-20L. REPLACED SUPPORT ANGLE OF J10-BOX. LOCATED AT BS 380 AND LEVEL OF S-20L IAW B737-300 SRM 21-40-02 51-10-02 ITEM 8 AND DRAWING 65-58146.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CRACK ON THE CLIP LOCATED AT BS 380 AND S-22L IN E/E COMPARTMENT. REPLACED TIE CLIP LOCATED AT BS 380 AND S-22L IN E/E COMPARTMENT IAW SRM B737-300 51-10-02 ITEM 8. INSTALLED FASTENERS IAW SRM B737-300 51-40-02 AND DRAWING 65-46525.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CRACK ON SUPPORT ANGLE LOCATED AT BS 344 BETWEEN S-20L AND S-21L IN E/E COMPARTMENT. REPLACED SUPPORT ANGLE LOCATED AT BS 344 BETWEEN S-20L AND S-21L IN E/E COMPARTMENT IAW B737-300 SRM 51-40-02 B737-300 SRM 51-10-02 AND DRAWING 65-54892.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CRACK ON SUPPORT ANGLE LOCATED AT BS 328 BETWEEN S-20L AND S-21L IN E/E COMPARTMENT. REPLACED SUPPORT ANGLE LOCATED AT BS 328 BETWEEN S-20L AND S-21L IN E/E COMPARTMENT IAW B737-300 SRM 51-40-02 SRM 51-10-02 AND DRAWING 65-54892.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CORROSION ON STRINGER 23L BETWEEN BS 344 AND 351.2 IN E/E COMPARTMENT. REPAIRED STRINGER 23L BETWEEN BS 330 TO BS 360 E/E COMPARTMENT IAW SRM B737-300 53-00-03-2R-1 REPAIR 1 DETAIL VII.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CORROSION ON SHEAR TIE BETWEEN S-27L AND S-28L AT BS 312 IN E/E COMPARTMENT. REPLACED HEAR TIE AND FASTENERS BETWEEN S-27L AND S-28L AT BS 312 IN E/E COMPARTMENT IAW B737-300 SRM 51-40-02 51-10-02 ITEM 8 AND DRAWING # 65-45810.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CORROSION ON STRINGER 25L BETWEEN BS 294.5 AND BS 344+2" IN E/E COMPARTMENT. REPAIRED STRINGER 25L BETWEEN BS 294.5 TO BS 325 E/E COMPARTMENT IAW SRM B737-300 53-00-03-2R-1 REPAIR 1 DETAIL VI.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CORROSION ON FLOORBEAM LOCATED AT BS 986.5 AND BETWEEN RBL 45 TO LBL 45 GALLEY AREA FLOOR STRUCTURE. REPAIRED FLOORBEAM IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CRACK ON TIE CLIP LOCATED AT BS 360 AND STR 5L FWD PAX CABIN. REPLACED TIE CLIP LOCATED AT BS 360 AND STR 5L FWD PAX CABIN IAW SRM B737-300 51-10-02 PART 8 AND DRAIWNG 58280.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CRACK ON UPPER CHORD OF FLOORBEAM LOCATED AT BS 328 AND LBL 28 APPROX FLOOR STRUCTURE FWD PAX CABIN. REPAIRED UPPER CHORD OF FLOORBEAM LOC AT BS 328 AND LBL 28 APPROX FLOOR STRUCTURE FWD PAX CABIN IAW SRM B737-300 53-10-51.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CRACK ON ANGLE AT THE MAIN DECK FLOOR STRUCTURE BETWEEN BS 927 AND BS 947.5, BBL 0. REPLACED ANGLE AND FASTENERS LOC AT THE MAIN DECK FLOOR STRUCTURE BETWEEN BS 927 AND BS 947.5 BBL 0 IAW B737-300 SRM 51-40-02 AND DRAWING 69-36656.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CRACK ON ANGLE LOCATED BETWEEN BS 277 TO BS 291 BETWEEN STR 11R TO 10R FWD GALLEY DOOR CUTOUT. REPLACED ANGLE LOCATED BETWEEN BS 277 TO BS 291 BETWEEN STR 11R TO STR 10R FWD GALLEY DOOR CUTOUT IAW SRM B737-300 51-10-02, 51-40-02 AND DRAWING 65-45807.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CRACK VERTICAL ANGLE AT FLOORBEAM BS 328 AND LBL 45.6. REPLACED ANGLE CABIN IAW SRM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CRACK ON ANGLE LOCATED BETWEEN BS 277 TO BS 291 BETWEEN STR 9R TO STR 10R FWD GALLEY DOOR CUTOUT. REPLACED ANGLE LOCATED BETWEEN BS 277 TO BS 291 BETWEEN S-9R TO S-10R FWD GALLEY DOOR CUTOUT IAW SRM B737-300 51-10-02 51-40-02 AND DRAWING 65-45807.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CRACK ON ANGLE LOCATED BS 328 RBL 30 APPROX IN PAX CABIN FLOOR STRUCTURE. REPLACED ANGLE LOC BS 328 RBL 30 APPROX IN PAX CABIN FLOOR STRUCTURE IAW B737-300 SRM 51-10-02 ITEM 8 B737-300 SRM 51-40-02 AND DRAWING 65-45812.

Part: ANGLE — CRACKED (NR 1 PYLON) · airframe 82,394 hrs · 62,305 cycles

CRACK LOWER ANGLE AT ACCESS PANEL 5743L ON STRUT FAIRING ENGINE 1. REPLACED ANGLE IAW SRM DRAWING.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CORROSION ON INTERCOSTAL AT BS 1006 TO 1016 LBL 6 GALLEY AREA FLOOR STRUCTURE. REPLACED INTERCOSTAL IAW SRM AND DRAWING.

Part: ANGLE — CRACKED (NR 2 PYLON) · airframe 82,394 hrs · 62,305 cycles

CRACK ON LOWER ANGLE AT ACCESS PANEL 5843R STRUT FAIRING ENGINE 2. REPLACED ANGLE IAW SRM AND DRAWING.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CRACK ON STR CHANNEL AT STR 7L AND BS 360 PAX CABIN. REPLACED CHANNEL IAW SRM AND EO.

Part: PLATE — CRACKED (LT WING) · airframe 82,394 hrs · 62,305 cycles

CRACK MAIN TRACK COVER PLATE INBOARD SIDE OF SLAT NR 2 LEFT WING. REPLACED MAIN TRACK COVER PLATE INBOARD SIDE OF SLAT NR 2 LEFT WING IAW DRAWING AND CMM

Part: STRAP — CRACKED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CRACK ON H-STRAP LOCATED BETWEEN BS 294.5 TO BS 312 AND STR 10L FWD PAX CABIN. REPLACED H-STRAP LOC BETWEEN BS 294.5 TO BS 312 AND STR 10L FWD PAX CABIN IAW B737-300 SRM 51-40-02 AND 51-10-02 ITEM 8 AND DRAWING 65-17684.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CRACK ON STRINGER CHANNEL LOCATED AT STRINGER 4L AND BS 360 IN FWD PAX CABIN. REPLACED SPLICE STRINGER LOCATED AT BS 360 AND S-4L IN PAX CABIN IAW EA N.1-353-21257 REV 0 AND EO N.AEM-HC53-553/12.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CRACK ON INTERCOSTAL WEB AT BS 294.5 TO 303.9 AT STR 7L INTERNAL AREA ENTRY DOOR. REMOVED AND REPLACED WEB IAW SRM AND DRAWING.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CRACK TIE CLIP IN CARGO COMPARTMENT AT BS 787 STR 21R. REPLACED TIE CLIP IAW SRM AND DRAWING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CRACK ON ANGLE LOCATED AT BS 312 AND STR 2L CROW AREA FWD PAX CABIN. REPLACED ANGLE AND FASTENERS LOCATED AT BS 312 AND STR 2L CROWN AREA FWD PAX CABIN IAW B737-300 SRM 51-40-02 AND DRAWING 65-54487.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CRACK ON ANGLE LOCATED BETWEEN BS 277 TO BS 291 AT LEVEL STR 13R FWD GALLEY DOOR CUTOUT. REPLACED ANGLE LOCATED BETWEEN BS 277 TO BS 291 AT LEVEL STR 13R FWD GALLEY DOOR CUTOUT IAW B737-300 SRM 51-10-02 ITEM 8 AND SRM 51-40-02 AND DRAWING #65-45807.

Part: SKIN — CRACKED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CRACK EXTERNAL SKIN AT GALLEY DOOR UPPER CORNER CRACK L 0.35. REMOVED AND REPLACED FUSELAGE SKIN AND BEAR STRAP IAW EO.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CRACK ON TIE CLIP IN THE AFT CARGO COMPARTMENT AT BS 787, STR 20R. REPLACED TIE CLIP IN THE AFT CARGO COMPARTMENT AT BS 787 STR 20R IAW B737-300 SRM 51-10-02-0G-0 ITEM 8, B737-300 SRM 51-40-02-0G-0 AND DRAWING 65-46550 DUE TO CRACK IS NOT PERM

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CRACK ON SUPPORT IN CARGO COMPARTMENT AT BS 727 BULKHEAD STRUCTURE BBL 0. REPLACED SUPPORT FITTING IAW SRM AND DRAWING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CRACK ANGLE AT BS 348.2 AT STR 15L ENTRY DOOR CUTOUT. REMOVED AND REPLACED ANGLE IAW AND DRAWING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CRACK STUB FRAME AT BS 294.5 STR 7R GALLEY DOOR. REPLACED FRAME IAW SRM AND DWG.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CRACK ON BRACKET LOCATED BS 1016 RBL 7 AT LEVEL S-6R AFT PAX CABIN. REPLACED BRACKET LOCATED BS 1016 RBL 7 AT LEVEL S-6R AFT PAX CABIN IAW SRM B737-300 51-10-02, 51-40-02 AND DRAWING 65C20808.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CRACK TIE CLIP AT CARGO COMPARTMENT BS 787 STR 22R. REPLACED TIE CLIP IAW SRM AND DRAWING.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CRACK TIE CLIP IN CARGO COMPARTMENT AT BS 787 STR 20R. REPLACED TIE CLIP IAW SRM AND DRAWING.

Part: SKIN — CRACKED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CRACK ON ENTRY DOOR UPPER CORNER OF ENTRY DOOR L 0.26. REMOVED AND REPLACED SKIN IAW SRM.

Part: ANGLE — CRACKED (FLAP TRACK) · airframe 82,394 hrs · 62,305 cycles

CRACK ANGLE AT I/B FLAP TRACK FAIRING 3 LEFT WING. REMOVED AND REPLACED ANGLE IAW SRM AND DRAWING.

Part: SKIN — CRACKED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CRACK ON FUSELAGE SKIN COMMON TO THE AFT ENTRY DOOR CUTOUT, STA 986.5+2" AND BETWEEN S-7L TO S-8L. PERFORMED REPAIR PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CRACK ON AFT UPPER CUT OUT CORNER OF AFT GALLEY DOOR. PERFORMED REPAIR PER SRM.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 82,394 hrs · 62,305 cycles

CRACK ANGLE AT O/B OF FLAP TRACK FAIRING 3 LEFT WING. REMOVED AND REPLACED ANGLE IAW SRM AND DRAWING.

Part: SUPPORT ANGLE — CRACKED (TE FLAP) · airframe 82,394 hrs · 62,305 cycles

CRACK ANGLE AT INTERNAL AREA I/B OF FLAP TRACK FAIRING 3 LEFT WING. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: TIE CLIP — CORRODED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CORROSION ON TIE CLIP IN THE AFT CARGO COMPARTMENT AT BS 794.3, STRINGER 26R. REPLACED TIE CLIP LOC AFT CARGO COMPARTMENT AT BS 794.3 S-26R IAW B737-300 SRM 51-10-02 ITEM 8 SRM 51-40-02 AND DRAWING 65-47959.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CORROSION ON INBOARD AND OUTBOARD SIDE OF STRINGER 25L IN THE AFT CARGO COMPARTMENT BETWEEN BS 967 AND BS 986.5. REPLACED STRINGER IAW B737-300 SRM 51-10-02 AND DRAWING AND INSTALLED FASTENERS IAW B737 SRM 51-40-02.

Part: SKIN — CRACKED (KRUEGER FLAP) · airframe 82,394 hrs · 62,305 cycles

CRACK ON KRUEGER FLAP SKIN LOCATED AT LEVEL LES 213 LEFT WING. PERFORMED REPAIR ON FIXED LEADING EDGE SKIN AT THE KRUEGER FLAP SEAL DOOR CUTOUT AT LES 213 LEFT WING IAW EA 1-A57-0503 REV 4.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CORROSION ON TIE CLIP IN THE AFT CARGO COMPARTMENT AT BS 807, STRINGER 26R. REPLACED TIE CLIP LOC IN THE AFT CARGO COMPARTMENT AT BS 807, STRINGER 26R IAW B737-300 SRM 51-40-02 AND B737-300 51-10-02 ITEM 8 DWG

Part: FRAME — CORRODED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CORROSION FACE OF FRAME IN THE CARGO COMPARTMENT AT BS 787 BETWEEN STR 26R AND 27R. REPAIRED FRAME IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CRACK ON LONGITUDINAL FLOORBEAM WEB AT LBL 24.5 AND BS 712.5 IN CENTER WING BOX. REPAIRED WEB PER SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CORROSION ON WEB IN THE AFT CARGO COMPARTMENT BETWEEN BS 807 AND BS 827 STRINGER 27R. REPLACED WEB IN THE AFT CARGO COMPARTMENT BETWEEN BS 807 AND BS 827 STRINGER 27R IAW B737-300 SRM 51-10-02 AND DRAWING 65-47958.

Part: FRAME — CORRODED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CORROSION ON FWD AND AFT FACE OF FRAME IN THE AFT CARGO COMPARTMENT AT BS 787 BETWEEN STR 27L AND STR 27R. REPAIRED FRME IN THE AFT CARGO COMPARTMENT AT BS 787 BETWEEN STR 27L AND STR 27R IAW B737-300 SRM 53-00-07-2R-3 REPAIR 3 DUE TO REMOVED

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CRACK ON LONGITUDINAL FLOORBEAM WEB AT LBL 24.5 AND BS 707.5 IN CENTER WING BOX. REPAIRED WEB PER EA AND EO.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CORROSION ON ANGLE IN THE AFT CARGO COMPARTMENT AT BS 787, STRINGER 27R. REPLACED ANGLE IN THE AFT CARGO COMPARTMENT AT BS 787, STRINGER 27R IAW SRM B737-300 51-10-02, 51-40-02 AND DRAWING #69-43238

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CRACK ON LONGITUDINAL FLOORBEAM WEB AT RBL 24.5 AND BS 707.5 IN CENTER WING BOX. REPAIRED WEB IAW EA AND EO.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CRACK ON LONGITUDINAL FLOORBEAM WEB AT LBL 24.5 AND BS 715 IN CENTER WING BOX. REPAIRED WEB EA AND EO.

Part: POST — CRACKED (COCKPIT) · airframe 82,394 hrs · 62,305 cycles

CRACK ON RIVETS HEAD (2EA) LOCATED ON BS211.8 AND AT LEVEL STR 9L WINDOW POST LT SIDE. REPLACED FASTENERS (2 EA) LOCATED ON BS 211.8 AND AT LEVEL STR 9L WINDOW POST LT SIDE IAW SRM B737-300 51-40-02 AND DRAWING 65-45800.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CORROSION ON STRINGER 26L LOCATED AT BS 500A+16" FWD CARGO COMPARTMENT. REPAIRED STRINGER 26L LOCATED AT BS 500A+16" FWD CARGO COMPARTMENT IAW SRM B737-300 53-00-03-2R-1 (FROM BSTA 500A TO BSTA 500C+12").

Part: STRINGER — CORRODED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CORROSION ON STR 26R LOCATED BETWEEN BS 500 TO BS 500A FWD CARGO COMPARTMENT. REPAIRED STR 26R LOCATED BETWEEN BS 500 TO BS 500A +19" FWD CARGO COMPARTMENT IAW B737-300 SRM 53-00-03-2R-1 REPAIR 1 DETAIL VII.

Part: BEAM — CORRODED (RT HORIZ STAB) · airframe 82,394 hrs · 62,305 cycles

CORROSION ON UPPER BEAM LOCATED AT HORIZONTAL STAB RIGHT AND STAB STA 92.70 APPROX REAR SPAR. REPAIRED UPPER T/E BEAM LOCATED AT HORIZONTAL STAB RIGHT AND STAB STA 92.70 APPROX REAR SPAR IAW B737-300 SRM 55-10-13-2R-3 REPAIR 3 DETAIL II.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CORROSION ON STRINGER SPLICE LOCATED AT BS 540 AND S-27R IN AIR CONDITIONING DISTRIBUTION BAY. REPLACED STRINGER SPLICE LOCATED AT BS 540 S-27R IN AIR CONDITIONING DISTRIBUTION BAY IAW SRM B737-300 51-40-02, 51-10-02 AND DRAWING 65-45769.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CORROSION ON FRAME LOCATED AT BS 500B AND BETWEEN STR 28R TO 27R CARGO COMPARTMENT. REPAIRED SHEAR TIE IAW SRM.

Part: BRACKET — DAMAGED (CABIN) · airframe 82,394 hrs · 62,305 cycles

DAMAGE ON HARDWARE PLATE ASSY ADAPTER AT AFT GALLEY DOOR GIRT BAR FLOOR BRACKET. REPLACED HARDWARE ASSY AT AFT GALLEY DOOR GIRT BAR FLOOR BRACKET IAW AMM 25-61-51.

Part: FRAME — CORRODED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CORROSION ON FACE OF FRAME AT BS 500B AND BETWEEN STR 26L TO 27L CARGO COMPARTMENT. REPAIRED FRAME IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CRACK TIE CLIP LOCATED AT BS 440 AT LEVEL STR 28L CARGO COMPARTMENT. REPLACED TIE CLIP IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CORROSION ON FRAME LOCATED AT BS 500B AND BETWEEN STR 28R TO 27R CARGO COMPARTMENT. REPAIRED SHEAR TIE IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CRACK ON TIE CLIP LOCATED AT BS 500C AND S-28R IN FWD CARGO COMPARTMENT. REPLACED TIE CLIP LOC, AT BS 500C AND STR 28R IN FWD CARGO COMPARTMENT IAW B737-300 SRM 51-10-02 ITEM 8 AND B737-300 SRM 51-40-02 DRAWING 65C22909.

Part: WEB — CRACKED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CRACK ON WEB LOCATED BETWEEN BS 500B TO BS 500C AND S-26R FWD CARGO COMPARTMENT. REPLACED WEB LOCATED BETWEEN BS 500B TO BS 500C AND S-26R FWD CARGO COMPARTMENT IAW SRM B737-300 51-10-02 ITEM 8 AND SRM B737-300 51-40-02, DRAWING 69-41473.

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CRACK ON SCUFF PLATE LOCATED ON AFT LOWER CORNER OF AFT CARGO COMPARTMENT DOOR CUTOUT. SCUFF PLATE AFT CORNER OF AFT CARGO COMPARTMENT REPAIRED BY WELDS IN ACCORDANCE WITH EA 1-A53-2076 REV 10 (SCUFF PLATE AFT LOWER CONER).

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CRACK ON SCUFF PLATE LOCATED ON FWD LOWER CORNER OF AFT CARGO COMPARTMENT DOOR CUTOUT. SCUFF PLATE FWD CORNER OF AFT CARGO COMPARTMENT REPAIRED BY WELDS IN ACCORDANCE WITH EA 1-A53-2076 REV 10 (SCUFF PLATE FWD LOWER CORNER).

Part: FRAME — CORRODED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CORROSION ON FRAME LOCATED BS 500A BETWEEN S-25L TO S-26L FWD CARGO COMPARTMENT. PERFORMED REPAIR ON FRAME LOCATED BS 500A BETWEEN S-25L TO S-26L FWD CARGO COMPARTMENT IAW B737-300 SRM 53-00-07-2R-5.

Part: WEB — CRACKED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CRACK ON WEB LOCATED BETWEEN BS 500A TO 500B AND S-26L CARGO COMPARTMENT. REPLACED WEB IAW SRM DRAWING.

Part: SKIN — CRACKED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CRACK ON EXTERNAL SKIN LOCATED AT BS 420+13.5" AND STR 16R UPPER LOBE FUSELAGE. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CRACK ON FUSELAGE SKIN AT BS 420+7 ABOVE S-26L LOWER LOBE L=0.80. REPAIR FUSELAGE SKIN IAW EA EO.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CRACK ON TIE CLIP LOCATED BS 400 AND S-22R FWD CARGO COMPARTMENT. REPLACED TIE CLIP LOCATED BS 400 AND TSR 22R IN FWD CARGO COMPARTMENT IAW B737-300 SRM 51-10-02 ITEM 8, DRAWING 65-46526 AND B737-300 SRM 51-40-02.

Part: SKIN — CRACKED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CRACK ON EXTERNAL SKIN LOCATED AT BS 420+6" AND STR 16R UPPER LOBE FUSELAGE. REPAIRED EXTERNAL SKIN LOCATED BETWEEN BS 416 TO BS 453 AND STR 14R TO STR 17R UPPER LOBE FUSELAGE IAW SRM B737-300 53-00-01-2R-31.

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CRACK ON SCUFF PLATE LOCATED ON AFT LOWER CORNER OF FWD CARGO COMPARTMENT DOOR CUT OUT. SCUFF PLATE AFT CORNER OF FWD CARGO COMPARTMENT REPAIRED BY WELDS IN ACCORDANCE WITH EA 1-A53-2076 REV 10 (SCUFF PLATE AFT LOWER CORNER).

Part: FRAME — CORRODED (FUSELAGE) · airframe 82,394 hrs · 62,305 cycles

CORROSION ON FRAME LOCATED BS 500B BETWEEN S-25L TO S-26L CARGO COMPARTMENT. REPAIRED FRAME IAW SRM.

Part: MEC — FAULTY (NR 1 ENGINE) · airframe 82,237 hrs · 62,190 cycles

INFLIGHT SHUTDOWN NR 1 ENGINE ROLLED BACK AT FL350 DURING CROSSFEED. CROSSFEED VALVE APPEARED TO BE FUNCTIONING NORMALLY. SHUT NR 1 DOWN USING ENGINE FAILURE CHECKLIST DUE TO UNRESPONSIVE THROTTLE. REMOVED AND REPLACED MEC AND PUMP PER MT.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 82,191 hrs · 62,153 cycles

L1 DOOR EMERGENCY EVAC SLIDE COVER FELL OUT, DID NOT DEPLOY, STILL OPERATIONAL. RE-INSTALLED SLIDE PER MT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 82,021 hrs · 62,023 cycles

FWD ENTRY EMERGENCY LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 81,819 hrs · 61,868 cycles

AFT EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK IAW M/M.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 81,091 hrs · 61,312 cycles

AFT FLIGHT ATTENDANT FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT ASSY IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 80,773 hrs · 61,066 cycles

L2 DOOR LOWER EMERGENCY EXIT SIGN LIGHT BULB INOP. RELAMPED BULB PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,773 hrs · 61,065 cycles

SKIN CRACKED AT BS 872, STR 20L. REPAIRED SKIN IAW SRM & AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,773 hrs · 61,065 cycles

SKIN CRACKED BETWEEN BS 971 TO BS 972, STR 21L. REPAIRED SKIN CRACK PER ER AND EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 80,312 hrs · 60,696 cycles

FRAME CORRODED AT BS 727E, BETWEEN STR 27L TO STR 26L. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 80,312 hrs · 60,696 cycles

FRAME CORRODED AT BS 767, BETWEEN STR 26R TO STR 27R. REPAIRED FRAME SECTION PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 80,312 hrs · 60,696 cycles

STRINGER CLIP CORRODED AT BS 747, STR 26R. REMOVED AND REPLACED STR CLIP PER SRM & DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 80,312 hrs · 60,696 cycles

FRAME CORRODED AT BS 727C, BETWEEN STR 26L TO STR 27L. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 80,312 hrs · 60,696 cycles

FRAME CORRODED AT BS 747, STR 27L. REPAIRED FRAME PER ER.

Part: FRAME — CORRODED (FUSELAGE) · airframe 80,312 hrs · 60,696 cycles

FRAME CORRODED AT BS 767 BETWEEN STR 25R TO STR 26R. REPAIRED FRAME PER SRM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 80,312 hrs · 60,696 cycles

RT WING INBD FORE FLAP UPPER SIDE DELAMINATED. REPAIRED FORE FLAP IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,312 hrs · 60,696 cycles

FUSELAGE SKIN CRACKED AT BS 727E+13.5, STR 18R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,312 hrs · 60,696 cycles

CRACK IN FUSELAGE SKIN AT BS 759.25, STR 18R, .375. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 763.25 S19R) · airframe 80,312 hrs · 60,696 cycles

SKIN CRACKED AT BS 763.25, STR 19R. REPAIRED PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 80,312 hrs · 60,696 cycles

R2 DOOR LOWER EXIT LIGHT BULB INOP. REPLACED LIGHT BULB PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 80,312 hrs · 60,696 cycles

R1 DOOR EMERGENCY LIGHT BULB INOP. REPLACED BULB PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 80,312 hrs · 60,696 cycles

L1 DOOR EMERGENCY LOWER EXIT LIGHT BULB INOP. REPLACED BULB PER AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,312 hrs · 60,696 cycles

SKIN CRACKED AT BS 749, STR 18R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,312 hrs · 60,696 cycles

SKIN CRACKED AT BS 727-6.5, STR 21R. REPAIRED SKIN PER ER & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,312 hrs · 60,696 cycles

SKIN CRACK AT BS 727E+7.0, STR 21R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,312 hrs · 60,696 cycles

SKIN CRACKED AT BS 747-5.0, STR 21R. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 80,097 hrs · 60,539 cycles

R2 DOOR EMERGENCY EVAC SLIDE INADVERTANTLY FELL OUT, DID NOT DEPLOY, STILL OPERATIONAL. RE-INSTALLED SLIDE PER MT.

Part: ACTUATOR — MALFUNCTIONED (LT MLG) · airframe 79,745 hrs · 60,258 cycles

WHEN LOWERING GEAR, HAD RED LEFT MAIN GEAR LIGHT AND NO GREEN LIGHT. CYCLED GEAR WITH SAME RESULTS. MANUALLY EXTENDED GEAR AND GREEN ILLUMINATED. REMOVED AND REPLACED LT MLG DOWNLOCK ACTUATOR IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 79,445 hrs · 60,032 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 520+3, STR 8R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 79,445 hrs · 60,032 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 520-2, STR 8R. REPAIRED SKIN IAW EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 79,445 hrs · 60,032 cycles

DURING SCHEDULED OTS CHECK, FOUND FRAME CORRODED AT BS 967, LBL 2. REPAIRED FRAME IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 79,445 hrs · 60,032 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 967, LBL 2. REPAIRED SKIN IAW EA.

Part: FAIRING — CRACKED (LT WING) · airframe 82,644 hrs · 62,484 cycles

NR 3 FLAP TRACK FIXED FIXED FAIRING I/B SIDE HAS CRACK MOD. NR 3 FLAP TRACK FAIRING CRACKED ON INBOARD SIDE, REPAIRED IN ACCORDANCE WITH EA 1-A57-0553. REMOVED AND RE-INSTALLED ACCESS PANEL FWD OF NR 3 FLAP TRACK FAIRING IAW IAW SRM 51-40-02.

Part: SKIN — CRACKED (FUSELAGE) · airframe 79,442 hrs · 60,031 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND SKIN CRACKED AT BS 520-2, STR 8R. REPAIRED SKIN PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 7,942 hrs · 60,031 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND FRAME CORRODED AT BS 967, LBL 2. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 79,442 hrs · 60,031 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND SKIN CRACKED AT BS 520+3, STR 8R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,334 hrs · 59,166 cycles

DURING SCHEDULED 26Y CHECK FOUND, SKIN CRACKED AT BS 357, STR 13R. REPAIRED SKIN PER EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 78,334 hrs · 59,166 cycles

DURING SCHEDULED 26Y CHECK FOUND, STRINGER CORRODED BETWEEN BS 347-357, STR 25R. REPAIRED STRINGER PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 78,334 hrs · 59,166 cycles

DURING SCHEDULED 26Y CHECK FOUND, FRAME LOWER INNER CHORD CRACKED AT BS 616, RBL 67. REPAIRED CHORD PER EA.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 78,334 hrs · 59,166 cycles

DURING SCHEDULED 26Y CHECK FOUND, AFT CARGO BAY, CARGO RAIL CORRODED AT STA 847 RBL 14. REPAIRED RAIL PER EA.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 78,334 hrs · 59,166 cycles

DURING SCHEDULED 26Y CHECK FOUND, AFT CARGO BAY, CARGO RAIL CORRODED AT STA 859 RBL 3. REPAIRED RAIL PER EA.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 78,334 hrs · 59,166 cycles

DURING SCHEDULED 26Y CHECK FOUND, AFT CARGO BAY, CARGO RAIL CORRODED AT STA 727D+5 LBL 12. REPAIRED RAIL PER EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 78,334 hrs · 59,166 cycles

DURING SCHEDULED 26Y CHECK FOUND, STRINGER CORRODED BETWEEN BS 350-357 TO STR 22R. REPAIRED STRINGER PER SRM.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 78,334 hrs · 59,166 cycles

DURING SCHEDULED 26Y CHECK FOUND, AFT CARGO BAY, CARGO RAIL CORRODED AT STA 859 RBL 7.5. REPAIRED RAIL PER EA.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 78,334 hrs · 59,166 cycles

DURING SCHEDULED 26Y CHECK FOUND, AFT CARGO BAY, CARGO RAIL CORRODED AT STA 772 LBL 3. REPAIRED RAIL PER EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 78,334 hrs · 59,166 cycles

DURING SCHEDULED 26Y CHECK FOUND, STRINGER CORRODED BETWEEN BS 360-380 TO STR 24R. REPAIRED STRINGER PER SRM.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 78,334 hrs · 59,166 cycles

DURING SCHEDULED 26Y CHECK FOUND, AFT CARGO BAY, CARGO RAIL CORRODED AT STA 859 LBL 12. REPAIRED RAIL PER EA.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 78,333 hrs · 59,166 cycles

DURING SCHEDULED 26Y CHECK FOUND, THE STUB BEAM ATTACH ANGLE CRACKED AT BS 639 RBL 45. REPAIRED ANGLE IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 78,333 hrs · 59,166 cycles

DURING SCHEDULED 26Y CHECK FOUND, CRACK AT RBL 24.8 LONGITUDINAL FLOORBEAM UPPER CHORD BS 727B. REPAIRED CHORD PER ER.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 78,333 hrs · 59,166 cycles

DURING SCHEDULED 26Y CHECK FOUND, STRINGER 23 RT BS 347-357 CORRODED. REPAIRED STRINGER IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,334 hrs · 59,166 cycles

DURING SCHEDULED 26Y CHECK FOUND, SKIN CRACKED AT BS 374.5, STR 15R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,334 hrs · 59,166 cycles

DURING SCHEDULED 26Y CHECK FOUND, SKIN CORRODED BETWEEN BS 727B+6 TO BS 727C+14, BETWEEN STR 23L TO STR 25L. REMOVED AND REPLACED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,334 hrs · 59,166 cycles

DURING SCHEDULED 26Y CHECK FOUND, SKIN CRACKED AT BS 357, STR 22R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,334 hrs · 59,166 cycles

DURING SCHEDULED 26Y CHECK FOUND, SKIN CRACKED AT BS 755, STR 22L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,334 hrs · 59,166 cycles

DURING SCHEDULED 26Y CHECK FOUND, SKIN CRACKED AT BS 373, STR 26L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,334 hrs · 59,166 cycles

DURING SCHEDULED 26Y CHECK FOUND, SKIN CRACKED AT BS 373, STR 25L. REPAIRED SKIN PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 78,334 hrs · 59,166 cycles

DURING SCHEDULED 26Y CHECK FOUND, FRAME CORRODED AT BS 380, BETWEEN STR 25R TO STR 26R. REPAIRED FRAME.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 78,334 hrs · 59,166 cycles

DURING SCHEDULED 26Y CHECK FOUND, LONGITUDINAL FLOORBEAM CRACKED AT BS 727B, LBL 45.5. REPAIRED BEAM PER ER.

Part: FRAME — CORRODED (FUSELAGE) · airframe 78,334 hrs · 59,166 cycles

DURING SCHEDULED 26Y CHECK FOUND, FRAME CORRODED AT BS 345, BETWEEN RBL 16 TO RBL 22. REPAIRED FRAME PER SRM.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 78,334 hrs · 59,166 cycles

DURING SCHEDULED 26Y CHECK FOUND, RT CHORD CRACKED AT BS 616. REPAIRED CHORD PER EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 78,334 hrs · 59,166 cycles

DURING SCHEDULED 26Y CHECK FOUND, STRINGER CORRODED BETWEEN BS 350-357, STR 24R. REPAIRED STRINGER PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 78,334 hrs · 59,166 cycles

DURING SCHEDULED 26Y CHECK FOUND, SKIN CORRODED AT BS 344, BETWEEN STR 26R-27R. REPAIRED SKIN PER EA.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 78,334 hrs · 59,166 cycles

DURING SCHEDULED 26Y CHECK FOUND, AFT CARGO RAIL CORRODED AT BS 859, LBL 3. REPAIRED RAIL PER EA.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 78,334 hrs · 59,166 cycles

DURING SCHEDULED 26Y CHECK FOUND, STRINGER SPLICE CRACKED AT BS 727, STR 23L. REMOVED AND REPLACED SPLICE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,334 hrs · 59,166 cycles

DURING SCHEDULED 26Y CHECK FOUND, SKIN CRACKED AT BS 747, STR 22L. REPAIRED SKIN PER SRM.

Part: SKIN — DELAMINATED (SPOILER) · airframe 78,334 hrs · 59,166 cycles

DURING SCHEDULED 26Y CHECK FOUND, LT WING NR 4 SPOILER LOWER SURFACE DELAMINATED. REMOVED AND REPLACED SPOILER PER MM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 78,334 hrs · 59,166 cycles

DURING SCHEDULED 26Y CHECK FOUND, SKIN CORRODED BETWEEN BS 340 TO BS 360, BETWEEN STR 225-27R. REPAIRED SKIN PER EA.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 78,024 hrs · 58,908 cycles

DURING SCHEDULED OTS CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,024 hrs · 58,908 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 514D, STR 16L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,021 hrs · 58,907 cycles

DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT BS 887 + 13, STR 25L. REPAIRED SKIN PER SRM.

Part: LENS — LOOSE (CABIN) · airframe 78,021 hrs · 58,907 cycles

DURING SCHEDULED HC2 CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT LENS LOOSE AT ROW 2. REMOVED AND REPLACED LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,021 hrs · 58,907 cycles

DURING SCHEDULED HC2 CHECK, FOUND CRACK IN FUSELAGE AT STA 500D +14, STR 16L, ONE INCH FROM UNDER SKIN DOUBLER. REPAIR SKIN PER SRM.

Part: SKIN — CRACKED (R1 DOOR) · airframe 78,021 hrs · 58,907 cycles

DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR OUTER SKIN CORNER CRACKED AT BS 300, WL 274. REPAIRED SKIN PER SRM.

Part: ACTUATOR — FAULTY (LT MLG) · airframe 77,963 hrs · 58,866 cycles

AFTER LANDING GEAR RETRACTION ON TAKEOFF, RED LEFT GEAR LIGHT AND GREEN LEFT GEAR LIGHT REMAINED ILLUMINATED. RECYCLED GEAR RETRACTION IN UP AND OFF POSITION STILL SHOWED SAME LEFT GEAR LIGHTS AS BEFORE. REMOVED AND REPLACED LT MLG UPLOCK ACTUATOR PER MM.

Part: CIRCUIT CARD — FAULTY (E&E BAY) · airframe 77,954 hrs · 58,860 cycles

LT MLG RED UNSAFE LIGHT INDICATION, RECYCLED GEAR AND LIGHT WENT OUT. GEAR EXTENDED NORMALLY. REMOVED AND REPLACED M986 PC CARD PER MM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 77,898 hrs · 58,817 cycles

DURING SCHEDULED MV1 CHECK, FOUND STRINGER CRACKED AT BS 500C, STR 19R. REMOVED AND REPLACED STRINGER PER EA.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 77,898 hrs · 58,817 cycles

DURING SCHEDULED MV1 CHECK, FOUND BATTERY PACK INOP AT ROW 17. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,902 hrs · 58,821 cycles

DURING SCHEDULED MV3 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR UPPER HINGE CUTOUT AT LOWER AFT CORNER. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (L1 DOOR) · airframe 77,871 hrs · 58,797 cycles

DURING SCHEDULED MV3 CHECK, FOUND L2 DOOR LOWER GUIDE ARM CUTOUT CRACKED. REMOVED AND REPLACED L1 DOOR PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 77,193 hrs · 58,285 cycles

DURING SCHEDULED SPV CHECK, FOUND LT WING I/B FORE FLAP DELAMINATED. REPAIRED FORE FLAP PER MM.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 77,193 hrs · 58,285 cycles

DURING SCHEDULED SPV CHECK, FOUND RT WING I/B FORE FLAP UPPER SURFACE DELAMINATED. REPAIRED FORE FLAP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,193 hrs · 58,285 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 734E, STR 19L. REMOVED AND REPLACED SKIN PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,193 hrs · 58,285 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 500D, BETWEEN STR 20R TO STR 21R. REMOVED AND REPLACED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,193 hrs · 58,285 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 500C, BETWEEN STR 20L TO STR 21L. REMOVED AND REPLACED FRAME PER SRM.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 77,193 hrs · 58,285 cycles

DURING SCHEDULED SPV CHECK, FOUND LT WING I/B FORE FLAP UPPER SURFACE DELAMINATED. REPAIRED FORE FLAP PER SRM.

Part: COMPRESSOR — STALLED (NR 1 ENGINE) · airframe 76,550 hrs · 57,757 cycles

INFLIGHT SHUTDOWN/DIVERSION/DECLARED EMERGENCY. FL 330 CRUISE FLT - MULTIPLE COMPRESSOR STALL (LOUD BANGS) ENGINE GAUGES NR 1 FLUX. POWER IDLE COMPRESSOR STALL STOP. AT IDLE ENGINE SHUT ITSELF OFF. REMOVED AND REPLACED NR 1 ENGINE PER MT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,335 hrs · 57,580 cycles

DURING SCHEDULED HC1 CHECK, FOUND SKIN CRACKED AT BS 518, STR 16R. REPAIRED SKIN PER SRM.

Part: LENS — CRACKED (EVAC SLIDE) · airframe 76,335 hrs · 57,580 cycles

DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE LENS CRACKED. REMOVED AND REPLACED LENS PER MM.

Part: SIGN — DAMAGED (CABIN) · airframe 75,292 hrs · 56,797 cycles

DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR LOWER CORNER EMERGENCY EXIT SIGN DAMAGED. REMOVED AND REPLACED SIGN PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,772 hrs · 56,415 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND SKIN CRACKED AT BS 773, STR 18L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,772 hrs · 56,415 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND SKIN CRACKED AT BS 515D, STR 15L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,772 hrs · 56,415 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND SKIN CRACKED AT BS 786, STR 19L. REPAIRED SKIN PER EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 74,635 hrs · 56,319 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: CONTROL ROD — CORRODED (ELEVATOR TAB) · airframe 7,018 hrs · 55,858 cycles

DURING SCHEDULED CV CHECK, FOUND RT ELEVATOR TAB CONTROL RODS CORRODED. REMOVED AND REPLACED ROD ASSY PER EA.

Part: LIGHT — CRACKED (CABIN) · airframe 7,018 hrs · 55,858 cycles

DURING SCHEDULED CV CHECK, FOUND RT EMERGENCY EXIT LIGHT CRACKED AT ROW 2. REMOVED AND REPLACED LIGHT PER MM.

Part: CONTROL ROD — CORRODED (ELEVATOR TAB) · airframe 7,018 hrs · 55,858 cycles

DURING SCHEDULED CV CHECK, FOUND LT ELEVATOR TAB CONTROL RODS CORRODED. REMOVED AND REPLACED ROD ASSY'S PER EA.

Part: LIGHT — CRACKED (CABIN) · airframe 7,018 hrs · 55,858 cycles

DURING SCHEDULED CV CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT CRACKED AT ROW 2. REMOVED AND REPLACED LIGHT PER MM.

Part: COVER — MISSING (CABIN) · airframe 73,519 hrs · 55,509 cycles

R1 DOOR EMERGENCY EXIT COVER MISSING. INSTALLED COVER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,342 hrs · 55,383 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 980, STR 21L. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,338 hrs · 55,382 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 980, STR 21L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,338 hrs · 55,382 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 770, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,338 hrs · 55,382 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 760, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,338 hrs · 55,382 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 740E, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,267 hrs · 55,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT, BS 304, WL 234. REPAIRED SKIN PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 73,267 hrs · 55,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND CENTER WING BOX LONGITUDINAL FLOORBEAM CORRODED AT BS 670, BBL 0.07. REPAIRED BEAM PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 73,267 hrs · 55,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 662, BBL 0.07. REPAIRED BEAM PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,267 hrs · 55,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT, BS 304, WL 239. REPAIRED SKIN PER EA.

Part: LIGHT — CORRODED (CABIN) · airframe 73,267 hrs · 55,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT EEPLS LIGHT CORRODED AT ROW 4. REMOVED AND REPLACED EEPLS PER MM.

Part: LIGHT — CORRODED (CABIN) · airframe 73,267 hrs · 55,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT EEPLS LIGHT CORRODED AT ROW 2. REMOVED AND REPLACED EEPLS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,267 hrs · 55,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT, BS 291, WL 233. REPAIRED SKIN PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,267 hrs · 55,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 706, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 73,267 hrs · 55,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 669, BBL 0.07. REPAIRED BEAM PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 73,267 hrs · 55,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 668, BBL 0.07. REPAIRED BEAM PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 73,267 hrs · 55,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 661, BL 0. REPAIRED BEAM PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 73,267 hrs · 55,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM CORRODED AT BS 675, BBL 0.07. REPAIRED BEAM PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,267 hrs · 55,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT, BS 305, WL 257. REPAIRED SKIN PER SWA EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 73,267 hrs · 55,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 670, BBL 0.07. REPAIRED BEAM PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,267 hrs · 55,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT, BS 302, WL 234. REPAIRED SKIN PER SWA EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 73,267 hrs · 55,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND CENTER WING BOX FLOORBEAM CRACKED AT BS 727B, LBL 24.5. REPAIRED BEAM PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,267 hrs · 46,698 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,267 hrs · 55,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,267 hrs · 55,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,267 hrs · 55,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 15L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,267 hrs · 55,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 380, STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,267 hrs · 55,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 15L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,267 hrs · 55,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 787, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,267 hrs · 55,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 727B, STR 8L. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,267 hrs · 55,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 847, STR 9R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,267 hrs · 55,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 5R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,267 hrs · 55,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 847, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,267 hrs · 55,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 767, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,267 hrs · 55,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 767, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,267 hrs · 55,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,267 hrs · 55,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 597, STR 8L. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,267 hrs · 55,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 8L. REPAIRED CLIP PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,267 hrs · 55,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 907, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,267 hrs · 55,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 727B, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,267 hrs · 55,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 727E, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,267 hrs · 55,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 72,462 hrs · 54,763 cycles

FWD O/B EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 71,649 hrs · 54,191 cycles

DURING SCHEDULED SPV CHECK, FOUND RT KEEL BEAM CORRODED AT BETWEEN 500D TO BS 520. REPAIRED BEAM PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 71,649 hrs · 54,191 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 500D, STR 27L. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,639 hrs · 54,185 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 520, RBL 28. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 71,639 hrs · 54,185 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD CARGO SHEAR TIE CORRODED AT BS 500C, BETWEEN STR 26L TO STR 25L. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 71,639 hrs · 54,185 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CORRODED AT BS 500D, STR 27L. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 71,639 hrs · 54,185 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, RBL 18. REPAIRED SHEAR TIE PER SRM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 71,639 hrs · 54,185 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD LT OVER HEAD EMERGENCY EXIT LIGHT INOP. R&R BATTERY CHARGER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,350 hrs · 53,988 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 480, STR 17L. REPAIRED SKIN PER SRM.

Part: LENS — LOOSE (CABIN) · airframe 71,350 hrs · 53,988 cycles

FOUND RT EMERGENCY EXIT LIGHT LENS LOOSE. REPAIRED LENS PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,816 hrs · 53,597 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 892, STR 25R. REPAIRED SKIN PER SRM.

Part: BATTERY PACK — FAULTY (EMERGENCY LIGHT) · airframe 70,453 hrs · 53,331 cycles

DURING SCHEDULED MV2 CHECK, RT AFT CABIN EMERGENCY EXIT LIGHTS WILL NOT EXTINGUISH. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BALLAST — FAULTY (CABIN) · airframe 69,632 hrs · 52,707 cycles

CREW REPORTED VISIBLE SMOKE AND ELECTRICAL SMELL AT ROW 12 ABC. INSPECTED AND FOUND LIGHT BALLAST AT ROW 12 ABC CAUSE OF SMOKE. REMOVED AND REPLACED LIGHT BALLAST PER MM.

Part: HYDRAULIC LINE — KINKED (MLG WW) · airframe 69,560 hrs · 52,653 cycles

AIRTURN BACK - INFLIGHT HYDRAULIC A-SYSTEM LOW PRESSURE LIGHT ILLUMINATED. REMOVED AND REPLACED SUPPLY HOSE TO A-SYSTEM RESERVOIR PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,344 hrs · 51,762 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 792, STR 19L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,032 hrs · 51,529 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 410, STR 28L. REPAIRED SKIN PER SWA EA.

Part: BOLT — WORN (ELEVATOR TAB) · airframe 68,032 hrs · 51,529 cycles

DURING SCHEDULED BRDG CHECK, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED BUSHING AND BOLT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,032 hrs · 51,529 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 450, STR BL 0. REPAIRED SKIN PER SWA EA.

Part: TORQUE TUBE — WORN (ELEVATOR) · airframe 68,032 hrs · 51,529 cycles

DURING SCHEDULED BRDG CHECK, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED TORQUE TUBE PER MM.

Part: FITTING — WORN (SPOILER) · airframe 68,032 hrs · 51,529 cycles

DURING SCHEDULED BRDG CHECK, FOUND LT WING INBOARD GROUND SPOILER OUTBOARD ACTUATOR FITTING WORN. REPAIRED FITTING PER SWA EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,032 hrs · 51,529 cycles

DURING SCHEDULED BRDG CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 68,032 hrs · 51,529 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER 21R CORRODED AT BS 360. REPAIRED STRINGER PER SRM.

Part: TEE FITTING — CORRODED (FUSELAGE) · airframe 68,032 hrs · 51,529 cycles

DURING SCHEDULED BRDG CHECK, FOUND BULKHEAD LOWER TEE CHORD CORRODED AT BS 227, LBL 10 TO RBL 10. REPAIRED CHORD PER SWA EA.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 68,029 hrs · 51,523 cycles

DURING SCHEDULED BRDG CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (BS 410 S28L) · airframe 68,029 hrs · 51,523 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 410, STR 28L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 450) · airframe 68,029 hrs · 51,523 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 450, BL 0. REPAIRED SKIN PER SWA EA.

Part: FLAP TRACK — CRACKED (LT WING) · airframe 68,029 hrs · 51,923 cycles

DURING SCHEDULED BRDG CHECK, FOUND LT WING NR 2 FLAP TRACK CRACKED. REMOVED AND REPLACED FLAP TRACK PER SRM.

Part: FLAP TRACK — CRACKED (RT WING) · airframe 68,029 hrs · 51,923 cycles

DURING SCHEDULED BRDG CHECK, FOUND RT WING NR 7 FLAP TRACK CRACKED. REMOVED AND REPLACED FLAP TRACK PER SRM.

Part: TEE FITTING — CORRODED (BS 227) · airframe 68,029 hrs · 51,523 cycles

DURING SCHEDULED BRDG CHECK, FOUND BULKHEAD LOWER TEE CHORD CORRODED AT BS 227, BETWEEN LBL 10 AND RBL 10. REPAIRED TEE CHORD PER SWA EA.

Part: FLAP — DELAMINATED (LT WING) · airframe 68,029 hrs · 51,523 cycles

DURING SCHEDULED BRDG CHECK, FOUND LEFT WING INBOARD FOREFLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 68,029 hrs · 51,523 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER 21R CORRODED AT BS 360. REPAIRED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (BS 277 S10R) · airframe 68,029 hrs · 51,523 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,029 hrs · 51,523 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 730E, STR 18R. REPAIRED SKIN PER SWA EA.

Part: SLAT — CRACKED (LT WING) · airframe 68,029 hrs · 51,523 cycles

DURING SCHEDULED BRDG CHECK, FOUND LT WING NR 2 L/E SLAT CRACKED OUTBOARD END. REPAIRED SLAT PER SRM.

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 68,029 hrs · 51,523 cycles

DURING SCHEDULED C1 CHECK, FOUND LNG W/W CEILING PANEL WEB CUTOUT CRACKED AT OUTBOARD END. REPAIRED WEB PER ACO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,029 hrs · 51,523 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRAKCED AT R2 DOOR UPPER HINGE CUTOUT AFT END. REPAIRED SKIN PER SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 67,616 hrs · 51,208 cycles

DURING SCHEDULED SERVICE CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (RT WING SLAT) · airframe 67,048 hrs · 50,771 cycles

DURING SCHEDULED C4 CHECK, FOUND RIGHT WING NR 6 L/E SLAT CRACKED AT FWD END. REPAIRED SLAT PER SWA EA.

Part: SKIN — CRACKED (BS 747 S19R) · airframe 67,048 hrs · 50,771 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, STR 19R. REPAIRED SKIN PER SWA EA.

Part: SIGN — BROKEN (EMERGENCY LIGHT) · airframe 66,759 hrs · 50,528 cycles

DURING SCHEDULED PM CHECK, FOUND RIGHT OVERWING EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED EXIT SIGN PER MM.

Part: WINDOW — ARCED (COCKPIT) · airframe 66,177 hrs · 50,064 cycles

FLIGHT DECK R2 WINDOW ARCHED. REMOVED AND REPLACED R2 WINDOW PER MM.

Part: SLIDE — INOPERATIVE (L1 DOOR) · airframe 65,703 hrs · 49,690 cycles

L1 DOOR EMERGENCY EVAC SLIDE INOP. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,482 hrs · 49,516 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, STR 21L. REPAIRED SKIN PER SWA EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 65,394 hrs · 49,440 cycles

DURING SCHEDULED MV1 CHECK, FOUND RIGHT OVERWING EMERGENCY EXIT SIDEWALL LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,182 hrs · 49,263 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 730E, STR 18R. REPAIRED SKIN PER SWA EA.

Part: SKIN — DELAMINATED (LT FOREFLAP) · airframe 65,182 hrs · 49,263 cycles

DURING SCHEDULED C2 CHECK, FOUND LEFT WING INBOARD FOREFLAP DELAMINATED AT UPPER SURFACE. REMOVED AND REPLACED FOREFLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,115 hrs · 49,209 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT GARGO DOOR FWD LOWER CUTOUT. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,115 hrs · 49,209 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT GARGO DOOR AFT LOWER CUTOUT. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (BS 450) · airframe 65,115 hrs · 49,209 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE BELLY SKIN CRACKED AT RADIO ALT ANTENNA CUTOUT, BS 450. REPAIRED SKIN PER ER & BOEING SERVICE BULLETIN.

Part: FAILSAFE — CRACKED (BS 440 S27R) · airframe 65,115 hrs · 49,209 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME FAIL-SAFE CHORD CRACKED AT BS 440, STR 27R. REPAIRED CHORD PER SRM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 65,115 hrs · 49,209 cycles

DURING SCHEDULED SPV CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 64,226 hrs · 48,507 cycles

DURING SCHEDULED C1 CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT L2 DOOR. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: HYDRAULIC LINE — LEAKING (HYDRAULIC SYS) · airframe 64,210 hrs · 48,493 cycles

AIR TURN BACK, HYDRAULIC "B" SYSTEM FLUID LOSS. REMOVED AND REPLACED HYDRAULIC LINE AT "B" SYSTEM ACOUSTIC FILTER AND "B" SYSTEM RETURN FILTERS PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 63,608 hrs · 48,631 cycles

FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 63,581 hrs · 48,010 cycles

DURING SCHEDULED SERVICE CHECK, FOUND R2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED BULB PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,369 hrs · 47,852 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT BEAR STRAP. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,369 hrs · 47,852 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,369 hrs · 47,852 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 62,873 hrs · 47,479 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHT BATTERY CHARGER INOP AT BS 629. R&R BATTERY CHARGER PER MM.

Part: SKIN — CRACKED (BS 732D-742D) · airframe 62,381 hrs · 47,078 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 732D TO BS 742D, STR 20L TO STR 21L. REPAIRED SKIN PER SWA EA & SRM.

Part: SKIN — CRACKED (BS 747) · airframe 62,381 hrs · 47,078 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, STR 23R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 751) · airframe 62,381 hrs · 47,078 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 751, STR 19L. REPAIRED SKIN PER SWA EA.

Part: SKIN — DELAMINATED (RT WING FOREFLAP) · airframe 62,381 hrs · 47,078 cycles

DURING SCHEDULED C3 CHECK, FOUND RIGHT WING INBOARD T/E FOREFLAP DELAMINATED. REMOVED AND REPLACED FOREFLAP PER MM.

Part: SKIN — CRACKED (BS 837) · airframe 62,381 hrs · 47,078 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 837, STR 25L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 780) · airframe 62,381 hrs · 47,078 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 780, STR 24L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 727D) · airframe 61,374 hrs · 46,281 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D, STR 19L. REPAIRED SKIN PER SWA EA AND SRM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 60,630 hrs · 45,674 cycles

DURING SCHEDULED SERVICE CHECK, FOUND R2 DOOR EXTERNAL EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: WIRE — CHAFED (BLEED SYSTEM) · airframe 60,349 hrs · 45,450 cycles

DIVERSION/DECLARED EMERGENCY. CABIN ALTITUDE HORN SOUNDED, PERFORMRED EMERGENCY PROCEDURE AND INITIATED EMERGENCY DESCENT. REPAIRED WIRING HARNESS ON BLEED VALVE PER WDM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,268 hrs · 45,385 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STUB FRAME CRACKED AT BS 188, LEFT SIDE, WL 208. REPAIRED STUB FRAME PER SRM.

Part: FLOOR PANEL — CRACKED (COCKPIT) · airframe 60,268 hrs · 45,385 cycles

DURING SCHEDULED D-CHECK, FOUND 2 EA FUSELAGE FLOOR WEB CRACKS AT BS 188 TO BS 196, LEFT & RIGHT SIDE, WL 208. REMOVED AND REPLACED WEB SECTIONS PER SRM.

Part: STRINGER — CRACKED (AFT PRESS BLKHD) · airframe 60,258 hrs · 45,376 cycles

DURING SCHEDULED D-CHECK, FOUND BS 1016 AFT PRESS BULKHEAD RADIAL STRINGER CRACKED AT 8 O'CLOCK POSITION. REPAIRED RADIAL STRINGER PER SRM.

Part: SHEAR TIE — CORRODED (E & E BAY) · airframe 60,258 hrs · 45,376 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 360, STR 27L TO STR 28L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 60,258 hrs · 45,376 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CRACKED AT BS 727A + 17.5, RBL 44 & RBL 46, WL 208. REPAIRED FLOORBEAM PER BFG ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,258 hrs · 45,376 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 887, STR 9L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,258 hrs · 45,376 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STUB FRAME CRACKED AT BS 188, RIGHT SIDE, WL 208. REPAIRED STUB FRAME PER SRM.

Part: SPLICE — CORRODED (BS 360) · airframe 60,258 hrs · 45,376 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CORRODED AT BS 360, BETWEEN STR 27L & STR 28R. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: STRINGER — CORRODED (E & E BAY) · airframe 60,257 hrs · 45,375 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CORRODED AT BS 363, STR 25R. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: WEDGE — DELAMINATED (NR 4 SLAT) · airframe 60,257 hrs · 45,375 cycles

DURING SCHEDULED D-CHECK, FOUND NR 4 L/E SLAT UPPER INBOARD T/E WEDGE DELAMINATED. REMOVED AND REPLACED NR 4 SLAT PER MM.

Part: SPAR — CRACKED (WINGS) · airframe 60,257 hrs · 45,375 cycles

DURING SCHEDULED D-CHECK, FOUND LT & RT WING REAR SPAR UPPER CHORDS CRACKED AT MLG BEAM 2ND INBOARD CUTOUT HOLE. REMOVED AND REPLACED REAR SPAR UPPER CHORDS PER BFG ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,257 hrs · 45,375 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D + 7, STR 24L. REPAIRED SKIN PER SRM.

Part: WEDGE — DELAMINATED (NR 5 SLAT) · airframe 60,257 hrs · 45,375 cycles

DURING SCHEDULED D-CHECK, FOUND NR 5 L/E SLAT UPPER INBOARD T/E WEDGE DELAMINATED. REPAIRED NR 5 SLAT PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 60,257 hrs · 45,375 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE BS 1016 PRESS BULKHEAD DOME WEB CRACKED AT BL 0, WL 249. REPAIRED WEB PER BFG ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,257 hrs · 45,375 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 986, ABOVE L2 DOOR UPPER AFT CUTOUT. REPAIRED FRAME PER SRM.

Part: LUG — CORRODED (VERTICAL STAB) · airframe 60,257 hrs · 45,375 cycles

DURING SCHEDULED D-CHECK, FOUND LT & RT VERTICAL STAB FWD & AFT FAILSAFE CLEVIS LUG FACES CORRODED. REPAIRED LUG FACES PER BFG ER.

Part: LUG — CORRODED (VERTICAL STAB) · airframe 60,257 hrs · 45,375 cycles

DURING SCHEDULED D-CHECK, FOUND LT & RT VERTICAL STAB FITTING FWD & AFT PRIMARY CLEVIS LUG FACES CORRODED. REPAIRED LUG FACES PER BFG ER.

Part: FLOORBEAM — CORRODED (COCKPIT FLOOR) · airframe 60,257 hrs · 45,375 cycles

DURING SCHEDULED D-CHECK, FOUND COCKPIT FLOORBEAM UPPER CHORD CORRODED AT BS 260, LBL 9 TO RBL 9, WL 208. REPAIRED FLOORBEAM PER BFG ER.

Part: FRAME — CRACKED (BS 727E) · airframe 60,257 hrs · 45,375 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727E, STR 9L. REPAIRED FRAME PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 60,257 hrs · 45,375 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CRACKED AT BS 620, STR 4L. REPAIRED STRINGER PER SRM.

Part: SPLICE — CRACKED (BS 908) · airframe 60,257 hrs · 45,375 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CRACKED AT BS 908, STR 4L & STR 4R. REMOVED AND REPLACED STR SPLICE PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727A) · airframe 60,257 hrs · 45,375 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 2R. REMOVED AND REPLACED STR CLIP PER SRM.

Part: FRAME — CRACKED (BS 807) · airframe 60,257 hrs · 45,375 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 807, STR 9R. REPAIRED FRAME PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 60,257 hrs · 45,375 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN TEAR STRAP CORRODED AT BS 370, STR 25L. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (BS 578) · airframe 60,257 hrs · 45,375 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 578, STR 2L & STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 60,257 hrs · 45,375 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CORRODED AT BS 351 TO BS 370, STR 22L. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: FITTING — CORRODED (HORIZONTAL STAB) · airframe 60,257 hrs · 45,375 cycles

DURING SCHEDULED D-CHECK, FOUND LT & RT HORIZONTAL STAB FITTING LUG FACES CORRODED. REPAIRED LUG FACES PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,257 hrs · 45,375 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727C, STR 9L. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 60,257 hrs · 45,375 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 616, STR 7R TO STR 8R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,257 hrs · 45,375 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 727E, STR 22R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 616) · airframe 60,257 hrs · 45,375 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 616, BETWEEN STR 1 & STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 597) · airframe 60,257 hrs · 45,375 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 597, BETWEEN STR 2R & STR 9R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,257 hrs · 45,375 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727E, STR 23R TO STR 24R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (BS 597) · airframe 60,257 hrs · 45,375 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 597, BETWEEN STR 2L & STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,257 hrs · 45,375 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 663, STR 1, STR 2L & STR 2R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,257 hrs · 45,375 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 706, STR 2L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,257 hrs · 45,375 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 9L & STR 9R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,257 hrs · 45,375 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 9R. REPAIRED FRAME PER SRM.

Part: SPLICE — CRACKED (BS 536) · airframe 60,257 hrs · 45,375 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CRACKED AT BS 536, STR 10R. REMOVED AND REPLACED SPLICE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 60,257 hrs · 45,375 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 500C, BETWEEN STR 26L TO STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,257 hrs · 45,375 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,257 hrs · 45,375 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 500D, STR 3R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CORRODED (AFT CARGO BAY) · airframe 60,257 hrs · 45,375 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 767, LBL 10. REPAIRED FRAME PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 60,257 hrs · 45,375 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CORRODED AT BS 500B, STR 27R. REPAIRED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (BS 500A) · airframe 60,257 hrs · 45,375 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 500A, STR 16R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,257 hrs · 45,375 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 9L. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,257 hrs · 45,375 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 360, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 344) · airframe 60,257 hrs · 45,375 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 344, STR 11R & STR 13R. REMOVED AND REPLACED CLIPS PER SRM.

Part: SLIDE — READS LOW (L2 DOOR) · airframe 59,852 hrs · 45,044 cycles

DURING SCHEDULED RON, FOUND L2 DOOR EVAC SLIDE LOW PRESSURE IND. REMOVED AND REPLACED L2 DOOR EVAC SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,705 hrs · 44,930 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 500C, STRINGER 16L, CRACKED. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,629 hrs · 44,866 cycles

DURING SCHEDULED C4 CHECK, FOUND 3 EACH FUSELAGE SKIN CRACKS BETWEEN BS 440 AND BS 480, STRINGER 10R. REPAIRED SKIN SECTIONS PER EA.

Part: BEARING — WORN (LT ELEVATOR) · airframe 59,629 hrs · 44,866 cycles

DURING SCHEDULED C4 CHECK, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED LT ELEVATOR BEARING AND SLEEVE ON LT CLEVIS PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 59,293 hrs · 44,614 cycles

EEPLS STRIP FROM ROW 6 ABC TO ROW 8 ABC, LOOSE. SECURED EEPLS STRIP PER MM.

Part: SKIN — DELAMINATED (RT WING FLAP) · airframe 59,284 hrs · 44,608 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED RT OUTBOARD T/E AFT FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,651 hrs · 44,093 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 747, STRINGER 24R, CRACKED. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,651 hrs · 44,093 cycles

DURING SCHEDULED C3 CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS AT BS 727E, STRINGER 19R, BS 747, STRINGER 20R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (KEELBEAM) · airframe 58,642 hrs · 44,087 cycles

DURING SCHEDULED C3 CHECK, FOUND KEELBEAM SKIN AT BS 660, LBL 6.3, CRACKED. REPAIRED SKIN PER EA.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 57,051 hrs · 42,810 cycles

DURING SCHEDULED RON, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED. REPAIRED RT WING OUTBOARD T/E AFT FLAP PER SRM.

Part: LIGHT — LOOSE (CABIN) · airframe 56,884 hrs · 42,677 cycles

DURING SCHEDULED C1 CHECK, FOUND RT FWD EEPLS TRACK LOOSE. RESECURED EEPLS TRACK PER MM.

Part: CABLE — MISROUTED (ESCAPE SLIDE) · airframe 56,884 hrs · 42,677 cycles

DURING SCHEDULED 1/2D CHECK, FOUND L2 DOOR EVAC SLIDE CABLE MISROUTED. REROUTED L2 DOOR EVAC SLIDE CABLE PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 56,673 hrs · 42,503 cycles

L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,506 hrs · 42,363 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STRINGER 24L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,446 hrs · 42,318 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727, STRINGER 24L. REPAIRED SKIN PER SRM.

Part: FITTING — CRACKED (LT MLG) · airframe 55,950 hrs · 41,907 cycles

DURING SCHEDULED C4 CHECK, FOUND LT MLG ACTUATOR BEAM HANGER FWD MOUNT FITTING CRACKED. REMOVED AND REPLACED HANGER MOUNT FITTING PER MM.

Part: SLIDE — OUT OF LIMITS (AFT ENTRY DOOR) · airframe 54,968 hrs · 41,142 cycles

DURING SCHEDULED RON, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,733 hrs · 40,952 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT SVC DOOR FWD LOWER CORNER. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,733 hrs · 40,952 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED (15 EA) AT STR 4L, BS'S 500D, 571, 602, 625, 626, 628, 630, 631, 632, 647, 649, 653, 658, 669 AND 706. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,733 hrs · 40,952 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED (4 EA) AT STR 4R, BS'S 597, 727B, 685 AND 706. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,733 hrs · 40,952 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 450, STR 10R. REPAIRED SKIN PER SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 54,007 hrs · 40,356 cycles

DURING SCHEDULED C3 CHECK, FOUND KEELBEAM CORRODED AT BS 500D + 10 LT. REPAIRED KEELBEAM PER SWA EA.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 54,000 hrs · 40,351 cycles

DURING SCHEDULED C2 CHECK, FOUND LT WING T/E OUTBOARD AFT FLAP DELAMINATED AT LOWER SURFACE. REMOVED AND REPLACED FLAP ASSY PER MM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 54,000 hrs · 40,351 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT SERVICE DOOR LOWER EMERGENCY EXIT LIGHT LENS MISSING. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY.

Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 54,000 hrs · 40,351 cycles

DURING SCHEDULED C2 CHECK, FOUND 1 INCH LONG CRACK AT KEELBEAM CENTER PANEL, BS 685, STRINGER 28L. REPAIRED KEEL BEAM PANEL PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,908 hrs · 40,277 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED ( 4 EA ) AT BS 730 BELOW STR 19R, BS 727E ABOVE STR 23L, BS 764 ABOVE STR 20L & BS 730E BELOW STR 23R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,908 hrs · 40,277 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED ( 2 EA ) AT BS 725 @ STR 23R & BS 884 @ STR 24R. REPAIRED SKIN PER SRM.

Part: STRUCTURE — DELAMINATED (RT WING TE FLAP) · airframe 53,908 hrs · 40,277 cycles

DURING SCHEDULED A2 CHECK, FOUND RT INBD FOREFLAP DELAMINATED ON UPPER SURFACE. R&R RT INBD FOREFLAP PER MM.

Part: HINGE FITTING — BROKEN (LT WING SPOILER) · airframe 53,908 hrs · 40,277 cycles

DURING SCHEDULED A2 CHECK, FOUND BROKEN HINGE FITTING ON NR 4 GROUND SPOILER UPPER SIDE. R&R NR 4 GROUND SPOILER & OTBD ACTUATOR PER MM.

Part: GUIDE ARM — OUT OF ADJUST (SERVICE DOOR) · airframe 53,556 hrs · 39,995 cycles

FWD SERVICE DOOR ONLY OPENED PARTIALLY. ADJUSTED UPPER GUIDE ARM PER MM.

Part: SLIDE — OUT OF POSITION (AFT ENTRY DOOR) · airframe 53,556 hrs · 39,995 cycles

AFT ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF THE CONTAINER. REINSTALLED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,990 hrs · 39,549 cycles

DURING SCHEDULED SC CHECK, FOUND FUSELAGE SKIN CRACK BETWEEN BS 727D AND 727E AT STR 20L. REPAIRED SKIN PER SRM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 52,676 hrs · 39,287 cycles

AFT LOWER EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM.

Part: FITTING — LOOSE (ENTRY DOOR) · airframe 51,334 hrs · 38,191 cycles

DURING SCHEDULED C3 CHECK, FOUND EMERGENCY EVAC SLIDE GIRT BAR ATTACH FITTINGS, LOOSE FASTENERS AT FWD ENTRY DOOR. SECURED FASTENERS PER MM

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,334 hrs · 38,191 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, STR 22R. REPAIRED SKIN PER SRM.

Part: BATTERY — WEAK (CABIN) · airframe 51,009 hrs · 37,937 cycles

EMERGENCY EXIT LIGHTS ILLUMINATE WHEN SHIFTING PWR FROM A/C PWR TO GRD PWR. REMOVED AND REPLACED M1132 EMERGENCY LIGHT BATTERY PER MM.

Part: ROLLER — WORN (AILERON) · airframe 50,599 hrs · 37,627 cycles

BINDING IN AILERONS DURING FLAP MOVEMENT. REMOVED AND REPLACED CENTERING MECH CAM ROLLER PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 49,641 hrs · 36,882 cycles

DURING SCHEDULED C1 CHECK, FOUND EMERGENCY EXIT LIGHTS INOP AT FWD SERVICE AND AFT ENTRYWAYS. RELAMPED PER MM.

Part: FLAP — DELAMINATED (LH WING) · airframe 48,519 hrs · 35,982 cycles

DURING WALKAROUND INSPECTION FOUND LH INBD T/E FLAP DELAMINATED. R&R FLAP PER MM.

Part: HOUSING — BROKEN (CABIN) · airframe 47,971 hrs · 35,538 cycles

DURING SCHEDULED A1 CHECK, FOUND EMERGENCY EXIT LIGHT BATTERY HOUSING FUSE BROKEN. REMOVED AND REPLACED BATTERY HOUSING PER MM.

Part: SLIDE — UNSERVICEABLE (SERVICE DOOR) · airframe 47,233 hrs · 34,907 cycles

DURING SCHEDULED SERVICE CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED EMERGENCY EVAC SLIDE PER MM.

Part: CONTAINER — LOOSE (SERVICE DOOR) · airframe 46,950 hrs · 34,691 cycles

AFT SERVICE DOOR EMERGENCY EVAC SLIDE CONTAINER CAME LOOSE. INSPECTED SLIDE & RESECURED CONTAINER.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 46,488 hrs · 34,315 cycles

DURING SCHEDULED RON CHECK, FOUND 2 BULLNOSE EMERGENCY EXIT LIGHTS INOP AT LEFT AFT CABIN. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: GUSSET — CRACKED (SERVICE DOOR) · airframe 46,411 hrs · 34,251 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FWD SVC DOOR CRACKED AT AFT LOWER CORNER GUSSET. REPAIRED GUSSET PER BAC DWG.

Part: PRESSURE PANEL — CRACKED (LT MLG W/W) · airframe 46,411 hrs · 34,251 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BEADED PRESSURE WEB CRACKED AT BS 665, LBL 32. REPAIRED BEADED WEB PER TR T1-353-046.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,411 hrs · 34,251 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BS 178 BULKHEAD VERTICAL CHORD CRACKED AT LBL 5.7, WL 184. REPAIRED VERTICAL CHORD PER SRM.

Part: LENS — CRACKED (CABIN) · airframe 46,411 hrs · 34,251 cycles

DURING SCHEDULED 1/2D CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT LENS CRACKED. REPLACED LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,411 hrs · 34,251 cycles

DURING SCHEDULED 1/2D CHECK, FOUND 1.5 EXTERNAL FUSELAGE SKIN CRACK AT FWD SVC DOOR CUTOUT, AFT LOWER CORNER. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,411 hrs · 34,251 cycles

DURING SCHEDULED 1/2D CHECK, FOUND .75 INCH EXTERNAL FUSELAGE SKIN CRACK AT AFT SIDE OF EQUIPMENT EXHUAST CUTOUT. REPAIRED SKIN DOUBLER PER SWA ACO.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 46,411 hrs · 34,251 cycles

DURING SCHEDULED 1/2D CHECK, FOUND SHEAR TIE CORRODED AT BS 360. REPAIRED SHEAR TIE PER SRM.

Part: BEAM — CRACKED (NLG WW) · airframe 46,411 hrs · 34,251 cycles

DURING SCHEDULED 1/2D CHECK, FOUND 2.5 CRACK AT NLG ACTUATOR SUPPORT WEB, BS 232, BL 0, WL 184. REPAIRED WEB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,411 hrs · 34,251 cycles

DURING SCHEDULED 1/2D CHECK, FOUND EXTERNAL FUSELAGE SKIN CRACK AT BS 870, STR 23R. REPAIRED SKIN PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 46,411 hrs · 34,251 cycles

DURING SCHEDULED 1/2D CHECK, FOUND 2 BS 178 BULKHEAD WEB CRACKS AT WL 187.5, LBL 1 & RBL 1. REPAIRED BULKHEAD WEB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,411 hrs · 34,251 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500, RBL 1. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,411 hrs · 34,251 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT SVC DOOR CUTOUT, BS 294, WL 208. REPAIRED FRAME PER SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 46,411 hrs · 34,251 cycles

DURING SCHEDULED 1/2D CHECK, FOUND CREASE BEAM WEB CRACKED AT LT SIDE, BS 616 TO BS 639. REPAIRED CREASE BEAM WEB PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 46,411 hrs · 34,251 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BS 178 BULKHEAD WEB CRACKED AT RBL 4.75, WL 202. REPAIRED BULKHEAD WEB PER SRM.

Part: STRINGER CLIP — CRACKED (CABIN) · airframe 46,411 hrs · 34,251 cycles

DURING SCHEDULED 1/2D CHECK, FOUND 2 STRINGER CLIPS CRACKED AT BS 663, STRS 10R & 10L. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 46,411 hrs · 34,251 cycles

DURING SCHEDULED 1/2D CHECK, FOUND 3 BS 178 BULKHEAD WEB CRACKS AT WL 234, LBL 12, LBL 10 & RBL 10. REPAIRED BULKHEAD WEB PER SRM.

Part: SKIN — CORRODED (KEELBEAM) · airframe 45,517 hrs · 33,522 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND SKIN BULGED AT BS 741, KEEL BEAM, LT. REPAIRED SKIN PER RA 1-353-2387.

Part: SKIN — CRACKED (FUSELAGE) · airframe 45,494 hrs · 33,506 cycles

DURING SCHEDULED A1 CHECK, FOUND 3.5 FUSELAGE SKIN CRACK AT BS 750, STR 23R. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 44,929 hrs · 33,021 cycles

DURING SCHEDULED C4 CHECK, FOUND FWD SERVICE DOOR EMERGENCY LIGHT INOP. RELAMPED PER MM.

Part: LINE — CONTAMINATED (NR 1 ENGINE)

AIR TURNBACK, NR 1 ENG A-SYS HYD LOW PRESS LIGHT ILLUMINATED AND NLG WOULD NOT RETRACT. FOUND AIR TRAPPED ON NR 1 ENG HYD PUMP SUPPLY LINE WHICH WAS PREVIOUSLY REMOVED AND REPLACED BLED SYS. OPS CHECKED GOOD PER MM.

Part: SKIN — CRACKED (BS 767)

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED, BS 767, STRINGER 19L. REPAIRED SKIN PER SRM.

Part: BATTERY CHARGER — INOP (PAX DOORWAY)

DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY DOOR EVACUATION SLIDE EMERGENCY LIGHT INOP. REMOVED AND REPLACED FWD ENTRY DOOR SLIDE EMERGENCY LIGHT BATTERY CHARGER ASSY PER MM.

Part: LIGHT — LOOSE (ROW 23)

EMERGENCY OVERHEAD EXIT LIGHT AT ROW 23 CAME LOOSE. RESECURED LIGHT ASSY PER MM.

Part: WEB — MISDRILLED (BS 279)

DURING SCHEDULED TRANSITION CHECK, FOUND PREVIOUSLY PLUGED HOLE IN WEB AT BS 279 WL 192 LBL 16. REPAIRED PER BOEING MM.

Part: ANGLE — DAMAGED (BS 1000)

DURING SCHEDULED TRANSITION CHECK, FOUND ANGLE BS 1000, RBL 45, WL 208 HAS ELONGATED FASTENER HOLE. REMOVED AND REPLACED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 312)

DURING SCHEDULED TRAN CHECK, FOUND CORRODED FLOORBEAM AT BS 312, RBL 7 TO 25 LBL 10 TO 12, WL 207 TO 208. REMOVED AND REPLACED PER BOEING SRM.

Part: BULKHEAD PANEL — CRACKED (BS 380)

DURING SCHEDULED SERVICE CHECK, FOUND CRACKED FWD CARGO BAY FWD BULKHEAD PANEL AT BS 380 RBL 12 WL 183. REPAIRED PER BOEING SRM.

Part: SHEAR TIE — CRACKED (BS 344)

DURING SCHEDULED SERVICE CHECK, FOUND CRACKED SHEAR TIE AT BS 344 BETWEEN STR 20 AND 21 RT. REPAIRED PER BOEING SRM.

Part: SEAL — TORN (LT MLG)

DURING SCHEDULED SERVICE CHECK, FOUND TORN LT MLG BEAM PANEL FWD BULB SEAL. REMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — DENTED (BS 371-374)

DURING SCHEDULED SERVICE CHECK, FOUND DENTED SKIN DOUBLER AT BS 371 TO 374 BETWEEN STR 22 AND 23 RT. REMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — DENTED (BS 500/764-767)

DURING SCHEDULED SERVICE CHECK, FOUND DENTED SKIN JUST FWD AT BS 500B BETWEEN STR 20 AND 21 LT AND AT BS 764 TO 767, STR 21 TO 23. RT. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (BS 806)

DURING SCHEDULED TRAN CHECK, FOUND DENT BELOW AFT CARGO DOOR AT BS 806, STR 26 RT. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (BS 310)

DURING SCHEDULED TRAN CHECK, FOUND DENTED FUSELAGE EXTERIOR SKIN AT BS 310, STR 24R. REPAIRED PER BOEING SRM.

Part: SKIN — GOUGED (RT TE FOREFLAP)

DURING SERVICE CHECK, FOUND GOUGED AREA, RIGHT HAND I/B FOREFLAP UPPER SURFACE 13 FROM I/B END. REPAIRED PER BOEING SRM.

Part: BULKHEAD WEB — CRACKED (BS 178)

DURING SERVICE CHECK, FOUND CRACKED INDICATIONS AT BS 178 PRESSURE BULKHEAD WEB AT RBL 4.7, WL 201.5 TO 200.0 AND WL 198.4 TO 197.8. REPAIRED PER BOEING SRM.

Part: BULKHEAD WEB — CRACKED (BS 178)

DURING SERVICE CHECK, FOUND CRACKED BS 178 PRESSURE BULKHEAD WEB AT LBL 4.7, WL 201.25 - 200.25 AND WL 198.7 - 197.5. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (BS 500)

DURING SERVICE CHECK, FOUND NUMEROUS SKIN DENTS AT BS 500+10- 500A BETWEEN STR 21 AND 22 RT. REPAIRED PER BOEING SRM.

Part: PANEL — CRACKED (LT PYLON)

DURING SERVICE CHECK, FOUND CRACKED LT PYLON INBOARD SIDE, AT PANEL 5742, DOUBLER AT AFT EDGE OF PANEL CUTOUT. REMOVED AND REPLACED PER BOEING SRM.

Part: WEDGE — GOUGED (RT TE MIDFLAP)

DURING SERVICE CHECK, FOUND GOUGED R/W I/B MIDFLAP T/E WEDGE LOWER SURFACE AT I/B T/E CORNER. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 328)

DURING SERVICE CHECK, FOUND CORRODED FLOORBEAM AT BS 328, RBL 12-40, WL 207-208. REMOVED AND REPLACED PER BOEING SRM.

Part: WEB — DRILLED (BS 669)

DURING SERVICE CHECK, FOUND HORIZONTAL PRESSURE WEB HAS DRILL START ON LOWER SURFACE AT BS 669, LBL 23 AT MLG WHEEL WELL. REPAIRED PER BOEING SRM.