N349SW

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,755 hrs · 67,603 cycles

STRINGER CLIP CRACKED AT BS 500C STRINGER 16R. R & R CLIP IAW EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 77,755 hrs · 67,603 cycles

SHEAR TIE CRACKED AT BS 500A BETWEEN STRINGER 15R TO STRINGER 16R. R & R SHEAR TIE IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,755 hrs · 67,603 cycles

SKIN CRACKED AT BS 500B + 15" TO 17" STRINGER 16R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,755 hrs · 67,603 cycles

SKIN CRACKED AT BS 847 + 5.25" TO 6.125, STRINGER 15R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,755 hrs · 67,603 cycles

SKIN CRACKED AT BS 400 + 4" TO 7.25" STRINGER 16L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,755 hrs · 67,603 cycles

SKIN CRACKED AT BS 847 + 2.5" TO 5.75, STRINGER 15R, R & R DOUBLER IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,755 hrs · 67,603 cycles

SKIN CRACKED AT BS 500D + 16" TO 18" STRINGER 16R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,755 hrs · 67,603 cycles

SKIN CRACKED AT BS 500D + 14" TO 17" STRINGER 15R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,755 hrs · 67,603 cycles

SKIN CRACKED AT BS 727C + 6" STRINGER 14R. REPAIRED SKIN IAW EA.

Part: PANEL — CRACKED (FUSELAGE) · airframe 77,755 hrs · 67,603 cycles

WING TO BODY FAIRING PANEL 3378L CRACKED FASTENER HOLE. REPAIRED PANEL IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,755 hrs · 67,603 cycles

SKIN CRACKED AT BS 727C + 6 TO 8 INCHES STRINGER 14R. REPAIRED SKIN IAW MM.

Part: LENS — LOOSE (CABIN) · airframe 76,952 hrs · 66,993 cycles

LEFT EMERGENCY EXIT OVERHEAD DOOR SIGN LOOSE. R & R LENS IAW AMM.

Part: PUMP — FAULTY (NR 1 ENGINE) · airframe 76,465 hrs · 66,629 cycles

DIVERSION -- NR 2 ENG N1 FLUCUATES +/- 3.5 TO 4.0% NR 1 ENG VIB. CLIMBS TO 3 - 5 ALONG WITH THE N1 CHANGES. N1 AND VIB. WILL STABILIZE FOR PERIODS OF 5 TO 10 MINUTES BEFORE IT BEGINS THE CHANGES AGAIN. REMOVED AND REPLACED NR 1 ENG FUEL PUMP AND MAIN FWD CONTROL PER M/M.

Part: HINGE — CRACKED (NR 5 SPOILER) · airframe 76,045 hrs · 66,333 cycles

RIGHT WING NR 5 GROUND SPOILER O/B HINGE CRACKED. REMOVED AND REPLACED SPOILER PER MM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 75,862 hrs · 66,202 cycles

STRINGER SPLICE CRACKED SIDE OF BS STA 908 FRAME, STR 4L. R & R SPLICE IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,862 hrs · 66,202 cycles

SKIN CRACKED BELOW STR 15L AT BS 500A+ 6.25 TO 500A+7. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,862 hrs · 66,202 cycles

SKIN CRACKED ABOVE STR 26L AT BS 386.5 TO 387. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (LT WING) · airframe 75,862 hrs · 66,202 cycles

LEFT WING FIXED LEADING EDGE SKIN CRACKED AT O/B END OF NR 1 K-FLAP. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,862 hrs · 66,202 cycles

SKIN CRACKED ON THE AFT SIDE OF BS 360, 3 INCHES BELOW STR 2L AND 4.5 INCHES ABOVE STR 3L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 75,862 hrs · 66,202 cycles

LEFT WING NR 2 SLAT L/E SKIN IS CRACKED ON LOWER SURFACE, FWD OF O/B AUXILIARY TRACK. REPAIRED LEFT WING NR 2 SLAT I/B SKIN LOWER AFT SURFACE COMMON TO O/B AUX TRACK PER SRM 55-43-01-2R-6.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,862 hrs · 66,202 cycles

FUSELAGE SKIN CRACKED AT VERTICAL CHEM-MILL STRAP SIDE OF BS 908 BELOW STR 4L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,862 hrs · 66,202 cycles

SKIN CRACKED AT BS 783.5 TO 784.75, ABOVE STR-19L. REMOVED AND REPLACED SKIN ON T185187 (FUSE 5011) 87529U.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,862 hrs · 66,202 cycles

SKIN CRACKED AT BS 780.5 TO 781, BELOW STR-19L. REPAIRED SKIN IAW EA.

Part: LENS — NOT SEATED (CABIN) · airframe 75,862 hrs · 66,202 cycles

EMERGENCY LIGHT LENS AT SEAT ROW 20-21 LT NOT SEATED ON BIN BULLNOSE. REMOVED AND RE-INSTALLED EMERGENCY LIGHT LENS AT SEAT ROW 20-21 LT IAW AMM 33-51-21-962-001 STEPS C. (1) AND (3).

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,862 hrs · 66,202 cycles

SKIN CRACK AT BS 405 TO 406 ABOVE STR-26R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,862 hrs · 66,202 cycles

FUSELAGE SKIN CRACKED AT VERTICAL CHEM-MILL STRAP SIDE OF BS 908 BELOW STR 4L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,862 hrs · 66,202 cycles

CRACK IN SKIN AT CHEM-MILL STEP BS 265-266.25 ABOVE STRINGER 15R CRACK LENGTH 1.25" SUB-SURFACE. REMOVED AND REPAIRED DAMAGE PER SRM 53-00-01-2R-31 DETAIL XXX. 86750U, 02FEB13

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,862 hrs · 66,202 cycles

SKIN CRACKED AT CHEM-MILL STEP BS 270.25 TO 272.25 ABOVE STR 16R. REMOVED AND REPLACED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,862 hrs · 66,202 cycles

SKIN CRACKED AT BS 500A+4.5 TO 500A+6.5 BELOW STR 15R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,862 hrs · 66,202 cycles

SKIN CRACK AT BS 502 TO 503.25 ABOVE STR-17R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,862 hrs · 66,202 cycles

SKIN CRACKED AT BS 473.25 TO 475 ABOVE STR-16L. REPAIRED SKIN IAW EA.

Part: CONTROL PANEL — FAULTY (COCKPIT) · airframe 75,741 hrs · 66,114 cycles

DIVERSION -- DURING INITIAL CLIMB CABIN OVER PRESSURIZED. REMOVED AND REPLACED CABIN CONTROL PANEL PER MM.

Part: SIGN — BROKEN (CABIN) · airframe 75,656 hrs · 66,058 cycles

AFT EXIT SIGN BROKEN. REMOVED AND REPLACED LIGHT ASSY PER M/M.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 75,502 hrs · 65,949 cycles

LEFT AND RIGHT UPPER AND LOWER OVERWING EMERGENCY EXIT LIGHTS ARE INOP. REMOVED AND REPLACED BATTERY PACKS FOR LEFT AND RIGHT UPPER AND LOWER OVERWING EMERGENCY EXIT LIGHTS IAW M/M.

Part: INTERCOSTAL — BROKEN (CABIN) · airframe 75,502 hrs · 65,949 cycles

INTERCOSTAL IS BROKEN AT STA 380-STA 400 BL "0". REMOVED AND REPLACED INTERCOSTAL PER SRM 51-10-02 AND SRM 51-40-02.

Part: STRUCTURE — DAMAGED (LE SLAT) · airframe 75,502 hrs · 65,949 cycles

NR 4 SLAT OUTBOARD SLAT CAN HAS EVIDENCE OF INTERNAL DAMAGE. REPAIRED PER EA.

Part: STRUCTURE — DAMAGED (LE SLAT) · airframe 75,502 hrs · 65,949 cycles

3 SLAT OUTBOARD SLAT CAN HAS EVIDENCE OF INTERNAL DAMAGE. REPAIRED PER EA.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 75,502 hrs · 65,949 cycles

MAIN CABIN FLOOR STRUCTURE STA 888-890 CORROSION ON NR 1 SEAT TRACK. REPAIRED SEAT TRACK FROM STA 867 TO 907 LBL 45 PER SRM 53-00-52-2R-3 AND EA 1-353-21100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 75,502 hrs · 65,949 cycles

MAIN CABIN FLOOR STRUCTURE STA 871-873 CORROSION ON NR 1 SEAT TRACK. REPAIRED SEAT TRACK FROM STA 867 TO 907 LBL 45 PER SRM 53-00-52-2R-3 AND EA 1-353-21100.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,502 hrs · 65,949 cycles

FOUND FUSELAGE SKIN DAMAGED AT THREE AREAS (MARKED) WHERE DORSAL FIN APEX MATES TO FUSELAGE. REPAIRED PER EA.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 75,502 hrs · 65,949 cycles

RIGHT SIDE CENTER AIR DISTRIBUTION DUCT SUPPORT FITTING AT STA 907 IS CRACKED. REMOVED AND REPLACED BRACKET PER SRM 51-10-2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,502 hrs · 65,949 cycles

FRAME CRACKED AT STRINGER CUTOUT, BS 380 STR 26L. REPAIRED IAW SRM 53-00-07-2R.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,502 hrs · 65,949 cycles

AFT CARGO, FWD DOOR FRAME, INNER CLOSURE WEB CRACKED AT FWD LWR CORNER. REMOVED AND REPLACED FRAME PER SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 75,502 hrs · 65,949 cycles

FWD CARGO PIT, STA 500D+5", LBL 6", CORROSION ON LEFT KEEL BEAM ON O/B SIDE (MKD). REPAIRED LEFT KEEL BEAM AT STA 500D+5 PER SRM 53-30-12-2R-2.

Part: LIGHT — CRACKED (CABIN) · airframe 75,502 hrs · 65,949 cycles

LEFT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT CRACKED AT ROW 12. REMOVED AND REPLACED LIGHT PER MM.

Part: COVER — LOOSE (R2 DOOR) · airframe 75,244 hrs · 65,759 cycles

R2 DOOR SLIDE COVER LOOSE. REMOVED AND REPLACED DOOR SLIDE COVER PER AMM.

Part: FLAP — DELAMINATED (RT WING) · airframe 75,244 hrs · 65,759 cycles

RIGHT WING OUTBOARD AFT FLAP DELAMINATED ON TRAILING EDGE. REMOVED AND REPLACED AFT FLAP PER MM.

Part: SLAT — CHAFED (LT WING) · airframe 75,244 hrs · 65,759 cycles

NR 4 SLAT AFT UPPER INBOARD END CHAFED THROUGH PREVIOUS REPAIR. REPAIRED SLAT PER SRM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 75,219 hrs · 65,739 cycles

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

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 74,412 hrs · 65,110 cycles

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

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 74,390 hrs · 65,093 cycles

SHEAR TIE CORRODED AT BS 986.5, STR 25L. REMOVED AND REPLACED SHEAR TIE IAW SRM AND DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 74,390 hrs · 65,093 cycles

STRINGER CORRODED BETWEEN BS 968 TO BS 986.5, STR 25L. REMOVED AND REPLACED STRINGER IAW SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,390 hrs · 65,093 cycles

SKIN CRACKED AT BS 971, STR 24L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,390 hrs · 65,093 cycles

FUSELAGE SKIN CRACKED AT R2 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN IAW ER AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,390 hrs · 65,093 cycles

SKIN CRACKED AT BS 500A+ 6, STR 19L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,390 hrs · 65,093 cycles

SKIN CRACKED AT BS 500A+ 14, STR 19L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,390 hrs · 65,093 cycles

FUSELAGE SKIN CRACKED AT BS 380, STR 15R. REPAIRED SKIN PER ER AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,390 hrs · 65,093 cycles

SKIN CRACKED AT BS 500B+ 13, STR 16L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,390 hrs · 65,093 cycles

SKIN CRACKED AT BS 520, STR 13R. REPAIR SKIN IAW ER AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,384 hrs · 65,091 cycles

SKIN CRACKED AT BS 500A+6, STR 19L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,384 hrs · 65,091 cycles

SKIN CRACKED AT BS 500A+14, STR 19L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,384 hrs · 65,091 cycles

FUSELAGE SKIN CRACKED AT BS 380, STR 15R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,384 hrs · 65,091 cycles

SKIN CRACKED AT BS 500B+6, STR 16L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,384 hrs · 65,091 cycles

SKIN CRACKED AT BS 520, STR 13R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 265-271.3 S9L) · airframe 73,447 hrs · 64,378 cycles

FUSELAGE SKIN IS CRACKED AT BS 265 TO 271.3, S9L. REPAIRED SKIN IAW SRM 53-00-01.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,447 hrs · 64,378 cycles

FUSELAGE SKIN IS CRACKED FROM BS 265-271, STR 9L. REPAIRED SKIN PER SRM.

Part: MODULE — FAULTY (HYDRAULIC SYS) · airframe 72,091 hrs · 63,382 cycles

DECLARED EMERGENCY - AT FL340 HYDRAULIC FUMES AND SMOKE IN CABIN. REMOVED AND REPLACED HYDRAULIC AIR PRESSURE MODULE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,048 hrs · 63,348 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 500D+6, STR 16R. REPAIRED SKIN PER ER AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,063 hrs · 63,360 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND SKIN CRACKED AT BS 500B+5, STR 15R. REPAIRED SKIN IAW ER AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,063 hrs · 63,360 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND SKIN CRACKED AT BS 500D+6, STR 16R. REPAIRED SKIN IAW EA AND ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,048 hrs · 63,348 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 500B+5, STR 15R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,048 hrs · 63,348 cycles

DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT BS 500D+6, STR 16R. REPAIRED SKIN PER ER AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,048 hrs · 63,348 cycles

DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT BS 500B+5, STR 15R. REPAIRED SKIN PER ER AND EA.

Part: ACTUATOR — BROKEN (SPOILER) · airframe 71,999 hrs · 63,310 cycles

RT WING NR 5 GROUND SPOILER O/B ACTUATOR LOWER MOUNTING TAB BROKEN. REMOVED AND REPLACED ACTUATOR PER MM.

Part: SKIN — DELAMINATED (SPOILER) · airframe 71,136 hrs · 62,636 cycles

DURING SCHEDULED 16Y CHECK FOUND, RT WING NR 9 SPOILER LOWER SKIN DELAMINATED. REPAIRED SPOILER PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 71,136 hrs · 62,636 cycles

DURING SCHEDULED 16Y CHECK FOUND, CORROSION ON FWD AND AFT FACE OF FRAME LOCATED BS 727D BETWEEN STR 27L TO STR 27R AFT CARGO COMPARTMENT. REPAIRED SECTION OF FRAME IAW SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 71,136 hrs · 62,636 cycles

DURING SCHEDULED 16Y CHECK FOUND, AFT CARGO COMPARTMENT CORRODED ON INTERNAL SKIN ON BS .942 ST2 26L. REPAIRED SKIN IAW EO.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 71,136 hrs · 62,636 cycles

DURING SCHEDULED 22Y CHECK, FOUND CORROSION AFT CABIN CROSS BEAM, BS 986.5 BETWEEN BL 0 TO LBL 45. REPAIRED PER DOC.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 71,136 hrs · 62,636 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CRACK PAX CABIN, BS 380, STR 2L. REPAIRED PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 71,136 hrs · 62,636 cycles

DURING SCHEDULED 22Y CHECK, FOUND CRACK AFT PRESSURE BULKHEAD WEB, BS 1016. REPAIRED PER DOC.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,136 hrs · 62,636 cycles

DURING SCHEDULED 22Y CHECK, FOUND SKIN CRACK IN CHEM-MILLED AREA, BS 747+2.5 AND BELOW S-19L. REPAIRED PER DOC.

Part: SKIN — CORRODED (FUSELAGE) · airframe 71,136 hrs · 62,636 cycles

DURING SCHEDULED 22Y CHECK, FOUND CORROSION NOSE FWD COMPARTMENT BS 227.8, BETWEEN RBL 10 TO LBL 10. REPAIRED PER SRM.

Part: STRAP — CORRODED (FUSELAGE) · airframe 71,136 hrs · 62,636 cycles

DURING SCHEDULED 22Y CHECK FOUND CORROSION FWD CARGO COMPARTMENT ON TEAR STRAP, BS 500+9, STR 26R. REPAIRED PER DOC.

Part: WEB — CRACKED (FUSELAGE) · airframe 71,136 hrs · 62,636 cycles

DURING SCHEDULED 22Y CHECK, FOUND CRACK ON WEB, BS 227.8 RBL 16. REPAIRED PER DOC.

Part: WEB — CRACKED (FUSELAGE) · airframe 71,136 hrs · 62,636 cycles

DURING SCHEDULED 22Y CHECK, FOUND CRACK ON WEB, BS 227.8 LBL 16. REPAIRED PER DOC.

Part: SKIN — CRACKED (L1 DOOR) · airframe 71,136 hrs · 62,636 cycles

DURING SCHEDULED 22Y CHECK, FOUND CRACK ON INNER SKIN L1 DOOR. REPAIRED PER DOC.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 71,136 hrs · 62,636 cycles

DURING SCHEDULED 22Y CHECK, FOUND CRACK PAX CABIN, UPPER CHORD, BS 639 ON FLOORBEAM LBL 45.5 CENTER SECTION. REPAIRED PER DOC.

Part: STRUCTURE — CRACKED (RT WING) · airframe 71,136 hrs · 62,636 cycles

DURING SCHEDULED 22Y CHECK, FOUND CRACK FUEL TANK OF RIGHT WING, LWR CHORD, WBL 135.50, STR 2 TO STR 3. REPAIRED PER DOC.

Part: WEB — CORRODED (FUSELAGE) · airframe 71,136 hrs · 62,636 cycles

DURING SCHEDULED 22Y CHECK, FOUND CORROSION ON WEB ON FLOOR STRUCTURE AFT CABIN, BS 1006 TO BS 1016, STR 17R. REPAIRED PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,136 hrs · 62,636 cycles

DURING SCHEDULED 22Y CHECK, FOUND CRACK ON INTERNAL SKIN IN AFT CARGO COMPARTMENT, BETWEEN 727D, BETWEEN STR 27L TO STA 27. REPAIRED PER SWA DOC.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,136 hrs · 62,636 cycles

DURING SCHEDULED 22Y CHECK, FOUND CRACK UPPER AFT CORNER CUTOUT SKIN AFT OF AFT ENTRY DOOR, BS 980. REPAIRED PER SRM.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 71,136 hrs · 62,636 cycles

DURING SCHEDULED 22Y CHECK FOUND CORROSION ON CROSS BEAM LOCATED, BS 986.5, BL 0 TO RBL 45. REPAIRED PER DOC.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 71,136 hrs · 62,636 cycles

DURING SCHEDULED 22Y CHECK, FOUND CRACK ON STRINGER, BTW BS 294.5 AND BS 312, STR 22R. REPAIRED PER SRM.

Part: COVER — CRACKED (CABIN) · airframe 71,136 hrs · 62,636 cycles

DURING SCHEDULED 22Y CHECK, FOUND CRACK ON L1 EMERGENCY EXIT LIGHT. REPAIRED PER DOC.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,136 hrs · 62,636 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 803, STR 19L. REPAIRED SKIN PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,136 hrs · 62,636 cycles

DURING SCHEDULED 22Y CHECK, FOUND CRACK ON BODY FRAME, CENTER SECTION PAX COMPARTMENT BS 597, STR 17L. REPAIRED PER DOC.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,136 hrs · 62,636 cycles

DURING SCHEDULED 22Y CHECK, FOUND CRACK ON KEEL BEAM SKIN, BS 706, BELOW STR 27. REPAIRED PER DOC.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 71,136 hrs · 62,636 cycles

DURING SCHEDULED 22Y CHECK, FOUND CRACK IN AFT CARGO COMPARTMENT, BS 927, STR 26L. REPAIRED PER SRM.

Part: SOCKET — INOPERATIVE (CABIN) · airframe 71,136 hrs · 62,636 cycles

DURING SCHEDULED 22Y CHECK, FOUND BROKEN PLUG ON EMERGENCY EXIT LIGHT COVER, AFT GALLEY DOOR CUTOUT STRUCTURE, BS 993 AND BS 10006, STR 12R AND 13R. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,136 hrs · 62,636 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT UPPER AFT CORNER CUTOUT. REPAIRED SKIN PER SRM.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 71,136 hrs · 62,636 cycles

DURING SCHEDULED 22Y CHECK, FOUND CROSS BEAM LOWER SURFACE CORRODED AT BS 947.5, RBL 5. REPAIRED BEAM PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 71,136 hrs · 62,636 cycles

DURING SCHEDULED 22Y CHECK, FOUND CORROSION ON FLOORBEAM BS 1016, LBL 34 AFT PAX COMPARTMENT. REPAIRED PER SRM.

Part: SILL — CORRODED (FUSELAGE) · airframe 71,136 hrs · 62,636 cycles

DURING SCHEDULED 22Y CHECK, FOUND R1 DOOR LOWER SILL CHORD CORRODED BETWEEN BS 294.5 TO BS 332.1. REMOVED AND REPLACED CHORD PER BAC DWG.

Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 71,136 hrs · 62,636 cycles

DURING SCHEDULED 22Y CHECK, FOUND KEEL BEAM SKIN CRACKED AT BS 706, STR 27L. REMOVED AND REPLACED BEAM PER SRM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 71,136 hrs · 62,636 cycles

DURING SCHEDULED 22Y CHECK, FOUND RT WING O/B AFT FLAP DELAMINATED ON LOWER SURFACE. REMOVED AND REPLACED AFT FLAP PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,136 hrs · 62,636 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 2L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,136 hrs · 62,636 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 947, STR 25R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: SLAT — DELAMINATED (RT WING) · airframe 71,136 hrs · 62,636 cycles

DURING SCHEDULED 22Y CHECK, FOUND RT WING NR 4 SLAT DELAMINATED AT I/B END. REPAIRED SLAT PER SRM.

Part: BRACKET — CRACKED (EVAC SLIDE) · airframe 71,136 hrs · 62,636 cycles

DURING SCHEDULED 22Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE FWD BRACKET CRACKED. REMOVED AND REPLACED BRACKET PER SRM.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 71,136 hrs · 62,636 cycles

DURING SCHEDULED 22Y CHECK, FOUND LT WING I/B END FORE FLAP DELAMINATED AT LOWER SURFACE. REPAIRED FORE FLAP PER SRM.

Part: SLAT — DELAMINATED (RT WING) · airframe 71,136 hrs · 62,636 cycles

DURING SCHEDULED 22Y CHECK, FOUND RT WING NR 5 SLAT DELAMINATED AT I/B END. REPAIRED SLAT PER SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 71,136 hrs · 62,636 cycles

DURING SCHEDULED 22Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 859, LBL 8.10. REPAIRED CHANNEL PER SRM AND EA.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 71,136 hrs · 62,636 cycles

DURING SCHEDULED 22Y CHECK, FOUND CREASE BEAM CHANNEL CRACKED AT BS 616, LBL 64. REPAIRED CHANNEL PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,136 hrs · 62,636 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 2L. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR WEB — CRACKED (FUSELAGE) · airframe 71,136 hrs · 62,636 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR WEB CRACKED AT BS 616, STR 17L. REMOVED AND REPLACED WEB PER SRM AND BAC DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 71,136 hrs · 62,636 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CORRODED AT BS 867, BETWEEN STR 27R TO STR 27L. REPAIRED FRAME PER SRM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 71,136 hrs · 62,636 cycles

DURING SCHEDULED 22Y CHECK, FOUND SUPPORT ANGLE CORRODED BETWEEN BS 1000 TO BS 1016, STR 17R. R&R ANGLE PER SRM AND BAC DWG.

Part: SILL — CORRODED (FUSELAGE) · airframe 71,136 hrs · 62,636 cycles

DURING SCHEDULED 22Y CHECK, FOUND LOWER SILL CORRODED AT L1 DOOR BETWEEN BS 303.9 TO BS 360. REMOVED AND REPLACED SILL PER SRM AND BAC DWG.

Part: SPOILER — DELAMINATED (LT WING) · airframe 71,136 hrs · 62,636 cycles

DURING SCHEDULED 22Y CHECK, FOUND LT WING NR 1 SPOILER DELAMINATED. REPAIRED SPOILER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,136 hrs · 62,636 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 25L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,136 hrs · 62,636 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 21L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,136 hrs · 62,636 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 71,136 hrs · 62,636 cycles

DURING SCHEDULED 22Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 856, LBL 12.50. REPAIRED CHANNEL PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,136 hrs · 62,636 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 22L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,136 hrs · 62,636 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 18L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,136 hrs · 62,636 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 18L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,136 hrs · 62,636 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 23L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,136 hrs · 62,636 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 23L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,136 hrs · 62,636 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 5L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,136 hrs · 62,636 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 927, STR 20L. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 71,136 hrs · 62,636 cycles

DURING SCHEDULED 22Y CHECK, FOUND LT WING O/B AFT FLAP I/B END UPPER SURFACE DELAMINATED. REPAIRED AFT FLAP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,136 hrs · 62,636 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 9R. REMOVED AND REPLACED CLIP PER SRM.

Part: CABLE — FRAYED (EVAC SLIDE) · airframe 71,136 hrs · 62,636 cycles

DURING SCHEDULED 22Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE CABLE FRAYED. REMOVED AND REPLACED CABLE PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 71,136 hrs · 62,636 cycles

DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM CORRODED AT BS 328, LBL 28. REPAIRED BEAM PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,136 hrs · 62,636 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 5R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,136 hrs · 62,636 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,136 hrs · 62,636 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,136 hrs · 62,636 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: CABLE — FRAYED (EVAC SLIDE) · airframe 71,136 hrs · 62,636 cycles

DURING SCHEDULED 22Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE CABLE FRAYED. REMOVED AND REPLACED CABLE PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,136 hrs · 62,636 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,136 hrs · 62,636 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,136 hrs · 62,636 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 1121, STR 2L. REMOVED AND REPLACED SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,136 hrs · 62,636 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,136 hrs · 62,636 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,136 hrs · 62,636 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 71,136 hrs · 62,636 cycles

DURING SCHEDULED 22Y CHECK, FOUND CRACKS AROUND FLIGHT DECK FLOOR WEB STA 244 & 248, RBL 17 & 23. REPAIRED FLOOR WEB PER ACO.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 71,136 hrs · 62,636 cycles

DURING SCHEDULED 22Y CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACK, BETWEEN STA 708 AND STA 710, BL 0. REPAIRED PER SI.

Part: MOTOR — FAULTY (GASPER FAN) · airframe 71,105 hrs · 62,613 cycles

FLIGHT ATTENDANTS AND PASSENGERS COMPLAINED OF AN ODOR IN CABIN. REMOVED AND REPLACED GASPER FAN MOTOR ASSY PER MM.

Part: CLAMP — LOOSE (EVAC SLIDE) · airframe 70,862 hrs · 62,435 cycles

R1 DOOR EMERGENCY EVAC SLIDE CLAMP LOOSE IN CASE. SECURED SLIDE PER MT.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 70,405 hrs · 62,074 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,374 hrs · 62,050 cycles

DURING SCHEDULED OTS CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,374 hrs · 62,050 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 727E, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,374 hrs · 62,050 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 380, STR 15L. REPAIRIED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,374 hrs · 62,050 cycles

DURING SCHEDULED OTS CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,374 hrs · 62,050 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 803, STR 19L. REPAIRIED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,374 hrs · 62,050 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 729D, STR 19L. REPARIED SKIN PER EA.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 70,374 hrs · 62,050 cycles

DURING SCHEDULED OTS CHECK, FOUND KEEL BEAM FWD END LOWER SUPPORT ANGLE CORRODED. REPAIRED BEAM PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,374 hrs · 62,050 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 727B, STR 14R. REPARIED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 70,371 hrs · 62,048 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. ADJUSTED SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 69,738 hrs · 61,550 cycles

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

Part: SLIDE — LOOSE (R2 DOOR) · airframe 69,541 hrs · 61,398 cycles

DURING SCHEDULED HC2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,883 hrs · 60,894 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER AFT CORNER CUTOUT. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,881 hrs · 60,893 cycles

DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT BS 326.5, STR 17R. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,881 hrs · 60,893 cycles

DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT BS 503.5C, STR 15R. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (LT WING) · airframe 68,881 hrs · 60,893 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING SKIN CRACKED AT RSS 236. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,883 hrs · 60,894 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 328 -2.5", STR 17R. REPAIRED SKIN PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,883 hrs · 60,894 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500D, STR 14R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,883 hrs · 60,894 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 20R TO STR 21R. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (LT WING) · airframe 68,883 hrs · 60,894 cycles

DURING SCHEDULED SPV CHECK, FOUND LT WING UPPER SKIN CRACKED AT RSS 236. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,883 hrs · 60,894 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 503.5C, STR 15R. REPAIRED SKIN PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,883 hrs · 60,894 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,883 hrs · 60,894 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 500B, BETWEEN STR 20L TO STR 21L. REPAIRED FRAME PER SRM AND SI.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,883 hrs · 60,894 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 500B, BETWEEN STR 20R TO STR 21R. REPAIRED FRAME PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 67,494 hrs · 59,871 cycles

DURING SCHEDULED MV2 CHECK, FOUND STRINGER CLIP CRACKED AT BS 500, STR 16L. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,494 hrs · 59,871 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 500, BETWEEN STR 15L TO STR 16L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,494 hrs · 59,871 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 827, STR 16L. REPAIRED SKIN PER SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 67,494 hrs · 59,871 cycles

DURING SCHEDULED MV2 CHECK, FOUND CENTER CABIN OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,494 hrs · 59,871 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 767, BETWEEN STR 15L TO STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,494 hrs · 59,871 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 770, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,493 hrs · 59,870 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 759, STR 18R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,494 hrs · 59,871 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 759, STR 18R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,493 hrs · 59,870 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 932, STR 24L. REPAIRED SKIN PER EA.

Part: FLAP — DELAMINATED (RT WING) · airframe 67,281 hrs · 59,712 cycles

RIGHT WING FLAP O/B TRAILING EDGE DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 66,957 hrs · 59,475 cycles

DURING SCHEDULED MV1 CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,813 hrs · 59,372 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,816 hrs · 59,375 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED BETWEEN BS 974 TO BS 980, STR 21L. REPAIRED SKIN PER SWA EA.

Part: SLIDE — LOW PRESSURE (L2 DOOR) · airframe 65,916 hrs · 58,700 cycles

L2 DOOR EMERGENCY EVAC SLIDE PRESSURE LOW. REMOVED AND REPLACED SLIDE PER MM.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 65,658 hrs · 58,507 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE BEAR STRAP SKIN CRACKED AT R1 DOOR LOWER CUTOUT, BS 291, WL 232. REPAIRED SKIN PER AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,658 hrs · 58,507 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE BEAR STRAP SKIN CRACKED AT R1 DOOR UPPER HINGE CUTOUT, BS 291, WL 259. REPAIRED SKIN PER AAR EA.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 65,658 hrs · 58,507 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT OVERWING EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED BATTERY PACK PER ACO.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 65,658 hrs · 58,507 cycles

DURING SCHEDULED 20Y CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,658 hrs · 58,507 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE BEAR STRAP SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT, BS 303, BETWEEN WL 258 TO WL 260. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,658 hrs · 58,507 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE BEAR STRAP SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT, BS 291, BETWEEN WL 231 TO WL 232. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,658 hrs · 58,507 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE BEAR STRAP SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT, BETWEEN BS 303 TO BS 304, BETWEEN WL 236 TO WL 238. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 65,658 hrs · 58,507 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT OVERWING EMERGENCY EXIT SIGN LAMP BURNED OUT. RELAMPED PER MM.

Part: STRIP — MISSING (CABIN) · airframe 65,658 hrs · 58,507 cycles

DURING SCHEDULED 20Y CHECK, FOUND FWD CABIN EEPLS STRIP MISSING. INSTALLED STRIP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,658 hrs · 58,507 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE BEAR STRAP SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT, BS 291, WL 259. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 65,658 hrs · 58,507 cycles

DURING SCHEDULED 20Y CHECK, FOUND L2 DOOR EMERGENCY EXIT SIGN LAMP BURNED OUT. REMOVED AND REPLACED LAMP PER MM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 65,658 hrs · 58,507 cycles

DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM CRACKED AT BS 685, LBL 24. REPAIRED BEAM PER SRM.

Part: SLAT — DELAMINATED (RT WING) · airframe 65,658 hrs · 58,507 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT WING NR 5 SLAT I/B UPPER CORNER SURFACES DELAMINATED. REMOVED AND REPLACED SLAT PER SRM.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 65,658 hrs · 58,507 cycles

DURING SCHEDULED 20Y CHECK, FOUND SKIN DAMAGED BETWEEN BS 727B TO BS 727C, BETWEEN STR 20L TO STR 21L. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 65,658 hrs · 58,507 cycles

DURING SCHEDULED 20Y CHECK, FOUND R2 DOOR EMERGENCY EXIT SIGN LAMP BURNED OUT. REMOVED AND REPLACED LAMP PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,658 hrs · 58,507 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 18L. REMOVED AND REPLACED CLIP PER SRM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 65,658 hrs · 58,507 cycles

DURING SCHEDULED 20Y CHECK, FOUND R2 OVERWING EMERGENCY EXIT SIGN LAMP BURNED OUT. REMOVED AND REPLACED LAMP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,658 hrs · 58,507 cycles

DURING SCHEDULED 20Y CHECK, FOUND SKIN CRACKED AT BS 113, STR 15R. REPAIRED SKIN PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 65,658 hrs · 58,507 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500, LBL 0. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 65,658 hrs · 58,507 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 947, BETWEEN STR 25L TO STR 24L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 65,658 hrs · 58,507 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT WING NR 4 SLAT I/B UPPER SURFACE DELAMINATED. REPAIRED SLAT PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 65,658 hrs · 58,507 cycles

DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM OVER CENTER WING BOX UPPER CHORD CRACKED AT BS 665, RBL 1, WL 208. REPAIRED BEAM PER SI.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,658 hrs · 58,507 cycles

DURING SCHEDULED 20Y CHECK, FOUND SKIN CRACKED AT BS 303, STR 16L. REPAIRED SKIN PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 65,658 hrs · 58,507 cycles

DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM OVER CENTER WING BOX UPPER CHORD CRACKED AT BS 660, BBL 0, WL 208. REPAIRED BEAM PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,658 hrs · 58,507 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 18L. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 65,658 hrs · 58,507 cycles

DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM OVER CENTER WING BOX CRACKED AT BS 673, LBL 24. REPAIRED BEAM PER AAR EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,658 hrs · 58,507 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 227, STR 15R. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 65,658 hrs · 58,507 cycles

DURING SCHEDULED 20Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED BS 676, RBL 34.8. REPAIRED BEAM PER AAR EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 65,658 hrs · 58,507 cycles

DURING SCHEDULED 20Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED BETWEEN BS 663 TO BS 669, RBL 24.8. REPAIRED BEAM PER AAR EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 65,658 hrs · 58,507 cycles

DURING SCHEDULED 20Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 727B, RBL 45.5. REPAIRED BEAM PER AAR EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,658 hrs · 58,507 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 21R. REMOVED AND REPLACED CLIP PER SRM.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 65,658 hrs · 58,807 cycles

DURING SCHEDULED 20Y CHECK, FOUND MLG WHEEL WELL AFT BULKHEAD SUPPORT BEAM ATTACH FITTING CRACKED AT BS 728, LBL 45. REMOVED AND REPLACED FITTING PER SRM.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 65,658 hrs · 58,507 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT WING TRAILING EDGE O/B FORE FLAP UPPER SURFACE DELAMINATED. REPAIRED FORE FLAP PER SRM.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 65,658 hrs · 58,507 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT WING NR 5 SLAT O/B UPPER CORNER SURFACE DELAMINATED. REPAIRED SLAT PER SRM.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 65,658 hrs · 58,507 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT WING TRAILING EDGE I/B FORE FLAP UPPER SURFACE DELAMINATED. REPAIRED FORE FLAP PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 65,488 hrs · 58,384 cycles

DURING SCHEDULED HC1 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 65,158 hrs · 58,158 cycles

DURING SCHEDULED MV1 CHECK, FOUND OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,158 hrs · 58,158 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 500B, STR 15L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,158 hrs · 58,158 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 305, STR 18R. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 64,674 hrs · 57,808 cycles

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

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 64,674 hrs · 57,808 cycles

FOUND L2 DOOR SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,619 hrs · 57,773 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 465, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,619 hrs · 57,773 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 474, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,387 hrs · 57,618 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 435, STR 1. REPAIRED SKIN PER SWA EA.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 64,232 hrs · 57,500 cycles

DURING SCHEDULED SPV CHECK, FOUND EXTERNAL LT EMERGENCY EXIT LIGHT INOP AT AFT LOWER WING TO BODY FAIRING. REPLACED LIGHT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,678 hrs · 56,384 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 508D, 15L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,678 hrs · 56,384 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 737E, 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,678 hrs · 56,384 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 973, 23L. REPAIRED SKIN PER SRM.

Part: FAN — FAULTY (E&E BAY) · airframe 62,523 hrs · 56,259 cycles

CREW REPORTED ELECTRICAL ODOR IN CABIN. TURNED OFF RECIRC AND GASPER FANS, ODOR DISSIPATED. REMOVED AND REPLACED RECIRC FAN PER MM.

Part: WINDOW — ARCED (COCKPIT) · airframe 62,319 hrs · 56,116 cycles

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

Part: PRESSURE PANEL — CRACKED (NLG W/W) · airframe 61,344 hrs · 55,390 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT NLG W/W CEILING PANEL CRACKED AT BS 257.8. REPAIRED PANEL PER SWA EA.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 61,353 hrs · 55,398 cycles

DURING SCHEDULED MV2 CHECK, FOUND MID CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,353 hrs · 55,398 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500A, STR 17L. REPAIRED SKIN PER SRM.

Part: SIGN — LOOSE (EMERGENCY LIGHT) · airframe 61,078 hrs · 55,187 cycles

RIGHT OVERWING EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 60,838 hrs · 55,007 cycles

DURING SCHEDULED HC1 CHECK, FOUND RIGHT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. REMOVED AND REPLACED FLAP PER MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 60,448 hrs · 54,692 cycles

DURING SCHEDULED MV1 CHECK, FOUND RIGHT WING INBOARD T/E AFT FLAP DELAMINATED AT INBOARD T/E END. REMOVED AND REPLACED FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,448 hrs · 54,692 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 758, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,448 hrs · 54,692 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 312, STR 19R. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 60,214 hrs · 54,493 cycles

L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,106 hrs · 53,610 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 663.75, STR 1. REPAIRED FRAME PER ER.

Part: CREASE BEAM — CRACKED (BS 192 S17R) · airframe 59,106 hrs · 53,610 cycles

DURING SCHEDULED 18Y CHECK, FOUND CREASE BEAM WEB CRACKED AT BS 192.5, STR 17R. REPAIRED WEB PER SRM.

Part: STRINGER SPLICE — CRACKED (BS 360 S15L) · airframe 59,106 hrs · 53,610 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 15L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: FRAME — CRACKED (BS 188 S17R) · airframe 59,106 hrs · 53,610 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 188, STR 17R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 312 S6L) · airframe 59,106 hrs · 53,610 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 312, STR 6L. REPAIRED FRAME PER ER.

Part: STIFFENER — CRACKED (BS 1016 S9L) · airframe 59,106 hrs · 53,610 cycles

DURING SCHEDULED 18Y CHECK, FOUND AFT PRESSURE BULKHEAD STIFFENER CRACKED AT BS 1016, STR 9L. REPAIRED STIFFENER PER SRM.

Part: FLOORBEAM — CRACKED (BS 986) · airframe 59,106 hrs · 53,610 cycles

DURING SCHEDULED 18Y CHECK, FOUND FLOORBEAM CRACKED AT BS 986.5, RBL 5. REPAIRED FLOORBEAM PER ER.

Part: SKIN — CRACKED (BS 503D S12R) · airframe 59,106 hrs · 53,610 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 503D, STR 12R. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727C S4L) · airframe 59,106 hrs · 53,610 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 380 S16R) · airframe 59,106 hrs · 53,610 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 16R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (BS 400 S8L) · airframe 59,106 hrs · 53,610 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 440 S9L) · airframe 59,106 hrs · 53,610 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — CRACKED (BS 528) · airframe 59,106 hrs · 53,610 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE SKIN CRACKED AT AIR CONDITIONING DOOR CUTOUT RT FWD CORNER BS 528. REPAIRED SKIN PER ER.

Part: STRINGER CLIP — CRACKED (BS 727D S5R) · airframe 59,106 hrs · 53,610 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 400 S7L) · airframe 59,106 hrs · 53,610 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 440 S8L) · airframe 59,106 hrs · 53,610 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 616 S2R) · airframe 59,106 hrs · 53,610 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 2R. REMOVED AND REPLACED STR CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 294 S13L) · airframe 59,106 hrs · 53,610 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 13L. REMOVED AND REPLACED STR CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 616 S4L) · airframe 59,106 hrs · 53,610 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 4L. REMOVED AND REPLACED STR CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 616 S4R) · airframe 59,106 hrs · 53,610 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 4R. REMOVED AND REPLACED STR CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 597 S4L) · airframe 59,106 hrs · 53,610 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 4L. REMOVED AND REPLACED STR CLIP PER SRM.

Part: WEB — CRACKED (NLG W/W) · airframe 59,106 hrs · 53,610 cycles

DURING SCHEDULED 18Y CHECK, FOUND NLG W/W WEB CRACKED AT BS 251, LBL 7.75. REPAIRED WEB PER ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 59,106 hrs · 53,610 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 59,106 hrs · 53,610 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 12R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: PRESSURE PANEL — CRACKED (NLG W/W) · airframe 59,106 hrs · 53,610 cycles

DURING SCHEDULED 18Y CHECK, FOUND NLG WHEEL WELL WEB CRACKED AT BS 251, RBL 7.75. REPAIRED WEB PER ACO.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 59,106 hrs · 53,610 cycles

DURING SCHEDULED 18Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 460 TO BS 480, STR 17L. REMOVED AND REPLACED CREASE BEAM WEB PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 59,106 hrs · 53,610 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 359, STR 14L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: HOOK — LOOSE (L2 DOOR) · airframe 59,106 hrs · 53,610 cycles

DURING SCHEDULED 18Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK LOOSE. REMOVED AND REPLACED GIRT BAR HOOK PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,106 hrs · 53,610 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8R. REPAIRED FRAME PER SWA EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 59,106 hrs · 53,610 cycles

DURING SCHEDULED 18Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 440 TO BS 460, STR 17L. REMOVED AND REPLACED CREASE BEAM WEB PER SRM.

Part: HOOK — LOOSE (L1 DOOR) · airframe 59,106 hrs · 53,610 cycles

DURING SCHEDULED 18Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK LOOSE. REMOVED AND REPLACED GIRT BAR HOOK PER MM.

Part: FRAME — CRACKED (BS 616) · airframe 59,106 hrs · 53,610 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, LBL 65, WL 201. REPAIRED FRAME PER SRM.

Part: HOOK — LOOSE (R1 DOOR) · airframe 59,106 hrs · 53,610 cycles

DURING SCHEDULED 18Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR HOOK LOOSE. REMOVED AND REPLACED GIRT BAR HOOK PER MM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 59,106 hrs · 53,610 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE SKIN CORRODED AT GROUND AIR HOOK UP DOOR CUTOUT BS 528, LBL 3 TO RBL 3. REPAIRED SKIN PER SWA EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 59,021 hrs · 53,539 cycles

BULL NOSE EMERGENCY EXIT LIGHT INOP AT ROW 15 DEF. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SKIN — CRACKED (BS 376 S15L) · airframe 58,992 hrs · 53,519 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 376, STR 15L. REPAIRED SKIN PER SWA EA.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 58,805 hrs · 53,382 cycles

BULLNOSE EMERGENCY EXIT LIGHT COVER MISSING AT ROW 16 DEF. INSTALLED COVER PER MM.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 58,805 hrs · 53,382 cycles

BULLNOSE EMERGENCY EXIT LIGHT COVER MISSING AT ROW 1 DEF. INSTALLED COVER PER MM.

Part: SKIN — CRACKED (BS 750 S18L) · airframe 58,793 hrs · 53,372 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELGAE SKIN CRACKED AT BS 750, STR 18L. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 58,793 hrs · 53,372 cycles

DURING SCHEDULED C4 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 58,793 hrs · 53,372 cycles

DURING SCHEDULED C4 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: STRAP — CORRODED (FRAME) · airframe 57,784 hrs · 52,579 cycles

DURING SCHEDULED SPV CHECK, FOUND AFT CARGO DOOR CUTOUT FWD FRAME STRAP CORRODED AT BS 807, STR 25R. REMOVED AND REPLACED STRAP PER SRM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,346 hrs · 52,240 cycles

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

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,172 hrs · 52,094 cycles

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

Part: STRUCTURE — DELAMINATED (RT FOREFLAP) · airframe 56,846 hrs · 51,841 cycles

DURING SCHEDULED SPV CHECK, FOUND RIGHT WING OUTBOARD FORE FLAP DELAMINATED AT INBOARD SIDE. REMOVED AND REPLACED FORE FLAP PER MM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 56,379 hrs · 51,497 cycles

LEFT OVERWING EMERGENCY BULLNOSE LIGHT LENS LOOSE. REMOVED AND REPLACED LENS ASSY PER MM.

Part: SKIN — CRACKED (BS 378) · airframe 55,875 hrs · 51,124 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 378.5, LBL 3, AFT SIDE OF E & E COOLING DUCT CUTOUT. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 747) · airframe 55,663 hrs · 50,982 cycles

DURING WALKAROUND INSP, FOUND FUSELAGE SKIN CRACKED AT BS 747, STR 19R. REPAIRED SKIN PER SWA EA & SRM.

Part: SIGN — MISSING (CABIN) · airframe 55,440 hrs · 50,800 cycles

FOUND MID CABIN OVERHEAD EMERGENCY EXIT SIGN MISSING. INSTALLED SIGN PER MM.

Part: SKIN — CRACKED (BS 510D) · airframe 54,424 hrs · 49,985 cycles

DURING WALKAROUND INSP, FOUND FUSELAGE SKIN CRACKED AT BS 510D, STR 16L. REPAIRED SKIN PER SWA EA.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 53,483 hrs · 49,239 cycles

DURING SCHEDULED RON CHECK, FOUND L2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 53,446 hrs · 49,213 cycles

DURING SCHEDULED RON CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,203 hrs · 48,258 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 792, STRINGER 17L, CRACKED. REPAIRED SKIN PER EA.

Part: CABLE — MISROUTED (L2 DOOR SLIDE) · airframe 51,159 hrs · 47,416 cycles

DURING SCHEDULED C4 CHECK, FOUND L2 DOOR EVAC SLIDE CABLE MISROUTED. REROUTED L2 DOOR EVAC SLIDE CABLE PER MM.

Part: SKIN — DELAMINATED (RT WING FLAP) · airframe 51,159 hrs · 47,416 cycles

DURING SCHEDULED C4 CHECK, FOUND RT WING OUTBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED RT OUTBOARD T/E FLAP PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,391 hrs · 46,773 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FRAME AT BS 947, STRINGER 25R, CRACKED. REPAIRED FRAME SECTION PER SRM.

Part: SKIN — DELAMINATED (RT WING FLAP) · airframe 50,364 hrs · 46,747 cycles

DURING SCHEDULED 1/2D CHECK, FOUND RT WING INBOARD FORE FLAP DELAMINATED. REMOVED AND REPLACED RT INBOARD FORE FLAP PER MM.

Part: SKIN — DELAMINATED (RT WING SLAT) · airframe 50,364 hrs · 46,747 cycles

DURING SCHEDULED 1/2D CHECK, FOUND RT WING NR 4 L/E SLAT DELAMINATED. REMOVED AND REPLACED RT WING NR 4 L/E SLAT PER MM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 50,344 hrs · 46,734 cycles

DURING SCHEDULED 1/2D CHECK, FOUND R1 AND L1 DOOR EVAC SLIDES FWD AND AFT GIRT BAR FITTINGS CORRODED. REMOVED AND REPLACED R1 AND L1 DOOR EVAC SLIDES GIRT BAR FITTINGS PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 50,344 hrs · 46,734 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM AT BS 986.5, BL 0 TO RBL 18, CORRODED. REPAIRED FLOORBEAM SECTION PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,340 hrs · 46,731 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN AT AFT ENTRY DOOR LOWER FWD HINGE CUTOUT, CRACKED. REPAIRED SKIN PER ER.

Part: HOOK — CORRODED (GIRT BAR) · airframe 50,340 hrs · 46,731 cycles

DURING SCHEDULED 1/2D CHECK, FOUND L2 AND R2 DOOR EVAC DOOR SLIDES GIRT BAR DOOR HOOKS CORRODED. REMOVED AND REPLACED L2 AND R2 DOOR EVAC SLIDE GIRT BAR DOOR HOOKS PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 50,340 hrs · 46,731 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM AT BS 986, RBL 0 TO RBL 50, CORRODED. REPAIRED FLOORBEAM PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,340 hrs · 46,731 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FRAME AT BS 344, STRINGER 17L, CRACKED. REPAIRED FRAME PER ER.

Part: FITTING — CORRODED (FUSELAGE) · airframe 50,340 hrs · 46,731 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BOTH NLG ACTUATOR ROD FITTINGS, CORRODED. REPAIRED NLG FITTINGS PER ER.

Part: FITTING — CORRODED (R2 DOOR SLIDE) · airframe 50,340 hrs · 46,371 cycles

DURING SCHEDULED 1/2D CHECK, FOUND R2 DOOR EVAC SLIDE GIRT BAR FLOOR ATTACH FITTING ADAPTERS CORRODED. REMOVED AND REPLACED R2 DOOR EVAC SLIDE GIRT BAR ADAPTERS PER MM.

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT) · airframe 50,340 hrs · 46,731 cycles

DURING SCHEDULED 1/2D CHECK, FOUND R2 DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED OVERHEAD EMERGENCY EXIT LIGHT PER MM.

Part: GLOWSTRIP — WORN (CABIN) · airframe 50,340 hrs · 46,731 cycles

DURING SCHEDULED 1/2D CHECK, FOUND PHOTOLUMINESCENT STRIPS AT BS 336 AND BS 948, WORN. REMOVED AND REPLACED PHOTOLUMINESCENT STRIPS PER ACO.

Part: FRAME — CORRODED (FUSELAGE) · airframe 50,340 hrs · 46,731 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FRAME AT BS 787, STRINGER 22L TO STRINGER 25L, CORRODED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,340 hrs · 46,731 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FRAME AT BS 340, STRINGER 23L, CRACKED. REPAIRED FRAME SECTION PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 50,340 hrs · 46,731 cycles

DURING SCHEDULED 1/2D CHECK, FOUND 2 EA STRINGER SPLICES CRACKED AT BS 538, STR 10R, AND BS 908, STR 4R. REMOVED AND REPLACED BOTH STR SPLICES PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 50,340 hrs · 46,731 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 360, STR 14L. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,340 hrs · 46,731 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER TIE CLIP AT BS 500B, STRINGER 4R, CRACKED. REMOVED AND REPLACED STRINGER TIE CLIP PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 50,304 hrs · 46,731 cycles

DURING SCHEDULED 1/2D CHECK, FOUND CREASE BEAM AT R2 DOOR, CORRODED. REMOVED AND REPLACED CREASE BEAM SECTION PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,340 hrs · 46,731 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER TIE CLIP AT BS 500C, STRINGER 26R, CRACKED. REMOVED AND REPLACED TIE CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,203 hrs · 46,622 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 947, STRINGER 25R, CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,203 hrs · 46,622 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 500C, STRINGER 15L, CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,203 hrs · 46,622 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 737, BETWEEN STRINGER 18R AND 19R, CRACKED. REPAIRED SKIN PER SRM.

Part: CIRCUIT CARD — FAULTY (E/E BAY) · airframe 48,531 hrs · 45,290 cycles

AIR TURNBACK, LT MLG UNSAFE LIGHT WOULD NOT EXTINGUISH, CYCLED THE LANDING GEAR AND LIGHT REMAINED ILLUMINATED. REMOVED AND REPLACED M988 LOGIC CARD AND LEFT MLG UPLOCK SWITCH PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,440 hrs · 44,386 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 474, STR 18R. REPAIRED SKIN PER SRM.

Part: GIRT BAR — OUT OF ADJUST (ESCAPE SLIDE) · airframe 47,381 hrs · 44,336 cycles

DURING SCHEDULED C4 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,381 hrs · 44,336 cycles

DURING SCHEDULED C4 CHECK, FOUND BOTH FWD CABIN DOORS AND AFT SVC DOOR OVERHEAD EMERGENCY EXIT LIGHTS HAVE SEVERAL LAMPS INOP. RELAMPED EXIT LIGHTS PER MM.

Part: BUSHING — WORN (RT ELEVATOR) · airframe 47,381 hrs · 44,336 cycles

DURING SCHEDULED C4 CHECK, SWA SI 11138-55, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED RT ELEVATOR TAB NR 1 HINGE HARDWARE AND BUSHING PER MM.

Part: GIRT BAR — OUT OF ADJUST (ESCAPE SLIDE) · airframe 46,535 hrs · 43,685 cycles

DURING SCHEDULED C3 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,535 hrs · 43,685 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 12L. REPAIRED SKIN PER SRM.

Part: LENS — MISSING (CABIN) · airframe 46,422 hrs · 43,593 cycles

OVERHEAD BIN BULL NOSE EMERGENCY EXIT LIGHT LENS MISSING AT ROW 12 DEF. INSTALLED LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 45,613 hrs · 42,926 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D, STR 19R. REPAIRED SKIN PER SRM.

Part: LIGHT — LOOSE (CABIN) · airframe 44,695 hrs · 42,170 cycles

DURING SCHEDULED C1 CHECK, FOUND OVERHEAD BIN BULLNOSE EMERGENCY EXIT LIGHT LOOSE AT ROW NR 9 DEF. SECURED LIGHT PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 44,686 hrs · 42,163 cycles

RT OVERWING EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED EXIT LIGHT ASSY PER MM.

Part: WEB — CRACKED (FUSELAGE) · airframe 41,929 hrs · 39,862 cycles

DURING SCHEDULED 1/4D CHECK, FOUND WEB CRACKED .125 INCH LONG AT BS 178, WL 234 AND LBL 14. REPAIRED WEB PER SRM.

Part: STIFFENER — CRACKED (LT MLG W/W) · airframe 41,929 hrs · 39,862 cycles

DURING SCHEDULED 1/4D CHECK,(SI11051-53) FOUND VERTICAL STIFFENER CRACKED AT BS 663, LBL 6.15. REMOVED AND REPLACED VERTICAL STIFFENER PER SRM.

Part: FLOORBEAM — CORRODED (AFT CARGO) · airframe 41,929 hrs · 39,862 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM CORRODED AT BS 846, RBL 3. REPAIRED FLOORBEAM PER SWA RA.

Part: SHEAR TIE — CRACKED (AFT CARGO) · airframe 41,929 hrs · 39,862 cycles

DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE CRACKED AT BS 727A, STR 25L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (AFT CARGO DOOR) · airframe 41,929 hrs · 39,862 cycles

DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO DOOR, AFT FRAME CRACKED ABOVE LWR DOOR STOP FITTIING. REMOVED AND REPLACED AFT CARGO DOOR FRAME PER SRM.

Part: COVER — MISSING (CABIN) · airframe 41,135 hrs · 39,192 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS COVER MISSING AT AFT CABIN. INSTALLED EEPLS COVER PER MM.

Part: COVER — MISSING (CABIN) · airframe 41,135 hrs · 39,192 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS COVER & END CAP MISSING AT ROW # 1. INSTALLED COVER & END CAP PER MM.

Part: SLAT — CRACKED (LH WING) · airframe 41,135 hrs · 39,192 cycles

DURING SCHEDULED C1 CHECK, FOUND # 1L/E SLAT CRACKED APPROX 1/2 INCH AT 2ND AUX TRACK CUTOUT. REPAIRED SLAT PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 41,096 hrs · 39,165 cycles

DURING SCHEDULED A1 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED EXIT LIGHT PER MM.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 40,966 hrs · 39,054 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BEADED PRESS WEB CRACKED 2 EA AT BS 663, RBL 38 & LBL 32. REPAIRED PRESS WEB PER SWA T1-253-032.

Part: WEB — CRACKED (FUSELAGE) · airframe 40,966 hrs · 39,054 cycles

DURING SCHEDULED SPECIAL, FOUND A .75 LONG VERTICAL BEAM WEB CRACK AT BS 179, LBL 17.1 & WL 227. REPAIRED WEB PER SRM.

Part: TEE CHORD — CRACKED (FUSELAGE) · airframe 40,966 hrs · 39,054 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND T-CHORD CRACKED AT BS 178, LBL 5, WL 185. REPAIRED T-CHORD PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 40,966 hrs · 39,054 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD PRESS WEB CRACKED, RBL 15 & WL 207. REPAIRED BULKHEAD PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 40,966 hrs · 39,054 cycles

DURING SCHEDULED SPECIAL VISIT CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, LBL 17 & WL 184. REPAIRED WEB PER SWA RA.

Part: BEARING — WORN (LT ELEVATOR TAB) · airframe 40,229 hrs · 38,422 cycles

DURING SCHEDULED C4 CHECK, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 TAB HINGE BEARING PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 39,242 hrs · 37,626 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS LOOSE NEAR AFT GALLEY. SECURED EEPLS PER MM.

Part: LENS — LOOSE (CABIN) · airframe 39,242 hrs · 37,626 cycles

DURING SCHEDULED C3 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: LIGHT — CRACKED (CABIN) · airframe 39,185 hrs · 37,579 cycles

EMERGENCY EXIT LIGHT LENS LOOSE/CRACKED AT BULLNOSE, ROW 20 DEF. REPLACED LENS PER MM.

Part: SKIN — CRACKED (RT WING SLAT) · airframe 38,277 hrs · 36,830 cycles

DURING SCHEDULED C2 CHECK, FOUND NR 6 L/E SLAT LOWER SKIN CRACKED AT 2 FASTENER HOLES, APPROX 13 I/B OF ACTUATOR STOP. REPAIRED SLAT PER RA 1-A57-0691.

Part: GIRT BAR — OUT OF ADJ (CABIN) · airframe 38,277 hrs · 36,830 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT SERVICE AND FWD ENTRY DOOR GIRT ASSEMBLIES OUT OF ADJUSTMENT. REPOSITIONED BOTH SLIDE ASSY''S PER MM.

Part: COVER — LOOSE (CABIN FLOOR) · airframe 38,277 hrs · 36,830 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS TRACK COVER LOOSE BY FWD GALLEY. SECURED TRACK COVER PER MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 37,390 hrs · 36,085 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS INOP IN AFT GALLEY. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 36,432 hrs · 35,288 cycles

DURING SCHEDULED BC4 CHECK, FOUND EEPLS FWD END LOOSE. REPAIRED AND SECURED LIGHT ASSY PER MM.

Part: SKIN — CRACKED (BS 731)

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE EXTERNAL SKIN CRACKED, BS 731, STRINGER 19R. REPAIRED SKIN PER SRM.

Part: SKIN — DELAMINATED (RT TE FLAP)

DURING SCHEDULED C2 CHECK, FOUND RT OUTBOARD AFT FLAP DELAMINATED AT INBOARD CORNER. REPAIRED FLAP PER MM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D CHECK, FOUND BS 178 BULKHEAD CRACKED, RBL 4.7. REPAIRED BULKHEAD PER SRM.

Part: BATTERY PACK — DISCHARGED (EMER EXIT)

DURING SCHEDULED A1 CHECK, FOUND RT AFT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK ASSY PER MM.

Part: BULKHEAD — CORRODED (BS 178)

DURING SCHEDULED D-CHECK, FOUND 5 CRACKS AT BS 178 BULKHEAD BETWEEN LBL 6 RBL 6. REPAIRED BULKHEAD PER SRM.

Part: SKIN — CRACKED (HORIZ STAB)

DURING SCHEDULED D-CHECK, FOUND RT HORIZONTAL STAB LOWER SKIN CRACKED IN AFT SPAR, FWD OF NR 1 BALANCE BAY. REPAIRED SKIN PER BFG ER NR 99-5642 AND SRM.

Part: LENS — MISSING (ROW 9D)

DURING SCHEDULED D-CHECK, FOUND EMERGENCY EXIT LIGHT LENS MISSING IN BULLNOSE AT ROW 9D. REPLACED LENS ASSY PER MM.

Part: STRINGER — CRACKED (BS 1141)

DURING SCHEDULED D-CHECK, FOUND BS 1141, STRINGERS 5A LT AND 5A RT CRACKED AT LOWER CHORD. REPAIRED STRINGERS PER SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND CRACKED BULKHEAD, BS 178, RBL 1 - LBL 1. REPAIRED BULKHEAD PER SRM.

Part: BRACKET — CORRODED (PASSENGER DOOR)

DURING SCHEDULED D CHECK, FOUND CORROSION AT FWD ENTRY EVACUATION GIRT BAR FLOOR ATTACH BRACKET, BS 344. REMOVED AND REPLACED ATTACH BRACKET PER SRM.

Part: FRAME — CRACKED (BS 827 & 867)

DURING SCHEDULED D CHECK, FOUND 2 EA FUSELAGE FRAMES CRACKED BS 827, BS 867, BETWEEN STRINGERS 8R-9R. REPAIRED PER ER NR 99-5584.

Part: FRAME — CRACKED (BS 827, 907, 787)

DURING SCHEDULED D CHECK, FOUND 3 EA FUSELAGE FRAMES CRACKED BS 827, BS 907,BS 787, BETWEEN STRINGERS 8L-9L. REPAIRED PER ER NR 99-5584.

Part: FRAME — CRACKED (BS 500, 480, 440)

DURING SCHEDULED D CHECK, FOUND 4 EA FRAMES CRACKED, BS 500C, BS 480, BS 440, BETWEEN STRINGERS 8R-9R, AND BS 440, BETWEEN STRINGERS 8L-9L. REPAIRED FRAMES PER ER NR 99-5584.

Part: FLOORBEAM — CORRODED (BS 859)

DURING SCHEDULED D CHECK, FOUND AFT CARGO COMP FLOORBEAM CORRODED, BS 859,LBL 3.5 AND LBL 7.5. REPAIRED FLOORBEAM PER SRM.

Part: BRACKET — CORRODED (PASSENGER DOOR)

DURING SCHEDULED D-CHECK, FOUND CORROSION ON FWD ENTRY DOOR AFT GIRT BAR ATTACH FLOOR BRACKET. REMOVED AND REPLACED GIRT ATTACH BRACKET PER MM.

Part: FRAME — CRACKED (BS 727)

DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME AT BS 727D, BETWEEN STRINGERS 8L-9L. REPAIRED FRAME PER SRM.

Part: WEB — CORRODED (BS 747-767)

DURING SCHEDULED D CHECK, FOUND CORROSION ON CREASE WEB, BS 747-767, STRINGER 17R. REPAIRED WEB PER SRM.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING SCHEDULE SERVICE CHECK, FOUND FWD CABIN EMERGENCY TRACK LIGHTING INOP. REMOVED AND REPLACED CABIN FWD CABIN EMERGENCY TRACK LIGHT BATTERY PACK PER MM.

Part: INDICATOR — ERRATIC (NR 1 FUEL FLOW)

NR 1 ENGINE FUEL FLOW INDICATOR ERRATIC AND UNRELIABLE, READS ZERO AT TIMES. ALL OTHER ENG INDICATIONS NORMAL. REMOVED AND REPLACED NR 1 FLOW INDICATOR PER MM.

Part: SKIN — CRACKED (CARGO DOOR)

DURING SCHEDULED C4 CHECK, FOUND AFT CARGO DOOR HANDLE CUTOUT CRACKED AT AFT TOP CORNER APPROX .5. REPAIRED PER BOEING SRM.

Part: LIGHT — INOP (CABIN)

DURING SCHEDULED BC4 CHECK, FOUND CABIN AFT EMERGENCY TRACK LIGHT INOP AND ONE IS COVERED. RELAMPED LIGHT AND REPLACED END COVER ON FLOOR EGRESS LIGHTING PER M/M.

Part: SKIN — CRACKED (NR 1 LE FLAP)

DURING SCHEDULED BC 1 CHECK, FOUND CRACKED NR 1 L/E SLAT LOWER SKIN AT INBOARD AUX TRACK. REPAIRED PER BOEING SRM AND TYPICAL REPAIR T1-A57-015.

Part: SKIN — CRACKED (NR 2 LE FLAP)

DURING SCHEDULED BC 1 CHECK, FOUND CRACKED NR 2 L/E SLAT LOWER SKIN AT INBOARD AUX TRACK. REPAIRED PER BOEING TYPICAL REPAIR T1-A57-015 AND BOEING DRAWING 65C30133 SHEET 3.

Part: PANEL — CRACKED (FUSELAGE)

DURING SCHEDULED C4 CHECK, FOUND LWR FUSELAGE FIXED PANEL BELOW KEEL BEAM CRACKED. REPAIRED PER BOEING SRM.

Part: WIRE — CHAFED (B-HYD SYST)

EN ROUTE, EXPERIENCED B-SYSTEM HYDRAULIC OVERHEAT WARNING LIGHT. AIRCRAFT DIVERTED TO DAL AND MADE AN UNEVENTFUL LANDING. REPAIRED CHAFED TEMP SENSOR WIRING AT SUPPLY LINE.

Part: PUMP — MALFUNCTIONED (B-HYD SYST)

DIVERTED TO DAL, DUE TO B SYSTEM HYDRAULIC OVERHEAT LIGHT ILLUMINATING. LANDED WITHOUT INCIDENT. REMOVED AND REPLACED B ELECTRIC PUMP RUN PER BOEING M/M.

Part: BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED A2 CHECK, FOUND FWD SERVICE DOOR OVERHEAD EMERGENCY LIGHTS INOP. REPLACED BATTERY PER BOEING M/M.

Part: CARDS — MALFUNCTIONED (E/E BAY)

AFTER TAKEOFF, UNABLE TO RECEIVE LEFT MAIN GEAR UP AND LOCKED LIGHT. RETURNED TO DAL AND MADE AN UNEVENTFUL LANDING WITH NORMAL GEAR INDICATION. INSPECTED LANDING GEAR AND SENSORS, UNABLE TO DUPLICATE PROBLEM. REPLACED M986 AND M987 PER BOEING M/M, AS A PRECAUTION.

Part: SKIN — DENTED (BS 808)

DURING SCHEDULED 1/4 D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 808, BETWEEN STRINGERS 27R AND 27L. REPAIRED SKIN PER BOEING SRM.

Part: OIL PRESS IND — MALFUNCTIONED (NR 1 ENGINE)

DIVERTED TO PHX DUE TO NUMBER 1 ENGINE OIL PSI DROPPING TO YELLOW RANGE, APPROX 20 PSI. AIRCRAFT LANDED WITHOUT INCIDENT. PERFORMED ENGINE RUN PER BOEING M/M, OIL PRESSURE AND QUANTITY REMAINED IN NORMAL RANGE. CHECKED METAL CHIP DETECTORS AND FILTERS, PERFORMED ENGINE RUN A SECOND TIME, ALL NORMAL.

Part: EEL BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHT INOP. REPLACED AFT BATTERY PACK PER BOEING MM.