N525SW

Part: LENS — LOOSE (CABIN) · airframe 69,993 hrs · 66,167 cycles

RIGHT EMER EXIT LIGHT LENS COVER LOOSE. SECURED LENS IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,694 hrs · 65,808 cycles

SKIN CRACKED AT BS 520, STRINGER 8R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,694 hrs · 65,808 cycles

FUSELAGE SKIN CRACKED AT STATION 787+17 TO 787+19, STRINGER 23L. REPAIRED SKIN IAW SI.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,694 hrs · 65,808 cycles

FUSELAGE SKIN CRACKED, BETWEEN BS 482B+14 - 482B+17, STRINGER 8R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,694 hrs · 65,808 cycles

SKIN CRACKED AT BS 787+17.5, STRINGER 23L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,694 hrs · 65,808 cycles

SKIN CRACKED AT BS 943, STRINGER 4L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,694 hrs · 65,808 cycles

FUSELAGE SKIN CRACKED AT BS 415, STRINGER 1L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,694 hrs · 65,808 cycles

FUSELAGE SKIN CRACKED, BETWEEN BS 747+13 TO 747+13.5, BELOW STRINGER 19L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,694 hrs · 65,808 cycles

FUSELAGE SKIN CRACKED AT STATION 847+5, STRINGER 17L. REPAIRED SKIN IAW SI.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,694 hrs · 65,808 cycles

FUSELAGE SKIN CRACKED, BETWEEN BS 847+14.5 TO 847+16, ABOVE STRINGER 17L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,694 hrs · 65,808 cycles

FUSELAGE SKIN CRACKED AT STATION 767+13 TO 767+15, STRINGER 18L. REPAIRED SKIN IAW SI.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 69,485 hrs · 65,558 cycles

RIGHT OVERWING EMER EXIT SIGN LAMP INOPERATIVE. R & R LAMP ASSEMBLY IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,476 hrs · 65,549 cycles

SKIN CRACKED AT BS 747+17, STRINGER 19L. REPAIRED SKIN EA.

Part: LENS — LOOSE (CABIN) · airframe 69,168 hrs · 65,187 cycles

RIGHT OVERWING EXIT SIGN LENS LOOSE. R & R LENS IAW MM.

Part: SIGN — LOOSE (CABIN) · airframe 69,090 hrs · 65,097 cycles

RIGHT OVERWING EXIT SIGN LOOSE. SECURED SIGN ASSEMBLY IAW SIP.

Part: LIGHT — BROKEN (CABIN) · airframe 68,962 hrs · 64,949 cycles

AFT LAVATORY FWD WALL EMER EXIT LIGHT BROKEN. R & R LIGHT ASSEMBLY IAW AMM.

Part: STOP FITTING — CRACKED (FUSELAGE) · airframe 68,962 hrs · 64,949 cycles

L1 DOOR CUT OUT STOP FITTING CRACKED AT BS 348, STRINGER 14L. REPAIRED FITTING IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 68,962 hrs · 64,949 cycles

FLOORBEAM UPPER CHORD CRACKED AT BS 294, LBL 55. REPAIRED CHORD IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 68,962 hrs · 64,949 cycles

FRAME SHEAR TIE CORRODED AT BS 986, BETWEEN STR 20R - 21R. R & R SHEAR TIE IAW DWG & SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,962 hrs · 64,949 cycles

FRAME CRACKED AT BS 867, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,962 hrs · 64,949 cycles

FRAME CRACKED AT BS 867, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,962 hrs · 64,949 cycles

STRINGER CLIP CRACKED AT BS 907, STRINGER 4L. R & R CLIP IAW DWG & SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,962 hrs · 64,949 cycles

FUSELAGE SKIN CRACKED BETWEEN BS 787+10.5 - 787+12.4, STRINGER 27R. REPAIRED SKIN IAW EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,962 hrs · 64,949 cycles

STRINGER CLIP CRACKED AT BS 727B, STRINGER 8R. R & R CLIP IAW SI & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 68,962 hrs · 64,949 cycles

INTERCOSTAL CRACKED BETWEEN BS 277 TO 291, STRINGER 8R. R & R INTERCOSTAL IAW SRM & DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,962 hrs · 64,949 cycles

STRINGER CLIP CRACKED AT BS 616, STRINGER 5R. R & R CLIP IAW SRM & DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,962 hrs · 64,949 cycles

STRINGER CLIP CRACKED AT BS 927, STRINGER 24L. R & R CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,962 hrs · 64,949 cycles

STRINGER CLIP CRACKED AT BS 927, STRINGER 22L. R & R CLIP IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 68,962 hrs · 64,949 cycles

INTERCOSTAL CRACKED AT BS 360, STRINGER 4L. REPAIRED INTERCOSTAL IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,962 hrs · 64,949 cycles

AFT CARGO PIT FRAME CRACKED AT BS 986, STRINGER 20R. R & R FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,962 hrs · 64,949 cycles

FRAME CRACKED AT BS 947, STRINGER 19L. R & R FRAME IAW EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,962 hrs · 64,949 cycles

STRINGER CLIP CRACKED AT BS 440, STRINGER 8R. R & R CLIP IAW SI & DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 68,962 hrs · 64,949 cycles

AFT CARGO PIT FRAME AT BS 947, STRINGER 24L, AFT SIDE VERTICAL L CLIP CRACKED. R & R CLIP IAW SRM & DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,962 hrs · 64,949 cycles

STRINGER CLIP CRACKED AT BS 907, STRINGER 8R. R & R CLIP IAW SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,962 hrs · 64,949 cycles

STRINGER CLIP CRACKED AT BS 400, STRINGER 4R. R & R CLIP IAW SI & DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,962 hrs · 64,949 cycles

FUSELAGE STRINGER CLIP CRACKED AT BS 727B, STRINGER 8L. R & R CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,962 hrs · 64,949 cycles

FUSELAGE STRINGER CLIP CRACKED AT BS 727C, STRINGER 8L. R & R CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,962 hrs · 64,949 cycles

FUSELAGE STRINGER CLIP CRACKED AT BS 727C, STRINGER 10L. R & R CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,962 hrs · 64,949 cycles

STRINGER CLIP CRACKED AT BS 727A, STRINGER 9L. R & R CLIP IAW DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,962 hrs · 64,949 cycles

FUSELAGE STRINGER CLIP CRACKED AT BS 727C, STRINGER 6L. R & R CLIP IAW SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 68,962 hrs · 64,949 cycles

L1 DOOR SURROUND STRUCTURE STRINGER SPLICE CHANNEL, CRACKED AT BS 360, STRINGER 16L. R & R SPLICE IAW DWG & SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 68,962 hrs · 64,949 cycles

R1 DOOR SURROUND STRUCTURE UPPER FWD FRAME CRACKED AT BS 297, STRINGER 10R. R & R FRAME IAW SRM & DWG.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 68,962 hrs · 64,949 cycles

L1 DOOR CUT OUT FRAME CRACKED AT BS 348.2, STRINGER 15L. REPAIRED FRAME IAW EA.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 68,962 hrs · 64,949 cycles

L1 DOOR CUT OUT FRAME CRACKED AT BS 348.2, STRINGER 16L. REPAIRED FRAME IAW EA.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 68,962 hrs · 64,949 cycles

L1 DOOR FRAME INNER CHORD CRACKED AT BS 348.2. REPAIRED CHORD IAW EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,962 hrs · 64,949 cycles

STRINGER CLIP CRACKED AT BS 482A, STRINGER 5L. R & R CLIP IAW SI & DWG.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 68,962 hrs · 64,949 cycles

STRINGER SPLICE CRACKED AT BS 908, STRINGER 4R. R & R SPLICE IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,962 hrs · 64,949 cycles

STRINGER CLIP CRACKED AT BS 482A, STRINGER 8L. R & R CLIP IAW SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,962 hrs · 64,949 cycles

STRINGER CLIP CRACKED AT BS 482, STRINGER 16L. R & R CLIP IAW DWG & SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,962 hrs · 64,949 cycles

FUSELAGE STRINGER CLIP CRACKED AT BS 482A, STRINGER 9L. R & R CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,962 hrs · 64,949 cycles

STRINGER CLIP CRACKED AT BS 482B, STRINGER 5L. R & R CLIP IAW SI & DWG.

Part: HANDLE — CRACKED (EMERGENCY EXIT) · airframe 68,962 hrs · 64,949 cycles

RIGHT EMER EXIT HATCH UPPER HANDLE ASSEMBLY CRACKED. R & R HANDLE ASSEMBLY IAW AMM.

Part: HANDLE — CRACKED (EMERGENCY EXIT) · airframe 68,962 hrs · 64,949 cycles

LEFT EMER EXIT HATCH UPPER HANDLE ASSEMBLY CRACKED. R & R HANDLE ASSEMBLY IAW AMM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,962 hrs · 64,949 cycles

STRINGER CLIP CRACKED AT BS 440, STRINGER 8L. R & R CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,962 hrs · 64,949 cycles

FUSELAGE STRINGER CLIP CRACKED AT BS 440, STRINGER 4L. R & R CLIP IAW SRM.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 68,962 hrs · 64,949 cycles

AFT CARGO PIT CARGO DOORWAY UPPER SILL WEB CORRODED BETWEEN BS 847 - 867, STRINGER 18R. R & R WEB IAW SRM & DWG.

Part: BEAM — CRACKED (FUSELAGE) · airframe 68,962 hrs · 64,949 cycles

RIGHT STUB BEAM INNER CHORD CRACKED AT BS 616 LOWEST FASTENER HOLE. REPAIRED CHORD IAW EA.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 68,962 hrs · 64,949 cycles

SEAT TRACK CORRODED BETWEEN BS 344 - 354, LBL 45. REPAIRED SEAT TRACK IAW SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 68,962 hrs · 64,949 cycles

CREASE BEAM INNER CHORD CRACKED AT BS 616, RT SIDE FROM FASTENER HOLE. REPAIRED CHORD IAW EA.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 68,962 hrs · 64,949 cycles

CABIN SEAT TRACK CORRODED AT BS 887+11, RBL 45. R & R SEAT TRACK IAW SRM & DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 68,962 hrs · 64,949 cycles

SEAT TRACK CORRODED BETWEEN BS 344 - 420, LBL 45. REPAIRED SEAT TRACK IAW SRM.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 68,962 hrs · 64,949 cycles

SHEAR WEB ATTACH ANGLE CRACKED BETWEEN BS 428B - 520, BL 0. R & R ANGLE IAW SRM & DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,962 hrs · 64,949 cycles

STRINGER CLIP CRACKED AT BS 400, STRINGER 8L. R & R CLIP IAW SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,962 hrs · 64,949 cycles

STRINGER CLIP CRACKED AT BS 360, STRINGER 8L. R & R CLIP IAW SRM & DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,962 hrs · 64,949 cycles

STRINGER CLIP CRACKED AT BS 360, STRINGER 10L. R & R CLIP IAW SI & DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 68,962 hrs · 64,949 cycles

R2 DOOR WAY, CREASE BEAM VERTICAL FLANGE CORRODED BETWEEN BS 991 - 994. R & R BEAM IAW DWG & SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,962 hrs · 64,949 cycles

FUSELAGE STRINGER CLIP CRACKED AT BS 482, STRINGER 8L. R & R CLIP IAW SRM & DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 68,962 hrs · 64,949 cycles

FRAME CORRODED AT BS 992, STRINGER 17R. R & R FRAME IAW DWG & SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 68,962 hrs · 64,949 cycles

R2 DOOR WAY, CREASE BEAM UPPER SURFACE, OTBD FLANGE CORRODED BETWEEN BS 966 - 984. R & R BEAM IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,962 hrs · 64,949 cycles

FUSELAGE STRINGER CLIP CRACKED AT BS 616, STRINGER 5R. R & R CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,962 hrs · 64,949 cycles

STRINGER CLIP CRACKED AT BS 440, STRINGER 4L. R & R CLIP IAW SRM & DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,962 hrs · 64,949 cycles

STRINGER CLIP CRACKED AT BS 420, STRINGER 16R. R & R CLIP IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 68,962 hrs · 64,949 cycles

STRINGER TIE CLIP CRACKED AT BS 787, STRINGER 16L. R & R TIE CLIP IAW SRM & DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,962 hrs · 64,949 cycles

STRINGER CLIP CRACKED AT BS 847, STRINGER 9L. R & R CLIP IAW SRM & DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,962 hrs · 64,949 cycles

STRINGER CLIP CRACKED AT BS 380, STRINGER 16R. R & R CLIP IAW SRM & DWG.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 68,962 hrs · 64,949 cycles

STRINGER CRACKED AT BS 360+14, STRINGER 15R. R & R STRINGER SECTION IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,962 hrs · 64,949 cycles

STRINGER CLIP CRACKED AT BS 380, STRINGER 15R. R & R CLIP IAW SRM & DWG.

Part: SKIN — CORRODED (FUSELAGE) · airframe 68,962 hrs · 64,949 cycles

FORWARD CARGO PIT SKIN CORRODED AT BS 468, BETWEEN STRINGER 28R - 28L. REPAIRED SKIN IAW EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,962 hrs · 64,949 cycles

STRINGER CLIP CRACKED AT BS 747, STRINGER 16R. R & R CLIP IAW SRM & DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,962 hrs · 64,949 cycles

STRINGER CLIP CRACKED AT BS 827, STRINGER 16R. R & R CLIP IAW SRM & DWG.

Part: FLAP TRACK — CORRODED (LT WING) · airframe 68,962 hrs · 64,949 cycles

LEFT WING NR 4 FLAP TRACK FWD ATTACHMENT INBD LUG CORRODED ON OTBD & INBD INTERFACE. R & R NR 4 FLAP TRACK IAW SRM & AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,962 hrs · 64,949 cycles

UPPER CROWN SKIN CRACKED BETWEEN BS 414 TO 454, BETWEEN STRINGER 2L TO 4.5L. REPAIRED SKIN IAW MM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 68,962 hrs · 64,949 cycles

STRINGER SPLICE CORRODED AT BS 907, STRINGER 18L. R & R SPLICE IAW DWG & SRM.

Part: WEB — CRACKED (NLG WW) · airframe 68,962 hrs · 64,949 cycles

LEFT NOSE WW SIDE SKIN WEB CRACKED ALONG DOUBLER FWD EDGE. REPAIRED WEB IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,962 hrs · 64,949 cycles

FUSELAGE SKIN CRACKED AT BS 827-6, STRINGER 18L. REPAIRED SKIN IAW SRM & EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 68,962 hrs · 64,949 cycles

FRAME SHEAR TIE CORRODED AT BS 847, RBL 19. R & R SHEAR TIE IAW ACO.

Part: SKIN — CRACKED (LE SLAT) · airframe 68,962 hrs · 64,949 cycles

LEFT WING NR 1 SLAT SKIN 19'' FROM INBD ACTUATOR FASTENER HOLES CRACKED. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 68,962 hrs · 64,949 cycles

LEFT WING NR 1 SLAT SKIN 49'' FROM OTBD EDGE FASTENER HOLES CRACKED. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,962 hrs · 64,949 cycles

SKIN CRACKED AT BS 360+2, BETWEEN STRINGER 5R - 6R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,962 hrs · 64,949 cycles

SKIN CRACKED AT BS 360+2, BETWEEN STRINGER 2L - 3L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 68,962 hrs · 64,949 cycles

LEFT WING NR 1 SLAT LOWER TE SKIN, OTBD EDGE FASTENER HOLES CRACKED. R & R SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,962 hrs · 64,949 cycles

FUSELAGE SKIN CRACKED AT BS 907, STRINGER 4L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,962 hrs · 64,949 cycles

SKIN CRACKED AT BS 360+2, BETWEEN STRINGER 5R - 6R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,962 hrs · 64,949 cycles

FUSELAGE SKIN CRACKED AT BS 360+14, STRINGER 26L. REPAIRED SKIN IAW EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 68,962 hrs · 64,949 cycles

FLOORBEAM T CAP CORRODED AT BS 986.5. REPAIRED T CAP IAW EA.

Part: WEDGE — DELAMINATED (TE FLAP) · airframe 68,867 hrs · 64,840 cycles

RIGHT WING INBD TE MID FLAP WEDGE DELAMINATED. R & R WEDGE IAW SRM.

Part: SIGN — BROKEN (CABIN) · airframe 67,809 hrs · 63,661 cycles

AFT EXIT SIGN BROKEN. R & R SIGN IAW SIP.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,791 hrs · 63,642 cycles

SKIN CRACKED AT BS 767+7 STRINGER 19L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,791 hrs · 63,642 cycles

SKIN CRACKED AT BS 420+10 BETWEEN STRINGER 17R TO 18R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,791 hrs · 63,642 cycles

SKIN CRACKED AT BS 380+5 STRINGER 26L. REPAIRED SKIN IAW EA.

Part: SLAT — CRACKED (RT WING) · airframe 67,257 hrs · 63,066 cycles

RIGHT WING LE NR 5 SLAT OTBD CUT OUT CRACKED. REPAIRED NR 5 SLAT IAW EA.

Part: LIGHT — DIRTY (CABIN) · airframe 67,257 hrs · 63,066 cycles

RIGHT EEPLS DIRTY BETWEEN ROW 18 TO ROW 20. CLEANED EEPLS IAW MM.

Part: SKIN — CRACKED (RT WING) · airframe 67,179 hrs · 62,978 cycles

RIGHT WING LE CRACKED AT NR 5 SLAT OTBD AUXILIARY TRACK CUT OUT CRACKED. REPAIRED CUT OUT IAW SRM.

Part: HOUSING — BROKEN (CABIN) · airframe 66,654 hrs · 62,440 cycles

LT EMERGENCY EXIT LIGHTS BATTERY SUPPLY PACK HOUSING BROKEN. R & R HOUSING IAW AMM.

Part: LENS — LOOSE (EXIT SIGN) · airframe 66,402 hrs · 62,179 cycles

R2 DOOR EMERGENCY EXIT SIGN LENS ASSEMBLY LOOSE. R & R LENS ASSEMBLY IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,068 hrs · 61,844 cycles

FUSELAGE SKIN CRACKED AT STATION 920 TO STATION 923.2, STRINGER 25R. REPAIRED SKIN IAW SRM & SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,068 hrs · 61,844 cycles

FUSELAGE SKIN CRACKED AT STATION 784, STRINGER 22L. REPAIRED SKIN IAW SRM & SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,068 hrs · 61,844 cycles

FUSELAGE SKIN CRACKED AT STATION 946 TO STATION 948.3, STRINGER 24R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,068 hrs · 61,844 cycles

CHEM MILL SKIN CRACKED AT BS 764, STRINGER 23L. REPAIRED SKIN IAW SRM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 65,491 hrs · 61,232 cycles

LT OVERWING EMERGENCY EXIT SIGN BULBS INOPERATIVE. R & R BULBS IAW AMM.

Part: FLAP TRACK — CORRODED (TE FLAP) · airframe 65,331 hrs · 61,044 cycles

RT WING NR 8 FLAP TRACK CORRODED. R&R NR 8 FLAP TRACK IAW AMM.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 64,906 hrs · 60,541 cycles

SUPPORT BRACKET CRACKED AT BS 380, BETWEEN STR 20L TO STR 21L. R & R BRACKET IAW SRM AND DWG.

Part: FLAP — DELAMINATED (RT WING) · airframe 64,906 hrs · 60,541 cycles

RIGHT WING INBD FORE FLAP DELAMINATED. REPAIRED FORE FLAP IAW SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 64,906 hrs · 60,541 cycles

STRAP CRACKED BETWEEN BS 312 TO BS 344, STR 17. R & R STRAP IAW SRM AND DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 64,906 hrs · 60,541 cycles

WEB CRACKED BETWEEN BS 312 TO BS 303.9, STR 28L. REPAIRED WEB IAW SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 64,906 hrs · 60,541 cycles

AFT BULKHEAD DOME WEB CRACKED AT BS 1016, STR 21R. REPAIRED WEB IAW EO AND EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 64,906 hrs · 60,541 cycles

BULKHEAD WEB CRACKED BS 1016, STR 15R. REPAIRED WEB IAW EO AND EA.

Part: STIFFENER — CRACKED (TE FLAP) · airframe 64,906 hrs · 60,541 cycles

RT WING NR 6 FLAP TRACK FAIRING STIFFENER CRACKED AT WBL 183.4. R & R STIFFENER IAW SRM AND DWG.

Part: STIFFENER — CRACKED (TE FLAP) · airframe 64,906 hrs · 60,541 cycles

LEFT WING NR 3 FLAP TRACK FAIRING STIFFENER CRACKED AT WBL 183.4. R & R STIFFENER IAW SRM AND DWG.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 64,906 hrs · 60,541 cycles

BULKHEAD CHORD CORRODED AT BS 227.8, BETWEEN LBL 5 TO RBL 5. R & R CHORD IAW SRM AND DWG.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 64,906 hrs · 60,541 cycles

STIFFENER CORRODED AT BS 227.8, BL 0. R & R STIFFENER IAW SRM AND DWG.

Part: LIGHT — DELAMINATED (CABIN) · airframe 64,906 hrs · 60,541 cycles

EEPLS DELAMINATED ALONG PAX CABIN. R & R EEPLS IAW AMM AND DWG.

Part: STRINGER SPLICE — CRACKED (BS 360) · airframe 64,906 hrs · 60,541 cycles

STRINGER SPLICE CRACKED AT BS 360, STR 15R. R & R SPLICE IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 64,906 hrs · 60,541 cycles

TIE CLIP CRACKED AT BS 787, STR 20R. R & R TIE CLIP IAW SRM AND DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 64,906 hrs · 60,541 cycles

STRINGER CORRODED AT BS 863, STR 26R. REPAIRED STRINGER IAW SRM.

Part: RETAINER — CORRODED (TE FLAP) · airframe 64,906 hrs · 60,541 cycles

LEFT WING INBD FLAP, INBD CARRAIGE FWD ROLLER ASSY CORRODED. R & R RETAINER IAW CMM.

Part: WEB — CRACKED (FUSELAGE) · airframe 64,906 hrs · 60,541 cycles

WEB CRACKED BETWEEN BS 312 TO BS 312+11, BETWEEN AND STR 28L TO STR 28R. REMOVED AND REPLACED WEB IAW SRM AND DRAWING.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 64,906 hrs · 60,541 cycles

BULKHEAD WEB CRACKED AT BS 1016, STR 6R. REPAIRED WEB IAW EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 64,906 hrs · 60,541 cycles

BULKHEAD WEB CRACKED AT BS 1016, STR 6R. REPAIRED WEB IAW EO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 64,906 hrs · 60,541 cycles

BULKHEAD WEB CRACKED AT BS 1016, STR 6L. REPAIRED WEB IAW SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 64,906 hrs · 60,541 cycles

BULKHEAD WEB CRACKED BS 1016, STR 6R. REPAIRED WEB IAW EO AND EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 64,906 hrs · 60,541 cycles

BULKHEAD WEB CRACKED AT BS 1016, STR 6L+ 2. REPAIRED WEB IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 64,906 hrs · 60,541 cycles

FLOORBEAM WEB CRACKED AT BS 713, RBL 24.8. REPAIRED WEB IAW EA.

Part: RIB — CRACKED (RT WING) · airframe 64,906 hrs · 60,541 cycles

RT WING LOWER CHORD RIB CRACKED AT WBL 135.5 BETWEEN S-2 AND S-3. REPAIRED RIB IAW EA.

Part: RIB — CRACKED (LT WING) · airframe 64,906 hrs · 60,541 cycles

LT WING LOWER CHORD RIB CRACKED AT WBL 135.5 BETWEEN S-2 AND S-3. REPAIRED RIB IAW SWA EA.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 64,906 hrs · 60,541 cycles

ATTACH CLIP CRACKED AT BS 348.2, STR 15L. R & R ANGLE IAW SRM AND DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 64,906 hrs · 60,541 cycles

FLOORBEAM CORRODED AT BS 967, LBL 27.5. REPAIRED BEAM IAW EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 64,906 hrs · 60,541 cycles

ANGLE CRACKED AT BS 294.5, STR 13L. REMOVED AND REPLACED ANGLE PER SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,906 hrs · 60,541 cycles

FRAME CRACKED AT BS 294.5, STR 4L. REPAIRED FRAME IAW AND EA.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 64,906 hrs · 60,541 cycles

DOOR Z ANGLE CORRODED BETWEEN BS 294.5 AND BS 344, RBL 61. R & R Z ANGLE IAW SRM AND DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 64,906 hrs · 60,541 cycles

WEB CRACKED AT BS. 294.5+2, RBL 55. R & R WEB IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 64,906 hrs · 60,541 cycles

TIE CLIP CRACKED AT BS 360, STR 5L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 64,906 hrs · 60,541 cycles

FLOORBEAM CORRODED AT BS 344, BL 0. REPAIRED BEAM IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,906 hrs · 60,541 cycles

FRAME WEB CRACKED AT BS 277, STR 16L. REPAIRED WEB IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,906 hrs · 60,541 cycles

SKIN CRACKED AT BS 827+15, STR 17L. REPAIRED SKIN IAW SRM.

Part: BULKHEAD — CRACKED (NLG WW) · airframe 64,906 hrs · 60,541 cycles

NLG WHEEL WELL SIDE PANEL CRACKED AT BS 243.7 + 3.5, LBL 16. REPAIRED PANEL IAW SRM.

Part: PANEL — CRACKED (NLG WW) · airframe 64,906 hrs · 60,541 cycles

NLG WHEEL WELL SIDE PANEL CRACKED AT BS 243.7, RBL 16. REPAIRED PANEL IAW SRM.

Part: REVEAL — CRACKED (FUSELAGE) · airframe 64,906 hrs · 60,541 cycles

R1 DOOR CUTOUT AFT UPPER REVEAL CRACKED AT BS 312+13, BETWEEN STR 7R TO STR 8R. R & R REVEAL IAW SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,906 hrs · 60,541 cycles

L1 DOOR UPPER HINGE CUTOUT CRACKED. REMOVED AND REPLACED CUTOUT IAW SRM.

Part: ANGLE — CRACKED (RT WING) · airframe 64,906 hrs · 60,541 cycles

RIGHT WING T/E ANGLE CRACKED AT RSS 533 T/E AREA. R & R ANGLE IAW SRM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 64,906 hrs · 60,541 cycles

FWD ENTRY DOOR CUTOUT ANGLE CRACKED AT BS 348.2, BETWEEN STR 11L TO STR 12L. R & R ANGLE IAW SRM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 64,906 hrs · 60,541 cycles

ANGLE CRACKED AT BS 291, BETWEEN STR 10R TO STR 11R. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: REVEAL — CRACKED (FUSELAGE) · airframe 64,906 hrs · 60,541 cycles

L1 DOOR CUTOUT FWD UPPER REVEAL CRACKED AT BS 312, BETWEEN STR 6L TO STR 7L. R & R REVEAL IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 64,906 hrs · 60,541 cycles

RIGHT WING NR 8 T/E SUPPORT ANGLE CRACKED LOCATED UNDER SURFACE. R & R FASTENERS IAW SRM AND DWG.

Part: PANEL — CRACKED (NLG WW) · airframe 64,906 hrs · 60,541 cycles

NLG WHEEL WELL SIDE PANEL CRACKED AT BS 243.7, LBL 16. REPAIRED PANEL IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 64,906 hrs · 60,541 cycles

FWD GALLEY DOOR CUTOUT FITTING CRACKED AT BS 332.1, STR 8R. REPAIRED FITTING IAW EA.

Part: FITTING — CRACKED (FUSELAGE) · airframe 64,906 hrs · 60,541 cycles

FWD GALLEY DOOR CUTOUT CRACKED BETWEEN BS 291.5 TO BS 297, STR 8R. REPAIRED FITTING IAW EO AND EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 64,906 hrs · 60,541 cycles

FWD ENTRY DOOR CUTOUT CRACKED ON AFT LOWER REVEAL AT BS 344, STR 17L. R & R ANGLE IAW SRM AND DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 64,906 hrs · 60,541 cycles

DOOR Z ANGLE CORRODED BETWEEN BS 312 AND BS 344, LBL 59. R & R Z ANGLE IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,906 hrs · 60,541 cycles

FRAME CRACKED AT BS 277, STR 16L. REPAIRED WEB IAW EA.

Part: PANEL — CRACKED (NLG WW) · airframe 64,906 hrs · 60,541 cycles

NLG WHEEL WELL SIDE PANEL CRACKED AT BS 251.6, RBL 16. REPAIRED PANEL IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,906 hrs · 60,541 cycles

FRAME OTBD CHORD CRACKED AT BS 727, STR 18A RT SIDE. REPAIRED FRAME IAW EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 64,906 hrs · 60,541 cycles

AFT BULKHEAD, AFT SIDE DOME WEB CRACKED AT BS 1016, STR 15R. REPAIRED WEB IAW EO AND EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 64,906 hrs · 60,541 cycles

FRAME CORRODED AT BS 482A, BETWEEN STR 28R AND STR 28L. REPAIRED FRAME IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 64,906 hrs · 60,541 cycles

SUPPORT ANGLE CRACKED BETWEEN BS 927 TO BS 947.5, BL0. R & R ANGLE IAW SRM AND DWG.

Part: ANGLE — CRACKED (TE FLAP) · airframe 64,906 hrs · 60,541 cycles

RIGHT WING FLAP TRACK T/E INTERNAL ANGLE CRACKED AT WBL 183.40. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: RETAINER — CRACKED (TE FLAP) · airframe 64,906 hrs · 60,541 cycles

LEFT WING FLAP TRACK FAIRING SEAL RETAINER CRACKED ON ACCESS PANEL 3501L. REMOVED AND REPLACED RETAINER IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 64,906 hrs · 60,541 cycles

FRAME CORRODED AT BS 482B, STR 28L FWD CARGO COMPARTMENT. REMOVED AND REPLACED SHEAR TIE IAW SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,906 hrs · 60,541 cycles

SKIN CRACKED AT BS 440+5, STR 26L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,906 hrs · 60,541 cycles

SKIN CRACKED AT BS 420+5.5, STR 26L. REPAIRED SKIN IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,906 hrs · 60,541 cycles

FRAME OUTBOARD CHORD CRACKED AT BS 727, STR 18A LT SIDE. REPAIRED FRAME IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 64,906 hrs · 60,541 cycles

LONGITUDINAL FLOORBEAM WEB CRACKED BETWEEN BS 707 AND BS 709, RBL 24.8. REPAIRED WEB IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 64,906 hrs · 60,541 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 667.5, LBL 24.8. REPAIRED CHORD IAW EA.

Part: SKIN PANEL — CORRODED (FUSELAGE) · airframe 64,906 hrs · 60,541 cycles

KEEL BEAM SKIN PANEL CORRODED BETWEEN BS 616 AND BS 639, BL 0. R & R PANEL IAW EA.

Part: RETAINER — CRACKED (TE FLAP) · airframe 64,906 hrs · 60,541 cycles

RIGHT NR 5 FLAP TRACK FAIRING PLATE RETAINER CRACKED. REMOVED AND REPLACED RETAINER IAW SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,906 hrs · 60,541 cycles

EXTERNAL CROWN SKIN CRACKED AT BS 380 + 13, STR 1. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,906 hrs · 60,541 cycles

SKIN CRACKED AT BS 482B + 12, STR 16L. REPAIRED SKIN IAW EA.

Part: RETAINER — CRACKED (TE FLAP) · airframe 64,906 hrs · 60,541 cycles

LEFT NR 4 FLAP TRACK FAIRING PLATE RETAINER CRACKED. REMOVED AND REPLACED RETAINER IAW SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,906 hrs · 60,541 cycles

SKIN CRACKED AT BS 291.5, STR 4R. REPAIRED SKIN IAW SRM.

Part: FITTING — CORRODED (R2 DOOR) · airframe 64,906 hrs · 60,541 cycles

R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR FITTINGS CORRODED. R & R FITTING IAW SRM.

Part: RUB STRIP — CRACKED (VERTICAL STAB) · airframe 64,906 hrs · 60,541 cycles

RUB STRIP CRACKED AT ON ACCESS PANEL 9501 VERTICAL STABILIZER DOOR LEFT SIDE. REMOVED AND REPLACED RUB STRIP IAW SRM AND DWG.

Part: FITTING — CORRODED (R1 DOOR) · airframe 64,906 hrs · 60,541 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FITTINGS CORRODED. R & R FITTING IAW SRM.

Part: HOOK — LOOSE (R1 DOOR) · airframe 64,702 hrs · 60,337 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR HOOKS LOOSE. SECURED HOOKS PER M/M.

Part: SKIN — CRACKED (FUSELAGE)

FUSELAGE SKIN CRACKED AT BS 384, STR 15R. REPAIRED SKIN PER EA.

Part: COFFEEMAKER — FAULTY (GALLEY) · airframe 63,782 hrs · 59,388 cycles

PRIOR TO 10,000FT, F/A CALLED & SAID SMELLED STRONG ODOR WHICH SEEMED TO BE SOMETHING BURNING. AFTERWARD, WE BOTH SMELLED A STRONG ODOR IN THE COCKPIT. TURNED GALLEY POWER OFF AND SMELL DISSIPATED. NO SMOKE NOTED AND SMELL SEEMED TO BE ELECTRICAL. REMOVED AND REPLACED FWD GALLEY COFFEEMAKER IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,694 hrs · 59,291 cycles

FUSELAGE SKIN CRACKED AT BS 400, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,694 hrs · 59,291 cycles

FUSELAGE SKIN CRACKED AT BS 767, STR 24L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,694 hrs · 59,291 cycles

FUSELAGE SKIN CRACKED BS 400, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,462 hrs · 59,087 cycles

FUSELAGE SKIN CRACKED AT BS 887 +14, STR 25R. REPAIRED SKIN PER SRM.

Part: LATCH — INOPERATIVE (L1 DOOR) · airframe 62,618 hrs · 58,543 cycles

L1 DOOR EMERGENCY EVAC SLIDE LATCH INOP. REMOVED AND REPLACED LATCH IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,619 hrs · 58,543 cycles

SKIN CRACKED AT BS 767+ 17, STR 24L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,619 hrs · 58,543 cycles

FUSELAGE SKIN CRACKED AT BS 787+13, STR 22L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,519 hrs · 58,467 cycles

SKIN CRACKED AT BS 947, 3 FEET FOWARD OF OUTFLOW VALVE. REPAIRED SKIN PER SRM.

Part: GASPER FAN — FAULTY (AC BAY) · airframe 62,408 hrs · 58,387 cycles

DURING CRUISE FLT ATTENDANT CALLED AND REPORTED A STRONG ACRID SMELL STRONGEST NEAR ROW 3. NO ABNORMAL INDICATIONS NOTED. TURNED OFF GASPER FAN SMELL DISSIPATED (DISAPPEAR) ON APPROACH SMELL CAME BACK. NO VISABLE SMOKE. REMOVED AND REPLACED GASPER FAN PER M/M.

Part: LIGHT — DIRTY (CABIN) · airframe 61,655 hrs · 57,913 cycles

FWD CABIN EMERGENCY FLOOR FLUORESCENT TRACK DIRTY. CLEANED EMERGENCY LIGHT PER MM.

Part: LIGHT — DIRTY (CABIN) · airframe 61,655 hrs · 57,913 cycles

LEFT FWD CABIN EMERGENCY FLOOR FLUORESCENT TRACK BETWEEN ROW 3 TO 5 DIRTY. CLEANED EMERGENCY LIGHT PER MM.

Part: LENS — BROKEN (CABIN) · airframe 61,583 hrs · 57,872 cycles

R2 DOOR EMERGENCY LIGHT LENS BROKEN. REMOVED AND REPLACED LENS IAW MM.

Part: WIRE HARNESS — BROKEN (NR 1 ENGINE) · airframe 60,603 hrs · 57,224 cycles

INFLIGHT SHUTDOWN/DECLARED EMERGENCY. NR 1 EGT STARTED FLUCTUATING AT CRUISE ALT WITH AN OCCASIONAL EGT LIGHT ILLUMINATING. REDUCED THRUST LEVER TO KEEP WITHIN LIMITS WHEN EGT PEGGED TO HIGH SIDE AND EGT LIGHT ON. REMOVED AND REPLACED EGT PROBE HARNESS ASSY IAW MM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 60,354 hrs · 57,063 cycles

DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM WEB CRACKED BETWEEN BS 707 TO BS 713, BL 0. REPAIRED WEB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,354 hrs · 57,063 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR LOWER CORNER CUTOUT. REPAIRED SKIN IAW SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 60,354 hrs · 57,063 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CORRODED AT BS 794, STR 26R. REPAIRED STRINGER PER ER.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 60,354 hrs · 57,063 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO FLOOR SUPPORT CORRODED AT BS 772, LBL 12. REPAIRED SUPPORT IAW EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 60,354 hrs · 57,063 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CORRODED AT BS 787, BETWEEN STR 26L TO STR 27L. REPAIRED FRAME IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 60,354 hrs · 57,063 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO FRAME CORRODED AT BS 794, BETWEEN STR 27R TO STR 25R. REMOVED AND REPLACED FRAME IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 60,354 hrs · 57,063 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO FLOOR SUPPORT CORRODED AT BS 772, LBL 8. REPAIRED SUPPORT IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 60,354 hrs · 57,063 cycles

DURING SCHEDULED 20Y CHECK, FOUND LONGITUINDAL FLOORBEAM UPPER O/B CHORD CRACKED AT BS 727B, RBL 24. REPAIRED CHORD PER ER AND EA.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 60,354 hrs · 57,063 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,354 hrs · 57,063 cycles

DURING SCHEDULED 20Y CHECK, FOUND SKIN CRACKED AT BS 727C+8, STR 23L. REPAIRED SKIN IAW SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 60,354 hrs · 57,063 cycles

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

Part: ACTUATOR — FAULTY (KRUEGER FLAP) · airframe 60,175 hrs · 56,933 cycles

AIR TURNBACK - NR 2 KRUEGER FLAP SHOWS FULLY EXTENDED WITH FLAP HANDLE FULL UP. REMOVED AND REPLACED NR 2 L/E FLAP ACTUATOR PER MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 60,107 hrs · 56,883 cycles

DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 59,881 hrs · 56,729 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT WING AFT I/B FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,885 hrs · 56,730 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 967 STR 24L. REPAIRED SKIN PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 59,556 hrs · 56,489 cycles

DURING SCHEDULED OTS CHECK FOUND, AFT PRESSURE BULKHEAD WEB CRACKED AT LOWER EDGE OF PIE PANEL AT 12 O'CLOCK IN AND OUT OF FASTENER RIGHT ABOVE DOME PLUG BS 1016. REPAIRED WEB IAW SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 59,556 hrs · 56,489 cycles

DURING SCHEDULED MV2 CHECK FOUND, AFT PRESSURE BULKHEAD WEB CRACKED AT LOWER EDGE OF SIDE PANEL. REMOVED AND REPLACED WEB PER SRM.

Part: COOLING FAN — FAULTY (E&E BAY) · airframe 59,533 hrs · 56,475 cycles

DIVERSION / DECLARED EMERGENCY, WITH EQUIP COOLING FAN IN NORM POSITION, HEARD NOISE AND ELECTRICAL ODOR IN COCKPIT. REMOVED AND REPLACED EQUIP COOLING FAN VALVE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,115 hrs · 56,197 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND SKIN CRACKED AT BS 767, STR 22L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,115 hrs · 56,197 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND SKIN CRACKED AT BS 442.5, STR 1. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,115 hrs · 56,197 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND SKIN CRACKED AT BS 807, STR 24L. REPAIRED SKIN PER EA.

Part: SKIN — PUNCTURED (ELEVATOR) · airframe 56,576 hrs · 54,374 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT ELEVATOR UPPER SURFACE PUNCTURED. REMOVED AND REPLACED ELEVATOR PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,435 hrs · 54,271 cycles

DURING SCHEDULED CV CHECK, FOUND SKIN CRACKED AT BS 884, STR 24R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,628 hrs · 53,727 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CUTOUT CRACKED AT R1 DOOR LOWER AFT CORNER. REPAIRED SKIN PER SRM.

Part: BRACKET — BROKEN (GIRT BAR) · airframe 55,453 hrs · 53,613 cycles

L2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR BRACKET SPRING BROKEN. REMOVED AND REPLACED BRACKET PER MM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 54,795 hrs · 53,220 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 947 TO BS 952, STR 24L. REPAIRED SKIN PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 54,795 hrs · 53,220 cycles

DURING SCHEDULED 18Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 666.5, LBL 24.8. REPAIRED BEAM PER AAR EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 54,795 hrs · 53,220 cycles

DURING SCHEDULED 18Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 660, BBL .07. REPAIRED BEAM PER SI.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,795 hrs · 53,220 cycles

DURING SCHEDULED 18Y CHECK, FOUND SKIN CRACKED AT BS 947.5, STR 23L. REPAIRED SKIN PER AAR EA.

Part: SKIN — CORRODED (FUSELAGE) · airframe 54,795 hrs · 53,220 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE SKIN CORRODED BETWEEN BS 948 TO BS 950, BETWEEN STR 25L TO STR 26L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,795 hrs · 53,220 cycles

DURING SCHEDULED 18Y CHECK, FOUND LT AFT FUSELAGE SKIN CRACKED AT BS 753, STR 24L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,795 hrs · 53,220 cycles

DURING SCHEDULED 18Y CHECK, FOUND SKIN CRACKED AT BS 927, STR 23L. REPAIRED SKIN PER AAR EA.

Part: SKIN — CORRODED (FUSELAGE) · airframe 54,795 hrs · 53,220 cycles

DURING SCHEDULED 18Y CHECK, FOUND FWD CARGO COMPARTMENT SKIN CORRODED AT BS 498B, LBL 11. REPAIRED SKIN PER AAR EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,795 hrs · 53,220 cycles

DURING SCHEDULED 18Y CHECK, FOUND FRAME CRACKED AT BS 482A, BETWEEN STR 20L TO STR 21L. REPAIRED FRAME PER SI.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,795 hrs · 53,220 cycles

DURING SCHEDULED 18Y CHECK, FOUND SKIN CRACKED AT BS 527, RBL 5. REPAIRED SKIN PER AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,795 hrs · 53,220 cycles

DURING SCHEDULED 18Y CHECK, FOUND SKIN CRACKED AT BS 527, LBL 5. REPAIRED SKIN PER AAR EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 54,795 hrs · 53,220 cycles

DURING SCHEDULED 18Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 727B, LBL 43. REPAIRED BEAM PER AAR EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,795 hrs · 53,220 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 947, STR 27R. REMOVED AND REPLACED CLIP PER SRM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 54,795 hrs · 53,220 cycles

DURING SCHEDULED 18Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 54,795 hrs · 53,220 cycles

DURING SCHEDULED 18Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITION SLIDE PER MT.

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 54,795 hrs · 53,220 cycles

DURING SCHEDULED 18Y CHECK, FOUND AFT CARGO COMPARTMENT DOOR FRAME CRACKED AT LOWER I/B FASTENER HOLE ON AFT SIDE FRAME, LOWER STOP FITTING. REMOVED AND REPLACED FRAME PER SRM.

Part: COVER — BROKEN (R1 DOOR) · airframe 54,795 hrs · 53,220 cycles

DURING SCHEDULED 18Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE COVER BROKEN. REMOVED AND REPLACED COVER PER EA.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 54,795 hrs · 53,220 cycles

DURING SCHEDULED 18Y CHECK, FOUND LT WING NR 2 SLAT, I/B TRAILING EDGE WEDGE UPPER SURFACE DELAMINATED. REPAIRED WEDGE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 54,795 hrs · 53,220 cycles

DURING SCHEDULED 18Y CHECK, FOUND SHEAR TIE CORRODED AT BS 520, LBL 11. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: LENS — LOOSE (CABIN) · airframe 54,697 hrs · 53,160 cycles

RIGHT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LENS PER MM.

Part: SLIDE — UNSERVICEABLE (L1 DOOR) · airframe 54,240 hrs · 52,872 cycles

DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATOR OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,927 hrs · 52,673 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 979, STR 23L. REPAIRED SKIN PER SRM.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 53,887 hrs · 52,645 cycles

FWD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 53,886 hrs · 52,645 cycles

FWD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM.

Part: SIGN — LOOSE (CABIN) · airframe 53,425 hrs · 52,341 cycles

RT OVERWING EMERGENCY EXIT SIGN LOOSE. REMOVED AND REPLACED SIGN PER MM.

Part: LIGHT — MISSING (CABIN) · airframe 52,967 hrs · 52,026 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,557 hrs · 51,692 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 892, STR 25L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,557 hrs · 51,692 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,557 hrs · 51,692 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,557 hrs · 51,692 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 931, STR 24L. REPAIRED SKIN PER SRM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 52,352 hrs · 51,507 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING NR 2 SLAT UPPER T/E WEDGE DELAMINATED. REPAIRED WEDGE PER MM.

Part: TAB — DELAMINATED (LT AILERON) · airframe 52,352 hrs · 51,507 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING AILERON TAB DELAMINATED AT I/B AND O/B TRAILING EDGE. REMOVED AND REPLACED TAB PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,352 hrs · 51,507 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 52,234 hrs · 51,403 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT WING I/B AFT FLAP DELAMINATED. REPLACED FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,814 hrs · 51,033 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BETWEEN BS 967 TO BS 986, STR 20L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,808 hrs · 51,025 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 425, STR 1R. REPAIRED SKIN PER SWA EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 51,669 hrs · 50,927 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 440, STR 14R TO STR 15R. REPAIRED PER AAR EA.

Part: SLIDE — LOW PRESSURE (L2 DOOR) · airframe 51,393 hrs · 50,728 cycles

DURING SCHEDULED MV2 CHECK, L2 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 50,861 hrs · 50,327 cycles

L2 DOOR EVAC SLIDE FELL OUT OF CONTAINER. DID NOT DEPLOY. INSTALLED SLIDE ASSY PER MM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 49,641 hrs · 49,399 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 440, STR 14R. REPAIRED SHEAR TIE PER EA.

Part: BUSHING — WORN (LT ELEVATOR) · airframe 49,641 hrs · 49,399 cycles

DURING SCHEDULED SPV CHECK, LT ELEVATOR TAB NR 2 HINGE FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 2 HINGE BUSHING PER MM.

Part: BEARING — WORN (RT ELEVATOR) · airframe 49,637 hrs · 49,397 cycles

DURING SCHEDULED SPV CHECK, RIGHT ELEVATOR TAB NR 1 HINGE FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 HINGE BEARING AND BOLT PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,637 hrs · 49,397 cycles

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

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 49,637 hrs · 49,397 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 14R. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 49,637 hrs · 49,397 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CREASED AT BS 370, STR 4L. REPAIRED SKIN PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,551 hrs · 49,107 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 277, STR 16L. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,637 hrs · 49,397 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 49,551 hrs · 49,107 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500, STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,637 hrs · 49,397 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 460, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,637 hrs · 49,397 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 460, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,637 hrs · 49,397 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,637 hrs · 49,397 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,637 hrs · 49,397 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 49,637 hrs · 49,397 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 908, STR 4L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: STRINGER CLIP — CRACKED (BS 360 S11L) · airframe 49,637 hrs · 49,397 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,637 hrs · 49,397 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 482B, STR 6L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,637 hrs · 49,397 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,637 hrs · 49,397 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,637 hrs · 49,397 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 482B, STR 6L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,637 hrs · 49,397 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 2R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,637 hrs · 49,391 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,637 hrs · 49,397 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,637 hrs · 49,397 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L AND STR 8R. REPAIRED FRAME PER SWA EA.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 49,287 hrs · 49,067 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,260 hrs · 49,042 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 907 S8-9L) · airframe 49,177 hrs · 48,957 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, BETWEEN STR 8L TO STR 9L. REPAIRED FRAME PER SWA EA.

Part: PANEL — CRACKED (BS 717) · airframe 49,130 hrs · 48,914 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT KEEL BEAM PANEL CRACKED AT BS 717. REPAIRED PANEL PER SRM.

Part: FRAME — CRACKED (BS 907 S8L) · airframe 49,130 hrs · 48,914 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA.

Part: CABLE — FRAYED (L2 DOOR SLIDE) · airframe 49,130 hrs · 48,914 cycles

DURING SCHEDULED 16Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE CABLE FRAYED. REMOVED AND REPLACED CABLE PER MM.

Part: FRAME — CRACKED (BS 907 S8L) · airframe 49,130 hrs · 48,914 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA.

Part: CREASE BEAM — CORRODED (BS 947-995) · airframe 49,130 hrs · 48,914 cycles

DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM CHORD CORRODED BETWEEN BS 947 AND BS 995, RBL 50. REPAIRED CHORD PER SRM.

Part: STRINGER — CORRODED (BS 908) · airframe 49,136 hrs · 48,914 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER 4L CRACKED AT BS 908. REPAIRED STRINGER PER SRM.

Part: CREASE BEAM — CORRODED (BS 320-338) · airframe 49,136 hrs · 48,914 cycles

DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM CORRODED BETWEEN BS 320 AND BS 338, LBL 70. REPAIRED CREASE BEAM PER SRM.

Part: STRINGER CLIP — CRACKED (BS 400 S8L) · airframe 49,130 hrs · 48,914 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 8L. REMOVED ANAD REPLACED STRINGER CLIP PER SRM.

Part: SKIN — WORN (FUSELAGE) · airframe 49,130 hrs · 48,941 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SKIN AT UPPER BS 1008, RBL 12.75, WORN. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (BS 887 S2R) · airframe 49,130 hrs · 48,914 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 2R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: HOOK — LOOSE (R1 DOOR GIRT BAR) · airframe 49,130 hrs · 48,914 cycles

DURING SCHEDULED 16Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR HOOK LOOSE. SECURED HOOK PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 48,911 hrs · 48,689 cycles

DURING SCHEDULED SPV CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, LBL 4.75. REPAIRED WEB PER SWA EA.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 48,736 hrs · 48,525 cycles

DURING SCHEDULED MV4 CHECK, FOUND R1 DOOR CUTOUT FWD FRAME CENTER STUB FRAME CRACKED. REPAIRED FRAME PER SWA EA.

Part: BRACKET — BROKEN (FORE FLAP) · airframe 47,962 hrs · 47,774 cycles

LEFT WING OUTBOARD FORE FLAP BRACKET BROKEN OFF. REMOVED AND REPLACED FORE FLAP PER MM.

Part: CONTROLLER — ARCED (COCKPIT) · airframe 47,950 hrs · 47,764 cycles

FLIGHT COMPARTMENT L2 WINDOW ARCING. REMOVED AND REPLACED L2 WINDOW AND WINDOW HEAT CONTROLLER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,822 hrs · 47,627 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 930, STR 21L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,417 hrs · 46,179 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 375, BL 0. REPAIRED SKIN PER SWA EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 46,417 hrs · 46,179 cycles

DURING SCHEDULED BRDG CHECK, FOUND AFT PRESSURE BULKHEAD DOME CAP WEB CRACKED AT BS 1016, 9 O'CLOCK POSITION. REPAIRED BULKHEAD DOME CAP PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 46,417 hrs · 46,179 cycles

DURING SCHEDULED BRDG CHECK, FOUND AFT PRESSURE BULKHEAD DOME CAP WEB CRACKED AT BS 1016, 7 O'CLOCK POSITION. REPAIRED BULKHEAD DOME CAP PER SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 46,417 hrs · 46,179 cycles

DURING SCHEDULED BRDG CHECK, FOUND AFT PRESSURE BULKHEAD STIFFENER CRACKED AT BS 1016, 7 O'CLOCK POSITION. REPAIRED SIFFENER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,417 hrs · 46,179 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,417 hrs · 46,179 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,417 hrs · 46,179 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: CREASE BEAM — CORRODED (BS 847-867) · airframe 46,417 hrs · 46,179 cycles

DURING SCHEDULED BRDG CHECK, FOUND RT CREASE BEAM WEB CORRODED AT BS 847 TO BS 867. REPAIRED BEAM PER SRM & SWA EA.

Part: FLAP SYSTEM — VIBRATION (LT FORE FLAP) · airframe 46,015 hrs · 45,761 cycles

SLIGHT VIBRATION IN AIRCRAFT WHEN FLAPS ARE MOVING DOWN THRU 5 DEGREES. REMOVED AND REPLACED LT WING T/E INBOARD FORE FLAP PER MM.

Part: ACTUATOR — INOPERATIVE (SPOILER) · airframe 46,002 hrs · 45,751 cycles

AIRFRAME VIBRATION WITH FLAPS AT 5 DEGREES. REMOVED AND REPLACED NR 3 SPOILER ACTUATOR PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 45,577 hrs · 45,304 cycles

DURING SCHEDULED C2 CHECK, FOUND L1 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: DOOR FRAME — CRACKED (R1 DOOR) · airframe 45,577 hrs · 45,304 cycles

DURING SCHEDULED C2 CHECK, FOUND R1 DOOR LOWER FRAME WEB CRACKED AT AFT LOWER DOOR STOP. REMOVED AND REPLACED R1 DOOR PER MM.

Part: BOLT — LOOSE (FORE FLAP) · airframe 45,576 hrs · 45,303 cycles

AIRFRAME VIBRATION WHEN FLAPS EXTEND FROM 2 TO 5. REMOVED AND REPLACED LT WING INBOARD TRACK FITTING FORE FLAP BOLTS PER MM.

Part: PRESSURE PANEL — CRACKED (NLG W/W) · airframe 45,291 hrs · 44,990 cycles

DURING SCHEDULED PM CHECK, FOUND NLG W/W CEILING PANELS CRACKED AT RT BS 250 AND LT BS 250. REPAIRED CEILING PANELS PER SWA EA.

Part: CABLE — MISROUTED (L1 DOOR SLIDE) · airframe 44,764 hrs · 44,418 cycles

DURING SCHEDULED C1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED EVAC SLIDE CABLE PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 44,226 hrs · 43,836 cycles

EEPLS TRACK LOOSE AT ROW 6. REMOVED AND REPLACED EEPLS PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 43,066 hrs · 42,616 cycles

DURING SCHEDULED SERVICE CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SKIN — DELAMINATED (RT WING TE FLAPS) · airframe 43,017 hrs · 42,555 cycles

DURING SCHEDULED RON CHECK, FOUND RT WING INBOARD T/E AFT FLAP DELAMINATED. REPAIRED AFT FLAP PER SWA EA & SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 42,781 hrs · 42,318 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 11R. REPAIRED SKIN PER SWA EA.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 42,225 hrs · 41,714 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FWD, CENTER & AFT CABIN EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACKS PER MM.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 42,151 hrs · 41,634 cycles

DURING SCHEDULED A2 CHECK, AFT CABIN EMERGENCY LIGHTS INOP WHEN POWER REMOVED. REMOVED AND REPLACED AFT POWER SUPPLY PER MM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 40,442 hrs · 29,936 cycles

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

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 39,361 hrs · 38,790 cycles

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

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 39,010 hrs · 38,467 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BEADED PRESSURE WEB AT BS 663, RBL 40, CRACKED. REPAIRED BEADED PRESSURE WEB PER SRM.

Part: FASTENER — LOOSE (GIRT BAR HOOK) · airframe 39,010 hrs · 38,467 cycles

DURING SCHEDULED 1/4D CHECK, FOUND L1 DOOR EVAC SLIDE GIRT BAR HOOKS LOOSE. REMOVED AND REPLACED L1 DOOR EVAC SLIDE HOOK FASTENERS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 38,782 hrs · 38,249 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 937, STRINGER 24L, CRACKED. REPAIRED SKIN PER SRM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 38,782 hrs · 38,249 cycles

DURING SCHEDULED C2 CHECK, FOUND RT EMERGENCY EXIT LIGHT INOP. RELAMPED EMERGENCY EXIT LIGHT PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 37,405 hrs · 36,965 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND 2 EA CRACKS AT BS 178 BULKHEAD WEB LBL 7, WL 213 AND LBL 5, WL 213. REPAIRED BULKHEAD WEB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,405 hrs · 36,965 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME T-CHORD CRACKED AT BS 188, WL 207, RT SIDE. REPAIRED FRAME PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 37,405 hrs · 36,963 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD WEB CRACKED AT WL 187, RBL 1. REPAIRED WEB PER SRM.

Part: SLIDE — DISLODGED (SERVICE DOOR) · airframe 36,580 hrs · 36,189 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF CONTAINER WHEN OPENING THE DOOR. REMOVED AND REPLACED SLIDE PER MM.

Part: GASPER FAN — FAILED (E/E BAY) · airframe 36,526 hrs · 36,137 cycles

ELECTRICAL SMELL THROUGHOUT CABIN. FOUND GASPER FAN CIRCUIT BREAKER POPPED. REMOVED AND REPLACED GASPER FAN PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 36,166 hrs · 35,785 cycles

DURING SCHEDULED C3 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE OUT OF POSITION AND CABLE MISROUTED. REPOSITIONED SLIDE AND REROUTED CABLE PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 31,140 hrs · 31,077 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED (3 EA) BETWEEN STRS 8R AND 9R, BS 380, 747 AND 787. REPAIRED FRAMES PER BFG ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 31,140 hrs · 31,077 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED (4 EA) BETWEEN STRS 8L AND 9L, BS 520, 747, 787 AND 827. REPAIRED FRAMESPER BFG ER.

Part: SHEAR TIE — CRACKED (FWD CABIN) · airframe 31,140 hrs · 31,077 cycles

DURING SCHEDULED D CHECK, FOUND 2 EA SHEAR TIES CRACKED, BS 344 AND BS 360, BETWEEN STRINGERS 14R-15R. REPAIRED SHEAR TIES PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 31,140 hrs · 31,077 cycles

DURING SCHEDULED 1/4D CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 22R. REMOVED AND REPLACED STR CLIP PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,978 hrs · 30,920 cycles

EEPLS INOP FWD CABIN. REMOVED AND REPLACED LIGHT BASE AND INSTALLED END CAP SPACER PER MM.

Part: SLIDE — LOOSE (AFT ENTRY DOOR) · airframe 30,936 hrs · 30,875 cycles

AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR LANYARD LOOSE. SECURED LANYARD PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 30,928 hrs · 30,865 cycles

EEPLS LOOSE IN CABIN. SECURED EEPLS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,781 hrs · 29,741 cycles

EEPLS INOP AT MID CABIN. REPAIRED EEPLS PER MM.

Part: LIGHT — OUT OF POSITION (CABIN) · airframe 29,347 hrs · 29,329 cycles

R/H OVERWING EMERGENCY EXIT LIGHT OUT OF POSITION. REPOSITIONED LIGHT ASSY PER MM.

Part: COVER — MISSING (CABIN) · airframe 28,998 hrs · 28,988 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS TRACK COVERS MISSING. INSTALLED TRACK COVERS PER MM.

Part: COVER — BROKEN (CABIN) · airframe 28,771 hrs · 28,776 cycles

EEPLS TRACK COVER BROKEN. REMOVED AND REPLACED TRACK COVER PER MM.

Part: LENS — MISSING (CABIN FLOOR) · airframe 28,417 hrs · 28,428 cycles

EEPLS RED LENS MISSING AT MID CABIN. INSTALLED LENS PER MM.

Part: LIGHT — LOOSE (CABIN FLOOR) · airframe 28,417 hrs · 28,428 cycles

EEPLS PULLED UP LOOSE. REPAIRED EEPLS PER MM.

Part: COVER — LOOSE (CABIN) · airframe 28,105 hrs · 28,113 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS TRACK COVER LOOSE AT ROW 12. SECURED TRACK COVER PER MM.

Part: CHARGER — INOPERATIVE (GALLEY) · airframe 27,861 hrs · 27,697 cycles

DURING SCHEDULED SERVICE CHECK, FOUND AFT SVC DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: LIGHT — LOOSE (ROW 6) · airframe 27,601 hrs · 27,615 cycles

EGRESS LIGHT LENS ASSY LOOSE AT ROW 6. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — MISSING (CABIN) · airframe 27,203 hrs · 27,217 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS MISSING AFT END CAP AND LOOSE AT FWD END. INSTALLED AFT END CAP AND REMOVED AND REPLACED FWD END CAP PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 27,162 hrs · 27,141 cycles

EEPLS TRACK LOOSE AT ROW 2. SECURED WIRING AND COVER PER MM.

Part: COVER — LOOSE (CABIN FLOOR) · airframe 27,045 hrs · 27,048 cycles

EEPLS TRACK COVERS LOOSE. SECURED TRACK COVER PER MM.

Part: WIRE — EXPOSED (CABIN) · airframe 26,748 hrs · 26,757 cycles

EEPLS WIRING EXPOSED AT MID CABIN. REPAIRED TRACK LIGHT ASSY PER MM.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 26,739 hrs · 26,747 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND AFT SERVICE DOOR EXTERNAL EMERGENCY EXIT LIGHT INOPERATIVE. R&R BATTERY PACK PER MM.

Part: COVER — CRACKED (CABIN) · airframe 26,023 hrs · 26,023 cycles

SECTION OF EEPL TRACK COVER CRACKED. R & R TRACK COVER SECTION PER MM.

Part: SKIN — CRACKED (SERVICE DOORWAY)

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED ON AFT SERVICE DOOR LOWER FWD CUT OUT. REPAIRED SKIN PER SWA RA NR 1-553-2164.

Part: BULKHEAD CHORD — CRACKED (BS 178)

DURING SCHEDULED 1/4D CHECK, FOUND BS 178, RT SIDE CHORD CRACKED, RBL 26. REMOVED AND REPLACED CHORD SECTION PER SRM.

Part: BATTERY PACK — DISCHARGED (ROW 8-10)

DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT ROW 8-10. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: WIRE — BROKEN (ROW 6-7)

EEPLS WIRE BROKEN AT ROWS 6-7. REMOVED AND REPLACED EEPLS ASSY PER MM.

Part: LIGHT — INOPERATIVE (ROW 6 & 7)

EMERGENCY ESCAPE FLOOR TRACK LIGHT INOP AT ROWS 6 AND 7. RELAMPED 2 EA LIGHTS PER MM.

Part: COALESCER — CONTAMINATED (CABIN)

ODOR NOTED IN CABIN, BECAME MORE PRONOUNCED AFTER ENGINE START. ODOR BEST DESCRIBED AS BURNED TOAST, UNABLE TO DETERMINE SOURCE OF ODOR. CHANGED LT WATER SEPARATOR AND RT SEPARATOR BAG AS PER M/M. RAN ENGINES AT POWER WITH A/C PACKS BOTH ON, NO NOTICEABLE ODOR IN CABIN OR COCKPIT.

Part: LIGHT — INOPERATIVE (ROW 6)

DURING SCHEDULED A2 CHECK, FOUND EMERGENCY TRACK LIGHT INOP AT ROW 6. RESEATED TRACK LIGHT CONNECTOR PER BOEING MM.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED RON CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT R2 EXIT IDENTIFIER BULLNOSE AT 18L AND 20R FLOOR PROX AT 16-19. REPLACED BATTERY PACK AT DOOR R2 POSITION PER BOEING MM.

Part: LIGHT — INOPERATIVE (CABIN)

DURING WALKAROUND CHECK, CABIN FLOOR TRACK LIGHTING AT ROW 7 INOP AND MISSING COVER. REPLACED LIGHT ASSEMBLY AND COVER, OP CHECKED PER BOEING M/M.

Part: LIGHTS — INOPERATIVE (CABIN)

DURING WALKAROUND, FOUND 2 CABIN FLOOR TRACK LIGHTS INOP AT ROW 7. REPLACED AS REQUIRED PER BOEING M/M.

Part: SKIN — GOUGED (PAX DOOR CUTOUT)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN GOUGED 15.5 BELOW AFT ENTRY DOOR. REPAIRED PER BOEING SRM.

Part: LATCH LEVER — MALFUNCTIONED (LANDING GEAR)

AFTER TAKEOFF, LANDING GEAR LEVER WOULD NOT PASS OFF POSITION WITHOUT USING OVERRIDE. FLIGHT CONTINUED AND LANDED NORMALLY. REMOVED AND REPLACED LANDING GEAR LATCH LEVER AND PRESSURE WARNING CIRCUIT BREAKER ON P6-3 PANEL. OPS CHECKED GOOD PER BOEING M/M.

Part: BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED A-CHECK, FOUND FWD ENTRY EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY PACK PER BOEING M/M.