N627SW

Part: CONTROL PANEL — FAULTED (AUTO FLIGHT SYS) · airframe 67,701 hrs · 53,093 cycles

MCP FAILED IN FLIGHT NO AUTO-FLIGHT SYSTEMS OPERATIVE. REMOVED AND REPLACED MCP PANEL, IAW B737 AMM 22-11-34. OPERATIONS CHECK GOOD.

Part: GIRT BAR — LOOSE (L1 DOOR) · airframe 67,024 hrs · 52,708 cycles

L1 DOOR SLIDE GIRT BAR ANGLES ARE LOOSE. SECURED GIRT BAR ASSEMBLY IAW SIP & AMM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 66,248 hrs · 52,172 cycles

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

Part: DOOR FRAME — CRACKED (L1 DOOR) · airframe 66,248 hrs · 52,172 cycles

L1 DOOR AFT STOP 6TH FROM TOP, FRAME CRACKED INSIDE CUTOUT ON DOOR. R&R DOOR ASSEMBLY PER MM.

Part: LENS — LOOSE (CABIN) · airframe 65,985 hrs · 52,003 cycles

RT OVERWING EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: TRANSMITTER — MALFUNCTIONED (FLAP POSITION) · airframe 65,744 hrs · 51,839 cycles

WHILE CONFIGURING FOR LANDING, FLAP 1 WAS SELECTED AND THE FLAP GAUGE INDICATED LESS THAN COMMANDED. FLAPS WITH NEEDLE SPLIT ON GAUGE & LE TRANSIT LIGHT ILLUMINATED. R & R THE RIGHT FLAP POSITION TRANSMITTER IAW MM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 65,566 hrs · 51,727 cycles

LEFT OVERHEAD BULLNOSE EMERGENCY LIGHT, INOPERATIVE BETWEEN ROWS 10 TO 18. R & R THE BATTERY PACK IAW AMM.

Part: LIGHT — BROKEN (CABIN) · airframe 65,429 hrs · 51,637 cycles

L1 DOOR EMERGENCY EXIT LIGHT BASE BROKEN. R&R BASE ASSEMBLY PER MM.

Part: ACTUATOR — FAULTY (LE SLAT) · airframe 64,763 hrs · 51,182 cycles

AIR TURNBACK, NR 3 KRUEGER REMAINED EXTENDED. R&R NR 3 KRUEGER FLAP ACTUATOR AMM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 63,337 hrs · 50,231 cycles

FLOORBEAM STABILIZER STRAP CRACKED AT BS 344, BL 0. R & R STRAP IAW SRM & DWG.

Part: ATTACH BRACKET — CRACKED (LT WING) · airframe 63,337 hrs · 50,231 cycles

LEFT WING FIRE BOX ACCESS PANEL ATTACH BRACKET CRACKED, AT OTBD SIDE OF NR 3 FLAP TRACK CANOE. R & R BRACKET IAW SRM.

Part: BRACKET — CRACKED (RT WING) · airframe 63,337 hrs · 50,231 cycles

RIGHT WING UPPER SPAR CHORD BRACKET CRACKED AT RSS 235. R & R BRACKET IAW DWG & EA.

Part: BRACKET — CRACKED (LT WING) · airframe 63,337 hrs · 50,231 cycles

LEFT WING BRACKET COMMON TO UPPER SPAR CHORD CRACKED AT RSS 235. R & R BRACKET IAW DWG & EA.

Part: FITTING — CRACKED (RT WING) · airframe 63,337 hrs · 50,231 cycles

RIGHT WING FWD BEAM FITTING CRACKED AT RSS 225.14, LOWER FWD FASTENER COMMON TO LOWER CHORD. REPAIRED FITTING IAW ER & EA.

Part: FITTING — CRACKED (LT WING) · airframe 63,337 hrs · 50,231 cycles

LEFT WING FWD MLG BEAM FITTING CRACKED AT 5 - 7 HOLE POSITIONS. REPAIRED FITTING IAW ER & EA.

Part: SPAR — CRACKED (RT WING) · airframe 63,337 hrs · 50,231 cycles

RIGHT WING REAR SPAR UPPER CHORD CRACKED AT RSS 285, BETWEEN HOLE 4, 5 & 12. REPAIRED CHORD IAW EA.

Part: LINK — CORRODED (LT MLG) · airframe 63,337 hrs · 50,231 cycles

LEFT MLG SUPPORT BEAM INBD SWING LINKS CORRODED. R & R SWING LINK ASSEMBLY IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 63,337 hrs · 50,231 cycles

LEFT WING REAR SPAR UPPER CHORD CRACKED, BETWEEN RSS 220 - 285. REPAIRED CHORD IAW EA.

Part: LINK — CORRODED (RT MLG) · airframe 63,337 hrs · 50,231 cycles

RIGHT MLG SUPPORT BEAM INBD SWING LINK CORRODED. R & R SWING LINK ASSEMBLY IAW EA.

Part: SUPPORT FITTING — CRACKED (LT WING) · airframe 63,337 hrs · 50,231 cycles

LEFT WING CRACKED, FOUND IN THE AFT SUPPORT FITTING AT NR 5 HOLE, RSS 222. REPAIRED FITTING IAW EA.

Part: SPAR — CRACKED (RT WING) · airframe 63,337 hrs · 50,231 cycles

RIGHT WING REAR SPAR WEB CRACKED, BETWEEN RSS 211 - 238, BETWEEN HOLE NR 4, 5, 7, 8 & 12. REPAIRED WEB IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 63,337 hrs · 50,231 cycles

LEFT WING REAR SPAR WEB CRACKED, BETWEEN RSS 220 - 223. REPAIRED WEB IAW EA.

Part: SUPPORT FITTING — CRACKED (RT WING) · airframe 63,337 hrs · 50,231 cycles

RIGHT WING NR 5 HOLE MLG AFT SUPPORT FITTING CRACKED. REPAIRED FITTING IAW ER & EA.

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 62,544 hrs · 49,725 cycles

AFT WINDSCREEN LT EMER FLASHLIGHT STRAP BROKEN. R & R STRAP IAW SOPM.

Part: SKIN — CRACKED (L1 DOOR) · airframe 62,544 hrs · 49,725 cycles

L1 DOOR FWD SIDE, OUTER SKIN CRACKED, FROM BOTTOM ON DOOR EDGE. REPAIRED SKIN IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 62,544 hrs · 49,725 cycles

FORWARD CARGO PIT FRAME, CORRODED AT 500A, BETWEEN STRINGER 27R - 28R. REPAIRED FRAME IAW SRM.

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 62,544 hrs · 49,725 cycles

SHEAR WEB CORRODED, BETWEEN BS 986 - 1016, RBL 60. R & R SHEAR WEB IAW SRM & DWG.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 62,544 hrs · 49,725 cycles

AFT CARGO SUPPORT ANGLE BRACKET CRACKED AT BS 807, RBL 8.1. R & R BRACKET IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 62,544 hrs · 49,725 cycles

INTERCOSTAL CRACKED, BETWEEN BS 867 - 887, STRINGER 25R. R & R INTERCOSTAL IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 62,544 hrs · 49,725 cycles

SHEAR CLIP CRACKED AT BS 360, STRINGER 5L. R & R SHEAR CLIP IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 62,544 hrs · 49,725 cycles

LEFT CREASE BEAM WEB CORRODED, BETWEEN BS 500 - 500A. R & R WEB IAW SRM & DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 62,544 hrs · 49,725 cycles

LEFT CREASE BEAM WEB CORRODED, BETWEEN BS 500A - 500B. R & R WEB IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 62,544 hrs · 49,725 cycles

LEFT CREASE BEAM WEB CORRODED, BETWEEN BS 847 - 867. R & R WEB IAW SRM & DWG.

Part: TEE FITTING — CRACKED (FUSELAGE) · airframe 62,544 hrs · 49,725 cycles

FORWARD GALLEY DOOR CUT OUT INTERCOSTAL T CHORD CRACKED AT BS 332.1, STRINGER 8A. REPAIRED T CHORD IAW ER & EA.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 62,544 hrs · 49,725 cycles

LEFT CREASE BEAM CHORD CRACKED AT BS 639. REPAIRED CHORD IAW ER & EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,544 hrs · 49,725 cycles

SHEAR TIE CORRODED AT BS 727E, BETWEEN STRINGER 26R - 27R. REPAIRED SHEAR TIE IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 62,544 hrs · 49,725 cycles

FLOORBEAM CORRODED AT BS 986, RBL 45. REPAIRED FLOORBEAM IAW ER & EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,544 hrs · 49,725 cycles

SHEAR TIE CORRODED AT BS 887, BETWEEN STRINGER 19L - 20L. R & R SHEAR TIE IAW SRM & DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 62,544 hrs · 49,725 cycles

SHEAR TIE CORRODED AT BS 787, BETWEEN STRINGER 25 - 26R. R & R FRAME ASSEMBLY IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,544 hrs · 49,725 cycles

SHEAR TIE CORRODED AT BS 947.5, BETWEEN STRINGER 25L - 26L. R & R SHEAR TIE IAW SRM & DWG.

Part: TAIL CONE — DELAMINATED (FUSELAGE) · airframe 62,295 hrs · 49,564 cycles

TAIL CONE DELAMINATED AT 8 O CLOCK BELOW STROBE. REPAIRED TAIL CONE IAW EA.

Part: LENS — CRACKED (CABIN) · airframe 61,860 hrs · 49,257 cycles

R1 DOOR OVERHEAD EMER EXIT LIGHT LENS CRACKED. REPAIRED LENS IAW EA.

Part: SLAT — DELAMINATED (LT WING) · airframe 60,563 hrs · 48,340 cycles

LEFT WING NR 1 SLAT DELAMINATED INBD AFT CORNER. R & R NR 1 SLAT IAW AMM.

Part: FLAP — DELAMINATED (LT WING) · airframe 60,563 hrs · 48,340 cycles

LEFT WING OTBD AFT FLAP DELAMINATED AT OTBD AREA. R & R AFT FLAP IAW MM.

Part: FITTING — CRACKED (LT SPOILER) · airframe 60,563 hrs · 48,340 cycles

LEFT WING INBD GND SPOILER INBD ACTUATOR FITTING CRACKED. R & R FITTING IAW AMM.

Part: FAIRING — DELAMINATED (TE FLAP) · airframe 60,563 hrs · 48,340 cycles

LEFT WING INBD FLAP OTBD TRACK FAIRING DELAMINATED INBD AFT AREA. REPAIRED FAIRING IAW SRM.

Part: SLAT — DELAMINATED (RT WING) · airframe 60,563 hrs · 48,340 cycles

RIGHT WING NR 4 SLAT TE WEDGE INBD END DELAMINATED. R & R NR 4 SLAT ASSEMBLY IAW AMM.

Part: STRAP — DISPLACED (CABIN) · airframe 60,563 hrs · 48,340 cycles

RIGHT EMER EXIT HATCH THE ESCAPE STRAP DISPLACED. REINSTALLED STRAP IAW AMM.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 58,845 hrs · 47,208 cycles

AFT CARGO DOOR SKIN OUTER HANDLE CUT OUT CRACKED AT RADIUS OF UPPER AFT CORNER. REPAIRED SKIN IAW EA.

Part: FLAP — DELAMINATED (LT WING) · airframe 58,839 hrs · 47,204 cycles

LEFT WING INBD TE AFT FLAP DELAMINATED. R & R AFT FLAP IAW MM.

Part: ATTACH BRACKET — CRACKED (L1 DOOR) · airframe 58,171 hrs · 46,722 cycles

L1 DOOR LOWER SWEEPER SEAL ATTACH BRACKET CRACKED ON BOTH SIDES OF FASTENER. R & R DOOR ASSEMBLY IAW MM.

Part: SIGN — BROKEN (CABIN) · airframe 57,966 hrs · 46,574 cycles

FORWARD ENTRY LOWER EMERGENCY EXIT SIGN BROKEN. R & R SIGN ASSEMBLY IAW MM.

Part: DOOR FRAME — CRACKED (R1 DOOR) · airframe 57,030 hrs · 45,919 cycles

R1 DOOR LOWER FRAME AT LOWER AFT STOP ATTACH AREA CRACKED. R & R DOOR IAW MM.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 56,547 hrs · 45,599 cycles

RT CHORD CRACKED AT BS 727, LOWER FASTENER ROW OF S-18A. REPAIRED CHORD IAW EA.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 56,547 hrs · 45,599 cycles

LT CHORD CRACKED AT BS 727, LOWER FASTENER ROW OF S-18A. REPAIRED CHORD IAW EA.

Part: STRAP — CRACKED (FUSELAGE) · airframe 56,547 hrs · 45,599 cycles

STRAP CRACKED BETWEEN BS 312 TO BS 348, RBL 31.6. R & R STRAP IAW SRM & DRAWING.

Part: SKIN — DELAMINATED (RT SPOILER) · airframe 56,547 hrs · 45,599 cycles

RT WING UPPER EDGE NR 5 GROUND SPOILER SKIN DELAMINATED. R & R NR 5 SPOILER IAW MM.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 56,547 hrs · 45,599 cycles

RT WING TE SUPPORT ANGLE CRACKED AT NR 6 FAIRING. R & R ANGLE IAW SRM.

Part: ACCESS PANEL — CRACKED (RT PYLON) · airframe 56,547 hrs · 45,599 cycles

RT WING PYLON STRUT ACCESS PANEL 5851R CRACKED. REPAIRED PANEL IAW SRM.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 56,547 hrs · 45,599 cycles

LT WING SUPPORT ANGLE CRACKED AT FSS 182. R & R ANGLE IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,547 hrs · 45,599 cycles

FRAME INNER CHORD CRACKED AT BS 348.2, STRINGER 17L. R & R CHORD IAW EO & EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 56,547 hrs · 45,599 cycles

FWD ENTRY DOOR SURROUND SUPPORT TIE CLIP CRACKED AT BS 348.2, STRINGER 15L. R & R TIE CLIP IAW SRM & DRAWING.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 56,547 hrs · 45,599 cycles

MLW WW PRESS WEB CRACKED AT BS 675, RBL 45.5. REPAIRED WEB IAW SRM.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 56,547 hrs · 45,599 cycles

MLG WW PRESS WEB CRACKED AT BS 675, LBL 24.5+5.5. REPAIRED WEB IAW SRM.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 56,547 hrs · 45,599 cycles

RT CHORD LOWER FASTENER FWD FROM CHORD CENTER LINE CRACKED AT BS 727, STRINGER 18A. REPAIRED CHORD IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 56,547 hrs · 45,599 cycles

FLOOR BEAM UPPER CHORD CRACKED AT BS 727B, LBL 45.5. REPAIRED CHORD IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,547 hrs · 45,599 cycles

LT FRAME OTBD CHORD CRACKED AT BS 727 FWD FLANGE, 1.0" FWD FROM CHORD CENTER LINE & LOWER FASTENER ROW OF S-18A. REPAIRED CHORD IAW EA.

Part: ACCESS PANEL — CRACKED (RT HORIZ. STAB) · airframe 56,547 hrs · 45,599 cycles

RT HORIZONTAL STABILIZER ACCESS PANEL N9224R CRACKED. R & R PANEL IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 56,547 hrs · 45,599 cycles

FLOOR BEAM UPPER CHORD CRACKED AT STATION 727B, LBL 45.5. REPAIRED CHORD IAW EA.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 56,547 hrs · 45,599 cycles

MAIN WW PRESSURE DECK CRACKED AT BS 663.75, LBL 24.5. REPAIRED DECK IAW SRM.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 56,547 hrs · 45,599 cycles

MAIN WW PRESSURE DECK CRACKED AT BS 675, RBL 45.5. REPAIRED DECK IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,547 hrs · 45,599 cycles

FRAME CRACKED AT BS 500B, BETWEEN STRINGER 21L & 22L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,547 hrs · 45,599 cycles

LT FRAME OTBD CHORD CRACKED AT BS 727, STRINGER 18A. REPAIRED CHORD IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 56,547 hrs · 45,599 cycles

LONGITUDINAL FLOOR BEAM CRACKED AT BS 727B, RBL 45.5. REPAIRED BEAM IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 56,547 hrs · 45,599 cycles

SEAT TRACKS CRACKED AT BS 727B, LBL 45.5. REPAIRED SEAT TRACK IAW SRM & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,547 hrs · 45,599 cycles

LT FWD FLANGE FRAME CHORD CRACKED AT BS 727, STRINGER 18A. REPAIRED CHORD IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,547 hrs · 45,599 cycles

LT SIDE FRAME OTBD CHORD CRACKED AT BS 727, STRINGER 18A. REPAIRED CHORD IAW EA.

Part: LENS — BROKEN (CABIN) · airframe 56,512 hrs · 45,581 cycles

FWD ENTRY EMERGENCY EXIT LENS OTBD OF FLIGHT ATTENDANT JUMP SEAT BROKEN. R & R LENS IAW AMM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 56,230 hrs · 45,364 cycles

AFT INBD EMERGENCY FLASHLIGHT BATTERY INDICATOR INOPERATIVE. R & R BATTERY IAW MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 55,946 hrs · 45,145 cycles

LT WING OTBD AFT FLAP DELAMINATED. REPAIRED AFT FLAP IAW SRM.

Part: SUPPORT CHANNEL — CORRODED (FUSELAGE) · airframe 55,946 hrs · 45,145 cycles

ANTENNA SUPPORT CHANNEL CORRODED AT STATION 727D+15. REPAIRED CHANNEL IAW SRM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 55,893 hrs · 45,104 cycles

FWD LEFT INTERIOR EMERGENCY EXIT SIGN INOPERATIVE. RELAMPED SIGN IAW AMM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 55,893 hrs · 45,104 cycles

AFT RT INTERIOR EMERGENCY EXIT SIGN INOPERATIVE. RELAMPED SIGN IAW AMM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 55,893 hrs · 45,104 cycles

AFT LT INTERIOR EMERGENCY EXIT SIGN INOPERATIVE. RELAMPED SIGN IAW AMM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 55,888 hrs · 45,103 cycles

STRINGER CRACKED AT STATION 530, STRINGER 4L. REPAIRED STRINGER IAW SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,888 hrs · 45,103 cycles

STRINGER CLIP CRACKED AT STATION 380, STRINGER 8L. R&R CLIP IAW SRM & DRAWING.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,888 hrs · 45,103 cycles

LT BS 847+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLE NR 5. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,888 hrs · 45,103 cycles

LT BS 867+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLE NR 2,3,4, & 5. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,888 hrs · 45,103 cycles

LT BS 827+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES NR 10. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,888 hrs · 45,103 cycles

LT BS 787+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLE NR 12 & HOLES 1,2,9. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,888 hrs · 45,103 cycles

LT BS 807+10 LOWER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLE NR 2 & HOLE NR 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,888 hrs · 45,103 cycles

LT BS 887+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLE NR 9 & HOLE NR 7. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,888 hrs · 45,103 cycles

LT BS 787+10 LOWER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLES 3,4,5,9. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,888 hrs · 45,103 cycles

LT BS 767+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 1,2,3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,888 hrs · 45,103 cycles

LT BS 867+10 LOWER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLE NR 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,888 hrs · 45,103 cycles

LT BS 847+10 LOWER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLES 2,3. REPAIRED SKIN IAW SB.

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 55,553 hrs · 44,852 cycles

L1 DOOR EMERGENCY EXIT LIGHT COVER LOOSE. SECURED COVER IAW MM.

Part: SIGN — LOOSE (CABIN) · airframe 55,510 hrs · 44,822 cycles

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

Part: SKIN PANEL — DELAMINATED (FUSELAGE) · airframe 54,751 hrs · 44,284 cycles

BS 727E TO 867 DISBONDED AND GAPS WERE DISCOVERED ALONG THE UPPER EDGE OF THE LOWER SKIN PANEL AT THE STR 4R LAP JOINT. R & R SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,751 hrs · 44,284 cycles

FUSELAGE HAS 1.5" SUB SURFACE SKIN CRACK AT BS 727E + 11" ABOVE STR 4R. REPAIR COMPLETED PER EA 1-353-21709.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,751 hrs · 44,284 cycles

FUSELAGE HAS 3" SUB-SURFACE SKIN CRACK AT BS 827 + 12" ABOVE STR 4R. REPAIR COMPLETED PER EA 1-353-21707 FACT AS A RESULT OF POST REPAIR INSPECTION.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,751 hrs · 44,284 cycles

FUSELAGE HAS 2" SUB SURFACE SKIN CRACK AT BS 807 + 14" ABOVE STR 4R. REPAIR COMPLETED ON NRC C789497. REPAIR COVERED IN ONE EA 1-353-21707.

Part: LENS — UNSECURE (CABIN) · airframe 53,974 hrs · 43,719 cycles

L1 DOOR EMERGENCY LIGHT LENS FELL OFF. RE-INSTALLED LENS PER M/M.

Part: GIRT BAR — LOOSE (L1 DOOR) · airframe 53,925 hrs · 43,681 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR LOOSE. SECURED GIRT BAR IAW AMM.

Part: SLAT — DELAMINATED (RT WING) · airframe 53,745 hrs · 43,547 cycles

NR 6 SLAT I/B SIDE DELAMINATED. REMOVED AND REPLACED SLAT ASSY PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 53,745 hrs · 43,547 cycles

LEFT OUTBOARD AFT FLAP DELAMINATED AT NR 2 FAIRING CONTACT AREA. REMOVED AND REPLACED FLAP ASSY PER MM.

Part: SLAT — DELAMINATED (LT WING) · airframe 53,745 hrs · 43,547 cycles

LEFT WING NR 2 SLAT UPPER TRAILING EDGE OUTBOARD CORNER DELAMINATED. REMOVED AND REPLACED NR 2 SLAT PER AMM.

Part: COVER — OUT OF POSITION (CABIN) · airframe 53,522 hrs · 43,384 cycles

L1 DOOR EMERGENCY EXIT LIGHT COVER CAME OFF. RE-INSTALLED COVER IAW AMM.

Part: LENS — BROKEN (CABIN) · airframe 53,204 hrs · 43,134 cycles

L1 DOOR LOWER EMERGENCY LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: LENS — LOOSE (CABIN) · airframe 53,136 hrs · 43,079 cycles

FORWARD ENTRY DOOR EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,112 hrs · 43,063 cycles

FUSELAGE SKIN CRACKED AT BS 839, STR 10R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,112 hrs · 43,063 cycles

FUSELAGE SKIN CRACKED AT BS 858, STR 10R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,112 hrs · 43,063 cycles

FUSELAGE SKIN CRACKED AT BS 727D + 10, STR 10L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,112 hrs · 43,063 cycles

FUSELAGE SKIN CRACKED AT BS 727A + 11, STR 10R. REPAIRED SKIN CRACKED PER EA.

Part: COVER — LOOSE (EXIT SIGN) · airframe 52,661 hrs · 42,722 cycles

L1 DOOR LOWER EMERGENCY EXIT SIGN COVER LOOSE. RE-SECURED COVER PER AMM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 52,576 hrs · 42,650 cycles

FLOORBEAM STABILIZER STRAP CRACKED AT BS 344, LBL 10. REMOVED AND REPLACED STRAP IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 52,576 hrs · 42,650 cycles

LEFT WING NR 1 SLAT LEADING EDGE SKIN CRACKED. REPAIRED SKIN IAW SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,576 hrs · 42,650 cycles

CONTROL CABIN EMERGENCY LIGHT INOP. RELAMPED LIGHT PER AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,576 hrs · 42,650 cycles

SKIN CRACKED AT BS 877+10, STR 4R. REPAIRED SKIN IAW EA AND ER.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,675 hrs · 41,955 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 500C, BETWEEN STR 27R TO STR 28R. REPAIRED FRAME IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,675 hrs · 41,955 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 400, BETWEEN STR 24R TO STR 25R. REPAIRED FRAME IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 51,675 hrs · 41,955 cycles

DURING SCHEDULED 16Y CHECK, FOUND UPPER CHORD FLOORBEAM CRACKED AT BS 294.5, LBL 53. REPAIRED BEAM IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,675 hrs · 41,955 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGR CLIP CRACKED AT BS 360, STR 11L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,675 hrs · 41,955 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 500B, BETWEEN STR 28L TO STR 28R. REPAIRED FRAME IAW SRM.

Part: FITTING — CORRODED (FUSELAGE) · airframe 51,675 hrs · 41,955 cycles

DURING SCHEDULED 16Y CHECK, FOUND LONGITUDINAL FLOORBEAM CLIP CRACKED AT BS 639, RBL 45.5. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 51,675 hrs · 41,955 cycles

DURING SCHEDULED 16Y CHECK, FOUND CHORD CORRODED BETWEEN BS 947 TO BS 1006, RBL 48. REMOVED AND REPLACED CHORD IAW SRM AND DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 51,675 hrs · 41,955 cycles

DURING SCHEDULED 16Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 727B, RBL 24.8. REPAIRED CHORD IAW EA.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 51,675 hrs · 41,955 cycles

DURING SCHEDULED 16Y CHECK, FOUND CHORD CORRODED BETWEEN BS 907.7 TO BS 986.5+12, LBL 50. REMOVED AND REPLACED CHORD IAW SRM AND DWG.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 51,675 hrs · 41,955 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT WING I/B FORE FLAP UPPER SKIN DELAMINATED AT I/B END. REPAIRED FORE FLAP IAW MM.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 51,675 hrs · 41,955 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT WING I/B FORE FLAP SKIN DELAMINATED. REPAIRED FORE FLAP PER SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 51,675 hrs · 41,955 cycles

DURING SCHEDULED 16Y CHECK, FOUND WEB CORRODED BETWEEN BS 787 TO BS 807, STR 17L. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,675 hrs · 41,955 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 787, BETWEEN STR 27R TO STR 27L. REPAIRED FRAME IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,675 hrs · 41,955 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME INNER CHORD CRACKED AT BS 616, STR 16R. REPAIRED CHORD PER EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,675 hrs · 41,955 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 500A, BETWEEN STR 28L TO STR 28R. REPAIRED FRAME IAW SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,675 hrs · 41,955 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR CUTOUT LOWER CORNER. REPAIRED SKIN IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,675 hrs · 41,955 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 767, BETWEEN STR 27R TO STR 27L. REPAIRED FRAME IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 51,675 hrs · 41,955 cycles

DURING SCHEDULED 16Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 706, RBL 24.8. REPAIRED BEAM IAW EO.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,675 hrs · 41,955 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 727D, BETWEEN STR 25L TO STR 26L. REPAIRED FRAME IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 51,675 hrs · 41,955 cycles

CRACK ON FLOORBEAM AT LBL 70.53 BS 520. REPAIRED BEAM IAW EA AND EO.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,675 hrs · 41,955 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 344, STR 27R. REMOVED AND REPLACED FRAME IAW SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,675 hrs · 41,955 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 328, STR 7R. REMOVED AND REPLACED SHEAR TIE IAW SRM AND DWG.

Part: SPOILER — PUNCTURED (RT WING) · airframe 51,675 hrs · 41,955 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT WING NR 6 SPOILER PUNCTURED. REPAIRED SPOILER IAW SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 51,675 hrs · 41,955 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CORRODED BETWEEN BS 348.5 TO BS 360, STR 8L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 51,675 hrs · 41,955 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 907, STR 27R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 51,675 hrs · 41,955 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 907, STR 26R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,675 hrs · 41,955 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 4L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,675 hrs · 41,955 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 11L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 51,675 hrs · 41,955 cycles

DURING SCHEDULED 16Y CHECK, FOUND LONGITUDINAL FLOORBEAM ATTACH CLIP CRACKED AT BS 639, RBL 45.5. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,675 hrs · 41,955 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 986.5, BETWEEN STR 27R TO STR 27L. REMOVED AND REPLACED SHEAR TIE IAW SRM AND DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 51,675 hrs · 41,955 cycles

CORROSION ON STRINGER 20R BETWEEN BS 986 TO BS 1006. REPAIRED STRINGER IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,675 hrs · 41,955 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 16R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,675 hrs · 41,955 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 11R. REMOVED AND REPLACED CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,675 hrs · 41,955 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 19L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,675 hrs · 41,955 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 11R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 51,675 hrs · 41,955 cycles

DURING SCHEDULED 16Y CHECK, FOUND FITTING CRACKED AT S 332.1, STR 8R. REMOVED AND REPLACED FITTING IAW SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,675 hrs · 41,955 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 1006, BETWEEN STR 26R TO STR 26L. REMOVED AND REPLACED SHEAR TIE IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,675 hrs · 41,955 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 16R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,675 hrs · 41,955 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 10L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 51,675 hrs · 41,955 cycles

DURING SCHEDULED 16Y CHECK, FOUND LONGITUDINAL FLOORBEAM CLIP CRACKED AT BS 639, LBL 45.5. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,675 hrs · 41,955 cycles

CRACK ON FUSELAGE SKIN LOCATED ON BS 907 AT STR 18L. REPAIRED FUSELAGE SKIN IAW EO AND EA.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 51,675 hrs · 41,955 cycles

DURING SCHEDULED 16Y CHECK, FOUND ATTACH ANGLE CRACKED AT BS 294.5, STR 13L. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,675 hrs · 41,955 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 11L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,675 hrs · 41,955 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 11R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,675 hrs · 41,955 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663.75, STR 10R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,675 hrs · 41,955 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663.75, STR 10L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 51,675 hrs · 41,955 cycles

CRACKS ON VERTICAL BEAM WEB BS 178, RBL 5.7. REPAIRED WEB IAW AND EO.

Part: WEB — CRACKED (FUSELAGE) · airframe 51,675 hrs · 41,955 cycles

WEB CRACK FOUND AT RBL 45.5 AND BS 616. REPAIRED WEB IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,675 hrs · 41,955 cycles

CRACK FOUND ON EDGE OF FRAME WEB LOCATED AT BS 616 AND 6" BELOW OF STR 17L. REPAIRED WEB IAW EO AND EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 51,675 hrs · 41,955 cycles

CRACK ON UPPER FLANGE OF FLOORBEAM LOCATED BS 947.5 AND LBL 53.5. REPAIRED CHORD IAW EA AND EO.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 51,675 hrs · 41,955 cycles

CORROSION ON UPPER FLANGE OF FLOORBEAM LOCATED BS 947.5 AND BETWEEN RBL 24.5 TO LBL 24.5 AFT CABIN. REPAIRED CHORD IAW EA AND EO.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 51,675 hrs · 41,955 cycles

CORROSION ON FLANGE OF FLOORBEAM LOCATED BS 967 AT RBL4. REPAIRED BEAM IAW SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 51,675 hrs · 41,955 cycles

CRACK ON CREASE BEAM LOCATED BS 520 AT STR 17L. REPAIRED BEAM IAW EA AND EO.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 51,675 hrs · 41,955 cycles

CRACK ON WEB OF LONGITUDINAL FLOORBEAM LBL 24.5 AND BS 705. REPAIRED WEB IAW EA AND EO.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 51,675 hrs · 41,955 cycles

CRACK ON FLOORBEAM UPPER CHORD AT LBL 24.75 AND BS 668. REPAIRED FLOORBEAM UPPER CHORD IAW EA AND EO.

Part: BEAM — CRACKED (FUSELAGE) · airframe 51,675 hrs · 41,955 cycles

CRACK FOUND STUB BEAM AT BS 616 LT SIDE. REPLACED STUB BEAM IAW SRM AND EA.

Part: BEAM — CRACKED (FUSELAGE) · airframe 51,675 hrs · 41,955 cycles

CRACK FOUND AT STUB BEAM BS 616 RT SIDE. REPLACED STUB BEAM IAW EA AND EO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,675 hrs · 41,955 cycles

CRACK FOUND AT BS 616 FRAME INNER CHORD LT SIDE WL 221. REPAIRED FRAME IAW EO AND EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,675 hrs · 41,955 cycles

CORROSION ON FRAME LOCATED AT BS 500A BETWEEN S 28L AND S 28R FWD CARGO COMPARTMENT. REPAIRED FRAME IAW SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,675 hrs · 41,955 cycles

CRACKS ON EXTERNAL SKIN CUTOUT OF OUTFLOW VALVE LOCATED BS 360+19" AND BL 0. REPAIRED SKIN BETWEEN BS 360 AND BS 403 FROM S-26L TO S-26R IAW EA.

Part: COVER — LOOSE (CABIN) · airframe 50,966 hrs · 41,418 cycles

L1 DOOR EMERGENCY EXIT LIGHT COVER LOOSE. REMOVED AND REPLACED LIGHT PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 50,242 hrs · 40,859 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT OVERWING EMERGENCY EXIT SIDEWALL LIGHT INOP. REMOVED AND REPLACED LAMP PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 49,783 hrs · 40,523 cycles

DURING SCHEDULED MV3 CHECK FOUND, R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: COVER — LOOSE (CABIN) · airframe 49,318 hrs · 40,171 cycles

L1 DOOR EMERGENCY EXIT COVER LOOSE. SECURED COVER PER MM.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 49,267 hrs · 40,133 cycles

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

Part: LENS — BROKEN (CABIN) · airframe 47,804 hrs · 39,010 cycles

L1 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: LENS — LOOSE (CABIN) · airframe 47,241 hrs · 38,585 cycles

L1 DOOR EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: LENS — LOOSE (CABIN) · airframe 46,797 hrs · 42,226 cycles

EMERGENCY EXIT LIGHT LENS LOOSE AT L1 DOOR. REMOVED AND REPLACED LENS PER MM.

Part: RETAINER — LOOSE (GIRT BAR) · airframe 46,374 hrs · 37,912 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR RETAINER LOOSE. SECURED RETAINER PER MM.

Part: GIRT BAR — LOOSE (EVAC SLIDE) · airframe 46,337 hrs · 37,885 cycles

DURING SCHEDULED 14Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR LOOSE. SECURED GIRT BAR PER MM.

Part: COVER — CRACKED (CABIN) · airframe 46,337 hrs · 37,885 cycles

DURING SCHEDULED 14Y CHECK, FOUND LT EEPLS COVER CRACKED BETWEEN ROW 4 TO ROW 11. REMOVED AND REPLACED COVER PER MM.

Part: COVER — CRACKED (CABIN) · airframe 46,337 hrs · 37,885 cycles

DURING SCHEDULED 14Y CHECK, FOUND RT EEPLS COVER CRACKED BETWEEN ROW 8 TO ROW 12. REMOVED AND REPLACED COVER PER MM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 46,338 hrs · 37,885 cycles

DURING SCHEDULED 14Y CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 727D TO BS 727E. REMOVED AND REPLACED WEB PER SRM.

Part: LENS — LOOSE (CABIN) · airframe 45,986 hrs · 37,620 cycles

L1 DOOR EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: LENS — BROKEN (CABIN) · airframe 44,056 hrs · 36,168 cycles

L1 DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: SKIN — CRACKED (RT WING) · airframe 44,028 hrs · 36,144 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING L/E SKIN CRACKED AT STA 213. REPAIRED SKIN PER SWA EA.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 44,028 hrs · 36,144 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING I/B AFT FLAP DELAMINATED ON LOWER SURFACE. REMOVED AND REPLACED AFT FLAP PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 43,989 hrs · 36,115 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 867, STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 43,989 hrs · 86,115 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 867, STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: BATTERY — FAILED (CABIN) · airframe 43,989 hrs · 36,115 cycles

DURING SCHEDULED SPV CHECK, EEPLS FAILED OPERATIONAL CHECK. CHARGED BATTERIES PER MT.

Part: FUSE — BLOWN (CABIN) · airframe 43,989 hrs · 36,115 cycles

DURING SCHEDULED MV1 CHECK, FOUND RT AFT LOWER EMERGENCY EXIT LIGHT INOP. R&R EXIT LIGHT BATTERY FUSE PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 43,688 hrs · 35,899 cycles

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

Part: LENS — MISSING (CABIN) · airframe 43,073 hrs · 35,471 cycles

L1 DOOR EMERGENCY EXIT LIGHT LENS MISSING. REMOVED AND REPLACED LENS PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 42,351 hrs · 34,944 cycles

DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 42,351 hrs · 34,944 cycles

DURING SCHEDULED HC1 CHECK, FOUND L2 DOOR SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: MOUNT BRACKET — CRACKED (EVAC SLIDE) · airframe 42,351 hrs · 34,944 cycles

DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR SLIDE MOUNT BRACKET CRACKED. REMOVED AND REPLACED BRACKET PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 42,351 hrs · 34,944 cycles

DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: COVER — MISSING (CABIN) · airframe 42,337 hrs · 34,931 cycles

FOUND EEPLS LIGHT COVER MISSING AT FWD ENTRY DOOR. INSTALLED COVER PER MM.

Part: SIGN — BROKEN (CABIN) · airframe 41,090 hrs · 33,995 cycles

DURING SCHEDULED MV2 CHECK, FOUND FWD CABIN EMEMRGECY EXIT SIGN BROKEN. R&R EXIT SIGN PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 40,586 hrs · 33,630 cycles

DURING SCHEDULED 12Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: LENS — CRACKED (CABIN) · airframe 40,586 hrs · 33,630 cycles

DURING SCHEDULED 12Y CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LENS PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 40,586 hrs · 33,630 cycles

DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, RBL 7 TO RBL 14. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 40,586 hrs · 33,630 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 767, LBL 4 TO LBL 14, WL 152. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 40,586 hrs · 33,630 cycles

DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CRACKED AT BS 727E, LBL 7 TO LBL 12. REPAIRED SHEAR TIE PER SRM.

Part: SKIN — DELAMINATED (L/E SLAT) · airframe 40,586 hrs · 33,630 cycles

DURING SCHEDULED 12Y CHECK, FOUND LEFT WING NR 2 L/E SLAT INBOARD UPPER SURFACE DELAMINATED. REPAIRED SLAT PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 40,586 hrs · 33,630 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 807, BL 0 AND LBL 10. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,586 hrs · 33,630 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727E, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,586 hrs · 33,630 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,586 hrs · 33,630 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8L. REPAIRED FRAME PER SWA EA.

Part: SKIN — WORN (FUSELAGE) · airframe 40,586 hrs · 33,630 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE SKIN WORN AT BS 881 TO BS 907, BETWEEN STR 2L AND STR 2R. REPAIRED SKIN PER SRM.

Part: PRESSURE PANEL — CRACKED (NLG W/W) · airframe 40,586 hrs · 33,630 cycles

DURING SCHEDULED 12Y CHECK, FOUND NLG W/W CEILING PANEL WEB CUTOUT CRACKED AT BS 252, RBL 8. REPAIRED WEB PER ACO.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 40,586 hrs · 33,630 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 947, STR 27R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,586 hrs · 33,630 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,586 hrs · 33,630 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 767, RBL 16. REPAIRED FRAME PER SRM.

Part: SLAT — DELAMINATED (RT WING) · airframe 40,586 hrs · 33,630 cycles

DURING SCHEDULED 12Y CHECK, FOUND RIGHT WING NR 4 L/E SLAT DELAMINATED AT OUTBOARD CORNER. REPAIRED SLAT PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 40,586 hrs · 33,630 cycles

DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 787, RBL 7 TO RBL 15, WL 152. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,586 hrs · 33,630 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,586 hrs · 33,630 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,586 hrs · 33,630 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,586 hrs · 33,630 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,856 hrs · 33,630 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,856 hrs · 33,630 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 40,586 hrs · 33,630 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 40,586 hrs · 33,630 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 787, RBL 16, WL 152. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,856 hrs · 33,630 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,586 hrs · 33,630 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,586 hrs · 33,630 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,856 hrs · 33,630 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,856 hrs · 33,630 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA.

Part: BEARING — CORRODED (ELEVATOR TAB) · airframe 40,856 hrs · 33,630 cycles

DURING SCHEDULED 12Y CHECK, FOUND RIGHT ELEVATOR TAB NR 1 HINGE BEARING CORRODED. REMOVED AND REPLACED BEARING PER BOEING DRAWING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,586 hrs · 33,630 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,856 hrs · 33,630 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,586 hrs · 33,630 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,856 hrs · 33,630 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,856 hrs · 33,630 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,586 hrs · 33,630 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,586 hrs · 33,630 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER SWA EA.

Part: LENS — OUT OF POSITION (CABIN) · airframe 39,998 hrs · 33,212 cycles

L1 DOOR EMERGENCY EXIT LIGHT LENS FELL OFF. INSTALLED LENS PER MM.

Part: LENS — OUT OF POSITION (CABIN) · airframe 39,987 hrs · 33,202 cycles

L1 DOOR EMERGENCY EXIT LIGHT LENS FELL OUT. INSTALLED LENS PER MM.

Part: GLOWSTRIP — WORN (CABIN) · airframe 39,102 hrs · 32,528 cycles

DURING SCHEDULED HC1 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 1 DEF. REMOVED AND REPLACED STRIP PER MM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 38,716 hrs · 32,224 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD CARGO DOOR CUTOUT FWD FRAME CRACKED AT NR 2 DOOR STOP. REMOVED AND REPLACED FRAME PER ACO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 37,443 hrs · 31,238 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER AFT CORNER. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 37,443 hrs · 31,238 cycles

DURING SCHEDULED HC2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 37,443 hrs · 31,238 cycles

DURING SCHEDULED HC2 CHECK, FOUND LEFT WING INBOARD FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.

Part: GLOWSTRIP — MISSING (CABIN) · airframe 37,202 hrs · 31,048 cycles

EEPLS PHOTOLUMIESCENT STRIP MISSING AT ROW 15 ABC. INSTALLED STRIP PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 35,372 hrs · 29,625 cycles

DURING SCHEDULED MV2 CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT L1 DOOR. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LENS — OUT OF POSITION (CABIN) · airframe 35,305 hrs · 29,374 cycles

FOUND L1 DOOR EMERGENCY EXIT LIGHT LENS FELL OFF. INSTALLED LIGHT LENS PER MM.

Part: COVER — OUT OF POSITION (CABIN) · airframe 35,255 hrs · 29,529 cycles

EMERGENCY EXIT LIGHT COVER FELL OFF AT L1 DOOR. INSTALLED LIGHT COVER PER MM.

Part: HINGE — CRACKED (PAX DOORWAY) · airframe 33,989 hrs · 28,513 cycles

DURING SCHEDULED 10Y CHECK, FOUND FWD ENTRY DOOR CUTOUT, LOWER HINGE FITTING CRACKED AT FWD TOP CORNER. REMOVED AND REPLACED FWD ENTRY DOOR LOWER HINGE FITTING PER EA AND SRM.

Part: LIGHT — WORN (CABIN) · airframe 33,989 hrs · 28,513 cycles

DURING SCHEDULED 10Y CHECK, FOUND EEPLS STRIPS WORN AT BS 270 TO BS 947. REMOVED AND REPLACED EEPLS STRIPS PER MM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 33,989 hrs · 28,513 cycles

DURING SCHEDULED 10Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 2R. REPAIRED STRINGER SPLICE PER SRM.

Part: SIGN — CRACKED (CABIN) · airframe 33,989 hrs · 28,513 cycles

DURING SCHEDULED 10Y CHECK, FOUND R2 DOOR EMERGENCY EXIT SIGN CRACKED. REMOVED AND REPLACED EMERGENCY EXIT SIGN PER MM.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 33,989 hrs · 28,513 cycles

DURING SCHEDULED 10Y CHECK, FOUND FLOORBEAM SUPPORT CRACKED AT BS 380 TO BS 400, BL 0. REMOVED AND REPLACED FLOORBEAM SUPPORT PER EA.

Part: TAB — DELAMINATED (LT ELEVATOR) · airframe 33,989 hrs · 28,513 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT ELEVATOR TAB DELAMINATED AT HINGE CUTOUTS. REPAIRED LT ELEVATOR TAB PER SRM.

Part: TAB — CRACKED (LT ELEVATOR) · airframe 33,989 hrs · 28,513 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT ELEVATOR TRIM TAB INBOARD END CRACKED. REPAIRED LT TRIM TAB PER SRM.

Part: HOOK — LOOSE (R1 DOOR) · airframe 33,989 hrs · 28,513 cycles

DURING SCHEDULED 10Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR HOOK LOOSE. SECURED R1 DOOR FWD GIRT BAR HOOK PER MM.

Part: HOOK — LOOSE (R1 DOOR) · airframe 33,989 hrs · 28,513 cycles

DURING SCHEDULED 10Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR RETAINING HOOK LOOSE. SECURED HOOK PER SRM.

Part: HOOK — LOOSE (L1 DOOR) · airframe 33,989 hrs · 28,513 cycles

DURING SCHEDULED 10Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR RETAINING HOOKS LOOSE. SECURED HOOKS PER SRM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 33,639 hrs · 28,248 cycles

L1 DOOR UPPER EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: COVER — BROKEN (EMER EXIT SIGN) · airframe 33,508 hrs · 28,146 cycles

R1 DOOR LOWER EXIT SIGN ATTACH POINT BROKEN. REMOVED AND REPLACED SIGN COVER PER MM.

Part: LIGHT — CRACKED (CABIN) · airframe 33,471 hrs · 28,110 cycles

DURING SCHEDULED A1 CHECK, FOUND EEPLS STRIP CRACKED BETWEEN ROWS 6 TO 10 ABC. REMOVED AND REPLACED STRIP PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 32,118 hrs · 27,030 cycles

DURING SCHEDULED C4 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: HOOK — LOOSE (L2 DOOR GIRT BAR) · airframe 32,118 hrs · 27,030 cycles

DURING SCHEDULED C4 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK LOOSE. SECURED HOOK PER MM.

Part: MEC — FAULTY (NR 2 ENGINE) · airframe 31,588 hrs · 26,602 cycles

INFLIGHT SHUTDOWN & DECLARED EMERGENCY. AT 31,000 FT NR 2 ENGINE FLAMEOUT WHEN THRUST LEVER PLACED IN IDLE. RESTARTED NR 2 ENGINE, ALL SYSTEMS NORMAL, EXCEPT NR 2 ENGINE EGT 100 DEGREES HIGHER THAN NR 1 ENGINE EGT AFTER RESTART. REMOVED AND REPLACED NR 2 ENGINE FUEL PUMP & MEC, FUEL FILTER & SPAR VALVE ACTUATOR PER MM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 31,285 hrs · 26,366 cycles

EMERGENCY EXIT LIGHT LENS FELL OFF NEXT TO L1 DOOR. SECURED LENS PER MM.

Part: BUSHING — WORN (RT ELEVATOR TAB) · airframe 31,273 hrs · 26,357 cycles

DURING SCHEDULED C3 CHECK, RT ELEVATOR TAB FAILED THE FREE PLAY CHECK. REMOVED AND REPLACED NR 1 HINGE BUSHING & HARDWARE PER MM.

Part: COVER — OUT OF POSITION (CABIN) · airframe 31,048 hrs · 26,176 cycles

DURING SCHEDULED RON CHECK, FWD ENTRY EMERGENCY LIGHT COVER FELL OFF. INSTALLED COVER PER MM.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 31,013 hrs · 26,144 cycles

DURING SCHEDULED SERVICE CHECK, FOUND L1 DOOR LOWER EMERGENCY EXIT LIGHT COVER MISSING. INSTALLED COVER PER MM.

Part: LENS — DISLODGED (EMERGENCY LIGHT) · airframe 30,887 hrs · 26,038 cycles

L1 DOOR EMERGENCY EXIT LIGHT LENS FELL OFF. INSTALLED LENS PER MM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 30,644 hrs · 25,850 cycles

L1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 30,429 hrs · 25,678 cycles

L1 DOOR EMERGENCY EXIT LENS BROKEN. REMOVED AND REPLACED L1 DOOR EMERGENCY EXIT LENS PER MM.

Part: COVER — WORN (EMERGENCY LIGHT) · airframe 30,418 hrs · 25,668 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD END OF EEPLS COVER WORN. REMOVED AND REPLACED EEPLS COVER PER MM.

Part: SKIN — DELAMINATED (LT WING FLAP) · airframe 29,417 hrs · 24,923 cycles

DURING SCHEDULED C1 CHECK, FOUND LEFT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED LEFT T/E FLAP PER MM.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 28,821 hrs · 24,447 cycles

FWD ENTRY DOOR EMERGENCY EXIT LIGHT LENS, BROKEN. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM.

Part: SKIN — DELAMINATED (RT WING SLAT) · airframe 28,541 hrs · 24,223 cycles

DURING SCHEDULED C4 CHECK, FOUND RIGHT WING NR 5 L/E SLAT WEDGE, DELAMINATED. REMOVED AND REPLACED NR 5 L/E SLAT WEDGE PER MM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 28,497 hrs · 24,181 cycles

L1 DOOR EVAC SLIDE FELL OUT, DID NOT DEPLOY. REINSTALLED L1 DOOR EVAC SLIDE PER MM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 28,485 hrs · 24,174 cycles

L1 DOOR EVAC SLIDE FELL OUT, DID NOT DEPLOY. REINSTALLED L1 DOOR EVAC SLIDE PER MM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 28,160 hrs · 23,904 cycles

DURING SCHEDULED A2 CHECK, FOUND EMERGENCY EXIT LIGHT LENS AT L2 DOOR LOOSE. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 25,598 hrs · 21,782 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD GALLEY OVERHEAD EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 25,056 hrs · 21,353 cycles

FWD SVC DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF CONTAINER. REMOVED AND REPLACED SLIDE PER MM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 24,673 hrs · 21,038 cycles

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

Part: SLIDE — OUT OF ADJUST (FWD ENTRY DOOR) · airframe 23,733 hrs · 20,300 cycles

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

Part: TRUNNION PIN — CORRODED (RT MLG) · airframe 23,733 hrs · 20,300 cycles

DURING SCHEDULED C3 CHECK, FOUND RT MLG TRUNNION PIN CORRODED. REMOVED AND REPLACED RT MLG TRUNNION PIN PER MM.

Part: SLIDE — OUT OF ADJUST (AFT SVC DOOR) · airframe 23,733 hrs · 20,300 cycles

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

Part: FLAP — DELAMINATED (LT WING) · airframe 22,859 hrs · 19,627 cycles

DURING SCHEDULED C2 CHECK, FOUND LT T/E OTBD AFT FLAP DELAMINATED. REMOVED AND REPLACED LEFT T/E OTBD AFT FLAP PER MM.

Part: SLIDE — OUT OF ADJUST (AFT ENTRY DOOR) · airframe 22,803 hrs · 19,580 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 22,803 hrs · 19,580 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS LOOSE IN AFT CABIN. SECURED EEPLS PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 21,915 hrs · 18,882 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS LOOSE AT ROW 9. SECURED EEPLS PER MM.

Part: SLIDE — LOOSE (FWD ENTRY DOOR) · airframe 21,778 hrs · 18,759 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE FALLING OUT OF CONTAINER. SECURED SLIDE PER MM.

Part: SLIDE — FRAYED (AFT ENTRY DOOR) · airframe 21,064 hrs · 18,187 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR STRAP FRAYED. REPAIRED SLIDE PER MM.

Part: WINDOW — CRACKED (COCKPIT) · airframe 20,165 hrs · 17,464 cycles

DECLARED EMERGENCY, DIVERSION, L2 COCKPIT WINDOW CRACKED IN FLIGHT. REMOVED AND REPLACED WINDOW PER MM.

Part: LIGHT — INOPERATIVE (ENTRY DOOR) · airframe 20,155 hrs · 17,459 cycles

DURING SCHEDULED CHECK, FOUND FWD ENTRY DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EXIT LIGHT PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 19,292 hrs · 16,796 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM.

Part: LENS — LOOSE (CABIN) · airframe 19,203 hrs · 16,725 cycles

FWD ENTRY DOOR EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 18,429 hrs · 16,100 cycles

DURING SCHEDULED RON, FOUND FWD RT EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EXIT LIGHT BATTERY PACK PER MM.

Part: LIGHT — BROKEN (ENTRY DOOR) · airframe 17,550 hrs · 15,366 cycles

FWD ENTRY DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY PER MM.

Part: DOOR FRAME — CRACKED (SERVICE DOOR) · airframe 17,462 hrs · 15,287 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FWD SVC DOOR FWD FRAME CRACKED AT CUTOUT FOR NR 3 STOP. REPAIRED FRAME PER SWA TR.

Part: BEARING — WORN (AILERON TAB) · airframe 17,462 hrs · 15,284 cycles

DURING SCHEDULED 1/2D CHECK, FOUND PLAY AT LH WING AILERON TAB, OTBD HINGE BRACKET. R&R BEARING PER MM.

Part: COVER — MISSING (CABIN) · airframe 17,371 hrs · 15,210 cycles

EEPLS TRACK COVER MISSING AT ROW 2. REPLACED TRACK COVER PER MM.

Part: WIRE — EXPOSED (CABIN) · airframe 17,350 hrs · 15,193 cycles

EEPLS WIRING EXPOSED AT ROW 14. SECURED EEPLS WIRING PER MM.

Part: BUSHING — WORN (AILERON TAB) · airframe 17,313 hrs · 15,158 cycles

DURING SCHEDULED C4 CHECK, FOUND RT WING AILERON TAB BUSHINGS WORN AT THREE HINGES. R&R AILERON TAB PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,035 hrs · 14,940 cycles

DURING SCHEDULED A2 CHECK, FOUND NUMEROUS EEPLS BULBS INOP. RELAMPED EEPLS PER MM.

Part: COVER — MISSING (CABIN) · airframe 16,825 hrs · 14,761 cycles

EEPLS WIRING EXPOSED. REPLACED MISSING TRACK COVER PER MM.

Part: COVER — MISSING (CABIN FLOOR) · airframe 16,312 hrs · 14,347 cycles

EEPLS TRACK COVER MISSING. REPLACED TRACK COVER PER MM.

Part: SLIDE — OUT OF ADJ (SERVICE DOOR) · airframe 16,273 hrs · 14,317 cycles

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

Part: CONNECTOR — INOPERATIVE (CABIN) · airframe 15,896 hrs · 14,007 cycles

EMERGENCY NOT ARMED LIGHT INOP, LIGHT WOULD NOT EXTINGUISH. RE-SEATED CANNON PLUG ON DIMMING MODULE PER MM.

Part: COVER — MISSING (CABIN) · airframe 14,720 hrs · 13,283 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS LENS MISSING AT ROW 6. INSTALLED LENS COVER PER MM.

Part: SKIN — DELAMINATED (TE FLAP)

DURING SCHEDULED C3 CHECK, FOUND RT WING INBOARD AFT FLAP DELAMINATED ON OUTBOARD LOWER CORNER. REPAIRED FLAP PER SWA RA NR 1-357-0785.

Part: SKIN — DELAMINATED (TE FLAP)

DURING SCHEDULED C3 CHECK, FOUND LT WING INBOARD AFT FLAP DELAMINATED ON OUTBOARD UPPER AND LOWER END. REMOVED AND REPLACED FLAP ASSY PER MM.

Part: INDICATOR — MOVED (ESCAPE SLIDE)

DURING SCHEDULED C3 CHECK, FOUND AFT SERVICE DOOR EVACUATION SLIDE PRESSURE INDICATOR OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM.

Part: SLIDE — LOOSE (PAX DOOR)

AFT ENTRY DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. INSTALLED SLIDE ASSY PER MM.

Part: WIRE — LOOSE (ROW 15)

EMERGENCY ESCAPE FLOOR TRACK LIGHT INOP AT ROW 15. RESECURED WIRES AT TRACK LIGHTING PER MM.

Part: SKIN — PUNCTURED (LT TE FOREFLAP)

DURING SCHEDULED A1 CHECK, FOUND LEFT I/B FOREFLAP HAS .75 INCH PUNCTURE AT BOTTOM SIDE, 36 INCHES FROM I/B END. REPAIRED PER SWA RA NR 1-357-0655 AND SRM.

Part: SLIDE — DEPLOYED (ENTRY DOOR)

AT GATE, FWD ENTRY DOOR ESCAPE SLIDE ACCIDENTALLY DEPLOYED. REPLACED SLIDE ASSEMBLY PER BOEING M/M.