N628SW

Part: SKIN — CRACKED (TE FLAP) · airframe 65,424 hrs · 51,650 cycles

LT WING INBOARD FORE FLAP SKIN CRACKED UNDER CENTER MOUNT PAD FOR THE FORE FLAP TRACK. R&R FORE FLAP IAW MM.

Part: SENSOR — FAULTY (NR 2 ENGINE) · airframe 65,112 hrs · 51,424 cycles

NR 2 BLEED LIGHT ILLUMINATED, LEFT DUCT PRESSURE LOW AT FL 360. QRH; THE ALTITUDE WARNING SOUNDED. DECLARED AN EMERGENCY, EMERGENCY DESCENT TO 10,000' THEN SMOKE AND FUMES IN COCKPIT. EMERGENCY MASK IN CABIN DEPLOYED. R & R THE NR 2 ENGINE 450 DEGREE SENSOR IAW AMM.

Part: LIGHT — DISCOLORED (CABIN) · airframe 64,666 hrs · 51,140 cycles

EMERGENCY LIGHT DISCOLORED AT NR 3 GALLEY. R & R THE LIGHT IAW AMM.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 64,666 hrs · 51,140 cycles

LEFT WING TRAILING EDGE UPPER SHELF PANEL SUPPORT ANGLE CRACKED. R & R THE SUPPORT ANGLE IAW SRM.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 64,399 hrs · 50,969 cycles

FORWARD INBOARD EMERGENCY FLASHLIGHT INOPERATIVE. R & R BATTERY IAW MM.

Part: RETAINING CLIP — LOOSE (R1 DOOR) · airframe 63,672 hrs · 50,481 cycles

R1 DOOR AFT GIRT BAR STORAGE CLIP LOOSE. SECURED CLIP IAW SIP.

Part: RETAINING CLIP — BROKEN (CABIN) · airframe 62,934 hrs · 49,999 cycles

RIGHT OVERWING EMER EXIT SIGN LENS RETAINING CLIP BROKEN. R & R LENS ASSEMBLY IAW AMM.

Part: SKIN — DELAMINATED (LT SPOILER) · airframe 62,853 hrs · 49,948 cycles

LEFT WING NR 0 SPOILER BOARD DELAMINATED, AT TE UPPER SURFACE. R & R NR 0 SPOILER IAW MM.

Part: LENS — LOOSE (EXIT SIGN) · airframe 62,853 hrs · 49,948 cycles

RIGHT MID CABIN EMER EXIT SIGN LENS LOOSE. R & R LENS IAW AMM.

Part: SPOILER — OUT OF ADJUST (RT WING) · airframe 62,501 hrs · 49,711 cycles

RIGHT WING GND SPOILER OUT OF ADJUSTMENT. R & R SPOILER IAW AMM.

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 62,160 hrs · 49,473 cycles

AFT CARGO COMPARTMENT, DOOR CRACKED ON AFT LOWER CORNER FRAME. R & R DOOR ASSEMBLY IAW AMM.

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 62,160 hrs · 49,473 cycles

AFT CARGO COMPARTMENT, DOOR CRACKED ON FWD LOWER CORNER FRAME. R & R DOOR ASSEMBLY IAW AMM.

Part: SLIDE — UNSECURE (L1 DOOR) · airframe 62,160 hrs · 49,473 cycles

L1 DOOR EMER EVAC SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY, STILL OPERATIONAL. RE-INSTALLED SLIDE IAW MT.

Part: PLATE — CRACKED (FUSELAGE) · airframe 62,160 hrs · 49,473 cycles

LEFT SIDE WING TO BODY FAIRING PLATE CRACKED AT BS 727, AT LOWER FUSELAGE. R & R PLATE IAW SRM.

Part: FITTING — CRACKED (RT SPOILER) · airframe 62,160 hrs · 49,473 cycles

RIGHT WING NR 5 INBD GND SPOILER FITTING CRACKED. R & R FITTING IAW SRM & DWG.

Part: FLAP — DELAMINATED (RT WING) · airframe 62,160 hrs · 49,473 cycles

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

Part: SKIN — DELAMINATED (TE FLAP) · airframe 62,160 hrs · 49,473 cycles

RIGHT WING OTBD FORE FLAP DELAMINATED AT UPPER SURFACE. REPAIRED FORE FLAP IAW SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 62,160 hrs · 49,473 cycles

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

Part: ANGLE — CRACKED (LT WING) · airframe 62,160 hrs · 49,473 cycles

LEFT WING ANGLE, CRACKED AT INBD FLAP, OTBD TRACK FAIRING. R & R ANGLE IAW SRM & DWG.

Part: ANGLE — CRACKED (RT WING) · airframe 62,160 hrs · 49,473 cycles

RIGHT WING INBD FLAP OTBD TRACK FAIRING ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.

Part: BRACKET — CRACKED (LT WING) · airframe 62,160 hrs · 49,473 cycles

LEFT WING BRACKET CRACKED ON OF INBD FLAP, OTBD TRACK FAIRING INTERNAL AREA. R & R BRACKET IAW SRM & DWG.

Part: SCUFF PLATE — CRACKED (L2 DOOR) · airframe 62,160 hrs · 49,473 cycles

L2 DOOR CTR SCUFF PLATE CRACKED. REPAIRED SCUFF PLATE IAW EA.

Part: FLAP TRACK — CORRODED (TE FLAP) · airframe 62,160 hrs · 49,473 cycles

LEFT WING NR 4 FLAP TRACK CORRODED ON 4 ON HOLE. REPAIRED FLAP TRACK IAW CMM.

Part: FLAP TRACK — CORRODED (TE FLAP) · airframe 62,160 hrs · 49,473 cycles

RIGHT WING NR 5 FLAP TRACK HOLE CORRODED. REPAIRED NR 5 FLAP TRACK IAW CMM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,160 hrs · 49,473 cycles

TIE CLIP CRACKED AT BS 400, STRINGER 21L. R & R TIE CLIP IAW SRM & DWG.

Part: LINK ASSY — CORRODED (RT MLG) · airframe 62,160 hrs · 49,473 cycles

RIGHT MLG SWING LINK ASSEMBLY CORRODED. REPAIRED LINK ASSEMBLY IAW EO & EA.

Part: LINK — CORRODED (LT MLG) · airframe 62,160 hrs · 49,473 cycles

LEFT MLG SWING ATTACH LINK ASSEMBLY ON INTERNAL HOLE CORRODED. REPAIRED LINK ASSEMBLY IAW EO & EA.

Part: FITTING — CRACKED (FUSELAGE) · airframe 62,160 hrs · 49,473 cycles

CLIP CRACKED AT BS 336, STRINGER 21L. R & R CLIP IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 62,160 hrs · 49,473 cycles

CLIP ANGLE CRACKED AT BS 328, STRINGER 21L. R & R ANGLE IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 62,160 hrs · 49,473 cycles

WEB INTERCOSTAL CRACKED, BETWEEN BS 312 - 324, BETWEEN STRINGER 28L - 28R. R & R WEB IAW SRM & DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 62,160 hrs · 49,473 cycles

LOWER NOSE COMPARTMENT INTERNAL STRUCTURE, ANGLE CLIP CRACKED AT BS 294.5, STRINGER 23L. R & R CLIP IAW DWG & SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 62,160 hrs · 49,473 cycles

WEB INTERCOSTAL CRACKED, BETWEEN BS 294.5 - 312, BETWEEN STRINGER 28L - 27R. R & R WEB IAW DWG.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 62,160 hrs · 49,473 cycles

WEB CRACKED AT BS 178, RBL 17. REPAIRED WEB IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,160 hrs · 49,473 cycles

FORWARD CARGO COMPARTMENT TIE CLIP, CRACKED AT BS 500D, STRINGER 19R. R & R TIE CLIP IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 62,160 hrs · 49,473 cycles

FORWARD CARGO COMPARTMENT ANGLE, CRACKED AT BS 380, STRINGER 26R. R & R ANGLE IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 62,160 hrs · 49,473 cycles

FORWARD CARGO COMPARTMENT, ANGLE CRACKED AT BS 400, STRINGER 26R. R & R ANGLE IAW SRM & DWG.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 62,160 hrs · 49,473 cycles

WEB CRACKED AT BS 178, RBL 17.0. REPAIRED WEB IAW SRM.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 62,160 hrs · 49,473 cycles

FORWARD CARGO COMPARTMENT CHANNEL CRACKED, BETWEEN BS 420 - 440, STRINGER 26R. R & R CHANNEL IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,160 hrs · 49,473 cycles

FRAME CRACKED AT BS 520, BETWEEN STRINGER 21L TO 22L. REPAIRED FRAME IAW EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 62,160 hrs · 49,473 cycles

WEB INTERCOSTAL CRACKED, BETWEEN BS 500B - 500C, STRINGER 26R. R & R INTERCOSTAL IAW SRM & DWG.

Part: SPAR — CRACKED (LT WING) · airframe 62,160 hrs · 49,473 cycles

LEFT WING REAR SPAR, UPPER CHORD UPPER FASTENER HOLE CRACKED AT RSS 223.14. REPAIRED CHORD IAW EA.

Part: SPAR — CRACKED (RT WING) · airframe 62,160 hrs · 49,473 cycles

RIGHT WING REAR SPAR WEB FASTENER HOLE CRACKED, BETWEEN RSS 215.97 TO 224.14. REPAIRED SPAR WEB IAW EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 62,160 hrs · 49,473 cycles

KEEL BEAM T ANGLE CRACKED AT BS 639. R & R T ANGLE IAW SRM & DWG.

Part: SUPPORT FITTING — CRACKED (RT WING) · airframe 62,160 hrs · 49,473 cycles

RIGHT WING REAR SPAR AT AFT SUPPORT FITTING CRACKED, BETWEEN RSS 215.97 TO 224.14. R & R FITTING IAW EA.

Part: SPAR — CRACKED (RT WING) · airframe 62,160 hrs · 49,473 cycles

RIGHT WING REAR SPAR, UPPER CHORD FASTENER HOLE CRACKED, BETWEEN RSS 215.97 TO 224.14. REPAIRED CHORD IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,160 hrs · 49,473 cycles

FUSELAGE SKIN CRACKED, BETWEEN BS 777 - 818, BETWEEN STRINGER 22R - 26R. REPAIRED SKIN IAW EO & EA.

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 62,160 hrs · 49,473 cycles

FORWARD CARGO AFT CORNER SCUFF PLATE, CRACKED AT LOWER FUSELAGE. REPAIRED SCUFF PLATE IAW EA.

Part: HINGE — CRACKED (FUSELAGE) · airframe 62,160 hrs · 49,473 cycles

KEEL BEAM PANEL, HINGE AT LOWER FUSELAGE CRACKED AT BS 663.75. R & R HINGE IAW SRM & DWG.

Part: SKIN — DELAMINATED (RT HORIZ STAB) · airframe 62,160 hrs · 49,473 cycles

RIGHT HORIZONTAL STABILIZER ELEVATOR UPPER SKIN DELAMINATED AT STATION 53.5. REPAIRED SKIN IAW SRM.

Part: SKIN — DELAMINATED (RT HORIZ STAB) · airframe 62,160 hrs · 49,473 cycles

RIGHT HORIZONTAL STABILIZER ELEVATOR UPPER SKIN DELAMINATED AT STATION 102. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (RT WING) · airframe 62,160 hrs · 49,473 cycles

RIGHT WING FIXED LE SKIN AT KRUEGER FLAP, SEAL DOOR CUT OUT CRACKED AT BS 208. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 62,160 hrs · 49,473 cycles

LEFT WING FIXED LE SKIN CRACKED AT KRUEGER FLAP SEAL DOOR CUT OUT AT BS 208. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,160 hrs · 49,473 cycles

SKIN CRACKED AT BS 326.5, STRINGER 17R. REPAIRED SKIN IAW EA & SRM.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 62,160 hrs · 49,473 cycles

PRESSURE DECK WEB CRACKED, BETWEEN BS 664 - 675, RBL 40. REPAIRED WEB IAW SRM.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 62,160 hrs · 49,473 cycles

MAIN WW PRESS DECK CRACKED, BETWEEN BS 664 - 675, BETWEEN BL 0 - LBL 24.5. REPAIRED DECK IAW SRM & EA.

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 62,160 hrs · 49,473 cycles

FORWARD GALLEY AREA, EMER FLASHLIGHT SAFETY STRAP BROKEN. R & R STRAP IAW CMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,160 hrs · 49,473 cycles

SKIN CRACKED AT BS 520+7, STRINGER 28L. REPAIRED SKIN IAW EA.

Part: SKIN — DELAMINATED (FUSELAGE) · airframe 62,160 hrs · 49,473 cycles

TAIL CONE FUSELAGE EXTERNAL SKIN DELAMINATED AT BS 1156+10, LBL 8. REPAIRED SKIN IAW SRM.

Part: SKIN PANEL — DELAMINATED (FUSELAGE) · airframe 62,160 hrs · 49,473 cycles

KEEL BEAM EXTERNAL SKIN PANEL DELAMINATED AT BS 663.75, AT LOWER FUSELAGE. R & R PANEL IAW SRM.

Part: WEB — CRACKED (NLG WW) · airframe 62,160 hrs · 49,473 cycles

RIGHT NOSE WW WEB CRACKED AT BS 246.7, WL 169, AT 7 O CLOCK. REPAIRED WEB IAW SRM & EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 62,160 hrs · 49,473 cycles

SEAT TRACK CRACKED AT BS 727B, LBL 24.75. REPAIRED SEAT TRACK IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 62,160 hrs · 49,473 cycles

CENTER WING BOX LONGITUDINAL FLOORBEAM, WEB CRACKED AT BS 706, RBL 24.50. REPAIRED WEB IAW EA.

Part: HINGE — BROKEN (RT SPOILER) · airframe 61,420 hrs · 48,935 cycles

NUMBER 4 INBD SPOILER ACTUATOR HINGE BROKEN. R & R SPOILER IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,254 hrs · 48,826 cycles

L2 DOOR CUT OUT FWD LOWER CORNER SKIN CRACKED BETWEEN BS 967 - 951, STRINGER 17L. REPAIRED SKIN IAW SRM & EA.

Part: LENS — CRACKED (L1 DOOR) · airframe 60,487 hrs · 48,304 cycles

L1 DOOR SLIDE EMER EVAC SLIDE COVER LENS CRACKED. R & R LENS IAW AMM & MT.

Part: FILTER — DIRTY (AC BAY) · airframe 59,275 hrs · 47,462 cycles

FLIGHT ATTENDANT REPORTED SMELLING BURNED RUBBER SMELL DURING CRUISE. R & R RECIRCULATION FAN FILTER IAW MM.

Part: SPRING — BROKEN (CARGO DOOR) · airframe 59,613 hrs · 47,721 cycles

AFT CARGO DOOR HANDLE SPRING BROKEN. R & R SPRING IAW MM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 58,768 hrs · 47,097 cycles

FORWARD CABIN EMER FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT IAW AMM.

Part: LENS — MISSING (CABIN) · airframe 58,369 hrs · 46,802 cycles

RIGHT OVERWING EMER EXIT LIGHT LENS MISSING. INSTALLED LENS IAW MM.

Part: FITTING — CORRODED (FUSELAGE) · airframe 57,376 hrs · 46,132 cycles

FRAME FITTING CORRODED AT BS 1016, STRINGER 24R. R & R FITTING IAW SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,332 hrs · 46,104 cycles

RT EMERGENCY EXIT LIGHT INOPERATIVE AT ROW 20. R & R LIGHT IAW AMM.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 57,023 hrs · 45,899 cycles

RT WING PANEL 8714 SUPPORT ANGLE CRACKED AT OTBD SIDE OF NR 2 ENG FIXED TE. R & R ANGLE IAW SRM & DRAWING.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 57,023 hrs · 45,899 cycles

RT WING OTBD AFT FLAP INBD END DELAMINATED ON LOWER SURFACE & UPPER SURFACE. REPAIRED AFT FLAP IAW SRM.

Part: RIB — CRACKED (LT WING) · airframe 57,023 hrs · 45,899 cycles

LT WING RIB LOWER CHORD AT WBL 135.5 CRACKED. R & R CHORD IAW EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 57,023 hrs · 45,899 cycles

RT WING NR 6 SLAT SKIN CRACKED AT INBD AUXILIARY TRACK. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 57,023 hrs · 45,899 cycles

RT WING NR 5 SLAT SKIN CRACKED AT INBD AUXILIARY TRACK. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 57,023 hrs · 45,899 cycles

LT WING NR 2 SLAT SKIN CRACKED AT OTBD AUXILIARY TRACK. REPAIRED SKIN IAW SRM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 56,680 hrs · 45,667 cycles

AFT OVERHEAD DOOR EMERGENCY EXIT SIGNS INOPERATIVE. RELAMPED SIGN IAW AMM.

Part: SLIDE — LOW PRESSURE (L2 DOOR) · airframe 56,675 hrs · 45,666 cycles

L2 DOOR EMERGENCY EVAC SLIDE PRESSURE LOW. R & R SLIDE IAW SWA MT.

Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 56,675 hrs · 45,666 cycles

R1 DOOR EMERGENCY EVAC SLIDE PRESSURE LOW. R & R SLIDE IAW SWA MT.

Part: LENS — BROKEN (CABIN) · airframe 56,675 hrs · 45,666 cycles

R2 DOOR AFT GALLEY EMERGENCY LIGHT LENS BROKEN. R & R LENS IAW AMM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 56,675 hrs · 45,666 cycles

L1 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 56,675 hrs · 45,666 cycles

FWD LT FLASHLIGHT BATTERY INOPERATIVE. R & R BATTERY IAW MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,675 hrs · 45,666 cycles

STRINGER CLIP CRACKED AT BS 639, STRINGER 4L. R & R CLIP IAW SRM & DRAWING.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,675 hrs · 45,666 cycles

STRINGER CLIP CRACKED AT STATION 360, STRINGER 2L. R & R CLIP IAW SRM & DRAWING.

Part: FORGING — CRACKED (FUSELAGE) · airframe 56,675 hrs · 45,666 cycles

RT BS 887+10 WINDOW FORGING CRACKED AT HOLE NR 4. R & R FORGING IAW BAC DRAWING.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 56,675 hrs · 45,666 cycles

STRINGER SPLICE CRACKED AT STATION 908, STRINGER 4L. R & R CHANNEL IAW DRAWING & SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,675 hrs · 45,666 cycles

RT BS 827+10 LOWER FORWARD SKIN CUTOUT CRACKED AT HOLE NR 3. R &R SKIN IAW DRAWING.

Part: SKIN — CRACKED (LE SLAT) · airframe 56,675 hrs · 45,666 cycles

LT WING NR 1 SLAT LE SKIN CRACKED. REPAIRED SLAT IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,675 hrs · 45,666 cycles

RT FS SKIN CRACKED AT BS 867+ 10, LOWER FWD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SERVICE BULLETIN.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,675 hrs · 45,666 cycles

RT BS 807+10 LOWER FORWARD SKIN CUTOUT CRACKED AT HOLE NR 2. R & R SKIN IAW DRAWING.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,675 hrs · 45,666 cycles

RT FS SKIN CRACKED AT BS 867+ 10, UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SERVICE BULLETIN.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,675 hrs · 45,666 cycles

RT FS SKIN CRACKED AT BS 767+ 10, UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SERVICE BULLETIN.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,675 hrs · 45,666 cycles

RT BS 847+10 LOWER FWD WINDOW SKIN CUTOUT CRACKED AT HOLE NR 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,675 hrs · 45,666 cycles

RT BS 827+10 LOWER FWD WINDOW SKIN CUTOUT CRACKED AT HOLE NR 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,675 hrs · 45,666 cycles

RT FS SKIN CRACKED AT BS 787+ 10, UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SERVICE BULLETIN.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,675 hrs · 45,666 cycles

RT BS 887+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 2,3,4,7,8. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,675 hrs · 45,666 cycles

RT BS 807+10 UPPER AFT SKIN CUTOUT CRACKED AT HOLES 2,4. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,675 hrs · 45,666 cycles

LT BS 887+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 2,6. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,675 hrs · 45,666 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,675 hrs · 45,666 cycles

RT FS SKIN CRACKED AT BS 867+ 10, LOWER FWD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SERVICE BULLETIN.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,675 hrs · 45,666 cycles

LT BS 767 +10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLE NR 2. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,675 hrs · 45,666 cycles

LT BS 827 +10 LOWER FWD WINDOW SKIN CUTOUT CRACKED AT HOLE NR 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,675 hrs · 45,666 cycles

LT BS 787+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 2,3,5. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,675 hrs · 45,666 cycles

LT BS 887 +10 LOWER FORWARD SKIN CUTOUT CRACKED AT HOLE NR 2. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,675 hrs · 45,666 cycles

LT BS 807+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 2,4 & 5. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,675 hrs · 45,666 cycles

LT BS 767 +10 LOWER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLE NR 2. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,675 hrs · 45,666 cycles

LT BS 867+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 2,4. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,675 hrs · 45,666 cycles

RT BS 807+10 LOWER FWD WINDOW SKIN CUTOUT CRACKED AT HOLE NR 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,675 hrs · 45,666 cycles

RT BS 827+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLE NR 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,675 hrs · 45,666 cycles

RT BS 847+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLE NR 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,675 hrs · 45,666 cycles

LT BS 787 +10 LOWER FWD WINDOW SKIN CUTOUT CRACKED AT HOLE NR 2. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,675 hrs · 45,666 cycles

RT BS 767+10 LOWER FWD WINDOW SKIN CUTOUT CRACKED AT HOLE NR 3. REPAIRED SKIN IAW SB.

Part: COVER — LOOSE (EMERGENCY EXIT) · airframe 56,464 hrs · 45,497 cycles

LT EMERGENCY EXIT WINDOW COVER LOOSE. SECURED COVER IAW SIP.

Part: SIGN — UNSECURE (CABIN) · airframe 56,373 hrs · 45,431 cycles

RT OVERHEAD EMERGENCY EXIT SIGN FELL OFF. SECURED SIGN IAW SIP.

Part: LENS — LOOSE (CABIN) · airframe 56,341 hrs · 45,398 cycles

RT EMERGENCY EXIT LENS COVER LOOSE AT ROW 12. SECURED COVER IAW MM.

Part: SIGN — BROKEN (CABIN) · airframe 56,219 hrs · 45,305 cycles

R1 DOOR EXIT SIGN BROKEN. R&R SIGN IAW MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 56,010 hrs · 45,141 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW S.I.P.

Part: FAN — FAULTY (AC BAY) · airframe 55,939 hrs · 45,092 cycles

STRANGE ODOR IN MID CABIN. R&R RECIRC FAN IAW M/M.

Part: SIGN — BROKEN (CABIN) · airframe 55,910 hrs · 45,069 cycles

FWD ENTRY EMERGENCY EXIT SIGN BROKEN. R&R SIGN IAW M/M.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 55,571 hrs · 44,809 cycles

L1 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT DID NOT DEPLOY. SECURED SLIDE PER MT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,534 hrs · 44,782 cycles

SKIN CRACKED AT STA 1000, STR 5R. REPAIRED SKIN PER EA.

Part: LENS — MISSING (CABIN) · airframe 54,745 hrs · 44,218 cycles

FORWARD ENTRY EMERGENCY EXIT SIDE LIGHT LENS MISSING. INSPECTED THEN REPLACED MISSING LENS PER AMM, OPS CHECKS GOOD.

Part: ANGLE — CRACKED (NR 2 AILERON) · airframe 54,639 hrs · 44,147 cycles

ANGLE IS CRACKED I/B SIDE OF NR 2 AILERON HINGE RIGHT WING. REMOVED AND REPLACED PER SRM 51-40-02.

Part: CABLE — MISROUTED (R2 DOOR) · airframe 54,639 hrs · 44,147 cycles

AFT SERVICE DOOR ESCAPE SLIDE GIRT CABLE ROUTED WRONG. REROUTED CABLE IAW M/M.

Part: LENS — UNSECURE (CABIN) · airframe 54,630 hrs · 44,141 cycles

CEILING AISLE EXIT LIGHT COVER FELL OFF. RE-INSTALLED LENS. OPS CHECK OK PER M/M.

Part: SLIDE — LOW PRESSURE (R2 DOOR) · airframe 54,105 hrs · 43,760 cycles

AFT SERVICE DOOR SLIDE GAUGE IN RED BAND. REMOVED & REPLACED AFT SERVICE DOOR SLIDE PER MT.

Part: FUSE — BLOWN (CABIN) · airframe 53,635 hrs · 43,409 cycles

EMERGENCY EXIT SIDEWALL LIGHT INOP. REMOVED AND REPLACED FUSE IAW MM.

Part: LENS — CRACKED (CABIN) · airframe 52,731 hrs · 42,703 cycles

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

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,448 hrs · 41,748 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 727E, STR 23L. REMOVED AND REPLACED FRAME IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,448 hrs · 41,748 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 993.5, RBL 54. REPAIRED FRAME IAW EA AND ER.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 51,448 hrs · 41,748 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CORRODED AT BS 500C, STR 26R. REMOVED AND REPLACED STRINGER PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,448 hrs · 41,748 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 867, BETWEEN STR 27L TO STR 27R. REPAIRED SHEAR TIE IAW EA AND ER.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,448 hrs · 41,748 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT FRAME CORRODED AT BS 727B, BETWEEN STR 27L TO STR 27R. REPAIRED FRAME IAW ER.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,448 hrs · 41,748 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 907, BETWEEN STR 27L TO STR 27R. REPAIRED SHEAR TIE IAW ER AND EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,448 hrs · 41,748 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 520, BETWEEN STR 20R TO STR 21R. REPAIRED FRAME IAW ER.

Part: FLAP — DELAMINATED (RT WING) · airframe 51,448 hrs · 41,748 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT WING FORE FLAP DELAMINATED T/E CORNER. REPAIRED FORE FLAP PER MM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,448 hrs · 41,748 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 767, STR 23L. REMOVED AND REPLACED FRAME IAW EA AND ER.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,448 hrs · 41,748 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727D, RBL 4. REPAIRED SHEAR TIE IAW EA AND ER.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 51,448 hrs · 41,748 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT SIDEWALL SUPPORT CORRODED AT BS 887, STR 25L. REMOVED AND REPLACED SUPPORT PER SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,448 hrs · 41,748 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 887, BETWEEN STR 26L TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER ER AND EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,448 hrs · 41,748 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT SHEAR TIE CORRODED AT BS 847, BETWEEN STR 26L TO STR 27L. REPAIRED SHEAR TIE IAW ER.

Part: SIGN — BROKEN (CABIN) · airframe 51,448 hrs · 41,748 cycles

DURING SCHEDULED 16Y CHECK, FOUND FWD EMERGENCY EXIT LIGHT SIGN BROKEN. REMOVED AND REPLACED SIGN ASSY. PER SWPM.

Part: WEB — CRACKED (FUSELAGE) · airframe 51,448 hrs · 41,748 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT WEB CRACKED, BETWEEN BS 794 TO BS 847. REMOVED AND REPLACED WEB PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,448 hrs · 41,748 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT SHEAR TIE CORRODED AT BS 747, BETWEEN STR 26R TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 51,448 hrs · 41,748 cycles

DURING SCHEDULED 16Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED BETWEEN BS 666 TO BS 670, LBL 25. REPAIRED CHORD PER ER AND EA.

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 51,448 hrs · 41,748 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT SHEAR WEB CORRODED BETWEEN BS 927 TO BS 947, RBL 3. REPAIRED WEB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,448 hrs · 41,748 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 294, STR 7R. REPAIRED FRAME IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 51,448 hrs · 41,748 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 986.5, BETWEEN RBL 4 TO RBL 45. REPAIRED CHORD PER ER.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 51,448 hrs · 41,748 cycles

DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 380 TO BS 400, BETWEEN RBL 64 TO RBL 70. REPAIRED WEB IAW SRM AND DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 51,448 hrs · 41,748 cycles

DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 500A TO BS 500B, BETWEEN RBL 64 TO RBL 70. REPAIRED WEB IAW SRM AND DWG.

Part: PANEL — DELAMINATED (NR 7 SPOILER) · airframe 51,448 hrs · 41,748 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT WING NR 7 SPOILER PANEL DELAMINATED. REMOVED AND REPLACED SPOILER PANEL PER MM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 51,448 hrs · 41,748 cycles

DURING SCHEDULED 16Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REMOVED AND REPLACED SLIDE PER MT.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 51,448 hrs · 41,748 cycles

DURING SCHEDULED 16Y CHECK, FOUND FWD GALLEY DOOR SURROUNDED INNER CHORD CRACKED AT BS 332.1, STR 8R. REMOVED AND REPLACED CHORD IAW SRM AND DWG.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 51,448 hrs · 41,748 cycles

DURING SCHEDULED 16Y CHECK FOUND, SHEAR TIE CRACKED AT BS 967, STR 7L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,448 hrs · 41,748 cycles

DURING SCHEDULED 16Y CHECK FOUND, LT FRAME I/B CHORD CRACKED AT BS 348, WL 208.5. REMOVED AND REPLACED CHORD IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,448 hrs · 41,748 cycles

DURING SCHEDULED 16Y CHECK FOUND, AFT CARGO COMPARTMENT SHEAR TIE CORRODED AT BS 847, RBL 2. REPAIRED SHEAR TIE PER SRM AND ER.

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 51,448 hrs · 41,748 cycles

DURING SCHEDULED 16Y CHECK FOUND, SHEAR WEB CORRODED AT BS 1026, LBL 14. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,448 hrs · 41,748 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,448 hrs · 41,748 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,448 hrs · 41,748 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,448 hrs · 41,748 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 559, STR 11L. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 51,448 hrs · 41,748 cycles

DURING SCHEDULED 16Y CHECK, FOUND INTERIOR STRINGER CRACKED AT STA 380, STR 15L. REMOVED AND REPAIRED STRINGER PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 51,448 hrs · 41,748 cycles

DURING SCHEDULED 16Y CHECK, FOUND CORROSION ON CREASE BEAM WEB BS 500-500A, LBL 64 - 70, WL 208. REPAIRED PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,448 hrs · 41,748 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT STR CUTOUT BS 947.5, STR 19L. REMOVED AND REPLACED FRAME PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 51,448 hrs · 41,748 cycles

DURING SCHEDULED 16Y CHECK, FOUND CORROSION ON CREASE BEAM WEB BS 727A-727B, RBL 64-70, WL 208. REPAIRED BEAM PER SRM.

Part: RETAINER — WORN (GIRT BAR) · airframe 51,448 hrs · 41,748 cycles

DURING SCHEDULED 16Y CHECK, FOUND L1 DOOR ESCAPE SLIDE GIRT BARS RETAINERS WORN. REMOVED AND REPLACED WORN RETAINERS PER MM.

Part: SKIN — DAMAGED (SPOILER) · airframe 51,448 hrs · 41,748 cycles

DURING SCHEDULED 16Y CHECK, FOUND DENT NR 7 SPOILER DELAMINATED ON UPPER SURFACE. REMOVED AND REPLACED SPOILER PER MM.

Part: RETAINER — WORN (GIRT BAR) · airframe 51,448 hrs · 41,748 cycles

DURING SCHEDULED 16Y CHECK, FOUND R1 DOOR ESCAPE SLIDE GIRT BARS RETAINERS WORN. REMOVED AND REPLACED WORN RETAINERS PER MM.

Part: STRINGER CLIP — DAMAGED (FUSELAGE) · airframe 51,448 hrs · 41,748 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP DAMAGED AT BS 500B+12, STR 27R. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,448 hrs · 41,748 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 807, BETWEEN STR 26L TO STR 27L. REMOVED AND REPLACED SHEAR TIE IAW SRM.

Part: FAN — FAULTY (AC BAY) · airframe 50,189 hrs · 40,789 cycles

FLIGHT ATTENDANTS SMELLED ELECTRICAL SMOKE. FOUND RECIRCULATION FAN INOP. REMOVED AND REPLACED FAN PER MM.

Part: COVER — MISSING (CABIN) · airframe 49,555 hrs · 40,320 cycles

DURING SCHEDULED SPV CHECK FOUND, L1 DOOR THRESHOLD FORWARD EMERGENCY LIGHT LENS COVER MISSING. INSTALLED COVER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,332 hrs · 40,149 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 432, STR 4L. REPAIRED SKIN PER EA AND ATS ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,670 hrs · 39,666 cycles

DURING SCHEDULED SPV CHECK, FOUND RT FRAME CRACKED AT BS 492, AT NR 5 STOP FITTING. REMOVED AND REPLACED FRAME PER ACO.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 48,670 hrs · 39,666 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 500, BETWEEN STR 26R TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: COVER — BROKEN (CABIN) · airframe 48,082 hrs · 39,227 cycles

OVERHEAD EMERGENCY EXIT LIGHT COVER BROKEN AT ROW 2. REMOVED AND REPLACED COVER PER MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 47,426 hrs · 38,690 cycles

DURING SCHEDULED MV1 CHECK, FOUND RT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 46,952 hrs · 38,309 cycles

L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 46,306 hrs · 37,816 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CRACKED AT BS 380, STR 8R. REMOVED AND REPLACED STRINGER PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 46,306 hrs · 37,816 cycles

DURING SCHEDULED 14Y CHECK, FOUND FWD CABIN FLOORBEAM CORRODED AT BS 328, BBL 0. REMOVED AND REPLACED T-CAP PER SRM.

Part: LIGHT — DAMAGED (CABIN) · airframe 46,306 hrs · 37,816 cycles

DURING SCHEDULED 14Y CHECK, FOUND EEPLS DAMAGED. REMOVED AND REPLACED EEPLS PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,306 hrs · 37,816 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 11L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,306 hrs · 37,816 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 5R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,306 hrs · 37,816 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 5R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,306 hrs · 37,816 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 6R. REMOVED AND REPLACED CLIP PER SRM.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 46,306 hrs · 37,816 cycles

DURING SCHEDULED 14Y CHECK, FOUND LT WHEEL WELL OVERHEAD BULKHEAD PRESSURE DECK WEB CRACKED AT BS 665, LBL 31. REMOVED AND REPLACED WEB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,306 hrs · 37,816 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: COVER — BROKEN (CABIN) · airframe 46,099 hrs · 37,677 cycles

R1 DOOR EMERGENCY EXIT LIGHT COVER BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 45,990 hrs · 37,599 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: LENS — CRACKED (CABIN) · airframe 42,250 hrs · 37,085 cycles

DURING SCHEDULED CV CHECK, FOUND EXIT LIGHT LENS CRACKED ABOVE L1 DOOR. REMOVED AND REPLACED LIGHT ASSY PER SI.

Part: SKIN — CRACKED (FUSELAGE) · airframe 44,584 hrs · 36,601 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 44,581 hrs · 36,600 cycles

DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER ER.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 44,584 hrs · 36,601 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 44,581 hrs · 36,600 cycles

DURING SCHEDULED HC2 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 20. RELAMPED PER MM.

Part: SUPPORT ANGLE — CRACKED (RT MLG WW) · airframe 44,581 hrs · 36,600 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT MLG WHEEL WELL AFT LOWER BULKHEAD SUPPORT ANGLE CRACKED. REMOVED AND REPLACED ANGLE PER SRM.

Part: SPOILER — DELAMINATED (RT WING) · airframe 44,581 hrs · 36,600 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING NR 5 GROUND SPOILER DELAMINATED. REMOVED AND REPLACED SPOILER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 44,581 hrs · 36,600 cycles

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

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 44,581 hrs · 36,600 cycles

DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: SUPPORT FITTING — CRACKED (R1 DOOR) · airframe 44,581 hrs · 36,600 cycles

DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR LOWER AFT INNER STRUCTURE SUPPORT FITTING CRACKED. REMOVED AND REPLACED FITTING PER SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 44,581 hrs · 36,600 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING O/B TRAILING EDGE FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM.

Part: SLIDE — UNSERVICEABLE (R2 DOOR) · airframe 43,716 hrs · 35,979 cycles

DURING SCHEDULED MV4 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATOR OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MT.

Part: WIRE — DAMAGED (LT MLG) · airframe 42,911 hrs · 35,414 cycles

AIR TURNBACK, LANDING GEAR RETRACTION LT MAIN SHOWED UNSAFE. CYCLED GEAR WITH SAME INDICATION. REPAIRED UPLOCK SENSOR WIRE PER MM.

Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 42,902 hrs · 35,406 cycles

DURING SCHEDULED HC1 CHECK, FOUND RT KEEL BEAM CRACKED BETWEEN ACCESS PANELS NR 1506L TO PANEL NR1507L. REPAIRED BEAM PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 40,209 hrs · 33,404 cycles

DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500D, STR 27L TO STR 28L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 40,208 hrs · 33,402 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 807, STR 26R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 40,208 hrs · 33,402 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 767, STR 26R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 40,208 hrs · 33,402 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 907, STR 26R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 40,208 hrs · 33,402 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 807, STR 26L TO BS 27R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 40,208 hrs · 33,402 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 807, STR 26R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 40,208 hrs · 33,402 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 727E, STR 27L TO 27R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 40,208 hrs · 33,402 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 787, STR 26R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 40,208 hrs · 33,402 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 747, STR 26R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 40,208 hrs · 33,402 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 500C, STR 28L. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 40,208 hrs · 33,402 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 27R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 40,208 hrs · 33,402 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 29L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 40,208 hrs · 33,402 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 500D, STR 26R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 40,208 hrs · 33,402 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 867, STR 25R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,208 hrs · 33,402 cycles

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

Part: FRAME — CORRODED (FUSELAGE) · airframe 40,208 hrs · 33,402 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 500B, STR 28R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,208 hrs · 33,402 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,208 hrs · 33,402 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,208 hrs · 33,402 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,208 hrs · 33,452 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,208 hrs · 33,402 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,208 hrs · 33,402 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,208 hrs · 33,402 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,208 hrs · 33,402 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,054 hrs · 32,543 cycles

DURING SCHEDULED MV1 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT) · airframe 39,043 hrs · 32,535 cycles

DURING SCHEDULED MV1 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 38,405 hrs · 32,037 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 37,990 hrs · 31,678 cycles

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

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 37,861 hrs · 31,559 cycles

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

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 36,292 hrs · 30,360 cycles

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

Part: FRAME — CRACKED (BS 616) · airframe 33,883 hrs · 28,479 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, RBL 64, WL 201. REPAIRED FRAME SECTION PER ER.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 33,883 hrs · 28,479 cycles

DURING SCHEDULED 10Y CHECK, FOUND COCKPIT FLOORBEAM UPPER CHORD CORRODED AT BS 259.5, BETWEEN LBL 11 TO RBL 11, WL 208. REPAIRED FLOORBEAM PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 33,883 hrs · 28,479 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 440, STR 26R. REPAIRED FRAME PER SRM.

Part: BRACKET — BROKEN (R2 DOOR SLIDE) · airframe 33,883 hrs · 28,479 cycles

DURING SCHEDULED 10Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE FWD ATTACH MOUNT BRACKET BROKEN. REMOVED AND REPLACED BRACKET PER MM.

Part: FLOOR SUPPORT — CORRODED (BS 270) · airframe 33,883 hrs · 28,479 cycles

DURING SCHEDULED 10Y CHECK, FOUND COCKPIT FLOOR SUPPORT CORRODED AT BS 270, BETWEEN LBL 11 TO RBL 11. REMOVED AND REPLACED Z-CHORD PER SRM.

Part: BEAM — CORRODED (AFT CARGO) · airframe 33,883 hrs · 28,479 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE VERTICAL BEAM WEB CORRODED AT BS 795, RBL 20, WL 157. REMOVED AND REPLACED VERTICAL BEAM WEB SECTION PER SRM.

Part: FRAME — CRACKED (BS 480 S8L-8R) · airframe 33,883 hrs · 28,479 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, BETWEEN STR 8L & STR 8R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 867 S7-8L) · airframe 33,883 hrs · 28,479 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, BETWEEN STR 7L TO STR 8L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 907 S7-8L) · airframe 33,883 hrs · 28,479 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, BETWEEN STR 7L TO STR 8L & STR 7R TO STR 8R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 400 S8L-8R) · airframe 33,883 hrs · 28,479 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, BETWEEN STR 8L & STR 8R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (BS 663 S10L) · airframe 33,883 hrs · 28,479 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 663, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (BS 360 S8R) · airframe 33,883 hrs · 28,479 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 787 S8L-8R) · airframe 33,883 hrs · 28,479 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, BETWEEN STR 7L TO STR 8L & STR 7R TO STR 8R. REPAIRED FRAME PER SRM.

Part: CREASE BEAM — CRACKED (BS 638) · airframe 33,883 hrs · 28,479 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE CREASE BEAM INBOARD CHORD CRACKED AT BS 638, LBL 65 TO LBL 68, WL 208. REPAIRED CREASE BEAM PER SRM.

Part: FITTING — CORRODED (HORIZONTAL STAB) · airframe 33,883 hrs · 28,479 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT & RT HORIZONTAL STAB FITTING LUG FACES CORRODED. REPAIRED LUG FACES PER SRM.

Part: FRAME — CRACKED (BS 380 S8L) · airframe 33,883 hrs · 28,479 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 727D S7-8L) · airframe 33,883 hrs · 28,479 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, BETWEEN STR 7L & STR 8L. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CRACKED (BS 440 S14-15R) · airframe 33,883 hrs · 28,479 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 440, BETWEEN STR 14R TO STR 15R. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (BS 294) · airframe 33,883 hrs · 28,479 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 294.5, STR 13L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (BS 440 S8L-8R) · airframe 33,883 hrs · 28,479 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, BETWEEN STR 8L & STR 8R. REPAIRED FRAME PER SRM.

Part: FLOORBEAM — CORRODED (BS 328) · airframe 33,883 hrs · 28,479 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FLOORBEAM UPPER CHORD CORRODED AT BS 328, BETWEEN LBL 36 TO RBL 60. REPAIRED UPPER CHORD PER SRM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 32,278 hrs · 27,193 cycles

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

Part: SKIN — WORN (FUSELAGE) · airframe 29,560 hrs · 25,014 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN FROM BS 860 TO BS 1006, UNDER DORSAL FIN, WORN. REPAIRED SKIN PER EA.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 29,491 hrs · 24,967 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 29,326 hrs · 24,830 cycles

DURING SCHEDULED C1 CHECK, FOUND 2 EACH SKIN CRACKS AT LOWER KEEL BEAM BETWEEN BS 660 AND BS 724, AND BETWEEN RBL 6.30 AND LBL 6.30. REPAIRED KEEL BEAM SKIN SECTIONS PER EA.

Part: SKIN — DELAMINATED (RT FORE FLAP) · airframe 29,296 hrs · 24,806 cycles

DURING SCHEDULED C1 CHECK, FOUND RT WING INBOARD T/E FORE FLAP DELAMINATED. REMOVED AND REPLACED RT FORE FLAP PER MM.

Part: CABLE — FRAYED (R2 DOOR GIRT BAR) · airframe 29,296 hrs · 24,806 cycles

DURING SCHEDULED C1 CHECK, FOUND R2 DOOR EVAC SLIDE GIRT BAR CABLE FRAYED. REMOVED AND REPLACED R2 DOOR EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 28,989 hrs · 24,548 cycles

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

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 28,800 hrs · 24,386 cycles

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

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 28,692 hrs · 24,301 cycles

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

Part: LENS — MISSING (EMERGENCY LIGHT)

DURING SCHEDULED PM CHECK, FOUND AFT EMERGENCY EXIT OVERHEAD LIGHT LENS MISSING. REMOVED AND REPLACED LIGHT LENS PER MM. SWAA (M)

Part: SKIN — DELAMINATED (RT WING FLAP) · airframe 28,413 hrs · 24,065 cycles

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

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 28,400 hrs · 24,053 cycles

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

Part: SLIDE — MALFUNCTIONED (L1 DOOR) · airframe 26,676 hrs · 22,674 cycles

L1 DOOR EVAC SLIDE PARTIALLY DEPLOYED AT GATE. REMOVED AND REPLACED L1 DOOR EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 26,573 hrs · 22,590 cycles

DURING SCHEDULED C2 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM.

Part: TAB — CRACKED (RT ELEVATOR) · airframe 25,537 hrs · 21,767 cycles

DURING SCHEDULED 1/4D CHECK, FOUND RT ELEVATOR TAB CRACKED AT NR 2 HINGE CUTOUT LOWER SURFACE. REMOVED AND REPLACED TAB PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 24,885 hrs · 21,250 cycles

EEPLS LOOSE AT ROW NR 8. REMOVED AND REPLACED EEPLS STRIP AT ROW NR 8 PER MM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 24,064 hrs · 20,494 cycles

DURING SCHEDULED C4 CHECK, FOUND LT OUTBD AFT T/E FLAP DELAMINATED ON LOWER SURFACE INBD END. REMOVED AND REPLACED LT OUTBD AFT T/E FLAP PER MM.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 24,675 hrs · 21,077 cycles

DURING SCHEDULED C4 CHECK, FOUND LT OUTBD AFT T/E FLAP DELAMINATED AT INBD END LOWER SURFACE. REMOVED AND REPLACED LT OUTBD AFT T/E FLAP PER MM

Part: PIN — CORRODED (LT MLG TRUNION) · airframe 23,932 hrs · 20,472 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LEFT MLG TRUNNION PIN CORRODED. REMOVED AND REPLACED LEFT MLG TRUNNION PIN PER MM.

Part: STRUT — CORRODED (LT MLG) · airframe 23,932 hrs · 20,472 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LEFT MLG STRUT OUTER CYLINDER CORRODED. REMOVED AND REPLACED LEFT MLG OUTER CYLINDER PER MM.

Part: BUSHING — WORN (RT ELEV) · airframe 22,346 hrs · 19,233 cycles

DURING SCHEDULED SERVICE CHECK, SI-11139-55, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED RT ELVEVATOR TAB NR 1 HINGE FITTING BUSHINGS PER MM

Part: CABLE — LOOSE (AFT SVC DOOR) · airframe 21,884 hrs · 18,847 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE CABLE LOOSE. SECURED SLIDE CABLE PER MM.

Part: SLIDE — OUT OF ADJUST (FWD SVC DOOR) · airframe 21,884 hrs · 18,847 cycles

DURING SCHEDULED C1 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: LENS — CRACKED (CABIN) · airframe 20,071 hrs · 17,371 cycles

DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LENS PER MM.

Part: FIRE DETECTOR — MALFUNCTIONED (CARGO BAY) · airframe 19,634 hrs · 17,048 cycles

DECLARED EMERGENCY AND AIR TURNBACK, SHORTLY AFTER T/O FWD CARGO BAY FIRE ALARM LIGHT ILLUMINATED WITH AUDIO ALARM. EXECUTED THE CHECKLIST, FIRED BOTH BOTTLES. INSPECTED FWD CARGO BIN, NO EVIDENCE OF FIRE OR OVER HEATING. OK TO CONTINUE PER MEL. LATER AT BWI, REMOVED AND REPLACED CCU, FIRE BOTTLES, METERING VALVE, DIVERTER VALVE AND 4 EA SDU'S FOR FWD CARGO. PERFORMED PRESS LEAK AND FIRE SUPPRESSION SYSTEM FUNCTIONAL TEST PER MM. SYSTEM TEST NORMAL, NO FAULTS FOUND.

Part: LANYARD — OUT OF POSITION (CARGO DOOR) · airframe 14,715 hrs · 12,994 cycles

AIR TURNBACK, FWD CARGO LIGHT ILLUMINATED AFTER TAKEOFF. ACFT CABIN WOULD NOT PRESSURIZE. FOUND FWD CARGO DOOR BUNGEE CHORD HITTING ROLLER. REPOSITIONED BUNGEE CHORD. OPS CHECK GOOD PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,667 hrs · 12,956 cycles

EEPLS INOP AT ROWS 14 - 16. REMOVED AND REPLACED EEPLS SECTION PER MM.

Part: LIGHT — INOPERATIVE (ROW 15) · airframe 14,646 hrs · 12,942 cycles

EEPLS INOP FROM ROW 15 TO OVERWING EXIT. REPAIRED WIRING PER MM.

Part: WIRE — DAMAGED (CABIN) · airframe 13,773 hrs · 12,213 cycles

EEPLS WIRING EXPOSED ON SEVERAL SECTIONS. REPAIRED EEPLS WIRING AND REINSTALLED TRACK COVERS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,452 hrs · 11,940 cycles

EEPLS LOOSE AND INOPERATIVE AT MID CABIN. SECURED TRACK LIGHTS PER MM.

Part: SLIDE — DISCHARGED (CABIN)

DURING SCHEDULED RON, FOUND AFT SERVICE DOOR EVACUATION SLIDE PRESS IND LOW. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: GIRT — OUT OF POSITION (PAX DOORWAY)

DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY AND SERVICE DOOR EVACUATION SLIDE GIRT ASSY'S EXTENDING OUT OF LIMITS. ADJUSTED SLIDE ASSY'S PER MM.

Part: COMPRESSOR — BIRD STRIKE (NR 1 ENGINE)

AIR TURNBACK, MULTIPLE BIRD STRIKES DURING TAKEOFF. PERFORMED BIRD STRIKE INSPECTION ON AIRFRAME. NO DEFECT NOTED. LATER DISCOVERED 3 EA NR 1 ENG FAN BLADES BENT. REMOVED AND REPLACED FAN BENT FAN BLADES AND PERFORMED BORESCOPE INSPECTION ON BOTH ENGS. NO OTHER DEFECTS NOTED.

Part: WIRE — LOOSE (ROW 15)

WIRES LOOSE AT EMERGENCY ESCAPE FLOOR TRACK LIGHTS AT ROW 15. SECURED WIRES PER MM.

Part: WIRE — BROKEN (ROW 12-17)

EMERGENCY EXIT LIGHTS ROW 12-17 INOP DUE TO BROKEN WIRE DISCOVERED IN FLIGHT. REPAIRED FLOOR TRACK LIGHTING PER M/M.

Part: BATTERY — DISCHARGED (CABIN)

DURING PREFLIGHT, FOUND LEFT OVERWING EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK PER BOEING M/M.