N622SW

Part: SENSOR — FAULTY (NLG) · airframe 66,167 hrs · 52,331 cycles

AIR TURNBACK/DECLARED EMERGENCY, ON TAKEOFF NOSE GEAR RED & GREEN INDICATOR LIGHTS REMAINED ILLUMINATED. R&R NOSE LANDING GEAR DOWN SENSOR PER MM.

Part: ESCAPE ROPE — UNSECURE (CABIN) · airframe 65,832 hrs · 52,111 cycles

LT EMERGENCY EXIT SAFETY ROPE FELL OUT. REPOSITIONED EXIT ROPE PER AMM.

Part: SIGN — UNSECURE (CABIN) · airframe 65,832 hrs · 52,111 cycles

LT EMERGENCY EXIT SIGN FELL. SECURED SIGN PER AMM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 65,550 hrs · 51,918 cycles

EMERGENCY LIGHT LENS MISSING NEXT TO R2 DOOR. INSTALLED THE LENS IAW MM.

Part: FAIRING — DELAMINATED (RT WING TE FLAP) · airframe 65,220 hrs · 51,692 cycles

RIGHT WING INBOARD FLAP OUTBOARD TRACK FAIRING DELAMINATED. REPAIRED THE FAIRING IAW SRM.

Part: ACTUATOR — FAULTY (NLG LOCK) · airframe 64,880 hrs · 51,454 cycles

NOSE GEAR FAILED TO RETRACT ON 2 ATTEMPTS IAW QRC. DECLARED AN EMERGENCY AND RETURN TO DEPARTURE. R & R NOSE LANDING GEAR LOCK ACTUATOR IAW AMM.

Part: ACTUATOR — FAULTY (NLG) · airframe 64,317 hrs · 51,088 cycles

ON TAKEOFF, RAISED LANDING GEAR HANDLE AND NOSE WHEEL REMAINED EXTENDED. RECYCLED GEAR AN ON NEXT ATTEMPT NOSE GEAR WAS UP AND LOCKED, NO LIGHTS. R & R NOSE GEAR LOCK ACTUATOR IAW AMM.

Part: SIGN — LOOSE (EMERGENCY LIGHTS) · airframe 64,252 hrs · 51,047 cycles

FORWARD ENTRY EXIT SIGN LOOSE. R & R THE SIGN IAW AMM.

Part: SLIDE — BROKEN (L1 DOOR) · airframe 64,064 hrs · 50,925 cycles

L1 DOOR EMERGENCY EVAC SLIDE LATCH BROKEN. R & R SLIDE IAW MAINTENANCE.

Part: SLAT — CRACKED (LT WING) · airframe 63,590 hrs · 50,611 cycles

LEFT WING NR 1 SLAT LE CRACKED FROM INBD SIDE. R & R 1 SLAT IAW MM.

Part: ANGLE — CRACKED (TE FLAP) · airframe 62,781 hrs · 50,073 cycles

LEFT WING INBD FLAP, OTBD TRACK FAIRING OTBD AFT L ANGLE CRACKED. R & R L ANGLE IAW SRM.

Part: ANGLE — CRACKED (RT WING) · airframe 62,781 hrs · 50,073 cycles

RIGHT WING TE INBD PANEL AFT L ANGLE CRACKED. R & R L ANGLE IAW SRM.

Part: ANGLE — CRACKED (TE FLAP) · airframe 62,781 hrs · 50,073 cycles

LEFT WING INBD FLAP, OTBD TRACK FAIRING, INBD AFT L ANGLE CRACKED. R & R L ANGLE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,781 hrs · 50,073 cycles

SHEAR TIE CORRODED AT BS 520, BETWEEN LBL 8 TO RBL 10. R & R SHEAR TIE IAW SRM & DWG.

Part: SKIN — CRACKED (RT WING) · airframe 62,781 hrs · 50,073 cycles

RIGHT WING UPPER SKIN CRACKED FASTENER HOLES AFT OF REAR SPAR, BETWEEN RSS 265 - 270. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 62,781 hrs · 50,073 cycles

RIGHT WING UPPER WING SKIN TE CRACKED AT FASTENER HOLE RSS 255.5. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 62,781 hrs · 50,073 cycles

LEFT WING UPPER SKIN CRACKED, AT FASTENER HOLE AFT OF REAR SPAR, AT RSS 270. REPAIRED SKIN IAW ER & EA.

Part: FITTING — CRACKED (LT WING) · airframe 62,781 hrs · 50,073 cycles

LEFT WING REAR SPAR AFT BEAM TO SPAR FITTING CRACKED AT FASTENER HOLE, UPPER ROW APPROX, RSS 223. REPAIRED FITTING IAW ER & EA.

Part: SPAR — CRACKED (RT WING) · airframe 62,781 hrs · 50,073 cycles

RIGHT WING REAR SPAR UPPER CHORD CRACKED AT RSS 223. REPAIRED CHORD IAW ER & EA.

Part: SPAR — CRACKED (LT WING) · airframe 62,781 hrs · 50,073 cycles

LEFT WING REAR SPAR, UPPER CHORD CRACKED, AT FASTENER HOLE UPPER ROW APPROX RSS 223. REPAIRED CHORD IAW ER & EA.

Part: SPAR — CRACKED (RT WING) · airframe 62,781 hrs · 50,073 cycles

RIGHT WING REAR SPAR WEB CRACKED, AT FASTENER HOLE UPPER ROW, APPROX RSS 223 COMMON TO AFT FITTING UPPER INBD HOLE. REPAIRED WEB ER & EA.

Part: FITTING — CRACKED (RT WING) · airframe 62,781 hrs · 50,073 cycles

RIGHT WING REAR SPAR AFT BEAM TO SPAR FITTING CRACKED, AT UPPER ROW INBD HOLE. REPAIRED FITTING IAW ER & EA.

Part: SPAR — CRACKED (LT WING) · airframe 62,781 hrs · 50,073 cycles

LEFT WING REAR SPAR WEB CRACKED, AT FASTENER HOLE COMMON TO UPPER CHORD, UPPER ROW APPROX RSS 223. REPAIRED WEB ER & EA.

Part: LINK — CORRODED (LT MLG) · airframe 62,781 hrs · 50,073 cycles

LEFT MLG SUPPORT BEAM, SWING LINK ASSEMBLY CORRODED. R & R SWING LINK ASSEMBLY IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,781 hrs · 50,073 cycles

PNEUMATIC SERVICE DOOR SKIN CUT OUT CRACKED AT THE FWD LT CORNER. REPAIRED CUT OUT IAW SRM.

Part: LENS — LOOSE (CABIN) · airframe 62,565 hrs · 49,921 cycles

CENTER AISLE CEILING MOUNT, EMER EXIT LIGHT LENS ASSEMBLY LOOSE. SECURED LENS IAW MM.

Part: LENS — LOOSE (CABIN) · airframe 62,379 hrs · 49,791 cycles

RIGHT OVERWING EXIT, EMER EXIT LIGHT LENS LOOSE. SECURED LENS IAW MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,272 hrs · 49,715 cycles

SHEAR TIE CORRODED AT BS 500B, BETWEEN STRINGER 26L - 27L. REPAIRED SHEAR TIE IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 62,272 hrs · 49,715 cycles

FLOORBEAM UPPER CHORD OTBD FLANGE, CRACKED AT BS 727B, RBL 24.82. REPAIRED FLANGE IAW EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,272 hrs · 49,715 cycles

SHEAR TIE CORRODED AT BS 500B, BETWEEN STRINGER 27L - 28L. REPAIRED SHEAR TIE IAW SRM.

Part: COVER — BROKEN (CABIN) · airframe 62,272 hrs · 49,715 cycles

G1 EXIT LIGHT COVER BROKEN. R & R COVER IAW AMM.

Part: WEB — CRACKED (FUSELAGE) · airframe 62,272 hrs · 49,715 cycles

MAIN CABIN FLOOR WEB CRACKED AT BS 1002, RBL 40. R & R WEB IAW SRM & DWG.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 62,272 hrs · 49,715 cycles

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

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 62,272 hrs · 49,715 cycles

FORWARD ENTRY DOOR SURROUND STRUCTURE STRINGER SPLICE, CRACKED AT BS 360, STRINGER 14L. R & R SPLICE IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,272 hrs · 49,715 cycles

AFT RT GALLEY DOOR SKIN CUT OUT CRACKED, LOWER FWD CORNER. REPAIRED SKIN IAW ER & EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 62,272 hrs · 49,715 cycles

LEFT CREASE BEAM WEB CORRODED, BETWEEN BS 802 TO 827. REPAIRED WEB IAW SRM & DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 62,272 hrs · 49,715 cycles

SPLICE ANGLE CORRODED AT BS 1016, BETWEEN STRINGER 26R - 27R. R & R SPLICE ANGLE IAW ER & EA.

Part: WIRE — DISCONNECTED (CABIN) · airframe 62,272 hrs · 49,715 cycles

AFT LAVATORY EMER EXIT INDICATOR LIGHT CONNECTOR WIRE D10084 DISCONNECTED. REPAIRED WIRE IAW AMM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 62,272 hrs · 49,715 cycles

FLOOR BEAM CORRODED AT BS 967, RBL 26. REPAIRED FLOORBEAM IAW SRM.

Part: WIRE — DISCONNECTED (CABIN) · airframe 62,272 hrs · 49,715 cycles

AFT LAVATORY EMER EXIT INDICATOR LIGHT CONNECTOR WIRE D10082 DISCONNECTED. REPAIRED WIRE IAW AMM.

Part: STIFFENER — CRACKED (RT MLG WW) · airframe 62,272 hrs · 49,715 cycles

VERTICAL STIFFENER CRACKED AT BS 663.75, RBL 6.15. REPAIRED STIFFENER IAW EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 62,272 hrs · 49,715 cycles

RIGHT CREASE BEAM WEB CORRODED, BETWEEN BS 867 - 887. R & R WEB IAW DWG & SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 62,272 hrs · 49,715 cycles

LEFT CREASE BEAM WEB CORRODED, BETWEEN BS 827 - 847. R & R WEB IAW SRM & DWG.

Part: LENS — DAMAGED (CABIN) · airframe 62,272 hrs · 49,715 cycles

FORWARD GALLEY EXIT LIGHT LENS DAMAGED. R & R LENS IAW AMM.

Part: SLAT — CORRODED (RT WING) · airframe 62,272 hrs · 49,715 cycles

RIGHT WING NR 4 LE SLAT OTBD MAIN SLAT TRACK, CORRODED ON BOTTOM SIDE. R & R SLAT IAW CHM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 62,272 hrs · 49,715 cycles

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

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 62,272 hrs · 49,715 cycles

RIGHT CREASE BEAM INBD CHORD CORRODED, BETWEEN BS 985 - 995, RBL 46. R & R CHORD IAW SRM & DWG.

Part: COVER — LOOSE (CABIN) · airframe 61,933 hrs · 49,470 cycles

RIGHT DOOR MID CABIN EMER EXIT LIGHT LENS COVER LOOSE. SECURED COVER IAW SIP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 60,983 hrs · 48,814 cycles

EMERGENCY EXIT BULLNOSE LIGHT INOPERATIVE AT 12 ABC. FOUND OVERHEAD BIN ATTACH BOLT BINDING LIGHT ASSEMBLY. REPOSITIONED BOLT & OPERATIONS CHECKED GOOD IAW MM. .

Part: CARRIAGE — CORRODED (TE FLAP) · airframe 60,841 hrs · 48,722 cycles

LEFT WING FLAP CARRIAGE NR 3 OTBD HALF AFT BOLT HOLE CORRODED. R & R CARRIAGE ARM IAW CMM.

Part: CARRIAGE — CORRODED (TE FLAP) · airframe 60,841 hrs · 48,722 cycles

LEFT WING FLAP TRACK CARRIAGE NR 3 INBD HALF AFT ROLLER BOLT HOLE CORRODED. R & R CARRIAGE ARM IAW CMM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,841 hrs · 48,722 cycles

LEFT FRAME OTBD CHORD LOWER FWD CRACKED AT BS 727. R & R CHORD IAW EA.

Part: FUSE — BLOWN (CABIN) · airframe 59,906 hrs · 48,116 cycles

LEFT CABIN EMER EXIT LIGHT INOPERATIVE BETWEEN ROW 1 - 3. R & R FUSE IAW AMM.

Part: PANEL — CRACKED (NR 2 PYLON) · airframe 59,906 hrs · 48,116 cycles

NUMBER 2 ENG PYLON PANEL 5869 UPPER AFT FASTENER HOLE CRACKED. REPAIRED PANEL IAW SRM.

Part: BRACKET — DIRTY (CABIN) · airframe 58,902 hrs · 47,388 cycles

L1 DOOR GIRT BAR FLOOR CLIP INOPERATIVE. CLEANED GIRT BAR FLOOR BRACKET IAW MM.

Part: GUSSET — CRACKED (R1 DOOR) · airframe 57,535 hrs · 46,477 cycles

R1 DOOR GUSSET CRACKED. R & R R1 DOOR IAW AMM.

Part: CASTING — CRACKED (LT SPOILER) · airframe 57,535 hrs · 46,477 cycles

LT WING INBD GND SPOILER ACTUATOR INBD CASTING CRACKED AT UPPER BOLT HOLE. R & R CASTING IAW SRM.

Part: FLAP — OUT OF ADJUST (RT WING) · airframe 57,535 hrs · 46,477 cycles

RT WING INBD AFT FLAP OUT OF ADJUSTMENT. ADJUSTED AFT FLAP IAW AMM.

Part: SPOILER — DELAMINATED (LT WING) · airframe 57,535 hrs · 46,477 cycles

LT WING INBD NR 4 GND SPOILER DELAMINATED. R & R SPOILER IAW AMM.

Part: LENS — LOOSE (CABIN) · airframe 57,211 hrs · 46,249 cycles

RT OVERWING LOWER EMERGENCY EXIT LIGHT LENS LOOSE. REPAIRED LENS IAW MM.

Part: RESISTOR — INOPERATIVE (COCKPIT) · airframe 56,867 hrs · 46,016 cycles

COCKPIT EMERGENCY EXIT LIGHT IN DOME LIGHT ASSEMBLY INOPERATIVE. REPAIRED RESISTOR IAW BSWPM & AMM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,867 hrs · 46,016 cycles

FRAME CRACKED AT STATION 420, STRINGER 3L. REPAIRED FRAME IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,867 hrs · 46,016 cycles

SKIN CRACKED AT STATION 380, STRINGER 14R AT LOWER ROW FASTENER HOLE CRACKED. REPAIRED SKIN IAW SWA EA.

Part: STRINGER CLIP — BROKEN (FUSELAGE) · airframe 56,867 hrs · 46,016 cycles

STRINGER CLIP BROKEN AT BS 847, STRINGER 1. R & R CLIP IAW SRM & BAC DRAWING.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 56,867 hrs · 46,016 cycles

STRINGER SPLICE CRACKED AT STATION 360, STRINGER 8L. R & R SPLICE IAW SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,867 hrs · 46,016 cycles

STRINGER CLIP CRACKED AT STATION 420, STRINGER 9R. R & R CLIP IAW DRAWING & SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,867 hrs · 46,016 cycles

STRINGER CLIP CRACKED AT STATION 440, STRINGER 9R. R & R CLIP IAW DRAWING & SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,867 hrs · 46,016 cycles

LT BS 867+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLE 3. REPAIRED SKIN IAW EA & TC.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,867 hrs · 46,016 cycles

RT BS 827+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLE 4 & HFEC CRACK INDICATION AT HOLE 3. REPAIRED SKIN IAW SB & TC.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,867 hrs · 46,016 cycles

LT BS 400+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLE 4,8. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,867 hrs · 46,016 cycles

LT BS 460+10 UPPER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLE 4. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,867 hrs · 46,016 cycles

LT BS 500C+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 3,5,6,8. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,867 hrs · 46,016 cycles

LT BS 480+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 4 - 88. REPAIRED SKIN IAW TC & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,867 hrs · 46,016 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,867 hrs · 46,016 cycles

LT BS 827+10 LOWER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLE 3. REPAIRED SKIN IAW SB & TC.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,867 hrs · 46,016 cycles

LT BS 827+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 2,3. REPAIRED SKIN EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,867 hrs · 46,016 cycles

LT BS 867+10 LOWER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLES 3,12. REPAIRED SKIN IAW SB & TC.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,867 hrs · 46,016 cycles

LT BS 460+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 4,5,8. REPAIRED SKIN IAW TC & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,867 hrs · 46,016 cycles

LT BS 500B+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 1,3,4,5,7,8.. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,867 hrs · 46,016 cycles

LT BS 807+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 2,3. REPAIRED SKIN IAW SB & TC.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,867 hrs · 46,016 cycles

LT BS 500A+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 4-8. REPAIRED SKIN IAW TC & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,867 hrs · 46,016 cycles

LT BS 480+10 UPPER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLES 3,4,6,7,8. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,867 hrs · 46,016 cycles

FUSELAGE SKIN CRACKED AT LT BS 420+10, LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,867 hrs · 46,016 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,867 hrs · 46,016 cycles

LT BS 847+10 LOWER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLES 3,6,7,8. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,867 hrs · 46,016 cycles

RT BS 807+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLE 3. REPAIRED SKIN IAW TC & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,867 hrs · 46,016 cycles

LT BS 380+10 UPPER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLES 2 - 6. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,867 hrs · 46,016 cycles

LT BS 380+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 5,6,7. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,867 hrs · 46,016 cycles

RT BS 787+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT INDICATION AT HOLE 3. REPAIRED SKIN IAW SB & TC.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,867 hrs · 46,016 cycles

RT BS 887+10 LOWER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLE 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,867 hrs · 46,016 cycles

RT BS 867+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLE 3. REPAIRED SKIN IAW SB &TC.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,867 hrs · 46,016 cycles

LT BS 500+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 3 - 8. REPAIRED SKIN IAW SB & TC.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,867 hrs · 46,016 cycles

RT BS 767+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLE 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,867 hrs · 46,016 cycles

LT BS 360+10 UPPER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLES 4-7. REPAIRED SKIN IAW TC.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 56,867 hrs · 46,016 cycles

STRINGER CRACKED AT BS 380, STRINGER 8R. REPAIRED STRINGER IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,867 hrs · 46,016 cycles

LT BS 400+10 UPPER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLES 3 - 6. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,867 hrs · 46,016 cycles

LT BS 847+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLE 1,3,5. REPAIRED SKIN IAW SB &TC.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,867 hrs · 46,016 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,867 hrs · 46,016 cycles

RT BS 767+10 LOWER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLE 3. REPAIRED SKIN IAW SB & TC.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 56,735 hrs · 45,905 cycles

AFT CARGO COMPARTMENT BRACKET CRACKED AT BS 727, BETWEEN STRINGER 27L TO STRINGER 27R. R&R BRACKET IAW SRM & DRAWING.

Part: SHEAR WEB — CRACKED (FUSELAGE) · airframe 56,735 hrs · 45,905 cycles

SHEAR WEB CRACKED BETWEEN BS 348.2 TO BS 351.2, BETWEEN STRINGER 17L TO STRINGER 15L. R&R SHEAR WEB IAW SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 56,735 hrs · 45,905 cycles

FWD CARGO DOOR CUTOUT FRAME WEB CRACKED AT BS 440, STRINGER 24R. R&R FRAME IAW EA.

Part: ANGLE — CRACKED (RT WING) · airframe 56,735 hrs · 45,905 cycles

RT WING TE ANGLE CRACKED AT CAVITY RSS 546. R&R ANGLE IAW SRM & DRAWING.

Part: LENS — BROKEN (CABIN) · airframe 56,735 hrs · 45,905 cycles

R2 DOOR EMERGENCY EXIT SIGN UPPER POSITION LENS ASSEMBLY BROKEN. R&R LENS IAW AMM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 56,735 hrs · 45,905 cycles

VERTICAL BEAM WEB CRACKED AT BS 178, RBL 5.7. REPAIRED WEB IAW EA & EO.

Part: LENS — BROKEN (CABIN) · airframe 56,735 hrs · 45,905 cycles

L1 DOOR EMERGENCY EXIT SIGN UPPER POSITION LENS ASSEMBLY BROKEN. R&R LENS IAW AMM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 56,735 hrs · 45,905 cycles

VERTICAL BEAM WEB CRACKED AT BS 178 RBL 5.7. REPAIRED WEB IAW EA.

Part: STRIP — CRACKED (THRUST REVERSER) · airframe 56,735 hrs · 45,905 cycles

NR 1 ENGINE THRUST REVERSER OTBD FWD EDGE STRIP CRACKED. R&R STRIP IAW SRM & DRAWING.

Part: WEB — CRACKED (NLG WW) · airframe 56,735 hrs · 45,905 cycles

LT SIDE NLG WW WEB CRACKED AT BS 243.7+3.5 WL 169. REPAIRED WEB IAW EA.

Part: ATTACH ANGLE — CRACKED (LT HORIZ STAB) · airframe 56,735 hrs · 45,905 cycles

LT HORIZONTAL STABILIZER CENTER SECTION ATTACH ANGLE CRACKED. R&R ANGLE IAW SRM & DRAWING.

Part: FRAME — MISSING (FUSELAGE) · airframe 56,735 hrs · 45,905 cycles

FRAME OF INTER CHORD MISSING AT BS 348.2 STRINGER 15L. INSTALLED CHORD IAW EO & EA.

Part: LATCH — CRACKED (RT WING) · airframe 56,735 hrs · 45,905 cycles

RT WING ACCESS PANEL NR 6540R LATCH CRACKED. R&R LATCH IAW SRM.

Part: ATTACH ANGLE — CRACKED (RT HORIZ STAB) · airframe 56,735 hrs · 45,905 cycles

RT HORIZONTAL STABILIZER CENTER SECTION ATTACH ANGLE CRACKED. R&R ANGLE IAW SRM & DRAWING.

Part: ACCESS PANEL — CRACKED (RT WING) · airframe 56,735 hrs · 45,905 cycles

RT WING ACCESS PANEL PLATE CRACKED ON PANEL NR 6531R. R&R PANEL IAW SRM & DRAWING.

Part: ANGLE — CRACKED (LT WING) · airframe 56,735 hrs · 45,905 cycles

LT WING INBD TE STRUCTURE ANGLE CRACKED AT WBL 184.63. R&R ANGLE IAW SRM & DRAWING.

Part: SKIN — CRACKED (LE SLAT) · airframe 56,735 hrs · 45,905 cycles

RT WING NR 6 INBD EDGE SLAT SKIN CRACKED. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 56,735 hrs · 45,905 cycles

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

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 56,735 hrs · 45,905 cycles

AFT CARGO COMPARTMENT STIFFENER CORRODED BETWEEN BS 1006 TO BS 1016, STRINGER 26R. R&R STIFFENER IAW SRM & DRAWING.

Part: SHIM — CRACKED (LT WING) · airframe 56,735 hrs · 45,905 cycles

LT WING FIXED TE SUPPORT STRUCTURE ACCESS PANEL 5735L SHIM CRACKED. R&R SHIM IAW SRM & DRAWING.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 56,735 hrs · 45,905 cycles

BULKHEAD LOWER CHORD CORRODED AT BS 1016, BL 0. REPAIRED CHORD IAW EO & EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 56,735 hrs · 45,905 cycles

FRAME CORRODED AT BS 947.5, BETWEEN STRINGER 27L TO STRINGER 27R. REPAIRED FRAME IAW SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 56,735 hrs · 45,905 cycles

STRINGER CORRODED AT BS 947.5 STRINGER 27L. REPAIRED STRINGER IAW SRM.

Part: PLATE — CRACKED (FUSELAGE) · airframe 56,735 hrs · 45,905 cycles

AFT CARGO COMPARTMENT PLATE CRACKED AT BS 794 BETWEEN STRINGER 25R TO STRINGER 24R. R&R PLATE IAW SRM & DRAWING.

Part: PLATE — CRACKED (RT HORIZ STAB) · airframe 56,735 hrs · 45,905 cycles

RT HORIZONTAL STABILIZER ACCESS PANEL 9226R PLATE CRACKED. R&R PLATE IAW SRM & DRAWING.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 56,735 hrs · 45,905 cycles

LONGITUDINAL FLOOR BEAM UPPER CHORD CRACKED AT BS 668.0 LBL 24.8. REPAIRED CHORD IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,735 hrs · 45,905 cycles

L2 DOOR FORWARD LOWER DOOR SKIN CUT OUT CRACKED BETWEEN BS 927 TO BS 987, BETWEEN STRINGER 15L TO STRINGER 20L. REPAIRED SKIN IAW EO & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,735 hrs · 45,905 cycles

L2 DOOR FWD LOWER CORNER FS SKIN CRACKED BETWEEN BS 927 TO BS 987 BETWEEN STRINGER 15L TO STRINGER 20L. REPAIRED SKIN 987 IAW EO & EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 56,735 hrs · 45,905 cycles

LONGITUDINAL FLOOR BEAM UPPER CHORD CRACKED AT BS 664.0 LBL 24.8. REPAIRED CHORD IAW EA.

Part: STRAP — CORRODED (FUSELAGE) · airframe 56,735 hrs · 45,905 cycles

STRAP CORRODED AT BS 947.5 STRINGER 27L. R&R STRAP IAW SRM & DRAWING.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 56,735 hrs · 45,905 cycles

AFT CARGO DOOR HANDLE CUTOUT CRACKED. REPAIRED SKIN IAW EA.

Part: LIGHT — LOOSE (CABIN) · airframe 56,008 hrs · 45,384 cycles

RIGHT EEPLS LOOSE AT ROW 8. SECURED EEPLS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,569 hrs · 45,059 cycles

FUSELAGE SKIN CRACKED AT BS 420 + 12, STR 10R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,569 hrs · 45,059 cycles

FUSELAGE SKIN CRACKED AT BS 727A + 10 2.4, STR 10R. REPAIRED SKIN PER EA.

Part: GASPER FAN — FAULTY (E&E BAY) · airframe 55,253 hrs · 44,854 cycles

ACRID SMELL IN CENTER OF CABIN DIVERTED TO SDF. VISIBLE HAZE IN CABIN. SMELLED ELECTRICAL. REMOVED AND REPLACED GASPER FAN PER M/M, OPS CHECKS GOOD.

Part: GLOWSTRIP — LOOSE (CABIN) · airframe 54,975 hrs · 44,674 cycles

PHOTOLUMINESCENT FLOOR TRACK LIGHT STRIP LOOSE AT ROW 7&8 DEF. REMOVED AND REPLACED PHOTOLUMINESCENT FLOOR TRACK LIGHT STRIP AT ROW 7, 8 DEF PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 54,133 hrs · 44,069 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: PRESSURE PANEL — CRACKED (MLG WW) · airframe 54,133 hrs · 44,069 cycles

MAIN WHEEL WELL CEILING BEADED WEB CRACKED AT BS 664, LBL 32. REPAIRED WEB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,021 hrs · 43,985 cycles

SKIN CRACKED AT BS 747+4, STR 10R. REPAIRED SKIN PER EA.

Part: SPINDLE — CORRODED (TE FLAP) · airframe 54,013 hrs · 43,978 cycles

LEFT WING NR 2 FLAP CARRIAGE SPINDLE THERMAL COATING AND BASE METAL CORRODED. REMOVED AND REPLACED NR 2 SPINDLE FLAP CARRIAGE ASSY PER MT.

Part: SLIDE — LOOSE (R1 DOOR) · airframe 53,362 hrs · 43,469 cycles

R1 DOOR SLIDE LOOSE. RE-INSTALLED SLIDE PER MT.

Part: FLAP — DELAMINATED (LT WING) · airframe 53,234 hrs · 43,376 cycles

LEFT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER AMM.

Part: FLAP — DELAMINATED (RT WING) · airframe 52,790 hrs · 43,024 cycles

RT WING INBD FORE FLAP DELAMINATED. REPAIRED FLAP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,790 hrs · 43,024 cycles

R1 DOOR FUSELAGE SKIN CUTOUT CRACKED FWD LOWER EDGE, BS 259. REPAIRED SKIN IAW ER AND EA.

Part: FLAP — DELAMINATED (RT WING) · airframe 52,339 hrs · 42,689 cycles

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

Part: ACTUATOR — FAULTY (LE SLAT) · airframe 51,566 hrs · 42,090 cycles

AIR TURNBACK - LT WING L/E FLAP TRANSIT LIGHT ON. TRANSIT LIGHT FOR NR 2 & 4 SLATS ILLUMINATED ON OVERHEAD PANEL. CYCLED FLAPS TO ZERO WITH NO L/E FLAP MOVEMENT. REMOVED AND REPLACED NR 4 SLAT ACTUATOR PER MM.

Part: FUSE — FAULTY (COCKPIT) · airframe 51,542 hrs · 42,070 cycles

DIVERSION - L/E FLAPS TRANSIT LIGHT WITH L/E SLATS AND L/E FLAPS EXTENDED AT POSITION 2, 3, 4 WITH FLAP LEVER UP AFTER TAKEOFF. REMOVED AND REPLACED L/E SLAT EXTENDED FUSE PER MM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 51,509 hrs · 42,043 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CORRODED BETWEEN BS 907 TO BS 1016, STR 21R. REPAIRED STRINGER IAW DWG.

Part: SKIN — CORRODED (FUSELAGE) · airframe 51,509 hrs · 42,043 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,509 hrs · 42,043 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 947.5, STR 25R. REMOVED AND REPLACED CLIP IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,509 hrs · 42,043 cycles

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

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 51,509 hrs · 42,043 cycles

DURING SCHEDULED 16Y CHECK, FOUND INNER CHORD CORRODED BETWEEN BS 947.5 TO BS 1006, STR 17R. REMOVED AND REPLACED CHORD IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,509 hrs · 42,043 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 500C, BETWEEN STR 26L TO STR 27L. REPAIRED FRAME IAW SRM AND DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 51,509 hrs · 42,043 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 727D+5, RBL 3.0. REPAIRED CHANNEL IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 51,509 hrs · 42,043 cycles

DURING SCHEDULED 16Y CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED BETWEEN BS 707 TO BS 712, RBL 24.5. REPAIRED WEB IAW EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,509 hrs · 42,043 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 993.5, STR 17R. REPAIRED FRAME IAW EA.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 51,509 hrs · 42,043 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT ANGLE CORRODED AT BS 747, STR 27R. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,509 hrs · 42,043 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 867, BETWEEN STR 26R TO STR 27R. REPAIRED FRAME IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 51,509 hrs · 42,043 cycles

DURING SCHEDULED 16Y CHECK, FOUND WEB CRACKED BETWEEN BS 707 TO BS 712, LBL 24.8. REPAIRED WEB IAW EO.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,509 hrs · 42,043 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 500A, BETWEEN STR 26L TO STR 27L. REPAIRED FRAME IAW SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,509 hrs · 42,043 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500D, BETWEEN STR 27R TO STR 28R. REMOVED AND REPLACED SHEAR TIE IAW SRM AND DWG.

Part: BEAM — CRACKED (FUSELAGE) · airframe 51,509 hrs · 42,043 cycles

DURING SCHEDULED 16Y CHECK, FOUND STUB BEAM CRACKED AT BS 639, RBL 45.5. REPAIRED BEAM IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,509 hrs · 42,043 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKD AT BS 188, STR 17L. REPAIRED FRAME IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,509 hrs · 42,043 cycles

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

Part: WEB — CORRODED (FUSELAGE) · airframe 51,509 hrs · 42,043 cycles

DURING SCHEDULED 16Y CHECK, FOUND FWD CARGO COMPARTMENT WEB CORRODED BETWEEN BS 500C TO BS 500D, STR 17L. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,509 hrs · 42,043 cycles

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

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,509 hrs · 42,043 cycles

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

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,509 hrs · 42,043 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 500C, BETWEEN STR 26R TO STR 27R. REPAIRED FRAME IAW SRM AND DWG.

Part: BRACKET — DAMAGED (FUSELAGE) · airframe 51,509 hrs · 42,043 cycles

DURING SCHEDULED 16Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE FWD FLOOR BRACKET DAMAGED. REMOVED AND REPLACED BRACKET IAW MM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 51,509 hrs · 42,043 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CRACKED AT BS 380, STR 5L. REPAIRED STRINGER IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,509 hrs · 42,043 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 907, BETWEEN STR 27L TO STR 27R. REPAIRED FRAME IAW SRM.

Part: LIGHT — DELAMINATED (CABIN) · airframe 51,509 hrs · 42,043 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT EEPLS DELAMINATED. REMOVED AND REPLACED EEPLS IAW MM.

Part: LIGHT — DELAMINATED (CABIN) · airframe 51,509 hrs · 42,043 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT EEPLS DELAMINATED. REMOVED AND REPLACED EEPLS IAW MM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,509 hrs · 42,043 cycles

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

Part: BRACKET — DAMAGED (FUSELAGE) · airframe 51,509 hrs · 42,043 cycles

DURING SCHEDULED 16Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE AFT FLOOR BRACKET DAMAGED. REMOVED AND REPLACED BRACKET IAW MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,509 hrs · 42,043 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685+10, RBL 24.5. R&R CLIP IAW SRM AND DWG.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 51,509 hrs · 42,043 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CRACKED BETWEEN BS 500+18 TO BS 500D+5, STR 4L. REPAIRED STRINGER IAW SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 51,509 hrs · 42,043 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CRACKED AT BS 380+7, STR 4L. REPAIRED STRINGER IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,509 hrs · 42,043 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 1006, BETWEEN STR 27L TO STR 27R. REMOVED AND REPLACED SHEAR TIE IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,509 hrs · 42,043 cycles

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

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 51,509 hrs · 42,043 cycles

DURING SCHEDULED 16Y CHECK, FOUND SUPPORT ANGLE CRACKED AT BS 685+10, LBL 24.5. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 51,509 hrs · 42,043 cycles

DURING SCHEDULED 16Y CHECK, FOUND SUPPORT ANGLE CORRODED BETWEEN BS 967 TO BS 986, RBL 50. REMOVED AND REPLACED ANGLE PER SRM AND DWG.

Part: COVER — BROKEN (CABIN) · airframe 51,509 hrs · 42,043 cycles

DURING SCHEDULED 16Y CHECK, FOUND FWD EMERGENCY EXIT LIGHT COVER BROKEN. REMOVED AND REPLACED COVER IAW MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,509 hrs · 42,043 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 51,509 hrs · 42,043 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 4L. REMOVED AND REPLACED STRINGER IAW SRM AND DWG.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 51,509 hrs · 42,043 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN DOUBLER CORRODED BETWEEN BS 727E TO BS 747, BETWEEN STR 26R TO STR 27R. REMOVED AND REPLACED DOUBLER IAW SRM AND DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 51,509 hrs · 42,043 cycles

DURING SCHEDULED 16Y CHECK, FOUND WEB CRACKED BETWEEN BS 707.5 TO BS 712, BL 0.07. REPAIRED WEB PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,509 hrs · 42,043 cycles

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

Part: WEB — CORRODED (FUSELAGE) · airframe 51,509 hrs · 42,043 cycles

DURING SCHEDULED 16Y CHECK, FOUND FWD CARGO COMPARTMENT WEB CORRODED BETWEEN BS 500 TO BS 500A, STR 17L. REMOVED AND REPLACED WEB IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,509 hrs · 42,043 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 460, STR 16R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,509 hrs · 42,043 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,509 hrs · 42,043 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 (BS 887 S4L) · airframe 51,509 hrs · 42,043 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 4L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (BS 727A S25R) · airframe 51,509 hrs · 42,043 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 25R. REMOVED AND REPLACED STRINGER CLIP IAW SRM AND DWG.

Part: FLOORBEAM — CRACKED (BS 727B) · airframe 51,509 hrs · 42,043 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CRACKED AT BS 727B, LBL 45.5. REPAIRED FLOORBEAM IAW SRM.

Part: STRINGER CLIP — CRACKED (BS 727A S25L) · airframe 51,509 hrs · 42,043 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 25L. REMOVED AND REPLACED STRINGER CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,509 hrs · 42,043 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,509 hrs · 42,043 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 2R. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,509 hrs · 42,043 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 4L. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: FLASHLIGHT — BROKEN (CABIN) · airframe 51,509 hrs · 42,043 cycles

DURING SCHEDULED 16Y CHECK, FOUND FWD EMERGENCY FLASHLIGHT BASE BROKEN. REMOVED AND REPLACED FLASHLIGHT IAW MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,509 hrs · 42,043 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 5R. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,509 hrs · 42,043 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 51,509 hrs · 42,043 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 11L. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,509 hrs · 42,043 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 10R. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,509 hrs · 42,043 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,509 hrs · 42,043 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 4L. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,509 hrs · 42,043 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 22L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 52,052 hrs · 42,526 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER SPLICE CORRODED AT BS 907, STR 22R. REMOVED AND REPLACED SPLICE IAW SRM AND DWG.

Part: ACTUATOR — FAULTY (LT MLG) · airframe 50,492 hrs · 41,286 cycles

RAISE MLG, LT MLG RED LIGHT ILLUMINATED. GEAR HANDLE TO OFF MAIN EXTENDED. RAISED HANDLE TO UP. REMOVED AND REPLACED MLG UPLOCK ACTUATOR PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 50,003 hrs · 40,904 cycles

DURING SCHEDULED SPV CHECK, FOUND R1 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BULB PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,003 hrs · 40,904 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 616+11, STR 4L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,003 hrs · 40,904 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 633.75+10, STR 4L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,003 hrs · 40,904 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 616+9, STR 4L. REPAIRED SKIN PER EA.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 50,003 hrs · 40,904 cycles

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

Part: CHARGER — INOPERATIVE (CABIN) · airframe 49,787 hrs · 40,743 cycles

DURING SCHEDULED SPV CHECK, FOUND LT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT INOP BETWEEN ROW 2 TO ROW 6. REMOVED AND REPLACED BATTERY CHARGER ASSY PER MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 49,787 hrs · 40,743 cycles

DURING SCHEDULED SPV CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITONED SLIDE PER MT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 49,213 hrs · 40,323 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT OVERHEAD EMERGENCY EXIT LIGHT INOP AT ROW 2. REMOVED AND REPLACED LIGHT PER MM.

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 48,984 hrs · 40,151 cycles

DURING SCHEDULED HC1 CHECK, FOUND AFT EMERGENCY FLASHLIGHT STRAPS BROKEN. REMOVED AND REPLACED STRAPS PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 48,975 hrs · 40,146 cycles

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

Part: SIGN — LOOSE (CABIN) · airframe 47,742 hrs · 39,214 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 47,654 hrs · 39,143 cycles

DURING SCHEDULED MV1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: SLAT — DELAMINATED (LT WING) · airframe 47,314 hrs · 38,874 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND LT WING NR 2 SLAT O/B END DELAMINATED. REMOVED AND REPLACED NR 2 SLAT PER MM.

Part: SIGN — LOOSE (CABIN) · airframe 46,979 hrs · 38,610 cycles

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

Part: BLOWER — FAULTY (E&E BAY) · airframe 46,822 hrs · 38,493 cycles

AIR TURNBACK - EQUIP COOLING, OFF LIGHT ILLUMINATED. HEAT SMELL DISSIPATED IMMEDIATELY IN COCKPIT BUT LINGERED IN CABIN. FOUND NORMAL EQUIPMENT COOLING BLOWER AND CHECK VALVE BAD. REMOVED AND REPLACED BLOWER, CHECK VALVE AND HEPA FILTER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,644 hrs · 38,358 cycles

DURING SCHEDULED CV CHECK, FOUND SKIN CRACKED AT BS 1000, STR 5R. REPAIRED SKIN PER SRM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 46,015 hrs · 37,888 cycles

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

Part: FRAME — CORRODED (FUSELAGE) · airframe 45,850 hrs · 37,761 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CORRODED AT BS 767, BETWEEN STR 26L TO STR 26R. REPAIRED FRAME PER ER.

Part: FRAME — CORRODED (FUSELAGE) · airframe 45,850 hrs · 37,761 cycles

DURING SCHEDULED 14Y CHECK, FOUND AFT CARGO COMPARTMENT FRAME CORRODED AT BS 807, BETWEEN STR 26R TO STR 27R. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 45,850 hrs · 37,761 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CORRODED AT BS 787, BETWEEN STR 27R TO STR 26R. REPAIRED FRAME PER ER.

Part: FRAME — CORRODED (FUSELAGE) · airframe 45,850 hrs · 37,761 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CORRODED AT BS 787 BETWEEN STR 27L TO STR 27R. REPAIRED FRAME PER SRM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 45,850 hrs · 37,761 cycles

DURING SCHEDULED 14Y CHECK, FOUND L1 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM.

Part: SPOILER — DELAMINATED (RT WING) · airframe 45,850 hrs · 37,761 cycles

DURING SCHEDULED 14Y CHECK, FOUND RT WING NR 6 FLIGHT SPOILER DELAMINATED. REMOVED AND REPLACED SPOILER PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,850 hrs · 37,761 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 15R. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 44,250 hrs · 36,591 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING I/B FORE FLAP UPPER SURFACED DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,716 hrs · 35,517 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT EMERGENCY EXIT LIGHT INOP AT ROW 12. RELAMPED LIGHT PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,648 hrs · 35,471 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT EMERGENCY EXIT LIGHT INOP AT ROW 12. RELAMPED LIGHT PER MM.

Part: COVER — LOOSE (CABIN) · airframe 41,470 hrs · 34,616 cycles

RIGHT OVERWING EXIT LIGHT COVER LOOSE. REMOVED AND REPLACED EXIT LIGHT COVER PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,673 hrs · 34,029 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED SKIN PER SRM.

Part: BEARING — WORN (RT ELEVATOR) · airframe 40,651 hrs · 34,016 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,651 hrs · 34,016 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 40,651 hrs · 34,016 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SLAT — DELAMINATED (LT WING) · airframe 40,651 hrs · 34,016 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,651 hrs · 34,016 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 40,651 hrs · 34,016 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 40,651 hrs · 34,016 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 40,651 hrs · 34,016 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 40,651 hrs · 34,016 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 40,651 hrs · 34,016 cycles

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

Part: HOOK — LOOSE (GIRT BAR) · airframe 40,651 hrs · 34,016 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 40,651 hrs · 34,016 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,651 hrs · 34,016 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,651 hrs · 34,016 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,651 hrs · 34,016 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,651 hrs · 34,016 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,651 hrs · 34,016 cycles

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

Part: BATTERY — DISCHARGED (CABIN) · airframe 40,096 hrs · 33,615 cycles

DURING SCHEDULED SERVICE CHECK, FOUND AFT LT FUSELAGE EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: SLAT — DELAMINATED (RT WING) · airframe 39,753 hrs · 33,344 cycles

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

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 36,318 hrs · 30,624 cycles

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

Part: WINDOW — ARCED (COCKPIT) · airframe 35,944 hrs · 30,337 cycles

L2 WINDOW ARCING INFLIGHT, TURNED OFF L2 WINDOW HEAT ARCHING STOPPED. REMOVED AND REPLACED L2 WINDOW PER MM.

Part: BOLT — OUT OF POSITION (EVAC SLIDE) · airframe 34,112 hrs · 28,933 cycles

DURING SCHEDULED C2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE LATCH BOLT OUT OF POSITION. REPOSITIONED BOLT PER MM.

Part: BOLT — OUT OF POSITION (L2 DOOR SLIDE) · airframe 34,112 hrs · 28,933 cycles

DURING SCHEDULED C2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE LATCH BOLT OUT OF POSITION. REPOSITIONED BOLT PER MM.

Part: FLOORBEAM — CRACKED (BS 947) · airframe 30,271 hrs · 25,897 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FLOORBEAM CRACKED AT BS 947.5, LBL 53.5. REPAIRED FLOORBEAM IAW BFG ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,283 hrs · 28,287 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME INBD CHORD CRACKED AT BS 616, WL 202, RT SIDE. REPAIRED FRAME PER BFG ER.

Part: FITTING — CORRODED (HORIZONTAL STAB) · airframe 33,283 hrs · 28,287 cycles

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

Part: CREASE BEAM — CORRODED (BS 370-410) · airframe 33,283 hrs · 28,287 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE CREASE BEAM WEB CORRODED BETWEEN BS 370 TO BS 410, RBL 70. REPAIRED WEB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,283 hrs · 28,287 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT FWD CARGO DOOR CUTOUT, FWD FRAME NR 5 STOP FITTING. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (BS 867) · airframe 33,283 hrs · 28,287 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 907) · airframe 33,283 hrs · 28,287 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (BS 597) · airframe 33,282 hrs · 28,287 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 597, STR 3R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 685) · airframe 33,282 hrs · 28,287 cycles

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

Part: STRINGER CLIP — CRACKED (BS 727D) · airframe 33,283 hrs · 28,287 cycles

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

Part: STRINGER CLIP — CRACKED (BS 787) · airframe 33,283 hrs · 28,287 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 787, STR 4L. REMOVED AND REPLACED CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (BS 807) · airframe 33,283 hrs · 28,287 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 807, STR 4L. REMOVED AND REPLACED CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (BS 727E) · airframe 33,283 hrs · 28,287 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 727E, STR 4L. REMOVED AND REPLACED CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (BS 727C) · airframe 33,283 hrs · 28,287 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 727C, STR 4L. REMOVED AND REPLACED CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (BS 747) · airframe 33,283 hrs · 28,287 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 747, STR 4L. REMOVED AND REPLACED CLIP IAW SRM.

Part: CLIP — CRACKED (FUSELAGE) · airframe 33,283 hrs · 28,287 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 827, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: ANGLE — CORRODED (BS 270) · airframe 33,283 hrs · 28,287 cycles

DURING SCHEDULED D CHECK, FOUND COCKPIT FLOOR Z-CHORD CORRODED AT BS 270, LBL 10, WL 208. REMOVED AND REPLACED Z-CHORD IAW SRM.

Part: FRAME — CRACKED (BS 867) · airframe 33,283 hrs · 28,287 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME IAW SRM.

Part: CLIP — CRACKED (FUSELAGE) · airframe 33,283 hrs · 28,287 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 767, STR 4L. REMOVED AND REPLACED CLIP IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,283 hrs · 28,287 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 747) · airframe 33,283 hrs · 28,287 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME PER SRM.

Part: FLOORBEAM — CRACKED (BS 327) · airframe 33,283 hrs · 28,287 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FLOORBEAM STIFFENER CRACKED AT BS 327, RBL 35, WL 201. REPAIRED FLOORBEAM PER SRM.

Part: STRINGER — CRACKED (BS 867) · airframe 33,283 hrs · 28,287 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CRACKED AT BS 867, STR 4L. REPAIRED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (BS 867) · airframe 33,283 hrs · 28,287 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 867, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (BS 787) · airframe 33,283 hrs · 28,287 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (BS 847) · airframe 33,283 hrs · 28,287 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 847, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (BS 400) · airframe 33,283 hrs · 28,287 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 360) · airframe 33,283 hrs · 28,287 cycles

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

Part: SPLICE — CRACKED (BS 907) · airframe 33,283 hrs · 28,287 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER SPLICE CRACKED AT BS 907, STR 4L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,283 hrs · 28,287 cycles

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

Part: MIXER BOX — FAULTY (SPOILER) · airframe 30,649 hrs · 26,206 cycles

CREW REPORTS AILERONS BINDING. REMOVED AND REPLACED SPOILER MIXER AND RATIO CHANGER PER MM.

Part: SLIDE — LOOSE (R1 DOOR) · airframe 29,808 hrs · 25,546 cycles

R1 DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM.

Part: SKIN — WORN (FUSELAGE) · airframe 29,275 hrs · 25,128 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 875 TO BS 887, STRINGER 4L TO STRINGER 4R, WORN. REPAIRED SKIN PER ACO AND EA.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 28,337 hrs · 24,392 cycles

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

Part: STRIP — LOOSE (CABIN) · airframe 26,612 hrs · 23,021 cycles

ON LANDING F/A DISCOVERED EEPLS STRIP LOOSE. REPAIRED EEPLS STRIP PER MM.

Part: BEARING — WORN (RT ELEVATOR) · airframe 24,566 hrs · 21,354 cycles

DURING SCHEDULED C4 CHECK, SWA SI 11038-55, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED CONTROL ROD BEARING PER OHM.

Part: PIN — CORRODED (LT MLG) · airframe 23,654 hrs · 20,637 cycles

DURING SCHEDULED C3 CHECK, FOUND LT MLG TRUNION PIN CORRODED. REMOVED AND REPLACED TRUNION PIN PER MM.

Part: BUSHING — WORN (LT ELEVATOR) · airframe 21,403 hrs · 18,741 cycles

DURING SCHEDULED SERVICE CHECK, SWA SI 11111-55, FOUND LT ELEVATOR TAB NR 2 AND NR 3 HINGES WORN. REMOVED AND REPLACED LEFT ELEVATOR TAB NR 2 AND NR 3 HINGE BUSHINGS PER MM.

Part: BRACKET — LOOSE (FWD ENTRY DOOR) · airframe 21,211 hrs · 18,593 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR BRACKET LOOSE. SECURED BRACKET PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 20,988 hrs · 18,398 cycles

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

Part: SLIDE — OUT OF ADJUST (FWD ENTRY DOOR) · airframe 20,814 hrs · 18,263 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SLIDE — LOOSE (FWD ENTRY DOOR) · airframe 20,822 hrs · 18,270 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE LOOSE IN CONTAINER. SECURED SLIDE PER MM.

Part: SKIN — DELAMINATED (LT T/E FLAP) · airframe 17,160 hrs · 15,208 cycles

DURING SCHEDULED 1/2D CHECK, FOUND LT WING T/E OUTBOARD AFT FLAP DELAMINATED AT INBOARD SIDE. REMOVED AND REPLACED AFT FLAP PER MM.

Part: SKIN — DELAMINATED (LT T/E FLAP) · airframe 17,160 hrs · 15,208 cycles

DURING SCHEDULED 1/2D CHECK, FOUND LT WING INBOARD T/E AFT FLAP DELAMINATED AT OUTBOARD SIDE. REMOVED AND REPLACED AFT FLAP PER MM.

Part: GUSSET — CRACKED (SVC DOOR) · airframe 17,160 hrs · 15,208 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FWD SVC DOOR AFT LOWER GUSSET CRACKED AT OUTBD FASTENER HOLE. REPAIRED GUSSET PER BAC DWG.

Part: FRAME — CRACKED (SVC DOOR) · airframe 17,160 hrs · 15,208 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FWD SVC DOOR AFT LOWER FRAME CRACKED, OUTBD OF 3RD FASTENER HOLE. REPAIRED FRAME PER BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 17,160 hrs · 15,208 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STR CLIP CRACKED AT BS 580, STR 11R. REMOVED AND REPLACED STR CLIP PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,456 hrs · 12,916 cycles

DURING SCHEDULED C1 CHECK, FOUND EMERGENCY EXIT LIGHT AT FWD ENTRY INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: BRACKET — LOOSE (ESCAPE SLIDE)

DURING SCHEDULED C4 CHECK, FOUND FWD ENTRY DOOR EVACUATION SLIDE GIRT BAR STOWAGE BRACKET LOOSE. REMOVED AND REPLACED BRACKET FASTENER PER MM.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED SPECIAL VISIT, FOUND EEPLS INOP AT FWD SECTION. TIGHTENED LIGHTING CONNECTOR PER MM. OPS CK GOOD..

Part: BRACKET — LOOSE (SLIDE)

FWD SERVICE DOOR EVACUATION SLIDE GIRT BAR AFT MOUNT BRACKET LOOSE. REMOVED AND REPLACED BRACKET ASSY PER MM.

Part: SLIDE — DETACHED (FWD ENTRY)

FWD ENTRY DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM.

Part: SIGN — BROKEN (PASSENGER DOOR)

DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EXIT SIGN LENS BROKEN. REMOVED AND REPLACED SIGN PER MM.

Part: SKIN — HOLE (FUSELAGE)

DURING SCHEDULED SERVICE CHECK, FOUND A 1 INCH HOLE IN FUSELAGE SKIN AFT OF AFT SERVICE DOOR. REPAIRED PER BOEING SRM.