N615SW

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 67,840 hrs · 53,927 cycles

FORWARD CARGO DOOR CUTOUT FORWARD CORNER SCUFF PLATE CRACKED. REPAIRED SCUFF PLATE PER EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 67,840 hrs · 53,927 cycles

STRINGER CRACKED AT BS 867, STR 24L. REPAIRED STRINGER IAW DWG.

Part: HINGE — CRACKED (RT SPOILER) · airframe 67,343 hrs · 53,560 cycles

RT WING NR 5 GROUND SPOILER SECOND HINGE FROM INBOARD SIDE CRACKED. R&R SPOILER PER AMM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 67,343 hrs · 53,560 cycles

BULKHEAD STRINGER CRACKED AT BS 663, STR 6R. REPAIRED STRINGER PER SRM.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 66,250 hrs · 52,832 cycles

NUMBER 5 LE SLAT DELAMINATED AFT OTBD UPPER SURFACE. R & R SLAT IAW MM.

Part: SLIDE — OPEN (L1 DOOR) · airframe 66,004 hrs · 52,675 cycles

L1 DOOR ESCAPE SLIDE CONTAINER OPEN. R & R SLIDE IAW MT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,808 hrs · 52,538 cycles

FUSELAGE SKIN CRACKED AT BS 952, STRINGER 11R. REPAIRED SKIN IAW EA.

Part: ENGINE — STALLED (LEFT) · airframe 65,776 hrs · 52,520 cycles

DIVERSION & INFLIGHT SHUTDOWN. DECLARED EMER INFLIGHT, AT FL 330 CRUISE NOTICED AN AIRFRAME VIBRATION WITH NO INCREASE IN ENG VIBRATION GAUGES. SMALL COMPRESSOR STALL POP & LT ENG ROLLED BACK TO 50% N2 HAD MOMENTARY SMELL OF SMOKE VIBRATION, CONTINUED WITH LT THRUST LEVER AT IDLE LT ENG SECURED. R & R NR 1 ENG IAW MT.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 65,000 hrs · 52,012 cycles

RIGHT WING NR 6 LE SLAT UPPER SKIN DELAMINATED. REPAIRED SLAT IAW SRM.

Part: SLAT — DELAMINATED (LT WING) · airframe 64,973 hrs · 51,991 cycles

LEFT WING NR 2 LE SLAT DELAMINATED. R & R SLAT ASSEMBLY IAW MM.

Part: WIRE HARNESS — FAULTY (NR 1 ENGINE) · airframe 64,839 hrs · 51,901 cycles

ON CLIMB OUT, ABOUT 6 - 7K WITH POWER SET FOR CLIMB THRUST, NR 1 EGT FLUCTUATED UP TO 1018 EGT SEVERAL TIMES, THEN BACK. ENG VIB ALSO JUMPED TO ABOUT 1.8. R & R NR 1 ENG HARNESS UPPER RT IAW AMM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 64,432 hrs · 51,615 cycles

L1 DOOR EMER EVAC SLIDE OUT OF ADJUSTMENT. ADJUSTED SLIDE IAW MT.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 63,550 hrs · 50,981 cycles

FORWARD CARGO COMPARTMENT KEEL BEAM CORRODED BETWEEN BS 500 TO 540, STRINGER 28L. REPAIRED KEEL BEAM IAW SRM & DWG.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 63,550 hrs · 50,981 cycles

FORWARD CARGO COMPARTMENT KEEL BEAM CORRODED BETWEEN BS 520 - 520+6, STRINGER 28L. REPAIRED KEEL BEAM IAW SRM & DWG.

Part: ANGLE — CRACKED (LT WING) · airframe 63,550 hrs · 50,981 cycles

LEFT WING AFT TRACK FAIRING ANGLE CRACKED ON OTBD SIDE. R & R ANGLE IAW SRM & DWG.

Part: FRAME — CRACKED (LT PYLON) · airframe 63,550 hrs · 50,981 cycles

LEFT WING AFT PYLON FRAME CRACKED AT BS 363.65. R & R FRAME IAW SRM & DWG.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 63,550 hrs · 50,981 cycles

AFT CARGO COMPARTMENT AREA SUPPORT CLIP CRACKED AT BS 807, STRINGER 25R. R & R CLIP IAW SRM & DWG.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 63,550 hrs · 50,981 cycles

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

Part: SKIN — CORRODED (FUSELAGE) · airframe 63,550 hrs · 50,981 cycles

KEEL BEAM SKIN ASSEMBLY CORRODED BETWEEN BS 607 TO 630, BETWEEN LBL 6.30 - RBL 6.30. REPAIRED SKIN IAW EO & EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 63,550 hrs · 50,981 cycles

JOGGLE AREA OF CHANNEL CORRODED AT BS 767+5, LBL 8.10. REPAIRED JOGGLE IAW EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 63,550 hrs · 50,981 cycles

JOGGLE AREA OF CHANNEL CORRODED AT BS 767+5, RBL 3. REPAIRED JOGGLE IAW EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 63,550 hrs · 50,981 cycles

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

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 63,550 hrs · 50,981 cycles

L2 DOOR STUB FRAME CRACKED AT BS 947.5+11, STRINGER 17L. REPAIRED STUB FRAME IAW EO & EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 63,550 hrs · 50,981 cycles

CHANNEL CORRODED AT BS 767+5, LBL 3.0. REPAIRED CHANNEL IAW EA.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 63,550 hrs · 50,981 cycles

LEFT WING INBD FORE FLAP DELAMINATED ON UPPER SKIN AT 49.50 FROM OTBD EDGE. REPAIRED FORE FLAP IAW SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 63,550 hrs · 50,981 cycles

AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 767+5, RBL 8.10. REPAIRED CHANNEL IAW EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 63,550 hrs · 50,981 cycles

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

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 63,550 hrs · 50,981 cycles

STRINGER SPLICE CRACKED AT BS 360, STRINGER 4L. R & R SPLICE IAW EO & EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,550 hrs · 50,981 cycles

AFT CARGO COMPARTMENT FRAME CORRODED AT BS 747, BETWEEN STRINGER 26L TO 27L. REPAIRED FRAME IAW SRM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 63,550 hrs · 50,981 cycles

LEFT WING INBD FORE FLAP DELAMINATED ON UPPER SKIN. REPAIRED FORE FLAP IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,550 hrs · 50,981 cycles

AFT CARGO COMPARTMENT FRAME CORRODED AT BS 787, BETWEEN STRINGER 27L - 27R. REPAIRED FRAME IAW SRM & DWG.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 63,550 hrs · 50,981 cycles

STUB FRAME CRACKED AT BS 947+11, STRINGER 17R, 9 O CLOCK AFT GALLEY DOOR. REPAIRED STUB FRAME IAW EA.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 63,550 hrs · 50,981 cycles

LEFT WING INBD FORE FLAP DELAMINATED ON UPPER SKIN. REPAIRED FORE FLAP IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,550 hrs · 50,981 cycles

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

Part: FITTING — CRACKED (FUSELAGE) · airframe 63,550 hrs · 50,981 cycles

ANGLE CLIP CRACKED AT BS 323.7, STRINGER 21L. R & R ANGLE CLIP IAW SRM & DWG.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 63,550 hrs · 50,981 cycles

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

Part: FITTING — CRACKED (FUSELAGE) · airframe 63,550 hrs · 50,981 cycles

CLIP CRACKED AT BS 294.5, STRINGER 23L. R & R CLIP IAW SRM & DWG.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 63,550 hrs · 50,981 cycles

AFT CARGO COMPARTMENT CHANNEL CRACKED AT BS 727E, LBL 3.0. REPAIRED CHANNEL IAW SRM & DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 63,550 hrs · 50,981 cycles

CHANNEL CORRODED AT BS 727D+5, LBL 3.0. REPAIRED CHANNEL IAW EA.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 63,550 hrs · 50,981 cycles

AFT CARGO COMPARTMENT STIFFENER CRACKED AT BS 727, STRINGER 27R. R & R STIFFENER IAW SRM & DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 63,550 hrs · 50,981 cycles

SHEAR TIE CORRODED AT BS 947.5, BETWEEN STRINGER 26L TO 27L. R & R SHEAR TIE IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,550 hrs · 50,981 cycles

AFT CARGO COMPARTMENT FRAME CRACKED AT BS 727D, BETWEEN STRINGER 26L TO 27L. REPAIRED FRAME IAW SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 63,550 hrs · 50,981 cycles

FORWARD CABIN FLOOR STRUCTURE STRAP CRACKED BETWEEN BS 294.5+10 TO 344+5, LBL 10. R & R STRAP IAW SRM & DWG.

Part: CHANNEL — CORRODED (BS 727D) · airframe 63,550 hrs · 50,981 cycles

FOUND A CHANNEL CORRODED AT BS 727D+5, LBL 8.1. REPAIRED THE CHANNEL IAW EA.

Part: STRAP — CRACKED (FUSELAGE) · airframe 63,550 hrs · 50,981 cycles

FORWARD CABIN FLOOR STRUCTURE STRAP CRACKED BETWEEN BS 294.5+10 TO 344+5, RBL 34. R & R STRAP IAW SRM & DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,550 hrs · 50,981 cycles

AFT CARGO COMPARTMENT FRAME CORRODED AT BS 787, BETWEEN STRINGER 26L TO 27L. REPAIRED FRAME IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,550 hrs · 50,981 cycles

INTERCOSTAL WEB CRACKED AT BS 277, STRINGER 14R. R & R WEB IAW SRM & DWG.

Part: STRAP — CRACKED (FUSELAGE) · airframe 63,550 hrs · 50,981 cycles

FORWARD CABIN FLOOR STRUCTURE STRAP CRACKED BETWEEN BS 294.5+10 TO 344+5, BL 0. R & R STRAP IAW SRM & DWG.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 63,550 hrs · 50,981 cycles

AFT CARGO COMPARTMENT STIFFENER CRACKED AT BS 727, STRINGER 27L. R & R STIFFENER IAW SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 63,550 hrs · 50,981 cycles

FORWARD CABIN FLOOR STRUCTURE STRAP CRACKED BETWEEN BS 294.5+10 TO 344+5, LBL 48. R & R STRAP IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,550 hrs · 50,981 cycles

ANGLE CRACKED BETWEEN BS 927 TO 947.5, BL 0. R & R ANGLE IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,550 hrs · 50,981 cycles

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

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,550 hrs · 50,981 cycles

AFT CARGO COMPARTMENT ANGLE OF WEB CRACKED AT BS 947.5, BETWEEN STRINGER 24L - 25L. R & R ANGLE IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,550 hrs · 50,981 cycles

FORWARD CARGO COMPARTMENT CLIP ANGLE CRACKED AT BS 540, LBL 2. R & R CLIP ANGLE IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,550 hrs · 50,981 cycles

AFT CARGO COMPARTMENT ANGLE CRACKED BETWEEN BS 887 - 907, RBL 46. R & R ANGLE IAW SRM & DWG.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 63,550 hrs · 50,981 cycles

FORWARD CARGO COMPARTMENT KEEL BEAM CORRODED AT BS 500D+7.5, STRINGER 28L. REPAIRED KEEL BEAM IAW SRM & DWG.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 63,550 hrs · 50,981 cycles

FORWARD CARGO COMPARTMENT SUPPORT CLIP CRACK AT BS 380, STRINGER 26L. R & R CLIP IAW SRM & DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 63,550 hrs · 50,981 cycles

FORWARD CARGO COMPARTMENT WEB CRACKED AT BS 440, BETWEEN STRINGER 26R - 25R. R & R WEB IAW SRM & DWG.

Part: SKIN — CRACKED (RT WING) · airframe 63,550 hrs · 50,981 cycles

RIGHT WING FIXED LE UPPER SKIN CRACKED AT WBL 157. REPAIRED SKIN IAW EA.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 63,550 hrs · 50,981 cycles

FORWARD CARGO COMPARTMENT SUPPORT CLIP CRACK AT BS 380, STRINGER 26R. R & R CLIP IAW SRM & DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 63,550 hrs · 50,981 cycles

FLOORBEAM CRACKED AT BS 344, LBL 9. REPAIRED FLOORBEAM IAW SRM.

Part: BRACKET — CRACKED (RT WING) · airframe 63,550 hrs · 50,981 cycles

RIGHT WING TE BRACKET CRACKED AT WS 531. REPLACED BRACKET IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,550 hrs · 50,981 cycles

FRAME CRACKED AT BS 440, STRINGER 24R. R & R FRAME IAW SRM & DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 63,550 hrs · 50,981 cycles

FLOORBEAM WEB CRACKED AT BS 639, RBL 45.5. REPAIRED WEB IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,550 hrs · 50,981 cycles

FLOORBEAM UPPER CHORD FLANGE AT CORRODED AT BS 986.5, BETWEEN RBL 5 - 43. REPAIRED CHORD IAW EO & EA.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 63,550 hrs · 50,981 cycles

FUSELAGE Z ANGLE CORRODED AT STATION 986.5+4, RBL 47, WL 207. R & R ANGLE IAW SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 63,550 hrs · 50,981 cycles

WEB CORRODED BETWEEN BS 847 - 867, STRINGER 17L. R & R WEB IAW SRM & DWG.

Part: SKIN — CRACKED (L2 DOOR) · airframe 63,550 hrs · 50,981 cycles

L2 DOOR SKIN CRACKED AT BS 947.5+12, STRINGER 17L, LOWER FWD CORNER. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,550 hrs · 50,981 cycles

R1 DOOR AFT LOWER CORNER SKIN CRACKED AT BS 312+15, STRINGER 17R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,550 hrs · 50,981 cycles

R2 DOOR CUT OUT SKIN CRACKED AT BS 947.5+12, STRINGER 17R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,550 hrs · 50,981 cycles

AFT ENTRY DOOR LOWER FWD CORNER, SKIN CRACKED BETWEEN BS 947.5 TO 967+10, BETWEEN STRINGER 16L TO 19L. REPAIRED SKIN IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 63,550 hrs · 50,981 cycles

FLOORBEAM CRACKED AT STATION 708, LBL 24.8. REPAIRED BEAM IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 63,550 hrs · 50,981 cycles

FLOORBEAM CRACKED AT STATION 698 - 717, LBL 24.8. REPAIRED BEAM IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,550 hrs · 50,981 cycles

R1 DOOR LOWER CORNER BEAR STRAP SKIN CRACKED AT BS 312+15.5", STRINGER 17R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,550 hrs · 50,981 cycles

R1 DOOR EXTERNAL BEAR STRAP CUT OUT SKIN CRACKED AT BS 312+15, STRINGER 17R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,550 hrs · 50,981 cycles

R2 DOOR SKIN LOWER FWD CORNER CUT OUT CRACKED AT BS 947.5+10", STRINGER 17R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,550 hrs · 50,981 cycles

R1 DOOR FUSELAGE SKIN CRACKED AT BS 328, STRINGER 17R. REPAIRED SKIN IAW EO & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,550 hrs · 50,981 cycles

LEFT UPPER CORNER OF WINDOW POST C - D SKIN LOCATED CRACKED AT BS 219.8. REPAIRED SKIN IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 63,550 hrs · 50,981 cycles

LONGITUDINAL FLOORBEAM CRACKED AT STATION 707, LBL 24.8. REPAIRED FLOORBEAM IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 63,550 hrs · 50,981 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 663.75+3, RBL 24.8. REPAIRED CHORD IAW EO & EA.

Part: SPAR — CRACKED (RT WING) · airframe 63,550 hrs · 50,981 cycles

RIGHT WING REAR SPAR UPPER CHORD CRACKED AT RSS 215.97+5.9", AFT SUPPORT FITTING. REPAIRED CHORD IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 63,550 hrs · 50,981 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 663.75+7, RBL 24.8. REPAIRED CHORD IAW EO & EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 63,550 hrs · 50,981 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 663.75, LBL 24.8. REPAIRED CHORD IAW EO & EA.

Part: SPAR — CRACKED (LT WING) · airframe 63,550 hrs · 50,981 cycles

LEFT WING REAR SPAR UPPER CHORD CRACKED AT RSS 215.97+5.9", AFT SUPPORT FITTING. REPAIRED CHORD IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 63,550 hrs · 50,981 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 663.75+7, LBL 24.8. REPAIRED CHORD IAW EO & EA.

Part: SIGN — UNSECURE (CABIN) · airframe 63,549 hrs · 50,980 cycles

FORWARD EXIT SIGN FELL OFF. R & R SIGN ASSEMBLY IAW AMM.

Part: VSI — INOPERATIVE (COCKPIT) · airframe 63,494 hrs · 50,944 cycles

DIVERSION & DECLARED EMER. FIRST OFFICER'S VSI BLANK. R & R VERTICAL SPEED INDICATOR IAW AMM.

Part: LOCK — LOOSE (R1 DOOR) · airframe 63,436 hrs · 50,902 cycles

R1 DOOR AFT SLIDE LOCK LOOSE. SECURED LOCK ASSEMBLY IAW SIP.

Part: PUMP — MALFUNCTIONED (NR 1 ENGINE) · airframe 63,079 hrs · 50,650 cycles

AIR TURN BACK, ENG SHUTDOWN & DECLARED EMER AT 36,000'. WHILE CROSS FEEDING NR 1 ENG FLAME OUT. R & R NR 1 ENG DRIVEN FUEL PUMP IAW MT.

Part: LENS — LOOSE (CABIN) · airframe 62,857 hrs · 50,500 cycles

RIGHT BULLNOSE EMER LIGHT LENS LOOSE AT ROW 5. SECURED LENS IAW AMM.

Part: LENS — LOOSE (EXIT SIGN) · airframe 62,010 hrs · 49,956 cycles

LEFT OVERWING EMER EXIT SIGN LENS LOOSE. SECURED LENS IAW MM.

Part: DOOR FRAME — CRACKED (R1 DOOR) · airframe 61,592 hrs · 49,672 cycles

R1 DOOR CRACKED LOWER EDGE FRAME CRACKED AT AFT LOWER CORNER STOP FITTING. R & R DOOR IAW AMM.

Part: ANGLE — CRACKED (LT WING) · airframe 61,592 hrs · 49,672 cycles

LEFT WING UPPER WING SUPPORT UNDER PANEL 5735 26 INCHES AFT RS & 8 UP FROM NR 3 FLAP TRACK ANGLE CRACKED. R & R ANGLE IAW SRM.

Part: ANGLE — CRACKED (LG WW) · airframe 61,592 hrs · 49,672 cycles

LEFT WW CUT OUT FWD CURVED ANGLE CRACKED ON TOP CORNER. R & R ANGLE IAW SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 61,592 hrs · 49,672 cycles

E & E COMPARTMENT FLOOR SUPPORT STRAP CRACKED AT BS 328 RT SIDE. REPAIRED STRAP IAW SRM.

Part: LENS — MISSING (CABIN) · airframe 60,832 hrs · 49,104 cycles

LEFT EMER EXIT BULLNOSE LIGHT LENS MISSING AT ROW 14. INSTALLED LENS IAW AMM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 60,721 hrs · 49,017 cycles

L1 DOOR EMER EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW AMM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 60,721 hrs · 49,017 cycles

R1 DOOR EMER EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW AMM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 60,376 hrs · 48,771 cycles

R1 DOOR EMERGENCY EXIT SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.

Part: GASPER FAN — FAULTY (AC BAY) · airframe 60,216 hrs · 48,654 cycles

DURING DESCENT AT 6000. WE GOT A BURNING SMOKE. TURN OFF GASPER & THE BURNING SMELL WENT AWAY. FOUND GASPER FAN FAULTY. R & R GASPER FAN IAW MM.

Part: SIGN — LOOSE (CABIN) · airframe 59,772 hrs · 48,358 cycles

LT OVERWING EXIT SIGN LOOSE. SECURED EXIT SIGN IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 59,709 hrs · 48,312 cycles

LT OVERWING EMERGENCY EXIT DOOR SIDE WALL LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: SKIN — CRACKED (LE SLAT) · airframe 63,550 hrs · 50,981 cycles

NUMBER 1 LE SLAT SKIN CRACKED AT LOWER SURFACE. REPAIRED SLAT IAW SRM.

Part: ACTUATOR — FAILED (LE FLAP) · airframe 57,801 hrs · 46,920 cycles

AIR TURNBACK, LE FLAP TRANSIT LIGHT STAYED ON AFTER FLAP RETRACTION. RECYCLED FLAPS IAW QRH, ROLL NOTED AFTER RECYCLE. ON WALK AROUND FOUND NR 2 LE FLAP EXTENDED. R&R NR 2 LE FLAP ACTUATOR IAW MM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 57,617 hrs · 46,776 cycles

LEFT WING INBD T/E FORE FLAP UPPER SURFACE DELAMINATED. REPAIRED FORE FLAP IAW SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 57,617 hrs · 46,776 cycles

VERTICAL BEAM PRESSURE BULKHEAD WEB CRACKED AT 178, LBL 17.0. REPAIRED WEB IAW SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 57,617 hrs · 46,776 cycles

VERTICAL BEAM WEB CRACKED AT BS 178, LBL 5.7. REPAIRED WEB IAW SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 57,617 hrs · 46,776 cycles

PRESSURE BULKHEAD VERTICAL BEAMS CRACKED AT BS 178, RBL 17.0. REPAIRED WEB IAW SRM.

Part: SUPPORT — CRACKED (RT WING) · airframe 57,617 hrs · 46,776 cycles

RIGHT WING UPPER SURFACE, 2 EA NYLON NUTPLATE SUPPORTS FOR PANEL 58710R CRACKED. R & R SUPPORTS IAW SRM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 57,617 hrs · 46,776 cycles

L1 DOOR SURROUND STRUCTURE FWD WEB ANGLE CRACKED AT STA 348.2, STR 16L. R & R ANGLE IAW SRM AND DWG.

Part: PANEL — CRACKED (LT PYLON) · airframe 57,617 hrs · 46,776 cycles

LEFT WING UPPER SURFACE PYLON NUTPLATE SUPPORT FOR PANEL NR 57710L CRACKED. R & R PANEL IAW SRM AND DWG.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 57,617 hrs · 46,776 cycles

FORWARD ENTRY DOOR SURROUND STRUCTURE ATTACH CLIP CRACKED AT STA 360, STR 11L. R & R CLIP IAW DWG AND SRM.

Part: ANGLE — CRACKED (RT WING) · airframe 57,617 hrs · 46,776 cycles

RT WING OTBD AFT RIB ANGLE CRACKED AT RSS 533+12. R & R ANGLE IAW SRM & DWG.

Part: ANGLE — CRACKED (LT AILERON) · airframe 57,617 hrs · 46,776 cycles

LEFT WING T/E INBD AILERON RIB STRUCTURE ATTACH ANGLE CRACKED AT RSS 545. R & R ANGLE IAW SRM & DWG.

Part: SKIN — CRACKED (LE SLAT) · airframe 57,617 hrs · 46,776 cycles

RIGHT WING NUMBER 6 SLAT LOWER SURFACE AFT FASTENER ROW CRACKED AT 4 FASTENER HOLES, JUST INBOARD OF INBOARD AUX TRACK. REPAIRED SKIN IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 57,617 hrs · 46,776 cycles

WEB CRACKED AT BS 666, LBL 24.5. REPAIRED WEB IAW EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 57,617 hrs · 46,776 cycles

LEFT WING NR 2 SLAT LOWER SURFACE AFT FASTENER ROW CRACKED AT FASTENER HOLE AT OTBD AUX TRACK. REPAIRED NR 2 SLAT IAW AMM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 57,617 hrs · 46,776 cycles

FORWARD ENTRY DOOR SURROUND STRUCTURE, L-ANGLE CLIP ON UNDER SIDE OF WEB CRACKED AT STA 348.20, STR 15L. R & R L ANGLE IAW SRM AND DWG.

Part: PRESSURE DECK — CRACKED (FUSELAGE) · airframe 57,617 hrs · 46,776 cycles

PRESSURE DECK CRACKED BETWEEN STA 663 & STA 675, BETWEEN RBL 24 & RBL 45. R & R PRESSURE DECK IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,617 hrs · 46,776 cycles

LEFT MAIN WHEEL WELL FRAME FWD FLANGE CRACKED AT STA 727, STR 18A. REPAIRED CHORD IAW SWA EA.

Part: FRAME — CRACKED (RT MLG WW) · airframe 57,617 hrs · 46,776 cycles

RIGHT MAIN WW FRAME FWD FLANGE FWD LOWER CHORD CRACKED AT STA 727. STRINGER 18A. REPAIRED CHORD IAW SWA EA.

Part: PRESSURE DECK — CRACKED (FUSELAGE) · airframe 57,617 hrs · 46,776 cycles

PRESSURE DECK CRACKED BETWEEN STA 663 & 675, LBL 24 & LBL 45. R & R DECK IAW EA.

Part: LIGHT — INOPERATIVE (R1 DOOR) · airframe 56,784 hrs · 46,194 cycles

L1 AND R1 DOOR SLIDE LIGHTS INOP. REMOVED AND RELAMPED L1 AND R1 DOOR EMERGENCY SLIDE LIGHT IAW B737 AMM 33-51-22. OPS CHECKED OK IAW B737-300 AMM 33-51-22.

Part: LIGHT — INOPERATIVE (L1 DOOR) · airframe 56,784 hrs · 46,194 cycles

L1 AND R1 DOOR SLIDE LIGHTS INOP. REMOVED AND RELAMPED L1 AND R1 DOOR EMERGENCY SLIDE LIGHT IAW B737 AMM 33-51-22. OPS CHECKED OK IAW B737-300 AMM 33-51-22.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,784 hrs · 46,194 cycles

FASTENER HOLE CRACKED STA 500 S14R LAP LOWER ROW. REPAIRED FASTENER HOLE STA 500 S-14R LAP LOWER ROW IAW REO G15883 REV IR & EA 1-353-21616 REV - . FACT AS A RESULT OF POST REPAIR INSPECTION

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,784 hrs · 46,194 cycles

2EA FASTENER HOLES CRACKED STA 380 S14R LAP LOWER ROW. REPAIRED CRACKED FASTENER HOLES STA 380 S-14R LAP LOWER ROW IAW REO G15887 REV IR & EA 1-353-21612 REV -.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 56,784 hrs · 46,194 cycles

STA 908 S4R FACTORY STRINGER SPLICE CRACKED AT F FASTENER HOLE. REMOVED AND REPLACED STRINGER SPLICE AT STA 908 STR 4R IAW BAC DWG 65C35772 AND B737 SRM 51-40-02.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 56,784 hrs · 46,194 cycles

CRACKED FASTENER HOLE IN STRINGER STA 767 S1 DUE TO INCOMING REPAIR DOUBLER. C/W EA 1-353-21494 REV- & REO G15870 REV IR AT STA 767 S1 FACT AS A RESULT OF POST REPAIR INSPECTION

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,784 hrs · 46,194 cycles

RIGHT BS 807+10 LOWER FORWARD WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 3, 9. REPAIRED RIGHT BS 807 +10 LOWER FORWARD WINDOW CORNER IAW SB 737-53-1306 REV 2 AS PER TASK CARD 10074, STEP 8. FACT AS A RESULT OF POST REPAIR INSPECTION.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,784 hrs · 46,194 cycles

RIGHT BS 787+10 UPPER WINDOW SKIN CUTOUT CRACKED AT HOLE 2. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,784 hrs · 46,194 cycles

RIGHT BS 827+10 UPPER AFT WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 2 ,3. REPAIRED RIGHT BS 827 +10 UPPER AFT WINDOW CORNER IAW SB 737-53-1306, R2, SECT 3.B.3 AS PER TASK CARD 10074, STEP 8.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,784 hrs · 46,194 cycles

LEFT BS 767+10 UPPER AFT WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 2, 3. REPAIRED LEFT BS 767 +10 UPPER AFT WINDOW CORNER IAW EA 1-353-21599 REV - , REO G15846 REV IR.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,784 hrs · 46,194 cycles

LEFT BS 787+10 UPPER AFT WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 1, 2, 3, 5. LEFT BS 787+10 UPPER AFT WINDOW CORNER SKIN CRACKS AT HOLES 3, 5 INCORPORATED INTO REPAIR ACCOMPLISHED ON NRC M026522 IAW EA -353-21599 REV -, REO-G15846 REV IR.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,784 hrs · 46,194 cycles

LEFT BS 887+10 UPPER AFT WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLE NR 2. LEFT BS 887+10 UPPER AFT WINDOW, SKIN CRACK AT HOLE NR 2 INCORPORATED INTO REPAIR ACCOMPLISHED ON NRC M026522 IAW EA 1-353-21617 REV -, REO-G15845 REV IR.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,784 hrs · 46,194 cycles

RIGHT BS 887+10 UPPER AFT WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 2, 3. REPAIRED RIGHT BS 887+10 UPPER AFT WINDOW CORNER IAW EA 1-353-21546 REV-, REO G15851 REV IR FACT AS A RESULT OF POST REPAIR INSPECTION.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,784 hrs · 46,194 cycles

LEFT BS 867+10 UPPER AFT WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 2, 3, 6. REPAIRED LEFT BS 867 +10 UPPER AFT WINDOW CORNER IAW EA 1-353-21617 REV - , REO G15845 REV IR.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,784 hrs · 46,194 cycles

RIGHT BS 867+10 LOWER FORWARD WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 2, 3, 9. REPAIRED RIGHT BS 867 +10 LOWER FORWARD WINDOW IAW SB 737-53-1306 R2 SECT 3.B.3. AS PER TASK CARD 10074, STEP 8. FACT AS A RESULT OF POST REPAIR INSPECTION.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,784 hrs · 46,194 cycles

RIGHT BS 727D+10 LOWER FORWARD WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLE NR 3. REPAIRED RIGHT BS 727D+10 LOWER FORWARD WINDOW CORNER IAW EA 1-353-21527 REV-, REO G15850 REV IR FACT AS A RESULT OF POST REPAIR INSPECTION.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,784 hrs · 46,194 cycles

LEFT BS 727+10 UPPER AFT WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 4, 5, 7. REPAIRED LEFT BS 727 +10 UPPER AFT WINDOW CORNER IAW EA 1-353-21514 REV - , REO G15847 REV IR. FACT AS A RESULT OF POST REPAIR INSPECTION.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,784 hrs · 46,194 cycles

LEFT BS 827+10 UPPER AFT WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 2, 3, 7. REPAIRED LEFT BS 827 +10 UPPER AFT WINDOW CORNER IAW BOEING SB 737-53-1306 REV 2 AND TASK CARD 10075, STEP 8. FACT AS A RESULT OF POST REPAIR INSPECTION

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,784 hrs · 46,194 cycles

RIGHT BS 807+10 UPPER AFT WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 2, 3. REPAIRED RIGHT BS 807+10 UPPER AFT WINDOW CORNER IAW SB737-53-1306 REV 2 SECT 3.B.3 AS PER TASK CARD 10074 STEP 8 FACT AS A RESULT OF POST REPAIR INSPECTION

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,784 hrs · 46,194 cycles

LEFT BS 807+10 UPPER WINDOW SKIN CUTOUT CRACKED AT HOLES 2, 3, 4, 6, 7, 9. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,784 hrs · 46,194 cycles

LEFT BS 767+10 LOWER FORWARD WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 2, 3. REPAIRED LEFT BS 767 +10 LOWER FORWARD WINDOW CORNER IAW BOEING SB 737-53-1306 REV 2 SECT 3.B.3. PER TASK CARD 10075, REV 3 STEP 8.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,784 hrs · 46,194 cycles

LEFT BS 887+10 LOWER FORWARD WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 2, 3. REPAIRED LEFT BS 887+10 LOWER FORWARD WINDOW CORNER IAW BOEING SB737-53-1306 REV 2 AND TASK CARD 10075 STEP 8 FACT AS A RESULT OF POST REPAIR INSPECTION.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,784 hrs · 46,194 cycles

RIGHT BS 767+10 LOWER FORWARD WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 3 ,4. REPAIRED RIGHT BS 767 +10 LOWER FORWARD WINDOW CORNER IAW SB 737-53-1306 R2 SECT 3.B.3 AS PER TASK CARD 10074, STEP 8.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,784 hrs · 46,194 cycles

RIGHT BS 867+10 UPPER AFT WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 2, 3, 4. REPAIRED RIGHT BS 867 +10 UPPER AFT WINDOW CORNER IAW SB 737-53-1306 REV 2 SECT 3.B.3 AS PER TASK CARD 10074, STEP 8. FACT AS A RESULT OF POST REPAIR INSPECTION.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,784 hrs · 46,194 cycles

RIGHT BS 787+10 LOWER FORWARD WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLE NR 2. REPAIRED RIGHT BS 787+10 LOWER FORWARD WINDOW CORNER IAW SB737-53-1306 REV 2 SECT 3.B.3 AS PER TASK CARD 10074 STEP 8 FACT AS A RESULT OF POST REPAIR INSPECTION

Part: SIGN — LOOSE (CABIN) · airframe 56,630 hrs · 46,088 cycles

OVERWING EXIT "EXIT" SIGN CAPTAIN SIDE LOOSE. RE-ATTACHED CAPT SIDE "EMERGENCY EXIT" SIGN AT OVERWING EXIT AS PER AMM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 56,539 hrs · 46,015 cycles

STRINGER TIE CLIP CRACKED AT BS 867 AT S-4R. REMOVED AND REPLACED TIE CLIP AT BS 867 AT 4R REF SRM 51-40-02.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,539 hrs · 46,015 cycles

FOUND INDICATION OF 1.5" SUBSURFACE SKIN CRACK AT BS 727E + 6" ABOVE STR 2R. REPAIRED PER EA 1-353-21145 FACT AS A RESULT OF POST REPAIR INSPECTION

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,539 hrs · 46,015 cycles

FOUND INDICATION OF SUBSURFACE CRACK ABOVE S10 L AT BS S10 + 8. C/W EA # 1-A53-5808.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,539 hrs · 46,015 cycles

FOUND INDICATION OF 2.75" SUBSURFACE SKIN CRACK AT BS 867 + 10" ABOVE STR 4R. REPAIRED PER EA 1-A53-5808

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,539 hrs · 46,015 cycles

SUBSURFACE SKIN CRACKED AT BS 747+8" ABOVE STR 4R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,539 hrs · 46,015 cycles

FOUND INDICATION OF 1" SUBSURFACE SKIN CRACK AT BS 727B + 8.5" ABOVE STR 4R. REPAIRED PER EA 1-A53-5808

Part: COVER — MISSING (CABIN) · airframe 56,254 hrs · 45,813 cycles

FWD GALLEY EEPLS COVER MISSING. INSTALLED COVER PER M/M.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,951 hrs · 45,597 cycles

SKIN CRACKED AT BS 787+7, BETWEEN STR 4 TO STR 10. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,951 hrs · 45,597 cycles

SKIN CRACKED AT BS 727E, STR 4R. REPAIRED SKIN PER EA.

Part: FLAP — DELAMINATED (LT WING) · airframe 55,723 hrs · 45,439 cycles

LEFT WING I/B FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP IAW AMM.

Part: LENS — BROKEN (CABIN) · airframe 55,584 hrs · 45,332 cycles

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

Part: MEC — MALFUNCTIONED (NR 2 ENGINE) · airframe 55,323 hrs · 45,122 cycles

UPON DESCENT BOTH ENGINES ROLLED BACK. REMOVED AND REPLACED CIT SENSOR, VBV GEAR MOTOR, MEC AND FUEL PUMP PER MM.

Part: LENS — BROKEN (CABIN) · airframe 53,144 hrs · 43,497 cycles

R2 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REINSTALLED LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,059 hrs · 43,432 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 887+8, STR 10L. REPAIRED SKIN PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,054 hrs · 43,431 cycles

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

Part: LENS — BROKEN (CABIN) · airframe 53,054 hrs · 43,431 cycles

DURING SCHEDULED 16Y CHECK, FOUND FWD GALLEY AREA EMERGENCY EXIT SIGN LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: WEB — CORRODED (FUSELAGE) · airframe 53,054 hrs · 43,431 cycles

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

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 53,054 hrs · 43,431 cycles

DURING SCHEDULED 16Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 727B, RBL 45.5. REPAIRED CHORD PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 53,054 hrs · 43,431 cycles

DURING SCHEDULED 16Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 727B, RBL 24.5. REPAIRED CHORD PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,054 hrs · 43,431 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 188, LBL 32. REPAIRED FRAME IAW SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 53,054 hrs · 43,431 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER SPLICE CHANNEL CRACKED AT BS 360, STR 15L. REMOVED AND REPLACED CHANNEL PER SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,054 hrs · 43,431 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED BETWEEN BS 1156 TO BS 1180. REPAIRED SKIN PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 53,054 hrs · 43,431 cycles

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

Part: FRAME — CORRODED (FUSELAGE) · airframe 53,054 hrs · 43,431 cycles

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

Part: FRAME — CORRODED (FUSELAGE) · airframe 53,054 hrs · 43,431 cycles

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

Part: FRAME — CORRODED (FUSELAGE) · airframe 53,054 hrs · 43,431 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,054 hrs · 43,431 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 11R. REMOVED AND REPLACED CLIP PER SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 53,054 hrs · 43,431 cycles

DURING SCHEDULED 16Y CHECK, FOUND UPPER WEB CORRODED BETWEEN BS 400 TO BS 420, STR 17R. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,054 hrs · 43,431 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 947.5, STR 26L. REMOVED AND REPLACED CLIP PER SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 53,054 hrs · 43,431 cycles

DURING SCHEDULED 16Y CHECK, FOUND WEB CORRODED BETWEEN BS 500A TO BS 500B, STR 17R. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,054 hrs · 43,431 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,054 hrs · 43,431 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,054 hrs · 43,431 cycles

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

Part: WEB — CRACKED (FUSELAGE) · airframe 53,054 hrs · 43,431 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLIGHT DECK FLOOR WEB CRACKED AT BS 246.6, RBL 22.5. REPAIRED WEB PER ACO.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,054 hrs · 43,431 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,054 hrs · 43,431 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 22L. REMOVED AND REPLACED CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,054 hrs · 43,431 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 22L. REMOVED AND REPLACED CLIP IAW SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,631 hrs · 43,111 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 52,505 hrs · 43,009 cycles

R2 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CASE, DID NOT DEPLOY. RE-INSTALLED SLIDE PER MT.

Part: SIGN — LOOSE (CABIN) · airframe 52,039 hrs · 42,644 cycles

DURING SCHEDULED M1 CHECK, FOUND LT OVERWING EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM.

Part: COVER — LOOSE (CABIN) · airframe 51,423 hrs · 42,181 cycles

LT OVERWING EMERGENCY EXIT LIGHT COVER LOOSE. SECURED COVER PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 51,233 hrs · 42,042 cycles

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

Part: FLAP — DELAMINATED (RT WING) · airframe 51,233 hrs · 42,042 cycles

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

Part: SLIDE — UNSERVICEABLE (L1 DOOR) · airframe 50,172 hrs · 41,238 cycles

DURING SCHEDULED MV1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 49,567 hrs · 40,754 cycles

DURING SCHEDULED HC1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT.

Part: COVER — LOOSE (CABIN) · airframe 49,388 hrs · 40,599 cycles

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

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 47,966 hrs · 39,536 cycles

DURING SCHEDULED 14Y CHECK, FOUND RT KEEL BEAM CORRODED AT BS 807. REPAIRED BEAM PER EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 47,964 hrs · 39,532 cycles

DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 807, LBL 13. REPAIRED SHEAR TIE PER SRM.

Part: STRUCTURE — CRACKED (CARGO DOOR) · airframe 47,964 hrs · 39,532 cycles

DURING SCHEDULED 14Y CHECK, FOUND AFT CARGO DOOR LOWER T-CHORD FWD END CRACKED. REMOVED AND REPLACED DOOR PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 47,964 hrs · 39,532 cycles

DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 1006, BETWEEN STR 27L TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRUCTURE — CRACKED (CARGO DOOR) · airframe 47,964 hrs · 39,532 cycles

DURING SCHEDULED 14Y CHECK, FOUND AFT CARGO DOOR LOWER T-CHORD AFT END CRACKED. REMOVED AND REPLACED DOOR PER SRM.

Part: LIGHT — DAMAGED (CABIN) · airframe 47,964 hrs · 39,532 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,964 hrs · 39,532 cycles

DURING SCHEDULED 14Y CHECK, FOUND SKIN CRACKED AT BS 379, LBL 3. REPAIRED SKIN PER EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 47,964 hrs · 39,532 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CRACKED AT BS 291, STR 5R. REPAIRED STRINGER SECTION PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,964 hrs · 39,532 cycles

DURING SCHEDULED 14Y CHECK, FOUND SKIN CRACKED AT BS 394, RBL 2. REPAIRED SKIN PER SRM AND PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,964 hrs · 39,532 cycles

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

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 47,964 hrs · 39,532 cycles

DURING SCHEDULED 14Y CHECK, FOUND FLOORBEAM CRACKED AT BS 670, RBL 24. REPAIRED BEAM PER EA.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 47,964 hrs · 39,532 cycles

DURING SCHEDULED 14Y CHECK, FOUND LT KEEL BEAM CORRODED BETWEEN BS 546 TO BS 745. REMOVED AND REPLACED BEAM SECTION PER SRM.

Part: SKIN — CRACKED (FUSLAGE) · airframe 47,588 hrs · 39,240 cycles

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

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 47,401 hrs · 39,100 cycles

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

Part: SIGN — INOPERATIVE (CABIN) · airframe 46,788 hrs · 38,639 cycles

DURING SCHEDULED SPV CHECK, FOUND R1 DOOR LOWER EMERGENCY EXIT SIGN LIGHT BULB INOP. RELAMPED SIGN PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 45,795 hrs · 37,916 cycles

DURING SCHEDULED MV2 CHECK, FOUND EMERGENCY EXIT BULLNOSE LIGHT INOP AT ROW 8. RELAMPED PER MM.

Part: LENS — LOOSE (CABIN) · airframe 45,774 hrs · 37,899 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT BULLNOSE EMERGENCY EXIT LIGHT LENS LOOSE AT ROW 2. REMOVED AND REPLACED LENS PER MM.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 45,048 hrs · 37,403 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 43,876 hrs · 36,519 cycles

DURING SCHEDULED SPV CHECK, FOUND VERTICAL STIFFENER CRACKED AT BS 663, RBL 6.15. REPAIRED STIFFENER PER SWA EA.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 43,452 hrs

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

Part: SEAL — TORN (AFT CARGO DOOR) · airframe 42,992 hrs · 35,882 cycles

DIVERSION/DECLARED EMERGENCY, AT FL 360 THE CABIN WARNING HORN SOUNDED. VERIFIED LOSS OF CABIN PRESSURE. ACCOMPLISHED EMERGENCY DESCENT CHECKLIST, DECLARED EMERGENCY. INSPECTED AIRCRAFT FOUND AFT CARGO DOOR SEAL TORN AND PARTIALLY OUT OF TRACK. REMOVED AND REPLACED DOOR SEAL PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 41,965 hrs · 35,171 cycles

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

Part: CABLE — FRAYED (L1 DOOR) · airframe 41,668 hrs · 34,953 cycles

DURING SCHEDULED BRDG CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE CABLE FRAYED. REMOVED AND REPLACED CABLE PER MM.

Part: STRINGER CLIP — CRACKED (BS 360 S8R) · airframe 41,668 hrs · 34,953 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 827 S8L) · airframe 41,663 hrs · 34,953 cycles

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

Part: FRAME — CRACKED (BS 440 S8L/R) · airframe 41,663 hrs · 34,953 cycles

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

Part: FRAME — CRACKED (BS 500A S8R) · airframe 41,663 hrs · 34,953 cycles

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

Part: STRINGER CLIP — CRACKED (BS 360 S8R) · airframe 41,668 hrs · 34,953 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 727D S8L) · airframe 41,668 hrs · 34,953 cycles

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

Part: FRAME — CRACKED (BS 907 S8L) · airframe 41,668 hrs · 34,953 cycles

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

Part: FRAME — CRACKED (BS 867 S8L) · airframe 41,668 hrs · 34,953 cycles

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

Part: FRAME — CRACKED (BS 787 S8L) · airframe 41,668 hrs · 34,953 cycles

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

Part: FRAME — CRACKED (BS 500C S8L) · airframe 41,668 hrs · 34,953 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 727B S8L) · airframe 41,668 hrs · 34,953 cycles

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

Part: FRAME — CRACKED (BS 480 S8L) · airframe 41,668 hrs · 34,953 cycles

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

Part: FRAME — CRACKED (BS 747 S8L) · airframe 41,668 hrs · 34,953 cycles

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

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 41,668 hrs · 34,953 cycles

DURING SCHEDULED BRDG CHECK, FOUND NLG W/W SNUBBER ATTACHMENT FITTING CRACKED AT RBL 7.75. REPAIRED FITTING PER ACO.

Part: FRAME — CRACKED (BS 500A S8L) · airframe 41,668 hrs · 34,953 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 400 S8L) · airframe 41,668 hrs · 34,953 cycles

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

Part: LENS — LOOSE (CABIN) · airframe 39,211 hrs · 33,008 cycles

MID CABIN EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LIGHT LENS PER MM.

Part: CABLE — MISROUTED (EVAC SLIDE) · airframe 39,060 hrs · 32,894 cycles

DURING SCHEDULED SPV CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED EVAC SLIDE CABLE PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 38,950 hrs · 32,815 cycles

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

Part: SIGN — LOOSE (CABIN) · airframe 38,691 hrs · 32,609 cycles

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

Part: SIGN — LOOSE (EMERGENCY EXIT) · airframe 38,557 hrs · 32,496 cycles

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

Part: LENS — OUT OF POSITION (CABIN) · airframe 38,186 hrs · 32,221 cycles

LEFT OVERWING EMERGENCY EXIT LIGHT LENS FELL OFF. INSTALLED LIGHT LENS PER MM.

Part: SWITCH — FAULTY (EMERGENCY LIGHT) · airframe 37,368 hrs · 31,578 cycles

EMERGENCY LIGHTS -NOT ARMED LIGHT- REMAINS ON WITH SWITCH IN ANY POSITION. REMOVED AND REPLACED EMERGENCY LIGHT SWITCH PER MM.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 36,808 hrs · 31,148 cycles

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

Part: LENS — MISSING (EMERGENCY LIGHTS) · airframe 35,755 hrs · 30,343 cycles

LEFT OVERWING EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,139 hrs · 29,121 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT FWD CARGO DOOR FWD FRAME, NR 5 STOP FITTING CUTOUT. REPAIRED FRAME PER BFG ER.

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 34,139 hrs · 29,121 cycles

DURING SCHEDULED D CHECK, FOUND LT AND RT VERTICAL STAB ATTACH FITTINGS CLEVIS LUG FACES CORRODED. REPAIRED LUG FACES PER BFG ER.

Part: FRAME — CRACKED (BS 616) · airframe 34,139 hrs · 29,121 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, LBL 65, WL 203. REPAIRED FRAME PER BFG ER.

Part: FRAME — CRACKED (BS 303) · airframe 34,139 hrs · 29,121 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 303, STR 16L. REPAIRED FRAME PER BFG ER.

Part: FITTING — CORRODED (HORIZONTAL STAB) · airframe 34,139 hrs · 29,121 cycles

DURING SCHEDULED D CHECK, FOUND LT AND RT HORIZONTAL STAB ATTACH FITTING LUG FACES CORRODED. REPAIRED LUG FACES PER BFG ER.

Part: FRAME — CRACKED (BS 907) · airframe 34,139 hrs · 29,121 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907 BETWEEN STR 8L & STR 9L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 360) · airframe 34,139 hrs · 29,121 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 9R. REPAIRED FRAME PER SRM.

Part: DOUBLER — CORRODED (BS 983) · airframe 34,139 hrs · 29,121 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DOUBLER CORRODED AT BS 983, STR 23R TO STR 24R. REPAIRED SKIN DOUBLER PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 34,139 hrs · 29,121 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 787, LBL 17, WL 149. REPAIRED SHEAR TIE PER SRM.

Part: FLOORBEAM — CORRODED (BS 986) · airframe 34,139 hrs · 29,121 cycles

DURING SCHEDULED D-CHECK, FOUND CABIN FLOORBEAM CORRODED AT BS 986, LBL 35 TO LBL 45, WL 208. REPAIRED FLOORBEAM PER SRM.

Part: FRAME — CRACKED (BS 907) · airframe 34,139 hrs · 29,121 cycles

DURING SCHEDULED D-CHECK, FOUND CABIN FUSELAGE FRAME CRACKED AT BS 907, STR 9R. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CORRODED (BS 767) · airframe 34,139 hrs · 29,121 cycles

DURING SCHEDULED D-CHECK, FOUND CABIN FUSELAGE SHEAR TIE CORRODED AT BS 767, LBL 2 TO RBL 2, WL 156. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (BS 400) · airframe 34,139 hrs · 29,121 cycles

DURING SCHEDULED D-CHECK, FOUND CABIN FUSELAGE FRAME CRACKED AT BS 400, STR 9R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 787) · airframe 34,139 hrs · 29,121 cycles

DURING SCHEDULED D-CHECK, FOUND CABIN FUSELAGE FRAME CRACKED AT BS 787, STR 9L & STR 9R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 727D) · airframe 34,139 hrs · 29,121 cycles

DURING SCHEDULED D-CHECK, FOUND CABIN FUSELAGE FRAME CRACKED AT BS 727D, STR 9L. REPAIRED FRAME PER SRM.

Part: CLIP — CRACKED (BS 480) · airframe 34,139 hrs · 29,121 cycles

DURING SCHEDULED D-CHECK, FOUND CABIN FUSELAGE STR CLIP CRACKED AT BS 480, STR 15R. REMOVED AND REPLACED STR CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 480) · airframe 34,139 hrs · 29,121 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 480, STR 15R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (BS 400) · airframe 34,139 hrs · 29,121 cycles

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

Part: FRAME — CRACKED (BS 480) · airframe 34,139 hrs · 29,121 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CRACKED (BS 500) · airframe 34,139 hrs · 29,121 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 500, BETWEEN RBL 1 TO RBL 2. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: BRACKET — CORRODED (GIRT BAR) · airframe 34,139 hrs · 29,121 cycles

DURING SCHEDULED D-CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR BRACKETS CORRODED. REMOVED AND REPLACED BRACKETS PER SRM.

Part: SHEAR TIE — CORRODED (BS 787) · airframe 34,139 hrs · 29,121 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 787, RBL 17. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (BS 767) · airframe 34,139 hrs · 29,121 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 767, BETWEEN LBL 2 TO RBL 12. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CORRODED (BS 787) · airframe 34,139 hrs · 29,121 cycles

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

Part: CREASE BEAM — CORRODED (BS 460-480) · airframe 34,139 hrs · 29,121 cycles

DURING SCHEDULED D-CHECK, FOUND RIGHT CREASE BEAM WEB CORRODED BETWEEN BS 460 TO BS 480. REPAIRED CREASE BEAM WEB PER SRM.

Part: CREASE BEAM — CORRODED (BS 380-400) · airframe 34,139 hrs · 29,121 cycles

DURING SCHEDULED D-CHECK, FOUND RT CREASE BEAM WEB CORRODED BETWEEN BS 380 TO BS 400. REPAIRED CREASE BEAM WEB PER SRM.

Part: STRINGER CLIP — CRACKED (BS 578) · airframe 34,139 hrs · 29,121 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 578, STR 11R. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOORBEAM — CORRODED (BS 270) · airframe 34,139 hrs · 29,121 cycles

DURING SCHEDULED D-CHECK, FOUND COCKPIT FLOORBEAM CORRODED AT BS 270, BETWEEN LBL 6 TO RBL 6. REPAIRED FLOORBEAM PER SRM.

Part: FRAME — CRACKED (BS 727D) · airframe 34,139 hrs · 29,121 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8L & STR 8R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 907) · airframe 34,139 hrs · 29,121 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8R TO STR 9R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 787) · airframe 34,139 hrs · 29,121 cycles

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

Part: FRAME — CRACKED (BS 867) · airframe 34,139 hrs · 29,121 cycles

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

Part: FRAME — CRACKED (BS 747) · airframe 34,139 hrs · 29,121 cycles

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

Part: CREASE BEAM — CORRODED (BS 727D-727E) · airframe 34,139 hrs · 29,121 cycles

DURING SCHEDULED D-CHECK, FOUND LT CREASE BEAM WEB CORRODED BETWEEN BS 727D TO BS 727E. REPAIRED CREASE BEAM WEB SECTION PER SRM.

Part: FRAME — CRACKED (BS 827) · airframe 34,139 hrs · 29,121 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8R TO STR 9R. REPAIRED FRAME PER SRM.

Part: FLOORBEAM — CORRODED (BS 986) · airframe 34,139 hrs · 29,121 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FLOORBEAM CORRODED AT BS 986, BETWEEN LBL 35 TO LBL 45. REPAIRED FLOORBEAM PER SRM.

Part: LENS — DISLODGED (MID CABIN) · airframe 34,033 hrs · 29,030 cycles

RIGHT OVERWING EMERGENCY EXIT LIGHT LENS FELL OFF. INSTALLED LENS PER MM.

Part: GEARBOX — MAKING METAL (NR 2 ENGINE) · airframe 33,994 hrs · 29,005 cycles

DURING SCHEDULED A1 CHECK, FOUND METAL CHIPS IN NR 2 ENGINE FWD OIL MAGNETIC CHIP DETECTOR. REMOVED AND REPLACED NR 2 TRANSFER GEARBOX ASSY PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 33,423 hrs · 28,569 cycles

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

Part: DRAG BRACE — WORN (NLG) · airframe 32,952 hrs · 28,185 cycles

VIBRATION FELT AT NLG. REMOVED & REPLACED NLG LOWER DRAG BRACE ASSY PER MM DUE TO WORN BEARING.

Part: SLIDE — UNSERVICEABLE (L1 DOOR) · airframe 32,359 hrs · 27,723 cycles

DURING SCHEDULED PM CHECK, FOUND L1 DOOR EVAC SLIDE PRESSURE IND OUT OF LIMITS. REMOVED AND REPLACED L1 DOOR EVAC SLIDE PER MM.

Part: STRUCTURE — CRACKED (HINGE BOX) · airframe 31,983 hrs · 27,416 cycles

DURING SCHEDULED C4 CHECK, FOUND FWD ENTRY DOOR CUTOUT LOWER HINGE BOX, CRACKED. REMOVED AND REPLACED FWD ENTRY DOOR HINGE BOX PER SRM.

Part: BUSHING — WORN (RT ELEVATOR) · airframe 31,977 hrs · 27,410 cycles

DURING SCHEDULED C4 CHECK, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 ELEVATOR TAB BUSHING PER MM.

Part: CONTROL MODULE — LEAKING (MLG W/W) · airframe 31,915 hrs · 27,362 cycles

DIVERSION/DECLARED EMERGENCY. AT CRUISE ALTITUDE LOST B-SYSTEM HYDRAULIC FLUID QUANTITY. REMOVED AND REPLACED B-SYSTEM BRAKE CONTROL MODULE PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 31,409 hrs · 26,968 cycles

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

Part: OUTFLOW VALVE — FAULTY (CABIN PRESSURE) · airframe 28,270 hrs · 24,425 cycles

LOSS OF CABIN PRESSURE LEVEL AT FL290, CABIN PRESS REACHED FL220. UNCONTROLABLE IN MANUAL MODE. GOOD BLEED AIR PRESSURE DURING DEPRESSURIZATION. REMOVED AND REPLACED MAIN OUTFLOW VALVE AND CABIN PRESSURE CONTROLLER PER MM.

Part: SLIDE — DISLODGED (SERVICE DOOR) · airframe 27,466 hrs · 23,764 cycles

DURING SCHEDULED RON, FWD SVC DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM.

Part: FITTING — LOOSE (GIRT BAR) · airframe 27,466 hrs · 23,764 cycles

FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT BAR LOOSE IN FLOOR ATTACH FITTINGS. ADJUSTED FITTINGS PER MM.

Part: SLIDE — LOOSE (SERVICE DOOR) · airframe 27,366 hrs · 23,686 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE LOOSE IN CONTAINER. SECURED SLIDE PER MM.

Part: SLIDE — LOOSE (R2 DOOR) · airframe 27,366 hrs · 23,686 cycles

AFT SERVICE DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. SECURED SLIDE INTO CONTAINER PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 25,902 hrs · 22,490 cycles

DURING SCHEDULED 1/4D CHECK, FOUND RT SIDE CHORD CRACKED AT BS 178, WL 209. REMOVED AND REPLACED RT CHORD PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 25,902 hrs · 22,490 cycles

DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED AT BS 400, WL 148 AND LBL 17. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 25,902 hrs · 22,490 cycles

DURING SCHEDULED 1/4D CHECK, FOUND LT SIDE CHORD CRACKED AT BS 178, WL 208. REMOVED AND REPLACED LT CHORD PER SRM.

Part: WINDOW — CRACKED (COCKPIT) · airframe 24,563 hrs · 51,429 cycles

R-1 COCKPIT WINDOW ARCING AND DELAMINATING, OUTER PANE CRACKED. REMOVED AND REPLACED R-1 WINDOW PER MM.

Part: STRAP — BROKEN (CABIN) · airframe 22,722 hrs · 19,979 cycles

EMERGENCY FLASH LIGHT STRAP BROKEN AT AFT F/A STATION. REMOVED AND REPLACED STRAP PER MM.

Part: ROD END — WORN (ELEVATOR TAB) · airframe 22,703 hrs · 19,965 cycles

DURING SCHEDULED PM CHECK, SWA SI 11111-55, BOTH LT AND RT ELEVATOR TABS FAILED FREE PLAY INSPECTION. REMOVED AND REPLACED BOTH LT AND RT ELEVATOR TAB OUTBOARD ROD END ASSY'S PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 19,969 hrs · 17,734 cycles

DURING SCHEDULED C3 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJ (ENTRY DOOR) · airframe 19,969 hrs · 17,732 cycles

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

Part: LENS — LOOSE (CABIN) · airframe 19,969 hrs · 17,734 cycles

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

Part: ENGINE — LEAKING (NR 1) · airframe 19,608 hrs · 17,421 cycles

ON TAKEOFF SMOKE APPEARED IN COCKPIT DUE TO OIL SEAL LEAK INTO BLEED SYS. REMOVED AND REPLACED NR 1 ENG PER MM.

Part: LENS — MISSING (CABIN) · airframe 19,221 hrs · 17,123 cycles

DURING SCHEDULED A2 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 19,015 hrs · 16,938 cycles

DURING SCHEDULED C2 CHECK, FOUND RT WING OUTBD T/E FLAP DELAMINATED AT INBD END. REMOVED AND REPLACED FLAP PER MM.

Part: FILTER — CLOGGED (EE BAY) · airframe 18,620 hrs · 16,603 cycles

AT APPROX 4000 FEET, ELECTRICAL FUMES PRESENT IN COCKPIT. NO SMOKE OBSERVED. C/W BOTH ENGS BORESCOPE INSP, REMOVED AND REPLACED A/C COALESCER BAGS, INSP ACM''S, INSP FWD E&E COMPT AND E&E EQUIPMENT IN COCKPIT. NO DEFECT NOTED. FOUND RADAR FILTER CLOGGED, SUSPECT RADAR R/T OVERHEAT. CLEANED FILTER. OPS CK GOOD PER MM.

Part: LENS — LOOSE (CABIN) · airframe 18,017 hrs · 16,098 cycles

DURING SCHEDULED C1 CHECK, FOUND EMERGENCY EXIT LIGHT LENS LOOSE AT R/H OVERWING EXIT. R&R LENS PER MM.

Part: LENS — MISSING (CABIN) · airframe 17,739 hrs · 15,871 cycles

FWD SVC DOOR EMERGENCY EXIT LIGHT LENS COVER MISSING. REPLACED LENS COVER PER MM.

Part: LENS — BROKEN (AFT LAVATORY) · airframe 17,348 hrs · 15,559 cycles

DURING SCHEDULED 1/2D CHECK, FOUND AFT LAV EMERGENCY LIGHT LENS COVER WITH BROKEN MOUNT CLIP. REMOVED AND REPLACED LENS PER MM.

Part: FRAME — CRACKED (SERVICE DOOR) · airframe 17,348 hrs · 15,559 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FWD SVC DOOR AFT LWR FRAME CRACKED. REPAIRED FRAME PER DRW 69-69854.

Part: STRINGER CLIP — CRACKED (CABIN) · airframe 17,348 hrs · 15,559 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STR CLIP CRACKED AT BS 663, STR 10L. REMOVED AND REPLACED STR CLIP PER SRM.

Part: LENS — MELTED (GALLEY LIGHT)

AFT GALLEY HAS A BURNING ODOR. FOUND AFT GALLEY WORK LIGHT BULB MELTING LENS ASSY. PULLED/COLLARED WORKLIGHT C/B AND DEFERRED PER MEL.

Part: FLASHLIGHT — INOPERATIVE (CABIN)

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

Part: SLIDE — DISCHARGED (SERVICE DOOR)

AFT SERVICE DOOR EVACUATION SLIDE PRESS IND LOW. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: COVER — MISSING (CABIN)

EEPLS TRACK COVER MISSING AT MID CABIN. REPLACED COVER PER MM.

Part: KEEL BEAM — CRACKED (BS 700 & 715)

DURING SCHEDULED C4 CHECK, FOUND 2 EACH CRACKS ON KEEL BEAM SKIN, BS 700, AND BS 715. REPAIRED KEEL BEAM PER SWA RA NR 1-353-2141.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING SCHEDULED A1 CHECK, FOUND FWD EEPLS LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SLIDE — DETACHED (PASSENGER DOOR)

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

Part: BULB — FAILED (CABIN)

DURING SCHEDULED C3 CHECK, FOUND EMERGENCY EVACUATION FLOOR TRACK LIGHTING INOP AT OVERWING EXIT. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SLIDE — LOW PRESSURE (L2 DOOR)

DURING SCHEDULED SERVICE CHECK, FOUND L-2 DOOR ESCAPE SLIDE PRESSURE GAGE READING LOW. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: BATTERY — DISCHARGED (CABIN)

EMERGENCY LIGHT BATTERY PACKS REQUIRED REPLACEMENT DUE TO EXTENDED USE. REMOVED AND REPLACED BATTERY PACKS PER M/M (7 EA), OPS CKS OK.