N647SW

Part: SKIN — CRACKED (LT WING SLAT) · airframe 61,238 hrs · 47,695 cycles

LEFT WING LEADING EDGE NR 1 SLAT SKIN INBOARD AUXILIARY TRACK CRACKED. REPAIRED THE SKIN IAW SRM.

Part: OIL COOLER — LEAKING (NR 2 CSD) · airframe 60,641 hrs · 47,315 cycles

DURING FLIGHT, NR 2 GENERATOR LOW PRESSURE LIGHT BEGAN FLICKERING CONTINUOUSLY. NR 2 GENERATOR BUSS LIGHT ILLUMINATED. DID NOT RESET. APU STARTED AND PUT ON NR 2 BUSS. LOW PRESSURE LIGHT ILLUMINATES STEADY. NR 2 GENERATOR FREQUENTLY ERRATIC 385-400. DISCONNECTED CSD. FOUND NR 2 ENGINE CSD OIL COOLER LEAKING OIL. REPLACED THE NR 2 ENGINE CSD OIL COOLER IAW AMM 24-11-21.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 60,488 hrs · 47,218 cycles

R2 DOOR EMERGENCY EXIT LIGHT BULB INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 60,488 hrs · 47,218 cycles

RIGHT OVERWING SIDEWALL EMERGENCY EXIT LIGHT BULB INOPERATIVE. R & R LIGHT IAW AMM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 60,488 hrs · 47,218 cycles

R2 DOOR ESCAPE SLIDE OUT OF ADJUST. ADJUSTED THE SLIDE IAW CC.

Part: HINGE FITTING — LOOSE (RT SPOILER) · airframe 60,488 hrs · 47,218 cycles

RIGHT WING NR 5 GROUND SPOILER PIVOT BEARING LOOSE IN HINGE FITTING AT INBD CENTER LOCATION WBL 119.25. R & R FITTING IAW AMM & SRM.

Part: STRINGER CLIP — CORRODED (BS 344) · airframe 60,488 hrs · 47,218 cycles

STRINGER CLIP CORRODED AT BS 344, STRINGER 16R. R & R THE STRINGER CLIP IAW SRM & DWG.

Part: TEE FITTING — CORRODED (BS 322-344) · airframe 60,488 hrs · 47,218 cycles

TEE ANGLE CORRODED BETWEEN BS 322 - 344, STRINGER 10R. R & R THE TEE ANGLE IAW SRM & DWG

Part: INTERCOSTAL — CRACKED (BS 927-947) · airframe 60,488 hrs · 47,218 cycles

AFT CARGO COMPARTMENT INTERCOSTAL CORRODED BETWEEN BS 927 - 947, RBL 13. R & R THE INTERCOSTAL IAW SRM AND DWG.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 60,488 hrs · 47,218 cycles

RIGHT WING INBOARD AFT FLAP DELAMINATED ON OUTBOARD SIDE OF TRAILING EDGE. REPAIRED FORE FLAP IAW SRM.

Part: FITTING — CRACKED (VERTICAL STAB) · airframe 60,488 hrs · 47,218 cycles

VERTICAL STABILIZER LT PANEL 9505 AFT SKATE ANGLE CLIP CRACKED ON FORWARD EDGE. R & R CLIP IAW DWG AND SRM.

Part: INTERCOSTAL — CORRODED (BS 332-344) · airframe 60,488 hrs · 47,218 cycles

INTERCOSTAL CORRODED BETWEEN BS 332 - 344, STRINGER 10R. R & R INTERCOSTAL IAW SRM & DWG.

Part: INTERCOSTAL — CORRODED (BS 332-344) · airframe 60,488 hrs · 47,218 cycles

INTERCOSTAL CORRODED BETWEEN BS 332 - 344, STRINGER 11R. R & R THE INTERCOSTAL IAW SRM & DWG.

Part: DOOR FRAME — BROKEN (L1 DOOR) · airframe 60,488 hrs · 47,218 cycles

AFT SIDE OF L1 DOOR FRAME CORNER CHORD BROKEN AT BS 344, WL 208 LOWER NUT PLATE. R & R CHORD IAW DWG.

Part: INTERCOSTAL — CORRODED (BS 332-344) · airframe 60,488 hrs · 47,218 cycles

INTERCOSTAL CORRODED BETWEEN BS. 332 - 344, STRINGER 8R. R & R THE INTERCOSTAL IAW SRM & DWG.

Part: TEE FITTING — CORRODED (BS 332) · airframe 60,488 hrs · 47,218 cycles

TEE FITTING CORRODED BETWEEN BS 332, STRINGER 8R. R & R THE TEE FITTING IAW SRM & DWG.

Part: LINK ASSY — CORRODED (LT MLG) · airframe 60,488 hrs · 47,218 cycles

LEFT MLG SWING LINK CORRODED. REPAIRED SWING LINK IAW EA.

Part: LINK — CORRODED (RT MLG) · airframe 60,488 hrs · 47,218 cycles

RIGHT MAIN LANDING GEAR SWING LINK CORRODED. REPAIRED THE SWING LINK IAW EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 60,488 hrs · 47,218 cycles

STRINGER CORRODED BETWEEN BS 322-BS 344, STR 19R. R & R STRINGER IAW ER AND SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 60,488 hrs · 47,218 cycles

INTERCOSTAL CORRODED BETWEEN BS 322 TO BS 344, STR 5R. R & R INTERCOSTAL IAW SRM & DWG.

Part: INTERCOSTAL — CORRODED (B 332-344) · airframe 60,488 hrs · 47,218 cycles

INTERCOSTAL CORRODED BETWEEN BS 332 - 344, STRINGER 16R. R & R THE INTERCOSTAL IAW SRM AND DWG.

Part: INTERCOSTAL — CORRODED (BS 322-344) · airframe 60,488 hrs · 47,218 cycles

INTERCOSTAL CORRODED BETWEEN BS 322 - 344, STRINGER 7R. R & R THE INTERCOSTAL IAW SRM & DWG.

Part: BRACKET — CRACKED (RT WING) · airframe 60,488 hrs · 47,218 cycles

RIGHT WING BRACKET CRACKED COMMON TO UPPER REAR SPAR AT APPROXIMATELY RSS 235. R & R BRACKET IAW DWG AND SRM.

Part: SKIN — CRACKED (LT WING) · airframe 60,488 hrs · 47,218 cycles

LEFT WING UPPER SKIN TRAILING EDGE CRACKED AT BETWEEN RSS 270 TO 240. REPAIRED THE SKIN IAW ER AND EA.

Part: SKIN — CRACKED (RT WING) · airframe 60,488 hrs · 47,218 cycles

RIGHT WING UPPER T/E SKIN CRACKED AT RSS 238.84 TO RSS 249.04, FORWARD AND AFT OF 1 EA FASTENER HOLE. REPAIRED SKIN IAW ER AND EA.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 60,488 hrs · 47,218 cycles

RT MAIN WHEEL WELL PRESSURE DECK CRACKED AT BS 667, RBL 40.0. REPAIRED DECK IAW SRM.

Part: FITTING — CRACKED (RT WING) · airframe 60,488 hrs · 47,218 cycles

RIGHT WING REAR SPAR FORWARD MLG FITTING CRACKED AT APPROXIMATELY RSS 224.14, NR 5 HOLE. REPAIRED FITTING ER AND EA.

Part: BEAR STRAP — CRACKED (BS 986) · airframe 60,488 hrs · 47,218 cycles

L2 DOOR CUTOUT UPPER AFT CORNER BEAR STRAP CRACKED AT BS 986.5. REPAIRED THE BEAR STRAP IAW SRM.

Part: SPAR — CRACKED (LT WING) · airframe 60,488 hrs · 47,218 cycles

LEFT WING REAR SPAR WEB CRACKED AT RSS 211 TO 238. REPAIRED THE SPAR WEB IAW ER & EA.

Part: SPAR — CRACKED (RT WING) · airframe 60,488 hrs · 47,218 cycles

RIGHT WING REAR SPAR WEB CRACKED BETWEEN RSS 211 TO 238. REPAIRED THE SPAR WEB IAW ER & EA.

Part: SPAR — CRACKED (RT WING) · airframe 60,488 hrs · 47,218 cycles

RIGHT WING REAR SPAR UPPER CHORD CRACKED AT APPROXIMATELY RSS 224.14, NR 5 HOLE. REPAIRED CHORD IAW ER AND EA.

Part: SPAR — CRACKED (LT WING) · airframe 60,488 hrs · 47,218 cycles

LEFT WING REAR SPAR CRACKED AT RSS 224.14 TO 285. REPAIRED THE SPAR IAW ER & EA.

Part: FITTING — CRACKED (LT WING SPAR) · airframe 60,488 hrs · 47,218 cycles

LEFT WING REAR SPAR AFT FITTING CRACKED AT APPROXIMATELY RSS 224.14. REPAIRED THE FITTING IAW ER & EA.

Part: SPAR — CRACKED (RT WING) · airframe 60,488 hrs · 47,218 cycles

RIGHT WING REAR SPAR CRACKED AT APPROXIMATELY RSS 285. REPAIRED THE SPAR IAW ER & EA.

Part: ANGLE — CRACKED (RT WING) · airframe 60,488 hrs · 47,218 cycles

RIGHT WING TRAILING EDGE COVE ANGLE CRACKED AT RSS. 545. R & R THE ANGLE IAW DWG AND SRM.

Part: BRACKET — CRACKED (LT WING) · airframe 60,488 hrs · 47,218 cycles

LEFT WING UPPER REAR SPAR BRACKET CRACKED AT APPROXIMATELY RSS 235. R & R THE BRACKET IAW DWG AND SRM.

Part: STRINGER SPLICE — CORRODED (BS 907) · airframe 60,488 hrs · 47,218 cycles

STRINGER SPLICE CORRODED AT BS 907, STRINGER 22. R & R THE STRINGER SPLICE IAW SRM & DWG.

Part: SEAT TRACK — CORRODED (BS 727D) · airframe 60,488 hrs · 47,218 cycles

SEAT TRACK CORRODED AT BS 727D+5, LBL 7. R & R SEAT TRACK IAW SRM & EA.

Part: FRAME — CORRODED (BS 312) · airframe 60,488 hrs · 47,218 cycles

FRAME CORRODED AT BS 312, STRINGER 28R. REPAIRED THE FRAME IAW SRM & DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 60,488 hrs · 47,218 cycles

SHEAR TIE CORRODED AT BS 727C, BETWEEN STR 23L TO STR 23R. R & R FRAME IAW SRM AND DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 60,488 hrs · 47,218 cycles

FLOOR TRACK CORRODED AT BS 727D+5, RBL 7. REPAIRED FLOOR TRACK IAW EA.

Part: STRINGER SPLICE — CORRODED (BS 904) · airframe 60,488 hrs · 47,218 cycles

STRINGER SPLICE CORRODED AT BS 904, STRINGER 22R. REPAIRED THE STRINGER SPLICE IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 60,488 hrs · 47,218 cycles

FLOOR TRACK CORRODED AT BS 772, LBL 2. REPAIRED ANGLE IAW EA.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 60,488 hrs · 47,218 cycles

FLOOR TRACK ANGLE CORRODED AT BS 772, RBL 7. REPAIRED ANGLE IAW EA.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 60,488 hrs · 47,218 cycles

BELLY DRAIN REINFORCING RING DOUBLER CORRODED AT BS 727E+3, BETWEEN STR 26R TO STR 27R. R & R DOUBLER IAW SRM.

Part: SEAT TRACK — CORRODED (BS 727D) · airframe 60,488 hrs · 47,218 cycles

SEAT TRACK CORRODED AT BS 727D+5, LBL 2. / REPAIRED SEAT TRACK IAW SRM & EA.

Part: BRACKET — CRACKED (RT WING) · airframe 60,488 hrs · 47,218 cycles

RIGHT WING FIREBOX LOWER AFT SPAR CHORD LOWER BRACKET CRACKED APPROXIMATELY RSS 278. R & R BRACKET IAW DWG.

Part: DOOR FRAME — CRACKED (R1 DOOR) · airframe 60,488 hrs · 47,218 cycles

R1 DOOR CUTOUT LOWER AFT CORNER CRACKED AT BS 327, WL 209.5. REPAIRED CUTOUT IAW SRM.

Part: DOUBLER — CRACKED (BS 343) · airframe 60,488 hrs · 47,218 cycles

L1 DOOR BEAR STRAP SKIN LOWER AFT CORNER CRACKED AT BS 343.5, WL 209. REPAIRED THE BEAR STRAP IAW SRM.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 60,488 hrs · 47,218 cycles

LEFT WING OUTBOARD FORE FLAP DELAMINATED. REPAIRED THE FLAP IAW SRM.

Part: STRINGER SPLICE — CORRODED (BS 907) · airframe 60,488 hrs · 47,218 cycles

STRINGER SPLICE CORRODED AT BS 907, STRINGER 22R. REPAIRED THE STRINGER SPLICE IAW SRM & DWG.

Part: STRINGER CLIP — CRACKED (BS 927) · airframe 60,488 hrs · 47,218 cycles

STRINGER CLIP CRACKED AT BS 927, STRINGER 21R. R & R THE STRINGER CLIP IAW DWG AND SRM.

Part: STRINGER CLIP — CORRODED (BS 727E) · airframe 60,488 hrs · 47,218 cycles

STRINGER CLIP CORRODED AT BS 727E, STRINGER 23L. R & R THE STRINGER CLIP IAW SRM & DWG.

Part: SHEAR TIE — CORRODED (BS 500B) · airframe 60,488 hrs · 47,218 cycles

SHEAR TIE CORRODED AT BS 500B, BETWEEN STRINGERS 26 - 27L. REPAIRED THE SHEAR TIE IAW SRM & DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 60,488 hrs · 47,218 cycles

FRAME CORRODED AT BS 747, BETWEEN STR 26R TO STR 27R. REPAIRED FRAME IAW SRM.

Part: FRAME — CORRODED (BS 767) · airframe 60,488 hrs · 47,218 cycles

FRAME CORRODED AT BS 767, BETWEEN STRINGERS 27R & 27L. REPAIRED THE FRAME IAW SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 60,488 hrs · 47,218 cycles

STRINGER CLIP CORRODED AT BS 747, STR 26L. R & R CLIP IAW SRM & DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 60,488 hrs · 47,218 cycles

SHEAR TIE CORRODED AT BS 500C, BETWEEN STR 26L TO STR 27L. REPAIRED SHEAR TIE IAW SRM.

Part: FRAME — CORRODED (BS 500D) · airframe 60,488 hrs · 47,218 cycles

FUSELAGE FRAME CORRODED AT BS 500D, BETWEEN STRINGERS 27 - 28L. REPAIRED THE FRAME IAW SRM.

Part: SKIN — CRACKED (LT WING) · airframe 59,413 hrs · 46,487 cycles

LEFT WING UPPER SKIN CRACKED, AT WBL 189. REPAIRED SKIN IAW EA.

Part: GLOWSTRIP — DELAMINATED (CABIN) · airframe 58,516 hrs · 45,911 cycles

FORWARD ENTRYWAY PHOTO LUMINESCENT STRIP DELAMINATED. R & R STRIP IAW AMM.

Part: LIGHT — DAMAGED (CABIN) · airframe 58,516 hrs · 45,911 cycles

RIGHT EMER PATH LIGHTNING DAMAGED AT ROW 4. R & R EEPLS IAW AMM.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 58,357 hrs · 45,800 cycles

FLOORBEAM SUPPORT CRACKED AT BS 328, RBL 40. REPAIRED SUPPORT IAW SRM.

Part: FUSE — FAULTY (HYDRAULIC SYS) · airframe 57,249 hrs · 45,003 cycles

DIVERSION, WITH FLAPS EXTENDED AT 15, LE DEVICES DID NOT EXTEND AFTER TOUCHDOWN, LED EXTENDED & STAYED EXTENDED AFTER FLAPS RETRACTED. R & R B SYS LE EXTEND & RETRACT HYD FUSES IAW AMM.

Part: SWITCH — FAULTY (LE FLAP) · airframe 57,249 hrs · 45,003 cycles

DIVERSION, IN CLIMB WITH FLAPS UP NR 3 LT IN TRANSIT LIGHT ON OVERHEAD ANNUNCIATOR ON. R & R S172 NR 3 K FLAP UP SWITCH IAW AMM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 57,050 hrs · 44,865 cycles

AFT PRESS BULKHEAD WEB CRACKED ON Y CHORD AFT FASTENER ROW BETWEEN THE 3 RIVETS BELOW STRINGER 6L. REPAIRED WEB IAW SRM & EA.

Part: LENS — UNSERVICEABLE (EXIT SIGN) · airframe 56,784 hrs · 44,681 cycles

FORWARD ENTRY EXIT SIGN LENS FELL OUT. REINSTALLED LENS IAW AMM.

Part: LENS — UNSECURE (CABIN) · airframe 56,512 hrs · 44,495 cycles

FORWARD ENTRY EMER EXIT LIGHT LENS FELL OFF. R & R LIGHT ASSEMBLY IAW MM.

Part: SLIDE — LOOSE (L2 DOOR) · airframe 56,108 hrs · 44,208 cycles

L2 DOOR EMER EVAC SLIDE GIRT LOOSE. SECURED SLIDE IAW MT & AMM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,876 hrs · 44,055 cycles

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

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 55,876 hrs · 44,055 cycles

FUSELAGE INTERCOSTAL CRACKED AT STATION 663 TO 685, BETWEEN STRINGER 8L & 9L. R & R INTERCOSTAL IAW SRM.

Part: STRINGER CLIP — DAMAGED (FUSELAGE) · airframe 55,876 hrs · 44,055 cycles

STRINGER CLIP DAMAGED AT STATION 727A, STRINGER 9R. R & R CLIP IAW SRM.

Part: STRINGER CLIP — DAMAGED (FUSELAGE) · airframe 55,876 hrs · 44,055 cycles

STRINGER CLIP DAMAGED AT STATION 727A, STRINGER 9L. R & R CLIP IAW SRM.

Part: STRINGER CLIP — DAMAGED (FUSELAGE) · airframe 55,876 hrs · 44,055 cycles

STRINGER CLIP DAMAGED AT STATION 727B, STRINGER 9L. R & R CLIP IAW SRM.

Part: STRINGER CLIP — DAMAGED (FUSELAGE) · airframe 55,876 hrs · 44,055 cycles

STRINGER CLIP DAMAGED AT STATION 727A, STRINGER 9L. R & R CLIP IAW SRM.

Part: STRINGER CLIP — BROKEN (FUSELAGE) · airframe 55,876 hrs · 44,055 cycles

STRINGER CLIP BROKEN AT STATION 727A, STRINGER 1. R & R CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,876 hrs · 44,055 cycles

STRINGER CLIP CRACKED AT STATION 480, STRINGER 9L. R & R CLIP IAW SRM.

Part: FORGING — CRACKED (FUSELAGE) · airframe 55,876 hrs · 44,055 cycles

LEFT FUSELAGE WINDOW FORGING CRACKED AT STATION 807+10. R & R FORGING IAW DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,876 hrs · 44,055 cycles

RIGHT FUSELAGE SKIN CRACKED AT STATION 767+10, LOWER FWD WINDOW CUT OUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,876 hrs · 44,055 cycles

LEFT FUSELAGE SKIN CRACKED AT STATION 867+10, LOWER FWD WINDOW CUT OUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,876 hrs · 44,055 cycles

LEFT FUSELAGE SKIN CRACKED AT STATION 887+10, UPPER AFT WINDOW CORNER. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,876 hrs · 44,055 cycles

RIGHT FUSELAGE SKIN CRACKED AT STATION 727B+10, LOWER FWD WINDOW CORNER. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,876 hrs · 44,055 cycles

RIGHT FUSELAGE SKIN CRACKED AT STATION 727E+10, LOWER FWD WINDOW CORNER. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,876 hrs · 44,055 cycles

RIGHT FUSELAGE SKIN CRACKED AT STATION 887+10, UPPER AFT WINDOW CORNER. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,876 hrs · 44,055 cycles

LEFT FUSELAGE SKIN CRACKED AT STATION 727C+10, UPPER AFT WINDOW CORNER. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,876 hrs · 44,055 cycles

RIGHT FUSELAGE SKIN CRACKED AT STATION 827+10, LOWER FWD WINDOW CUT OUT CORNER. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,876 hrs · 44,055 cycles

RIGHT FUSELAGE SKIN CRACKED AT STATION 807+10, LOWER FWD WINDOW CUT OUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,876 hrs · 44,055 cycles

LEFT FUSELAGE SKIN CRACKED AT STATION 767+10, UPPER AFT WINDOW CORNER. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,876 hrs · 44,055 cycles

RIGHT FUSELAGE SKIN CRACKED AT STATION 847+10, UPPER AFT WINDOW CUT OUT CORNER. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (ENTRY DOOR) · airframe 55,359 hrs · 43,695 cycles

FORWARD ENTRY DOOR CRACKED AT LOWER HINGE INNER SKIN. REPAIRED DOOR IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,208 hrs · 43,580 cycles

L2 DOOR FWD LOWER STUB FRAME LOWER FASTENER HOLE CUT OUT CRACKED. REPAIRED CUT OUT IAW EA.

Part: COVER — DELAMINATED (CABIN) · airframe 55,208 hrs · 43,580 cycles

LEFT EEPLS COVER DELAMINATED. R & R COVER IAW DWG.

Part: COVER — DELAMINATED (CABIN) · airframe 55,208 hrs · 43,580 cycles

RIGHT EEPLS COVER DELAMINATED. R & R COVER IAW DWG.

Part: RIB — CRACKED (RT WING) · airframe 55,208 hrs · 43,580 cycles

RIGHT WING RIB LOWER CHORD CRACKED AT WBL 135.5 BETWEEN STRINGER 2 TO 3. REPAIRED RIB IAW EA.

Part: RIB — CRACKED (LT WING) · airframe 55,208 hrs · 43,580 cycles

LEFT WING RIB LOWER CHORD CRACKED AT WBL 135.5 BETWEEN STRINGER 2 TO 3. REPAIRED RIB IAW EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 55,208 hrs · 43,580 cycles

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

Part: SKIN — CRACKED (L2 DOOR) · airframe 55,208 hrs · 43,580 cycles

L2 DOOR LOWER FWD CORNER SKIN CRACKED AT BS 961+2 STRINGER 17L. REPAIRED SKIN IAW SRM.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 55,208 hrs · 43,580 cycles

PRESSURE DOME CORRODED AT BS 1016 BETWEEN LBL 3 TO RBL 3. REPAIRED DOME IAW SRM & EA.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 55,208 hrs · 43,580 cycles

MAIN WW PRESS DECK WEB CRACKED AT BS 674 LBL 39. REMOVED WEB IAW EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 55,208 hrs · 43,580 cycles

FORWARD LT CABIN CREASE BEAM WEB CORRODED BETWEEN BS 400 TO 420. REPAIRED WEB IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,208 hrs · 43,580 cycles

FRAME OUTER CHORD CRACKED AT BS 727 STRINGER 18A RT. REPAIRED CHORD IAW EA.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 55,208 hrs · 43,580 cycles

AFT LT CABIN CREASE BEAM OUTER CHORD SPLICE ANGLE CORRODED AT BS 907. R & R ANGLE IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,208 hrs · 43,580 cycles

FRAME OTBD CHORD FWD FLANGE CRACKED AT BS 727 STRINGER 18A RT. REPAIRED CHORD IAW EA.

Part: OIL TANK — FAULTY (NR 1 ENGINE) · airframe 53,734 hrs · 42,546 cycles

DIVERSION OIL PRESS NOTED TO CHANGE WITH PRESS ALTITUDE OF CRUISE N2 SETTINGS, FL 370 + 18 PSI, FL 340 = 22 PSI FL 260 = 30 PSI, FL 100 = 40 PSI. R & R NR 1 ENG OIL TANK IAW MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 53,587 hrs · 42,447 cycles

RT WING AFT FLAP DELAMINATED. R & R AFT FLAP IAW MM.

Part: DOOR FRAME — CRACKED (R1 DOOR) · airframe 53,587 hrs · 42,447 cycles

R1 DOOR LOWER EDGE FRAME CRACKED AT AFT CORNER. R & R DOOR IAW MM.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 53,526 hrs · 42,409 cycles

LT MAIN WW STRUT CUTOUT UPPER FWD AERODYNAMIC FAIRING, AFT CURVED ATTACH ANGLE CRACKED. R & R ANGLE IAW DRAWING & SRM.

Part: LENS — MISSING (EXIT SIGN) · airframe 52,728 hrs · 41,857 cycles

R2 DOOR EMERGENCY EXIT SIGN ON WALL LENS MISSING. INSTALLED LENS IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,481 hrs · 41,663 cycles

L1 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REPAIRED LIGHT IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,481 hrs · 41,663 cycles

R1 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REPAIRED LIGHT IAW MM.

Part: SPOILER — DELAMINATED (LT WING) · airframe 52,450 hrs · 41,636 cycles

LT WING FLIGHT SPOILER DELAMINATED. R&R SPOILER IAW MM.

Part: FITTING — OUT OF ADJUST (L1 DOOR) · airframe 52,226 hrs · 41,468 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR CLIPS OUT OF ADJUSTMENT. ADJUSTED CLIPS IAW MT.

Part: WINDOW — ARCED (COCKPIT) · airframe 52,061 hrs · 41,325 cycles

R1 WINDOW ARCED AT TOP OF INBD EDGE. R&R R1 WINDOW & HEAT CONTROLLER IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,922 hrs · 41,236 cycles

CROWN SKIN CRACKED AT STATION 727A, STRINGER 10L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 51,915 hrs · 41,229 cycles

LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT AFT SPAR APPROX STAB STA 127. REPAIRED DOUBLER IAW EA.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 51,915 hrs · 41,229 cycles

LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT AFT SPAR APPROX STAB STA 174. REPAIRED DOUBLER IAW EA.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 50,885 hrs · 40,500 cycles

THREE EA AFT OUTBOARD EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,736 hrs · 39,667 cycles

SKIN CRACKED AT BS 520+7, STR 10R. REPAIRED SKIN PER EA.

Part: ACTUATOR — LEAKING (NR 6 SPOILER) · airframe 49,373 hrs · 39,400 cycles

RIGHT WING NR 6 FLIGHT SPOILER ACTUATOR LEAKED. REMOVED AND REPLACED ACTUATOR IAW AMM.

Part: ACTUATOR — LEAKING (NR 2 SPOILER) · airframe 49,373 hrs · 39,400 cycles

RIGHT WING NR 2 FLIGHT SPOILER ACTUATOR LEAKED. REMOVED AND REPLACED ACTUATOR IAW AMM.

Part: ACTUATOR — LEAKING (NR 7 SPOILER) · airframe 49,373 hrs · 39,400 cycles

RIGHT WING NR 7 FLIGHT SPOILER ACTUATOR LEAKED. REMOVED AND REPLACED ACTUATOR IAW AMM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 49,373 hrs · 39,400 cycles

SHEAR TIE CRACKED AT BS 360, BETWEEN STR 19R TO STR 20R. REMOVED AND REPLACED SHEAR TIE IAW SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,373 hrs · 39,400 cycles

FUSELAGE SKIN CRACKED AT BS 360, BETWEEN STR 17R TO STR 18R. REPAIRED SKIN IAW EO AND EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 49,373 hrs · 39,400 cycles

SHEAR TIE CRACKED AT BS 520, BETWEEN STR 28L TO STR 28R. REMOVED AND REPLACED SHEAR TIE IAW SRM AND DWG.

Part: SLAT — CRACKED (RT WING) · airframe 49,373 hrs · 39,400 cycles

RIGHT WING NR 4 SLAT CRACKED. RIGHT NR 4 SLAT IAW SRM AND DWG.

Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 49,373 hrs · 39,400 cycles

LEFT KEEL BEAM CRACKED BETWEEN BS 520 TO BS 540. REPAIRED KEEL BEAM IAW EO & EA.

Part: SLAT — DELAMINATED (RT WING) · airframe 49,373 hrs · 39,400 cycles

RIGHT WING NR 5 SLAT DELAMINATED BETWEEN STA 243.40 AND STA 254.40. REPAIRED NR 5 SLAT IAW SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 49,373 hrs · 39,400 cycles

RIGHT BULKHEAD WEB CRACKED AT BS 178. REMOVED AND REPLACED WEB IAW ACO.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 49,373 hrs · 39,400 cycles

STRINGER SPLICE CORRODED AT BS 366, STR 27L. REMOVED AND REPLACED SPLICE IAW SRM AND DWG.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 49,373 hrs · 39,400 cycles

LEFT SIDE CHORD CRACKED AT BS 178, BETWEEN WL 207 AND WL 217. REMOVED AND REPLACED CHORD IAW ACO.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 49,373 hrs · 39,400 cycles

RIGHT SIDE CHORD CRACKED AT BS 178 BETWEEN WL 207 AND WL 217. REMOVED AND REPLACED CHORD IAW ACO NO.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 49,373 hrs · 39,400 cycles

STRINGER SPLICE CORRODED AT BS 791, STR 21R. REMOVED AND REPLACED SPLICE IAW SRM AND DWG.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 49,373 hrs · 39,400 cycles

STRINGER SPLICE CORRODED AT BS 791, STR 22R. REMOVED AND REPLACED SPLICE IAW SRM & DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 49,373 hrs · 39,400 cycles

STRINGER CORRODED BETWEEN BS 1018 TO BS 1138, RIGHT SIDE OF TORQUE BOX IN SECTION 48. REMOVED AND REPLACED STRINGER IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 49,373 hrs · 39,400 cycles

TIE CLIP CRACKED AT BS 328, STR 20L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,373 hrs · 39,400 cycles

FRAME CRACKED AT BS 188, STR 17L. REPAIRED FRAME IAW SRM AND DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 49,373 hrs · 39,400 cycles

STRINGER CORRODED BETWEEN BS 1088 TO BS 1156, RIGHT SIDE OF TORQUE BOX IN SECTION 48. REMOVED AND REPLACED STRINGER IAW SRM AND DWG.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 49,373 hrs · 39,400 cycles

DOUBLER CRACKED BETWEEN BS 360 TO BS 380, BETWEEN STR 28L TO STR 28R. REMOVED AND REPLACED DOUBLER IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 49,373 hrs · 39,400 cycles

TIE CLIP CRACKED AT BS 907, STR 8R. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 49,373 hrs · 39,400 cycles

TIE CLIP CRACKED AT BS 578, STR 11R. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 49,373 hrs · 39,400 cycles

TIE CLIP CRACKED AT BS 663.75, STR 10R. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 49,373 hrs · 39,400 cycles

CLIP CRACKED AT BS 706, STR 11R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 49,373 hrs · 39,400 cycles

TIE CLIP CRACKED AT BS 947.5, STR 25R. REMOVED AND REPLACED TIE CLIP IAW SRM & EA.

Part: FITTING — CRACKED (FUSELAGE) · airframe 49,373 hrs · 39,400 cycles

CLIP CRACKED AT BS 559, STR 11R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 49,373 hrs · 39,400 cycles

CLIP CRACKED AT BS 597, STR 11R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 49,373 hrs · 39,400 cycles

TIE CLIP CRACKED AT BS 663.75, STR 10L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 49,373 hrs · 39,400 cycles

ANGLE CRACKED AT BS 947.5, STR 25R. REMOVED AND REPLACED ANGLE IAW SRM, DWG, AND EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,373 hrs · 39,400 cycles

FRAME CRACKED AT BS 947.5, STR 25R. REPAIRED FRAME IAW EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 49,373 hrs · 39,400 cycles

TIE CLIP CRACKED AT BS 827, STR 9R. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 49,373 hrs · 39,400 cycles

CLIP CRACKED AT BS 706, STR 11L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 49,373 hrs · 39,400 cycles

WEB CORRODED BETWEEN BS 887 TO BS 907, STR 17R. REMOVED AND REPLACED WEB IAW EO AND EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 49,373 hrs · 39,400 cycles

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

Part: WEB — CORRODED (FUSELAGE) · airframe 49,373 hrs · 39,400 cycles

WEB CORRODED BETWEEN BS 460 TO BS 480, STR 17R. REMOVED AND REPLACED WEB IAW SRM & DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 49,373 hrs · 39,400 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 727B, RBL 45.5. REPAIRED CHORD IAW EO AND EA.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 49,373 hrs · 39,400 cycles

CREASE BEAM CRACKED AT BS 637, RBL 63. REMOVED AND REPLACED BEAM IAW SRM AND DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 49,373 hrs · 39,400 cycles

STRINGER CORRODED AT BS 947.5, STR 21R. REMOVED AND REPLACED STRINGER IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 49,373 hrs · 39,400 cycles

TIE CLIP CRACKED AT BS 360, STR 8R. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 49,373 hrs · 39,400 cycles

FLOORBEAM CRACKED AT BS 947.5, LBL 53. REPAIRED BEAM IAW EA AND EO.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 49,373 hrs · 39,400 cycles

TIE CLIP CRACKED AT BS 380, STR 8L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 49,373 hrs · 39,400 cycles

FLOORBEAM CRACKED BS 328, BETWEEN LBL 35.0 AND LBL 49.0. REPAIRED BEAM IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 49,373 hrs · 39,400 cycles

Z-ANGLE CORRODED BETWEEN BS 291.5 TO BS 360, STR 17R. REMOVED AND REPLACED Z-ANGLE IAW SRM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 49,373 hrs · 39,400 cycles

FLOORBEAM ANGLE CRACKED AT BS 328, RBL 58. REMOVED AND REPLACED ANGLE IAW DWG AND SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 49,373 hrs · 39,400 cycles

TIE CLIP CRACKED AT BS 727E, STR 26R. REMOVED AND REPLACED TIE CLIP IAW SRM & DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 49,373 hrs · 39,400 cycles

WEB CRACKED BETWEEN BS 312 TO BS 328, RBL 31. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 49,373 hrs · 39,400 cycles

FRAME CORRODED AT BS 500C, BETWEEN STR 27L TO STR 28L. REPAIRED FRAME IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,373 hrs · 39,400 cycles

STUB FRAME CRACKED AT BS 296.5, STR 7R. REPAIRED FRAME IAW EO AND EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 49,373 hrs · 39,400 cycles

WEB CRACKED AT BS 294.5+3, RBL 55. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 49,373 hrs · 39,400 cycles

FLOORBEAM CORRODED AT BS 967, RBL 27. REPAIRED CHORD IAW EO AND EA.

Part: FITTING — CRACKED (FUSELAGE) · airframe 49,373 hrs · 39,400 cycles

CLIP CRACKED AT BS 360, STR 11L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 49,373 hrs · 39,400 cycles

FRAME CORRODED AT BS 500, BETWEEN STR 28R TO STR 28L. REPAIRED FRAME IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 49,373 hrs · 39,400 cycles

FITTING CRACKED AT BS 332.1, STR 8R. REMOVED AND REPLACED FITTING IAW SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,373 hrs · 39,400 cycles

SKIN CRACKED AT BS 947.5 +11, STR 17R. REPAIRED SKIN IAW EO AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,373 hrs · 39,400 cycles

LEFT FLIGHT COMPARTMENT WINDOW C-D POST SKIN CRACKED AT BS 219. 8, STR 9L. REPAIRED SKIN IAW EO AND EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 49,373 hrs · 39,400 cycles

FRAME CORRODED AT BS 767, BETWEEN STR 25L TO STR 26L. REPAIRED FRAME IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 49,373 hrs · 39,400 cycles

FRAME CORRODED AT BS 727E, BETWEEN STR 26R TO STR 27R. REPAIRED FRAME IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,373 hrs · 39,400 cycles

FRAME CRACKED AT BS 727E, BETWEEN STR 25R TO STR 26R. REPAIRED FRAME IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 49,373 hrs · 39,400 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 727B, LBL 45.5. REPAIRED CHORD IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 49,373 hrs · 39,400 cycles

FLOORBEAM CRACKED AT BS 669, LBL 24.5. REPAIRED CHORD IAW EO AND EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 49,373 hrs · 39,400 cycles

WEB CRACKED AT BS 709, LBL 24.5. REPAIRED WEB IAW EO AND EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 49,373 hrs · 39,400 cycles

WEB CRACKED AT BS 709, BBL 0.07. REPAIRED WEB IAW EA AND EO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,364 hrs · 39,394 cycles

SKIN CUTOUT CRACKED AT BS 520+7, STR 28R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,364 hrs · 39,394 cycles

FUSELAGE SKIN CRACKED AT BS 360+18, STR 28L. REPAIRED SKIN IAW EO AND EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 49,364 hrs · 39,394 cycles

FLOORBEAM CRACKED AT BS 670.5, LBL 24.5. REPAIRED CHORD IAW EO AND EA.

Part: SIGN — BROKEN (CABIN) · airframe 49,118 hrs · 39,202 cycles

L1 DOOR EMERGENCY EXIT SIGN COVER BROKEN. REMOVED AND REPLACED SIGN ASSY IAW M/M.

Part: LENS — BROKEN (CABIN) · airframe 47,027 hrs · 37,615 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND EMERGENCY EXIT LIGHT LENS BROKEN AT ROW 22. REMOVED AND REPLACED LENS PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 46,097 hrs · 36,870 cycles

DURING SCHEDULED 14Y CHECK FOUND, SHEAR TIE CORRODED AT BS 807, BETWEEN STR 27L TO STR 27R. REPAIRED SHEAR TIE PER ER AND EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 46,097 hrs · 36,870 cycles

DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 847, BETWEEN STR 27L TO STR 27R. REPAIRED SHEAR TIE PER ER AND EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 46,097 hrs · 36,870 cycles

DURING SCHEDULED 14Y CHECK FOUND, FLOORBEAM UPPER FLANGE CHORD CORRODED AT BS 986, RBL 44. REPAIRED BEAM PER EA AND ER.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 46,097 hrs · 36,870 cycles

DURING SCHEDULED 14Y CHECK FOUND, KEEL BEAM CORRODED AT BS 787, STR 27L. REPAIRED BEAM PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,097 hrs · 36,870 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 25R. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 46,097 hrs · 36,870 cycles

DURING SCHEDULED 14Y CHECK, FOUND AFT CARGO FLOOR SUPPORT CORRODED AT BS 727D+6, LBL 8. REPAIRED SUPPORT PER EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 46,097 hrs · 36,870 cycles

DURING SCHEDULED 14Y CHECK, FOUND AFT CARGO FLOOR SUPPORT CORRODED AT BS 727D+6, RBL 8. REPAIRED SUPPORT PER EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 46,097 hrs · 36,870 cycles

DURING SCHEDULED 14Y CHECK, FOUND AFT CARGO SHEAR TIE CORRODED AT BS 907, BETWEEN STR 27L TO STR 27R. REPAIRED SHEAR TIE PER EA.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 46,097 hrs · 36,870 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 847, STR 25R. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 46,097 hrs · 36,870 cycles

DURING SCHEDULED 14Y CHECK, FOUND AFT CARGO FLOOR SUPPORT CORRODED AT BS 727D+6, LBL 3. REPAIRED SUPPORT PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 46,097 hrs · 36,870 cycles

DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727D, BETWEEN STR 26R TO STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 46,097 hrs · 36,870 cycles

DURING SCHEDULED 14Y CHECK, FOUND AFT CARGO FLOOR SUPPORT CORRODED AT BS 727D+6, RBL 3. REPAIRED SUPPORT PER SRM.

Part: LENS — MISSING (CABIN) · airframe 46,097 hrs · 36,870 cycles

DURING SCHEDULED 14Y CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 46,097 hrs · 36,870 cycles

DURING SCHEDULED 14Y CHECK, FOUND LONGITUDINAL FLOORBEAM ATTACH CLIP CRACKED AT BS 639, LBL 45.5. REMOVED AND REPLACED CLIP ER AND EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 46,097 hrs · 36,870 cycles

DURING SCHEDULED 14Y CHECK, FOUND AFT CARGO FLOOR SUPPORT CORRODED AT BS 767+6, RBL 3. REPAIRED SUPPORT PER EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 46,097 hrs · 36,870 cycles

DURING SCHEDULED 14Y CHECK, FOUND AFT CARGO FLOOR SUPPORT CORRODED AT BS 767+6, LBL 3. REPAIRED SUPPORT PER EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 46,097 hrs · 39,870 cycles

DURING SCHEDULED 14Y CHECK, FOUND AFT CARGO SHEAR TIE CORRODED AT BS 747, BETWEEN STR 27R TO STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 46,097 hrs · 39,870 cycles

DURING SCHEDULED 14Y CHECK, FOUND AFT CARGO FLOOR SUPPORT CORRODED AT BS 767+6, LBL 8. REPAIRED SUPPORT PER EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 46,097 hrs · 39,870 cycles

DURING SCHEDULED 14Y CHECK, FOUND AFT CARGO FLOOR SUPPORT CORRODED AT BS 767+6, RBL 8. REPAIRED SUPPORT PER EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 46,097 hrs · 39,870 cycles

DURING SCHEDULED 14Y CHECK, FOUND AFT CARGO SHEAR TIE CORRODED AT BS 727C, BETWEEN STR 26L TO STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 46,097 hrs · 36,870 cycles

DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 907, BETWEEN STR 26L TO STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 46,097 hrs · 36,870 cycles

DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 927, BETWEEN STR 26R TO STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 46,097 hrs · 36,870 cycles

DURING SCHEDULED 14Y CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, LBL 17.0. REPAIRED WEB PER SRM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 45,503 hrs · 36,445 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,425 hrs · 34,902 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 380, STR 3R. REPAIRED SKIN PER AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,425 hrs · 34,902 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 470, STR 4R. REPAIRED SKIN PER AAR EA.

Part: LENS — MISSING (CABIN) · airframe 42,751 hrs · 34,423 cycles

L2 DOOR EMERGENCY EXIT LIGHT LENS MISSING. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 42,439 hrs · 34,182 cycles

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

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 40,565 hrs · 32,814 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT WING NR 2 SLAT I/B TRAILING EDGE WEDGE DELAMINATED. REPAIRED WEDGE PER SWA EA.

Part: SLAT — DELAMINATED (LT WING) · airframe 40,565 hrs · 32,814 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT NR 2 SLAT DELAMINATED. REPAIRED NR 2 SLAT PER SRM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 40,507 hrs · 32,774 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: COVER — MISSING (CABIN) · airframe 40,343 hrs · 32,656 cycles

L2 DOOR EEPLS COVER MISSING. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 40,229 hrs · 32,569 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: RETAINER — LOOSE (L1 DOOR) · airframe 40,229 hrs · 32,569 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FWD STOW MOUNT LOOSE. SECURED RETAINER PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 40,063 hrs · 32,452 cycles

DURING SCHEDULED 12Y CHECK, FOUND VERTICAL BEAM CRACKED AT BS 178, RBL 17, WL 230. REPAIRED BEAM PER SRM.

Part: SLAT — DELAMINATED (LT WING) · airframe 40,063 hrs · 32,452 cycles

DURING SCHEDULED 12Y CHECK, FOUND LT WING O/B LEADING EDGE NR 2 SLAT DELAMINATED. REPAIRED SLAT PER SRM.

Part: SLAT — DELAMINATED (RT WING) · airframe 40,063 hrs · 32,452 cycles

DURING SCHEDULED 12Y CHECK, FOUND RT WING NR 5 SLAT I/B UPPER CORNER DELAMINATED. REPAIRED SLAT PER SRM.

Part: LIGHT — CRACKED (CABIN) · airframe 40,063 hrs · 32,452 cycles

DURING SCHEDULED 12Y CHECK, FOUND FWD EEPLS CRACKED. REMOVED AND REPLACED EEPLS PER MM.

Part: SLAT — DELAMINATED (RT WING) · airframe 40,063 hrs · 32,452 cycles

DURING SCHEDULED 12Y CHECK, FOUND RT WING NR 5 SLAT O/B UPPER CORNER DELAMINATED. REPAIRED SLAT PER SRM.

Part: SLAT — DELAMINATED (RT WING) · airframe 40,063 hrs · 32,452 cycles

DURING SCHEDULED 12Y CHECK, FOUND RT WING NR 6 SLAT O/B UPPER CORNER DELAMINATED. REPAIRED SLAT PER SRM.

Part: SKIN — PUNCTURED (L1 DOOR) · airframe 40,063 hrs · 32,452 cycles

DURING SCHEDULED 12Y CHECK, FOUND L1 DOOR INNER SKIN FWD OF DOOR WINDOW ABOVE DOOR HANDLE SKIN PUNCTURED. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 40,063 hrs · 32,452 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 25L. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 440,063 hrs · 32,452 cycles

DURING SCHEDULED 12Y CHECK, FOUND LT WING O/B LEADING EDGE NR 1 SLAT LOWER T/E SKIN CRACKED. REPAIRED SLAT PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 440,063 hrs · 32,452 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 5L. REMOVED AND REPLACED CLIP PER SRM.

Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 39,850 hrs · 32,288 cycles

DURING SCHEDULED MV1 CHECK, FOUND RT KEEL BEAM LOWER SKIN CRACKED AT BS 715. REPAIRED BEAM PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,372 hrs · 39,400 cycles

RIGHT KEEL BEAM LOWER SKIN CRACKED BETWEEN BS 705 TO BS 727. REPAIRED SKIN IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 39,251 hrs · 31,862 cycles

DURING SCHEDULED SPECIAL VISIT CHECK, FOUND SHEAR TIE CORRODED AT BS 767, STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 39,257 hrs · 31,867 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 767 BETWEEN STR 26L TO STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 39,251 hrs · 31,862 cycles

DURING SCHEDULED SPECIAL VISIT CHECK, FOUND SHEAR TIE CORRODED AT BS 747, STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 39,251 hrs · 31,862 cycles

DURING SCHEDULED SPECIAL VISIT CHECK, FOUND SHEAR TIE CORRODED AT BS 767, STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 39,231 hrs · 31,851 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 440, LOWER DOOR STOP. REMOVED AND REPLACED FRAME PER SWA ACO.

Part: FLAP — DELAMINATED (LT WING) · airframe 39,231 hrs · 31,851 cycles

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

Part: COVER — MISSING (CABIN) · airframe 39,197 hrs · 31,828 cycles

L2 DOOR EMERGENCY EXIT SIGN COVER MISSING. REMOVED AND REPLACED SIGN PER MM.

Part: FLOORBEAM — CORRODED (BS 270) · airframe 39,057 hrs · 31,736 cycles

DURING SCHEDULED MV2 CHECK, FOUND FLOORBEAM SUPPORT CORRODED AT BS 270, RBL 12. REMOVED AND REPLACED BEAM PER SRM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 35,700 hrs · 29,292 cycles

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

Part: SLIDE — OUT OF LIMITS (L2 DOOR) · airframe 35,420 hrs · 29,091 cycles

L2 DOOR EMERGENCY EVAC SLIDE OUT OF LIMITS. REMOVED AND REPLACED L2 DOOR EMERGENCY EVAC SLIDE PER MM.

Part: SLIDE — LOW PRESSURE (L1 DOOR) · airframe 35,471 hrs · 29,128 cycles

L1 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: DOOR — OUT OF ADJUST (COCKPIT) · airframe 34,902 hrs · 28,682 cycles

F/O'S ESCAPE ROPE DOOR DOES NOT OPEN. ADJUSTED DOOR PER MM.

Part: LENS — BROKEN (CABIN) · airframe 34,527 hrs · 28,369 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,987 hrs · 27,940 cycles

DURING SCHEDULED 10Y CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,968 hrs · 27,925 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 706, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FLAP — DELAMINATED (LT WING) · airframe 33,968 hrs · 27,925 cycles

DURING SCHEDULED 10Y CHECK, FOUND LEFT WING INBOARD T/E AFT FLAP DELAMINATED AT OUTBOARD END. REPAIRED FLAP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,968 hrs · 27,925 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,968 hrs · 27,925 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,968 hrs · 27,925 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,968 hrs · 27,925 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,968 hrs · 27,925 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FITTING — CORRODED (L1 DOOR) · airframe 33,968 hrs · 27,925 cycles

DURING SCHEDULED 10Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED GIRT BAR FITTING PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,968 hrs · 27,925 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,968 hrs · 27,925 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FITTING — CORRODED (L1 DOOR) · airframe 33,968 hrs · 27,925 cycles

DURING SCHEDULED 10Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CORRODED. REMOVED AND REPLACED GIRT BAR FITTING PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,968 hrs · 27,925 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727A, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,968 hrs · 27,925 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 807, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,968 hrs · 27,925 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,968 hrs · 27,925 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 580, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FITTING — CORRODED (HORIZ STAB) · airframe 33,968 hrs · 27,925 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,968 hrs · 27,925 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,968 hrs · 27,925 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L AND STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 867 S8L) · airframe 33,968 hrs · 27,925 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 727B S8L) · airframe 33,968 hrs · 27,925 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 400 S8L) · airframe 33,968 hrs · 27,925 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 907 S8R) · airframe 33,968 hrs · 27,925 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 787 S10L) · airframe 33,968 hrs · 27,925 cycles

DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: CREASE BEAM — CORRODED (BS 312-344 S17L) · airframe 33,968 hrs · 27,925 cycles

DURING SCHEDULED 10Y CHECK, FOUND CREASE BEAM CHORD CORRODED BETWEEN BS 312 AND BS 344, STR 17L. REPAIRED CHORD PER SRM.

Part: FRAME — CRACKED (BS 827 S8R) · airframe 33,968 hrs · 27,925 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 727C S10L) · airframe 33,968 hrs · 27,925 cycles

DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,968 hrs · 27,925 cycles

DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,968 hrs · 27,925 cycles

DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,968 hrs · 27,925 cycles

DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 847, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,968 hrs · 27,925 cycles

DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 6R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,968 hrs · 27,925 cycles

DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,968 hrs · 27,925 cycles

DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,968 hrs · 27,925 cycles

DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,968 hrs · 27,925 cycles

DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727F, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SLAT — CRACKED (RT WING) · airframe 33,959 hrs · 27,916 cycles

DURING SCHEDULED C1 CHECK, FOUND RIGHT WING NR 6 L/E SLAT CRACKED AT INBOARD L/E. REPAIRED SLAT PER SWA EA.

Part: LENS — LOOSE (CABIN) · airframe 33,849 hrs · 27,843 cycles

LEFT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LIGHT LENS PER MM.

Part: STRUCTURE — CRACKED (NR 6 SLAT) · airframe 33,657 hrs · 27,699 cycles

DURING SCHEDULED C1 CHECK, FOUND RIGHT WING NR 6 L/E SLAT CRACKED AT OUTBOARD T/E. REPAIRED SLAT PER SWA EA.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 33,053 hrs · 27,234 cycles

DURING SCHEDULED A1 CHECK, FOUND LEFT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: GLOWSTRIP — WORN (CABIN) · airframe 32,785 hrs · 27,039 cycles

EEPLS PHOTO LUMINESCENT STRIP WORN AT ROW 6 ABC TO ROW 8 ABC. REMOVED AND REPLACED PHOTO LUMINESCENT STRIP PER MM.

Part: GLOWSTRIP — WORN (CABIN) · airframe 31,789 hrs · 26,234 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 2 DEF. REMOVED AND REPLACED PHOTOLUMINESCENT STRIP PER MM.

Part: LATCH — BROKEN (ESCAPE ROPE DOOR) · airframe 31,512 hrs · 26,063 cycles

FIRST OFFICER'S EMERGENCY ESCAPE ROPE DOOR LATCH BROKEN. REMOVED AND REPLACED DOOR LATCH PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 31,022 hrs · 25,667 cycles

DURING SCHEDULED MV1 CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: STRIP — LOOSE (CABIN) · airframe 30,269 hrs · 25,063 cycles

EEPLS STRIP LOOSE AT ROW 9 ABC. SECURED EEPLS PER MM.

Part: SLIDE — MISINSTALLED (L1 DOOR) · airframe 29,228 hrs · 24,271 cycles

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

Part: HINGE — CRACKED (L1 DOOR) · airframe 27,225 hrs · 22,660 cycles

DURING SCHEDULED C2 CHECK, FOUND L1 DOOR UPPER HINGE BOX LOWER RADIUS CRACKED. REMOVED AND REPLACED UPPER HINGE BOX PER SRM.

Part: SKIN — DELAMINATED (RT WING FOREFLAP) · airframe 25,362 hrs · 21,261 cycles

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

Part: LATCH — LOOSE (L2 GIRT BAR) · airframe 25,362 hrs · 21,261 cycles

DURING SCHEDULED C4 CHECK, FOUND L2 DOOR EVAC SLIDE GIRT BAR FWD FLOOR LATCH LOOSE. SECURED L2 DOOR EVAC SLIDE FWD FLOOR LATCH PER MM.

Part: ENGINE — LEAKING (NR 3) · airframe 22,235 hrs · 18,741 cycles

SMOKE SMELL IN THE CABIN. SUSPECTED NR 2 ENG, NR 3 BEARING OIL SEAL FAILURE. REMOVED AND REPLACED NR 2 ENG PER MT.

Part: SKIN — DELAMINATED (LT WING FLAP) · airframe 21,575 hrs · 18,214 cycles

DURING SCHEDULED C4 CHECK, FOUND LT OUTBD AFT T/E FLAP DELAMINATED AT INBOARD CORNER. REMOVED AND REPLACED OUTBOARD AFT T/E FLAP PER MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 20,683 hrs · 17,486 cycles

DURING SCHEDULED C3 CHECK, FOUND RT INBD AFT T/E FLAP DELAMINATED AT OUTBD END. REMOVED AND REPLACED RT INBD AFT T/E FLAP PER MM.

Part: SLIDE — OUT OF ADJUST (L1 AND L2 DOORS) · airframe 19,764 hrs · 16,737 cycles

DURING SCHEDULED C2 CHECK, FOUND BOTH ENTRY DOOR EVACUATION SLIDES OUT OF ADJUST. REPOSITIONED BOTH SLIDES PER MM

Part: TRUNNION PIN — CORRODED (LT/RT MLG) · airframe 19,180 hrs · 16,275 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BOTH LT AND RT MLG TRUNNION PINS CORRODED. REMOVED AND REPLACED BOTH LT AND RT MLG TRUNNION PINS PER MM.

Part: ROD END — WORN (ELEVATOR) · airframe 18,927 hrs · 16,062 cycles

DURING SCHEDULED SERVICE CHECK, SWA SI 11139-55, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED LEFT ELEVATOR TAB AFT OTBD CONTROL ROD END PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 17,864 hrs · 15,172 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 17,169 hrs · 14,630 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER TIE CLIP CRACKED AT BS 767, STR 25L. REMOVED AND REPLACED TIE CLIP PER SRM.

Part: FLOORBEAM — CORRODED (AFT CARGO) · airframe 17,169 hrs · 14,630 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 772, LBL 3, LBL 8 AND RBL 3. REPAIRED FLOORBEAM PER SWA RA.

Part: COVER — CRACKED (CABIN) · airframe 16,669 hrs · 14,229 cycles

DURING SCHEDULED RON, FOUND EEPLS COVER CRACKED AT ROW NR 3. REMOVED AND REPLACED COVER PER MM.

Part: SLIDE — OUT OF ADJ (ENTRY DOOR) · airframe 13,992 hrs · 12,085 cycles

DURING SCHEDULED C4 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUSTMENT. ADJUSTED SLIDE ASSY PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 13,992 hrs · 12,085 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS LOOSE AT ROWS 8 & 9. SECURED EEPLS PER MM.

Part: SLIDE — OUT OF ADJ (ENTRY DOOR) · airframe 13,339 hrs · 11,529 cycles

FWD DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. READJUSTED EVAC SLIDE ASSY PER MM.

Part: MODULE — INOPERATIVE (MLG WW) · airframe 12,373 hrs · 10,678 cycles

DIVERSION, LOST NR 1 & NR 2 ENG DRIVEN HYD PUMPS, LOW PRESS LIGHTS ILLUMINATED. PRESS AND QUANTITIES REMAINED NORMAL. REMOVED AND REPLACED RESERVOIR PRESS MODULE, OPS CHECK GOOD. LEAK CHECK GOOD AND CHECKED CASE DRAIN FILTERS PER MM.

Part: RETAINER — LOOSE (ENTRY DOOR) · airframe 12,058 hrs · 10,512 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR GIRT BAR FWD RETAINER HOOK LOOSE. SECURED RETAINER HOOK PER MM.

Part: COVER — WORN (CABIN) · airframe 12,058 hrs · 10,512 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS TRACK COVER WORN AT EMERGENCY EXIT. R&R TRACK COVER PER MM.

Part: PROXIMITY SWITCH — INOPERATIVE (NLG) · airframe 11,634 hrs · 10,149 cycles

DURING GEAR RETRACTION ON TAKEOFF, NOSE GEAR RED LIGHT REMAINED ILLUMINATED THE ENTIRE FLIGHT UNTIL EXTENSION. GEAR EXTENSION WAS NORMAL. REMOVED AND REPLACED 846 PROX SWITCH PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR)

FWD SERVICE DOOR EMERGENCY ESCAPE SLIDE NOT STOWED PROPERLY IN CONTAINER. REPOSITIONED SLIDE PROPERLY PER MM.

Part: EGT IND — INOPERATIVE (NR 1 ENGINE)

EN ROUTE, AIRCRAFT DIVERT TO MDW DUE TO NR 1 EGT INOPERATIVE. AIRCRAFT MADE AN UNEVENFUL LANDING. REMOVED AND REPLACED NR 1 EGT INDICATOR PER BOEING MM.

Part: SKIN — PUNCTURED (FUSELAGE)

DURING SCHEDULED RON CHECK, FOUND LT FUSELAGE BEHIND LT WING HAS A LARGE HOLE, FROM BEING STRUCK BY BAGGAGE CART. REPAIRED PER BOEING SRM.

Part: APU — INOPERATIVE (AFT FUSELAGE)

AT GATE NOTICED SMOKE IN CABIN. HEAVY SMOKE OUT OF APU TAILPIPE, APU INOP. REMOVED AND REPLACED APU PER BOEING MM.

Part: HYD SYST — OVERSERVICED (A-HYD SYST)

ON TAKEOFF, CREW NOTED A RUBBER TYPE BURN SMELL COMING THROUGH DUCT SYSTEM. NO VISIBLE SMOKE. ODOR DISSIPATED AT LOWER THRUST SETTING. AIRCRAFT RETURNED TO MDW AND MADE AN UNEVENTFUL LANDING. INSPECTED AIRCRAFT, FOUND A SYSTEM HYD RESERVOIR OVERSERVICED. DESERVICED TO PROPER LEVEL AND PERFORMED ENGINE POWER ASSURANCE RUN PER BOEING M/M.