N621SW

Part: LENS — MISSING (CABIN) · airframe 66,393 hrs · 52,416 cycles

R1 DOOR EMERGENCY "EXIT" LIGHT COVER LENS MISSING. INSTALLED LENS PER SIP.

Part: LENS — LOOSE (CABIN) · airframe 65,989 hrs · 52,143 cycles

R1 DOOR EMERGENCY EXIT LIGHT LENS LOOSE. R&R LIGHT ASSEMBLY PER SIP.

Part: FLAP — DELAMINATED (RT WING) · airframe 65,070 hrs · 51,560 cycles

RIGHT WING OTBD AFT FLAP DELAMINATED ON INBD LOWER CORNER. R & R AFT FLAP IAW AMM.

Part: BRACKET — CRACKED (TE FLAP) · airframe 65,070 hrs · 51,560 cycles

LEFT WING INBD FLAP, OTBD TRACK, OTBD UPPER ANGLE CRACKED. R & R BRACKET IAW SRM.

Part: LENS — LOOSE (EXIT SIGN) · airframe 64,733 hrs · 51,345 cycles

FORWARD ENTRY EXIT SIGN LENS LOOSE. R & R LENS IAW SIP.

Part: SKIN — CRACKED (RT WING) · airframe 63,996 hrs · 50,845 cycles

RIGHT WING REAR SPAR UPPER CHORD SKIN CRACKED, AT RSS 226.1. REPAIRED SKIN IAW ER & EA.

Part: SKIN — CRACKED (RT WING) · airframe 63,996 hrs · 50,845 cycles

RIGHT WING UPPER SKIN CRACKED, AT FASTENER HOLE COMMON TO THE SKIN TE, AT RSS 253. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 63,996 hrs · 50,845 cycles

RIGHT WING UPPER SKIN, TE FASTENER HOLE COMMON TO THE REAR SPAR UPPER CHORD CRACKED AT RSS 205. REPAIRED SKIN IAW EA & ER.

Part: SKIN — CRACKED (LT WING) · airframe 63,996 hrs · 50,845 cycles

LEFT WING LOWER SURFACE OF WING UPPER SKIN CRACKED BETWEEN, RSS. 253 - 266. REPAIRED SKIN IAW EA.

Part: FITTING — CRACKED (LT MLG) · airframe 63,996 hrs · 50,845 cycles

LEFT MLG OTBD D FITTING CRACKED AT RSS 224.14, HOLE NR 5. REPAIRED FITTING IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 63,996 hrs · 50,845 cycles

LEFT WING, WING UPPER SKIN CRACKED IN THE HOLE LOCATED AT LT RSS 221. REPAIRED SKIN IAW EA.

Part: SUPPORT FITTING — CRACKED (RT WING) · airframe 63,996 hrs · 50,845 cycles

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

Part: LINK — CORRODED (RT MLG) · airframe 63,996 hrs · 50,845 cycles

RIGHT MLG SUPPORT BEAM SWING LINK CORRODED ON FACE & EMANATING FROM BUSHING. R & R LINK ASSEMBLY IAW AMM & EA.

Part: SPAR — CRACKED (RT WING) · airframe 63,996 hrs · 50,845 cycles

RIGHT WING REAR SPAR, UPPER CHORD CRACKED AT THE NR 5 AFT FITTING HOLE. REPAIRED CHORD IAW ER & EA.

Part: SPAR — CRACKED (RT WING) · airframe 63,996 hrs · 50,845 cycles

RIGHT WING REAR SPAR WEB CRACKED AT THE NR 5 AFT FITTING HOLE. REPAIRED WEB IAW ER & EA.

Part: SPAR — CRACKED (LT WING) · airframe 63,996 hrs · 50,845 cycles

LEFT WING REAR SPAR WEB CRACKED, AT THE NR 5 AFT FITTING HOLE, BETWEEN RSS 211 - 238. REPAIRED WEB IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 63,996 hrs · 50,845 cycles

LEFT WING REAR SPAR, UPPER CHORD CRACKED AT THE NR 5 AFT FITTING HOLE AT RSS 285. REPAIRED CHORD IAW IA.

Part: WINDSHIELD — ARCED (COCKPIT) · airframe 63,965 hrs · 50,827 cycles

DIVERSION & DECLARED EMER. R1 WINDSHIELD ARCED, THEN CRACKED AT FL 370. R & R R1 WINDSHIELD IAW AMM.

Part: LENS — UNSECURE (CABIN) · airframe 63,233 hrs · 50,333 cycles

R1 DOOR EMER EXIT SIGN LIGHT, LENS IN FWD GALLEY FELL OFF. REPAIRED LENS IAW EA.

Part: LENS — LOOSE (CABIN) · airframe 63,057 hrs · 50,209 cycles

AFT CABIN OVERHEAD EXIT SIGN LENS COVER LOOSE. R & R COVER IAW AMM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 63,057 hrs · 50,209 cycles

SHEAR TIE CRACKED, BETWEEN BS 927 - 947, STRINGER 26R. R & R SHEAR TIE IAW SRM & DWG.

Part: SHEAR WEB — CRACKED (FUSELAGE) · airframe 63,057 hrs · 50,209 cycles

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

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 63,057 hrs · 50,209 cycles

STRINGER SPLICE CRACKED AT BS 360, STRINGER 2L. R & R STRINGER SPLICE IAW EA & AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,057 hrs · 50,209 cycles

FORWARD LOWER CORNER OF AFT GALLEY DOOR CUT OUT CRACKED. REPAIRED CUT OUT IAW SRM.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 63,057 hrs · 50,209 cycles

L1 DOOR SURROUND STRUCTURE, ATTACH CLIP CRACKED AT BS 348.2, STRINGER 16L. R & R CLIP IAW SRM & DWG.

Part: RIB — CRACKED (RT WING) · airframe 63,057 hrs · 50,209 cycles

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

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 63,057 hrs · 50,209 cycles

L1 DOOR CUT OUT AROUND FASTENER SHEAR TIE CORRODED AT BS 302, STRINGER 14L. R & R CLIP IAW SRM & DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 63,057 hrs · 50,209 cycles

SHEAR TIE CORRODED AT BS 500C, STRINGER 24R. R & R SHEAR TIE IAW DWG & SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 63,057 hrs · 50,209 cycles

SHEAR TIE CORRODED AT BS 500B, BETWEEN BL 0 TO LBL 6. REPAIRED SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 63,057 hrs · 50,209 cycles

SHEAR TIE CORRODED AT BS 500A, BETWEEN RBL 5 TO LBL 3. R & R SHEAR TIE IAW SRM.

Part: BEAM — CRACKED (FUSELAGE) · airframe 63,057 hrs · 50,209 cycles

LONGITUDINAL BEAM UPPER CHORD CRACKED AT BS 727B, RBL 24.8. REPAIRED CHORD IAW EA & ER.

Part: ATTACH FITTING — CORRODED (FLAP TRACK) · airframe 63,057 hrs · 50,209 cycles

LEFT WING NR 1 FLAP TRACK, AFT OTBD ATTACH FITTING CORRODED ON UPPER SURFACE. R & R FITTING IAW SRM & DWG.

Part: SUPPORT FITTING — CORRODED (RT WING) · airframe 63,057 hrs · 50,209 cycles

RIGHT WING NR 7 FLAP TRACK AFT SUPPORT FITTING CORRODED. REPAIRED FITTING IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 63,057 hrs · 50,209 cycles

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

Part: SUPPORT FITTING — CORRODED (FLAP TRACK) · airframe 63,057 hrs · 50,209 cycles

RIGHT WING NR 8 FLAP, AFT TRACK SUPPORT FITTING CORRODED AT OTBD BOLT HOLE, UPPER SURFACE. R & R FITTING IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,057 hrs · 50,209 cycles

FORWARD CARGO COMPARTMENT, FRAME CRACKED AT BS 500B, STRINGER 20R. REPAIRED FRAME IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 63,057 hrs · 50,209 cycles

FRAME SHEAR TIE, CORRODED AT BS 1006, BETWEEN STRINGER 27L - 27R. R & R SHEAR TIE IAW SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 63,057 hrs · 50,209 cycles

STRINGER CORRODED BETWEEN BS 898 - 902, STRINGER 21R. REPAIRED STRINGER IAW SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 63,057 hrs · 50,209 cycles

STRINGER CORRODED AT BS 987, STRINGER 25L. REMOVED & REPAIRED STRINGER IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 63,057 hrs · 50,209 cycles

FRAME SHEAR TIE, CORRODED AT BS 747, STRINGER 27L. R & R SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 63,057 hrs · 50,209 cycles

SHEAR TIE CORRODED AT BS 947, BETWEEN STRINGER 25R - 26R. R & R SHEAR TIE IAW SRM & DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 63,057 hrs · 50,209 cycles

LEFT INBD CREASE BEAM CHORD CORRODED, BETWEEN BS 950 TO 994, LBL 65. R & R CHORD IAW SRM & DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 63,057 hrs · 50,209 cycles

SHEAR TIE CORRODED AT BS 787, STRINGER 27L. REPAIRED SHEAR TIE IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 63,057 hrs · 50,209 cycles

RIGHT CREASE BEAM WEB CORRODED BETWEEN BS 440 - 460. R & R WEB IAW SRM & DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,057 hrs · 50,209 cycles

FRAME LOWER FLANGE CORRODED AT BS 1006, BETWEEN STRINGER 22R - 23R. REPAIRED FLANGE IAW EA & DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 63,057 hrs · 50,209 cycles

CREASE BEAM WEB CORRODED BETWEEN BS 807 - 827 LT. R & R WEB IAW SRM & DWG.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 63,057 hrs · 50,209 cycles

AFT PRESS BULKHEAD WEB CORRODED AT BS 1016, BETWEEN STRINGER 26L - 26R. REPAIRED WEB IAW EA.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 63,057 hrs · 50,209 cycles

AFT PRESS BULKHEAD CHANNEL STIFFENER CORRODED AT BS 1016, BETWEEN STRINGER 27L - 27R. REPAIRED STIFFENER IAW EA.

Part: BRACKET — CRACKED (LT WING) · airframe 61,662 hrs · 49,234 cycles

LEFT WING UPPER TE PANEL CRACKED BRACKET AT THE OTBD SIDE OF PYLON. R & R BRACKET IAW SRM.

Part: ANGLE — DAMAGED (FUSELAGE) · airframe 60,528 hrs · 48,444 cycles

INTERCOSTAL ANGLE DAMAGED AT BS 348.2, BETWEEN STRINGER 13L TO 17L. R & R ANGLE IAW EA.

Part: SPOILER — CRACKED (LT WING) · airframe 60,141 hrs · 48,166 cycles

LEFT WING INBD SPOILER CRACKED. R & R SPOILER IAW AMM.

Part: RETAINER — CRACKED (VERTICAL STAB) · airframe 59,968 hrs · 48,041 cycles

VERTICAL STABILIZER PANEL 9507 RETAINER CRACKED. R & R RETAINER IAW SRM.

Part: LENS — LOOSE (CABIN) · airframe 59,968 hrs · 48,041 cycles

LEFT EMER EXIT OVERHEAD LENS COVER LOOSE. R & R COVER IAW AMM.

Part: SLIDE — DEPLOYED (L2 DOOR) · airframe 59,840 hrs · 47,957 cycles

L2 DOOR EMER EVAC SLIDE DEPLOYED DURING EMER. R & R SLIDE IAW MT.

Part: SMOKE WARNING — FALSE ACTIVATION (COCKPIT) · airframe 59,840 hrs · 47,957 cycles

DIVERSION & DECLARED EMER. DIVERTED FOR FIRE INDICATION IN FWD CARGO BIN. FWD CARGO BIN INSPECTION SHOWED NO EVIDENCE OF FIRE OR HEAT DAMAGE. R & R LT CARGO HALON BOTTLE IAW MM.

Part: SLIDE — DEPLOYED (L1 DOOR) · airframe 59,840 hrs · 47,957 cycles

L1 DOOR EMER EVAC SLIDE DEPLOYED FOR EVACUATION. R & R SLIDE IAW MT.

Part: SMOKE WARNING — FALSE ACTIVATION (COCKPIT) · airframe 59,840 hrs · 47,957 cycles

DIVERSION & DECLARED EMER. DIVERTED FOR FIRE INDICATION IN FWD CARGO BIN. FWD CARGO BIN INSPECTION SHOWED NO EVIDENCE OF FIRE OR HEAT DAMAGE. R & R RT CARGO HALON BOTTLE IAW MM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 58,793 hrs · 47,230 cycles

L1 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OFF, DID NOT DEPLOY, STILL OPERATIONAL. REINSTALLED SLIDE IAW MT.

Part: ACTUATOR — FAULTY (LT MLG) · airframe 58,522 hrs · 47,038 cycles

AIR TURN BACK RED LT GEAR LIGHT ILLUMINATED WITH GEAR HANDLE UP. WHEN HANDLE MOVED TO OFF GREEN LT GEAR LIGHT ILLUMINATES WITH ADDITIONAL WIND NOISE. R & R LT MLG RETRACT ACTUATOR IAW MM.

Part: SLAT — CRACKED (RT WING) · airframe 58,111 hrs · 46,755 cycles

RT WING NR 6 SLAT CRACKED. REPAIRED SLAT IAW SRM.

Part: SUPPORT BRACKET — CRACKED (RT PYLON) · airframe 57,501 hrs · 46,344 cycles

RT PYLON SUPPORT BRACKETS FOR PANEL 58710R CRACKED IN SEVERAL AREAS. R & R BRACKET IAW AMM.

Part: PUMP — FAILED (NR 2 ENGINE) · airframe 57,399 hrs · 46,273 cycles

IN FLIGHT SHUT DOWN, DIVERSION NR 2 ENGINE ROLLED BACK & SHUT DOWN IN FLIGHT. R & R NR 2 ENGINE MEC FUEL PUMP ASSEMBLY IAW MT.

Part: SLAT — DELAMINATED (RT WING) · airframe 56,936 hrs · 45,912 cycles

RT WING NR 5 SLAT OTBD UPPER CORNER DELAMINATED. R&R NR 5 SLAT IAW MM.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 56,921 hrs · 45,897 cycles

VERTICAL L ANGLE CRACKED AT AFT SIDE OF CUTOUT FOR PANEL 5858R. R&R BRACKET IAW SRM & DRAWING.

Part: STRAP — CRACKED (FUSELAGE) · airframe 56,921 hrs · 45,897 cycles

FLOOR BEAM STABILIZER STRAP CRACKED AT BS 312, RBL 31. R&R STRAP IAW SRM.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 56,921 hrs · 45,897 cycles

LT WING TE AILERON WIPER WEB SUPPORT ANGLE CRACKED AT RSS 545. R&R ANGLE IAW SRM.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 56,921 hrs · 45,897 cycles

LT WING TE UPPER PANEL SUPPORT ANGLE CRACKED JUST OTBD OF PYLON. R&R ANGLE IAW SRM.

Part: FITTING — CRACKED (LT WING) · airframe 56,921 hrs · 45,897 cycles

LT WING TE UPPER PANEL MIDDLE SUPPORT ANGLE FORWARD CLIP ON INNER PART OF PYLON INBD SIDE CRACKED. R&R CLIP IAW SRM.

Part: PANEL — CRACKED (NLG WW) · airframe 56,921 hrs · 45,897 cycles

NLG WW LT PANEL CRACKED AT BS 246. REPAIRED PANEL IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 56,921 hrs · 45,897 cycles

SHEAR TIE CORRODED AT BS 767, BETWEEN STRINGER 26L AND STRINGER 27L. REPAIRED SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 56,921 hrs · 45,897 cycles

SHEAR TIE CORRODED AT BS 807, BETWEEN STRINGER 27L AND STRINGER 27R. REPAIRED SHEAR TIE IAW SRM.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 56,921 hrs · 45,897 cycles

CHORD CRACKED AT BS 727, STRINGER 18A LT IN THE LOWER FWD HOLE. REPAIRED CHORD IAW ER & EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 56,921 hrs · 45,897 cycles

SHEAR TIE CORRODED AT BS 767, BETWEEN STRINGER 27L & STRINGER 27R. REPAIRED SHEAR TIE IAW SRM.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 56,921 hrs · 45,897 cycles

MAIN WW PRESSURE DECK WEB CRACKED AT BS 664, LBL 33. REPAIRED WEB IAW ER & EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 56,921 hrs · 45,897 cycles

SHEAR TIE CORRODED AT STATION 767, BETWEEN STRINGER 25L & STRINGER 26L. REPAIRED SHEAR TIE IAW SRM.

Part: SHEAR TIE — DAMAGED (FUSELAGE) · airframe 56,921 hrs · 45,897 cycles

SHEAR TIE PILLOWING AT BS 807, BETWEEN STRINGER 26R & STRINGER 27R. REPAIRED SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 56,921 hrs · 45,897 cycles

SHEAR TIE CORRODED AT BS 767, BETWEEN STRINGER 27R & STRINGER 26R. REPAIRED SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 56,921 hrs · 45,897 cycles

SHEAR TIE CORRODED STATION 807, BETWEEN STRINGER 25L & STRINGER 26L. REPAIRED SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 56,921 hrs · 45,897 cycles

FRAME SHEAR TIE CORRODED AT BS 807, BETWEEN STRINGER 26L & STRINGER 27L. REPAIRED SHEAR TIE IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,921 hrs · 45,897 cycles

AFT ENTRY DOOR CUT OUT FWD LOWER CORNER CRACKED. REPAIRED CUT OUT IAW SRM.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 56,921 hrs · 45,897 cycles

MAIN WW PRESSURE DECK WEB CRACKED AT BS 664, LBL 15. REPAIRED WEB IAW ER & EA.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 56,921 hrs · 45,897 cycles

CHORD CRACKED AT BS 727, STRINGER 18A RT IN THE LOWER FWD HOLE. REPAIRED CHORD IAW ER & EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 56,921 hrs · 45,897 cycles

SHEAR TIE CORRODED AT BS 947, BETWEEN STRINGER 27L & STRINGER 27R. R&R SHEAR TIE IAW SRM.

Part: ACCESS PANEL — CRACKED (FUSELAGE) · airframe 56,921 hrs · 45,897 cycles

ACCESS PANEL 5864R CRACKED AT CORNER OF FASTENER HOLE. REPAIRED PANEL IAW SRM.

Part: BAR — LOOSE (RT MLG DOOR) · airframe 56,424 hrs · 45,527 cycles

RIGHT GEAR MIDDLE DOOR LOWER FWD LINK LOOSE. R & R BAR IAW AMM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 56,402 hrs · 45,509 cycles

L1 DOOR EMERGENCY EXIT FLOOR SIGN LOOSE. SECURED LENS IAW MM.

Part: COVER — DETACHED (CABIN) · airframe 56,194 hrs · 45,360 cycles

RIGHT OVERWING EXIT LIGHT COVER FELL OFF. SECURED COVER PER M/M.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 55,914 hrs · 45,167 cycles

STRINGER CRACKED AT BS 484, STR 2L. REPAIRED STRINGER IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,914 hrs · 45,167 cycles

SKIN CRACKED AT BS 380, STR 14L. REPAIRED SKIN IAW EA.

Part: STRINGER CLIP — DAMAGED (FUSELAGE) · airframe 55,914 hrs · 45,167 cycles

STRINGER CLIP DAMAGED AT STA 420, STR 14R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — DAMAGED (FUSELAGE) · airframe 55,914 hrs · 45,167 cycles

STRINGER CLIP DAMAGED AT STA 400, STR 14R REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — DAMAGED (FUSELAGE) · airframe 55,914 hrs · 45,167 cycles

STRINGER CLIP DAMAGED AT STA 400, STR 14R. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,914 hrs · 45,167 cycles

SKIN CRACKED AT BS 380, STR 14R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,914 hrs · 45,167 cycles

FUSELAGE SKIN CRACKED AT STA 847+10, LEFT UPPER AFT WINDOW CUTOUT. REPAIRED FUSELAGE SKIN EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,914 hrs · 45,167 cycles

FUSELAGE SKIN CRACKED AT STA 827+10 LEFT UPPER AFT WINDOW CUTOUT CORNER. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,914 hrs · 45,167 cycles

FUSELAGE SKIN CRACKED AT STA 847+10, RIGHT LOWER FWD WINDOW CORNER CUTOUT. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,914 hrs · 45,167 cycles

FUSELAGE SKIN CRACKED AT RIGHT LOWER FORWARD WINDOW CORNER, BS 787+10. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,914 hrs · 45,167 cycles

FUSELAGE SKIN CRACKED AT STA 887+10, RIGHT UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,914 hrs · 45,167 cycles

FUSELAGE SKIN CRACKED AT STA 867+10, RIGHT UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,914 hrs · 45,167 cycles

FUSELAGE SKIN CRACKED AT STA 867+10, RIGHT LOWER FWD WINDOW CORNER CUTOUT. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,914 hrs · 45,167 cycles

FUSELAGE SKIN CRACKED AT RIGHT UPPER AFT WINDOW CORNER, BS 767+10. REPAIRED SKIN PER SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,914 hrs · 45,167 cycles

RIGHT BS 827+10 UPPER AFT WINDOW SKIN CUTOUT AT HOLES 2, 3, 4, 6 CRACKED. REMOVED AND REPLACED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,914 hrs · 45,167 cycles

RIGHT BS 767+10 LOWER FWD WINDOW SKIN CUTOUT AT HOLES 1, 3, 4, 9 CRACKED. REMOVED AND REPLACED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,914 hrs · 45,167 cycles

FUSELAGE SKIN CRACKED AT STA 767+10, LEFT LOWER FWD WINDOW CUTOUT CORNER. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,914 hrs · 45,167 cycles

LEFT BS 867+10 LOWER FORWARD WINDOW SKIN CUTOUT HAS HFEC CRACK INDICATION AT HOLES 3, 4. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,914 hrs · 45,167 cycles

RIGHT BS 807+10 UPPER AFT WINDOW SKIN CUTOUT AT HOLES 2, 3, 9 CRACKED. REMOVED AND REPLACED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,914 hrs · 45,167 cycles

FUSELAGE SKIN CRACKED AT STA 807+10 LEFT UPPER AFT WINDOW CUTOUT CORNER. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,914 hrs · 45,167 cycles

FUSELAGE SKIN CRACKED AT STA 847+10, RIGHT UPPER AFT WINDOW CUTOUT. REPAIRED FUSELAGE SKIN EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,914 hrs · 45,167 cycles

FUSELAGE SKIN CRACKED AT STA 887+10, LEFT UPPER AFT WINDOW CUTOUT. REPAIRED FUSELAGE SKIN EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,914 hrs · 45,167 cycles

LEFT BS 887+10 LOWER FORWARD WINDOW SKIN CUTOUT HAS HFEC CRACK INDICATION AT HOLES 3,4. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,914 hrs · 45,167 cycles

FUSELAGE SKIN CRACKED AT STA 807+10, LEFT LOWER FWD WINDOW CORNER CUTOUT. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,914 hrs · 45,167 cycles

FUSELAGE SKIN CRACKED AT RIGHT UPPER AFT WINDOW CORNER, BS 767+10. REPAIRED SKIN PER SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,914 hrs · 45,167 cycles

FUSELAGE SKIN CRACKED AT STA 727+10, LEFT UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,914 hrs · 45,167 cycles

FUSELAGE SKIN CRACKED AT STA 787+10, LEFT LOWER FWD WINDOW CORNER CUTOUT. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,914 hrs · 45,167 cycles

FUSELAGE SKIN CRACKED AT STA 847+10, LEFT LOWER FWD WINDOW CORNER CUTOUT. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,914 hrs · 45,167 cycles

LEFT BS 867+10 UPPER AFT WINDOW SKIN CUTOUT HAS HFEC CRACK INDICATION AT HOLE 3. REPAIRED SKIN IAW SB.

Part: STRINGER CLIP — DAMAGED (FUSELAGE) · airframe 55,914 hrs · 45,167 cycles

STR CLIP DAMAGED AT STA 727E, STR 4R. REMOVED AND REPLACED STR CLIP PER SRM.

Part: STRINGER CLIP — DAMAGED (FUSELAGE) · airframe 55,914 hrs · 45,167 cycles

STR CLIP AT DAMAGED AT STA 727D, STR 3R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — DAMAGED (FUSELAGE) · airframe 55,914 hrs · 45,167 cycles

STR CLIP DAMAGED AT STA 727D, STR 4R. REMOVED AND REPLACED STR CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,801 hrs · 45,086 cycles

FUSELAGE CRACKED AT 727D +6 STR 4R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,801 hrs · 45,086 cycles

FUSELAGE CRACKED AT 727E +10 STR 4R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,801 hrs · 45,086 cycles

FUSELAGE SKIN CRACKED AT BS 807, STR 4R. REPAIRED SKIN IAW EA.

Part: SIGN — BROKEN (CABIN) · airframe 55,503 hrs · 44,876 cycles

EMERGENCY EXIT SIGN LOCATED AT CENTER AISLE ROW 2 CRACKED AND MISSING LENS. REPAIRED CRACK AND INSTALLED NEW LENS IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,331 hrs · 44,004 cycles

RIGHT AFT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LAMP IAW MM.

Part: LENS — LOOSE (CABIN) · airframe 52,996 hrs · 42,986 cycles

RT OVERWING EMERGENCY EXIT SIGN LENS LOOSE. REMOVED AND REPLACED LENS PER AMM.

Part: SIGN — INOPERATIVE (CABIN) · airframe 52,956 hrs · 42,955 cycles

LEFT OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED SIGN ASSY PER MM. (SUBMITTED AS A SUPPLEMENT, COULDN`T FIND ORIGINAL CONTROL NUMBER.)

Part: SIGN — INOPERATIVE (CABIN) · airframe 52,956 hrs · 42,955 cycles

LEFT OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED SIGN ASSY PER MM. (SUBMITTED AS A SUPPLEMENT, COULDN`T FIND ORIGINAL CONTROL NUMBER.)

Part: TIRE — BLOWN (LT MLG) · airframe 52,763 hrs · 42,808 cycles

ABORTED TAKEOFF - NR 1 & NR 2 MLG TIRES BLEW ON TAKEOFF. R&R NR 1 & NR 2 MLG TIRES PER MM.

Part: LENS — LOOSE (CABIN) · airframe 52,757 hrs · 42,802 cycles

BOTH OVERWING EXIT LIGHT LENSES LOOSE. SECURED LENSES PER MM.

Part: WEB — CORRODED (FUSELAGE) · airframe 52,256 hrs · 42,431 cycles

DURING SCHEDULED 16Y CHECK, FOUND WEB CORRODED BETWEEN 332-1 TO BS 344, STR 17R. REPAIRED WEB IAW EA.

Part: HOSE — LEAKING (RAIN PROTECTION) · airframe 52,278 hrs · 42,450 cycles

AIR TURNBACK/DECLARED EMERGENCY, AFTER TAKEK OFF, ODOR THAT SMELLED EVERGREEN, IRRITANT TO THROAT. FOUND RAIN REPELLENT HOSE LEAKED. SECURED HOSE PER MM.

Part: WEB — CRACKED (NLG WW) · airframe 52,256 hrs · 42,431 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT NOSE LANDING GEAR WHEEL WELL WEB CRACKED BETWEEN BS 235 TO BS 259, WL 170. REPAIRED WEB IAW EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 52,256 hrs · 42,431 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT STRINGER CORRODED BETWEEN BS 1088 TO BS 1138. REMOVED AND REPLACED STRINGER PER SRM AND DWG.

Part: BRACKET — CORRODED (R1 DOOR) · airframe 52,256 hrs · 42,431 cycles

DURING SCHEDULED 16Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTINGS CORRODED. REMOVED AND REPLACED BRACKET IAW MM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 52,256 hrs · 42,431 cycles

DURING SCHEDULED 16Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTINGS CORRODED. REMOVED AND REPLACED FITTING IAW SRM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 52,256 hrs · 42,431 cycles

DURING SCHEDULED 16Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTINGS CORRODED. REMOVED AND REPLACED FITTING IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 52,256 hrs · 42,431 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM UPPER CHORD CRACKED AT BS 947.5, LBL 52. REPAIRED CHORD IAW EO AND EA.

Part: PANEL — CRACKED (FUSELAGE) · airframe 52,256 hrs · 42,431 cycles

DURING SCHEDULED 16Y CHECK, FOUND KEEL BEAM SKIN PANEL CRACKED BETWEEN BS 663.75 TO BS 727. REMOVED AND REPLACED PANEL IAW EA.

Part: BRACKET — CORRODED (L1 DOOR) · airframe 52,256 hrs · 42,431 cycles

DURING SCHEDULED 16Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTINGS CORRODED. REMOVED AND REPLACED BRACKET IAW MM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 52,256 hrs · 42,431 cycles

DURING SCHEDULED 16Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTINGS CORRODED. REMOVED AND REPLACED FITTING IAW SRM.

Part: BRACKET — CORRODED (R1 DOOR) · airframe 52,256 hrs · 42,431 cycles

DURING SCHEDULED 16Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTINGS CORRODED. REMOVED AND REPLACED BRACKET IAW MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,256 hrs · 42,431 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 294.5+1, STR 7R. REPAIRED FRAME EO AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,256 hrs · 42,431 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED BETWEEN BS 860 TO BS 885. REPAIRED SKIN IAW SRM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 52,256 hrs · 42,431 cycles

DURING SCHEDULED 16Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTINGS CORRODED. REMOVED AND REPLACED FITTING IAW SRM.

Part: BRACKET — CORRODED (L1 DOOR) · airframe 52,256 hrs · 42,431 cycles

DURING SCHEDULED 16Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTINGS CORRODED. REMOVED AND REPLACED BRACKET IAW MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,256 hrs · 42,431 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 616, WBL 208. REMOVED AND REPLACED FRAME IAW EO AND EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,256 hrs · 42,431 cycles

DURING SCHEDULED 16Y CHECK, FOUND FWD GALLEY EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 52,256 hrs · 42,431 cycles

DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM CRACKED AT BS 616, STR 17L. REPAIRED BEAM IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 52,256 hrs · 42,431 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM WEB CRACKED AT BS 639, LBL 45.5. REPAIRED WEB IAW EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,256 hrs · 42,431 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,256 hrs · 42,431 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 616, BETWEEN STR 14L TO STR 18L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,256 hrs · 42,431 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 616, STR 14L. REPAIRED FRAME IAW EA.

Part: BATTERY — DISCHARGED (CABIN) · airframe 52,256 hrs · 42,431 cycles

DURING SCHEDULED 16Y CHECK, FOUND G4 GALLEY EMERGENCY EXIT LIGHT INOP. CHARGED BATTERY PER MM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 52,256 hrs · 42,431 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM WEB CRACKED AT BS 708.5, LBL 24.5. REPAIRED WEB IAW EO AND EA.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 52,256 hrs · 42,431 cycles

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

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 52,256 hrs · 42,431 cycles

DURING SCHEDULED 16Y CHECK, FOUND INNER CHORD CORRODED BETWEEN BS 294 TO BS 360, STR 17L. REMOVED AND REPLACED CHORD IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,256 hrs · 42,431 cycles

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

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 52,256 hrs · 42,431 cycles

DURING SCHEDULED 16Y CHECK, FOUND INNER CHORD CORRODED BETWEEN BS 259 TO BS 344, STR 17R. REMOVED AND REPLACED CHORD IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,256 hrs · 42,431 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 787, BETWEEN STR 26R TO STR 27R. REMOVED AND REPLACED FRAME IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,256 hrs · 42,431 cycles

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

Part: WEB — CORRODED (FUSELAGE) · airframe 52,256 hrs · 42,431 cycles

DURING SCHEDULED 16Y CHECK, FOUND WEB CORRODED BETWEEN BS 312 TO BS 344, LBL 60. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,256 hrs · 42,431 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 348.2, STR 17L. REMOVED AND REPLACED FRAME IAW SRM AND DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 52,256 hrs · 42,431 cycles

DURING SCHEDULED 16Y CHECK, FOUND STUB BEAM WEB CRACKED AT BS 685, LBL 45.5. REMOVED AND REPLACED WEB PER SRM AND DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 52,256 hrs · 42,431 cycles

DURING SCHEDULED 16Y CHECK, FOUND WEB CRACKED AT BS 520+7, BETWEEN STR 22R TO STR 24R. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 52,256 hrs · 42,431 cycles

DURING SCHEDULED 16Y CHECK, FOUND WEB CORRODED BETWEEN BS 291.5 BS 294.5, STR 17R. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 52,256 hrs · 42,431 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 859, RBL 8.10. REPAIRED CHANNEL IAW EA.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 52,256 hrs · 42,431 cycles

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

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 52,256 hrs · 42,431 cycles

DURING SCHEDULED 16Y CHECK, FOUND UPPER CHORD FLOORBEAM CORRODED AT BS 312, BETWEEN RBL 20 TO RBL 37. REPAIRED BEAM IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,256 hrs · 42,431 cycles

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

Part: WEB — CORRODED (FUSELAGE) · airframe 52,256 hrs · 42,431 cycles

DURING SCHEDULED 16Y CHECK, FOUND WEB CORRODED BETWEEN BS 294.5 BS 328, RBL 59. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,256 hrs · 42,431 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE WINDOW SKIN CRACKED AT BS 211.8, STR 9L. REPAIRED AT SKIN IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,256 hrs · 42,431 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 20L. REMOVED AND REPLACED CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,256 hrs · 42,431 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,256 hrs · 42,431 cycles

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

Part: WEB — CRACKED (FUSELAGE) · airframe 52,256 hrs · 42,431 cycles

DURING SCHEDULED 16Y CHECK, FOUND WEB CRACKED AT BS 178+2.5, LBL 5.7. REPAIRED WEB IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,256 hrs · 42,431 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,256 hrs · 42,431 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,256 hrs · 42,431 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,256 hrs · 42,431 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,256 hrs · 42,431 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,256 hrs · 42,431 cycles

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

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 52,256 hrs · 42,431 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,256 hrs · 42,431 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 21L. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,256 hrs · 42,431 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,256 hrs · 42,431 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,256 hrs · 42,431 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10L. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,256 hrs · 42,431 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 26L. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,256 hrs · 42,431 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,256 hrs · 42,431 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 52,256 hrs · 42,431 cycles

R1 DOOR CUTOUT LOWER SILL WEB CORRODED BETWEEN BS 332.1 TO BS 344, STR 17R. REPAIRED WEB IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,284 hrs · 41,696 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 500-5.5, STR 4L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 51,284 hrs · 41,696 cycles

DURING SCHEDULED OTS CHECK, FOUND LT WING NR 2 SLAT O/B SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,280 hrs · 41,695 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 500+5.5, STR 4L. REPAIRED SKIN PER SRM.

Part: SKIN — DELAMINATED (LT WING SPOILER) · airframe 51,002 hrs · 41,472 cycles

DURING SCHEDULED HC2 CHECK FOUND, LT WING NR 3 FLIGHT SPOILER UPPER SKIN DELAMINATED. REMOVED AND REPLACED SPOILER PER AMM.

Part: SKIN — DELAMINATED (NR 5 SLAT RT) · airframe 51,002 hrs · 41,472 cycles

DURING SCHEDULED HC2 CHECK FOUND, RT WING NR 5 SLAT O/B END IS DELAMINATED. REMOVED AND REPLACED SLAT ASSY IAW MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 51,002 hrs · 41,472 cycles

DURING SCHEDULED HC2 CHECK FOUND, R-2 DOOR SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 51,002 hrs · 41,472 cycles

DURING SCHEDULED HC2 CHECK FOUND, LT WING O/B AFT FLAP DELAMINATED ON LWR SKIN. REMOVED AND REPLACED AFT FLAP PER AMM.

Part: SKIN — CRACKED (LT WING) · airframe 51,002 hrs · 41,472 cycles

DURING SCHEDULED HC2 CHECK FOUND, LT WING FIXED L/E SKIN CRACKED PROGRESSING FROM PREVIOUS ROUTE OUT AT I/B RADIUS OF O/B SPRING DOOR CUTOUT. REPAIRED SKIN PER EA.

Part: SLAT TRACK — CRACKED (NR 1 SLAT) · airframe 51,002 hrs · 41,472 cycles

DURING SCHEDULED HC2 CHECK FOUND, LT WING FIXED L/E HAS AN APPX .312 INCH CRACKED AT NR 1 SLAT O/B AUX TRACK CURTAIN CUTOUT. REPAIRED SLAT PER EA 1-357-6028.

Part: LIGHT — BROKEN (CABIN) · airframe 50,039 hrs · 40,762 cycles

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

Part: ATTACH FITTING — BROKEN (SPOILER) · airframe 48,843 hrs · 39,860 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT WING I/B NR 4 GROUND SPOILER ATTACH LUG BROKEN. REMOVED AND REPLACED NR 4 SPOILER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,115 hrs · 38,568 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,115 hrs · 38,568 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,115 hrs · 38,568 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 7R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,115 hrs · 38,568 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,115 hrs · 38,568 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 597, STR 8R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,115 hrs · 38,568 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,115 hrs · 38,568 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 480, STR 8L. REPAIRED FRAME PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,115 hrs · 38,568 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 47,115 hrs · 38,568 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 4L. REMOVED AND REPLACED SPLICE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,115 hrs · 38,568 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,115 hrs · 38,568 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,115 hrs · 38,568 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,115 hrs · 38,568 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 47,115 hrs · 38,568 cycles

DURING SCHEDULED 14Y CHECK, FOUND BULKHEAD VERTICAL BEAM WEB CRACKED BETWEEN BS 178 TO BS 180, RBL 5.7. REPAIRED WEB PER ER.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 47,115 hrs · 38,568 cycles

DURING SCHEDULED 14Y CHECK, FOUND RT KEEL BEAM CORRODED BETWEEN BS 720 TO BS 726. REPAIRED BEAM PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,115 hrs · 38,568 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,115 hrs · 38,568 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 907, STR 8R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,115 hrs · 38,568 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 520, STR 8R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,115 hrs · 38,568 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,115 hrs · 38,568 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 727D, STR 8L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,115 hrs · 38,568 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,115 hrs · 38,568 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,115 hrs · 38,568 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,115 hrs · 38,568 cycles

DURING SCHEDULED 14Y CHECK, FOUND SKIN CRACKED AT BS 525, STR 11R. REPAIRED SKIN PER ER.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 47,115 hrs · 38,568 cycles

DURING SCHEDULED 14Y CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED BETWEEN BS 707 TO BS 714, BBL 0. REPAIRED WEB PER SI.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,115 hrs · 38,568 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 867, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,115 hrs · 38,568 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 827, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,115 hrs · 38,568 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 480, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,115 hrs · 38,568 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 597, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,115 hrs · 38,568 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 440, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,115 hrs · 38,568 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 520, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,115 hrs · 38,568 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 907, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,115 hrs · 38,568 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 787, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,115 hrs · 38,568 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 400, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,115 hrs · 38,568 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,115 hrs · 38,568 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 9L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 47,115 hrs · 38,568 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CRACKED BETWEEN BS 378 TO BS 384, STR 2L. REMOVED AND REPLACED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,115 hrs · 38,568 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,115 hrs · 38,568 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 787, STR 8R. REPAIRED FRAME PER EA.

Part: RIB — CRACKED (TE FLAP) · airframe 47,115 hrs · 38,568 cycles

DURING SCHEDULED 14Y CHECK, FOUND RT WING I/B MID FLAP I/B AFT RIB CRACKED. REMOVED AND REPLACED RIB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,115 hrs · 38,568 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,115 hrs · 38,568 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 9L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,115 hrs · 38,568 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,115 hrs · 38,568 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,115 hrs · 38,568 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 9L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,115 hrs · 38,568 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,115 hrs · 38,568 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,115 hrs · 38,568 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 9L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,115 hrs · 38,568 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,115 hrs · 38,568 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,115 hrs · 38,568 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 599D, STR 5R. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 47,115 hrs · 38,568 cycles

DURING SCHEDULED 14Y CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 707, BL 0. REPAIRED WEB PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 47,115 hrs · 38,568 cycles

DURING SCHEDULED 14Y CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 709, BL 0. REPAIRED WEB PER SRM.

Part: LIGHT — BROKEN (CABIN) · airframe 46,897 hrs · 38,399 cycles

DURING SCHEDULED CV CHECK, FOUND RT OVERHEAD BULLNOSE EMERGENCY EXIT LIGHT BROKEN AT ROW 8. REMOVED AND REPLACED LIGHT PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 46,727 hrs · 38,275 cycles

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

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 46,542 hrs · 38,144 cycles

L1 DOOR FELL OUT OF CONTAINER. DID NOT DEPLOY. INSTALLED SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 46,124 hrs · 37,831 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 45,813 hrs · 37,596 cycles

L1 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF CONTAINER. RE-INSTALLED SLIDE PER MT.

Part: SLAT — DELAMINATED (RT WING) · airframe 44,627 hrs · 36,739 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING NR 5 SLAT O/B EDGE DELAMINATED. REMOVED AND REPLACED SLAT PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 44,251 hrs · 36,481 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT SIDE AFT EMERGENCY EXIT BULLNOSE LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: ACTUATOR — FAULTY (RT MLG) · airframe 43,931 hrs · 36,256 cycles

DURING GEAR EXTENSION HAD RT MLG UNSAFE INDICATION. USED CHECK LIST, MANUAL EXTENSION PER CHECK LIST, GEAR SAFE, UNEVENTFUL LANDING. REMOVED AND REPLACED THE MLG ACTUATOR PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 43,592 hrs · 36,026 cycles

DURING SCHEDULED SPV CHECK, FOUND LT VERTICAL BEAM WEB CRACKED AT BS 178, RBL 17, WL 232. REPAIRED WEB PER SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 43,011 hrs · 35,630 cycles

DURING SCHEDULED MV2 CHECK, FOUND L1 EMERGENCY EXIT ESCAPE SLIDE LIGHT INOP. REMOVED AND REPLACED BATTERY ASSY PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 42,957 hrs · 35,586 cycles

DURING SCHEDULED MV2 CHECK, FOUND EMERGENCY EXIT LIGHTS INOP AT ROW 1 THRU ROW 6. REMOVED AND REPLACED BATTERY PACKS PER AMM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 42,813 hrs · 35,483 cycles

RT FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 42,863 hrs · 35,449 cycles

DURING SCHEDULED MV2 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHTS INOP BETWEEN ROW 2 DEF AND ROW 6 DEF. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 42,529 hrs · 35,303 cycles

DURING SCHEDULED SPV CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED AT OUTBOARD END. REMOVED AND REPLACED FLAP PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 41,238 hrs · 34,318 cycles

DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 41,133 hrs · 34,291 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 410, BL 0. REPAIRED SKIN PER BOEING SB.

Part: MECHANISM — DIRTY (R2 WINDOW) · airframe 41,133 hrs · 34,291 cycles

DURING SCHEDULED BRDG CHECK, FOUND FLIGHT DECK R2 WINDOW DOES NOT OPEN WHEN EXTERNAL EMERGENCY RELEASE HANDLE IS PULLED. CLEAN AND LUBED HANDLE MECHANISM PER MM.

Part: CABLE — FRAYED (EVAC SLIDE) · airframe 41,133 hrs · 34,291 cycles

DURING SCHEDULED CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE CABLE FRAYED. REMOVED AND REPLACED EVAC SLIDE CABLE PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 41,133 hrs · 34,291 cycles

DURING SCHEDULED BRDG CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SLAT — CRACKED (LT WING) · airframe 41,133 hrs · 34,291 cycles

DURING SCHEDULED A1 CHECK, FOUND LT WING NR 1 L/E SLAT CRACKED AT INBOARD END. REPAIRED SLAT PER SRM.

Part: ATTACH FITTING — CORRODED (HORIZONTAL STAB) · airframe 33,586 hrs · 28,420 cycles

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

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 33,586 hrs · 28,420 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,586 hrs · 28,420 cycles

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

Part: FRAME — CRACKED (BS 616) · airframe 33,586 hrs · 28,420 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, RBL 65, WL 201. REPAIRED FRAME PER BFG ER.

Part: BRACKET — CRACKED (GIRT BAR) · airframe 33,586 hrs · 28,420 cycles

DURING SCHEDULED D CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR AFT LOWER FLOOR BRACKET CRACKED. REMOVED AND REPLACED BRACKET PER SRM.

Part: BRACKET — CRACKED (GIRT BAR) · airframe 33,586 hrs · 28,420 cycles

DURING SCHEDULED D CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR FWD LOWER FLOOR BRACKET CRACKED. REMOVED AND REPLACED BRACKET PER SRM.

Part: FRAME — CORRODED (BS 294) · airframe 33,586 hrs · 28,420 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 294, STR 18R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (BS 359) · airframe 33,586 hrs · 28,420 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 359, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CORRODED (BS 947) · airframe 33,586 hrs · 28,420 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME FAILSAFE CHORD CORRODED AT BS 947, RBL 13. REPAIRED FRAME PER SRM.

Part: FLOORBEAM — CORRODED (COCKPIT FLOOR) · airframe 33,586 hrs · 28,420 cycles

DURING SCHEDULED D CHECK, FOUND COCKPIT FLOOR Z-CHORD CORRODED AT BS 270, BETWEEN LBL 6 TO RBL 11. REMOVED AND REPLACED Z-CHORD PER SRM.

Part: CREASE BEAM — CORRODED (BS 887-907) · airframe 33,586 hrs · 28,420 cycles

DURING SCHEDULED D-CHECK, FOUND RT CREASE BEAM WEB CORRODED BETWEEN BS 887 TO BS 907, WL 208. REPAIRED CREASE BEAM WEB PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727B) · airframe 33,586 hrs · 28,420 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 727B, STR 16L. REMOVED AND REPLACED CLIP PER SRM.

Part: CREASE BEAM — CORRODED (BS 500A-500B) · airframe 33,586 hrs · 28,420 cycles

DURING SCHEDULED D-CHECK, FOUND RT CREASE BEAM WEB CORRODED BETWEEN BS 500A TO BS 500B, WL 208. REPAIRED CREASE BEAM WEB PER SRM.

Part: FRAME — CRACKED (BS 500C) · airframe 33,586 hrs · 28,420 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 400) · airframe 33,586 hrs · 28,420 cycles

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

Part: CREASE BEAM — CORRODED (BS 500B-500C) · airframe 33,586 hrs · 28,420 cycles

DURING SCHEDULED D CHECK, FOUND RT CREASE BEAM WEB CORRODED BETWEEN BS 500B TO BS 500C, WL 208. REPAIRED CREASE BEAM WEB PER SRM.

Part: FRAME — CRACKED (BS 827) · airframe 33,586 hrs · 28,420 cycles

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

Part: FRAME — CRACKED (BS 380) · airframe 33,586 hrs · 28,420 cycles

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

Part: FRAME — CRACKED (BS 907) · airframe 33,586 hrs · 28,420 cycles

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

Part: STRINGER CLIP — CRACKED (BS 685) · airframe 33,586 hrs · 28,420 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 685, STR 13R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 706) · airframe 33,586 hrs · 28,420 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 706, STR 11R. REMOVED AND REPLACED CLIP PER SRM.

Part: ANGLE — CORRODED (VERTICAL STAB) · airframe 33,586 hrs · 28,420 cycles

DURING SCHEDULED D-CHECK, FOUND VERTICAL STAB FITTING RIGHT AFT DRAG ANGLE CORRODED. REMOVED AND REPLACED DRAG ANGLE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,586 hrs · 28,420 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 706, STR 13L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,586 hrs · 28,420 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 706, STR 11L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,586 hrs · 28,420 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,586 hrs · 28,420 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 706, STR 13R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,586 hrs · 28,420 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 685, STR 13L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,586 hrs · 28,420 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 578, STR 12R. REMOVED AND REPLACED CLIP PER SRM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 33,547 hrs · 28,393 cycles

R1 DOOR EVACUATION SLIDE PRESS INDICATOR OUT OF VIEW. ADJUSTED SLIDE ASSY PER MM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 33,347 hrs · 28,241 cycles

FWD GALLEY EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 33,294 hrs · 28,190 cycles

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

Part: SKIN — DELAMINATED (RT WING FLAP) · airframe 33,179 hrs · 28,099 cycles

DURING SCHEDULED RON CHECK, FOUND RIGHT OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: BATTERY PACK — INOPERATIVE (FWD GALLEY) · airframe 32,916 hrs · 27,884 cycles

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

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 32,789 hrs · 27,794 cycles

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

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,278 hrs · 27,373 cycles

DURING SCHEDULED RON CHECK, FOUND 2 EA CABIN EMERGENCY BULLNOSE LIGHTS INOP AT FWD CABIN, LT SIDE. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — DELAMINATED (RT FOREFLAP) · airframe 31,911 hrs · 27,062 cycles

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

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,562 hrs · 26,787 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND L1 DOOR LOWER EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,562 hrs · 26,787 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND L1 & R1 DOOR EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACKS PER MM.

Part: CABLE — MISROUTED (L2 DOOR GIRT BAR) · airframe 30,340 hrs · 25,860 cycles

DURING SCHEDULED A2 CHECK, FOUND 2 EACH GIRT BAR CABLES MISROUTED AT R2 AND L2 DOOR EVAC SLIDES. REROUTED CABLES PER MM.

Part: CABLE — MISROUTED (L2 DOOR SLIDE) · airframe 29,961 hrs · 25,559 cycles

DURING SCHEDULED C2 CHECK, FOUND L2 DOOR EVAC SLIDE CABLE MISROUTED. REROUTED L2 DOOR EVAC SLIDE CABLE PER MM.

Part: CABLE — FRAYED (R2 DOOR SLIDE) · airframe 29,961 hrs · 25,559 cycles

DURING SCHEDULED C2 CHECK, FOUND R2 DOOR EVAC SLIDE CABLE FRAYED. REMOVED AND REPLACED R2 DOOR EVAC SLIDE CABLE PER MM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 29,680 hrs · 25,320 cycles

DURING SCHEDULED SERVICE, FOUND FWD LT EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 29,030 hrs · 24,773 cycles

DURING SCHEDULED C1 CHECK, FOUND LT FWD ENTRY DOOR LOWER HINGE BOX FITTING AFT EDGE, CRACKED. REMOVED AND REPLACED HINGE BOX FITTING PER SRM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 29,025 hrs · 24,770 cycles

DURING SCHEDULED C1 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 28,862 hrs · 24,636 cycles

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

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 28,034 hrs · 23,974 cycles

DURING SCHEDULED RON, FOUND LT OVERWING EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: LENS — LOOSE (OVERWING EXIT) · airframe 27,140 hrs · 23,276 cycles

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

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 27,123 hrs · 23,261 cycles

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

Part: BUSHING — WORN (LT ELEVATOR) · airframe 26,242 hrs · 22,531 cycles

DURING SCHEDULED C2 CHECK, (SI 11138-55), LT ELEVATOR TAB FAILED FREEPLAY CHECK. REMOVED AND REPLACED LT ELEVATOR TAB NR 1 HINGE ATTACH BUSHING/HARDWARE.

Part: BUSHING — WORN (STAB TRIM WHEEL) · airframe 26,031 hrs · 22,352 cycles

EXCESSIVE VIBRATION IN STAB TRIM WHEEL WHEN TRIM IS APPLIED. REMOVED AND REPLACED RT OUTBD STAB TRIM WHEEL BUSHING PER MM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 25,665 hrs · 22,060 cycles

DURING SCHEDULED 1/D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 807, BETWEEN STR 27L AND STR 27R. REPAIRED FRAME PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 25,665 hrs · 22,066 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD ENTRY DOOR CRACKED AT AFT FRAME ON 5TH FROM TOP STOP PIN CUTOUT. REPAIRED FRAME PER SWA EA.

Part: SKIN — CRACKED (RT WING SLAT) · airframe 25,371 hrs · 21,812 cycles

DURING SCHEDULED C1 CHECK, FOUND NR 6 L/E SLAT LOWER SKIN CRACKED INBOARD OF ACTUATOR. REPAIRED SKIN PER SWA EA.

Part: STRIP — LOOSE (CABIN) · airframe 24,518 hrs · 21,115 cycles

EEPLS PHOTOLUMINESCENT STRIP LOOSE BETWEEN ROWS NR 6 AND NR 8 ABC. REMOVED AND REPLACED STRIP PER MM.

Part: BLADE — CRACKED (NR 2 ENGINE) · airframe 23,209 hrs · 20,061 cycles

DURING SCHEDULED SERVICE CHECK, (MTSI) FOUND 7 EA HPT BLADES WITH T/E AXIAL CRACKS ON NR 2 ENG. REMOVED AND REPLACED NR 2 ENG PER MM.

Part: PUSHROD — WORN (ELEVATOR TAB) · airframe 22,171 hrs · 19,194 cycles

AIR TURNBACK, DECLARED EMERGENCY, DURING CLIMB AIRCRAFT STARTED SEVERE VIBRATION. REMOVED AND REPLACED LT ELEVATOR ASSY AND TAB. REMOVED AND REPLACED LEFT AND RT ELEVATOR TAB PUSHROD ASSY'S PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,653 hrs · 18,792 cycles

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

Part: SLIDE — DEFECTIVE (ENTRY DOOR) · airframe 20,842 hrs · 18,146 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. REMOVED AND REPLACED SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 20,487 hrs · 17,851 cycles

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

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 18,161 hrs · 15,921 cycles

DURING SCHEDULED C1 CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT AFT CABIN. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: RETAINER — LOOSE (CABIN) · airframe 18,161 hrs · 15,921 cycles

DURING SCHEDULED C1 CHECK, FOUND FLASHLIGHT HOLDER LOOSE IN FWD SECTION. SECURED FLASHLIGHT HOLDER PER MM.

Part: INDICATOR — OUT OF TOLERANCE (EVAC SLIDE) · airframe 17,669 hrs · 15,513 cycles

DURING SCHEDULED A2 CHECK, FOUND AFT ENTRY & SVC DOOR EMERGENCY EVAC SLIDE PRESS INDICATOR OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE ASSY''''S PER MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 17,308 hrs · 15,218 cycles

DURING SCHEDULED 1/2D CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP, INBOARD SECTION, DELAMINATED. REPAIRED AFT FLAP ASSY PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,308 hrs · 15,218 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BROKEN RECEPTACLE AT RT OVERWING EMERGENCY EXIT LIGHT. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: DOOR FRAME — CRACKED (FWD ENTRY) · airframe 17,308 hrs · 15,218 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FWD ENTRY DOOR AFT FRAME CRACKED AT 3RD FROM BOTTOM STOP FITTING. REPAIRED DOOR FRAME PER SRM.

Part: DOOR FRAME — CRACKED (FWD PAX DOORWAY) · airframe 17,308 hrs · 15,218 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FWD ENTRY DOOR AFT FRAME CRACKED AT 3RD FROM BOTTOM STOP FITTING. REPAIRED DOOR FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (CABIN) · airframe 17,308 hrs · 15,218 cycles

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

Part: COVER — CRACKED (CABIN) · airframe 17,140 hrs · 15,080 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS TRACK COVER CRACKED AT ROW 15. R&R TRACK COVER PER MM.

Part: LIGHT — INOPERATIVE (ROW 18) · airframe 16,346 hrs · 14,408 cycles

EEPLS INOP AT ROW 18. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: CONNECTOR — LOOSE (NR 1 ENGINE) · airframe 15,939 hrs · 14,042 cycles

ABORTED TAKEOFF, NR 1 ENG EGT IND 1230 DEG AT TAKEOFF POWER. SECURED NR 1 ENG EGT HARNESS CONNECTOR AT ENG. OPS CHECK GOOD PER MM.

Part: WIRE — DISCONNECTED (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP AT ROW 15. RECONNECTED PULLED WIRES PER MM.

Part: LIGHT — MISSING (ROW 17)

DURING SCHEDULED C3 CHECK, FOUND EEPLS TRACK SECTION MISSING AT ROW 17. REPLACED SECTION PER MM.

Part: LENS — MISSING (CABIN)

DURING SCHEDULED C3 CHECK, FOUND FWD END OF EEPLS TRACK LOOSE AND LENS MISSING. SECURED TRACK AND REPLACED LENS PER MM.

Part: LIGHT — INOPERATIVE (ROW 19)

DURING SCHEDULED RON CHECK, FOUND EEPLS LIGHT INOP AT ROW 19. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SLIDE — DEPLOYED (PASSENGER DOOR)

DURING SCHEDULED RON CHECK, FWD ENTRY DOOR SLIDE WAS ACCIDENTALLY DEPLOYED. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: ROD END — OUT OF POSITION (NR 1 LE FLAP)

LEADING EDGE FLAP TRANSIT LIGHT REMAINED ILLUMINATED WITH FLAP HANDLE IN THE UP POSITION. NR 1 LE FLAP ANNUNCIATOR INDICATED AMBER, NOT IN THE FULL UP POSITION. RECYCLED FLAPS FROM 1 DEG TO 0 WITH NO CHANGE. AIRCRAFT RETURNED TO SLC. REMOVED AND REPLACED LT O/B KRUEGER FLAP POSITION INDICATION ARM-ROD END, OPS CK GOOD PER M/M.

Part: SKIN — DENTED (BS 807)

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE DENTED AND CREASED AT BS 807 BELOW CARGO DOOR. REPAIRED PER BOEING SRM.

Part: BULB — FAILED (CABIN)

DURING SCHEDULED C3 CHECK, FOUND LT OVERWING EMERGENCY EXIT SIDEWALL LIGHT IS INOP. RELAMPED PER BOEING MM, OPS CHECK GOOD.

Part: WIRE — LOOSE (CABIN)

DURING WALKAROUND CHECK, FOUND EMERGENCY EXIT LIGHT (PORT SIDE) AFT OF OW EXIT HAS EXPOSED WIRE AND IS INOP. RECONNECTED WIRES AND INSTALLED COVER PER BOEING MM.

Part: WIRE — DISCONNECTED (CABIN)

DURING WALKAROUND CHECK, FOUND EMERGENCY EXIT TRACK LIGHT WIRE BROKEN. RECONNECTED WIRES PER BOEING M/M.

Part: SKIN — GOUGED (BS 430)

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 430, RIGHT SIDE, BELOW SKIN CAP BEAM. REPAIRED PER BOEING SRM.

Part: ANTI-ICE VALVE — FAILED (NR 1 ENGINE)

AFTER TAKEOFF, NUMBER 1 ENGINE COWL ANTI-ICE VALVE FAILED AFTER TAKEOFF AND WOULD NOT OPEN. AIRCRAFT RETURNED TO PHX, DUE TO WEATHER AND MADE AN UNEVENTFUL LANDING. REPLACED VALVE AND RAN ENGINE PER BOEING M/M.

Part: LIGHT — LOOSE (CABIN)

DURING SCHEDULED RON CHECK, FOUND EMERGENCY EXIT LIGHTS INOP AT ROW 11. RESECURED LIGHT ASSEMBLY WIRE TERMINAL AND OP CHECKED PER BOEING M/M.

Part: BATTERY — DISCHARGED (CABIN)

DURING WALKAROUND, FOUND FLOOR TRACK LIGHTING INOP AT ROWS 14 THROUGH 18. REPLACED POWER SUPPLIES AND OP CHECKED PER BOEING M/M.

Part: WIRE — LOOSE (CABIN)

DURING BOARDING, PASSENGER KICKED FLOOR TRACK LIGHTING COVER AND ASSOCIATED WIRING LOOSE, DISABLING 10 WHITE LIGHTS. REPLACED COVER, REPAIRED WIRES AND REPLACED BATTERY PACK PER BOEING M/M.

Part: WIRE — DISCONNECTED (CABIN)

DURING RON CHECK, FOUND 2 WHITE FLOOR TRACK LIGHTS INOP AND WIRING EXPOSED. REMOVED AND REPLACED WIRING PER BOEING M/M.

Part: LIGHT — INOPERATIVE (CABIN)

AT GATE FOUND EMERGENCY TRACK LIGHTING INOP AT ROW 23. REINSTALLED WIRING AND ADJUSTED TRACKS.

Part: CIRCUIT BREAKER — TRIPPED (LANDING GEAR)

AFTER TAKEOFF, CREW WAS UNABLE TO RAISE LANDING GEAR HANDLE. RETURNED TO DAL AND MADE AN UNEVENTFUL LANDING. RESET LANDING GEAR LATCH C/B AND RETRACTION TESTED GEAR PER BOEING M/M.