N355SW

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 77,067 hrs · 65,191 cycles

LEFT WING LE NR 2 SLAT, OTBD TE WEDGE DELAMINATED ON CORNER. R & R NR 2 SLAT IAW MM.

Part: SKIN — DELAMINATED (RT SPOILER) · airframe 76,762 hrs · 64,965 cycles

RIGHT WING NR 9 SPOILER BOARD, UPPER SKIN PANEL DELAMINATED. R & R SPOILER IAW MM.

Part: SKIN PANEL — DELAMINATED (RT SPOILER) · airframe 76,762 hrs · 64,965 cycles

RIGHT WING NR 6 FLIGHT SPOILER BOARD, UPPER SKIN PANEL DELAMINATED. R & R NR 6 SPOILER IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,945 hrs · 64,358 cycles

SKIN CRACKED BETWEEN BS 375.75 - 376.50, STRINGER 8L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,945 hrs · 64,358 cycles

SKIN CRACKED AT BS 362, STRINGER 1L. REPAIRED SKIN IAW SRM.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 75,893 hrs · 64,310 cycles

L1 DOOR SLIDE LOOSE. SECURED SLIDE IAW MT.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 75,714 hrs · 64,175 cycles

R1 DOOR EMER EVAC SLIDE GIRT BAR AFT HOLD CLAMP OUT OF POSITION. REPOSITIONED SLIDE IAW SIP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 75,435 hrs · 63,958 cycles

RIGHT EMER EXIT SIDE WALL LIGHT INOPERATIVE. RELAMPED LIGHT IAW MM.

Part: BRACKET — BROKEN (R2 DOOR) · airframe 75,357 hrs · 63,899 cycles

R2 DOOR EMER EVAC SLIDE GIRT BAR CLAMSHELL BRACKET BROKEN. R & R BRACKET IAW MT.

Part: FITTING — CORRODED (RT WING) · airframe 75,248 hrs · 63,824 cycles

RIGHT WING MID SPAR FITTING CORRODED. R & R FITTING IAW SRM.

Part: SIGN — LOOSE (CABIN) · airframe 74,832 hrs · 63,494 cycles

RIGHT EMER EXIT SIGN ABOVE OVERWING DOOR LOOSE. SECURED SIGN IAW SIP.

Part: LENS — MISSING (CABIN) · airframe 74,391 hrs · 63,195 cycles

LEFT EMER EXIT BULLNOSE LIGHT LENS MISSING AT ROW 6. INSTALLED LENS IAW AMM.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 73,887 hrs · 62,836 cycles

FRAME BRACKET CRACKED AT BS 328 LBL 6. REPAIRED BRACKET IAW SRM & DWG.

Part: SKIN SPLICE — CRACKED (TAILCONE) · airframe 73,887 hrs · 62,836 cycles

TAIL CONE, APU EXHAUST AFT MOUNTING RING AT 3 O'CLOCK POSITION INTERIOR SKIN SPLICE CRACKED. R & R SKIN SPLICE IAW SRM & DWG.

Part: SKIN SPLICE — CRACKED (TAILCONE) · airframe 73,887 hrs · 62,836 cycles

TAIL CONE, APU EXHAUST AFT MOUNTING RING AT 9 O'CLOCK POSITION INTERIOR SKIN SPLICE CRACKED. R & R SKIN SPLICE IAW SRM & DWG.

Part: LENS — BROKEN (CABIN) · airframe 73,887 hrs · 62,836 cycles

LEFT NR 6 STOW BIN LOWER BULLNOSE EMER LIGHT LENS BROKEN. R & R LENS IAW AMM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 73,887 hrs · 62,836 cycles

ANGLE CRACKED AT BS 328 LBL 46. R & R ANGLE IAW DWG & SRM.

Part: PLATE — CRACKED (EMERGENCY LIGHT) · airframe 73,887 hrs · 62,836 cycles

R1 DOOR EMER EXIT SIDEWALL LIGHT MOUNT PLATE CRACKED. R & R LIGHT ASSEMBLY IAW AMM.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 73,887 hrs · 62,836 cycles

AFT PRESS BULKHEAD LOWER WEB CORRODED AT BS 1016 RBL 1. REPAIRED WEB IAW EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 73,887 hrs · 62,836 cycles

LEFT CREASE BEAM WEB CORRODED AT BS 788. REPAIRED WEB IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 73,887 hrs · 62,836 cycles

CREASE BEAM CORRODED BETWEEN BS 947.5 TO 986.5 RBL 54. R & R CREASE BEAM IAW DWG & SRM.

Part: FITTING — CORRODED (L1 DOOR) · airframe 73,887 hrs · 62,836 cycles

L1 DOOR EMER EVAC SLIDE AFT GIRT BAR FITTING SUPPORT ANGLE CORRODED. R & R FITTING IAW DWG & AMM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 73,887 hrs · 62,836 cycles

FORWARD CABIN FLOOR INTERCOSTAL CRACKED AT BS 344 BL 0. R & R INTERCOSTAL IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 73,887 hrs · 62,836 cycles

ANGLE CRACKED AT BS 328 LBL 46. R & R ANGLE IAW DWG & SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 73,887 hrs · 62,836 cycles

CABIN FWD WET AREA FLOORBEAM UPPER FLANGE ANGLE CRACKED AT BS 328, RBL 24. REPAIRED ANGLE IAW SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 73,887 hrs · 62,836 cycles

SHEAR TIE CRACKED AT BS 277 BETWEEN STRINGER 10L TO 11L. R & R SHEAR TIE IAW SRM & DWG.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 73,887 hrs · 62,836 cycles

ANGLE ATTACH CLIP CRACKED AT BS 348 STRINGER 11L. R & R CLIP IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,887 hrs · 62,836 cycles

FRAME WEB CRACKED AT BS 727D LBL 3 ATTACH FASTENER FOR NR 3 VHF ANTENNA. REPAIRED WEB IAW EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 73,887 hrs · 62,836 cycles

ANGLE CRACKED AT BS 348 STRINGER 10L. R & R ANGLE IAW DWG & SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 73,887 hrs · 62,836 cycles

ANGLE CRACKED AT BS 294.5, STRINGER 11L. R & R ANGLE IAW DWG & SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 73,887 hrs · 62,836 cycles

FLOOR PANEL SUPPORT ANGLE CRACKED BETWEEN BS 927 TO 947, LBL. R & R ANGLE IAW SRM & DWG.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 73,887 hrs · 62,836 cycles

FRAME AT L1 DOOR INNER CHORD CRACKED AT BS 348.2 STRINGER 17L. R & R CHORD IAW EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 73,887 hrs · 62,836 cycles

ANGLE CRACKED AT BS 360 STRINGER 11L. R & R ANGLE IAW SRM & DWG.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 73,887 hrs · 62,836 cycles

L1 DOOR AREA, CREASE BEAM CRACKED AT BS 348.2 AT ATTACH FASTENER HOLE FOR FRAME INNER CHORD. R & R BEAM IAW DWG & SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 73,887 hrs · 62,836 cycles

AFT PRESS BULKHEAD WEB CRACKED AT BS 1016 BL 0. REPAIRED WEB IAW EA.

Part: ANGLE — CRACKED (TE FLAP TRACK) · airframe 73,887 hrs · 62,836 cycles

RIGHT WING NR 6 FLAP TRACK FAIRING INBD SIDE ANGLE AT CROSS BRACE FWD SIDE CRACKED. R & R ANGLE IAW SRM & DWG.

Part: WEB — CRACKED (NLG WW) · airframe 73,887 hrs · 62,836 cycles

LEFT NOSE WW VERTICAL WEB CRACKED AT BS 259. REPAIRED WEB IAW SRM.

Part: PANEL — DELAMINATED (RT MLG WW) · airframe 73,887 hrs · 62,836 cycles

LOWER EXTERNAL FUSELAGE RT MLG FWD FAIRING PANEL AT WHEEL CUT OUT DELAMINATED. REPAIRED PANEL IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,887 hrs · 62,836 cycles

LEFT STATION 727 FRAME OTBD CHORD FWD FLANGE FWD LOWER HOLE CRACKED. REPAIRED CHORD IAW EA.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 73,887 hrs · 62,836 cycles

RIGHT WW PRESS DECK WEB CRACKED AT BS 664 RBL 17. REPAIRED WEB IAW EA.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 73,887 hrs · 62,836 cycles

LEFT WING NR 2 SLAT TE WEDGE OTBD AFT CORNER DELAMINATED. REPAIRED NR 2 SLAT IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,887 hrs · 62,836 cycles

RIGHT FRAME OTBD CHORD FWD FLANGE CRACKED AT BS 727. REPAIRED CHORD IAW EA.

Part: SKIN — WORN (TE FLAP) · airframe 73,616 hrs · 62,636 cycles

LEFT WING OTBD MID FLAP LEADING WORN. R & R MID FLAP IAW MM.

Part: GASPER FAN — FAULTY (AC BAY) · airframe 73,110 hrs · 62,278 cycles

AIR TURN BACK, CLIMBING THRU 700 MSL SMOKE & FUMES IN THE CABIN. LEVELED OFF AT 11,000 MSL. R & R GASPER FANS ASSEMBLY IAW MM.

Part: LIGHT — LOOSE (CABIN) · airframe 72,701 hrs · 61,987 cycles

RIGHT EMERGENCY EXIT BULLNOSE LIGHT LOOSE AT ROW 15. R & R LIGHT IAW AMM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 72,189 hrs · 61,650 cycles

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

Part: HINGE — BROKEN (RT SPOILER) · airframe 71,939 hrs · 61,488 cycles

RT WING INBD NR 5 SPOILER HINGE BROKEN. R & R SPOILER IAW MM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 71,743 hrs · 61,356 cycles

LT HORIZONTAL STAB LOWER SURFACE SKIN CRACKED AT REAR SPAR. REPAIRED SKIN IAW SRM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 71,508 hrs · 61,193 cycles

EMERGENCY EXIT LIGHT L1076 INOPERATIVE. R & R M1137 IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,508 hrs · 61,193 cycles

FUSELAGE SKIN CRACKED AT BS 346, STRINGER 2L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,508 hrs · 61,193 cycles

FUSELAGE SKIN CRACKED AT BS 340, STRINGER 2L. REPAIRED SKIN IAW SRM.

Part: CSD — FAULTY (NR 1 ENGINE) · airframe 71,489 hrs · 61,177 cycles

AIR TURN BACK, INFLIGHT SHUTDOWN CSD LOW OIL CAME ON AT LEVEL OFF. RETURNED TO BWI NR 1ENGINE. R & R NR 1 CSD, CSD OIL COOLER & CASE DRAIN FILTER IAW MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 70,305 hrs · 60,248 cycles

LT AFT EMERGENCY EXIT LIGHT FOR AFT ENTRY SLIDE INOPERATIVE. R&R BATTERY PACK IAW MM.

Part: CONTROLLER — FAULTY (CABIN PRESSURE) · airframe 70,185 hrs · 60,155 cycles

AIR TURNBACK/DECLARED EMERGENCY CLIMBING THROUGH APPROXIMATELY FL 290 THE "CABIN ALTITUDE" LIGHT ILLUMINATED W/CABIN ALTITUDE WARNING HORN. R & R CABIN PRESSURE CONTROLLER IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,777 hrs · 59,864 cycles

FORWARD ENTRY DOOR LOWER EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,777 hrs · 59,864 cycles

AFT ENTRY DOOR LOWER EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,777 hrs · 59,864 cycles

AFT SERVICE DOOR LOWER EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,777 hrs · 59,864 cycles

FUSELAGE SKIN CRACKED AT BS 940, STR 4L. REPAIRED SKIN IAW SRM.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 69,777 hrs · 59,864 cycles

L2 DOOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED POWER SUPPLY PER AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,777 hrs · 59,864 cycles

FUSELAGE SKIN CRACKED AT BS 415, STR 2R. REPAIRED SKIN IAW ER AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,777 hrs · 59,864 cycles

FUSELAGE SKIN CRACKED AT BS 362, STR 8R. REPAIRED SKIN IAW ER AND EA.

Part: LENS — LOOSE (EXIT SIGN) · airframe 69,608 hrs · 59,747 cycles

LEFT OVERWING EMERGENCY EXIT OVERHEAD SIGN LENS LOOSE. SECURED LENS PER M/M.

Part: SPOILER — BROKEN (LT WING) · airframe 69,553 hrs · 59,705 cycles

LEFT WING GROUND SPOILER O/B ATTACHMENT POINT FOR ACTUATOR BROKEN. REMOVED AND REPLACED SPOILER PER MM.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 68,851 hrs · 59,193 cycles

FWD ENTRY DOOR ESCAPE SLIDE IS VERY LOOSE IN SLIDE COMPARTMENT AND EXCESS FABRIC IS HANGING OUT OF COMPARTMENT. RE-INSTALLED ESCAPE SLIDE IN COMPARTMENT PER M/M.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,678 hrs · 59,072 cycles

CRACK IN FUSELAGE SKIN JUST ABOVE &4L AT BS 950 APPROX 3.5" LONG. REPAIRED PER SRM 53-00-01-2R-31. REPAIR 3L. THIS IS A CATEGORY REPAIR.

Part: PRESSURE PANEL — CRACKED (MLG WW) · airframe 68,352 hrs · 58,814 cycles

MAIN WHEEL WELL CEILING BEADED WEB CRACKED AT BS 672, LBL 43. REPAIRED WEB PER EA.

Part: CHANNEL — CRACKED (LT WING) · airframe 68,281 hrs · 58,761 cycles

LEFT WING CHANNEL CRACKED AT WBL 191.0. REMOVED AND REPLACED CHANNEL IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 68,281 hrs · 58,761 cycles

TIE CLIP CRACKED BETWEEN BS 500 TO BS 500A, STR 28L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 68,281 hrs · 58,761 cycles

STRINGER CORRODED AT BS 1006+3, STR 27L. REPAIRED STRINGER IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 68,281 hrs · 58,761 cycles

SUPPORT ANGLE CRACKED AT BS 540, STR 24L. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: FLAP — PUNCTURED (RT WING) · airframe 68,281 hrs · 58,761 cycles

RIGHT WING INBOARD FORE FLAP PUNCTURED. REPAIRED FORE FLAP IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 68,281 hrs · 58,761 cycles

WEB CRACKED BETWEEN BS 520 TO BS 540, BETWEEN STR 22R TO STR 24R. REMOVED AND REPLACED WEB IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 68,281 hrs · 58,761 cycles

TIE CLIP CRACKED AT BS 380, STR 21L. REMOVED AND REPLACED TIE CLIP IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 68,281 hrs · 58,761 cycles

TIE CLIP CRACKED AT BS 380, STR 22L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 68,281 hrs · 58,761 cycles

TIE CLIP CRACKED AT BS 380, STR 26L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 68,281 hrs · 58,761 cycles

STRINGER SPLICE CRACKED AT BS 360, STR 4R. REMOVED AND REPLACED SPLICE IAW SRM AND DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 68,281 hrs · 58,761 cycles

WEB CRACKED BS 887, BETWEEN STR 20R AND STR 21R. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 68,281 hrs · 58,761 cycles

FRAME CORRODED AT BS 344, STR 27R. REPAIRED FRAME WEB IAW EO AND EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 68,281 hrs · 58,761 cycles

SUPPORT ANGLE CRACKED AT BS 927, STR 21R. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 68,281 hrs · 58,761 cycles

WEB SUPPORT ANGLE CRACKED AT BS 294.5, STR 23L. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 68,281 hrs · 58,761 cycles

STRINGER SPLICE CRACKED AT BS 360, STR 6R. REMOVED AND REPLACED SPLICE IAW SRM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 68,281 hrs · 58,761 cycles

ANGLE CRACKED AT BS 540, BETWEEN STR 28L TO STR 28R. REMOVED AND REPLACED ANGLE IAW SRM & DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 68,281 hrs · 58,761 cycles

CHANNEL CORRODED AT BS 767+5, LBL 12.50. REPAIRED CHANNEL IAW EA.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 68,281 hrs · 58,761 cycles

STRINGER SPLICE CRACKED AT BS 727, STR 23R. REMOVED AND REPLACED SPLICE IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 68,281 hrs · 58,761 cycles

TIE CLIP CRACKED AT BS 727E, STR 23L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 68,281 hrs · 58,761 cycles

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

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 68,281 hrs · 58,761 cycles

TIE CLIP CRACKED AT BS 767, STR 23L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: WEB — CRACKED (NLG WW) · airframe 68,281 hrs · 58,761 cycles

NLG WHEEL WELL FASTENER HOLE CRACKED AT BS 243.5, LBL 16.0. REPAIRED WEB IAW SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 68,281 hrs · 58,761 cycles

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

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 68,281 hrs · 58,761 cycles

TIE CLIP CRACKED AT BS 727A, STR 25L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG AND SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 68,281 hrs · 58,761 cycles

TIE CLIP CRACKED AT BS 747, STR 22L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 68,281 hrs · 58,761 cycles

TIE CLIP CRACKED AT BS 727D, STR 25L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 68,281 hrs · 58,761 cycles

TIE CLIP CRACKED AT BS 727B, STR 22L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 68,281 hrs · 58,761 cycles

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

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 68,281 hrs · 58,761 cycles

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

Part: WEB — CORRODED (FUSELAGE) · airframe 68,281 hrs · 58,761 cycles

WEB CORRODED BETWEEN BS 420 TO BS 440, STR 17L. REPAIRED WEB IAW EO AND EA.

Part: SKIN — CORRODED (FUSELAGE) · airframe 68,281 hrs · 58,761 cycles

SKIN CORRODED AT BS 520, BETWEEN STR 27R AND STR 28R. REPAIRED SKIN IAW EO AND EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 68,281 hrs · 58,761 cycles

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

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 68,281 hrs · 58,761 cycles

LEFT SUPPORT ANGLE CRACKED AT BS 727A. REMOVED AND REPLACED ANGLE IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 68,281 hrs · 58,761 cycles

TIE CLIP CRACKED AT BS 500C, STR 20R. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,281 hrs · 58,761 cycles

SKIN CRACKED AT BS 1156+5, RBL 3. REPAIRED SKIN IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 68,281 hrs · 58,761 cycles

TIE CLIP CRACKED AT BS 500D, STR 23R. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 68,281 hrs · 58,761 cycles

SHEAR TIE CORRODED AT BS 500D, BETWEEN STR 28L AND STR 28R. REMOVED AND REPLACED SHEAR TIE IAW SRM AND DWG.

Part: ANGLE — CRACKED (LT HORIZ STAB) · airframe 68,281 hrs · 58,761 cycles

LEFT HORIZONTAL STABILIZER CENTER SECTION ANGLE CRACKED AT BS 1121, LBL 10. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 68,281 hrs · 58,761 cycles

WEB CORRODED BETWEEN BS 420 TO BS 440, STR 17R. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 68,281 hrs · 58,761 cycles

FRAME CORRODED AT BS 747, BETWEEN STR 25R TO STR 26R. REPAIRED FRAME IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 68,281 hrs · 58,761 cycles

TIE CLIP CRACKED AT BS 767, STR 25R. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 68,281 hrs · 58,761 cycles

WEB CORRODED BETWEEN BS 400 TO BS 420, STR 17R. REPAIRED WEB IAW EO AND EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 68,281 hrs · 58,761 cycles

WEB ANGLE CRACKED AT BS 767+5, STR 25R. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 68,281 hrs · 58,761 cycles

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

Part: ANGLE — CRACKED (FUSELAGE) · airframe 68,281 hrs · 58,761 cycles

ANGLE CRACKED AT BS 400, STR 26R. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 68,281 hrs · 58,761 cycles

CHANNEL CORRODED BETWEEN BS 727D TO BS 727E, LBL 8.10. REPAIRED CHANNEL IAW EA.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 68,281 hrs · 58,761 cycles

SUPPORT ANGLE CORRODED AT FWD ENTRY DOOR AT LEVEL STR 17L. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 68,281 hrs · 58,761 cycles

ANGLE CRACKED AT BS 540, BETWEEN STR 21R TO STR 22R. REPAIRED ANGLE IAW SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 68,281 hrs · 58,761 cycles

KEEL BEAM CORRODED BETWEEN BS 500D AND BS 520, STR 28R. REPAIRED BEAM IAW EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 68,281 hrs · 58,761 cycles

TIE CLIP CRACKED AT BS 297, STR 28R. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 68,281 hrs · 58,761 cycles

WEB CRACKED BETWEEN BS 400 TO BS 420, STR 26R. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 68,281 hrs · 58,761 cycles

CHANNEL CORRODED AT BS 859.7, LBL 8.10. REPAIRED CHANNEL IAW EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 68,281 hrs · 58,761 cycles

CHANNEL CORRODED AT BS 859.7, LBL 3. REPAIRED CHANNEL IAW EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 68,281 hrs · 58,761 cycles

CHANNEL CORRODED AT BS 727D+5, LBL 3. REPAIRED CHANNEL IAW EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 68,281 hrs · 58,761 cycles

TIE CLIP CRACKED AT BS 480, STR 26L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 68,281 hrs · 58,761 cycles

TIE CLIP CRACKED AT BS 947.5, STR 26L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 68,281 hrs · 58,761 cycles

PRESSURE BULKHEAD STIFFENER CRACKED AT BS 727, STR 27R. REMOVED AND REPLACED STIFFENER IAW SRM AND DWG.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 68,281 hrs · 58,761 cycles

STIFFENER CRACKED AT BS 727, STR 27L. REMOVED AND REPLACED STIFFENER IAW SRM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 68,281 hrs · 58,761 cycles

ANGLE CRACKED AT BS 500B, STR 26L. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 68,281 hrs · 58,761 cycles

CHANNEL CORRODED AT BS 727D+5, RBL 3. REPAIRED CHANNEL IAW EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 68,281 hrs · 58,761 cycles

TIE CLIP CRACKED AT BS 500C, STR 27L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 68,281 hrs · 58,761 cycles

CHANNEL CORRODED AT BS 727D+5, RBL 8.10. REPAIRED CHANNEL IAW EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 68,281 hrs · 58,761 cycles

TIE CLIP CRACKED AT BS 727B, STR 25L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 68,281 hrs · 58,761 cycles

AFT CARGO COMPARTMENT ANGLE CRACKED AT BS 947.5, BETWEEN STR 25R TO STR 24R. REMOVED AND REPLACED ANGLE IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,281 hrs · 58,761 cycles

SKIN CRACKED AT BS 360+2, BETWEEN STR 5R TO STR 6R. REPAIRED SKIN IAW EA.

Part: DOOR — CRACKED (R1 DOOR) · airframe 68,281 hrs · 58,761 cycles

FORWARD GALLEY DOOR FWD LOWER CORNER SKIN CRACKED. REMOVED AND REPLACED DOOR IAW AMM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 68,281 hrs · 58,761 cycles

SKIN CORRODED BETWEEN BS 520 AND BS 540, BETWEEN STR 28L AND STR 28R. REPAIRED SKIN IAW EO AND EA.

Part: BATTERY — DISCHARGED (CABIN) · airframe 67,837 hrs · 58,435 cycles

AFT GALLEY EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 67,754 hrs · 58,377 cycles

LEFT EMERGENCY EXIT LIGHT INOP AT ROW 5. RELAMPED LIGHT PER AMM.

Part: SIGN — LOOSE (CABIN) · airframe 67,754 hrs · 58,377 cycles

AFT EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER SOPM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 67,754 hrs · 58,377 cycles

R2 DOOR EMERGENCY EXIT SIGN BULB INOP. RELAMPED SIGN ASSY PER AMM.

Part: LIGHT — LOOSE (CABIN) · airframe 67,754 hrs · 58,377 cycles

EMERGENCY LIGHT LOOSE BETWEEN ROW 5 TO ROW 6. SECURED LIGHT IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 66,870 hrs · 57,719 cycles

R1 DOOR EMERGENCY LIGHT INOP. RELAMPED LIGHT PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 66,870 hrs · 57,719 cycles

L2 DOOR EMERGENCY EXI LIGHT BULB INOP. RELAMPED LIGHT PER AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,866 hrs · 57,718 cycles

FUSELAGE SKIN CRACKED AT BS 303, STR 13L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,865 hrs · 57,717 cycles

SKIN CRACKED AT BS 305, STR 13L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,865 hrs · 57,717 cycles

FUSELAGE SKIN CRACKED AT BS 305, STR 13L. REPAIRED SKIN PER SRM.

Part: TAB — CRACKED (LT AILERON) · airframe 66,865 hrs · 57,717 cycles

LT WING AILERON TAB CRACKED AT NR 3 HINGE FITTING CUTOUT. REMOVED AND REPLACED TAB IAW MM.

Part: LIGHT — BROKEN (CABIN) · airframe 66,217 hrs · 57,223 cycles

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

Part: LENS — LOOSE (CABIN) · airframe 66,081 hrs · 57,133 cycles

DURING SCHEDULED CV CHECK FOUND LT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: LIGHT — WORN (CABIN) · airframe 66,081 hrs · 57,133 cycles

DURING SCHEDULED CV CHECK FOUND EEPLS WORN BETWEEN ROW 9 TO ROW 10. REMOVED AND REPLACED EEPLS PER MM.

Part: LENS — LOOSE (CABIN) · airframe 65,493 hrs · 56,685 cycles

AFT CABIN EMERGENCY EXIT LIGHT LENS LOOSE AT ROW 22. SECURED LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,217 hrs · 56,474 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,217 hrs · 56,474 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR UPPER CORNER CUTOUT. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,214 hrs · 56,473 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,217 hrs · 56,474 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR UPPER CORNER CUTOUT. REPAIRED SKIN PER SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 64,872 hrs · 56,197 cycles

DURING SCHEDULED MV1 CHECK, FOUND RT MID CABIN OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,375 hrs · 55,816 cycles

DURING SCHEDULED CV CHECK FOUND, SKIN CRACKED AT BS 420+16, STR 2R. REPAIRED SKIN PER EA.

Part: FLAP — DELAMINATED (LT WING) · airframe 64,375 hrs · 55,816 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,887 hrs · 62,836 cycles

FUSELAGE CROWN SKIN CRACKED AT BS 420+16, STRINGER 2R. REPAIRED SKIN IAW EA.

Part: DOOR FRAME — CRACKED (R1 DOOR) · airframe 63,432 hrs · 55,093 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND R1 DOOR VERTICAL FRAME CRACKED. REMOVED AND REPLACED DOOR PER MM.

Part: MODULE — FAULTY (E&E BAY) · airframe 63,203 hrs · 54,909 cycles

NR 2 ENG FIRE LIGHT INDICATION ERRATIC WITH A-LOOP SELECTED. REMOVED AND REPLACED M279 FIRE DETECTION UNIT PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 63,133 hrs · 54,859 cycles

DURING SCHEDULED 18Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,133 hrs · 54,859 cycles

DURING SCHEDULED 18Y CHECK, FOUND L2 DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM.

Part: DOOR FRAME — CRACKED (R2 DOOR) · airframe 63,133 hrs · 54,859 cycles

DURING SCHEDULED 18Y CHECK, FOUND R2 DOOR FWD EDGE FRAME UPPER DOOR ARM CUTOUT, CRACKED AT LOWER FORWARD CORNER. REMOVED AND REPLACED FRAME PER BAC DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 63,133 hrs · 54,859 cycles

DURING SCHEDULED 18Y CHECK, FOUND FLIGHT DECK FLOOR WEB CRACKED AT BS 246.6, RBL 23.5. REPAIRED WEB PER ACO.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 63,133 hrs · 54,859 cycles

DURING SCHEDULED 18Y CHECK, FOUND CENTER WING BOX LONGITUDINAL FLOORBEAM CRACKED AT BS 639, RBL 45.5. REMOVED AND REPLACED ANGLE PER SRM AND BAC DWG.

Part: ATTACH BRACKET — CRACKED (R2 DOOR) · airframe 63,133 hrs · 54,859 cycles

DURING SCHEDULED 18Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE ATTACH BRACKET CRACKED. REMOVED AND REPLACED BRACKET PER SOPM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 63,133 hrs · 54,859 cycles

DURING SCHEDULED 18Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 709, BBL 0.07. REPAIRED BEAM PER SRM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 63,133 hrs · 54,859 cycles

DURING SCHEDULED 18Y CHECK, FOUND RT WING NR 5 SLAT T/E WEDGE DELAMINATED AT I/B END. REPAIRED WEDGE PER SRM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 63,133 hrs · 54,859 cycles

DURING SCHEDULED 18Y CHECK, FOUND RT WING NR 4 SLAT T/E WEDGE DELAMINATED AT O/B END. REPAIRED WEDGE PER SRM.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 63,133 hrs · 54,859 cycles

DURING SCHEDULED 18Y CHECK, FOUND L1 DOOR FRAME FWD CUTOUT LOWER ATTACH ANGLE CRACKED AT BS 294.5, STR 11L. REMOVED AND REPLACED ANGLE PER SRM AND BAC DWG.

Part: SPOILER — DELAMINATED (RT WING) · airframe 63,123 hrs · 54,852 cycles

RIGHT WING NR 8 GROUND SPOILER DELAMINATED. REMOVED AND REPLACED SPOILER PER MM.

Part: ACTUATOR — LEAKING (SPOILER) · airframe 62,881 hrs · 54,667 cycles

AIR TURNBACK,ON TAKEOFF AT ROTATION LOST ALL A SYSTEM HYDRAULIC FLUID. REMOVED AND REPLACED NR 3 FLIGHT SPOILER ACTUATOR PER MM.

Part: SIGN — BROKEN (CABIN) · airframe 62,854 hrs · 54,644 cycles

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

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 61,047 hrs · 53,283 cycles

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

Part: LIGHT — BROKEN (CABIN) · airframe 60,596 hrs · 52,953 cycles

DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR LOWER EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 60,227 hrs · 52,680 cycles

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

Part: SLAT — DELAMINATED (WING) · airframe 59,463 hrs · 52,078 cycles

DURING SCHEDULED MV1 CHECK, FOUND NR 5 SLAT DELAMINATED. REMOVED AND REPLACED NR 5 SLAT PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 58,704 hrs · 51,499 cycles

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

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 57,082 hrs · 50,345 cycles

DURING SCHEDULED 16Y CHECK, FOUND L1 DOOR SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 57,082 hrs · 50,345 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING NR 2 SLAT O/B TRAILING EDGE UPPER SURFACE DELAMINATED. REMOVED AND REPLACED SLAT PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,082 hrs · 50,345 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 8. RELAMPED LIGHT PER MM.

Part: STRIP — DAMAGED (CABIN) · airframe 57,082 hrs · 50,345 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT EEPLS STRIP DAMAGED. R&R STRIP PER MM.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 57,082 hrs · 50,345 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING NR 2 SLAT O/B TRAILING EDGE UPPER SURFACE DELAMINATED. REMOVED AND REPLACED SLAT PER MM.

Part: STRIP — DAMAGED (CABIN) · airframe 57,082 hrs · 50,345 cycles

DURING SCHEDULED 16Y CHECK, FOUND R/H EEPLS STRIP DAMAGED. R&R STRIP PER MM.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 57,082 hrs · 50,345 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING NR 5 SLAT I/B END TOP SIDE DELAMINATED. REMOVED AND REPLACED SLAT PER MM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 57,082 hrs · 50,345 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM WEB CRACKED AT BS 294, LBL 52. REPAIRED WEB PER EA.

Part: SLAT — DELAMINATED (RT WING) · airframe 57,082 hrs · 50,345 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING NR 5 SLAT O/B SIDE DELAMINATED. REPAIRED SLAT PER SRM.

Part: HOUSING — BROKEN (CABIN) · airframe 57,082 hrs · 50,345 cycles

DURING SCHEDULED 16Y CHECK, FOUND R1 DOOR EMERGNECY EXIT LIGHT HOUSING BROKEN. REMOVED AND REPLACED LIGHT HOUSING PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,082 hrs · 50,345 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 328, STR 21L. REMOVED AND REPLACED CLIP PER SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 57,082 hrs · 50,345 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING O/B AFT FLAP DELAMINATED. REPAIRED FLAP PER SRM.

Part: LENS — CRACKED (CABIN) · airframe 57,082 hrs · 50,345 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CABIN CENTER EMERGENCY EXIT SIGN LENS CRACKED. REMOVED AND REPLACED LENS PER MM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 57,052 hrs · 50,324 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM TEE CAP CRACKED AT BS 294, LBL 52. REPAIRED BEAM PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 57,082 hrs · 50,345 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 685, STR 15L. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,082 hrs · 50,345 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 17R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,082 hrs · 50,345 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,082 hrs · 50,345 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 15L. REMOVED AND REPLACED CLIP PER SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 57,082 hrs · 50,345 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT WING I/B FORE FLAP T/E DELAMINATED. REPAIRED FLAP PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 57,082 hrs · 50,345 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 1L. REMOVED AND REPLACED SPLICE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,082 hrs · 50,345 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 11R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,082 hrs · 50,345 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 24L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,082 hrs · 50,345 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,082 hrs · 50,345 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 328, STR 21L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,082 hrs · 50,345 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 336, STR 21L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,082 hrs · 50,345 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 11L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,082 hrs · 50,345 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 22L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,082 hrs · 50,345 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 23L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,082 hrs · 50,345 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 13L. REMOVED AND REPLACED CLIP PER SRM.

Part: WEB — CRACKED (BS 188) · airframe 57,082 hrs · 50,345 cycles

DURING SCHEDULED 16Y CHECK, FOUND WEB CRACKED AT BS 188, RBL 45. REPAIRED WEB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,082 hrs · 50,345 cycles

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

Part: LIGHT — LOOSE (CABIN) · airframe 57,082 hrs · 50,345 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT OVERHEAD BULLNOSE LIGHT LOOSE AT ROW 13 ABC. SECURED LIGHT PER SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 57,082 hrs · 50,345 cycles

DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM CRACKED AT R1 DOOR. REPAIRED BEAM PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,082 hrs · 50,345 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 947D, STR 22L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,082 hrs · 50,345 cycles

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

Part: FLAP — DELAMINATED (LT WING) · airframe 56,099 hrs · 49,637 cycles

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

Part: HANDLE — DIRTY (COCKPIT) · airframe 55,894 hrs · 49,483 cycles

WITH LANDING GEAR HANDLE IN DOWN POSITION HAD THREE GREEN AND THREE RED LIGHTS ILLUMINATED. CYCLED GEAR UP AND DOWN, ALL INDICATIONS NORMAL. CLEANED AND LUBED GEAR HANDLE PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 55,677 hrs · 49,329 cycles

DURING SCHEDULED SPV CHECK, FOUND LEFT AFT FUSELAGE EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 55,677 hrs · 49,329 cycles

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

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 55,677 hrs · 49,329 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,677 hrs · 49,329 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 25L. REPAIRED FRAME PER ER.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 55,677 hrs · 49,329 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 520, STR 18R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 55,677 hrs · 49,329 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 520, STR 21R. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,677 hrs · 49,329 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 21L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 55,677 hrs · 49,329 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 15R. REPAIRED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,677 hrs · 49,329 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 390, RBL 2. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,677 hrs · 49,329 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 450, LBL 3. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,677 hrs · 49,329 cycles

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

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 55,677 hrs · 49,329 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 908, STR 15R. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 55,677 hrs · 49,329 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 15R CRACKED AT BS 380. REPAIRED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,677 hrs · 49,329 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,677 hrs · 49,329 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 2R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,677 hrs · 49,329 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,677 hrs · 49,329 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,677 hrs · 49,329 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 3R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,677 hrs · 49,329 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,677 hrs · 49,329 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 2L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,677 hrs · 49,329 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,677 hrs · 49,329 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 3R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 55,677 hrs · 49,329 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 4R CRACKED AT BS 500. REPAIRED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,677 hrs · 49,329 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,677 hrs · 49,329 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,677 hrs · 49,329 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,677 hrs · 49,329 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,677 hrs · 49,329 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 2L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,677 hrs · 49,329 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,677 hrs · 49,329 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 460, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,677 hrs · 49,329 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,677 hrs · 49,329 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,677 hrs · 49,329 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,677 hrs · 49,329 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,677 hrs · 49,329 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,677 hrs · 49,329 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,576 hrs · 49,254 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 733E AND BS 731E, STR 25L AND STR 22L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,127 hrs · 48,915 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 911, STR 22R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,127 hrs · 48,915 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 731E, STR 22L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 761 S10R) · airframe 54,534 hrs · 48,472 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 761, STR 10R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 753 S25L) · airframe 54,534 hrs · 48,472 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 753, STR 25L. REPAIRED SKIN PER SWA EA.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 54,145 hrs · 48,156 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS INOP AT ROW 6 ABC. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: ROD END — WORN (SPOILER ACTUATOR) · airframe 54,145 hrs · 48,156 cycles

DURING SCHEDULED C2 CHECK, FOUND RT WING NR 5 GROUND SPOILER OUTBOARD ACTUATOR ROD END BROKEN. REMOVED AND REPLACED ROD END PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 53,521 hrs · 47,664 cycles

DURING SPV CHECK, FOUND LEFT WING OUTBOARD T/E AFT FLAP DELAMINATED. REPAIRED FLAP ASSY PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,521 hrs · 47,664 cycles

DURING SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 794, STR 10R. REPAIRED SKIN PER SWA EA.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 53,520 hrs · 47,663 cycles

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

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 53,520 hrs · 47,663 cycles

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

Part: SKIN — CRACKED (BS 733 S21R) · airframe 53,007 hrs · 47,258 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 733, STR 21R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 822 S25R) · airframe 53,007 hrs · 47,258 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 822, STR 25R. REPAIRED SKIN PER SWA EA.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 52,504 hrs · 46,845 cycles

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

Part: O-RING — LEAKING (-A-HYD SYS) · airframe 52,448 hrs · 46,798 cycles

AIR TURNBACK/DECLARED EMERGENCY. TOTAL -A- SYSTEM HYDRAULIC FLUID AND PRESSURE LOSS. REMOVED AND REPLACED NR 2 SPOILER ACTUATOR O-RING PER MM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 52,404 hrs · 46,765 cycles

DURING SCHEDULED C4 CHECK, FOUND RT HORIZONTAL STAB SKIN CRACKED AT LOWER SURFACE STA 120. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 52,404 hrs · 46,765 cycles

DURING SCHEDULED C4 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: FAN — FAULTY (E/E BAY) · airframe 51,920 hrs · 46,390 cycles

FLIGHT ATTENDANT REPORTED BURNT RUBBER ODOR, TURNED OFF RECIRC FAN, ODOR DISSIPATED. REMOVED AND REPLACED RECIRC FAN PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 50,582 hrs · 45,258 cycles

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

Part: SKIN — CRACKED (BS 729E) · airframe 50,490 hrs · 45,287 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 729E, STR 24L. REPAIRED SKIN PER SWA EA.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 50,490 hrs · 45,287 cycles

DURING SCHEDULED C2 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 50,490 hrs · 45,287 cycles

DURING SCHEDULED C2 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 10 DEF. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 49,769 hrs · 44,695 cycles

DURING SCHEDULED C1 CHECK, FOUND RT HORIZONTAL STAB LOWER SURFACE SKIN CRACKED AT STA 107. REPAIRED SKIN PER SRM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 49,463 hrs · 44,467 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FWD GALLEY OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 49,463 hrs · 44,467 cycles

DURING SCHEDULED 1/2D CHECK, FOUND AFT GALLEY EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: TEE FITTING — CRACKED (AFT CARGO DOOR) · airframe 49,463 hrs · 44,467 cycles

DURING SCHEDULED 1/2D CHECK, FOUND AFT CARGO DOOR LOWER OUTBOARD TEE CRACKED AT FWD END. REMOVED AND REPLACED AFT CARGO DOOR PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,463 hrs · 44,467 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 500, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 49,463 hrs · 44,467 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CRACKED AT BS 500, STR 10R. REPAIRED STRINGER PER SRM.

Part: BELTFRAME — CORRODED (FUSELAGE) · airframe 49,463 hrs · 44,467 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE BELT FRAME CORRODED AT BS 727D, BETWEEN LBL 20 TO LBL 30. REPAIRED BELT FRAME PER SRM.

Part: BELTFRAME — CORRODED (FUSELAGE) · airframe 49,463 hrs · 44,467 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE BELT FRAME CORRODED AT BS 727D, BETWEEN RBL 20 TO RBL 30. REPAIRED BELT FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,463 hrs · 44,467 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 294.5, STR 7L. REMOVED AND REPLACED CLIP PER SRM.

Part: DOOR FRAME — CRACKED (R1 DOOR) · airframe 49,463 hrs · 44,467 cycles

DURING SCHEDULED 1/2D CHECK, FOUND R1 DOOR AFT FRAME CRACKED AT NR 4 STOP FITTING CUTOUT. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,463 hrs · 44,467 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, BETWEEN STR 20R & STR 21R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,463 hrs · 44,467 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, BETWEEN STR 20L & STR 21L. REPAIRED FRAME PER SWA EA.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 49,463 hrs · 44,467 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE BEADED PRESSURE WEB CRACKED AT BS 664, BETWEEN RBL 39 & RBL 40. REPAIRED WEB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,463 hrs · 44,467 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500B, BETWEEN STR 20L & STR 21L. REPAIRED FRAME PER SWA EA.

Part: FLOORBEAM — CORRODED (BS 772) · airframe 49,463 hrs · 44,467 cycles

DURING SCHEDULED 1/2D CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER FLANGE CORRODED AT BS 772, LBL 7. REPAIRED FLOORBEAM PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 787 S23R) · airframe 49,463 hrs · 44,467 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 787, STR 23R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 663) · airframe 49,463 hrs · 44,467 cycles

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

Part: SHEAR TIE — CRACKED (BS 360) · airframe 49,463 hrs · 44,467 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 360, BETWEEN STR 13L TO STR 14L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (BS 518D) · airframe 49,463 hrs · 44,467 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 518D, STR 12L. REPAIRED SKIN PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 663) · airframe 49,463 hrs · 44,467 cycles

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

Part: CREASE BEAM — CORRODED (BS 360-380) · airframe 49,463 hrs · 44,467 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE CREASE BEAM WEB CORRODED BETWEEN BS 360 TO BS 380, STR 17R. REPAIRED WEB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,463 hrs · 44,467 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR CUTOUT, FWD LOWER CORNER. REPAIRED SKIN PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 49,463 hrs · 44,467 cycles

DURING SCHEDULED 1/2D CHECK, FOUND LONGITUDINAL FLOORBEAM CORRODED AT BS 772, LBL 12. REPAIRED FLOORBEAM PER SWA EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 49,463 hrs · 44,467 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME ANGLE CRACKED AT R1 DOOR CUTOUT, BS 294.5, STR 17R. REPAIRED ANGLE PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 49,463 hrs · 44,467 cycles

DURING SCHEDULED 1/2D CHECK, FOUND LONGITUDINAL FLOOR BEAM CORRODED AT BS 663, BL 0. REPAIRED FLOOR BEAM PER SWA EA.

Part: BELTFRAME — CRACKED (FUSELAGE) · airframe 49,463 hrs · 44,467 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE BELTFRAME CRACKED AT LOWER INBD FLANGE, BS 616, STR 17R. REPAIRED BELTFRAME PER TRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 49,463 hrs · 44,467 cycles

DURING SCHEDULED 1/2D CHECK, FOUND LT WING INBD T/E AFT FLAP DELAMINATED. REPAIRED FLAP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,463 hrs · 44,467 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR LOWER HINGE CUTOUT, FWD LOWER CORNER. REPAIRED SKIN PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,463 hrs · 44,467 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 663, STR 11L. R&R CLIP PER SRM.

Part: STRUCTURE — DELAMINATED (T/E FLAP) · airframe 49,154 hrs · 44,244 cycles

DURING SCHEDULED A2 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM.

Part: SKIN — DELAMINATED (NR 5 SLAT) · airframe 48,827 hrs · 44,003 cycles

DURING SCHEDULED C4 CHECK, FOUND RT WING NR 5 L/E SLAT DELAMINATED AT OUTBOARD END. REPAIRED SLAT PER SRM.

Part: SKIN — CRACKED (BS 947) · airframe 48,827 hrs · 44,003 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947, STR 24R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 971) · airframe 48,667 hrs · 43,866 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 971, STR 21L. REPAIRED SKIN PER SWA EA & SRM.

Part: SKIN — CRACKED (BS 520) · airframe 48,667 hrs · 43,866 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 12L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 767) · airframe 48,037 hrs · 43,356 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 767, STR 23L. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 47,884 hrs · 43,240 cycles

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

Part: HOOK — OUT OF ADJUST (R2 DOOR SLIDE) · airframe 47,826 hrs · 43,193 cycles

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

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 47,517 hrs · 42,951 cycles

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

Part: SLIDE — OUT OF LIMITS (R2 DOOR) · airframe 47,194 hrs · 42,678 cycles

R2 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATOR OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 46,935 hrs · 42,455 cycles

DURING SCHEDULED C2 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,935 hrs · 42,455 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT A/C GROUND SERVICE DOOR CUTOUT, LT FWD CORNER, BS 520, STR 28L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,935 hrs · 42,455 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR CUTOUT, LOWER AFT CORNER. REPAIRED SKIN PER SWA EA.

Part: LIGHT — MISSING (CABIN) · airframe 46,854 hrs · 42,395 cycles

BULLNOSE EMERGENCY EXIT LIGHT MISSING AT ROW 2. INSTALLED LIGHT ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,104 hrs · 41,766 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727 E + 16, STR 24L. REPAIRED SKIN PER SRM.

Part: SKIN — DELAMINATED (LT WING FLAP) · airframe 46,104 hrs · 41,766 cycles

DURING SCHEDULED C1 CHECK, FOUND LT WING INBOARD AFT FLAP T/E DELAMINATED. REPAIRED FLAP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,104 hrs · 41,766 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,104 hrs · 41,766 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E + 6, STR 25R. REPAIRED SKIN PER SWA EA & SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,104 hrs · 41,766 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 948.5, L2 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,104 hrs · 41,766 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 948.5, R2 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 45,905 hrs · 41,625 cycles

BULLNOSE EMERGENCY EXIT LIGHT LENS BROKEN AT ROW 2. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 45,731 hrs · 41,488 cycles

DURING SCHEDULED SERVICE CHECK, FOUND MID CABIN EMERGENCY EXIT LIGHT BATTERY PACK WEAK. REMOVED AND REPLACED BATTERY PER MM.

Part: LIGHT — LOOSE (ROW 21 ABC) · airframe 45,089 hrs · 40,973 cycles

DURING SCHEDULED SERVICE CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT ASSEMBLY AT ROW 21 ABC, LOOSE. SECURED LIGHT ASSEMBLY PER MM.

Part: SKIN — CRACKED (LT OVERWING DOOR) · airframe 44,218 hrs · 40,278 cycles

DURING SCHEDULED C3 CHECK, FOUND LT OVERWING DOOR SKIN AT THE 12 O' CLOCK POSITION CRACKED. REMOVED AND REPLACED OVERWING DOOR PER MM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 44,065 hrs · 40,167 cycles

BULLNOSE EMERGENCY EXIT LIGHT LENS AT ROW 8 DEF, LOOSE. SECURED LIGHT LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,835 hrs · 39,965 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 937, STRINGER 24L, CRACKED. REPAIRED SKIN PER EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,997 hrs · 39,278 cycles

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

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 42,064 hrs · 38,553 cycles

DURING SCHEDULED SERVICE CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED L2 DOOR EMERGENCY EXIT LIGHT PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 41,091 hrs · 37,753 cycles

DURING SCHEDULED 1/4D CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 23L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FLOORBEAM — CORRODED (AFT CARGO) · airframe 41,091 hrs · 37,753 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM CORRODED AT BS 792, LBL 8. REPAIRED FLOORBEAM PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 41,091 hrs · 37,753 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) BS 727D AT STR 23L AND BS 941 AT STR 24L. REPAIRED SKIN PER SRM.

Part: SLIDE — DISLODGED (SERVICE DOOR) · airframe 39,842 hrs · 36,708 cycles

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

Part: LENS — MISSING (CABIN) · airframe 38,791 hrs · 35,855 cycles

DURING SCHEDULED C1 CHECK, FOUND OVERHEAD BIN BULLNOSE EMERGENCY LIGHT LENS MISSING AT ROW 5 DEF. INSTALLED LENS PER MM.

Part: SOLENOID — FAILED (COCKPIT) · airframe 37,466 hrs · 34,731 cycles

AIR TURNBACK, AFTER TAKEOFF LANDING GEAR WOULD NOT RETRACT. FOUND GEAR LEVER CONTROL LOCK SOLENOID INOP. REMOVED AND REPLACED SOLENOID PER MM.

Part: SLIDE — OUT OF ADJUST (BOTH AFT DOORS) · airframe 36,934 hrs · 34,289 cycles

DURING SCHEDULED C3 CHECK, FOUND BOTH AFT CABIN DOOR EMERGENCY EVAC SLIDE GIRT ASSY'S OUT OF ADJUST. ADJUSTED SLIDE'S PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 35,178 hrs · 32,880 cycles

DURING SCHEDULED C1 CHECK, FOUND EMERGENCY BULLNOSE LIGHT LOOSE AT ROW 3 ABC. REMOVED AND REPLACED RETAINER ASSY PER MM.

Part: SLIDE — UNSERVICEABLE (ENTRY DOOR) · airframe 33,225 hrs · 31,264 cycles

DURING SCHEDULED A1 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. Removed and replaced EMERGENCY EVAC SLIDE PER MM.

Part: LENS — MISSING (CABIN) · airframe 33,031 hrs · 31,094 cycles

OVERHEAD BIN BULLNOSE EMERGENCY EXIT LIGHT LENS MISSING AT ROW 20 DEF. REPLACED LENS PER MM.

Part: SLIDE — UNSERVICEABLE (ENTRY DOOR) · airframe 32,879 hrs · 30,951 cycles

DURING SCHEDULED D CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. R&R SLIDE ASSY PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,879 hrs · 30,951 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKS AT BS 727D, STR 9L & 9R. REPAIRED FRAMES PER SRM & BFG ER.

Part: FITTING — CORRODED (RT WING) · airframe 32,879 hrs · 30,951 cycles

DURING SCHEDULED D CHECK, FOUND RT WING MLG STAB SUPPORT BEAM FITTING CORRODED. R&R BEAM FITTING PER MM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 32,879 hrs · 30,951 cycles

DURING SCHEDULED D CHECK, FOUND SHEAR TIE CRACKED AT BS 360, BETWEEN STR 14L & 15L. R&R SHEAR TIE PER SRM & BAC DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,879 hrs · 30,951 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED AT BS 827 & BS 907, STR 9L. REPAIRED FRAMES PER SRM & BFG ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,879 hrs · 30,951 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKS AT BS 867, STR 9L & 9R. REPAIRED FRAMES PER SRM & BFG ER.

Part: FRAME — CORRODED (FUSELAGE) · airframe 32,879 hrs · 30,951 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 500, LBL 6 TO RBL 2, WL 148. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,879 hrs · 30,951 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,879 hrs · 30,951 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED AT BS 400, BS 480 & BS 787, STR 9R. REPAIRED FRAMES PER SRM & BFG ER.

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 32,879 hrs · 30,951 cycles

DURING SCHEDULED D-CHECK, FOUND VERT STAB FWD PRIMARY CLEVIS, FACE & BORE, CORRODED. REPAIRED FITTING PER BFG ER.

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 32,879 hrs · 30,951 cycles

DURING SCHEDULED D-CHECK, FOUND VERT STAB AFT PRIMARY CLEVIS, AFT LUG FACE AND BORE, CORRODED. REPAIRED FITTING PER BFG ER.

Part: FITTING — CORRODED (LT WING) · airframe 32,879 hrs · 30,951 cycles

DURING SCHEDULED D CHECK, FOUND LT WING MLG BEAM SUPPORT LINK FITTING CORRODED ON LUG FACE. R&R BEAM FITTING PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,879 hrs · 30,951 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 492, WL 160, R/H SIDE, INSIDE RADIUS. REPAIRED FRAME PER SRM.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 32,879 hrs · 30,951 cycles

DURING SCHEDULED D CHECK, FOUND EXTERNAL FUSELAGE SKIN CREASED AT BS 360+11, STR 5L. REPAIRED SKIN PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 32,879 hrs · 30,951 cycles

DURING SCHEDULED D CHECK, FOUND FLOOR BEAM CORRODED AT BS 986.5, RBL 35 TO RBL 45. R&R FLOORBEAM PER T1-453-037.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 32,879 hrs · 30,951 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE T-CHORD CORRODED AT BS 328, RBL 42 & RBL 49, LOWER SURFACE. REPAIRED FRAME PER SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 32,340 hrs · 30,509 cycles

DURING SCHEDULED C2 CHECK, FOUND RT WING T/E INBOARD AFT FLAP OUTBOARD LWR SURFACE DISBONDED. REPAIRED AFT FLAP ASSY PER SRM.

Part: BEAM — CRACKED (FUSELAGE) · airframe 32,317 hrs · 30,491 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD VERTICAL BEAM WEB CRACKED AT RBL 17.1, WL 227. REPAIRED VERTICAL BEAM WEB PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,317 hrs · 30,491 cycles

DURING SCHEDULED SPECIAL VISIT AT DALFORT, FOUND EMERGENCY EXIT LIGHT INOP AT BULLNOSE, ROW 7 ABC. REMOVED AND REPLACED LAMP PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 32,317 hrs · 30,491 cycles

DURING SCHEDULED SPECIAL VISIT AT DALFORT, FOUND 8 BS 178 BULKHEAD WEB CRACKS AT LBL 17.1 TO RBL 17.1, WL 198 TO WL 232. REPAIRED BULKHEAD WEB PER SRM.

Part: CAP — MISSING (FLOOR LIGHT) · airframe 31,432 hrs · 29,749 cycles

DURING SCHEDULED C1 CHECK, FOUND FWD EEPLS END CAP MISSING. INSTALLED END CAP PER MM.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 30,511 hrs · 28,940 cycles

DURING SCHEDULED C4 CHECK, FOUND LT WING OUTBD AFT FLAP DELAMINATED AT INB END. R&R FLAP ASSY PER MM.

Part: COVER — CRACKED (CABIN) · airframe 29,620 hrs · 28,164 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS AFT END TRACK COVER CRACKED. R&R TRACK COVER PER MM.

Part: RELAY — FAILED (CABIN)

AIR TURNBACK, DURING CLIMB, BOTH LEFT AND RIGHT IRS WENT TO DC FAIL C/W QRH PROCEDURES. NO HELP. REMOVED AND REPLACED RELAYS R-1, R-4, R-344. RAN ACFT ENGS AND APU. ALL INDICATIONS NORMAL PER MM.

Part: SLIDE — OUT OF POSITION (PAX DOOR)

FWD ENTRY DOOR EVACUATION SLIDE ASSY OUT OF POSITION. REPOSITIONED SLIDE ASSY PER MM.

Part: BULB — FAILED (ROW 4)

DURING SCHEDULED A1 CHECK, FOUND FLOOR TRACK LIGHT INOP AT FWD, AFT AND ROW 4 SECTIONS. REMOVED AND REPLACED BULB PER MM.

Part: TERMINAL — LOOSE (ROW 10)

DURING SCHEDULED 1/4D CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT ROW 10 LT OVERHEAD BIN. TIGHTENED LOOSE TERMINAL ON LIGHT ASSY, OPS CK GOOD PER M/M.

Part: BATTERY — DISCHARGED (CABIN)

DURING PREFLIGHT CHECK, FOUND FWD EMERGENCY FLASHLIGHT INOP. REPLACED BATTERY PER BOEING M/M.

Part: LIGHT — INOPERATIVE (PAX DOOR)

DURING SCHEDULED SERVICE CHECK, FWD ENTRYWAY FLASHLIGHT FAILED TEST. REPLACED BATTERY PACK PER BOEING M/M.

Part: SLIDE — LOW PRESS (R2 DOOR)

DURING A1 CHECK, FOUND R2 DOOR SLIDE PRESSURE LOW. REPLACED PER BOEING M/M.

Part: FRAME — CRACKED (CARGO DOORWAY)

DURING SCHEDULED BC3 CHECK, FOUND A .5 INCH CRACK IN FWD CARGO DOOR FWD FRAME JUST BELOW UPLOCK AT STOP CUTOUT. REPAIRED PER BOEING SRM.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING SCHEDULED 1/2 D-CHECK, FOUND EMERGENCY EXIT LIGHTING INOP IN VARIOUS CABIN LOCATIONS. REPLACED BATTERY PACKS PER BOEING M/M.

Part: GEAR PIN — NOT REMOVED (LANDING GEAR)

AFTER TAKEOFF, LANDING GEAR WOULD NOT RETRACT. AIRCRAFT RETURNED TO PHX AND MADE AN UNEVENTFUL LANDING. INSPECTED AIRCRAFT, REMOVED GEAR PINS.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING SCHEDULED B/C CHECK, FOUND EMERGENCY TRACK LIGHTING INOP AT ROWS 12 DEF AND 14ABC. REPLACED BATTERY PACK AND HOUSING PER BOEING M/M.

Part: EEL BATTERY — DISCHARGED (L2 DOOR)

DURING SCHEDULED SERVICE CHECK, FOUND LEFT AFT ENTRY DOOR EMERGENCY LIGHTING INOP. REPLACED BATTERY PACK PER BOEING M/M.