N659SW

Part: SKIN — CRACKED (FUSELAGE) · airframe 89,114 hrs · 67,105 cycles

FUSELAGE SKIN CRACKED AT STATION 559+12, STRINGER 10L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 89,114 hrs · 67,105 cycles

FUSELAGE SKIN CRACKED AT STATION 685+14, STRINGER 10R. REPAIRED SKIN IAW EA.

Part: LENS — MISSING (CABIN) · airframe 88,735 hrs · 66,822 cycles

L1 DOOR EMER EXIT LIGHT LENS MISSING. R & R LIGHT ASSEMBLY IAW AMM.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 88,695 hrs · 66,792 cycles

L1 DOOR EMER EVAC SLIDE LOOSE. SECURED SLIDE IAW MT.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 88,378 hrs · 66,558 cycles

L1 DOOR EMER EVAC SLIDE OUT OF POSITION. REPOSITION SLIDE IAW MT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 88,186 hrs · 66,414 cycles

L2 DOOR EMER LIGHT INOPERATIVE. R & R BULB IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 88,186 hrs · 66,414 cycles

R2 DOOR EMER LIGHT INOPERATIVE. R & R BULB IAW AMM.

Part: SLIDE — UNSECURE (L2 DOOR) · airframe 87,441 hrs · 65,844 cycles

L2 DOOR EMER EVAC SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY, STILL OPERATIONAL. REINSTALLED SLIDE IAW MT.

Part: FRAME — CORRODED (FUSELAGE) · airframe 87,292 hrs · 65,736 cycles

FRAME CORRODED AT BS 188, RBL 5. REPAIRED FRAME IAW EA.

Part: BUTT JOINT — CORRODED (FUSELAGE) · airframe 87,292 hrs · 65,736 cycles

SKIN BUTT SPLICE CORRODED AT BS 196.5+5, RBL 2. REPAIRED BUTT SPLICE IAW ER & EA.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 87,292 hrs · 65,736 cycles

LOWER OUTER CHORD AT FRAME CORRODED AT BS. 203.8, BETWEEN LBL 2 - 8. R & R CHORD IAW SRM & DWG.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 87,288 hrs · 65,735 cycles

FRAME INTERCOSTAL ATTACH ANGLE CORRODED AT BS 203, RBL 0+6. R & R ANGLE IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 87,106 hrs · 65,602 cycles

RIGHT WW FWD WHEEL CUT OUT CURVED LOWER CHORD ANGLE CRACKED ON THE OTBD END AT RBL 68. REPAIRED ANGLE IAW EA.

Part: STRUT — SHEARED (FUSELAGE) · airframe 87,106 hrs · 65,602 cycles

LEFT WW FWD WHEEL CUT OUT INBD ATTACH STRUT SHEARED AT LBL 48. R & R STRUT IAW SRM & DWG.

Part: STRUT — SHEARED (FUSELAGE) · airframe 87,106 hrs · 65,602 cycles

RIGHT WW FWD WHEEL CUT OUT INBD ATTACH STRUT SHEARED AT RBL 48. R & R STRUT IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 87,106 hrs · 65,602 cycles

LEFT WW FWD WHEEL CUT OUT CURVED LOWER CHORD ANGLE CRACKED ON THE OTBD END AT LBL 68. REPAIRED CHORD IAW SRM & DWG.

Part: COVER — LOOSE (CABIN) · airframe 86,603 hrs · 65,225 cycles

R2 DOOR EMER EXIT LIGHT COVER LOOSE. R & R COVER IAW AMM.

Part: WEB — CRACKED (FUSELAGE) · airframe 85,985 hrs · 64,783 cycles

FLOOR WEB CRACKED BETWEEN BS 1017 TO 1023 BETWEEN LBL 13 TO 17. R & R WEB IAW SRM.

Part: WIRE — BROKEN (CABIN) · airframe 85,985 hrs · 64,783 cycles

AFT EMER BATTERY WIRE BROKEN AT BS 967. REPAIRED WIRE IAW AMM.

Part: WIRE — BROKEN (CABIN) · airframe 85,985 hrs · 64,783 cycles

AFT GALLEY EMER BATTERY WIRE BROKEN AT BS 967. REPAIRED WIRE IAW & AMM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 85,985 hrs · 64,783 cycles

AFT CARGO BAY FLOOR SPLICE STRAP CRACKED AT BS 767. R & R STRAP IAW SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 85,985 hrs · 64,783 cycles

STRINGER CRACKED AT BS 500D STRINGER 8L. R & R STRINGER IAW SRM.

Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 85,985 hrs · 64,783 cycles

RIGHT KEEL BEAM CRACKED AT BS 540.9. REPAIRED KEEL BEAM IAW ER & EA.

Part: STRAP — CRACKED (FUSELAGE) · airframe 85,985 hrs · 64,783 cycles

FORWARD ENTRY DOOR CUT OUT UPPER HINGE H STRAP CRACKED AT BS 304 STRINGER 10L. R & R H STRAP IAW SRM & DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 85,985 hrs · 64,783 cycles

INTERCOSTAL CORRODED BETWEEN BS 352 TO 360 STRINGER 9L. REPAIRED INTERCOSTAL IAW ER & EA.

Part: STRAP — CRACKED (FUSELAGE) · airframe 85,985 hrs · 64,783 cycles

FORWARD ENTRY DOOR CUT OUT LOWER HINGE H STRAP CRACKED AT BS 304 STRINGER 13L. R & R H STRAP IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 85,985 hrs · 64,783 cycles

INTERCOSTAL CRACKED BETWEEN BS 295 TO 303 STRINGER 7L. R & R INTERCOSTAL IAW SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 85,985 hrs · 64,783 cycles

INTERCOSTAL CORRODED BETWEEN BS 352 TO 360 STRINGER 14L. REPAIRED INTERCOSTAL IAW ER & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 85,985 hrs · 64,783 cycles

FRAME CRACKED AT BS 663.75 STRINGER 3R. REPAIRED FRAME IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 85,985 hrs · 64,783 cycles

FRAME CRACKED AT BS 663.75 STRINGER 3L. REPAIRED FRAME IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 85,985 hrs · 64,783 cycles

STRINGER CLIP CRACKED AT BS 663.75 STRINGER 10R. R & R CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 85,985 hrs · 64,783 cycles

STRINGER CLIP CRACKED AT BS 500D STRINGER 8L. R & R CLIP IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 85,985 hrs · 64,783 cycles

BULKHEAD SPLICE ANGLE CRACKED AT BS 540 BETWEEN STRINGER 20L TO 23L. R & R ANGLE IAW ER & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 85,985 hrs · 64,783 cycles

FRAME CRACKED AT BS 663.75 STRINGER 2R. REPAIRED FRAME IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 85,985 hrs · 64,783 cycles

FIRST OFFICER`S C - D NR 1 WINDOW POST UPPER END CRACKED AT BS 215 NR 1 WINDOW. REPAIRED SKIN IAW SRM & EA & ER.

Part: WEB — CRACKED (FUSELAGE) · airframe 85,985 hrs · 64,783 cycles

FLIGHT DECK FLOOR WEB CRACKED AT BS 259.5, BETWEEN LBL 4 TO LBL 9. REPAIRED WEB IAW EA.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 85,985 hrs · 64,783 cycles

AFT GALLEY DOOR BEAR STRAP CUT OUT CRACKED AT AFT UPPER CORNER. REPAIRED BEAR STRAP IAW SRM.

Part: DOOR — CRACKED (FUSELAGE) · airframe 85,985 hrs · 64,783 cycles

NOSE BAY DOOR CRACKED AT BS 1103 AFT SIDE ON VERTICAL ANGLE AT CUT OUT. R & R DOOR IAW AMM.

Part: SKATE ANGLE — CRACKED (TE FLAP) · airframe 85,985 hrs · 64,783 cycles

RIGHT WING NR 7 FWD FLAP TRACK FAIRING OTBD SKATE ANGLE CRACKED AT REAR SPAR. REPAIRED ANGLE IAW SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 85,985 hrs · 64,783 cycles

BULKHEAD WEB CRACKED AT BS 1016 STRINGER 6L. REPAIRED WEB IAW ER & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 85,985 hrs · 64,783 cycles

FUSELAGE SKIN CRACKED AT BS 528 LBL 5. REPAIRED SKIN IAW ATS ER & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 85,985 hrs · 64,783 cycles

FUSELAGE SKIN CRACKED BETWEEN BS 526 TO 528 RBL 5. REPAIRED SKIN IAW ATS ER & EA.

Part: DOUBLER — DELAMINATED (TE FLAP) · airframe 85,985 hrs · 64,783 cycles

RIGHT WING INBD FORE FLAP UPPER SURFACE DOUBLER DELAMINATED. REPAIRED FORE FLAP IAW SRM.

Part: SUPPORT ANGLE — CRACKED (NR 1 PYLON) · airframe 85,985 hrs · 64,783 cycles

LEFT WING NR 1 PYLON INBD SUPPORT CLIP FOR UPPER AFT PANEL SUPPORT ANGLE CRACKED. R & R ANGLE IAW SRM.

Part: SUPPORT FITTING — CRACKED (RT WING) · airframe 85,985 hrs · 64,783 cycles

RIGHT WING HYD LINE SUPPORT BRACKET CRACKED ON INBD SIDE OF NR 5 SPOILER INBD ACTUATOR SUPPORT FITTING. R & R FITTING IAW SRM.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 85,985 hrs · 64,783 cycles

MAIN WW PRESS DECK CRACKED AT BS 665 LBL 40. REPAIRED DECK IAW EA & ER.

Part: SLAT — CRACKED (RT WING) · airframe 85,985 hrs · 64,783 cycles

RIGHT WING NR 4 SLAT INBD AFT FASTENER CRACKED. REPAIRED NR 4 SLAT IAW SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 85,984 hrs · 64,783 cycles

LEFT KEEL BEAM CORRODED AT BS 500C+15. R & R BEAM IAW SRM.

Part: PIN — MISSING (ESCAPE STRAP) · airframe 85,984 hrs · 64,783 cycles

LEFT EMER EXIT HATCH ESCAPE STRAP MISSING HOOK PIN. INSTALLED PIN ASSEMBLY IAW SOPM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 85,984 hrs · 64,783 cycles

FRAME CRACKED AT BS 727D BETWEEN LBL 2 RBL 2. REPAIRED FRAME IAW ER & EA.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 85,984 hrs · 64,783 cycles

FORWARD LOWER HOLE CHORD CRACKED AT BS 727 STRINGER 18A LT. REPAIRED CHORD IAW ER & EA.

Part: LENS — LOOSE (CABIN) · airframe 85,613 hrs · 64,511 cycles

CENTER OVERWING EEPLS LENS LOOSE. SECURED LENS IAW SIP.

Part: SIGN — BROKEN (CABIN) · airframe 84,842 hrs · 63,969 cycles

L1 DOOR EMERGENCY EXIT LIGHT FWD OF DOOR BROKEN. R & R SIGN IAW AMM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 84,723 hrs · 63,895 cycles

SHEAR TIE CRACKED AT BS 277, BETWEEN STRINGER 16L TO STRINGER 17L. R & R SHEAR TIE IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 84,723 hrs · 63,895 cycles

FUSELAGE SKIN CRACKED BETWEEN BS 272 TO BS 274, STRINGER 15L. REPAIRED SKIN IAW SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 84,723 hrs · 63,895 cycles

R1 DOOR EMERGENCY LIGHT ON SIDE WALL TOP LIGHTS INOPERATIVE. R & R LIGHT IAW AMM.

Part: ATTACH ANGLE — CRACKED (LT WING) · airframe 84,694 hrs · 63,876 cycles

LT WING UPPER TE FIXED PANEL INBD OF NR 4 SPOILER ATTACH ANGLE CRACKED. R & R ANGLE IAW SRM.

Part: SKIN — CRACKED (LT WING) · airframe 84,694 hrs · 63,876 cycles

LT WING LE SKIN CRACKED ABOVE NR 3 SLAT ACTUATOR. REPAIRED SKIN IAW SRM.

Part: FITTING — LOOSE (NR 4 SPOILER) · airframe 84,694 hrs · 63,876 cycles

LT WING NR 4 SPOILER INBD ACTUATOR ATTACH BRACKET LOOSE. R & R FITTING IAW SRM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 84,694 hrs · 63,876 cycles

RT WING IFOT FAIRING DELAMINATED AT MID FLAP ROLLER SCUFF PLATE. REPAIRED SKIN IAW EA.

Part: FLAP — DELAMINATED (LT WING) · airframe 83,710 hrs · 63,187 cycles

LT WING INBD AFT FLAP DELAMINATED. R & R AFT FLAP IAW MM.

Part: ACTUATOR — FAULTY (RT SPOILER) · airframe 83,614 hrs · 63,103 cycles

AFTER TO FROM SAT MOST INBD FLIGHT RT WING SPOILER REMAINED UP 4-5 INCHES, REMAINED SO REST OF FLIGHT. R&R NR 6 SPOILER ACTUATOR IAW MM.

Part: TORQUE TUBE — FAULTY (TE FLAP) · airframe 83,314 hrs · 62,860 cycles

DECLARED EMERGENCY, WHEN SELECTING FLAPS 30 DEG FROM 15 DEG LT TRAILING FLAP STOPPED AT 25 DEG RT TRAILING FLAP WENT TO 30 DEG. AFTER GO ROUND STRAIGHT & LEVEL FLIGHT REQUIRED 4 DEG LT AILERON. R&R RT WING TE INBD MOST FLAP TORQUE TUBE IAW AMM.

Part: SKIN — CRACKED (LE SLAT) · airframe 83,106 hrs · 62,706 cycles

LT WING NR 2 SLAT LOWER L/E SKIN CRACKED AT OUTBD AUX TRACK. REPAIRED SKIN IAW SRM.

Part: SLAT — CRACKED (RT WING) · airframe 83,106 hrs · 62,706 cycles

RT WING NR 5 SLAT LOWER L/E CRACKED AT ACTUATOR ATTACH POINT. REPAIRED NR 5 SLAT IAW SRM.

Part: LENS — LOOSE (CABIN) · airframe 83,073 hrs · 62,680 cycles

LT BULLNOSE EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LIGHTS IAW MM.

Part: LIGHT — LOOSE (CABIN) · airframe 83,073 hrs · 62,680 cycles

FWD ENTRY EMERGENCY EXIT LIGHT ASSEMBLY LOOSE. R&R LIGHT ASSEMBLY IAW AMM.

Part: HINGE — BROKEN (RT SPOILER) · airframe 82,114 hrs · 61,975 cycles

RIGHT WING GROUND SPOILER HINGE BROKEN. REMOVED AND REPLACED RIGHT GROUND SPOILER PER AMM.

Part: PANEL — DELAMINATED (LE SLAT) · airframe 81,410 hrs · 61,462 cycles

LEFT WING LOWER LEADING EDGE PANEL O/B OF NR 3 SLAT ACTUATOR DELAMINATED (MARKED). REPAIRED PER SRM 57-41-01-2R-8.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 80,753 hrs · 60,965 cycles

FLOORBEAM UPPER CHORD CRACKED AT BS 967, RBL 54. REPAIRED CHORD PER SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 80,753 hrs · 60,965 cycles

SUPPORT ANGLE CRACKED AT BS 660, LBL 26.5. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: STRAP — CRACKED (FUSELAGE) · airframe 80,753 hrs · 60,965 cycles

FRAME CRACKED STRAP AT BS 992.8, BETWEEN STR STR 10L TO STR 20L. REMOVED AND REPLACED STRAP IAW EO AND EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 80,753 hrs · 60,965 cycles

WEB CRACKED BETWEEN BS 727A TO 727B, STR 25L. REMOVED AND REPLACED WEB IAW SRM AND SRM DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 80,753 hrs · 60,965 cycles

WEB CRACKED BETWEEN BS 927 TO BS 947.5, STR 25R. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 80,753 hrs · 60,965 cycles

WEB CRACKED AT BS 344, RBL 0. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: SLAT — DELAMINATED (LT WING) · airframe 80,753 hrs · 60,965 cycles

LEFT WING NR 3 SLAT I/B EDGE DELAMINATED. REMOVED AND REPLACED NR 3 SLAT IAW AMM & SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 80,753 hrs · 60,965 cycles

WEB CORRODED BETWEEN BS 1006 TO BS 1016, STR 17L. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: WIRE — BROKEN (CABIN) · airframe 80,753 hrs · 60,965 cycles

WIRE BROKEN ON CONNECTOR AT BS 628. REPAIRED WIRE IAW SWPM.

Part: SIGN — INOPERATIVE (CABIN) · airframe 80,753 hrs · 60,965 cycles

EMERGENCY EXIT LIGHT ASSEMBLY INOP AT MID CABIN. REMOVED AND REPLACED SIGN IAW AMM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 80,753 hrs · 60,965 cycles

TIE CLIP CRACKED AT BS 360, STR 26R. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 80,753 hrs · 60,965 cycles

ANGLE CRACKED AT BS 328, BETWEEN STR 20L AND STR 21L. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 80,753 hrs · 60,965 cycles

TIE CLIP CRACKED AT BS 360, STR 25R. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 80,753 hrs · 60,965 cycles

ANGLE CRACKED AT BS 328+8, BETWEEN STR 20L AND STR 21L. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 80,753 hrs · 60,965 cycles

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

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 80,753 hrs · 60,965 cycles

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

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 80,753 hrs · 60,965 cycles

TIE CLIP CRACKED AT BS 360, STR 27L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 80,753 hrs · 60,965 cycles

ANGLE CRACKED AT BS 312+9, BETWEEN STR 20L AND STR 21L. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 80,753 hrs · 60,965 cycles

TIE CLIP CRACKED AT BS 380, STR 23L. REMOVED AND REPLACED TIE CLIP PER SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 80,753 hrs · 60,965 cycles

TIE CLIP CRACKED AT BS 312, STR 18R. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 80,753 hrs · 60,965 cycles

ANGLE CRACKED AT BS 947.5, STR 2R. REMOVED AND REPLACED ANGLE IAW SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 80,753 hrs · 60,965 cycles

LEFT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT INOP AT ROW 2. REMOVED AND REPLACED LIGHT IAW AMM.

Part: WEB — CRACKED (FUSELAGE) · airframe 80,753 hrs · 60,965 cycles

WEB CRACKED BETWEEN BS 344 TO BS 360, BL 0. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 80,753 hrs · 60,965 cycles

WEB CRACKED BETWEEN BS 277 TO BS 294.5, STR 14R. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 80,753 hrs · 60,965 cycles

SUPPORT ANGLE CRACKED BETWEEN STA 277 TO STA 294.5, BETWEEN STR 10R TO STR 11R. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 80,753 hrs · 60,965 cycles

R1 DOOR Z-ANGLE CORRODED ON LOWER SILL. REMOVED AND REPLACED Z-ANGLE IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 80,753 hrs · 60,965 cycles

TIE CLIP CRACKED AT BS 847, STR 19L. REMOVED AND REPLACED TIE CLIP IAW SRM & DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 80,753 hrs · 60,965 cycles

FRAME CORRODED AT BS 992.8, STR 17L. REPAIRED FRAME IAW EO AND EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 80,753 hrs · 60,965 cycles

FLOORBEAM UPPER CHORD CORRODED AT BS 986.5, BETWEEN RBL 15 TO RBL 45.5. REPAIRED BEAM IAW EO AND EA.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 80,753 hrs · 60,965 cycles

Z-ANGLE CORRODED BETWEEN BS 303.9 TO BS 348.2, STR 17R. REMOVED AND REPLACED Z-ANGLE IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 80,753 hrs · 60,965 cycles

FRAME CORRODED AT BS 1006, STR 19L. REPAIRED FRAME IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,753 hrs · 60,965 cycles

FUSELAGE SKIN CRACKED AT L1 DOOR UPPER COVER HINGE CUTOUT. REMOVED AND REPLACED SKIN IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 80,753 hrs · 60,965 cycles

FLOORBEAM CRACKED AT BS 663, LBL 24.8. REPAIRED WEB IAW EO AND EA.

Part: TIE CLIP — CORRODED (FUSELAGE) · airframe 80,753 hrs · 60,965 cycles

TIE CLIP CORRODED AT BS 986.5, STR 24R. REMOVED AND REPLACED TIE CLIP IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 80,753 hrs · 60,965 cycles

TIE CLIP CRACKED AT BS 1006, STR 21R. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,753 hrs · 60,965 cycles

FUSELAGE SKIN CRACKED AT L1 DOOR LOWER COVER HINGE CUTOUT. REMOVED AND REPLACED SKIN IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 80,753 hrs · 60,965 cycles

FRAME CRACKED AT BS 947.5, STR 18L. REMOVED AND REPLACED FRAME IAW SRM AND DWG.

Part: TIE CLIP — CORRODED (FUSELAGE) · airframe 80,753 hrs · 60,965 cycles

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

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 80,753 hrs · 60,965 cycles

TIE CLIP CRACKED AT BS 420, STR 23R. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 80,753 hrs · 60,965 cycles

SUPPORT ANGLE CRACKED AT BS 500B, LBL 21.8. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 80,753 hrs · 60,965 cycles

TIE CLIP CRACKED AT BS 500A, STR 22R. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 80,753 hrs · 60,965 cycles

TIE CLIP CRACKED AT BS 420, STR 22R. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 80,753 hrs · 60,965 cycles

TIE CLIP CRACKED AT BS 727B, STR 18R. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 80,753 hrs · 60,965 cycles

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

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 80,753 hrs · 60,965 cycles

CHANNEL CORROSION AT BS 727C+6, RBL 3. REPAIRED CHANNEL IAW EA AND SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 80,753 hrs · 60,965 cycles

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

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 80,753 hrs · 60,965 cycles

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

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 80,753 hrs · 60,965 cycles

TIE CLIP CRACKED AT BS 787, STR 20R. REMOVED AND REPLACED TIE CLIP IAW SRM & DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 80,753 hrs · 60,965 cycles

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

Part: FRAME — CORRODED (FUSELAGE) · airframe 80,753 hrs · 60,965 cycles

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

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 80,753 hrs · 60,965 cycles

CHANNEL CORROSION AT BS 794, RBL 3. REPAIRED CHANNEL IAW EA AND SRM.

Part: SLAT — DAMAGED (LT WING) · airframe 80,753 hrs · 60,965 cycles

LEFT WING NR 3 SLAT O/B EDGE OF TRAILING EDGE BROKEN. REMOVED AND REPLACED NR 3 SLAT IAW AMM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 80,753 hrs · 60,965 cycles

SUPPORT ANGLE CRACKED AT BS 727D, STR 24L. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 80,753 hrs · 60,965 cycles

SHEAR TIE CORRODED AT BS 500, BETWEEN STR 27R TO STR 28R. REPAIRED SHEAR TIE PER SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 80,753 hrs · 60,965 cycles

CHANNEL ANGLE CORRODED AT BS 727D+5, LBL 8.10. REMOVED AND REPLACED ANGLE IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,753 hrs · 60,965 cycles

FUSELAGE SKIN CRACKED AT BS 259.5+13, STR 16L. REPAIRED SKIN IAW SRM.

Part: TIE CLIP — CORRODED (FUSELAGE) · airframe 80,753 hrs · 60,965 cycles

TIE CLIP CORRODED AT BS 807, STR 26R. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: SLAT — CRACKED (RT WING) · airframe 80,753 hrs · 60,965 cycles

RIGHT WING NR 5 SLAT CRACKED. REPAIRED SLAT IAW SRM AND DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 80,753 hrs · 60,965 cycles

CHANNEL ANGLE CORRODED AT BS 727D+5, RBL 8.10. REMOVED AND REPLACED ANGLE IAW EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 80,753 hrs · 60,965 cycles

STRINGER CORRODED BETWEEN BS 480 TO BS 500, STR 27L. REPAIRED STRINGER IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 80,753 hrs · 60,965 cycles

SHEAR TIE CORRODED AT BS 500, BETWEEN STR 27L TO STR 28L. REMOVED AND REPLACED SHEAR TIE PER SRM AND DWG.

Part: LIGHT — DAMAGED (CABIN) · airframe 80,753 hrs · 60,965 cycles

EEPLS DAMAGED. REMOVED AND REPLACED EEPLS IAW AMM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 80,753 hrs · 60,965 cycles

STIFFENER CRACKED AT BS 727, LBL 6 AFT CARGO COMP. REMOVED AND REPLACED STIFFENER IAW SRM AND DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 80,753 hrs · 60,965 cycles

CHANNEL ANGLE CORRODED AT BS 727D+5, LBL 3.00. REMOVED AND REPLACED ANGLE IAW EA.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 80,753 hrs · 60,965 cycles

CHANNEL ANGLE CORRODED AT BS 727D+5, LBL 12.50. REMOVED AND REPLACED ANGLE IAW EA.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 80,753 hrs · 60,965 cycles

ANGLE CORRODED AT BS 727D+5, RBL 3.00. REMOVED AND REPLACED ANGLE IAW EA.

Part: LIGHT — BROKEN (CABIN) · airframe 80,753 hrs · 60,965 cycles

R2 DOOR EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY IAW AMM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 80,753 hrs · 60,965 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 663.75, LBL 24.5. REPAIRED CHORD IAW EA AND EO.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 80,753 hrs · 60,965 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD CRACK AT BS 727B, LBL 24.5. REPAIRED CHORD IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 80,753 hrs · 60,965 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 663.75, RBL 24.5. REPAIRED CHORD IAW EA AND EO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,753 hrs · 60,965 cycles

FUSELAGE SKIN CRACKED AT BS 251.6, STR 24L. REPAIRED SKIN IAW EO AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,753 hrs · 60,965 cycles

SKIN CRACKED AT BS 947.5, STR 11L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (R1 DOOR) · airframe 80,753 hrs · 60,965 cycles

R1 DOOR EXTERNAL SKIN CRACKED AT FWD EDGE UPPER HINGE CUTOUT. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (R1 DOOR) · airframe 80,753 hrs · 60,965 cycles

R1 DOOR EXTERNAL SKIN CRACKED BETWEEN BS 299 TO BS 304, STR 16R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,753 hrs · 60,965 cycles

SKIN CRACKED AT BS 947.5, STR 11R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 80,725 hrs · 60,938 cycles

RIGHT HORIZONTAL STABILIZER SKIN CRACKED O/B ON LOWER SKIN AT AFT SPAR. REPAIRED SKIN PER EA.

Part: SLIDE — LOOSE (R1 DOOR) · airframe 80,691 hrs · 60,913 cycles

R1 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE IAW AMM & MT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 80,655 hrs · 60,884 cycles

L2 DOOR AFT EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER AMM.

Part: SWITCH — FAULTY (E&E BAY) · airframe 80,020 hrs · 60,399 cycles

ON APPROACH LANDING GEAR SELECTED DOWN THREE GREEN AND THREE RED LIGHT ILLUMINATED CYCLED GEAR ALL INDICATIONS NORMAL. REMOVED AND REPLACED CONTROL LEVER SWITCH IAW M/M.

Part: CONNECTOR — LOOSE (COCKPIT) · airframe 79,982 hrs · 60,365 cycles

ALL RED & GREEN LANDING LIGHT INDICATORS REMAINED ILLUMINATED WITH GEAR HANDLE DOWN. TRIED TO RESEAT HANDLE WITH NO EFFECT. RECYCLED GEAR & RECEIVED A SAFE INDICATION FOR LANDING. FOUND DEBRIS ON GEAR HANDLE AND PIN NOT SECURED AT CONNECTOR D4. SECURED PIN AT CONNECTOR D4096P PER MM.

Part: FIRE WARNING — FALSE ACTIVATION (CARGO BAY) · airframe 79,512 hrs · 60,004 cycles

DIVERSION/DECLARED EMERGENCY -- AFT CARGO FIRE LIGHT ILLUMINATED INFLT DISCHARGED BOTH BOTTLES IN AFT CARGO BAY. INSPECTED AFT CARGO BIN, NO EVIDENCE OF FIRE FOUND. FOUND CUSTOMER BAGGAGE TO HAVE HAIR SPRAY PRODUCTS DISCHARGED IN CARGO BIN.

Part: FRAME — CRACKED (FUSELAGE) · airframe 79,248 hrs · 59,813 cycles

DURING SCHEDULED OTS CHECK, FOUND FRAME CRACKED AT BS 500B, BETWEEN STR 20L TO STR 21L. REPAIRED FRAME SECTION IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 79,248 hrs · 59,813 cycles

DURING SCHEDULED OTS CHECK, FOUND FRAME CRACKED AT BS 500D, BETWEEN STR 20L TO STR 21L. REPAIRED FRAME SECTION IAW EA.

Part: LENS — LOOSE (CABIN) · airframe 78,912 hrs · 59,548 cycles

DURING SCHEDULED CV CHECK, FOUND LT EEPLS LENS LOOSE AT ROW 13. SECURED LENS PER MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 78,457 hrs · 59,208 cycles

DURING SCHEDULED MV2 CHECK, FOUND FWD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: BEAM — CRACKED (FUSELAGE) · airframe 78,258 hrs · 59,058 cycles

DURING SCHEDULED SPV CHECK, FOUND RT STUB BEAM INNER CHORD CRACKED AT BS 616. REPAIRED CHORD IAW EA.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 78,258 hrs · 59,058 cycles

DURING SCHEDULED SPV CHECK, FOUND LT STUB BEAM ATTACH CLIP CRACKED AT BS 639, LBL 45.5. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 78,258 hrs · 59,058 cycles

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

Part: BATTERY — DISCHARGED (CABIN) · airframe 78,258 hrs · 59,058 cycles

DURING SCHEDULED SPV CHECK, FOUND L2 DOOR EMERGENCY EXIT SIGN INOP. CHARGED EMERGENCY EXIT BATTERIES IAW MM.

Part: ACTUATOR — FAULTY (LT MLG) · airframe 78,196 hrs · 59,015 cycles

AIR TURNBACK --LT MLG INDICATES UNSAFE ON RETRACTION. REMOVED HYDRAULIC PRESSURE (LANDING GEAR HANDLE OFF), CYCLED GEAR. SAME RESULT. REMOVED AND REPLACED LT MLG LOCK ACTUATOR IAW MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 77,937 hrs · 58,814 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: SIGN — LOOSE (CABIN) · airframe 77,391 hrs · 58,391 cycles

FWD EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 77,350 hrs · 58,358 cycles

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

Part: SKIN — CORRODED (FUSELAGE) · airframe 75,202 hrs · 56,707 cycles

DURING SCHEDULED 26Y CHECK, FOUND SKIN CORRODED AT BS 792, STR 20R. REPAIRED SKIN PER SRM AND EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 75,202 hrs · 56,707 cycles

DURING SCHEDULED 26Y CHECK, FOUND FRAME WEB CRACKED AT BS 303.9, 16L STOP FITTING. REPAIRED WEB PER AAR EA.

Part: FITTING — LOOSE (GIRT BAR) · airframe 75,205 hrs · 56,710 cycles

DURING SCHEDULED 26Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING LOOSE. REMOVED AND REPLACED FITTING PER MM.

Part: FITTING — LOOSE (GIRT BAR) · airframe 75,205 hrs · 56,710 cycles

DURING SCHEDULED 26Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING LOOSE. REMOVED AND REPLACED FITTING PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 75,202 hrs · 56,707 cycles

DURING SCHEDULED 26Y CHECK, FOUND EEPLS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: WEDGE — DELAMINATED (TE FLAP) · airframe 75,202 hrs · 56,707 cycles

DURING SCHEDULED 26Y CHECK, FOUND RT WING I/B MID FLAP T/E WEDGE LOWER SURFACE DELAMINATED. REPAIRED WEDGE PER SRM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 75,202 hrs · 56,707 cycles

DURING SCHEDULED 26Y CHECK, FOUND RT WING NR 5 SLAT O/B MID FLAP T/E WEDGE LOWER SURFACE DELAMINATED. REPAIRED WEDGE PER SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 75,202 hrs · 56,707 cycles

DURING SCHEDULED 26Y CHECK, FOUND FLOORBEAM VERTICAL ANGLE CRACKED AT BS 328, LBL 29. REMOVED AND REPLACED ANGLE PER BAC DWG.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 75,202 hrs · 56,707 cycles

DURING SCHEDULED 26Y CHECK, FOUND LT WING NR 3 SLAT O/B CORNER T/E WEDGE DELAMINATED. REPAIRED WEDGE PER SRM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 75,202 hrs · 56,707 cycles

DURING SCHEDULED 26Y CHECK, FOUND LT WING NR 2 SLAT O/B CORNER T/E WEDGE DELAMINATED. REPAIRED WEDGE PER SRM.

Part: LENS — LOOSE (CABIN) · airframe 75,202 hrs · 56,707 cycles

DURING SCHEDULED 26Y CHECK, FOUND RT EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LENS PER MM.

Part: LIGHT — FADED (CABIN) · airframe 74,634 hrs · 56,264 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT EEPLS FADED AT ROW 22. REMOVED AND REPLACED EEPLS PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 74,605 hrs · 56,243 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 74,343 hrs · 56,028 cycles

RIGHT OVERHEAD BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 8. REMOVED AND REPLACED BULB PER MM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 73,692 hrs · 55,539 cycles

DURING SCHEDULED SPV CHECK, FOUND LT KEEL BEAM CORRODED BETWEEN BS 737 TO BS 727A. REPAIRED BEAM PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 559, BETWEEN STR 13R TO STR 14R. REPAIRED FRAME PER SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND LT KEEL BEAM LOWER CHORD CORRODED AT BS 815. REPAIRED CHORD PER SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND LT KEEL BEAM LOWER CHORD CORRODED AT BS 741. REPAIRED CHORD PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 747, BETWEEN STR 27R TO STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED AT BS 731A, STR 26L. REMOVED AND REPLACED STRINGER PER SRM.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND DOORWAY FRAME DOUBLER CRACKED AT BS 794.5, BETWEEN STR 22R TO STR 26R. REMOVED AND REPLACED DOUBLER PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 747, BETWEEN STR 26L TO STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 847, BETWEEN STR 27L TO STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED AT BS 731A, STR 26L. REPAIRED STRINGER SECTION PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 727E, BETWEEN STR 26L TO STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 887, STR 13R. REPAIRED FRAME PER EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 807, BETWEEN STR 26L TO STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 807, BETWEEN STR 27L TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

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

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 787, BETWEEN STR 27R TO STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 26L. REMOVED AND REPLACED CLIP PER SRM.

Part: KEELBEAM — CRACKED (BS 741) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND RT KEEL BEAM SPLICE CRACKED AT BS 741. R&R BEAM PER SRM.

Part: STRAP — CORRODED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN BUTT STRAP SPLICE STRAP CORRODED AT BS 360, STR 23R. REPAIRED STRAP PER ER.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 787, BETWEEN STR 26L TO STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND LT KEEL BEAM CORRODED AT BS 727, LBL 6. REMOVED AND REPLACED BEAM PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 727D, BETWEEN STR 25L TO STR 26L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND LT KEEL BEAM CORRODED AT BS 741. REMOVED AND REPLACED KEEL BEAM PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 727D, BETWEEN STR 27L TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND AFT CARGO DOOR UPPER SILL WEB FRAME STRAP CRACKED AT BS 794, STR 18R. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 727C, BETWEEN STR 25L TO STR 26L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND AUX OUTBOARD BULKHEAD CHORD CRACKED AT BS 727, BL 0. REMOVED AND REPLACED CHORD PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND OUTBOARD CENTER BULKHEAD CHORD CRACKED AT BS 727, BL 0. REMOVED AND REPLACED CHORD PER SRM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CORRODED AT BS 360, STR 24L. REMOVED AND REPLACED SPLICE PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CORRODED BETWEEN BS 360 TO BS 390, STR 23R. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CORRODED BETWEEN BS 360 TO BS 390, STR 20R. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CORRODED AT BS 360, STR 24R. REMOVED AND REPLACED SPLICE PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CORRODED AT BS 360, STR 22R. REMOVED AND REPLACED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 19L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CORRODED AT BS 360, STR 25R. R&R STRINGER PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CORRODED AT BS 380, STR 24R. REMOVED AND REPLACED STRINGER PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CORRODED AT BS 355, STR 23R. REMOVED AND REPLACED STRINGER PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CORRODED AT BS 360, STR 27R. REPAIRED STRINGER PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 520, BETWEEN STR 23R TO STR 24R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 787, STR 24R. REPAIRED SKIN PER ACO.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND BUTT STRAP STRINGER SPLICE CORRODED AT BS 908, BETWEEN STR 25L TO STR 25R. REMOVED AND REPLACED STRAP PER DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 767, STR 21L. REPAIRED SKIN PER ACO.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 727C, BETWEEN STR 26R TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CORRODED BETWEEN BS 420 TO BS 440, STR 26L. REPAIRED SKIN PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 727B, BETWEEN STR 16L TO STR 17L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 875, STR 24L. REPAIRED SKIN PER ACO.

Part: SKIN — CORRODED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CORRODED BETWEEN BS 464 TO BS 456, STR 26L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 759, STR 21R. REPAIRED SKIN PER ACO.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 987, BETWEEN STR 24R TO STR 25R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 967, BETWEEN STR 24L TO STR 26L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 727A, STR 13R. REPAIRED FRAME PER ER.

Part: STRINGER — CORRODED (BS 987-1016 S25L) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CORRODED BETWEEN BS 987 TO BS 1016, STR 25L. REPAIRED STRINGER PER SRM.

Part: SHEAR TIE — CORRODED (BS 987 S27L/R) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 987, BETWEEN STR 27L TO STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: SKIN — CORRODED (BS 986-990) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CORRODED BETWEEN BS 986 TO BS 990, BETWEEN STR 24R TO STR 25R. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 21L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 22L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 21L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SECTION CORRODED AT BS 847, STR 10L. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 807, BETWEEN STR 16L TO STR 17L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

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

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 908, STR 25R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

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

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 20R. REMOVED AND REPLACED SPLICE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 500B, BETWEEN STR 15R TO STR 16R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 23R. REMOVED AND REPLACED SPLICE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 18L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 18R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

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

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CORRODED AT BS 727C, STR 24L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 18L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CORRODED AT BS 360, STR 23L. REMOVED AND REPLACED SPLICE PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SECTION CORRODED BETWEEN BS 955 TO BS 1016. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 947, BETWEEN STR 27L TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CORRODED AT BS 908, STR 21L. REMOVED AND REPLACED SPLICE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 19L. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 847, BETWEEN STR 16L TO STR 17L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 19L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 19L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 767D, STR 16L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CORRODED AT BS 727B, STR 24L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 15R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 22L. REMOVED AND REPLACED SPLICE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 15L. REMOVED AND REPLACED CLIP PER SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND L-ANGLE CORRODED AT BS 821, STR 18R. REMOVED AND REPLACED L-ANGLE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 500C, STR 13R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 847, STR 13L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 747, STR 13L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 827, STR 13L. REPAIRED FRAME PER EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED AT BS 887, STR 5L. REMOVED AND REPLACED STRINGER PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 967, BETWEEN STR 20R TO STR 21R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 5L. REMOVED AND REPLACED CLIP PER ACO.

Part: SKIN — CORRODED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND BELLY SKIN CORRODED BETWEEN BS 907 TO BS 1016, STR 25L. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 3L. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 7L. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 5R. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 1L. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 7R. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 6L. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 9L. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 4L. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 5L. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 10L. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 5R. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 7L. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 5L. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 8R. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 2R. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 5L. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 4R. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 6R. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 8L. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 7R. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 5L. REMOVED AND REPLACED CLIP PER SI.

Part: SHEAR TIE — CRACKED (BS 520 S11R) · airframe 73,487 hrs · 55,372 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 520, STR 11R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,487 hrs · 55,372 cycles

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

Part: UPLOCK ACTUATOR — FAULTY (LT MLG) · airframe 72,688 hrs · 54,764 cycles

AFTER TAKEOFF AND AFTER LANDING GEAR RETRACTION, LT MLG UNSAFE (RED) LIGHT REMAINED ILLUMINATED. CYCLED GEAR HANDLE AND LIGHT WENT OUT. REMOVED AND REPLACED BOTH UPLOCK ACTUATOR AND UPLOCK SENSOR MM.

Part: LIGHT — BROKEN (CABIN) · airframe 72,669 hrs · 54,753 cycles

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

Part: UPLOCK SENSOR — OUT OF ADJUST (LT MLG) · airframe 72,661 hrs · 54,749 cycles

AFTER TAKEOFF AND AFTER LANDING GEAR RETRACTION LT MLG UNSAFE (RED) LIGHT STAYED ILLUMINATED. GEAR HANDLE MOVED TO OFF POSITION THEN BACK UP. RED LIGHT EXTINGUISHED, GEAR HANDLE MOVED TO OFF. ADJUSTED UPLOCK SENSOR GAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,991 hrs · 53,554 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 747, STR 22R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,991 hrs · 53,554 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 258, WL 195, LT SIDE. REPAIRED SKIN PER SRM.

Part: BATTERY — LOOSE (CABIN) · airframe 70,301 hrs · 53,061 cycles

DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR LOWER INTERIOR EMERGENCY EXIT LIGHT INOP. SECURED BATTERY PER MM.

Part: BATTERY — LOOSE (CABIN) · airframe 70,301 hrs · 53,061 cycles

DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR LOWER INTERIOR EMERGENCY EXIT LIGHT INOP. SECURED BATTERY PER MM.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 70,218 hrs · 52,998 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT MLG W/W PRESSURE DECK WEB CRACKED AT BS 665 LBL 32. REPAIRED WEB PER SRM.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 70,218 hrs · 52,998 cycles

DURING SCHEDULED HC1 CHECK, FOUND RT MLG W/W PRESSURE DECK WEB CRACKED AT BS 665 RBL 40. REPAIRED WEB PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 70,218 hrs · 52,998 cycles

DURING SCHEDULED HC1 CHECK, FOUND AFT CARGO COMPARTMENT SHEAR TIE CORRODED AT BS 986. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,218 hrs · 52,998 cycles

DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR LOWER FWD FUSELAGE SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 70,024 hrs · 52,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND FWD CARGO COMPT SKIN CORRODED AT BS 500 TO 500A BETWEEN STR 28L TO 28R. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,024 hrs · 52,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 947.5, STR 25R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,024 hrs · 52,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 639, STR 17R. REPAIRED FRAME PER SRM.

Part: LENS — BROKEN (CABIN) · airframe 70,024 hrs · 52,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,024 hrs · 52,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 9R. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 70,024 hrs · 52,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND MAIN CABIN FLOORBEAM CRACKED AT BS 663 BL 0. REPAIRED BEAM PER DHN EA.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 70,024 hrs · 52,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT MLG W/W KEEL BEAM CORRODED AT BS 721. REPAIRED BEAM PER BOEING DRW.

Part: FLAP — DELAMINATED (LT WING) · airframe 70,024 hrs · 52,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT WING O/B AFT FLAP DELAMINATED. REPAIRED FLAP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,024 hrs · 52,863 cycles

DURING SCHEDULED 24Y CHECK, STRINGER CLIP CRACKED AT BS 500C TO BS 500D, STR 26R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,024 hrs · 52,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A TO BS 500B, STR 26R. REMOVED AND REPLACED CLIP PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,024 hrs · 52,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND L1 EMERGENCY EXIT DOOR LOWER LIGHT INOP. RELAMPED LIGHT PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,024 hrs · 52,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND R1 EMERGENCY EXIT DOOR LOWER LIGHT INOP. RELAMPED LIGHT PER MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 70,103 hrs · 52,916 cycles

FOUND R2 DOOR EMERGENCY EXIT ESCAPE SLIDE SIGHT GAUGE OUT OF POSITION. POSITIONED SLIDE PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,024 hrs · 52,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A S26L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 70,024 hrs · 52,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER 24L CORRODED AT BS 967. REPAIRED STRINGER PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,024 hrs · 52,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,024 hrs · 52,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 807 STR 27L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,024 hrs · 52,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 639, STR 17L AND STR 17R. REPAIRED FRAME PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,024 hrs · 52,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,024 hrs · 52,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787 STR 26R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,024 hrs · 52,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500B, STR 20R. REPAIRED FRAME PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 70,024 hrs · 52,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CORRODED AT STA 380 BETWEEN STR 27L & STR 28L. REPAIRED SKIN PER SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 70,024 hrs · 52,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT WING OUTBOARD FORE FLAP DELAMINATED AT INBOARD END. REMOVED AND REPLACED FLAP PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,024 hrs · 52,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,024 hrs · 52,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,024 hrs · 52,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: LENS — WORN (CABIN) · airframe 70,024 hrs · 52,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT LENS WORN. REMOVED AND REPLACED LENS PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,024 hrs · 52,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 26L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 70,024 hrs · 52,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CORRODED. AT BS 827, STR 25L. REPAIRED FRAME PER SRM.

Part: SLAT — DELAMINATED (LT WING) · airframe 70,024 hrs · 52,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT WING NR 2 L/E SLAT DELAMINATED AT INBOARD END. REPAIRED SLAT PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,024 hrs · 52,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 70,024 hrs · 52,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND FLOORBEAM CORRODED AT BS 773, LBL 8. REPAIRED FLOORBEAM PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,024 hrs · 52,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 847, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,024 hrs · 52,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,024 hrs · 52,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,024 hrs · 52,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,024 hrs · 52,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 2R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 70,024 hrs · 52,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 827, STR 25L TO STR 26L. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 70,024 hrs · 52,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 787, STR 26R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,024 hrs · 52,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787 STR 20R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 887 S8R) · airframe 70,024 hrs · 52,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 887, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FLOORBEAM — CRACKED (BS 773) · airframe 70,024 hrs · 52,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND FLOORBEAM CHANNEL CRACKED AT BS 773, LBL 12. REPAIRED FLOORBEAM CHANNEL PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,024 hrs · 52,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRIGNER CLIP CRACKED AT RIGHT BS 886, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOORBEAM — CORRODED (BS 860) · airframe 70,024 hrs · 52,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND FLOORBEAM CORRODED AT BS 860, RBL 8. REPAIRED FLOORBEAM PER SWA EA.

Part: FRAME — CRACKED (BS 867 S8R) · airframe 70,024 hrs · 52,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 380 S8R) · airframe 70,024 hrs · 52,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,024 hrs · 52,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 787 STR 26R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (BS 787 S22R) · airframe 70,024 hrs · 52,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 22R AND STR 21R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 370 S7L) · airframe 70,024 hrs · 52,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 370, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 380 S7L) · airframe 70,024 hrs · 52,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 70,024 hrs · 52,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND CORRODED KEEL BEAM AT BS 703, LBL 6.5. REPAIRED BEAM PER SRM.

Part: SKIN — CRACKED (BS 510 S12R) · airframe 69,585 hrs · 52,557 cycles

DURING SCHEDULED MV4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 510, STR 12R. REPAIRED SKIN PER SWA EA.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 69,120 hrs · 52,209 cycles

DURING SCHEDULED MV3 CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 68,701 hrs · 51,900 cycles

DURING SCHEDULED HC2 CHECK, FOUND LEFT KEEL BEAM CORRODED BETWEEN BS 518 AND BS 520, LBL 6.5. REPAIRED KEEL BEAM PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,692 hrs · 51,891 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 28L. REPAIRED SKIN PER SWA EA.

Part: ACTUATOR — FAULTY (LT MLG) · airframe 68,361 hrs · 51,645 cycles

CREW REPORTED LT MLG DID NOT EXTEND WITH GEAR HANDLE. CYCLED GEAR HANDLE RED LIGHTS REMAINED ILLUMINATED. LOWERED LT MLG MANUALLY. REMOVED AND REPLACED UPLOCK ACTUATOR AND TRANSFER CYLINDER PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,138 hrs · 51,496 cycles

DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,138 hrs · 51,496 cycles

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

Part: SKIN — CRACKED (BS 867 S24R) · airframe 67,429 hrs · 50,962 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 867 + 17, STR 24R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 984 S24R) · airframe 67,486 hrs · 50,998 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 984, STR 24R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 500D S12L) · airframe 67,429 hrs · 50,962 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D + 17, STR 12L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 517D S12L) · airframe 67,486 hrs · 50,998 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 517D, STR 12L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,794 hrs · 50,471 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 731, STR 23R. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 65,853 hrs · 49,721 cycles

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

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 65,787 hrs · 49,670 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,758 hrs · 49,647 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 870, STR 25R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,758 hrs · 49,647 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 890, STR 25R. REPAIRED SKIN PER SWA EA.

Part: BATTERY PACK — FAULTY (CABIN) · airframe 65,222 hrs · 49,221 cycles

DURING SCHEDULED BRDG CHECK, FOUND EMERGENCY EXIT LIGHT BATTERY PACK M9137 FAULTY. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAULTY (CABIN) · airframe 65,222 hrs · 49,221 cycles

DURING SCHEDULED BRDG CHECK, FOUND EMERGENCY EXIT LIGHT BATTERY PACK M9132 FAULTY. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LENS — BROKEN (CABIN) · airframe 65,220 hrs · 49,219 cycles

DURING SCHEDULED BRDG CHECK, FOUND AFT CABIN EMERGENCY EXIT SIGN LENS BROKEN. REMOVED AND REPLACED SIGN LENS PER MM.

Part: GLOWSTRIP — WORN (CABIN) · airframe 65,220 hrs · 45,219 cycles

DURING SCHEDULED BRDG CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 16 DEF. REMOVED AND REPLACED EEPLS STRIP PER MM.

Part: GLOWSTRIP — WORN (CABIN) · airframe 65,220 hrs · 45,219 cycles

DURING SCHEDULED BRDG CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 13 ABC. REMOVED AND REPLACED EEPLS STRIP PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,220 hrs · 49,219 cycles

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

Part: FITTING — CORRODED (R1 DOOR) · airframe 65,220 hrs · 49,219 cycles

DURING SCHEDULED BRDG CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITTING PER SRM.

Part: SKIN — CRACKED (BS 754 S19L) · airframe 64,762 hrs · 48,883 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 754, STR 19L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,426 hrs · 48,621 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 540, STR 17L. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 63,736 hrs · 48,093 cycles

DURING SCHEDULED C1 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SKIN — CRACKED (BS 308 S18R) · airframe 63,736 hrs · 48,093 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 308, STR 18R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 774 S21L) · airframe 63,736 hrs · 48,093 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 774, STR 21L. REPAIRED SKIN PER SWA EA.

Part: SIGN — BROKEN (EMERGENCY EXIT) · airframe 63,482 hrs · 47,901 cycles

LT OVERWING EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED EMERGENCY EXIT SIGN PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,121 hrs · 47,626 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 508, STR 16L. REPAIRED SKIN PER SRM.

Part: BELTFRAME — CORRODED (FUSELAGE) · airframe 62,857 hrs · 47,432 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE BELT FRAME CORRODED AT BS 747, STR 26R. REPAIRED FRAME PER SRM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 62,857 hrs · 47,432 cycles

DURING SCHEDULED C4 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 61,839 hrs · 46,634 cycles

DURING SCHEDULED C3 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SKIN — CRACKED (BS 729D-740D) · airframe 61,750 hrs · 46,552 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 729D TO BS 740D, STR 19R. REPAIRED SKIN PER SWA EA & SRM.

Part: LIGHT — INOPERATIVE (LT WING) · airframe 60,760 hrs · 45,816 cycles

DURING SCHEDULED A1 CHECK, FOUND EXTERNAL EMERGENCY EXIT LIGHT INOP AFT OF LT WING. RELAMPED LIGHT ASSY PER MM.

Part: SKIN — CRACKED (BS 884) · airframe 60,760 hrs · 45,816 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 884, STR 25R. REPAIRED SKIN PER SRM.

Part: TIRE — SEPARATED (LT MLG) · airframe 59,987 hrs · 45,207 cycles

AIR TURNBACK, NR 2 MAIN TIRE TREAD SEPARATED AND LOST A SYSTEM HYDRAULICS DURING MAIN GEAR RETRACTION. FOUND LT INBD GROUND SPOILER, LT AILERON BUS CABLE , 4 HYDRAULIC LINES AND LT INBD T/E AFT FLAP DAMAGED. REMOVED AND REPLACED MAIN TIRE ASSY, LT INBD T/E AFT FLAP, HYDRAULIC LINES AND LT INBD GROUND SPOILER PER MM.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 59,817 hrs · 45,058 cycles

DURING SCHEDULED SERVICE CHECK, FOUND AFT GALLEY LOWER EMERGENCY EXIT LIGHT INOP. REPAIRED WIRES TO LIGHT PER WDM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,985 hrs · 44,395 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR UPPER AFT CUTOUT. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,985 hrs · 44,395 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (L2 DOOR) · airframe 58,976 hrs · 44,388 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR UPPER AFT CUTOUT. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (R2 DOOR) · airframe 58,976 hrs · 44,388 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: SEAL — BLOWN (ACTUATOR) · airframe 58,538 hrs · 44,055 cycles

DIVERSION, DECLARED EMERGENCY. A-SYSTEM ENGINE LOW PRESSURE LIGHT ILLUMINATED, FOLLOWED BY A-SYSTEM HYDRAULIC FLUID LOSS. REMOVED AND REPLACED RT WING INBOARD FLIGHT SPOILER ACTUATOR O-RING PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,442 hrs · 43,972 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN AT BS 727E + 10, STRINGER 19R, CRACKED. REPAIRED SKIN PER SRM.

Part: SENSOR — FAULTY (LT MLG) · airframe 58,149 hrs · 43,755 cycles

LT MLG UNSAFE LIGHT ILLUMINATED IN FLIGHT. CYCLED GEAR HANDLE, NO HELP. REMOVED AND REPLACED LT MLG UPLOCK SENSOR PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 29,961 hrs · 25,559 cycles

DURING SCHEDULED D CHECK, FOUND BULKHEAD DOME CAP AT BS 1016, STRINGER 15L, CRACKED. REPAIRED SKIN PER ER.

Part: SPLICE — CORRODED (STRINGER) · airframe 57,207 hrs · 42,987 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER SPLICE AT BS 360, STRINGER 26L, CORRODED. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 57,207 hrs · 42,987 cycles

DURING SCHEDULED D CHECK, FOUND AFT PRESSURE BULKHEAD DOME CAP LAP SPLICE AT BS 1016, STRINGER 23R, CRACKED. REPAIRED BULKHEAD PER ER.

Part: FRAME — CORRODED (FUSELAGE) · airframe 57,207 hrs · 42,987 cycles

DURING SCHEDULED D CHECK, FOUND FRAME AT BS 360, BETWEEN STRINGER 27L AND STRINGER 27R, CORRODED. REPAIRED FRAME SECTION PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 57,207 hrs · 42,987 cycles

DURING SCHEDULED D CHECK, FOUND FLOORBEAM UPPER CHORD AT BS 259.5, LBL 11 TO RBL 11, CORRODED. REMOVED AND REPLACED FLOORBEAM CHORD SECTION PER SRM.

Part: FLOORBEAM — CORRODED (BS 1016) · airframe 57,207 hrs · 42,987 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS BS 1016, LBL 9 TO LBL 17, CORRODED. REPAIRED FLOORBEAM PER ER.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 57,207 hrs · 42,987 cycles

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

Part: FITTING — CORRODED (LT & RT WING) · airframe 57,207 hrs · 42,987 cycles

DURING SCHEDULED D-CHECK, FOUND BOTH RT AND LT MLG SUPPORT BEAM AFT STABILIZER FITTINGS CORRODED. REMOVED AND REPLACED FITTINGS PER MM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 57,207 hrs · 42,987 cycles

DURING SCHEDULED D-CHECK, FOUND AFT CARGO COMPARTMENT FRAME AT BS 847, RBL 30, CORRODED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 57,207 hrs · 42,987 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER 25R AT BS 370, CORRODED. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,207 hrs · 42,987 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 887, STRINGER 8L, CRACKED. REPAIRED FRAME PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 57,207 hrs · 42,987 cycles

DURING SCHEDULED D-CHECK, FOUND 2 EACH CRACKS AT BS 188 TO BS 196, STRINGER 17L AND BS 188 TO BS 196, STRINGER 17R. REMOVED AND REPLACED FLOORBEAM WEB SECTIONS PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 57,207 hrs · 42,987 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 380, LBL 6 TO RBL 6, CORRODED. REPAIRED FRAME SECTION PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 57,207 hrs · 42,987 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN AT BS 351 TO BS 361 STRINGER 28R, CORRODED. REPAIRED SKIN PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,207 hrs · 42,987 cycles

DURING SCHEDULED D-CHECK, FOUND 2 FRAMES AT BS 188, LBL 32 AND BS 188, RBL 32, CRACKED. REMOVED AND REPLACED FRAME SECTIONS PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 57,207 hrs · 42,987 cycles

DURING SCHEDULED D-CHECK, FOUND AFT CARGO DOOR FRAME CUTOUT FWD FRAME AFT FACE AT BS 794.3, RBL 25, WL 156, CORRODED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 57,207 hrs · 42,987 cycles

DURING SCHEDULED D-CHECK, FOUND 2 EACH BEAR STRAPS AT FWD ENTRY DOOR UPPER AND LOWER HINGE CUTOUTS, CRACKED. REPAIRED SKIN SECTIONS PER ER.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 57,207 hrs · 42,987 cycles

DURING SCHEDULED D-CHECK, FOUND BULKHEAD DOME CAP AT BS 1016, STRINGER 9L, CRACKED. REPAIRED BULKHEAD DOME CAP PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 57,207 hrs · 42,987 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM WEB AT BS 1010, LBL 39, CORRODED. REMOVED AND REPLACED FLOORBEAM WEB PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 57,207 hrs · 42,987 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM WEB AT BS 328, RBL 45, CORRODED. REPAIRED FLOORBEAM WEB PER ER.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 57,207 hrs · 42,987 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER AT BS 325, STRINGER 28R, CORRODED. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,207 hrs · 42,987 cycles

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

Part: SKIN — CRACKED (NR 2 K FLAP) · airframe 57,207 hrs · 42,987 cycles

DURING SCHEDULED D-CHECK, FOUND LT WING NR 2 L/E KRUEGER FLAP CRACKED. REMOVED AND REPLACED LT WING NR 2 L/E KRUEGER FLAP PER MM.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 57,207 hrs · 42,987 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE AT BS 360, STRINGER 26R, CORRODED. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 57,207 hrs · 42,987 cycles

DURING SCHEDULED D-CHECK, FOUND FWD SERVICE DOOR CUTOUT UPPER STUB FRAME FWD RADIUS, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 57,207 hrs · 42,987 cycles

DURING SCHEDULED D-CHECK, FOUND ZEE CHORD AT BS 270, RBL 11 TO LBL 11, CORRODED. REMOVED AND REPLACED CHORD PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 57,207 hrs · 42,987 cycles

DURING SCHEDULED D-CHECK, FOUND FWD CARGO DOOR CUTOUT AFT FRAME NR 5 STOP UPPER FLANGE, CRACKED. REMOVED AND REPLACED AFT FRAME SECTION PER ER.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 57,207 hrs · 42,987 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER 26L, AT BS 360, CORRODED. REPAIRED STRINGER PER SRM.

Part: FRAME — CRACKED (BS 847) · airframe 57,207 hrs · 42,987 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 847, STRINGER 8R CRACKED. REPAIRED FRAME SECTION PER SRM.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 57,207 hrs · 42,987 cycles

DURING SCHEDULED D-CHECK, FOUND AFT CARGO DOOR CUTOUT AFT FRAME FWD FACE, CORRODED. REMOVED AND REPLACED CARGO DOOR FRAME CUTOUT PER SRM.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 57,207 hrs · 42,987 cycles

DURING SCHEDULED D-CHECK, FOUND E&E COMPARTMENT STRINGER SPLICE AT BS 360, STRINGER 28L, CORRODED. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,207 hrs · 42,987 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP AT BS 277, STRINGER 15R, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 57,207 hrs · 42,987 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER 26L, AT BS 360, CORRODED. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: SKIN — CRACKED (RT HORZ STAB) · airframe 57,207 hrs · 42,987 cycles

DURING SCHEDULED D-CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN AT STATION 79, REAR SPAR, CRACKED. REPAIRED SKIN PER ER.

Part: FITTING — CORRODED (GIRT BAR) · airframe 5,727 hrs · 42,987 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,207 hrs · 42,987 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 480, STRINGER 8L, CRACKED. REPAIRED FRAME SECTION PER SRM.

Part: SPAR — CRACKED (RT WING) · airframe 57,207 hrs · 42,987 cycles

DURING SCHEDULED D-CHECK, FOUND RT WING UPPER REAR SPAR CHORD AT RSS 285, CRACKED. REMOVED AND REPLACED CHORD PER BAC DRAWING, ER, SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 57,207 hrs · 42,987 cycles

DURING SCHEDULED D CHECK, FOUND FLOORBEAM CHORD AT BS 294.5, LBL 12, CORRODED. REMOVED AND REPLACED FLOORBEAM CHORD SECTION PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 57,207 hrs · 42,987 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CHORD AT 328, LBL 12, CORRODED. REMOVED AND REPLACED FLOORBEAM CHORD SECTION PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 57,207 hrs · 42,987 cycles

DURING SCHEDULED D CHECK, FOUND FLOORBEAM CHORD AT BS 312, RBL 20 TO LBL 20, CORRODED. REMOVED AND REPLACED FLOORBEAM CHORD SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,207 hrs · 42,987 cycles

DURING SCHEDULED D CHECK, FOUND FRAME CHORD AT BS 616, LBL 65, WL 200, CRACKED. REMOVED AND REPLACED FRAME CHORD SECTION PER SB.

Part: FRAME — CORRODED (FUSELAGE) · airframe 57,207 hrs · 42,987 cycles

DURING SCHEDULED D CHECK, FOUND FRAME AT BS 994, RBL 44, CORRODED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (BS 767) · airframe 57,207 hrs · 42,987 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 767, STRINGER 8L & STRINGER 8R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (BS 440) · airframe 57,207 hrs · 42,987 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 440, STRINGER 8L & STRINGER 8R CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (BS 807) · airframe 57,207 hrs · 42,987 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 807, STRINGER 8L, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,207 hrs · 42,987 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,207 hrs · 42,987 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME AT BS 480, STRINGER 8R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,207 hrs · 42,987 cycles

DURING SCHEDULED D CHECK, FOUND FRAME AT BS 907, STRINGER 8R, CRACKED. REPAIRED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,207 hrs · 42,987 cycles

DURING SCHEDULED D CHECK, FOUND FRAME AT BS 747, STRINGER 8R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,207 hrs · 42,987 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CLIP AT BS 685, STRINGER 2L, CRACKED. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 57,207 hrs · 42,987 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER SPLICES AT BS 907, STRINGER 4R AND STRINGER 4L, CRACKED. REMOVED AND REPLACED STRINGER SPLICES PER SRM.

Part: SKIN — DELAMINATED (RT WING FLAP) · airframe 57,103 hrs · 42,895 cycles

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

Part: SKIN — CORRODED (FUSELAGE) · airframe 57,072 hrs · 42,869 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT RIGHT KEEL BEAM BS 500C TO RT KEELBEAM BS 500D, CORRODED. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,072 hrs · 42,869 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 787, STRINGER 25L, BS 747, STRINGER 23R, CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — DELAMINATED (RT WING FLAP) · airframe 57,072 hrs · 42,869 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,063 hrs · 42,862 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 787, STRINGER 20L, CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,063 hrs · 42,862 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 787, STRINGER 20L, CRACKED. REPAIRED SKIN PER SRM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 56,449 hrs · 42,360 cycles

DURING SPV, FOUND EMERGENCY EXIT LIGHTS RT MID CABIN, INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 56,449 hrs · 42,360 cycles

DURING SPV, FOUND BULKHEAD PRESSURE WEB AT BS 1016, RBL 2 TO LBL 2, CORRODED. REPAIRED PRESSURE WEB PER ER.

Part: BATTERY — INOPERATIVE (R2 DOOR) · airframe 56,449 hrs · 42,360 cycles

DURING SPV, FOUND R2 DOOR EVAC SLIDE LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: BRACKET — BROKEN (R2 DOOR SLIDE) · airframe 56,262 hrs · 42,214 cycles

DURING SCHEDULED C1 CHECK, FOUND R2 DOOR EVAC SLIDE FWD ATTACH BRACKET BROKEN. REMOVED AND REPLACED R2 DOOR EVAC SLIDE BRACKET PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 56,197 hrs · 42,160 cycles

DURING SCHEDULED RON, FOUND LT CENTER AFT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 56,030 hrs · 42,027 cycles

L1 DOOR EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED L1 DOOR EVAC SLIDE PER MM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 55,858 hrs · 41,893 cycles

L1 DOOR EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED THE L1 DOOR EVAC SLIDE INTO CONTAINER PER MM.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 55,791 hrs · 41,832 cycles

L1 DOOR EVAC SLIDE LOOSE. SECURED L1 DOOR EVAC SLIDE PER MM.

Part: MODULE — FAULTY (COCKPIT) · airframe 55,643 hrs · 41,710 cycles

AIRTURN BACK, POWER STANDBY LIGHT ILLUMNINATED IN FLIGHT. QRH PROCEDURES FOLLOWED. LIGHT WOULD NOT RESET. REMOVED AND REPLACED STANDBY POWER MODULE PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 55,468 hrs · 41,565 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,393 hrs · 41,510 cycles

DURING SCHEDULED C4 CHECK, FOUND R2 DOOR UPPER HINGE BOX FRAME ASSY BROKEN. REPAIRED UPPER HINGE BOX FRAME ASSY PER SRM.

Part: FRAME — CRACKED (L1 DOOR) · airframe 55,393 hrs · 41,510 cycles

DURING SCHEDULED C4 CHECK, FOUND L1 DOOR LOWER FRAME WEB CRACKED AT FWD STOP FITTING. REMOVED AND REPLACED L1 DOOR ASSY PER MM.

Part: CONTROL PANEL — FAULTY (COCKPIT) · airframe 55,104 hrs · 41,289 cycles

DIVERSION, CABIN ALTITUDE WARNING HORN SOUNDED, BOTH A/C PACKS SET IN HIGH AND NO HELP, OUTFLOW VALVE INDICATED FULL CLOSED. REMOVED AND REPLACED CABIN PRESS CONTROL PANEL AND RESEALED L1 DOOR HINGE AREAS PER MM.

Part: OIL SYSTEM — CONTAMINATED (NR 1 ENGINE) · airframe 53,888 hrs · 40,316 cycles

IN FLIGHT SHUTDOWN, DECLARED EMERGENCY, NR 1 ENGINE OIL PRESS LIGHT ILLUMINATED, OIL QUANITY WAS AT ZERO. FOUND TORLON CHIPS IN LUB UNIT, CLEANED AND REINSTALLED PER MM.

Part: SLIDE — LOOSE (ENTRY DOOR) · airframe 53,854 hrs · 40,288 cycles

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

Part: SKIN — DELAMINATED (T/E FLAP) · airframe 53,499 hrs · 40,000 cycles

DURING SCHEDULED C2 CHECK, FOUND RT INBD AFT T/E FLAP DELAMINATED ON LOWER SURFACE. REMOVED AND REPLACED RT INBD AFT T/E FLAP PER MM

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,253 hrs · 39,795 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 873 & BS 876, STR 22R. REPAIRED SKIN PER SRM.

Part: ENGINE — FAILED (LH WING) · airframe 52,734 hrs · 39,360 cycles

( IN-FLT SHUTDOWN, DECLARED EMERGENCY )……………………..DURING CLIMB # 1 ENGINE SHUTDOWN, WOULD NOT RESTART. R&R # 1 ENGINE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,012 hrs · 38,784 cycles

DURING SCHEDULED CHECK, FOUND FUSELAGE SKIN CRACKED (5 EA) BETWEEN BS 727D AND BS 887, BETWEEN STR 22L AND STR 25L. REPAIRED SKIN PER SRM.

Part: LENS — CRACKED (FWD ENTRY DOOR) · airframe 51,138 hrs · 38,091 cycles

DURING SCHEDULED BC3 CHECK, FOUND FWD ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LENS PER MM.

Part: DOOR — CRACKED (AFT CARGO) · airframe 50,747 hrs · 37,759 cycles

DURING SCHEDULED C3 CHECK, FOUND AFT CARGO DOOR CRACKED AT FWD END BETWEEN 2ND AND 3RD STOPS. REMOVED AND REPLACED AFT CARGO DOOR PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 50,747 hrs · 37,759 cycles

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

Part: SLIDE — LOOSE (AFT SVC DOOR) · airframe 50,743 hrs · 37,755 cycles

DURING SCHEDULED BC3 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE NYLON CORD HANGING OUT OF GIRT AREA. STOWED NYLON CORD PER MM.

Part: WEB — CRACKED (FUSELAGE) · airframe 49,415 hrs · 36,689 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, WL 234 AND LBL 11.0. REPAIRED WEB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,415 hrs · 36,689 cycles

DURING SCHEDULED 1/4D CHECK, FOUND CAPTIAN'S WINDOW POST SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 49,414 hrs · 36,687 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BULKHEAD WEB CRACKED (2 EA) AT BS 178, WL 218, LBL 11.5 AND WL 212.5, RBL 7.0. REPAIRED WEB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,413 hrs · 36,687 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD LOWER CORNER OF AFT CARGO DOOR CUTOUT. REPAIRED SKIN PER SWA RA.

Part: DOOR — CRACKED (FWD ENTRY DOOR) · airframe 49,413 hrs · 36,687 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD ENTRY DOOR FRAME CRACKED AT AFT DOOR STOP CUTOUT NR 6 FROM TOP. REMOVED AND REPLACED DOOR PER MM.

Part: DOOR FRAME — CRACKED (FWD ENTRY DOOR) · airframe 49,413 hrs · 36,687 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD ENTRY DOOR FRAME CRACKED AT AFT DOOR STOP CUTOUT NR 7 FROM TOP. REPAIRED FRAME PER SRM.

Part: FLOORBEAM — CORRODED (AFT CARGO) · airframe 49,413 hrs · 36,687 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM CORRODED AT BS 727B, LBL 2 TO LBL 12. REPAIRED FLOORBEAM PER SWA RA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,413 hrs · 36,687 cycles

DURING SCHEDULED 1/4D CHECK, FOUND STRINGER TIE CLIPS CRACKED AT BS 400, STR 28L AND STR 28R. REMOVED AND REPLACED STR CLIPS PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 49,413 hrs · 36,687 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BULKHEAD WEB CRACKED (2 EA) AT BS 178, WL 234, LBL 12 AND WL 210, RBL 7.0. REPAIRED WEB PER SRM.

Part: COVER — MISSING (CABIN) · airframe 49,413 hrs · 36,687 cycles

DURING SCHEDULED 1/4D CHECK, FOUND EMERGENCY EXIT LIGHT COVER MISSING ON FWD LAV WALL OTBD OF F/A SEAT. INSTALLED COVER PER MM.

Part: FUSE — FAILED (NLG) · airframe 48,559 hrs · 35,990 cycles

AIR TURNBACK, LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. REMOVED AND REPLACED NOSE GEAR RETRACTION FUSE PER MM, ADJUSTED GROUND SPOILER INTERLOCK CABLE AND LANDING GEAR SAFETY SENSORS PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 47,636 hrs · 35,261 cycles

OVERHEAD EMERGENCY LIGHT BROKEN AT ROW 22 R&R LIGHT ASSY PER MM.

Part: RETAINER — OUT OF POSITION (SERVICE DOOR) · airframe 47,378 hrs · 35,037 cycles

AIR TURNBACK, AFTER TAKEOFF A/C CABIN WOULD NOT PRESSURIZE. F/A REPORTED NOISE FROM AFT SVC DOOR. REPOSITIONED AFT SVC DOOR PRESS SEAL RETAINER PER MM.

Part: FITTING — CRACKED (LH WING) · airframe 13,374 hrs · 11,362 cycles

DURING SCHEDULED C3 CHECK, FOUND LH MLG BEAM HANGER FITTING CRACKED AT FWD END. R&R FITTING PER ALM INV. # SWA 10410.

Part: LENS — BROKEN (CABIN) · airframe 45,295 hrs · 33,273 cycles

DURING SCHEDULED C1 CHECK, FOUND LT & RT OVERWING EMERGENCY EXIT LIGHT LENSES BROKEN. REMOVED AND REPLACED LENS ASSYS PER MM.

Part: LENS — BROKEN (LT & RT OVERWING) · airframe 45,295 hrs · 33,273 cycles

DURING SCHEDULED C1 CHECK, FOUND LT & RT OVERWING EMERGENCY EXIT LIGHT LENSES BROKEN. REMOVED AND REPLACED LENS ASSY''S PER MM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 45,000 hrs · 33,020 cycles

DURING SCHEDULED RON CHECK, FOUND BS 663 BULKHEAD MLG W/W STIFFNER CRACKED AT RBL 3. R&R STIFFNER PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 44,909 hrs · 32,944 cycles

FWD ENTRY DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: STRAP — LOOSE (ESCAPE SLIDE) · airframe 44,412 hrs · 32,516 cycles

DURING SCHEDULED C4 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT STRAP PLAYOUT EXCESSIVE. REINSTALLED SLIDE ASSY PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 44,291 hrs · 32,413 cycles

DURING SCHEDULED SV CHECK, FOUND BS 178 BULKHEAD WEBS CRACKED AT WL 207, RBL 27 AND WL 207, LBL 27. REMOVED AND REPLACED WEBS PER SRM.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 51,365 hrs · 24,858 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS FWD SECTION INOP. REMOVED AND REPLACED FWD BATTERY PACK AND CHARGER PER MM.

Part: BRACKET — LOOSE (GIRT BAR) · airframe 42,702 hrs · 31,065 cycles

DURING SCHEDULED BC2 CHECK, FOUND AFT SERVICE DOOR EVACUATION SLIDE GIRT BAR STOW BRACKETS LOOSE. SECURED BRACKETS PER MM.

Part: ANGLE — CRACKED (BS 360)

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE ANGLE CRACKED, BS 360, LBL 68, WL 230. REMOVED AND REPLACED ANGLE PER SRM.

Part: BEAM — CRACKED (BS 707-710)

DURING SCHEDULED 1/2D CHECK, FOUND CENTER SECTION LONGITUDINAL BEAM CRACKED ON UPPER SURFACE BS 707-710, RBL 24.5. REPAIRED BEAM PER SRM.

Part: FLOORBEAM — CORRODED (BS 328)

DURING SCHEDULED 1/2D CHECK, FOUND CORROSION BS 328 FLOORBEAM UPPER FACE LBL 28. REPAIRED BEAM PER SRM.

Part: WIRE — BROKEN (BS 975)

DURING SCHEDULED 1/2D CHECK, FOUND EEPLS HAS BROKEN WIRE AT BATTERY PACK, BS 975. REMOVED AND REPLACED WIRING SECTION PER MM.

Part: LENS — MISSING (ROW 15)

DURING SCHEDULED C4 CHECK, FOUND EEPLS LENS MISSING AT ROW 15. REPLACED LENS PER MM.

Part: LIGHT — BURNED (ROW 7 & 8)

AIR TURNBACK, 10 MINS AFTER TAKEOFF F/A REPORTED AN ELECTRICAL ODOR AT MID CABIN. FOUND SIDEWALL LIGHT AT ROW 7 ABC AND 8 ABC BURNED INTERNALLY. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SKIN — CRACKED (BS 727)

DURING SCHEDULED SERVICE CHECK, FOUND A 4 INCH LONG CRACK AT FUSELAGE SKIN, BS 727D, STRINGER 24R. REPAIRED SKIN PER SRM.

Part: ACM — FAILED (AC COMPT)

AT FL350, F/A'S REPORTED STRONG FUMES AFT OF ROW 17 IN MAIN CABIN. TURNED OFF RECIRC FAN AND RIGHT PACK AND CLOSED ISOLATION VALVE. RETURNED TO BWI. FUMES WEAKENED NOTICEABLY. DEFERRED RIGHT PACK MEL. REPLACED BOTH COALESCER BAGS. OPERATED LEFT PACK WITH ENGINES AND APU, NO ODOR NOTED. REMOVED AND REPLACED ACM AND AIR SEPARATOR, OP CHECK GOOD PER MM.

Part: BULB — FAILED (PAX DOOR)

DURING SCHEDULED SC CHECK, FOUND AFT ENTRY DOOR EMERGENCY LIGHT INOP. RELAMPED AND OP CHECKED PER BOEING M/M.

Part: BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED CHECK, FOUND OVERWING EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY PACK PER BOEING M/M.

Part: SKIN — CRACKED (FUSELAGE)

DURING SCHEDULED CHECK, FOUND FUSELAGE SKIN CRACK BELOW EMERGENCY ESCAPE LIGHT LT SIDE BEHIND AFT WING TO BODY FAIRING. REPAIRED PER BOEING SRM.

Part: LIGHT — LOOSE (ROW 18)

DURING SCHEDULED A1 CHECK, FOUND EMERGENCY TRACK LIGHT COVER LOOSE FROM ROW 18 THROUGH AFT. RESECURED TRACK LIGHT PER BOEING MM.

Part: BULB — FAILED (CABIN)

DURING SCHEDULED TRAN CHECK, FOUND FWD SERVICE DOOR EMERGENCY EXIT LIGHT OUT. REPLACED BULB AT FWD EXTERIOR SERVICE DOOR EMERGENCY EXIT LIGHT PER BOEING MM.

Part: SKIN — DENTED (CARGO DOOR)

DURING SCHEDULED TRAN CHECK, FOUND AFT CARGO DOOR SKIN DENTED. REPAIRED PER BOEING MM.

Part: DOUBLER — CRACKED (GALLEY DOORWAY)

DURING SCHEDULED TRAN CHECK, FOUND FWD GALLEY DOOR LWR AFT INNER DOUBLER CRACKED IN AFT FRAME LOWER CORNER. REMOVED AND REPLACED PER BOEING SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED TRAN CHECK, FOUND CRACKED BS 178 BULKHEAD WL 188 RBL 5. REPAIRED PER BOEING SRM.

Part: SKIN — GOUGED (WINGS)

DURING SCHEDULED TRAN CHECK, FOUND L/E GAUGED AT NR 4 SLAT TAI CUTOUT. REPAIRED INTERNAL AND EXTERNAL SURFACES PER BOEING SRM.

Part: SKIN — CRACKED (BS 1032)

DURING SCHEDULED TRAN CHECK, FOUND EXTERNAL FUSELAGE SKIN GOUGED AT BS 1032 STR 9L. REMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — DELAMINATED (HORIZ STAB)

DURING SCHEDULED TRAN CHECK, FOUND DELAMINATED RT HORIZ STAB UPPER SURFACE O/B T/E PANEL. REMOVED AND REPLACED PER BOEING SRM.

Part: SHEAR TIE — CRACKED (BS 1006)

DURING SCHEDULED TRAN CHECK, FOUND CRACKED SHEAR TIE AT BS 1006 LBL 6 TO LBL 8 AFT BAY BETWEEN STR 27 RT AND 27 LT. REMOVED AND REPLACED PER BOEING SRM.

Part: FRAME — DAMAGED (BS 1006)

DURING SCHEDULED TRAN CHECK, FOUND DAMAGE AT FASTENER HOLES ON BS 1006 FRAME BL 0 BETWEEN STR 27L TO 27R. REMOVED AND REPLACED PER BOEING SRM.

Part: CLIP — DAMAGED (FUSELAGE)

DURING SCHEDULED TRAN CHECK, FOUND FRAME WITH 2 CLIPS ELONGATED HOLES LBL 20 AND 26. REMOVED AND REPLACED PER BOEING SRM.

Part: CHANNEL — DAMAGED (BS 986.5)

DURING SCHEDULED TRAN CHECK, FOUND HAT CHANNEL AT BS 986.5, WL 208 WITH ELONGATED HOLES LBL 22 TO 36. REPAIRED PER BOEING SRM.

Part: SKIN — GOUGED (BS 457)

DURING SCHEDULED TRAN CHECK, FOUND GOUGED SKIN AT BS 457, 2 ABOVE STR 27 RT. REPAIRED PER BOEING SRM.

Part: ANGLE — CRACKED (E/E COMPT)

DURING SCHEDULED TRAN CHECK, FOUND CRACKED E1-1 RACK, LEFT HAND SUPPORT ANGLE. REPAIRED PER BOEING SRM.

Part: WEB — DAMAGED (BS 1006-1016)

DURING SCHEDULED TRAN CHECK, FOUND BS 1006 TO 1016, LBL 28, WL 208 AND BS 1006 TO 1016, LBL 18, WL 208 WITH ELONGATED HOLES ON SHEAR WEB. REMOVED AND REPLACED PER BOEING SRM.

Part: FLOORBEAM — DAMAGED (BS 1006)

DURING SCHEDULED TRAN CHECK, FOUND FLOORBEAM AT BS 1006, LBL 16 AND 29 WITH ELONGATED HOLES. REPAIRED PER BOEING SRM.

Part: INTERCOSTAL — DAMAGED (PAX DOORWAY)

DURING SCHEDULED TRAN CHECK, FOUND DAMAGED INTERCOSTAL ON BOTTOM END OF FWD ENTRY DOOR ON FWD SIDE OF FWD ENTRY DOOR. REMOVED AND REPLACED PER BOEING SRM.

Part: ANGLE — CRACKED (RT HORIZ STAB)

DURING SCHEDULED TRAN CHECK, FOUND CRACKED AND GOUGED L-ANGLE BEHIND PANEL 9224 ON RT HORIZ STAB. REMOVED AND REPLACED PER BOEING SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED TRAN CHECK, FOUND CRACKED INDICATION NOTED DURING UT, BS 178 BULKHEAD, WL 198.3 TO 202.5, RBL 4.7 AND BS 178, WL 198.0 TO WL 202.5, LBL 4.7. REPAIRED PER BOEING SRM.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND AFT SERVICE AND ENTRY DOOR EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACKS PER BOEING MM.