N604SW

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 68,369 hrs · 54,271 cycles

R2 DOOR SLIDE OUT OF POSITION. REPOSITIONED THE SLIDE IAW MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 68,369 hrs · 54,271 cycles

R2 DOOR SLIDE OUT OF POSITION. REPOSITIONED THE SLIDE IAW MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 68,128 hrs · 54,120 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITON. REPOSITIONED SLIDE PER AMM.

Part: BULKHEAD — CRACKED (LT MLG WW) · airframe 67,705 hrs · 53,825 cycles

LEFT MAIN GEAR WHEEL WELL FORWARD BULKHEAD CRACKED AT BS 663, LBL 37. REPAIRED THE BULKHEAD IAW EA.

Part: BRACKET — LOOSE (L2 DOOR SLIDE) · airframe 67,705 hrs · 53,825 cycles

L2 DOOR EMERGENCY SLIDE FORWARD ATTACHMENT BRACKET LOOSE. SECURED THE BRACKET IAW SRM.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 67,705 hrs · 53,825 cycles

LT WEB CRACKED AT BS 663. REPAIRED WEB PER EA.

Part: WEB — CORRODED (FUSELAGE) · airframe 67,619 hrs · 53,762 cycles

AFT CARGO BAY BILGE VERTICAL WEB CORRODED BETWEEN BS 787 TO BS 794, RBL 21. R & R WEB IAW SRM & DWG.

Part: WEB — CORRODED (BS 767-787) · airframe 67,619 hrs · 53,762 cycles

AFT CARGO BAY BILGE VERTICAL WEB CORRODED BETWEEN BS 767 - 787, RBL 21. R & R THE WEB IAW SRM & DWG.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 67,619 hrs · 53,762 cycles

AFT CARGO FLOOR STR TO FRAME SUPPORT BRACKET CRACKED AT BS 927, STR 25R. R & R BRACKET IAW SRM.

Part: WEB — CORRODED (CARGO DOOR FRAME) · airframe 67,619 hrs · 53,762 cycles

AFT CARGO DOOR CUTOUT THRESHOLD WEB CORRODED. R & R THRESHOLD WEB IAW SRM & DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 67,619 hrs · 53,762 cycles

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

Part: GIRT BAR — CRACKED (R1 DOOR) · airframe 67,619 hrs · 53,762 cycles

R1 DOOR SLIDE FORWARD GIRT BAR HOOK SHROUD CRACKED. REPAIRED GIRT BAR ASSEMBLY IAW EA.

Part: FRAME — CORRODED (BS 727E) · airframe 67,619 hrs · 53,762 cycles

FRAME CORRODED AT BS 727E, BETWEEN STRINGERS 27L TO 27R. R & R FRAME IAW SRM.

Part: FRAME — CORRODED (BS 807) · airframe 67,619 hrs · 53,762 cycles

FRAME CORRODED AT BS 807, BETWEEN STRINGERS 27L - 27R. R & R THE FRAME IAW SRM AND DWG.

Part: FRAME — CORRODED (BS 767) · airframe 67,619 hrs · 53,762 cycles

FRAME CORRODED AT BS 767, BETWEEN STRINGER 27L - 27R. R & R THE FRAME IAW SRM AND DWG.

Part: SHEAR TIE — CORRODED (BS 867) · airframe 67,619 hrs · 53,762 cycles

SHEAR TIE CORRODED AT BS 867, BETWEEN STRINGERS 27L TO 27R. R & R THE SHEAR TIE IAW SRM.

Part: FRAME — CORRODED (BS 787) · airframe 67,619 hrs · 53,762 cycles

FRAME CORRODED AT BS 787, BETWEEN STRINGERS 27L - 27R. R & R THE FRAME IAW SRM & DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 67,619 hrs · 53,762 cycles

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

Part: INTERCOSTAL — CRACKED (BS 279) · airframe 67,619 hrs · 53,762 cycles

INTERCOSTAL WEB INNER RADIUS TRIM OUT CRACKED AT BS 279, STRINGER 14R. R & R THE INTERCOSTAL IAW ER AND EA.

Part: INTERCOSTAL — CRACKED (BS 277-291) · airframe 67,619 hrs · 53,762 cycles

INTERCOSTAL CRACKED BETWEEN BS 277 - 291.5, BETWEEN STRINGERS 11 - 12R. R & R THE INTERCOSTAL IAW ER AND EA.

Part: INTERCOSTAL — CRACKED (BS 277-291) · airframe 67,619 hrs · 53,762 cycles

INTERCOSTAL CRACKED BETWEEN BS 277 TO 291.5, STRINGER 14R. R & R INTERCOSTAL IAW ER AND EA.

Part: INTERCOSTAL — CRACKED (BS 277-291) · airframe 67,619 hrs · 53,762 cycles

INTERCOSTAL CRACKED BETWEEN BS 277 TO 291.5, BETWEEN STRINGERS 9 - 10R. R & R THE INTERCOSTAL IAW EA.

Part: INTERCOSTAL — CRACKED (BS 277-291) · airframe 67,619 hrs · 53,762 cycles

INTERCOSTAL CRACKED BETWEEN BS 277 - 291.5, BETWEEN STRINGERS 12 - 13R. R & R THE INTERCOSTAL IAW ER AND EA.

Part: ROD END — CORRODED (LT ELEVATOR TAB) · airframe 66,858 hrs · 53,237 cycles

LEFT ELEVATOR TAB BOTH CONTROL RODS AFT ROD ENDS CORRODED. R & R CONTROL RODS IAW EA.

Part: ROD END — CORRODED (RT ELEVATOR TAB) · airframe 66,858 hrs · 53,237 cycles

RIGHT ELEVATOR TAB BOTH CONTROL RODS ENDS CORRODED FWD & AFT. R & R CONTROL RODS IAW EA.

Part: FAIRING — CORRODED (RT WING) · airframe 66,858 hrs · 53,237 cycles

RIGHT WING NR 5 FAIRING FWD ATTACH BEARING CORRODED. R & R FAIRING IAW MT.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 66,839 hrs · 53,224 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 65,966 hrs · 52,661 cycles

CENTER CABIN OVERHEAD BINS EMER LIGHT INOPERATIVE. R & R BULB IAW AMM.

Part: FAIRING — DELAMINATED (TE FLAP) · airframe 64,725 hrs · 51,844 cycles

LEFT WING NR 3 FLAP FAIRING DELAMINATED INBD AFT SIDE. REPAIRED NR 3 FLAP FAIRING IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 64,717 hrs · 51,836 cycles

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

Part: SHEAR WEB — CRACKED (FUSELAGE) · airframe 64,717 hrs · 51,836 cycles

SHEAR WEB CRACKED AT BS 440, BETWEEN STRINGER 26R - 27R. R & R SHEAR WEB IAW SRM & DWG.

Part: SKIN — CRACKED (LT WING) · airframe 64,717 hrs · 51,836 cycles

LEFT WING SKIN CRACKED AT UPPER SKIN. REPAIRED SKIN IAW EA.

Part: FITTING — CRACKED (LT WING) · airframe 64,717 hrs · 51,836 cycles

LEFT WING AFT SPAR, CRACKED IN FWD LG FITTING, COMMON TO UPPER SPAR CHORD. REPAIRED FITTING IAW EA.

Part: FITTING — CRACKED (LT WING) · airframe 64,717 hrs · 51,836 cycles

LEFT WING REAR SPAR, FWD LG BEAM FITTING CRACKED. REPAIRED FITTING IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 64,717 hrs · 51,836 cycles

LEFT WING TE UPPER SKIN AT REAR SPAR, FOUND CRACKED INDICATION IN FASTENER HOLE AFT FASTENER ROW AT WS 236. REMOVED SKIN IAW SRM & EA.

Part: SKIN — CRACKED (LT WING) · airframe 64,717 hrs · 51,836 cycles

LEFT WING TE UPPER SKIN AT REAR SPAR, CRACKED IN FASTENER HOLE AFT FASTENER ROW AT WS 255. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 64,717 hrs · 51,836 cycles

LEFT WING TE UPPER SKIN AT REAR SPAR, FOUND CRACKED IN FASTENER HOLE AFT FASTENER ROW AT WS 239. REPAIRED SKIN IAW SRM & EA.

Part: SKIN — CRACKED (LT WING) · airframe 64,717 hrs · 51,836 cycles

LEFT WING TE UPPER SKIN AT REAR SPAR FOUND CRACKED IN FASTENER HOLE, AFT FASTENER ROW WS 231. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 64,717 hrs · 51,836 cycles

LEFT WING TE EDGE UPPER SKIN AT REAR SPAR, CRACKED IN FASTENER HOLE AFT FASTENER ROW AT WS 259. REPAIRED SKIN IAW SRM & EA.

Part: SKIN — CRACKED (LT WING) · airframe 64,717 hrs · 51,836 cycles

LEFT WING TE UPPER SKIN AT REAR SPAR, FOUND CRACKED IN FASTENER HOLE AFT FASTENER ROW AT WS 254. REPAIRED SKIN IAW SRM & EA.

Part: SKIN — CRACKED (LT WING) · airframe 64,717 hrs · 51,836 cycles

LEFT WING TE UPPER SKIN CRACKED AT REAR SPAR AT WS 231. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 64,717 hrs · 51,836 cycles

LEFT WING TE UPPER SKIN AT REAR SPAR FOUND CRACKED IN FASTENER HOLE AFT FASTENER ROW AT WS 267. REPAIRED SKIN IAW SRM & EA.

Part: SPAR — CRACKED (LT WING) · airframe 64,717 hrs · 51,836 cycles

LEFT WING REAR SPAR, WEB CRACKED AT RSS 221. REPAIRED WEB IAW EA.

Part: FITTING — CRACKED (RT WING) · airframe 64,717 hrs · 51,836 cycles

RIGHT WING AFT SPAR, AFT GEAR BEAM FITTING CRACKED. REPAIRED FITTING IAW EA & DWG.

Part: SPAR — CRACKED (RT WING) · airframe 64,717 hrs · 51,836 cycles

RIGHT WING REAR SPAR, CRACKED IN SPAR UPPER CHORD, IN TOP CHORD ATTACH FASTENER HOLE AT RSS 221. REPAIRED CHORD IAW EA.

Part: SPAR — CRACKED (RT WING) · airframe 64,717 hrs · 51,836 cycles

RIGHT WING REAR SPAR, CRACKED IN SPAR WEB IN TOP CHORD ATTACH FASTENER HOLE AT RSS 221. REPAIRED WEB IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 64,717 hrs · 51,836 cycles

LEFT WING REAR SPAR UPPER CHORD, CRACKED AT RSS 221. REPAIRED CHORD IAW EA.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 64,717 hrs · 51,836 cycles

C1 DOOR CUT OUT FWD SIDE, FRAME CRACKED IN FRAME WEB AT NR 5 DOOR STOP FITTING AT LOWER OTBD CORNER OF AREA. R & R FRAME IAW ACO, SRM & DWG.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 64,717 hrs · 51,836 cycles

L1 DOOR CUTOUT, LOWER AFT CORNER, DOOR TRIM TO SKIN ATTACH ANGLE CRACKED. REPAIRED ANGLE IAW DWG.

Part: CASTING — CRACKED (RT SPOILER) · airframe 64,285 hrs · 51,522 cycles

RIGHT INBD GND SPOILER CRACKED AT ACTUATOR CASTING. R & R CASTING IAW SRM.

Part: COVER — LOOSE (EXIT SIGN) · airframe 63,471 hrs · 50,940 cycles

L1 DOOR EXIT SIGN COVER LOOSE. SECURED COVER IAW EA.

Part: DUCT — DELAMINATED (AC BAY) · airframe 62,732 hrs · 50,436 cycles

SMELL AROUND ROW 10. TURNED OFF GASPER FAN & SMELL WENT AWAY. FOUND A/C MIX CHAMBER DUCTS ASSEMBLY DELAMINATED & BLOWN OUT. R & R SAME IAW MM.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 62,269 hrs · 50,136 cycles

BENEATH WING TO BODY PANEL 3479R, SUB STRUCTURAL BRACKET CRACKED AT APPROX BS 540. R & R DOUBLER IAW DWG.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 62,269 hrs · 50,136 cycles

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

Part: SKIN — DELAMINATED (TE FLAP) · airframe 62,269 hrs · 50,136 cycles

RIGHT WING INBD FORE FLAP UPPER SKIN DELAMINATED. REPAIRED FORE FLAP IAW SRM.

Part: WIRE — BROKEN (CABIN) · airframe 62,269 hrs · 50,136 cycles

G4 GALLEY EXIT LIGHT WIRE BROKEN. REPAIRED LIGHT IAW MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,269 hrs · 50,136 cycles

FRAME OTBD CHORD CRACKED AT BS 727 STRINGER 18A LT SIDE BETWEEN 11 O'CLOCK & 5 O'CLOCK POSITION. REPAIRED CHORD IAW ACO & SRM.

Part: WIRE — BROKEN (CABIN) · airframe 62,269 hrs · 50,136 cycles

EXIT LIGHT AT AFT LAVATORY WIRE BROKEN. REPAIRED WIRE IAW WDM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,269 hrs · 50,136 cycles

FRAME OTBD CHORD CRACKED AT BS 727 STRINGER 18A RT SIDE AT 8 O'CLOCK POSITION. REPAIRED CHORD IAW ACO & SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,269 hrs · 50,136 cycles

FRAME OTBD CHORD CRACKED AT BS 727 STRINGER 18A LT SIDE AT 11 O'CLOCK POSITION. REPAIRED CHORD IAW ACO & SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,269 hrs · 50,136 cycles

FRAME OTBD CHORD CRACKED AT BS 727 STRINGER 18A RT SIDE AT 8 O'CLOCK POSITION. REPAIRED CHORD IAW ACO & SRM.

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 62,269 hrs · 50,136 cycles

RIGHT WING INBD TE VERTICAL ATTACH ANGLE CRACKED JUST OTBD OF NR 6 FLAP TRACK FAIRING. R & R ANGLE IAW DWG.

Part: TIP CAP — CRACKED (LT HORIZ STAB) · airframe 62,269 hrs · 50,136 cycles

LEFT HORIZONTAL STABILIZER OTBD TIP CRACKED. REPAIRED TIP IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,269 hrs · 50,136 cycles

SKIN CRACKED AT BS 727 STRINGER 1L. REPAIRED SKIN IAW EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 62,269 hrs · 50,136 cycles

STRINGER CRACKED AT BS 727 STRINGER 1L. REPAIRED STRINGER IAW EA.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 62,269 hrs · 50,136 cycles

SEAT TRACK CORRODED AT BS 996 RBL 18. R & R SEAT TRACK IAW SRM.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 62,269 hrs · 50,136 cycles

LOWER RT WING TO BODY FAIRING ATTACH TEE CHORD CRACKED AT BS 727. R & R CHORD IAW DWG.

Part: LIGHT — BROKEN (CABIN) · airframe 62,269 hrs · 50,136 cycles

FORWARD CABIN EEPLS BROKEN. R & R EEPLS IAW MM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 62,269 hrs · 50,136 cycles

LEFT CREASE BEAM WEB CORRODED BETWEEN BS 460 TO 480. R & R WEB IAW SRM & DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 62,269 hrs · 50,136 cycles

RIGHT MAIN CABIN CREASE BEAM WEB CORRODED BETWEEN BS 727D TO 727E. R & R WEB IAW SRM & DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 62,269 hrs · 50,136 cycles

LEFT CREASE BEAM WEB CORRODED BETWEEN BS 847 TO 867. REPAIRED WEB IAW SRM & DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 62,269 hrs · 50,136 cycles

STRINGER CLIP CRACKED AT BS 908 STRINGER 8L. R & R CLIP IAW DWG & SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 62,269 hrs · 50,136 cycles

STRINGER CLIP CRACKED AT BS 908 STRINGER 8R. R & R CLIP IAW DWG & SRM.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 62,269 hrs · 50,136 cycles

MAIN WW PRESS DECK WEB CRACKED AT BS 673 RBL 43. REPAIRED WEB IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 62,269 hrs · 50,136 cycles

FLOORBEAM INTERSECTION ANGLE CRACKED AT BS 727B RBL 45.5. R & R ANGLE IAW SRM & DWG.

Part: COVER — CRACKED (EXIT SIGN) · airframe 62,269 hrs · 50,136 cycles

AFT DOOR EMER EXIT BULLNOSE SIGN COVER CRACKED. R & R COVER IAW MM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 62,269 hrs · 50,136 cycles

AFT CARGO PIT FRAME CORRODED AT BS 907 BETWEEN RBL 5 TO LBL 5. R & R FRAME IAW SRM & DWG.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 62,269 hrs · 50,136 cycles

LOWER FWD CRACKED AT BS 727 STRINGER 18L IN THE INNER CHORD. R & R CHORD IAW EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 62,269 hrs · 50,136 cycles

RIGHT FLOORBEAM T CAP CORRODED AT BS 986. R & R T CAP IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,269 hrs · 50,136 cycles

FRAME CHORD LOWER FWD HOLE CRACKED AT BS 727 STRINGER 18AL, 3 O'CLOCK & 8 O'CLOCK POSITION. REPAIRED CHORD IAW EA.

Part: PANEL — CRACKED (NLG WW) · airframe 62,269 hrs · 50,136 cycles

NOSE WW RT FWD SIDE PANEL CRACKED BELOW SIDE PANEL 3103R. REPAIRED PANEL IAW SRM.

Part: TIP CAP — CRACKED (LT HORIZ STAB) · airframe 62,269 hrs · 50,136 cycles

LEFT HORIZONTAL STABILIZER OTBD TIP CRACKED. R & R TIP IAW MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,269 hrs · 50,136 cycles

FRAME CHORD LOWER FWD HOLE CRACKED AT BS 727 STRINGER 18AR, 9 O'CLOCK POSITION. REPAIRED CHORD IAW EA.

Part: PANEL — CRACKED (NLG WW) · airframe 62,269 hrs · 50,136 cycles

NOSE WW LT SIDE PANEL CRACKED BETWEEN SIDE PANELS 3104L & 3106L. R & R PANEL IAW SRM.

Part: LIGHT — MISSING (CABIN) · airframe 62,165 hrs · 50,059 cycles

LEFT FWD EEPLS MISSING AT ROW 1. INSTALLED EEPLS IAW MMM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 61,080 hrs · 49,306 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUSTMENT. ADJUSTED SLIDE IAW AMM.

Part: FLAP — DELAMINATED (LT WING) · airframe 60,205 hrs · 48,696 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,205 hrs · 48,696 cycles

FRAME CRACKED AT BS 348.2 BETWEEN STRINGER 13L TO STRINGER 7L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,205 hrs · 48,696 cycles

FRAME CRACKED AT BS 348.2 BETWEEN STRINGER 13L TO STRINGER 17L. REPAIRED FRAME IAW SWA EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 60,205 hrs · 48,696 cycles

INTERCOSTAL CRACKED AT BS 348 STRINGER 16L. REPAIRED INTERCOSTAL IAW EA.

Part: COVER — LOOSE (CABIN) · airframe 59,985 hrs · 48,545 cycles

FWD ENTRY EMERGENCY EXIT COVER LOOSE. SECURED COVER IAW SIP.

Part: MOUNT BRACKET — CRACKED (R2 DOOR) · airframe 59,350 hrs · 48,071 cycles

R2 DOOR EMERGENCY EVAC SLIDE FWD MOUNT BRACKET CRACKED. R&R BRACKET IAW AMM.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 58,833 hrs · 47,671 cycles

AFT CARGO DOOR CUTOUT LOWER AFT CORNER DOUBLER CRACKED. REPAIRED DOUBLER IAW EA.

Part: LENS — LOOSE (CABIN) · airframe 57,602 hrs · 46,760 cycles

EMERGENCY LIGHT LENS NOT SECURED IN BULLNOSE 19 D. ADJUSTED PER MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 57,602 hrs · 46,760 cycles

R2 DOOR SLIDE PRESSURE GAUGE NOT VISABLE IN WINDOW. REPOSITIONED GAUGE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,765 hrs · 46,158 cycles

L1 DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: SIGN — BROKEN (CABIN) · airframe 56,640 hrs · 46,072 cycles

L1 DOOR EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN PER M/M.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 56,522 hrs · 45,992 cycles

LONGITUDINAL FLOORBEAM CRACKED AT BS 709, BL 0. REPAIRED WEB PER SI & EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 56,522 hrs · 45,992 cycles

LONGITUDINAL FLOORBEAM CRACKED AT BS 713, BL 0. REPAIRED WEB PER SI & EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 56,522 hrs · 45,992 cycles

SHEAR TIE CORRODED AT BS 500C, BETWEEN STR 28LTO STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 56,522 hrs · 45,992 cycles

LONGITUDINAL FLOORBEAM CRACKED AT BS 708, BL 0. REPAIRED WEB PER SI & EA.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 56,522 hrs · 45,992 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD LOWER SURFACE ATTACH STRAP CRACKED AT BS 727A+17, RBL 24.8. REMOVED AND REPLACED GUSSET PER SRM.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 56,522 hrs · 45,992 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD LOWER SURFACE ATTACH STRAP CRACKED AT BS 727A+18, LBL 45.5. REMOVED AND REPLACED GUSSET PER SRM.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 56,522 hrs · 45,992 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD LOWER SURFACE ATTACH STRAP CRACKED AT BS 727A+18, RBL 24.8. REMOVED AND REPLACED GUSSET PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 56,522 hrs · 45,992 cycles

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

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 56,522 hrs · 45,992 cycles

LONGITUDINAL FLOORBEAM CRACKED AT BS 709, LBL 24.8. REPAIRED BEAM IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 56,522 hrs · 45,992 cycles

LONGITUDINAL FLOORBEAM CRACKED AT BS 710, LBL 24.8. REPAIRED BEAM IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 56,522 hrs · 45,992 cycles

LONGITUDINAL FLOORBEAM CRACKED AT BS 714, RBL 24.8. REPAIRED BEAM IAW EA.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 56,522 hrs · 45,992 cycles

CENTER FUEL TANK FRONT SPAR GUSSET CRACKED AT AFT END, LBL 53.75. REMOVED AND REPLACED GUSSET PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 56,522 hrs · 45,992 cycles

LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 707, LBL 24.8. REPAIRED WEB IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 56,522 hrs · 45,992 cycles

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

Part: SLAT — DELAMINATED (LT WING) · airframe 56,522 hrs · 45,992 cycles

LEFT WING NR 2 SLAT O/B TRAILING EDGE DELAMINATED. REPAIRED SLAT PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 56,522 hrs · 45,992 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,087 hrs · 45,661 cycles

L2 DOOR LOWER EMERGENCY LIGHT BULBS INOP. REMOVED AND REPLACED BULBS PER AMM.

Part: SKIN — PUNCTURED (RT ELEVATOR) · airframe 56,087 hrs · 45,661 cycles

RIGHT ELEVATOR PUNCTURED ON UPPER SURFACE APPROX 6.5 INCHES FROM TRAILING EDGE AND 41.5 INCHES FROM OUTBD END. REPAIRED ELEVATOR PER SRM.

Part: COVER — MISSING (CABIN) · airframe 56,052 hrs · 45,629 cycles

RIGHT OVERHEAD EMERGENCY EXIT LIGHT COVER MISSING AT ROW 19. INSTALLED COVER IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 55,598 hrs · 45,299 cycles

RIGHT EMERGENCY LIGHT INOP AT ROW 19. REMOVED AND REPLACED LIGHT IAW AMM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 55,598 hrs · 45,299 cycles

STRINGER CRACKED AT BS 727D, STR 5L. REPAIRED STRINGER IAW EA.

Part: STRINGER CLIP — CRACKED (BS 400 S8L) · airframe 55,598 hrs · 45,299 cycles

STRINGER CLIP CRACKED AT BS 400, STR 8L. REMOVED AND REPLACED STRINGER CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,598 hrs · 45,299 cycles

STRINGER CLIP CRACKED AT BS 1006, STR 6L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,598 hrs · 45,299 cycles

STRINGER CLIP CRACKED AT BS 967, STR 2R. REMOVED AND REPLACED CLIP IAW SRM & DWG.

Part: LENS — CRACKED (CABIN) · airframe 55,598 hrs · 45,299 cycles

OVERHEAD EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LENS IAW MM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 55,598 hrs · 45,299 cycles

SHEAR TIE CRACKED AT BS 947.5, BETWEEN STR 5L AND STR 6L. REMOVED AND REPLACED SHEAR TIE PER SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,598 hrs · 45,299 cycles

RT FUSELAGE SKIN CRACKED AT BS 380+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW BAC DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,598 hrs · 45,299 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 460+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,598 hrs · 45,299 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 807+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (BS 440) · airframe 55,598 hrs · 45,299 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 440+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (BS 500C) · airframe 55,598 hrs · 45,299 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 500C+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 55,558 hrs · 45,267 cycles

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

Part: LIGHT — LOOSE (CABIN) · airframe 55,501 hrs · 45,226 cycles

RT EMERGENCY EXIT BULLNOSE LIGHT LENS LOOSE AT ROW 8. SECURED LIGHT PER AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,272 hrs · 45,060 cycles

FUSELAGE SKIN CRACKED AT BS 727E+16, STR 1R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,272 hrs · 45,060 cycles

FUSELAGE SKIN CRACKED AT BS 847+7.5, STR 1L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,272 hrs · 45,060 cycles

FUSELAGE SKIN CRACKED AT BS 847+1.5,STR 1L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,272 hrs · 45,060 cycles

FUSELAGE SKIN CRACKED AT BS 727E+15, STR 2R. REPAIRED SKIN PER SRM & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,272 hrs · 45,060 cycles

FUSELAGE SKIN CRACKED AT BS 827+15, STR 2R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,272 hrs · 45,060 cycles

FUSELAGE SKIN CRACKED AT BS 847+6, STR 1. REPAIRED SKIN.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,272 hrs · 45,060 cycles

FUSELAGE SKIN CRACKED AT BS 787+4, STR 4R. REPAIRED SKIN PER REO & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,272 hrs · 45,060 cycles

FUSELAGE SKIN CRACKED AT BS 727E+16, STR 1. REPAIRED SKIN IAW EA.

Part: FASTENER — CRACKED (FUSELAGE) · airframe 55,271 hrs · 45,060 cycles

CREASE BEAM FASTENER CRACKED AT BS 616, STR 17R. REMOVED AND REPLACED FASTENER IAW SRM.

Part: BEAM — CRACKED (FUSELAGE) · airframe 55,272 hrs · 45,060 cycles

LT STUB BEAM CRACKED AT STA 616. REMOVED AND REPLACED STUB BEAM PER EA.

Part: FITTING — CRACKED (FUSELAGE) · airframe 55,272 hrs · 45,060 cycles

LT STUB BEAM ATTACHMENT CLIP CRACKED AT BS 639, LBL 45.5. REMOVED AND REPLACED CLIP IAW AND BAC DWG.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 55,272 hrs · 45,060 cycles

RT STUB BEAM ATTACHMENT CLIP CRACKED AT BS 639 RBL 45.5. REMOVED AND REPLACED CLIP IAW BAC DWG.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 55,272 hrs · 45,060 cycles

LT SIDE INNER CHORD CRACKED AT BS 616. REPAIRED CHORD PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,771 hrs · 44,697 cycles

DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E+6, STR 4R. REPAIRED SKIN PER EA & SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,771 hrs · 44,697 cycles

DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 807 TO BS 827, STR 4R. REPAIRED SKIN PER EA & SRM.

Part: LENS — LOOSE (CABIN) · airframe 54,165 hrs · 44,249 cycles

RT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT LENS LOOSE AT ROW 9. REMOVED AND REPLACED LENS IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,702 hrs · 43,115 cycles

DURING SCHEDULED 2HC1 CHECK FOUND, FUSELAGE SKIN CRACK FORWARD FROM AFT SERVICE DOOR LOWER HINGE CUTOUT AND BELOW FUSELAGE SCALLOP. REPAIRED PER DOC.

Part: SLIDE — LOOSE (ENTRY DOOR) · airframe 52,702 hrs · 43,115 cycles

DURING SCHEDULED 2HC1 CHECK FOUND, FWD ENTRY DOOR SLIDE GIRT OUTPLAY IS EXCESSIVE. ADJUSTED FWD ENTRY DOOR SLIDE GIRT PER AMM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 52,461 hrs · 42,938 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT WING EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LAMP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,960 hrs · 42,567 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED BETWEEN BS 845 TO BS 847, STR 1L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,960 hrs · 42,567 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 527, STR 10R. REPAIRED SKIN PER ER AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,960 hrs · 42,567 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 735A, STR 4R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,956 hrs · 42,566 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED BETWEEN BS 845 TO BS 847, STR 1L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,956 hrs · 42,566 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 527, STR 10R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,956 hrs · 42,566 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 727A, STR 4R. REPAIRED SKIN PER SRM.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 51,501 hrs · 42,226 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT FRAME WEB DAMAGED AT BS 235.8, WL 226. REPAIRED WEB PER EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 51,501 hrs · 42,226 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CRACKED AT BS 663.75, STR 16R. REPAIRED STRINGER PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,501 hrs · 42,226 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 5L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,501 hrs · 42,226 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 51,501 hrs · 42,226 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5. REPAIRED BEAM PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,501 hrs · 42,226 cycles

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

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 51,501 hrs · 42,226 cycles

DURING SCHEDULED 16Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 668, LBL 24.5. REPAIRED BEAM PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 51,501 hrs · 42,226 cycles

DURING SCHEDULED 16Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 727B, LBL 24. REMOVED AND REPLACED BEAM PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 51,501 hrs · 42,226 cycles

DURING SCHEDULED 16Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 727B-3, LBL 24. REPAIRED BEAM PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,501 hrs · 42,226 cycles

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

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 51,501 hrs · 42,226 cycles

DURING SCHEDULED 16Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 727B, LBL 45. REPAIRED CHORD PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,501 hrs · 42,226 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP DAMAGED AT BS 787, STR 9L. REMOVED AND REPLACED CLIP PER SRM.

Part: ANGLE — CRACKED (R1 DOOR) · airframe 51,501 hrs · 42,226 cycles

DURING SCHEDULED 16Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE CRACKED BETWEEN GIRT BAR SUPPORT ANGLE. REPAIRED ANGLE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,501 hrs · 42,226 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 16R. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 51,501 hrs · 42,226 cycles

DURING SCHEDULED 16Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 727B, RBL 45. REPAIRED BEAM PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 51,501 hrs · 42,226 cycles

DURING SCHEDULED 16Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 727B, RBL 24. REPAIRED BEAM PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,501 hrs · 42,226 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 500B, BETWEEN STR 20R TO STR 21R. REPAIRED FRAME PER SRM.

Part: CIRCUIT CARD — FAULTY (E&E BAY) · airframe 50,790 hrs · 41,666 cycles

AFTER RAISING GEAR ON TAKE OFF, RED "RIGHT" AND GREEN "RIGHT GEAR" LIGHTS WERE ON. LOWERED GEAR AND GEAR INDICATED ALL DOWN WITH THREE GREEN LIGHTS. REMOVED AND REPLACED M986 CIRCUIT CARD PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,516 hrs · 40,677 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 510A, STR 8L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (BS 500A S8L) · airframe 55,598 hrs · 45,299 cycles

FUSELAGE SKIN CRACKED AT BS 500A+10, STR 8L. REMOVED AND REPLACED SKIN PER SRM.

Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 49,308 hrs · 40,527 cycles

DURING SCHEDULED HC1 CHECK, FOUND MAIN WHEEL WELL KEEL BEAM LOWER SKIN CRACKED BETWEEN BS 660 TO BS 724. REPAIRED BEAM PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,308 hrs · 40,527 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED ON KEEL BEAM MAIN WHEEL WELL BETWEEN BS 698 TO BS 715. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 48,922 hrs · 440,265 cycles

DURING SCHEDULED MV3 CHECK, FOUND RT AFT LOWER EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: GIRT BAR — LOOSE (R1 DOOR) · airframe 47,759 hrs · 3,390 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR LOOSE. SECURED GIRT BAR PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,759 hrs · 3,390 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND SKIN CRACKED AT BS 836, STR 3L. REPAIRED SKIN PER SWA EA.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 47,759 hrs · 3,390 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND RT WING NR 5 SLAT T/E WEDGE DELAMINATED. REMOVED AND REPLACED SLAT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,598 hrs · 45,299 cycles

SKIN CRACKED AT BS 836, STR 3L. REPAIRED SKIN PER EA.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 47,759 hrs · 3,390 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND LT WING O/B AFT FLAP LOWER SURFACE DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: GIRT BAR — LOOSE (L1 DOOR) · airframe 47,759 hrs · 3,390 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,598 hrs · 45,299 cycles

SKIN CRACKED AT BS 836, STR 3L. REMOVED AND REPLACED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 47,154 hrs · 38,942 cycles

L1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CASE, DID NOT DEPLOY. SECURED SLIDE PER MT.

Part: WINDOW — ARCED (COCKPIT) · airframe 46,738 hrs · 38,651 cycles

R1 COCKPIT WINDOW ARCED. REMOVED AND REPLACED WINDOW PER MM.

Part: CONNECTOR — BROKEN (RT MLG) · airframe 46,642 hrs · 38,583 cycles

AT APPROXIMATELY 20,000 FT ON CLIMBOUT, RECEIVED RIGHT RED & GREEN LIGHT. CYCLED GEAR, LIGHTS EXTINGUISHED. REMOVED AND REPLACED CONNECTOR D4536P PER MM.

Part: SKIN — CRACKED (NLG WW) · airframe 46,030 hrs · 38,135 cycles

DURING SCHEDULED HC1 CHECK, FOUND NLG W/W LT SIDEWALL CRACKED FWD OF DOOR CONTROL PIVOT ROD. REPAIRED SIDEWALL SKIN PER SWA EA.

Part: TRACK — DELAMINATED (CABIN) · airframe 46,030 hrs · 38,135 cycles

DURING SCHEDULED HC1 CHECK, FOUND RT EEPLS TRACK DELAMINATED AT ROW 1. REMOVED AND REPLACED EEPLS PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 46,030 hrs · 38,135 cycles

DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMERGENCY EVACUATION SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 45,794 hrs · 38,037 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT RT R1 DOOR LOWER HINGE CUTOUT, BS 290, WL 228. REPAIRED SKIN PER ER.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 45,794 hrs · 38,037 cycles

DURING SCHEDULED SPV CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 377, RBL 70, WL 208. REMOVED AND REPLACED WEB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 45,794 hrs · 38,037 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT RT R1 DOOR LOWER HINGE CUTOUT, BS 304, WL 257. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 45,794 hrs · 38,037 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT, BS 304, WL 234. REPAIRED SKIN PER ER.

Part: WIRE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 45,794 hrs · 38,037 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD GALLEY EMERGENCY EXIT SIGN INOP. REPAIRED WIRE PER MM.

Part: DOOR FRAME — CRACKED (L2 DOORWAY) · airframe 45,894 hrs · 38,037 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT L2 DOOR LOWER AFT ENTRY CUTOUT. REMOVED AND REPLACED FRAME PER SRM.

Part: CREASE BEAM — CORRODED (BS 397) · airframe 45,894 hrs · 38,037 cycles

DURING SCHEDULED SPV CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 397, RBL 70, WL 208. REPAIRED WEB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 45,894 hrs · 38,037 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT, BS 290, WL 234. REPAIRED SKIN PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,894 hrs · 38,037 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,894 hrs · 38,037 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 45,894 hrs · 38,037 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 45,894 hrs · 38,037 cycles

DURING SCHEDULED SPV CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED BETWEEN BS 667 TO BS 671, RBL 24. REPAIRED CHORD PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,894 hrs · 38,037 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,894 hrs · 38,037 cycles

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

Part: FLASHLIGHT — BROKEN (CABIN) · airframe 45,894 hrs · 38,037 cycles

DURING SCHEDULED SPV CHECK, FOUND FLASHLIGHT IN AFT LT WINDSCREEN BROKEN. REMOVED AND REPLACED FLASHLIGHT ASSY PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,894 hrs · 38,037 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,894 hrs · 38,037 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,894 hrs · 38,037 cycles

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

Part: SKIN — CRACKED (HORIZ STAB) · airframe 42,733 hrs · 35,749 cycles

DURING SCHEDULED HC1 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT BS 131. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 42,074 hrs · 35,239 cycles

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

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 41,720 hrs · 34,966 cycles

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

Part: HOOK — LOOSE (L1 DOOR GIRT BAR) · airframe 41,382 hrs · 34,684 cycles

L1 DOOR EVAC SLIDE GIRT BAR HOOKS LOOSE. SECURED GIRT BAR HOOKS PER MM.

Part: SKIN — CRACKED (BS 410) · airframe 41,138 hrs · 34,489 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 410, LBL 1. REPAIRED SKIN PER SWA EA.

Part: GIRT BAR — CRACKED (R1 DOOR) · airframe 41,131 hrs · 34,481 cycles

DURING SCHEDULED BRDG CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING LOOSE. SECURED FITTING PER MM.

Part: GIRT BAR — CRACKED (L1 DOOR) · airframe 41,131 hrs · 34,481 cycles

DURING SCHEDULED BRDG CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING LOOSE. SECURED FITTING PER MM.

Part: GIRT BAR — CRACKED (R2 DOOR) · airframe 41,131 hrs · 34,481 cycles

DURING SCHEDULED BRDG CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING LOOSE. SECURED FITTING PER MM.

Part: BEARING — WORN (ELEVATOR TAB) · airframe 41,129 hrs · 34,479 cycles

DURING SCHEDULED BRDG CHECK, RIGHT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 HINGE BEARING AND BUSHING PER MM.

Part: BUSHING — WORN (ELEVATOR TAB) · airframe 41,129 hrs · 34,479 cycles

DURING SCHEDULED BRDG CHECK, RIGHT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 HINGE BUSHING PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 38,366 hrs · 32,369 cycles

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

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 35,899 hrs · 30,497 cycles

DURING SCHEDULED C1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: RELAY — FAULTY (COCKPIT) · airframe 35,716 hrs · 30,370 cycles

AIR TURNBACK, SMOKE AND BURNING ELECTRICAL SMELL IN COCKPIT AND CABIN. REMOVED AND REPLACED R3 RELAY IAW MM.

Part: SKIN — DELAMINATED (RT WING FLAP) · airframe 35,653 hrs · 30,326 cycles

DURING SCHEDULED RON, FOUND RT INBD T/E AFT FLAP DELAMINATED. REPAIRED FLAP PER SWA EA.

Part: BUSHING — FAILED (ELEVATOR TAB) · airframe 34,940 hrs · 29,723 cycles

DURING SCHEDULED C4 CHECK, RT ELEVATOR TAB FAILED THE FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR TAB NR 1 HINGE BUSHINGS & HARDWARE PER MM.

Part: HINGE BRACKET — CRACKED (L1 DOOR) · airframe 34,940 hrs · 29,723 cycles

DURING SCHEDULED C4 CHECK, FOUND L1 DOOR UPPER HINGE BOX FITTING CRACKED. REMOVED AND REPLACED UPPER HINGE BOX PER SRM.

Part: UPLOCK SENSOR — FAULTY (RT MLG) · airframe 34,829 hrs · 29,636 cycles

RT MLG UNSAFE LIGHT INDICATION, RECYCLED GEARS AND LIGHT EXTINGUISHED. REMOVED AND REPLACED RT MLG UPLOCK SENSOR PER MM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 33,169 hrs · 28,332 cycles

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

Part: BEAM — CRACKED (FUSELAGE) · airframe 32,785 hrs · 28,040 cycles

DURING SCHEDULED D-CHECK, FOUND STUB BEAM AT BS 616, RBL 64, CRACKED. REPAIRED STUB BEAM PER ER.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 32,785 hrs · 28,040 cycles

DURING SCHEDULED D-CHECK, FOUND FWD CARGO DOOR AFT FRAME, LOWER STOP FITTING, CRACKED. REPAIRED FRAME PER ER.

Part: DOOR FRAME — CORRODED (CARGO BAY) · airframe 32,785 hrs · 28,040 cycles

DURING SCHEDULED D-CHECK, FOUND AFT CARGO COMPARTMENT FRAME AT BS 787, RBL 10, CORRODED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FITTING — CORRODED (HORIZONTAL STAB) · airframe 32,785 hrs · 28,040 cycles

DURING SCHEDULED D-CHECK, FOUND HORIZONTAL STAB FITTING RT AND LT FWD AND AFT CLEVIS LUGS CORRODED. REPAIRED HORIZONTAL STAB PER ER.

Part: STRUCTURE — WARPED (RT FORE FLAP) · airframe 32,785 hrs · 28,040 cycles

DURING SCHEDULED D-CHECK, FOUND RT WING OUTBOARD T/E FORE FLAP, WARPED. REMOVED AND REPLACED RT WING OUTBOARD T/E FORE FLAP PER MM.

Part: RIB — CRACKED (LT WING) · airframe 32,785 hrs · 28,040 cycles

DURING SCHEDULED D-CHECK, FOUND LT AND RT WINGS LOWER RIB CHORDS AT WBL 135.5, CRACKED. REPAIRED RIB CHORDS PER ER.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 32,785 hrs · 28,040 cycles

DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB FROM BS 295 TO BS 299, RBL 55, CORRODED. REMOVED AND REPLACED WEB SECTION PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 32,785 hrs · 28,040 cycles

DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB FROM BS 330 TO BS 335, RBL 55, CORRODED. REMOVED AND REPLACED WEB SECTION PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 32,785 hrs · 28,040 cycles

DURING SCHEDULED D-CHECK, FOUND FWD CARGO COMPT FRAME AT BS 500B, BETWEEN LBL 6 AND RBL 6, CORRODED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 32,785 hrs · 28,040 cycles

DURING SCHEDULED D-CHECK, FOUND AFT CARGO COMPT FRAME AT BS 727E, BETWEEN RBL10 AND RBL 20, CORRODED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 32,785 hrs · 28,040 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP AT BS 747, STRINGER 26R, CORRODED. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 32,785 hrs · 28,040 cycles

DURING SCHEDULED D-CHECK, FOUND AFT CARGO COMPT FRAME AT BS 767, RBL 12, CORRODED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 32,785 hrs · 28,040 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM UPPER CHORD AT BS 270 FROM LBL 7 TO RBL 7, CORRODED. REMOVED AND REPLACED FLOORBEAM CHORD SECTION PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 32,785 hrs · 28,040 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM SHEAR WEB FROM BS 947 TO BS 1006, RBL 45, CORRODED. REMOVED AND REPLACED WEB PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 32,785 hrs · 28,040 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 767, BETWEEN LBL 7 AND LBL 18, CORRODED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 32,785 hrs · 28,040 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 500C, BETWEEN LBL 2 AND RBL 20, CORRODED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 32,785 hrs · 28,040 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE AT BS 907, STRINGER 4L, CRACKED. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,785 hrs · 28,040 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 360, STRINGER 8R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 32,785 hrs · 28,040 cycles

DURING SCHEDULED D-CHECK, FOUND FWD ENTRY DOOR EVAC SLIDE FWD AND AFT GIRT BAR FLOOR FITTINGS BRACKETS, CORRODED. REMOVED AND REPLACED FWD AND AFT GIRT BAR FITTINGS PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,785 hrs · 28,040 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 480, STRINGER 8L, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: STRUCTURE — CRACKED (BS 380-440) · airframe 38,785 hrs · 28,040 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED BETWEEN BS 380 AND BS 440, STRINGER 8L. REMOVED AND REPLACED STRUCTURE SECTION PER SRM.

Part: STRUCTURE — CRACKED (BS 787-867) · airframe 32,785 hrs · 28,040 cycles

DURING SCHEDULED D-CHECK, FOUND STRUCTURE CRACKED BETWEEN BS 787 AND BS 867, STRINGER 8L. REMOVED AND REPLACED STRUCTURE SECTION PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 32,785 hrs · 28,040 cycles

DURING SCHEDULED D-CHECK, FOUND FWD CARGO COMPARTMENT FRAME AT BS 500A, BETWEEN LBL 6 AND RBL 6, CORRODED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 32,785 hrs · 28,040 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM UPPER CHORD AT BS 312, LBL 2, CORRODED. REMOVED AND REPLACED FLOORBEAM CHORD PER SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 32,785 hrs · 28,040 cycles

DURING SCHEDULED D-CHECK, FOUND 2 EACH CREASE BEAM CHORDS CRACKED AT RIGHT BS 188 AND LEFT BS 188. REMOVED AND REPLACED CREASE BEAM CHORD SECTIONS PER SRM.

Part: FAN — OVERHEATED (E/E BAY) · airframe 31,629 hrs · 27,063 cycles

THIRTY MINUTES PRIOR TO LANDING, ELECTRICAL ODOR IN FWD PART OF CABIN. TURNED OFF GALLEY POWER, RECIRC FAN, GASPER FAN, SMELL SUBSIDED. REMOVED AND REPLACED RECIRC FAN PER MM.

Part: PANEL — CRACKED (FUSELAGE) · airframe 31,186 hrs · 26,690 cycles

DURING SCHEDULED C4 CHECK, FOUND LEFT KEELBEAM PANEL AT BS 660, BS 700, CRACKED. REPAIRED KEELBEAM PANEL PER SRM.

Part: SKIN — DELAMINATED (RT FOREFLAP) · airframe 31,186 hrs · 26,690 cycles

DURING SCHEDULED C4 CHECK, FOUND RIGHT WING INBOARD FOREFLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED INBOARD FOREFLAP PER MM.

Part: BEARING — WORN (LT ELEVATOR) · airframe 31,177 hrs · 26,682 cycles

DURING SCHEDULED C4 CHECK, RT AND LT ELEVATORS FAILED FREE PLAY CHECK. REMOVED AND REPLACED RT AND LT ELEVATOR INPUT ROD BEARINGS PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 31,177 hrs · 26,682 cycles

DURING SCHEDULED C4 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 30,160 hrs · 25,891 cycles

DURING SCHEDULED C3 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 30,162 hrs · 25,893 cycles

DURING SCHEDULED 1/4D CHECK, FOUND CORROSION ON AFT PRESSURE BULKHEAD WEB AT BS 1016, LBL 2 TO RBL 2. REPAIRED WEB PER ACO.

Part: STIFFENER — CORRODED (BULKHEAD) · airframe 30,162 hrs · 25,893 cycles

DURING SCHEDULED 1/4D CHECK, FOUND CORROSION ON AFT PRESSURE BULKHEAD CHANNEL STIFFNERS AT BS 1016, BL 0. REPAIRED PER ACO.

Part: CABLE — MISROUTED (L2 DOOR) · airframe 29,326 hrs · 25,217 cycles

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

Part: STRIP — DETERIORATED (CABIN) · airframe 29,326 hrs · 25,217 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS STRIP DETERIORATED AT LT AFT END. REMOVED AND REPLACED EEPLS SECTION PER MM.

Part: SLIDE — LOOSE (L2 DOOR) · airframe 28,731 hrs · 21,720 cycles

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

Part: CABLE — MISROUTED (ESCAPE SLIDE) · airframe 28,449 hrs · 24,505 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM.

Part: LIGHT — INOPERATIVE (MID CABIN) · airframe 27,814 hrs · 23,976 cycles

EEPLS SECTION INOP AT MID CABIN. REMOVED AND REPLACED EEPLS SECTION PER MM.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 26,599 hrs · 23,013 cycles

DURING SCHEDULED BC3 CHECK, FOUND RT WING INBOARD FOREFLAP UPPER SURFACE DELAMINATED IN A 6 INCH DIAMETER CENTER SECTION. REMOVED AND REPLACED INBOARD FOREFLAP PER MM.

Part: SLIDE — OUT OF POSITION (AFT SVC DOOR) · airframe 25,644 hrs · 22,257 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW AND CABLE MISROUTED. REPOSITIONED SLIDE AND REROUTED CABLE PER MM.

Part: CABLE — MISROUTED (CABLE) · airframe 25,644 hrs · 22,257 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 24,714 hrs · 21,521 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 767, ABOVE STR 13R. REPAIRED SKIN PER SRM.

Part: TAB — WORN (LT ELEVATOR) · airframe 24,404 hrs · 21,260 cycles

DURING SCHEDULED SERVICE CHECK, SWA SI 11111-55, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED LT ELEVATOR TAB PER MM.

Part: WEB — CRACKED (FUSELAGE) · airframe 22,848 hrs · 19,978 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED (2 EA) AT BS 178, WL201, RBL 5.0 AND LBL 5.0. REPAIRED WEB PER SRM.

Part: SKIN — CRACKED (MLG W/W) · airframe 21,992 hrs · 19,287 cycles

DURING SCHEDULED C2 CHECK, FOUND KEEL BEAM SKIN CRACKED 2 INCHES LONG, LH SIDE AT BS 682. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (AFT CARGO DOOR) · airframe 21,992 hrs · 19,287 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT CARGO DOOR SKIN CRACKED 3/8 INCH LONG AT BS 817. REPAIRED DOOR PER SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 20,527 hrs · 18,015 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RT WING OUTBD AFT FLAP DELAMINATED ON INBOARD END, UPPER AND LOWER SURFACES. REMOVED AND REPLACED AFT FLAP PER MM.

Part: DOOR — OUT OF ADJ (FWD ENTRY) · airframe 19,894 hrs · 17,499 cycles

AIR TURNBACK, AIRCRAFT FAILED TO PRESSURIZE DURING CLIMB. NO DOOR WARNING INDICATIONS. ADJUSTED FWD ENTRY DOOR PER MM. PRESSURIZED A/C & FOUND NO LEAKS PER MM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 19,685 hrs · 17,320 cycles

DURING SCHEDULED C3 CHECK, FOUND RT WING T/E INBOARD AFT FLAP DELAMINATED AT OUTBOARD LOWER CORNER. REMOVED AND REPLACED AFT FLAP ASSY PER MM.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 19,685 hrs · 17,320 cycles

DURING SCHEDULED C3 CHECK, FOUND LT WING T/E INBOARD AFT FLAP DELAMINATED ON OUTBOARD LOWER SURFACE. REPAIRED AFT FLAP PER SRM & RA 1-A57-0608.

Part: LIGHT — LOOSE (CABIN) · airframe 19,685 hrs · 17,320 cycles

DURING SCHEDULED C3 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT OUT OF RETAINER AT ROW 16. SECURED LIGHT ASSY PER MM.

Part: FRAME — CRACKED (BS 178)

DURING SCHEDULED 1/2D CHECK, FOUND BS 178 BULKHEAD LT AND RT SIDE CHORDS CRACKED, LBL AND RBL 26. REMOVED AND REPLACED CHORD SECTIONS PER SRM.

Part: LIGHT — LOOSE (GALLEY)

DURING SCHEDULED 1/2D CHECK, FOUND EMERGENCY EXIT LIGHT LOOSE AT FWD GALLEY. REMOVED AND REPLACED EXIT LIGHT ASSY PER MM.

Part: FLOORBEAM — CORRODED (BS 986)

DURING SCHEDULED 1/2D CHECK, FOUND BS 986 FLOORBEAM UPPER SURFACE CORRODED, RBL 36. REPAIRED BEAM PER SRM.

Part: LIGHT — DAMAGED (ROW 11)

EEPLS LENS MISSING AT ROW 11. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: WIRE — BROKEN (ROW 11-12)

DURING WALKAROUND CHECK, FOUND APPROX 4 EMERGENCY EXIT AISLE LIGHTS BETWEEN ROW 11 AND 12 ARE PULLED UP AND WIRES BROKEN. RECONNECTED WIRING TO LIGHT FIXTURES AND SECURED LIGHT LENSES, OPS CHECK GOOD.

Part: LIGHT — MISSING (CABIN)

DURING WALKAROUND CHECK, FOUND SMALL SECTION OF FLOOR TRACK LIGHTING MISSING MID CABIN AT EMERGENCY EXIT. REPLACED MISSING SECTION OF FLOOR TRACK LIGHTING AND CHECKED WONDERFUL PER BOEING MM.

Part: WIRE — LOOSE (CABIN)

DURING SCHEDULED WALKAROUND CHECK, FOUND OVERWING EMERGENCY FLOOR TRACK LIGHTING HAS LOOSE WIRE. RELAMPED AND RECONNECTED EMERGENCY FLOOR TRACK LIGHTS PER BOEING SRM.

Part: LIGHT — KICKED UP (CABIN)

DURING WALKAROUND CHECK, FOUND EMERGENCY TRACK LIGHTS KICKED UP AT MID CABIN. REINSTALLED TRACK, FOUND RED LIGHT OUT AT WING EXIT ROW AND PLACARDED PER MEL. RECONNECTED RED LAMP AT EMERGENCY EXIT ROW PER BOEING MM.

Part: BASE — INOPERATIVE (CABIN)

DURING WALKAROUND INSPECTION, FOUND EMERGENCY TRACK LIGHTS INOP AT ROW 14. REPLACED LIGHT BASE PER BOEING M/M.

Part: WIRE — EXPOSED (CABIN)

DURING WALKAROUND CHECK, FOUND EMERGENCY EXIT LIGHT WIRES AT EXIT ROW EXPOSED. REPAIRED WIRES PER BOEING M/M.

Part: LINKAGE — MISADJUSTED (NLG DOOR)

AFTER TAKEOFF, WHEN GEAR RETRACTED, NOSE GEAR UNSAFE LIGHT REMAINED ILLUMINATED. RECYCLED GEAR AND RECEIVED SAME INDICATION. VISUALLY CHECKED NOSE GEAR, UP AND LOCKED. LANDED AT STL WITHOUT INCIDENT, ADJUSTED NLG DOOR LINKAGE AND PERFORMED GEAR RETRACTION TEST PER BOEING M/M.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING SCHEDULED A1 CHECK, FOUND OVERHEAD EXIT SIGNS INOP. REPLACED BATTERY PACK PER BOEING M/M.

Part: BATT PACK BASE — INOPERATIVE (CABIN)

DURING SCHEDULED C3 CHECK, FOUND LEFT AFT EMERGENCY EXIT LIGHTING INOP. REPLACED BATTERY PACK BASE PER BOEING M/M.