N370SW

Part: LENS — CRACKED (EXTERIOR LIGHT) · airframe 70,998 hrs · 58,551 cycles

RIGHT AFT OF OVERWING EXTERIOR EXIT LIGHT LENS CRACKED. R & R LENS IAW MM.

Part: COVER — MISSING (EXIT SIGN) · airframe 70,790 hrs · 58,395 cycles

LEFT OVERWING EXIT SIGN COVER MISSING. INSTALLED COVER IAW AMM.

Part: LANYARD — LOOSE (CABIN) · airframe 70,746 hrs · 58,363 cycles

LEFT EMER HATCH DOOR ESCAPE LANYARD LOOSE. SECURED LANYARD IAW AMM.

Part: FLAP — DELAMINATED (LT WING) · airframe 70,333 hrs · 58,083 cycles

LEFT WING OTBD AFT FLAP DELAMINATED ON INBD LOWER SIDE. R & R AFT FLAP IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,309 hrs · 58,065 cycles

SKIN CRACKED AT BS 747+2, STINGER 1L. REPAIRED SKIN IAW SRM.

Part: LENS — BROKEN (L2 DOOR) · airframe 70,296 hrs · 58,054 cycles

L2 DOOR EMER LIGHT LENS BROKEN. R & R LENS IAW AMM.

Part: WEB — CRACKED (LT WING) · airframe 69,912 hrs · 57,776 cycles

LEFT WING REAR WEB BEHIND MLG BEAM FITTING CRACKED AT UPPER INBD MOST 2 HOLES. REPAIRED WEB IAW ER & EA.

Part: FITTING — CRACKED (RT WING) · airframe 69,912 hrs · 57,776 cycles

RIGHT WING REAR SPAR FWD BEAM TO SPAR FITTING CRACKED IN FASTENER HOLE COMMON TO UPPER CHORD UPPER ROW & 2ND HOLE INBD FROM INBD EDGE OF FITTING. REPAIRED FITTING IAW EA.

Part: SPAR — CRACKED (RT WING) · airframe 69,912 hrs · 57,776 cycles

RIGHT WING REAR SPAR WEB CRACKED IN INBD UPPER HOLE COMMON TO BEAM TO SPAR FITTING. REPAIRED WEB IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,912 hrs · 57,776 cycles

FUSELAGE SKIN CRACKED AT STATION 513.3, STRINGER 16L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,912 hrs · 57,776 cycles

FUSELAGE SKIN CRACKED BETWEEN BS 385 TO 385.5, STRINGER 15R. REPAIRED SKIN IAW EA.

Part: SPAR — CRACKED (RT WING) · airframe 69,912 hrs · 57,776 cycles

RIGHT WING REAR SPAR UPPER CHORD CRACKED AT MLG AFT SUPPORT FITTING. REPAIRED CHORD ER & EA.

Part: SPAR — CRACKED (LT WING) · airframe 69,912 hrs · 57,776 cycles

LEFT WING REAR SPAR UPPER CHORD CRACKED AT MLG AFT SUPPORT FITTING. REPAIRED CHORD IAW ER & EA.

Part: LENS — DIRTY (CABIN) · airframe 69,518 hrs · 57,478 cycles

RIGHT EMER EXIT LIGHT LENS COVER DIRTY. R & R LENS IAW MM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 68,726 hrs · 56,866 cycles

RIGHT OVERWING DOOR SIDEWALL SIGN LIGHT ASSEMBLY INOPERATIVE. R & R LIGHT ASSEMBLY IAW AMM.

Part: FLAP — DELAMINATED (RT WING) · airframe 67,823 hrs · 56,274 cycles

RIGHT WING OTBD AFT FLAP DELAMINATED INBD END. R & R IAW AMM.

Part: LENS — MISSING (CABIN) · airframe 67,814 hrs · 56,266 cycles

L1 DOOR EMER EXIT LIGHT COVER LENS MISSING. INSTALLED LENS IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 67,697 hrs · 56,173 cycles

FORWARD LAVATORY WALL EMER LIGHT BULB INOPERATIVE. R & R BULB IAW AMM.

Part: FAILSAFE — CRACKED (FUSELAGE) · airframe 67,697 hrs · 56,173 cycles

FORWARD CARGO COMPARTMENT FAIL SAFE CHORD CRACKED AT BS 440 BETWEEN STRINGER 14R TO 18R. R & R CHORD IAW SRM & DWG.

Part: FLAP — CORRODED (LT WING) · airframe 67,697 hrs · 56,173 cycles

LEFT WING FORE FLAP CTR TRACK OTBD FACE FWD CORRODED. REPAIRED FORE FLAP IAW CMM.

Part: TRANSMISSION — CORRODED (TE FLAP) · airframe 67,697 hrs · 56,173 cycles

RIGHT WING NR 5 AFT FLAP TRACK TRANSMISSION OTBD CORRODED. REPAIRED AFT FLAP IAW CMM.

Part: TIE CLIP — BROKEN (FUSELAGE) · airframe 67,697 hrs · 56,173 cycles

TIE CLIP BROKEN AT BS 887 STRINGER 1. R & R TIE CLIP IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,697 hrs · 56,173 cycles

SKIN CRACKED AT BS 480+ 8.25 STRINGER 16R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,697 hrs · 56,173 cycles

FUSELAGE SKIN CRACKED BETWEEN BS 500C+15 TO 530 BETWEEN STRINGER 14R TO 18R. REPAIRED SKIN IAW EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 67,697 hrs · 56,173 cycles

SHEAR TIE CRACKED AT BS 1040 BETWEEN STRINGER 2R TO 3R. R & R SHEAR TIE IAW SRM & DWG.

Part: SKIN — DELAMINATED (RT SPOILER) · airframe 67,697 hrs · 56,173 cycles

RIGHT WING NR 5 SPOILER UPPER SURFACE DELAMINATED. REPAIRED NR 5 SPOILER IAW SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 67,697 hrs · 56,173 cycles

FORWARD ENTRY DOOR SURROUND STRUCTURE STRAP CRACKED AT BS 348.2 STRINGER 16L. R & R STRAP IAW SRM & DWG.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 67,697 hrs · 56,173 cycles

FORWARD ENTRY DOOR SURROUND STRUCTURE ATTACHMENT CLIP CRACKED AT BS 348.2 STRINGER 16L. REPLACED CLIP IAW SRM & DWG.

Part: STIFFENER — CRACKED (TE FLAP) · airframe 67,697 hrs · 56,173 cycles

RIGHT WING NR 6 FLAP TRACK FAIRING STIFFENER CRACKED. R & R STIFFENER IAW SRM & DWG.

Part: ANGLE — CRACKED (TE FLAP) · airframe 67,697 hrs · 56,173 cycles

RIGHT WING NR 6 FLAP TRACK FAIRING ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,697 hrs · 56,173 cycles

FUSELAGE SKIN CRACKED BETWEEN BS 727+5 TO 727C+5 BETWEEN STRINGER 1 TO 4R. REPAIRED SKIN IAW EO & EA.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 67,697 hrs · 56,173 cycles

FORWARD CARGO DOOR CUT OUT FRAME WEB CRACKED AT BS 492 STRINGER 24R. R & R FRAME IAW EO & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 67,697 hrs · 56,173 cycles

FRAME CRACKED AT BS 440 STRINGER 24R. R & R FRAME IAW EO & EA.

Part: RIB — CRACKED (RT WING) · airframe 67,697 hrs · 56,173 cycles

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

Part: NUT PLATE — BROKEN (TE FLAP) · airframe 67,697 hrs · 56,173 cycles

LEFT WING NR 1 FLAP TRACK FAIRING SUPPORT ANGLE NUT PLATE BROKEN. R & R NUT PLATE IAW DWG & SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,697 hrs · 56,173 cycles

SKIN CRACKED AT BS 328+11 STRINGER 2R. REPAIRED SKIN IAW SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 67,697 hrs · 56,173 cycles

STRINGER SPLICE CRACKED AT BS 360 STRINGER 4L. R & R SPLICE IAW EA & EO.

Part: FITTING — CRACKED (TE FLAP TRACK) · airframe 67,697 hrs · 56,173 cycles

LEFT WING NR 3 FLAP TRACK INBD SIDE INTERNAL STRUCTURE CLIP CRACKED. R & R CLIP IAW SRM & DWG.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 67,697 hrs · 56,173 cycles

INNER CHORD CRACKED AT BS 348.2 STRINGER 17L. R & R CHORD IAW EO & EA.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 67,697 hrs · 56,173 cycles

RIGHT WING SUPPORT ANGLE CRACKED AT WING STATION 150 TE AREA. R & R ANGLE IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,697 hrs · 56,173 cycles

FUSELAGE SKIN CRACKED AT BS 500B+5 STRINGER 15R. REPAIRED SKIN IAW EO & EA.

Part: FLAP TRACK — CORRODED (TE FLAP) · airframe 67,697 hrs · 56,173 cycles

RIGHT WING NR 5 AFT FLAP TRACK INBD AFT HOLE CORRODED. REPAIRED AFT FLAP IAW CMM.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 67,697 hrs · 56,173 cycles

ATTACHMENT CLIP CRACKED AT BS 639 LBL 45.5. R & R CLIP IAW SRM & DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 67,697 hrs · 56,173 cycles

CLIP CRACKED AT BS 927 STRINGER 11R. R & R CLIP IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,697 hrs · 56,173 cycles

FUSELAGE SKIN CRACKED AT BS 520+7, STRINGER 28R. REPAIRED SKIN IAW SRM.

Part: SLAT — DELAMINATED (LE SLAT) · airframe 67,697 hrs · 56,173 cycles

RIGHT WING NR 5 SLAT OTBD AFT EDGE DELAMINATED. REPAIRED NR 5 SLAT IAW SRM.

Part: PLATE — CRACKED (FUSELAGE) · airframe 67,697 hrs · 56,173 cycles

STUB BEAM WEB PLATE CRACKED AT BS 639 BETWEEN LBL 45.5 TO LBL 52.5. R & R PLATE IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 67,697 hrs · 56,173 cycles

ANGLE CRACKED AT BS 967 STRINGER 2R. R & R ANGLE IAW SRM & DWG.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 67,697 hrs · 56,173 cycles

LONGITUDINAL FLOORBEAM ATTACHMENT CLIP CRACKED AT BS 639 RBL 45. R & R CLIP IAW SRM & DWG.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 67,697 hrs · 56,173 cycles

RIGHT EMER EXIT LAMP INOPERATIVE. R & R LAMP IAW CMM.

Part: WEB — CRACKED (NLG WW) · airframe 67,697 hrs · 56,173 cycles

LEFT NOSE WW SIDE WEB CRACKED AT BS 243.7+ 3.5 WL 169.1. REPAIRED WEB IAW EO & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 67,697 hrs · 56,173 cycles

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

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 67,697 hrs · 56,173 cycles

MAIN WW PRESS DECK WEB CRACKED AT BS 663.75 LBL 33.5. REPAIRED WEB IAW EA.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 67,697 hrs · 56,173 cycles

MAIN WW PRESS DECK WEB CRACKED AT BS 663.75 LBL 18.5. REPAIRED WEB IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 67,697 hrs · 56,173 cycles

FRAME OTBD CHORD FWD FLANGE CRACKED AT BS 727 STRINGER 18A LT SIDE. R & R CHORD IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,697 hrs · 56,173 cycles

SKIN CRACKED AT BS 927+3.5 STRINGER 21R. REPAIRED SKIN IAW EO & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 67,697 hrs · 56,173 cycles

FRAME OTBD CHORD FWD FLANGE CRACKED AT BS 727, STRINGER 18A LT FWD LOWER HOLE. REPAIRED CHORD IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 67,697 hrs · 56,173 cycles

CENTER WING BOX SEAT TRACK CRACKED AT BS 727B LBL 24.8. REPAIRED SEAT TRACK IAW EA.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 67,697 hrs · 56,173 cycles

MAIN WW PRESS DECK WEB CRACKED AT BS 663.75+2, RBL 42.5. REPAIRED WEB IAW SRM.

Part: SLIDE — UNSECURE (R1 DOOR) · airframe 67,495 hrs · 56,019 cycles

R1 DOOR EMER EVAC SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY & STILL OPERATIONAL. RE-INSTALLED SLIDE IAW MT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 67,051 hrs · 55,684 cycles

RIGHT OVERWING EMER EXIT SIDEWALL LIGHT INOPERATIVE. R & R LIGHT ASSEMBLY IAW AMM.

Part: GIRT BAR — LOOSE (R2 DOOR) · airframe 67,048 hrs · 55,683 cycles

R2 DOOR EMER EVAC SLIDE GIRT LOOSE. SECURED GIRT BAR IAW MT.

Part: HINGE FITTING — BROKEN (LT SPOILER) · airframe 66,805 hrs · 55,514 cycles

LEFT WING INBD GND SPOILER PANEL OTBD CTR HINGE FITTING BROKEN. R & R SPOILER IAW MM.

Part: FITTING — BROKEN (LT SPOILER) · airframe 66,805 hrs · 55,514 cycles

LEFT WING INBD GND SPOILER INBD ACTUATOR FITTING BROKEN AT LOWER ATTACH POINT. R & R FITTING IAW SRM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 65,602 hrs · 54,667 cycles

EXTERNAL EMERGENCY EXIT LIGHT INOPERATIVE AT LT AFT ENTRY DOOR. RELAMPED LIGHT IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,602 hrs · 54,667 cycles

SKIN CRACKED AT BS 413, STRINGER 2R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,602 hrs · 54,667 cycles

SKIN CRACKED AT BS 393, STRINGER 2R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,602 hrs · 54,667 cycles

SKIN CRACKED AT BS 500A+13, STRINGER 16L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,602 hrs · 54,667 cycles

SKIN CRACKED AT BS 492, STRINGER 16L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,602 hrs · 54,667 cycles

SKIN CRACKED AT BS 493.5, STRINGER 16L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,602 hrs · 54,667 cycles

SKIN CRACKED AT BS 500C+14, STRINGER 19L. REPAIRED SKIN IAW SRM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 65,602 hrs · 54,667 cycles

R2 DOOR INNER LOWER EMERGENCY LIGHT INOPERATIVE. R & R BATTERY CHARGER IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,602 hrs · 54,667 cycles

FUSELAGE CHEM MILL UPPER SKIN CRACKED AT BS 500B + 13, STRINGER 26L. REPAIRED SKIN IAW SRM.

Part: FDU — FAULTY (COCKPIT) · airframe 65,194 hrs · 54,369 cycles

ON LANDING ROLL FIRE WARNING LIGHTS & BELL CAME ON & WOULD NOT RESET, NO FIRE. HANDLES OR OTHER LIGHTS ILLUMINATED. R &R FIRE DETECTION UNIT IAW MM.

Part: COVER — OUT OF POSITION (R1 DOOR) · airframe 64,235 hrs · 53,618 cycles

R1 DOOR EMERGENCY EVAC SLIDE DEPLOY HANDLE COVER OUT OF POSITION. REPOSITIONED SLIDE COVER IAW MM.

Part: SLAT — DELAMINATED (RT WING) · airframe 62,304 hrs · 52,210 cycles

RIGHT WING NR 5 SLAT DELAMINATED. REPAIRED NR 5 SLAT IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,304 hrs · 52,210 cycles

TIE CLIP CRACKED AT BS 927, STR 21L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,304 hrs · 52,210 cycles

TIE-CLIP CRACKED AT BS 986.5, STR 27L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 62,304 hrs · 52,210 cycles

LEFT KEEL BEAM CRACKED BETWEEN BS 727 TO BS 663, LBL 6.5. REPAIRED KEEL BEAM IAW SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 62,304 hrs · 52,210 cycles

SKIN CORRODED AT BS 947.5, STR 26L. REPAIRED SKIN IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 62,304 hrs · 52,210 cycles

WEB CRACKED BETWEEN BS 440 TO BS 460, STR 26R. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: SLAT — CRACKED (RT WING) · airframe 62,304 hrs · 52,210 cycles

RIGHT WING NR 6 SLAT CRACKED LEADING EDGE BETWEEN STA 294.40 TO STA 306.40. REPAIRED SLAT IAW SRM.

Part: SLAT — CRACKED (RT WING) · airframe 62,304 hrs · 52,210 cycles

RIGHT WING NR 6 SLAT LEADING EDGE SLAT CRACKED AT STA 447.75. REPAIRED NR 6 SLAT IAW SRM.

Part: SLAT — CRACKED (RT WING) · airframe 62,304 hrs · 52,210 cycles

RIGHT WING NR 6 SLAT CRACKED LEADING EDGE BETWEEN STA 321.40 TO STA 334.40. REPAIRED SLAT IAW SRM.

Part: SLAT — CRACKED (RT WING) · airframe 62,304 hrs · 52,210 cycles

RIGHT WING NR 5 SLAT CRACKED AT LEADING EDGE BETWEEN STA 154.40 TO STA 170.40. REPAIRED SLAT IAW SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 62,304 hrs · 52,210 cycles

STRINGER SPLICE CRACKED AT BS 360, STR 15L. REMOVED AND REPLACED SPLICE IAW SRM AND DWG.

Part: FLAP — DELAMINATED (RT WING) · airframe 62,304 hrs · 52,210 cycles

RIGHT WING O/B FORE FLAP DELAMINATED. REPAIRED FORE FLAP IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 62,304 hrs · 52,210 cycles

CLIP CRACKED AT BS 348.20, STR 15L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 62,304 hrs · 52,210 cycles

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

Part: FRAME — CORRODED (FUSELAGE) · airframe 62,304 hrs · 52,210 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,304 hrs · 52,210 cycles

FRAME CRACKED AT BS 807, RBL 19.5. REPAIRED FRAME IAW EO AND EA.

Part: FLAP — DELAMINATED (RT WING) · airframe 62,304 hrs · 52,210 cycles

RIGHT WING OUTBOARD FORE FLAP DELAMINATED. REPAIRED FORE FLAP IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 62,304 hrs · 52,210 cycles

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

Part: FLAP — DELAMINATED (RT WING) · airframe 62,304 hrs · 52,210 cycles

RIGHT WING AFT FLAP O/B DELAMINATED. REPAIRED AFT FLAP IAW SRM.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 62,304 hrs · 52,210 cycles

LEFT WING NR 3 SLAT SKIN DELAMINATED. REPAIRED SKIN IAW SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 62,304 hrs · 52,210 cycles

LEFT WING OUTBOARD AFT FLAP DELAMINATED. REPAIRED AFT FLAP IAW SRM.

Part: FLAP — CHAFED (RT WING) · airframe 62,304 hrs · 52,210 cycles

RIGHT WING OUTBOARD FORE FLAP LEADING EDGE CHAFED. REPAIRED FORE FLAP AW EO AND EA.

Part: CARRIAGE — CORRODED (TE FLAP) · airframe 62,304 hrs · 52,210 cycles

RIGHT WING OUTBOARD MIDFLAP SPINDLE CARRIAGE CORRODED. REMOVED AND REPLACED SPINDLE CARRIAGE IAW MT.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,304 hrs · 52,210 cycles

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

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,304 hrs · 52,210 cycles

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

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,304 hrs · 52,210 cycles

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

Part: TIE CLIP — CORRODED (FUSELAGE) · airframe 62,304 hrs · 52,210 cycles

TIE CLIP CORRODED AT BS 360, STR 18L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 62,304 hrs · 52,210 cycles

ANGLE CRACKED AT BS 540, BETWEEN STR 24L TO STR 28L. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 62,304 hrs · 52,210 cycles

SUPPORT ANGLE CRACKED BETWEEN BS 294.5 TO BS 328, STR 26L. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 62,304 hrs · 52,210 cycles

SUPPORT CLIP CRACKED AT BS 294.5, STR 24L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: WEB — CRACKED (LT WING) · airframe 62,304 hrs · 52,210 cycles

LEFT WING WEB CRACKED INTERNAL AREA OF FUEL TANK, WBL 198.6. REPAIRED WEB IAW EA AND EO.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 62,304 hrs · 52,210 cycles

SUPPORT ANGLE CRACKED AT BS 312+8, STR 21L. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: WEB — CRACKED (RT WING) · airframe 62,304 hrs · 52,210 cycles

RIGHT WING WEB CRACKED AT WBL 198.60. REPAIRED WEB IAW EA AND EO.

Part: WEB — CRACKED (FUSELAGE) · airframe 62,304 hrs · 52,210 cycles

WEB CRACKED BETWEEN BS 344+8 TO BS 360, BL 0. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: STRUCTURE — CRACKED (LT WING) · airframe 62,304 hrs · 52,210 cycles

LEFT WING UPPER CHORD INTERNAL AREA OF FUEL TANK CRACKED AT WBL 114. REPAIRED CHORD IAW EO AND EA.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 62,304 hrs · 52,210 cycles

SUPPORT ANGLE CRACKED AT BS 328, STR 21L. REPLACED ANGLE IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 62,304 hrs · 52,210 cycles

SUPPORT ANGLE CRACKED AT BS 344+8.5, BETWEEN STR 25R TO STR 28R. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 62,304 hrs · 52,210 cycles

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

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,304 hrs · 52,210 cycles

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

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 62,304 hrs · 52,210 cycles

LEFT BULKHEAD WEB AND CHANNEL STIFFENER CORRODED AT BS 1016, BL 0. REPAIRED STIFFENER PER EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,304 hrs · 52,210 cycles

TIE CLIP CRACKED AT BS 947.5, STR 24R. REMOVED TIE CLIP IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 62,304 hrs · 52,210 cycles

SUPPORT ANGLE CRACKED BETWEEN BS 344 TO BS 360, BETWEEN STR 25R TO STR 27R. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: WEB — CRACKED (NLG WW) · airframe 62,304 hrs · 52,210 cycles

RIGHT SIDE PANEL WEB OF THE NLG WHEEL WELL CRACKED BETWEEN BS 243.7 TO BS 251.6. REPAIRED WEB IAW EA AND EO.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 62,304 hrs · 52,210 cycles

STRINGER SPLICE CORRODED AT BS 984, STR 23R. REMOVED AND REPLACED SPLICE IAW SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,304 hrs · 52,210 cycles

SHEAR TIE CORRODED AT BS 947.5, BETWEEN STR 24L TO STR 26L. REMOVED AND REPLACED SHEAR TIE IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,304 hrs · 52,210 cycles

TIE CLIP CRACKED AT BS 787, STR 21R. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,304 hrs · 52,210 cycles

SHEAR TIE CORRODED AT BS 480, BETWEEN STR 27R AND STR 28R. REPAIRED SHEAR TIE IAW SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 62,304 hrs · 52,210 cycles

WEB CORRODED BETWEEN BS 907 TO BS 927, STR 17L. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: STRAP — CRACKED (FUSELAGE) · airframe 62,304 hrs · 52,210 cycles

STRAP CRACKED BETWEEN BS 312 TO BS 344, LBL 10.5. REMOVED AND REPLACED STRAP IAW SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,304 hrs · 52,210 cycles

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

Part: WEB — CORRODED (FUSELAGE) · airframe 62,304 hrs · 52,210 cycles

WEB LOWER SURFACE CORRODED BETWEEN BS 847 TO BS 867, STR 17L. REMOVED AND REPLACED WEB IAW SRM & DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 62,304 hrs · 52,210 cycles

FRAME CORRODED AT BS 500C, BTWEEN STR 28L AND STR 28R. REPAIRED FRAME IAW SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 62,304 hrs · 52,210 cycles

STRAP CRACKED BETWEEN BS 312 TO BS 344, BL 0. REMOVED AND REPLACED STRAP IAW SRM AND DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 62,304 hrs · 52,210 cycles

WEB CORRODED BETWEEN BS 927 TO BS 947.5, STR 21L. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,304 hrs · 52,210 cycles

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

Part: SKIN — CRACKED (RUDDER) · airframe 62,304 hrs · 52,210 cycles

LEFT EXTERNAL SKIN OF RUDDER CRACKED AT LEVEL OF FIN WL 107.09+7. REPAIRED SKIN IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,304 hrs · 52,210 cycles

TIE CLIP CRACKED AT BS 727D, STR 20L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 62,304 hrs · 52,210 cycles

FRAME CORRODED AT BS 500B, BETWEEN STR 27R AND STR 28R. REPAIRED FRAME IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,304 hrs · 52,210 cycles

TIE CLIP CRACKED AT BS 787, STR 22R. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 62,304 hrs · 52,210 cycles

AFT CARGO COMPARTMENT TRACK CORRODED AT BS 860, RBL 13.80. REPAIRED TRACK IAW EA AND EO.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,304 hrs · 52,210 cycles

SHEAR TIE CORRODED AT BS 500, BETWEEN STR 27L AND STR 28L. REPAIRED SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,304 hrs · 52,210 cycles

SHEAR TIE CORRODED AT BS 500, BETWEEN STR 28L AND STR 28R. REPAIRED SHEAR TIE IAW SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 62,304 hrs · 52,210 cycles

CHANNEL CORRODED AT BS 860, RBL 3.0. REPAIRED CHANNEL IAW EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,304 hrs · 52,210 cycles

SHEAR TIE CORRODED AT BS 500, BETWEEN STR 27R AND STR 28R. REPAIRED FRAME IAW SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 62,304 hrs · 52,210 cycles

STRINGER CORRODED AT BS 965, STR 26R. REPAIRED STRINGER IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,304 hrs · 52,210 cycles

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

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,304 hrs · 52,210 cycles

TIE CLIP CRACKED AT BS 727B, STR 21L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 62,304 hrs · 52,210 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,304 hrs · 52,210 cycles

FRAME CRACKED AT BS 500B, BETWEEN STR 20L AND STR 21L. REPAIRED FRAME IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 62,304 hrs · 52,210 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 727B, RBL 24.8. REPAIRED BEAM IAW EA AND EO.

Part: FRAME — CORRODED (FUSELAGE) · airframe 62,304 hrs · 52,210 cycles

FRAME CORRODED AT BS 847 BETWEEN, STR 27L AND STR 27R. REPAIRED FRAME IAW EO AND EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,304 hrs · 52,210 cycles

FRAME CRACKED AT BS 500C, BETWEEN STR 20R AND STR 21R. REPAIRED FRAME IAW EO AND EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,304 hrs · 52,210 cycles

FRAME CRACKED AT BS 520, BETWEEN STR 20L TO STR 21L. REPAIRED FRAME IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 62,304 hrs · 52,210 cycles

WEB SUPPORT ANGLE CRACKED AT BS 380, STR 26L. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,304 hrs · 52,210 cycles

SKIN CRACKED BETWEEN BS 727D TO BS 727E, BETWEEN STR 27R TO STR 27L. REPAIRED SKIN IAW EA AND EO.

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 62,304 hrs · 52,210 cycles

FRAME CRACKED AT BS 845, AROUND STOP FITTING 5 OF THE AFT CARGO DOOR. REMOVED AND REPLACED AFT CARGO DOOR IAW AMM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 62,304 hrs · 52,210 cycles

FRAME CORRODED AT BS 907, BETWEEN STR 27R TO STR 27L. REPAIRED FRAME IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 62,304 hrs · 52,210 cycles

FRAME CORRODED AT BS 767, BETWEEN STR 26L TO STR 27L. REPAIRED FRAME IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,304 hrs · 52,210 cycles

TIE CLIP CRACKED AT BS 727A, STR 20L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 62,304 hrs · 52,210 cycles

FRAME CORRODED AT BS 927, BETWEEN STR 27R TO STR 27L. REPAIRED FRAME IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 62,304 hrs · 52,210 cycles

FRAME CORRODED AT BS 767, BETWEEN STR 27R TO STR 27L. REPAIRED FRAME IAW SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 62,304 hrs · 52,210 cycles

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

Part: FRAME — CORRODED (FUSELAGE) · airframe 62,304 hrs · 52,210 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,304 hrs · 52,210 cycles

BASE OF ANTENNA CRACKED BETWEEN BS 727D TO BS 727E STR 27L TO STR 27R IN AFT CARGO COMPARTMENT. REMOVED AND REPLACED SKIN IAW EA.

Part: CABLE — DAMAGED (R1 DOOR) · airframe 62,304 hrs · 52,210 cycles

R1 DOOR EMERGENCY EVAC SLIDE CABLE DAMAGED. REMOVED AND REPLACED CABLE IAW SRM.

Part: CABLE — DAMAGED (L1 DOOR) · airframe 62,304 hrs · 52,210 cycles

L1 DOOR EMERGENCY EVAC SLIDE CABLE DAMAGED. REMOVED AND REPLACED CABLE IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,304 hrs · 52,210 cycles

R1 DOOR AFT LOWER CUTOUT CORNER CRACKED. REPAIRED SKIN IAW EO.

Part: SLAT — DELAMINATED (LT WING) · airframe 62,304 hrs · 52,210 cycles

LEFT WING NR 1 SLAT DELAMINATED ON INBOARD EDGE. REPAIRED SLAT IAW SRM.

Part: SLAT — DELAMINATED (LT WING) · airframe 62,304 hrs · 52,210 cycles

LEFT WING NR 2 SLAT DELAMINATED ON INBOARD EDGE. REPAIRED SLAT IAW SRM.

Part: SLAT — DELAMINATED (LT WING) · airframe 62,304 hrs · 52,210 cycles

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

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 62,303 hrs · 52,210 cycles

RIGHT FUSELAGE AFT EMERGENCY LIGHT INOP. REMOVED & REPLACED BATTERY PACK PER AMM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,155 hrs · 52,082 cycles

FUSELAGE FRAME CRACK AT BS 932, STR 25R. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,071 hrs · 52,023 cycles

FUSELAGE SKIN CRACKED AT BS 344 + 3, STR 2L. REPAIRED SKIN PER SRM & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,954 hrs · 51,931 cycles

SKIN CRACKED AT BS 727E+3, STR 2R. REPAIRED SKIN PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 61,704 hrs · 51,736 cycles

STRINGER CRACKED AT BS 219.8, STR 27R. REPAIRED STRINGER PER ER AND EA.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 61,704 hrs · 51,736 cycles

STIFFENER CORRODED AT BS 227.8, LBL 3. REMOVED AND REPLACED STIFFENER IAW SRM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 61,704 hrs · 51,736 cycles

RIGHT WING I/B FORE FLAP UPPER SURFACE DELAMINATED. REPAIRED FORE FLAP PER SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 61,700 hrs · 51,734 cycles

RIGHT AFT EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 61,700 hrs · 51,734 cycles

RIGHT EMERGENCY EXIT AISLE LIGHTS INOP AT ROW 23. REMOVED AND REPLACED BATTERY PACK PER AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 61,700 hrs · 51,734 cycles

RIGHT AFT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 61,700 hrs · 51,734 cycles

LEFT EMERGENCY EXIT AISLE LIGHTS INOP AT ROW 21. REMOVED AND REPLACED BATTERY PACK PER AMM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 61,538 hrs · 51,606 cycles

L2 EXTERIOR EMERGENCY EXIT LIGHT INOP. CHARGED BATTERY PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 61,538 hrs · 51,606 cycles

L2 DOOR EMERGENCY LIGHT INOP. CHARGED EXIT LIGHT BATTERY PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 61,538 hrs · 51,606 cycles

EMERGENCY LIGHT ABOVE ROW 20 & 23 INOP. CHARGED BATTERY PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,538 hrs · 51,606 cycles

BS 616 RT LOWER FRAME INNER CHORD CRACKED AT FWD SIDE OF FRAME. REPAIRED FRAME PER EA.

Part: ATTACH FITTING — BROKEN (NR 4 SPOILER) · airframe 61,430 hrs · 51,520 cycles

LT WING NR 4 GROUND SPOILER ATTACH FITTING BROKEN. REMOVED AND REPLACED SPOILER PER MM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 61,296 hrs · 51,408 cycles

BS 616 RT FLOORBEAM CRACKED ON INNER CHORD. REPLACED BEAM IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,965 hrs · 50,415 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED BETWEEN BS 966 TO BS 968, STR 21L. REPAIRED SKIN IAW ER AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,965 hrs · 50,415 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 443, STR 2R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,965 hrs · 50,415 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 424, STR 1R. REPAIRED SKIN IAW ER.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 59,965 hrs · 50,415 cycles

DURING SCHEDULED OTS CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED. REPAIRED SKIN IAW ER AND EA.

Part: BATTERY — DISCHARGED (CABIN) · airframe 59,965 hrs · 50,415 cycles

DURING SCHEDULED OTS CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,961 hrs · 50,414 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND SKIN CRACKED AT BS 443, STR 2R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,961 hrs · 50,414 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND SKIN CRACKED AT BS 447, STR 2R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (HORIZSTAB) · airframe 59,961 hrs · 50,414 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,961 hrs · 50,414 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND SKIN CRACKED AT BS 454, STR 2R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,961 hrs · 50,414 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND SKIN CRACKED AT BS 424, STR 1. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,961 hrs · 50,414 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND SKIN CRACKED AT BS 454, STR 1. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,451 hrs · 47,166 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 852, STR 4R. REPAIRED SKIN PER ER AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,451 hrs · 47,166 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 467, STR 1. REPAIRED SKIN PER ER AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,451 hrs · 47,166 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 510A, STR 6R. REPAIRED SKIN PER ER AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,451 hrs · 47,166 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 852, STR 1. REPAIRED SKIN PER ER AND EA.

Part: TAB — DELAMINATED (AILERON) · airframe 584,884 hrs · 49,290 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING AILERON TAB DELAMINATED AT T/E. REMOVED AND REPLACED TAB PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 58,484 hrs · 49,290 cycles

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

Part: WINDOW — LOOSE (EVAC SLIDE) · airframe 58,484 hrs · 49,290 cycles

DURING SCHEDULED HC1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE GAUGE WINDOW LOOSE. REMOVED AND REPLACED WINDOW PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,389 hrs · 48,458 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 7R. REMOVED AND REPLACED CLIP PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 57,389 hrs · 48,458 cycles

DURING SCHEDULED SPV CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 670, RBL 24.5. REPAIRED BEAM PER EA.

Part: WIRE — BROKEN (CABIN) · airframe 57,389 hrs · 48,458 cycles

DURING SCHEDULED SPV CHECK, FOUND R1 DOOR EMERGENCY EXIT SIGN INOP. REPAIRED LIGHT WIRING PER WDM.

Part: FLAP — CHAFED (LT WING) · airframe 57,389 hrs · 48,458 cycles

DURING SCHEDULED SPV CHECK, FOUND LT WING O/B MID FLAP CHAFED. REPAIRED MID FLAP PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,389 hrs · 48,458 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 2R. REMOVED AND REPLACED CLIP PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,389 hrs · 48,458 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 1. REMOVED AND REPLACED CLIP PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,389 hrs · 48,458 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 3R. REMOVED AND REPLACED CLIP PER EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 57,389 hrs · 48,458 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 727D, BETWEEN STR 13R TO STR 14R. REMOVED AND REPLACED SHEAR TIE PER SRM AND BAC DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 57,389 hrs · 48,458 cycles

DURING SCHEDULED SPV CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 672, RBL 24.5. REPAIRED BEAM PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,389 hrs · 48,458 cycles

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

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 57,389 hrs · 48,458 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 520, BETWEEN STR 11R TO STR 13R. REMOVED AND REPLACED SHEAR TIE PER SRM AND BAC DWG.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 57,389 hrs · 48,458 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED AT BS 358, STR 14L. REMOVED AND REPLACED STRINGER PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,389 hrs · 48,458 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,389 hrs · 48,458 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 520, BETWEEN STR 20R TO STR 21R. REPAIRED FRAME PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 57,389 hrs · 48,458 cycles

DURING SCHEDULED SPV CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 665.75, LBL 24.5. REPAIRED CHORD PER EA.

Part: FLAP — CHAFED (RT WING) · airframe 57,389 hrs · 48,458 cycles

DURING SCHEDULED SPV CHECK, FOUND RT WING O/B FORE FLAP CHAFED. REPAIRED FORE FLAP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,389 hrs · 48,458 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 762, STR 4R. REPAIRED SKIN PER SRM.

Part: LIGHT — LOOSE (CABIN) · airframe 56,782 hrs · 47,975 cycles

DURING SCHEDULED MV2 CHECK, FOUND EEPLS LOOSE AT ROW 8. SECURED EEPLS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,585 hrs · 47,826 cycles

DURING SCHEDULED HC1 CHECK, FOUND SKIN CRACKED AT BS 769, STR 10R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,585 hrs · 47,826 cycles

DURING SCHEDULED HC1 CHECK, FOUND SKIN CRACKED AT BS 444.5, STR 10L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,585 hrs · 47,826 cycles

DURING SCHEDULED HC1 CHECK, FOUND SKIN CRACKED AT BS 791, STR 10L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,585 hrs · 47,826 cycles

DURING SCHEDULED HC1 CHECK, FOUND SKIN CRACKED AT BS 744E, STR 10R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,585 hrs · 47,826 cycles

DURING SCHEDULED HC1 CHECK, FOUND SKIN CRACKED AT BS 764, STR 10R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,585 hrs · 47,826 cycles

DURING SCHEDULED HC1 CHECK, FOUND SKIN CRACKED AT BS 785, STR 10R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,585 hrs · 47,826 cycles

DURING SCHEDULED HC1 CHECK, FOUND SKIN CRACKED AT BS 464.5, STR 10L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,343 hrs · 47,636 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 372, STR 15L. REPAIRED SKIN PER EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 56,339 hrs · 47,635 cycles

DURING SCHEDULED MV2 CHECK, FOUND SHEAR TIE CRACKED AT BS 400, BETWEEN STR 16L TO STR 17L. REPAIRED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,339 hrs · 47,635 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED BETWEEN BS 372 TO BS 379, STR 15L. REPAIRED SKIN PER ER.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 56,339 hrs · 47,635 cycles

DURING SCHEDULED MV2 CHECK, FOUND SHEAR TIE CRACKED AT BS 400, BETWEEN STR 15L TO STR 16L. REPAIRED SHEAR TIE PER SRM.

Part: LIGHT — WORN (CABIN) · airframe 55,791 hrs · 47,218 cycles

DURING SCHEDULED CV CHECK, FOUND RT EEPLS WORN AT ROW 12. REMOVED AND REPLACED EEPLS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,791 hrs · 47,218 cycles

DURING SCHEDULED CV CHECK, FOUND SKIN CRACKED AT BS 394, STR 10L. REPAIRED SKIN PER EA.

Part: PRIORITY VALVE — FAULTY (LT MLG) · airframe 55,757 hrs · 47,190 cycles

LEFT MLG WOULD NOT COME DOWN VIA GEAR HANDLE. MANUALLY EXTENDED MAIN GEAR THEN RECEIVED THREE DOWN AND LOCKED INDICATIONS. CYCLING OF NORMAL GEAR HANDLE DID NOT WORK. REMOVED AND REPLACED MLG PRIORITY MODULAR VALVE AND UPLOCK ACTUATOR PER MM.

Part: SELECTOR VALVE — FAULTY (LT MLG) · airframe 55,513 hrs · 47,018 cycles

LT MLG INDICATED UNSAFE (RED LIGHT) ON FINAL APPROACH. RAN CHECKLIST/MANUAL EXTENSION OF ALL 3 GEARS WORKED NORMALLY. REMOVED AND REPLACED LT MLG SELECTOR VALVE AND ADJUSTED LT MLG CONTROL CABLES PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 55,253 hrs · 46,817 cycles

DURING SCHEDULED SPV CHECK, FOUND RT LOWER EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LAMP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,093 hrs · 46,705 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 731B, STR 4R. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,093 hrs · 46,705 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 435, STR 1. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (LT WING) · airframe 55,096 hrs · 46,706 cycles

DURING SCHEDULED SPV CHECK, FOUND LT WING L/E SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,093 hrs · 46,705 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 508D, STR 10L. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,093 hrs · 46,705 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 506D, STR 15L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,093 hrs · 46,705 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 937, STR 24L. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,093 hrs · 46,705 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 740B, STR 4R. REPAIRED SKIN PER ER.

Part: FLAP — DELAMINATED (RT WING) · airframe 55,093 hrs · 46,705 cycles

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

Part: FLAP — DELAMINATED (LT WING) · airframe 55,093 hrs · 46,705 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND LT WING I/B FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 55,093 hrs · 46,705 cycles

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

Part: FLAP — DELAMINATED (RT WING) · airframe 55,093 hrs · 46,705 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND RT WING I/B FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,444 hrs · 46,224 cycles

DURING SCHEDULED CV CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR LOWER CUTOUT. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,591 hrs · 45,598 cycles

DURING SCHEDULED BC2 CHECK, FOUND SKIN CRACKED AT BS 727C, STR 4R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,591 hrs · 45,598 cycles

DURING SCHEDULED BC2 CHECK, FOUND SKIN CRACKED AT BS 910, STR 23R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,591 hrs · 45,598 cycles

DURING SCHEDULED BC2 CHECK, FOUND SKIN CRACKED AT BS 500, STR 16L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,591 hrs · 45,598 cycles

DURING SCHEDULED BC2 CHECK, FOUND SKIN CRACKED AT BS 727D, STR 4R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,579 hrs · 45,589 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND SKIN CRACKED AT BS 500, STR 16L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,579 hrs · 45,589 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND SKIN CRACKED AT BS 727D, STR 4R. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 53,579 hrs · 45,589 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,579 hrs · 45,589 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND SKIN CRACKED AT BS 727C, STR 4R. REPAIRED SKIN PER SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 52,398 hrs · 44,743 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,354 hrs · 44,709 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 303, L1 DOOR LOWER FWD HINGE CUTOUT. REPAIRED SKIN PER EA.

Part: CASTING — CRACKED (FUSELAGE) · airframe 52,354 hrs · 44,709 cycles

DURING SCHEDULED 16Y CHECK, FOUND L1 DOOR LOWER HINGE CASTING CRACKED. REMOVED AND REPLACED HINGE CASTING PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,354 hrs · 44,709 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 940-944, STRINGER 24L. REPAIRED SKIN PER EA.

Part: BATTERY — DISCHARGED (CABIN) · airframe 52,354 hrs · 44,709 cycles

DURING SCHEDULED 16Y CHECK, FOUND MID CABIN EMERGENCY EGRESS LIGHTS INOP. REMOVED AND REPLACED LIGHTS BATTERY PER MM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 52,354 hrs · 44,709 cycles

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

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 52,354 hrs · 44,709 cycles

DURING SCHEDULED 16Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 727A, LBL 45. REPAIRED BEAM PER AAR EA.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 62,354 hrs · 44,709 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM ATTACH FITTING CRACKED AT BS 540, RBL 32. REMOVED AND REPLACED FITTING PER SRM.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 62,354 hrs · 44,709 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM ATTACH FITTING CRACKED AT BS 540, LBL 32. REMOVED AND REPLACED FITTING PER SRM.

Part: LUG — BROKEN (SPOILER) · airframe 52,354 hrs · 44,709 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING NR 4 SPOILER SECOND FROM THE OTBD LUG BROKEN. REMOVED AND REPLACED SPOILER PER MM.

Part: SLAT — DELAMINATED (LT WING) · airframe 52,354 hrs · 44,709 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING NR 3 SLAT DELAMINATED AT AFT INBD CORNER. REPAIRED SLAT PER SRM.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 62,354 hrs · 44,709 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM ATTACH FITTING CRACKED AT BS 540, LBL 39. REMOVED AND REPLACED FITTING PER SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 52,354 hrs · 44,709 cycles

DURING SCHEDULED 16Y CHECK, FOUND LOWER FUSELAGE Z ANGLE CORRODED BETWEEN BS 767 TO BS 797, RBL 24. R&R ANGLE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,354 hrs · 44,709 cycles

DURING SCHEDULED 16Y CHECK, FOUND NOSE WHEEL WELL WEB SKIN CRACKED BETWEEN RT AND LT SNUBBER SPRING. REPAIRED SKIN PER ACO.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 52,354 hrs · 44,709 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT CREASE BEAM CORRODED BETWEEN BS 313 TO BS 324. REPAIRED BEAM PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 52,354 hrs · 44,709 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CORRODED BETWEEN BS 257 TO BS 259, BETWEEN LBL 57 TO LBL 59. REMOVED AND REPLACED BEAM PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 52,354 hrs · 44,709 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CORRODED AT BS 228, BETWEEN LBL 51 TO LBL 53. R&R BEAM PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 52,354 hrs · 44,709 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT CREASE BEAM CORRODED AT BS 895, STR 17L. REPLACED CREASE BEAM PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 52,354 hrs · 44,709 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT GALLEY DOOR CREASE BEAM CORRODED BETWEEN BS 947 TO BS 1008. REMOVED AND REPLACED BEAM PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,354 hrs · 44,709 cycles

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

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 52,354 hrs · 44,709 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT CREASE BEAM CORRODED AT BS 230. REMOVED AND REPLACED BEAM PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,354 hrs · 44,709 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, RBL 21. REMOVED AND REPLACED CLIP PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 52,354 hrs · 44,709 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT CREASE BEAM CORRODED AT BETWEEN BS 233 TO BS 307. REPAIRED BEAM PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 52,354 hrs · 44,709 cycles

DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM CORRODED BETWEEN BS 777 TO BS 784, STR 17R. REMOVED AND REPLACED BEAM PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,354 hrs · 44,709 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED BETWEEN BS 249 TO BS 250, BETWEEN STR 12R TO STR 13R. REMOVED AND REPLACED FRAME PER SRM.

Part: LENS — FADED (CABIN) · airframe 52,354 hrs · 44,709 cycles

DURING SCHEDULED 16Y CHECK, FOUND FWD LT LOWER CEILING PANEL EMERGENCY EXIT LIGHT LENS FADED. REMOVED AND REPLACED LENS PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 52,354 hrs · 44,709 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT SIDEWALL PANEL EMERGENCY EXIT LIGHT BASE BROKEN AT ROW 9. REMOVED AND REPLACED LIGHT PER MM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 52,354 hrs · 44,709 cycles

DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM CORRODED AT BS 727B, STR 17R. REMOVED AND REPLACED BEAM PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,354 hrs · 44,709 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 25R. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,354 hrs · 44,709 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 52,354 hrs · 44,709 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT AFT CREASE BEAM CORRODED BETWEEN BS 950 TO BS 990, WL 208. REPAIRED BEAM PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,354 hrs · 44,709 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,354 hrs · 44,709 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,354 hrs · 44,709 cycles

DURING SCHEDULED 16Y CHECK, FOUND FWD CARGO PIT FRAME CRACKED AT BS 500, BETWEEN RBL 1 TO RBL 5. REPAIRED FRAME PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 52,354 hrs · 44,709 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CRACKED AT BS 727E, STR 24L. REPAIRED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,354 hrs · 44,709 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 25R. R&R CLIP PER SRM.

Part: DOOR FRAME — CRACKED (AFT CARGO DOOR) · airframe 52,080 hrs · 44,522 cycles

DURING SCHEDULED HC2 CHECK, FOUND AFT CARGO DOOR FWD LOWER FRAME CRACKED. REMOVED AND REPLACED DOOR PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,546 hrs · 44,144 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 927, STR 25R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,546 hrs · 44,144 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 500C + 4, STR 15R. REPAIRED PER SWA EA.

Part: FAN — FAULTY (E&E BAY) · airframe 51,269 hrs · 43,947 cycles

AIR TURNBACK / DECLARED EMERGENCY. FLIGHT CREW REPORTED SMOKE IN CABIN. INSPECTED AIRCRAFT, FOUND GASPER FAN FAULTY. REMOVED AND REPLACED GASPER FAN PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 50,425 hrs · 43,355 cycles

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

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 50,356 hrs · 43,310 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,356 hrs · 43,310 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA.

Part: WEDGE — DELAMINATED (LT WING TE FLAP) · airframe 50,356 hrs · 43,310 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT WING INBOARD MID FLAP WEDGE DELAMINATED AT INBOARD END. REMOVED AND REPLACED WEDGE PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 50,356 hrs · 43,310 cycles

DURING SCHEDULED HC1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SKIN — CRACKED (BS 504 S15L) · airframe 49,473 hrs · 42,666 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 504C, STR 15L. REPAIRED SKIN PER SWA EA.

Part: LENS — LOOSE (CABIN) · airframe 49,091 hrs · 42,382 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,013 hrs · 42,331 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 48,966 hrs · 42,295 cycles

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

Part: SKIN — CRACKED (BS 733A S4R) · airframe 48,704 hrs · 42,098 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 733A, STR 4R. REPAIRED SKIN PER ER.

Part: SKIN — CORRODED (BS 957 S27L) · airframe 48,680 hrs · 42,081 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 957, STR 27L. REPAIRED SKIN PER ER.

Part: STRINGER — CORRODED (BS 960-967) · airframe 48,677 hrs · 42,079 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER 27L CORRODED BETWEEN BS 960 AND BS 967. REPAIRED STRINGER PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,677 hrs · 42,079 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,677 hrs · 42,079 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,677 hrs · 42,079 cycles

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

Part: RIB — CRACKED (NR 2 INLET) · airframe 48,677 hrs · 42,079 cycles

DURING SCHEDULED 14Y CHECK, FOUND NR 2 ENGINE INLET FWD BULKHEAD RIB CRACKED AT 10 O'CLOCK POSITION. REMOVED AND REPLACED BULKHEAD RIB PER SRM.

Part: RIB — CRACKED (NR 2 INLET) · airframe 48,677 hrs · 42,079 cycles

DURING SCHEDULED 14Y CHECK, FOUND NR 2 ENGINE INLET FWD BULKHEAD RIB CRACKED AT 2 O'CLOCK POSITION. REMOVED AND REPLACED BULKHEAD RIB PER SRM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 48,677 hrs · 42,079 cycles

DURING SCHEDULED 14Y CHECK, FOUND RT WING OUTBOARD FORE FLAP INBOARD END DELAMINATED. REPAIRED FLAP PER SRM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 48,621 hrs · 42,041 cycles

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

Part: FLAP — DELAMINATED (LT WING) · airframe 48,439 hrs · 41,908 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,439 hrs · 41,908 cycles

DURING SCHEDULED C2 CHECK, FOUND L2 FUSELAGE SKIN CRACKED AT LOWER HINGE CUTOUT LOWER END. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 519 S12L) · airframe 47,836 hrs · 41,425 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 519, STR 12L. REPAIRED SKIN PER SWA EA.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 47,658 hrs · 41,279 cycles

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

Part: SKIN — DELAMINATED (NR 5 SLAT) · airframe 46,479 hrs · 40,349 cycles

DURING SCHEDULED C4 CHECK, FOUND RT WING NR 5 L/E SLAT T/E WEDGE UPPER SURFACE DELAMINATED AT OUTBOARD END. REMOVED AND REPLACED SLAT PER MM.

Part: SKIN — DELAMINATED (NR 4 SLAT) · airframe 46,479 hrs · 40,349 cycles

DURING SCHEDULED C4 CHECK, FOUND RIGHT WING NR 4 L/E SLAT T/E WEDGE UPPER SURFACE DELAMINATED AT OUTBOARD END. REMOVED AND REPLACED SLAT PER MM.

Part: SKIN — DELAMINATED (RT WING FOREFLAP) · airframe 46,479 hrs · 40,349 cycles

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

Part: FRAME — CRACKED (BS 303 S16L) · airframe 45,420 hrs · 39,538 cycles

DURING SCHEDULED SPV CHECK, FOUND L1 DOOR FRAME CRACKED AT BS 303.9, STR 16L. REPAIRED FRAME SECTION PER EA.

Part: SKIN — CORRODED (BS 492 S28R) · airframe 45,410 hrs · 39,528 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN BEAR STRAP CORRODED AT BS 492, STR 28R. REPAIRED BEAR STRAP PER EA.

Part: SKIN — CRACKED (BS 515 S12R) · airframe 44,556 hrs · 38,857 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 515, STR 12R. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 44,556 hrs · 38,857 cycles

DURING SCHEDULED C2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: BALLAST — INOPERATIVE (EMERGENCY LIGHT) · airframe 44,424 hrs · 38,760 cycles

DURING SCHEDULED A2 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BALLAST PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 43,566 hrs · 38,095 cycles

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

Part: DAMPER — SHEARED (RT MLG) · airframe 42,892 hrs · 37,574 cycles

SEVERE VIBRATION FELT FROM RIGHT MLG. FOUND RIGHT MLG SHIMMY DAMPER BOLT SHEARED BETWEEN TORSION LINKS. REMOVED AND REPLACED RIGHT MLG SHIMMY DAMPER ASSY, NR 3 & NR 4 BRAKE LINES, NR 3 & NR 4 MAIN BRAKE ASSY, NR 3 & NR 4 MAIN TIRE/WHEEL ASSY AND RT MLG UPPER & LOWER TORSION LINKS PER MM.

Part: LIGHT — MISSING (CABIN) · airframe 42,546 hrs · 37,304 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS STRIP MISSING AT ROW 7 ABC & ROW 16 DEF. INSTALLED EEPLS PER MM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 41,431 hrs · 36,430 cycles

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

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 40,942 hrs · 36,014 cycles

DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: GLOWSTRIP — LOOSE (CABIN) · airframe 40,925 hrs · 35,994 cycles

DURING SCHEDULED A1 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP LOOSE AT FWD END. REMOVED AND REPLACED STRIP PER MM.

Part: BATTERY — FAULTY (EMERGENCY LIGHT) · airframe 40,904 hrs · 35,979 cycles

DURING SCHEDULED RON CHECK, LT & RT AFT CABIN EMERGENCY LIGHTS STAY CONSTANTLY ON. REMOVED AND REPLACED BATTERY & CHARGER ASSY PER MM.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 40,740 hrs · 35,863 cycles

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

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 40,740 hrs · 35,863 cycles

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

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 40,740 hrs · 35,863 cycles

DURING SCHEDULED C2 CHECK, FOUND R1 DOOR EXTERNAL EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 40,706 hrs · 35,832 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BS 1016 AFT PRESS BULKHEAD WEB CRACKED AT STR 7R. REPAIRED BS 1016 AFT PRESS BULKHEAD WEB PER SWA EA.

Part: LIGHT — INOPERATIVE (L1 DOOR) · airframe 40,206 hrs · 35,422 cycles

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

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 39,896 hrs · 35,171 cycles

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

Part: COVER — WORN (EMERGENCY LIGHT) · airframe 37,202 hrs · 32,990 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS COVER AT ROW 11 ABC AND ROW 12 ABC, WORN. REMOVED AND REPLACED EEPLS COVER PER MM.

Part: SKIN — DELAMINATED (LT WING FLAP) · airframe 36,236 hrs · 32,201 cycles

DURING SCHEDULED C1 CHECK, FOUND LT WING OUTBOARD AFT T/E FLAP LOWER INBOARD CORNER DELAMINATED. REMOVED AND REPLACED OUTBOARD FLAP PER MM.

Part: SKIN — DELAMINATED (RT WING FOREFLAP) · airframe 36,236 hrs · 32,201 cycles

DURING SCHEDULED C1 CHECK, FOUND RT WING INBOARD T/E FOREFLAP DELAMINATED. REMOVED AND REPLACED INBOARD FOREFLAP PER MM.

Part: LIGHT — SEPARATED (ROW 8-10) · airframe 36,201 hrs · 32,172 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS FLOOR TRACK SEPARATED FROM ROW 8 TO ROW 10 LT SIDE. REMOVED AND REPLACED FLOOR TRACK PER MM.

Part: STRIP — WORN (CABIN) · airframe 35,190 hrs · 31,356 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIPS WORN, ROW NR 1 ABC TO ROW NR 8 ABC, ROW NR 1 DEF TO NR 6 DEF AND ROW NR 8 DEF TO ROW NR 11 DEF. REMOVED AND REPLACED EEPLS STRIPS PER MM.

Part: AILERON — DELAMINATED (LT WING) · airframe 34,102 hrs · 30,450 cycles

DURING SCHEDULED PM CHECK, FOUND LT AILERON DELAMINATED AT T/E. REMOVED AND REPLACED LEFT AILERON PER MM.

Part: SLIDE — DISLODGED (AFT PAX DOOR) · airframe 33,767 hrs · 30,182 cycles

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

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 32,656 hrs · 29,281 cycles

DURING SCHEDULED D CHECK, FOUND LT HORIZONTAL STAB CRACKED ON LOWER SKIN AT STA 125 JUST FWD OF REAR SPAR. REPAIRED SKIN PER BFG ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,656 hrs · 29,281 cycles

DURING SCHEDULED D CHECK, FOUND FWD CARGO DOOR CUTOUT FWD FRAME CRACKED AT # 5 DOOR STOP. REPAIRED DOOR FRAME PER SWA T1.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,656 hrs · 29,281 cycles

DURING SCHEDULED D CHECK, FOUND FWD CARGO DOOR CUTOUT AFT FRAME CRACKED AT NR 5 DOOR STOP. REPAIRED FRAME PER SWA T1.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,656 hrs · 29,281 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED LT/RT AT BS 188, WL 208. REMOVED AND REPLACED FRAMES PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 32,656 hrs · 29,281 cycles

DURING SCHEDULED D CHECK, FOUND CREASE BEAM WEB CORRODED AT LBL 70, BS 727A + 18 & BS 727B + 9. REMOVED AND REPLACED CREASE BEAM SECTION PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 31,662 hrs · 28,428 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD CRACKED AT BS 178, WL 188 AND RBL 1.0. REPAIRED BULKHEAD PER SRM.

Part: FLAP — DELAMINATED (LH WING) · airframe 28,694 hrs · 26,091 cycles

DURING SCHEDULED BC1 CHECK, FOUND LH WING OUTBD T/E AFT FLAP DELAMINATED AT INBD T/E. REPAIRED FLAP PER SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 25,863 hrs · 23,719 cycles

DURING SCHEDULED C2 CHECK, FOUND RT WING TRAILING EDGE INBD AFT FLAP DELAMINATED AT OTBD END. R&R FLAP ASSY PER MM.

Part: BULKHEAD — CRACKED (LT MLG WW) · airframe 24,934 hrs · 22,965 cycles

DURING SCHEDULED C1 CHECK, FOUND LT MLG W/W FWD BULKHEAD WITH 4 INCH LONG CRACK BEHIND A-SYS HYD PRESSURIZATION MODULE. REPAIRED BULKHEAD PER RA 1-353-2365.

Part: CONNECTOR — LOOSE (NR 2 ENGINE) · airframe 24,806 hrs · 22,856 cycles

ABORTED TAKEOFF. NR 2 ENGINE EGT INDICATOR ERRATIC. CLEANED AND SECURED NR 2 ENG EGT INDICATOR CONNECTOR D1208. OPS CHECK GOOD PER MM.

Part: CONNECTOR — DIRTY (EXIT LIGHT) · airframe 24,351 hrs · 22,478 cycles

AFT SERVICE DOOR EMERGENCY EXIT LIGHT BLINKING. CLEANED EXIT LIGHT CONNECTOR PER MM. OPS CHECK GOOD.

Part: FRAME — CRACKED (FUSELAGE) · airframe 24,322 hrs · 22,454 cycles

DURING SCHEDULED 1/4D CHECK, FOUND CRACKED BS 178 BULKHEAD LT AND RT SIDE CHORDS, LBL 28.5 AND RBL 28.5. REMOVED AND REPLACED SIDE CHORD SECTIONS PER ACO AND SWA RA.

Part: WINDOW POST — CRACKED (COCKPIT) · airframe 24,322 hrs · 22,454 cycles

DURING SCHEDULED 1/4D CHECK, FOUND CRACKED R1 UPPER O/B COCKPIT WINDOW POST. REPAIRED POST PER SWA RA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 24,313 hrs · 22,443 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD CRACKED AT LBL 6.5, RBL 6.5 AND LBL 5.5. REPAIRED SKIN PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 24,313 hrs · 22,443 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD CRACKED, RBL 5.5. REPAIRED BULKHEAD PER SRM.

Part: COVER — BROKEN (CABIN) · airframe 24,313 hrs · 22,443 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD ENTRY DOOR EMERGENCY EXIT LIGHT COVER BROKEN. R&R COVER PER MM.

Part: SKIN — CRACKED (SEVICE DOOR) · airframe 24,066 hrs · 22,240 cycles

DURING SCHEDULED C4 CHECK, FOUND FWD SERVICE DOOR LOWER HINGE CUT OUT CRACKED AROUND UPPER AFT CORNER. REPAIRED SKIN PER SWA RA NR 1-352-0374.

Part: GIRT BAR — OUT OF ADJ (ESCAPE SLIDE) · airframe 24,066 hrs · 22,240 cycles

DURING SCHEDULED C4 CHECK, FOUND FWD ENTRY DOOR EVACUATION SLIDE GIRT ASSY OUT OF ADJUST. REINSTALLED SLIDE ASSY PER MM.

Part: SLIDE — DISLODGED (PAX DOOR) · airframe 23,692 hrs · 21,895 cycles

FWD ENTRY DOOR EVACUATION SLIDE CAME OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM.

Part: INDICATOR — ERRATIC (COCKPIT)

AIR TURNBACK, IN FLIGHT ENG SHUT DOWN, NR 2 ENG EGT INDICATOR EXCEEDED LIMITS WITH THRUST LEVERS AT IDLE. REMOVED AND REPLACED NR 2 ENG EGT INDICATOR PER MM.

Part: BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED CHECK, FOUND R2 DOOR EMERGENCY LIGHT (INSIDE) AND L2 OUTSIDE EMERGENCY LIGHT AND LAST 6 FLOOR EMERGENCY LIGHTS TURN OFF AFTER APPROX 10 SEC. REMOVED AND REPLACED EMERGENCY BATTERY PACK AT AFT ENTRY LIGHT POSITION, OPS CHECK GOOD.

Part: FLOORBEAM — CORRODED (BS 947.5)

DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM CORROSION AT BS 947.5 RBL 54. REPAIRED PER BOEING SRM.

Part: AIR DISTRIBUTION — ODOR (CABIN)

RETURNED TO AUS DUE TO NAUSEA TYPE ODOR IN CABIN. INSPECTED AC SYSTEM, NO DEFECTS NOTED. REMOVED AND REPLACED WATER SEPARATORS PER BOEING M/M.

Part: SKIN — GOUGED (BS 380)

DURING SCHEDULED B1 CHECK, FOUND TWO GOUGES ON FUSELAGE SKIN AT BS 380, AT WL 208 AND 216. REPAIRED BOTH PER BOEING STRUCTURAL RPAIR MANUAL.