N520SW

Part: SKIN — CRACKED (LT WING) · airframe 72,260 hrs · 68,209 cycles

LEFT WING REAR SPAR WBL 163, UPPER CHORD FWD ROW OF FASTENERS CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,260 hrs · 68,209 cycles

FUSELAGE SKIN CRACKED, BETWEEN BS 380+12 - 380+14, STRINGER 1L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,260 hrs · 68,209 cycles

FUSELAGE SKIN CRACKED AT BS 520+4, STRINGER 8R. REPAIRED SKIN IAW EA.

Part: SLIDE — LOOSE (R2 DOOR) · airframe 71,899 hrs · 67,769 cycles

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

Part: SKIN — DELAMINATED (RT SPOILER) · airframe 71,186 hrs · 66,912 cycles

RIGHT WING NR 9 FLIGHT SPOILER UPPER SURFACE DELAMINATED. R & R SPOILER IAW MM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 70,904 hrs · 66,577 cycles

RIGHT ENTRY DOOR EMER EXIT SIGN LIGHT INOPERATIVE. R & R BULB IAW MM.

Part: LENS — MISSING (EXIT SIGN) · airframe 70,714 hrs · 66,348 cycles

RIGHT OVERWING EMER EXIT SIGN LENS MISSING. INSTALLED LENS IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,246 hrs · 65,791 cycles

AFT GALLEY EMER EXIT LIGHT INOPERATIVE. RELAMPED EXIT LIGHT IAW MM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 70,246 hrs · 65,791 cycles

STRINGER SPLICE CRACKED AT BS 908 STRINGER 6L. REPAIRED SPLICE IAW EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 70,246 hrs · 65,791 cycles

LEFT WING NR 2 SLAT SKIN CRACKED INBD SIDE. REPAIRED SKIN IAW SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 70,246 hrs · 65,791 cycles

CHANNEL STRINGER CRACKED AT BS 727 STRINGER 23R. R & R CHANNEL IAW SRM & DWG.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 70,246 hrs · 65,791 cycles

CHANNEL STRINGER CRACKED AT BS 727 STRINGER 23L. R & R CHANNEL IAW SRM & DWG.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 70,246 hrs · 65,791 cycles

SHEAR TIE CRACKED AT BS 520 STRINGER 17L. R & R SHEAR TIE IAW SRM & DWG.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 70,246 hrs · 65,791 cycles

STRINGER SPLICE CRACKED AT BS 908 STRINGER 4L. R & R SPLICE IAW EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 70,246 hrs · 65,791 cycles

LEFT WING NR 2 SLAT SKIN CRACKED. REPAIRED SKIN IAW SRM.

Part: LENS — BROKEN (CABIN) · airframe 70,246 hrs · 65,791 cycles

LEFT DOOR EMER EXIT LENS ON SIDEWALL BROKEN. R & R LENS IAW MM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 70,246 hrs · 65,791 cycles

TIE CLIP CRACKED AT BS 727B STRINGER 4R. R & R TIE CLIP IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 70,246 hrs · 65,791 cycles

TIE CLIP CRACKED AT BS 727C STRINGER 4R. R & R TIE CLIP IAW SRM & DWG.

Part: SKIN — CRACKED (RT WING) · airframe 70,246 hrs · 65,791 cycles

RIGHT WING STRUT ASSEMBLY SKIN PANEL CRACKED AT STATION 289. R & R SKIN IAW SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 70,246 hrs · 65,791 cycles

STRINGER CRACKED AT BS 747+16.5 STRINGER 23L. REPAIRED STRINGER IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,246 hrs · 65,791 cycles

FRAME CRACKED AT BS 827, STRINGER 20L. REPAIRED FRAME IAW EO & EA.

Part: SKIN — DEBONDED (TE FLAP) · airframe 70,246 hrs · 65,791 cycles

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

Part: SKIN — DELAMINATED (TE FLAP) · airframe 70,246 hrs · 65,791 cycles

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

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 70,246 hrs · 65,791 cycles

STRINGER SPLICE CHANNEL CRACKED AT BS 907 STRINGER 6L. R & R CHANNEL IAW EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 70,246 hrs · 65,791 cycles

STRINGER CRACKED AT BS 1006+4, STRINGER 4L. REPAIRED STRINGER IAW EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 70,246 hrs · 65,791 cycles

WEB CRACKED AT BS 520 + 10 BETWEEN STRINGER 24L TO 22L. R & R WEB IAW SRM & DWG.

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 70,246 hrs · 65,791 cycles

CENTER SCUFF PLATE CRACKED ON AFT CARGO COMPARTMENT DOOR CUT OUT. REPAIRED SCUFF PLATE IAW EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 70,246 hrs · 65,791 cycles

WEB CRACKED AT BS 520 + 10 BETWEEN STRINGER 24R TO 22R WING TO BODY FAIRING STRUCTURE. R & R WEB IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,246 hrs · 65,791 cycles

FRAME CRACKED AT BS 360 BETWEEN STRINGER 13R TO 14R. REPAIRED FRAME IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 70,246 hrs · 65,791 cycles

ANGLE CRACKED BETWEEN BS 685 TO 706 RBL 24.5. R & R ANGLE IAW SRM & DWG.

Part: LINK ASSY — CRACKED (R1 DOOR) · airframe 70,246 hrs · 65,791 cycles

R1 DOOR UPPER HINGE LINK TORQUE TUBE STRUCTURE CRACKED. R & R LINK ASSEMBLY IAW AMM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 70,246 hrs · 65,791 cycles

ANGLE CRACKED AT BS 747 BETWEEN STRINGER 27L TO 27R. R & R ANGLE IAW SRM & DWG.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 70,246 hrs · 65,791 cycles

STRINGER SPLICE CHANNEL CRACKED AT BS 360, STRINGER 5R. REPAIRED CHANNEL IAW EA.

Part: DRAIN — CRACKED (CARGO BAY) · airframe 70,246 hrs · 65,791 cycles

FORWARD CGO COMPARTMENT BASE OF DRAIN CRACKED BETWEEN BS 380 TO 400 BETWEEN STRINGER 28L TO 27L. R & R BASE IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 70,246 hrs · 65,791 cycles

ANGLE CRACKED AT BS 747 BETWEEN STRINGER 27R TO 27L. R & R ANGLE IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,246 hrs · 65,791 cycles

FRAME CRACKED AT BS 188 STRINGER 17R. REPAIRED FRAME IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 70,246 hrs · 65,791 cycles

ANGLE CRACKED AT BS 767 BETWEEN STRINGER 27R TO 27L. R & R ANGLE IAW SRM & DWG.

Part: PLATE — CRACKED (FUSELAGE) · airframe 70,246 hrs · 65,791 cycles

PLATE CRACKED AT BS 794 BETWEEN STRINGER 23R TO 24R. R & R PLATE IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 70,246 hrs · 65,791 cycles

TIE CLIP CRACKED AT BS 727C STRINGER 10L. R & R TIE CLIP IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 70,246 hrs · 65,791 cycles

TIE CLIP CRACKED AT BS 807 STRINGER 10L. R & R TIE CLIP IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 70,246 hrs · 65,791 cycles

ANGLE CRACKED AT BS 794 STRINGER 18R. R & R ANGLE IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 70,246 hrs · 65,791 cycles

ANGLE CRACKED AT BS 482B STRINGER 19L. R & R ANGLE IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 70,246 hrs · 65,791 cycles

SUPPORT ANGLE OF WEB CRACKED AT BS 400 STRINGER 26L. R & R ANGLE IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,246 hrs · 65,791 cycles

FUSELAGE SKIN UPPER LOBE CRACKED AT BS 400+15, STRINGER 1L. REPAIRED SKIN IAW EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 70,246 hrs · 65,791 cycles

ANGLE CRACKED AT BS 460 STRINGER 21L. R & R ANGLE IAW SRM & DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,246 hrs · 65,791 cycles

STRINGER CLIP CRACKED AT STATION 727A STRINGER 19L. R & R CLIP IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 70,246 hrs · 65,791 cycles

WEB CRACKED BETWEEN BS 360 TO BS 351.2, BETWEEN STRINGER 28R TO 28L. R & R WEB IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,246 hrs · 65,791 cycles

FRAME INNER CHORD CRACKED AT BS 847, STRINGER 14R AT 6 O'CLOCK. REPAIRED FRAME IAW EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,246 hrs · 65,791 cycles

STRINGER CLIP CRACKED AT STATION 907 STRINGER 18L. R & R CLIP IAW SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 70,246 hrs · 65,791 cycles

STRINGER CRACKED AT BS 380 STRINGER 15L. REPAIRED STRINGER IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 70,246 hrs · 65,791 cycles

TIE CLIP CRACKED AT BS 767 STRINGER 16R. R & R TIE CLIP IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 70,246 hrs · 65,791 cycles

TIE CLIP CRACKED AT BS 907 STRINGER 4R. R & R TIE CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,246 hrs · 65,791 cycles

STRINGER CLIP CRACKED AT STATION 482 STRINGER 16R. R & R CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,246 hrs · 65,791 cycles

STRINGER CLIP CRACKED AT STATION 420 STRINGER 16R. R & R CLIP IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,246 hrs · 65,791 cycles

FRAME CHORD CRACKED AT BS 348.2, STRINGER 16L. REPAIRED CHORD IAW EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 70,246 hrs · 65,791 cycles

SHEAR TIE CRACKED AT BS 597, STRINGER 17L. REPAIRED SHEAR TIE IAW EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 70,246 hrs · 65,791 cycles

STRINGER CRACKED AT BS 400 STRINGER 8L. REPAIRED STRINGER IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,246 hrs · 65,791 cycles

STRINGER CLIP CRACKED AT STATION 827 STRINGER 16R. R & R CLIP IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 70,246 hrs · 65,791 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,246 hrs · 65,791 cycles

FRAME INNER CHORD CRACKED AT BS 847, STRINGER 14R. REPAIRED CHORD IAW EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 70,246 hrs · 65,791 cycles

STRINGER CRACKED AT BS 887 STRINGER 4R. REPAIRED STRINGER IAW SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 70,246 hrs · 65,791 cycles

STRINGER SPLICE CHANNEL CRACKED AT BS 360, STRINGER 5R. R & R CHANNEL IAW EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 70,246 hrs · 65,791 cycles

TIE CLIP CRACKED AT BS 482 STRINGER 16L. R & R TIE CLIP IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,246 hrs · 65,791 cycles

FRAME CRACKED AT BS 380 STRINGER 16R. REPAIRED FRAME IAW SRM.

Part: RIB — CRACKED (LT WING) · airframe 70,246 hrs · 65,791 cycles

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

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 70,246 hrs · 65,791 cycles

TIE CLIP CRACKED AT BS 380 STRINGER 10R. R & R TIE CLIP IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 70,246 hrs · 65,791 cycles

TIE CLIP CRACKED AT BS 706 STRINGER 1. R & R TIE CLIP IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 70,246 hrs · 65,791 cycles

TIE CLIP CRACKED AT BS 827 STRINGER 4L. R & R TIE CLIP IAW SRM & DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,246 hrs · 65,791 cycles

FUSELAGE STRINGER CLIP CRACKED AT STATION 360 STRINGER 5L. R & R CLIP IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 70,246 hrs · 65,791 cycles

TIE CLIP CRACKED AT BS 440 STRINGER 4R. R & R TIE CLIP IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 70,246 hrs · 65,791 cycles

TIE CLIP CRACKED AT BS 727B STRINGER 7L. R & R TIE CLIP IAW SRM.

Part: CROSSBEAM — CRACKED (CARGO DOOR) · airframe 70,246 hrs · 65,791 cycles

CROSSBEAM E T CHORD CRACKED AROUND FASTENERS ON AFT END. REPAIRED T CHORD IAW EA.

Part: CROSSBEAM — CRACKED (CARGO DOOR) · airframe 70,246 hrs · 65,791 cycles

CROSS BEAM E TCHORD CRACKED AROUND FASTENERS ON FWD END. REPAIRED TCHORD IAW EA.

Part: ANGLE — CRACKED (RT HORIZ STAB) · airframe 70,246 hrs · 65,791 cycles

RIGHT HORIZONTAL STABILIZER ACCESS PANEL 9226R ANGLE CRACKED. R & R ANGLE IAW SRM.

Part: ANGLE — CRACKED (LT HORIZ STAB) · airframe 70,246 hrs · 65,791 cycles

LEFT HORIZONTAL STABILIZER ANGLE OF ACCESS PANEL 9126L CRACKED. R & R ANGLE IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,246 hrs · 65,791 cycles

SKIN CRACKED AT BS 482B + 13, STRINGER 16L. REPAIRED SKIN IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,246 hrs · 65,791 cycles

FRAME CRACKED AT BS 482B BETWEEN STRINGER 20L TO 21L. REPAIRED FRAME IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,246 hrs · 65,791 cycles

SKIN CRACKED AT BS 482B+12.5, STRINGER 16R. REPAIRED SKIN IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,246 hrs · 65,791 cycles

FUSELAGE FRAME CRACKED AT BS 482 BETWEEN STRINGER 20R TO 21R. REPAIRED FRAME IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,246 hrs · 65,791 cycles

SKIN CRACKED AT BS 908+ 4.75, STRINGER 4L. REPAIRED SKIN IAW EO & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,246 hrs · 65,791 cycles

SKIN CRACKED AT BS 482B+5.75, STRINGER 16R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,246 hrs · 65,791 cycles

SKIN CRACKED AT BS 767 + 2.750, STRINGER 23L. REPAIRED SKIN IAW EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 70,246 hrs · 65,791 cycles

SHEAR TIE CRACKED AT BS 597 STRINGER 17L. REPAIRED SHEAR TIE IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,246 hrs · 65,791 cycles

SKIN CRACKED AT BS 767+7, STRINGER 22L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,246 hrs · 65,791 cycles

SKIN CRACKED AT BS 400+13.750, STRINGER 1L. REPAIRED SKIN IAW EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 70,246 hrs · 65,791 cycles

SHEAR TIE CRACKED AT BS 597 STRINGER 17R. R & R SHEAR TIE IAW EA.

Part: FITTING — CRACKED (FUSELAGE) · airframe 70,246 hrs · 65,791 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,246 hrs · 65,791 cycles

SKIN CRACKED AT BS 747 + 12, STRINGER 21L. REPAIRED SKIN IAW EA.

Part: PANEL — CRACKED (NLG WW) · airframe 70,246 hrs · 65,791 cycles

NLG WW SIDE PANEL CRACKED AT BS 259.5 RBL 16. REPAIRED PANEL IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,246 hrs · 65,791 cycles

SKIN CRACKED AT BS 420+2.5, STRINGER 1L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,246 hrs · 65,791 cycles

FUSELAGE SKIN CRACKED AT BS 360 STRINGER 2R. REPAIRED SKIN IAW EO & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,246 hrs · 65,791 cycles

SKIN CRACKED AT BS 747 + 16.5 STRINGER 24L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,246 hrs · 65,791 cycles

SKIN CRACKED AT BS 767+12, STRINGER 22L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,246 hrs · 65,791 cycles

SKIN CRACKED AT BS 747 + 3, STRINGER 23L. REPAIRED SKIN IAW EA.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 70,246 hrs · 65,791 cycles

MAIN WW PRESS DECK WEB CRACKED AT BS 665 LBL 19.750. REPAIRED WEB IAW EA.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 70,246 hrs · 65,791 cycles

LEFT SIDE FWD LOWER CHORD CRACKED AT BS 727 STRINGER 18A AT 3 & 8 O'CLOCK. REPAIRED CHORD IAW EA.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 70,246 hrs · 65,791 cycles

LEFT SIDE AFT LOWER CHORD CRACKED AT BS 727 STRINGER 18A AT 9 O'CLOCK. REPAIRED CHORD IAW EA.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 70,246 hrs · 65,791 cycles

RIGHT SIDE AFT LOWER CHORD CRACKED AT BS 727 STRINGER 18A AT 8 O'CLOCK. REPAIRED CHORD IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,246 hrs · 65,791 cycles

SKIN CRACKED AT BS 482B+6, STRINGER 16R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,246 hrs · 65,791 cycles

FUSELAGE SKIN CRACKED AT BS 927 + 13.75 STRINGER 21R. REPAIRED SKIN IAW EA.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 70,246 hrs · 65,791 cycles

MAIN WW PRESS DECK WEB CRACKED AT BS 665 LBL 7.5. REPAIRED WEB IAW EA.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 70,246 hrs · 65,791 cycles

RIGHT SIDE FWD LOWER CHORD CRACKED AT BS 727 STRINGER 18A AT 3 & 9 O'CLOCK. REPAIRED CHORD IAW EA.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 70,246 hrs · 65,791 cycles

LEFT SIDE FWD UPPER CHORD CRACKED AT BS 727 STRINGER 18A AT 3 & 9 O'CLOCK. R & R CHORD IAW EA.

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 70,246 hrs · 65,791 cycles

FORWARD CARGO DOOR LOWER AFT EDGE FRAME CRACKED. REPAIRED FRAME IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,246 hrs · 65,791 cycles

SKIN CRACKED AT BS 747+3, STRINGER 23L. REPAIRED SKIN IAW EA.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 70,246 hrs · 65,791 cycles

RIGHT SIDE AFT UPPER CHORD CRACKED AT BS 727 STRINGER 18A AT 3 & 9 O'CLOCK. REPAIRED CHORD IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,246 hrs · 65,791 cycles

SKIN CRACKED AT BS 482B+14, STRINGER 16R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,246 hrs · 65,791 cycles

SKIN CRACKED AT BS 400+15, STRINGER 1L. REPAIRED SKIN IAW EA.

Part: HOUSING — CRACKED (FUSELAGE) · airframe 68,752 hrs · 64,169 cycles

R1 DOOR UPPER HINGE HOUSING CRACKED. R & R HOUSING IAW EA & ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,752 hrs · 64,169 cycles

FUSELAGE SKIN CRACKED BETWEEN BS 804.25 TO BS 805, STRINGER 24L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,752 hrs · 64,169 cycles

FUSELAGE SKIN CRACKED BETWEEN BS 346 TO BS 347, STRINGER 2L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,752 hrs · 64,169 cycles

FUSELAGE SKIN CRACKED BETWEEN BS 800 TO BS 800.8, STRINGER 22L. REPAIRED SKIN IAW SRM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 68,752 hrs · 64,169 cycles

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

Part: ANGLE — CRACKED (LT WING) · airframe 68,752 hrs · 64,169 cycles

LT WING NO STEP PANEL OTBD ANGLE CRACKED AT THE AFT END. REPAIRED ANGLE IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,752 hrs · 64,169 cycles

R1 DOOR FUSELAGE SKIN LOWER HINGE CUTOUT CRACKED AT BS 292. REPAIRED CUTOUT IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,752 hrs · 64,169 cycles

FUSELAGE SKIN CRACKED BETWEEN BS 804.5 TO BS 805.5, STRINGER 18L. REPAIRED SKIN IAW EA.

Part: FITTING — CRACKED (TE FLAP) · airframe 68,341 hrs · 63,747 cycles

RT WING MID FLAP INBD TORQUE TUBE SUPPORT INBD FITTING FWD LOWER HOLE CRACKED. R & R MID FLAP IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,341 hrs · 63,747 cycles

RT OVERWING EMERGENCY EXIT INTERIOR LOWER LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,341 hrs · 63,747 cycles

FRAME CRACKED AT BS 520, BETWEEN STRINGER 20R & 21R. R & R FRAME IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,341 hrs · 63,747 cycles

FRAME CRACKED AT STATION 847, STRINGER 20R. REPAIRED FRAME IAW ACO.

Part: DOOR FRAME — CRACKED (R1 DOOR) · airframe 68,208 hrs · 63,616 cycles

R1 DOOR CRACKED LOWER EDGE FRAME AT LOWER AFT CORNER STOP FITTING. R & R DOOR IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,965 hrs · 63,348 cycles

FS SKIN CRACKED AT BS 400+3 STRINGER 16R. REPAIRED SKIN IAW EA.

Part: LIGHT — OUT OF POSITION (CABIN) · airframe 67,610 hrs · 62,947 cycles

LT EMERGENCY EXIT LIGHT STRIP OUT OF POSITION AT ROW 6. REPOSITIONED STRIP IAW SIP.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 67,312 hrs · 62,618 cycles

FORWARD LT EMERGENCY LIGHT BATTERY PACK CAPACITY LOW. R & R BATTERY PACK ASSY IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 67,312 hrs · 62,618 cycles

FLIGHT DECK EMERGENCY EXIT LIGHT INOP. R & R BATTERY PACK IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,312 hrs · 62,618 cycles

SKIN CRACKED AT BS 425, STR 1L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,312 hrs · 62,618 cycles

SKIN CRACKED AT BS 444, STR 1L. REPAIRED SKIN IAW SRM AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,312 hrs · 62,618 cycles

SKIN CRACKED AT BS 444, STR 1L. REPAIRED SKIN IAW EA & SRM.

Part: COVER — MISSING (CABIN) · airframe 66,444 hrs · 61,724 cycles

BIN 13F EMERGENCY EXIT LIGHT ON BIN MISSING. INSTALLED LIGHT LENS COVER PER M/M.

Part: LENS — LOOSE (CABIN) · airframe 66,404 hrs · 61,682 cycles

EMERGENCY EXIT BULL NOSE LIGHT AT ROW 13 DEF LENS LOOSE. SECURED LENS PER MM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 65,820 hrs · 61,082 cycles

TIE CLIP CRACKED AT BS 927, STR 24L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 65,820 hrs · 61,082 cycles

TIE CLIP CRACKED AT BS 967, STR 19L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: SHROUD — CRACKED (APU BAY) · airframe 65,820 hrs · 61,082 cycles

CRACK ON APU UPPER SHROUD INLET SIDE. REPLACED SHROUD INLET SIDE ON APU IAW SRM B737-500 51-10-02 ITEM 8 AND REMOVE AND RE-INSTALLED FASTENER AS PER SRM B737-500 51-40-02 AND DRAWING #65-68910.

Part: WEB — CRACKED (FUSELAGE) · airframe 65,820 hrs · 61,082 cycles

WEB CRACKED BETWEEN BS 927 + 10 TO BS 951, BETWEEN STR 11L AND STR 14L. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,820 hrs · 61,082 cycles

FRAME CRACKED AT BS 951, BETWEEN STR 11L TO STR 7L. REMOVED AND REPLACED FRAME IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 65,820 hrs · 61,082 cycles

SUPPORT ANGLE CRACKED AT BS 347, STR 8L. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,820 hrs · 61,082 cycles

FRAME CRACKED AT BS 492, STR 24R. REMOVED AND REPLACED FRAME IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,820 hrs · 61,082 cycles

FRAME CRACKED AT BS 947.5, STR 19L. REMOVED AND REPLACED FRAME IAW SRM.

Part: PANEL — CRACKED (FUSELAGE) · airframe 65,820 hrs · 61,082 cycles

CRACK ON PANEL LOCATED AT BS 1121 ON INLET AIR APU DUCT CUTOUT IN TORQUE BOX AREA. REMOVED AND REPLACED PANEL LOCATED AT BS 1121 ON INLET AIR APU CUTOUT IN TORQUE BOX AREA IAW SRM 51-40-02.

Part: WEB — CORRODED (FUSELAGE) · airframe 65,820 hrs · 61,082 cycles

WEB CORRODED BETWEEN BS 867 TO BS 887, STR 17R. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,820 hrs · 61,082 cycles

FRAME CRACKED AT BS 947.5, STR 19R. REMOVED AND REPLACED FRAME IAW SRM AND DWG.

Part: PLATE — CRACKED (FUSELAGE) · airframe 65,820 hrs · 61,082 cycles

CRACK ON PLATE LOC BS 794.5 AT LEVEL STR 25R IN AFT CARGO COMPARTMENT. REPLACED PLATE LOC BS 794.5 AT LEVEL STR 25R IN AFT CARGO COMPARTMENT IAW B737-500 SRM 51-40-02 AND DRAWING #65-47959.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 65,820 hrs · 61,082 cycles

STRINGER SPLICE CORRODED AT BS 907, STR 25R. REMOVED AND REPLACED SPLICE IAW SRM AND DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 65,820 hrs · 61,082 cycles

CORROSION ON WEB LOCATED BETWEEN BS 847 AND BS 867 AT LEVEL OF STR 17R IN AFT PAX CABIN. REPAIRED FUSELAGE CREASE BEAM WEB AT S-17R BETWEEN BS 847 AND BS 867 IAW EA 1-553-21021 REV 0 AND EO AEM-HC53-501/12 REV 0.

Part: WEB — CRACKED (NLG WW) · airframe 65,820 hrs · 61,082 cycles

LEFT NLG WHEEL WELL SIDE WEB CRACKED AT BS 243.7-4.5, WL 169. REPAIRED WEB IAW SRM.

Part: WEB — CRACKED (NLG WW) · airframe 65,820 hrs · 61,082 cycles

RIGHT NLG W/W SIDE WEB CRACKED AT BS 243.7+3.5, WL 169.1. REPAIRED WEB IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,820 hrs · 61,082 cycles

FUSELAGE SKIN CRACKED AT BS 951, STR 11L. REPAIRED SKIN IAW SRM.

Part: WEB — CRACKED (NLG WW) · airframe 65,820 hrs · 61,082 cycles

LEFT NLG WHEEL WELL SIDE WEB CRACKED AT BS 243.7-4.5, WL 169.1. REPAIRED WEB IAW SRM.

Part: WEB — CRACKED (NLG WW) · airframe 65,820 hrs · 61,082 cycles

RIGHT NLG WHEEL WELL SIDE WEB CRACKED AT BS 238+3.5, WL 169.1. REPAIRED WEB IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,820 hrs · 61,082 cycles

FRAME CRACKED AT BS 1040, BETWEEN STR 25L AND STR 26L. REPAIRED FRAME IAW EA AND EO.

Part: WEB — CRACKED (NLG WW) · airframe 65,820 hrs · 61,082 cycles

LEFT NLG WHEEL WELL WEB CRACKED AT BS 259.6, WL 169.1. REPAIRED WEB IAW SRM.

Part: WEB — CRACKED (NLG WW) · airframe 65,820 hrs · 61,082 cycles

LEFT NLG WHEEL WELL SIDE WEB CRACKED AT BS 243.7+3.5, WL 169.1. REPAIRED WEB IAW SRM.

Part: WEB — CRACKED (NLG WW) · airframe 65,820 hrs · 61,082 cycles

LEFT NLG WHEEL WELL SIDE WEB CRACKED AT BS 243.7+2.5, WL 169.1. REPAIRED WEB IAW SRM.

Part: WEB — CRACKED (NLG WW) · airframe 65,820 hrs · 61,082 cycles

LEFT NLG WHEEL WELL SIDE WEB CRACKED AT BS 243.7+4.5, WL 169.1. REPAIRED WEB IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 65,820 hrs · 61,082 cycles

TIE CLIP CRACKED AT BS 294.5, STR 12L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 65,820 hrs · 61,082 cycles

TIE CLIP CRACKED AT BS 360, STR 10L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: PLATE — CRACKED (FUSELAGE) · airframe 65,820 hrs · 61,082 cycles

CRACK ON PLATE IN LOWER HINGE LOCATED FWD ENTRY DOOR CUTOUT STRUCTURE. REPLACE PLATE (SHIELD) IN LOWER HINGE LOCATED FWD ENTRY DOOR CUTOUT STRUCTURE IAW B737-500 SRM 51-40-02 AND SRM 51-10-02 ITEM 8.

Part: PLATE — CRACKED (FUSELAGE) · airframe 65,820 hrs · 61,082 cycles

CRACK ON PLATE IN UPPER HINGE LOCATED FWD ENTRY DOOR CUTOUT STRUCTURE. REMOVED AND REPLACED PLATE IN SRM.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 65,820 hrs · 61,082 cycles

CRACK ON SUPPORT ANGLE LOCATED AT LEVEL OF RSS 544 TRAILING EDGE AREA OF RT WING. REMOVED AND REPLACED ANGLE IAW SRM AND DRAWING.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,820 hrs · 61,082 cycles

CRACK INDICATION ON AFT UPPER CORNER FORWARD ENTRY DOOR CUTOUT LOCATED BS 344 BELOW STR 6L. CRACK L =0.500" APPROX. REPAIRED FUSELAGE SKIN AT FWD ENTRY DOOR CUTOUT UPPER AFT CORNER LOCATED ON BS 328 TO BS 348.2+10" BETWEEN STR 5L TO STR 9L IAW EA.

Part: ANGLE — CRACKED (RT WING) · airframe 65,820 hrs · 61,082 cycles

CRACK ON ANGLE LOCATED AT WBL 183 TRAILING EDGE AREA OF RIGHT WING. REPLACED ANGLE AND FASTENERS IAW B737-500 SRM 51-10-02 ITEM 8 PAGE 8 DWG#65-50820 LOCATED AT WBL 183 TRAILING EDGE AREA OF RIGHT WING.

Part: STRAP — CRACKED (FUSELAGE) · airframe 65,820 hrs · 61,082 cycles

CRACK ON STRAP AT STA 328 LBL 45.6 OF E/E COMPARTMENT UPPER SURFACE. REPLACED STRAP AND FASTENERS LOC STA 312 TO STA 344 OF E/E COMPARTMENT UPPER SURFACE IAW B737-500 SRM 51-10-02 ITEM 8 PAGE 8 DWG 65C33970.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 65,820 hrs · 61,082 cycles

CRACK ON SUPPORT ANGLE AT WBL 71.24 LOWER SURFACE RIGHT WING. REPLACED SUPPORT ANGLE (ANGLE ASSY) LOCATED AT WBL 71.24 LOWER SURFACE RIGHT WING IAW SRM B737-500 51-10-02 AND DRAWING #65-50820.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 65,820 hrs · 61,082 cycles

CRACK ON SUPPORT ANGLE LOCATED AT WBL 71.24 + 14.5 TRAILING EDGE AREA LEFT WING. REPLACED SUPPORT ANGLE SEAL DEPRESSOR LOCATED AT WBL 71.24+14.5" TIE AREA LEFT WING IAW B737-500 SRM 51-10-02 ITEM 8, 51-40-02 AND DRAWING # 65-50820.

Part: ACCESS PANEL — CRACKED (RT WING) · airframe 65,820 hrs · 61,082 cycles

CRACK ON ACCESS PANEL 8501R OF RIGHT WING. REPAIRED ACCESS PANEL 8501R RIGHT WING IAW B737-500 SRM 51-70-10-2R-0.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 65,820 hrs · 61,082 cycles

CRACK ON SUPPORT ANGLE LOCATED AT RSS 533 TRAILING EDGE AREA LEFT WING. REPLACED SUPPORT ANGLE LOC AT RSS533 TRAILING EDGE AREA LEFT WING IAW B737-500 SRM 51-40-02 B737-500 SRM 51-10-02 ITEM8 AND DWG 65-46460.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,820 hrs · 61,082 cycles

CRACK ON FORWARD LOWER CORNER AFT ENTRY DOOR CUTOUT LOCATED BS 951+10" ABOVE STR 17L. REPAIRED SKIN IAW EA AND EO.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 65,820 hrs · 61,082 cycles

CRACK ON INTERCOSTAL WEB LOCATED BETWEEN BS 294.5 AND BS 303.9, STRINGER 16L, ON FWD STRUCTURE OF FWD ENTRY DOOR. REMOVED AND REPLACED WEB IAW SRM AND DRAWING.

Part: SKIN — CRACKED (LT WING) · airframe 65,820 hrs · 61,082 cycles

CRACK ON LEADING EDGE LOCATED AT LEVEL OF WBL 227 LOWER SURFACE LEFT WING. REPAIRED LEADING EDGE AT LEVEL OF WBL 227 LOWER SURFACE LEFT WING IAW SRM 51-70-17-0G-0 PARA 4G REP 7 B737-500.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 65,820 hrs · 61,082 cycles

CRACK ON THE RBL 24.5 LONGITUDINAL FLOORBEAM WEB AT LEVEL BS 708 IN CENTER WING SECTION STRUCTURE. REPAIRED BEAM IAW EO AND EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 65,820 hrs · 61,082 cycles

CRACK ON LONGITUDINAL FLOORBEAM UPPER CHORD DIRECTED DOWNWARD OF OVAL HOLE BS 663 AT LBL 24.5 CENTER WING SECTION STRUCTURE. REPAIRED BEAM IAW EO AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,820 hrs · 61,082 cycles

CRACKS ON EXTERNAL SKIN CUTOUT OF GROUND SERVICE AIR CONDITIONING LOCATED BETWEEN BS 520 TO BS 540 AND STR 28R TO STR 28L. REPAIRED FUSELAGE SKIN BETWEEN STA 482+8" AND STA 540, S-27L TO S-27R IAW EA AEM-HC53-490/12 R0, FOR INSPECTION REQUIREMENTS SEE TLD T027814 FACT AS A RESULT OF POST REPAIR INSPECTION.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 65,820 hrs · 61,082 cycles

AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, BL 0. REPAIRED WEB IAW SRM.

Part: LIGHT — OUT OF POSITION (CABIN) · airframe 65,043 hrs · 60,539 cycles

RIGHT FORWARD EMERGENCY EXIT LIGHT COVER FELL OFF. REMOVED AND REPLACED LIGHT ASSY PER M/M.

Part: LIGHT — LOOSE (CABIN) · airframe 63,339 hrs · 59,429 cycles

LT EEPLS LOOSE AT ROW 6. SECURED EEPLS PER MM.

Part: PRESSURE DECK — CRACKED (MLG WW) · airframe 62,887 hrs · 59,138 cycles

DURING SCHEDULED HC1 CHECK, FOUND MAIN WHEEL WELL PRESSURE DECK CRACKED AT BS 664.75, RBL 36. REPAIRED WEB IAW SRM AND EA.

Part: LENS — LOOSE (CABIN) · airframe 62,645 hrs · 58,978 cycles

LEFT EMERGENCY EXIT SIGN LENS LOOSE. SECURED LENS PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 62,318 hrs · 62,318 cycles

RT EEPLS LOOSE BETWEEN ROW 4 TO ROW 7. REMOVED AND REPLACED EEPLS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,288 hrs · 58,743 cycles

DURING SCHEDULED CV CHECK, FOUND SKIN CRACKED AT BS 749, STR 24L. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 62,135 hrs · 58,643 cycles

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

Part: LIGHT — LOOSE (CABIN) · airframe 61,988 hrs · 58,538 cycles

LT EEPLS LOOSE BETWEEN ROW 6 TO ROW 7. REMOVED AND REPLACED EEPLS PER MM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 61,554 hrs · 58,234 cycles

DURING SCHEDULED SPV CHECK, FOUND LONGITUDINAL FLOORBEAM ANGLE CRACKED AT BS 639, LBL 45.5. REPAIRED ANGLE PER EA.

Part: SKIN — CRACKED (R2 DOOR) · airframe 60,517 hrs · 57,524 cycles

DURING SCHEDULED MV3 CHECK, FOUND R2 DOOR CRACKED ON UPPER HINGE CUTOUT ON DOOR FRAME SKIN LOWER AFT CORNER. REMOVED AND REPLACED R2 DOOR PER MM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 60,177 hrs · 57,259 cycles

L2 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. RE-INSTALLED SLIDE PER MT.

Part: LENS — LOOSE (CABIN) · airframe 60,135 hrs · 57,227 cycles

DURING SCHEDULED 18Y CHECK, FOUND RT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT LENS LOOSE BETWEEN ROW 12 AND ROW 13. SECURED LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,135 hrs · 57,227 cycles

DURING SCHEDULED 18Y CHECK, FOUND SKIN CRACKED AT BS 389, STR 17L. REPAIRED SKIN PER EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 60,135 hrs · 57,227 cycles

DURING SCHEDULED 18Y CHECK, FOUND AFT CARGO CHANNEL CORRODED AT BS 772, RBL 8.10. REPAIRED CHANNEL PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,135 hrs · 57,227 cycles

DURING SCHEDULED 18Y CHECK, FOUND FRAME CRACKED AT BS 907, STR 21R. REPAIRED FRAME PER EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 60,135 hrs · 57,227 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CORRODED BETWEEN BS 440 TO BS 482, STR 28L. REPAIRED STRINGER PER SRM.

Part: FLAP — CRACKED (RT WING) · airframe 60,135 hrs · 57,227 cycles

DURING SCHEDULED 18Y CHECK, FOUND RT WING O/B MID FLAP UPPER CHORD CRACKED. REPAIRED MID FLAP PER EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 60,135 hrs · 57,227 cycles

DURING SCHEDULED 18Y CHECK, FOUND SHEAR TIE CORRODED AT BS 787, BETWEEN STR 25R TO STR 26R. REPAIRED SHEAR TIE PER SRM.

Part: BEAR STRAP — CORRODED (FUSELAGE) · airframe 60,135 hrs · 57,227 cycles

DURING SCHEDULED 18Y CHECK, FOUND AFT CARGO COMPARTMENT BEAR STRAP SKIN CORRODED BETWEEN BS 847 TO BS 867, BETWEEN STR 25R TO STR 26R. REPAIRED SKIN PER EA.

Part: BEAR STRAP — CORRODED (FUSELAGE) · airframe 60,135 hrs · 57,227 cycles

DURING SCHEDULED 18Y CHECK, FOUND AFT CARGO COMPARTMENT BEAR STRAP SKIN CORRODED AT BS 851, BETWEEN STR 23R TO STR 24R. REPAIRED SKIN PER EA.

Part: BEAR STRAP — CORRODED (FUSELAGE) · airframe 60,135 hrs · 57,227 cycles

DURING SCHEDULED 18Y CHECK, FOUND AFT CARGO COMPARTMENT BEAR STRAP SKIN CORRODED BETWEEN BS 827 TO BS 890, BETWEEN STR 22R TO STR 27R. REPAIRED SKIN PER EA.

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 60,135 hrs · 57,227 cycles

DURING SCHEDULED 18Y CHECK, FOUND VERTICAL STABILIZER LT SIDE FITTING CORRODED AT STA 1088. REMOVED AND REPLACED FITTING PER EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 60,135 hrs · 57,227 cycles

DURING SCHEDULED 18Y CHECK, FOUND FRAME CORRODED AT BS 482A, BETWEEN STR 28L TO STR 28R. REPAIRED FRAME PER EA.

Part: BEAR STRAP — CORRODED (FUSELAGE) · airframe 60,135 hrs · 57,227 cycles

DURING SCHEDULED 18Y CHECK, FOUND AFT CARGO BEAR STRAP SKIN CORRODED BETWEEN BS 767 TO BS 787, STR 25R. REPAIRED SKIN PER EA.

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 60,135 hrs · 57,227 cycles

DURING SCHEDULED 18Y CHECK, FOUND VERTICAL STABILIZER RT SIDE FITTING CORRODED AT STA 1088. REMOVED AND REPLACED FITTING PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,135 hrs · 57,227 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 21L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,135 hrs · 57,227 cycles

DURING SCHEDULED 18Y CHECK, FOUND FRAME CRACKED AT BS 927, BETWEEN STR 18L TO STR 19L. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — BROKEN (FUSELAGE) · airframe 60,135 hrs · 57,227 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP BROKEN AT BS 947.5, STR 25R. REMOVED AND REPLACED STR CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,135 hrs · 57,227 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 21R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 59,994 hrs · 57,134 cycles

L2 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. RE-INSTALLED SLIDE PER MT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,462 hrs · 56,757 cycles

DURING SCHEDULED HC1 CHECK, FOUND SKIN CRACKED AT BS 967, BETWEEN STR 26L TO STR 27L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,462 hrs · 56,757 cycles

DURING SCHEDULED HC1 CHECK, FOUND SKIN CRACKED AT BS 957, STR 21L. REPAIRED SKIN PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 59,457 hrs · 56,756 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND SKIN CORRODED AT BS 967, STR 26L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,457 hrs · 56,756 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND SKIN CRACKED AT BS 933, STR 24L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,457 hrs · 56,756 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND SKIN CRACKED AT BS 881, STR 24R. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 58,962 hrs · 56,409 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,787 hrs · 56,286 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 757, STR 22L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,787 hrs · 56,286 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 757, STR 23L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,787 hrs · 56,286 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 803, STR 19L. REPAIRED SKIN PER SRM.

Part: LIGHT — DELAMINATED (CABIN) · airframe 58,623 hrs · 56,164 cycles

DURING SCHEDULED CV CHECK, FOUND EEPLS DELAMINATED AT AFT GALLEY ENTRANCE. REMOVED AND REPLACED EEPLS PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 58,523 hrs · 56,164 cycles

L1 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY. RE-INSTALLED SLIDE PER MT.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 58,623 hrs · 56,164 cycles

L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. RE-INSTALLED SLIDE PER MT.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 58,179 hrs · 55,867 cycles

L1 DOOR SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY. RE-INSTALLED SLIDE PER MM.

Part: SENSOR — FAULTY (NR 1 ENGINE) · airframe 57,908 hrs · 55,679 cycles

DECLARED EMERGENCY. NR 1 ENGINE COMPRESSOR STALLED. REMOVED AND REPLACED NR 1 ENGINE MEC, FUEL PUMP AND CIT SENSOR PER MM.

Part: BEAM — CRACKED (R1 DOOR) · airframe 57,842 hrs · 55,630 cycles

DURING SCHEDULED HC2 CHECK, FOUND CABIN R1 DOOR AFT LOWER ACCESS BEAM CRACKED FROM EDGE FWD BELOW HI-LOKS. REMOVED AND REPLACED DOOR PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,389 hrs · 55,338 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 482 BETWEEN STR 20L TO STR 21L. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,174 hrs · 54,592 cycles

DURING HC1 CHECK, FOUND SKIN CRACKED AT BS 727D, STR 18L. REPAIRED SKIN PER SRM.

Part: SIGN — BROKEN (CABIN) · airframe 55,858 hrs · 54,401 cycles

R1 DOOR EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN PER MM.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 54,501 hrs · 53,440 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE BEAR STRAP SKIN CRACKED AT BS 303, WL 257. REPAIRED SKIN PER EA.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 54,501 hrs · 53,440 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT BEAR STRAP UPPER HINGE CUTOUT SKIN CRACKED AT BS 303, WL 257. REPAIRED SKIN PER AAR EA.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 54,501 hrs · 53,440 cycles

DURING SCHEDULED 16Y CHECK, FOUND MLG BULKHEAD VERTICAL STIFFENER CRACKED AT BS 727, LBL 6. REMOVED AND REPLACED STIFFENER PER SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 54,501 hrs · 53,440 cycles

DURING SCHEDULED 16Y CHECK, FOUND MLG BULKHEAD VERTICAL STIFFENER CRACKED AT BS 727, RBL 6. REMOVED AND REPLACED STIFFENER PER SRM.

Part: PRESSURE PANEL — DAMAGED (NLG WW) · airframe 54,501 hrs · 53,440 cycles

DURING SCHEDULED 16Y CHECK, FOUND NOSE WHEEL WELL CEILING WEB DAMAGED AT BS 277, RBL 16. REPAIRED WEB PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,501 hrs · 53,440 cycles

DURING SCHEDULED 16Y CHECK, FOUND RADIO ALTIMETER CUTOUT BELLY SKIN CRACKED AT BS 410. REPAIRED SKIN PER AAR EA.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 54,501 hrs · 53,440 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT HORIZONTAL STABILIZER SKIN CRACKED. REPAIRED SKIN PER AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,501 hrs · 53,440 cycles

DURING SCHEDULED 16Y CHECK, FOUND RADIO ALTIMETER CUTOUT BELLY SKIN CRACKED AT BS 350. REPAIRED SKIN PER AAR EA.

Part: SKIN — CORRODED (FUSELAGE) · airframe 54,501 hrs · 53,440 cycles

DURING SCHEDULED 16Y CHECK, FOUND NR 1 DME CUTOUT BELLY SKIN CORRODED BETWEEN BS 410 TO BS 465, LBL 0. REPAIRED SKIN PER SRM.

Part: WIRE — BROKEN (CABIN) · airframe 54,501 hrs · 53,440 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT EMERGENCY EXIT LIGHT WIRE BROKEN AT MID CABIN. REPAIRED WIRE PER SWPM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,501 hrs · 53,440 cycles

DURING SCHEDULED 16Y CHECK, FOUND RADIO ALTIMETER CUTOUT BELLY SKIN CRACKED AT BS 390. REPAIRED SKIN PER AAR EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 54,501 hrs · 53,440 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN ANGLE CRACKED AT BS 188, STR 17L. REPAIRED ANGLE PER SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 54,501 hrs · 53,440 cycles

DURING SCHEDULED 16Y CHECK, FOUND KEEL BEAM CORRODED AT BS 482, STR 28L. REPAIRED BEAM PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 54,501 hrs · 53,440 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 482, BETWEEN STR 28L TO STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 54,501 hrs · 53,440 cycles

DURING SCHEDULED 16Y CHECK, FOUND FWD ENTRY DOOR ANGLE CRACKED AT BS 300, STR 11L. REMOVED AND REPLACED ANGLE PER SRM.

Part: WEB — CRACKED (COCKPIT) · airframe 54,501 hrs · 53,440 cycles

DURING SCHEDULED 16Y CHECK, FOUND COCKPIT FLOOR WEB CRACKED AT BETWEEN BS 188 TO BS 196, STR 17L. REMOVED AND REPLACED WEB PER DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 54,501 hrs · 53,440 cycles

DURING SCHEDULED 18Y CHECK, FOUND FLOOR SUPPORT FRAME CRACKED AT BS 706, BETWEEN LBL 24 TO LBL 63. REMOVED AND REPLACED FRAME PER SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 54,501 hrs · 53,440 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER WEB SUPPORT ANGLE CRACKED AT BS 360, STR 8L. REMOVED AND REPLACED ANGLE PER SRM.

Part: MOUNT BRACKET — CRACKED (EVAC SLIDE) · airframe 54,501 hrs · 53,440 cycles

DURING SCHEDULED 16Y CHECK, FOUND R2 DOOR EMERGENCY EVACUATION SLIDE MOUNT BRACKETS CRACKED. REMOVED AND REPLACED BRACKET PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,501 hrs · 53,440 cycles

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

Part: CABLE — FRAYED (EVAC SLIDE) · airframe 54,501 hrs · 53,440 cycles

DURING SCHEDULED 16Y CHECK, FOUND R2 DOOR EMERGENCY EVACUATION SLIDE CABLE FRAYED. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 54,501 hrs · 53,440 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CRACKED AT BS 380, STR 13R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,501 hrs · 53,440 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 336, BETWEEN STR 20L TO STR 21L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,501 hrs · 53,440 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 320, BETWEEN STR 20L TO STR 21L. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,501 hrs · 53,440 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 460, STR 16L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,501 hrs · 53,440 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 328, BETWEEN STR 20L TO STR 21L. REPAIRED FRAME PER BOEING DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,501 hrs · 53,440 cycles

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

Part: STRAP — BROKEN (FUSELAGE) · airframe 54,501 hrs · 53,440 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT CREASE BEAM SPLICE STRAP BROKEN AT BS 531. REMOVED AND REPLACED SPLICE STRAP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,501 hrs · 53,440 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,501 hrs · 53,440 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 277, STR 16L. REPAIRED FRAME PER SRM.

Part: WEDGE — DELAMINATED (TE FLAP) · airframe 54,501 hrs · 53,440 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING INBD MIDFLAP WEDGE DELAMINATED AT OTBD END. REPAIRED WEDGE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,501 hrs · 53,440 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, LBL 25. R&R CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,501 hrs · 53,440 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, RBL 25. R&R CLIP PER SRM.

Part: LENS — LOOSE (CABIN) · airframe 53,239 hrs · 52,433 cycles

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

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 52,802 hrs · 52,094 cycles

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

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 52,388 hrs · 51,792 cycles

DURING SCHEDULED C3 CHECK, FOUND LT FWD FUSELAGE EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,388 hrs · 51,792 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT SERVICE DOOR CUTOUT FWD LOWER CORNER. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 50,551 hrs · 50,237 cycles

DURING SCHEDULED C1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 50,551 hrs · 50,237 cycles

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

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 50,532 hrs · 50,218 cycles

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

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 49,977 hrs · 49,691 cycles

R2 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM.

Part: FRAME — CRACKED (BS 296 S16R) · airframe 49,811 hrs · 49,507 cycles

DURING SCHEDULED SPV CHECK, FOUND STUB FRAME CRACKED AT BS 296, STR 16R. REPAIRED FRAME PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 49,811 hrs · 49,507 cycles

DURING SCHEDULED SPV CHECK, FOUND AFT CARGO DOOR CUTOUT FWD FRAME CRACKED NR 5 DOOR STOP. REPAIRED FRAME PER SRM.

Part: BULKHEAD — CRACKED (BS 1016 S7L) · airframe 49,811 hrs · 49,507 cycles

DURING SCHEDULED SPV CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, STR 7L. REPAIRED WEB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,811 hrs · 49,507 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,811 hrs · 49,507 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,811 hrs · 49,507 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,811 hrs · 49,507 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,811 hrs · 49,507 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,811 hrs · 49,507 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,811 hrs · 49,507 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727A, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,811 hrs · 49,507 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,811 hrs · 49,507 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 49,811 hrs · 49,507 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 908, STR 4R. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,811 hrs · 49,507 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 482, STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,811 hrs · 49,507 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 6L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,811 hrs · 49,507 cycles

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

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 49,811 hrs · 49,507 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 908, STR 4L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,811 hrs · 49,507 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,811 hrs · 49,507 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,811 hrs · 49,507 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,811 hrs · 49,507 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,811 hrs · 49,507 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,811 hrs · 49,507 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,811 hrs · 49,507 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,811 hrs · 49,507 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,811 hrs · 49,507 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,811 hrs · 49,507 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 482A, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,811 hrs · 49,507 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8R. REPAIRED FRAME PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,783 hrs · 49,486 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA.

Part: SPOILER — DELAMINATED (LT WING) · airframe 49,305 hrs · 49,025 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LEFT WING NR 0 GROUND SPOILER DELAMINATED. REMOVED AND REPLACED NR 0 SPOILER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,070 hrs · 48,803 cycles

DURING SCHEDULED SV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 10R. REPAIRED SKIN PER SRM & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,301 hrs · 48,013 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947, STR 24R. REPAIRED SKIN PER SWA EA.

Part: LENS — LOOSE (CABIN) · airframe 48,096 hrs · 47,799 cycles

BULL NOSE EMERGENCY EXIT LIGHT LENS LOOSE AT ROW 13 DEF. SECURED LENS PER MM.

Part: A/C PACK — ODOR (E&E BAY) · airframe 47,477 hrs · 47,122 cycles

AIR TURNBACK, CREW REPORTED HEAVY ELECTRICAL SMELL, BOTH COOLING PACKS FAILED, ALTERNATE COOLING PACK STARTED AFTER 10 MINUTES. REMOVED AND REPLACED NORMAL COOLING PACK PER MM.

Part: BOLT — WORN (RT ELEVATOR) · airframe 47,303 hrs · 46,935 cycles

DURING SCHEDULED C1 CHECK, RT ELEVATOR CONTROL TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED TAB NR 1 HINGE BOLT PER MM.

Part: FRAME — CRACKED (BS 639) · airframe 46,960 hrs · 46,551 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 639, STR 16R. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (BS 482A S20L) · airframe 46,960 hrs · 46,551 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 482A, STR 20L. REPAIRED FRAME SECTION PER SWA EA.

Part: SKIN — CORRODED (BS 791-863) · airframe 46,960 hrs · 46,551 cycles

DURING SCHEDULED 1/2D CHECK, FOUND AFT CARGO DOOR CUTOUT FUSELAGE SKIN BEAR STRAP CORRODED AT BS 791 TO BS 863, RBL 24. REPAIRED SKIN PER SWA EA.

Part: FRAME — CRACKED (BS 482A S20R) · airframe 46,960 hrs · 46,551 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 482A, STR 20R. REPAIRED FRAME SECTION PER SWA EA.

Part: SHEAR TIE — CORRODED (BS 867 S26R) · airframe 46,960 hrs · 46,551 cycles

DURING SCHEDULED 1/2D CHECK, FOUND SHEAR TIE CORRODED AT BS 867, STR 26R. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (BS 787 S23R) · airframe 46,960 hrs · 46,551 cycles

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

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 46,960 hrs · 46,551 cycles

DURING SCHEDULED 1/2D CHECK, FOUND SHEAR TIE CORRODED AT BS 482B, STR 28R. REMOVED AND REPLACED SHEAR TIE PER BOEING DRAWING AND SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 46,960 hrs · 46,551 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5, LBL 45. REPAIRED FLOORBEAM PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 294) · airframe 46,960 hrs · 46,551 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED AT BS 294.5, STR 11L. REPAIRED STRINGER CLIP PER SRM.

Part: SHEAR TIE — CRACKED (BS 420) · airframe 46,960 hrs · 46,551 cycles

DURING SCHEDULED 1/2D CHECK, FOUND SHEAR TIE CRACKED AT BS 420, STR 15R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: BRACKET — CORRODED (L1 DOOR SLIDE) · airframe 46,960 hrs · 46,551 cycles

DURING SCHEDULED 1/2D CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR BRACKET CORRODED. REMOVED AND REPLACED AFT GIRT BAR BRACKET PER SRM.

Part: STRINGER SPLICE — CRACKED (BS 360) · airframe 46,960 hrs · 46,551 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 15L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: STRINGER CLIP — CRACKED (BS 927) · airframe 46,960 hrs · 46,551 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED AT BS 927, STR 25R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SHEAR TIE — CRACKED (BS 360) · airframe 46,960 hrs · 46,551 cycles

DURING SCHEDULED 1/2D CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 14R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: BRACKET — CORRODED (L1 DOOR SLIDE) · airframe 46,960 hrs · 46,551 cycles

DURING SCHEDULED 1/2D CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR BRACKET CORRODED. REMOVED AND REPLACED FWD GIRT BAR BRACKET PER SRM.

Part: SKIN — CRACKED (BS 406) · airframe 46,960 hrs · 46,551 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT NR 2 RADIO ANTENNA CUTOUT, BS 406, RBL 1.5. REPAIRED SKIN PER SWA EA.

Part: FLOORBEAM — CORRODED (BS 986) · airframe 46,960 hrs · 46,551 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5, RBL 32. REPAIRED FLOORBEAM PER SRM.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 46,960 hrs · 46,551 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER 28R DAMAGED AT BS 380. REPAIRED STRINGER PER SRM.

Part: LINE — CHAFED (HYD SYSTEM) · airframe 43,388 hrs · 42,730 cycles

AIR TURNBACK, DECLARED EMERGENCY. LOST B-HYDRAULIC SYSTEM ON TAKEOFF. REMOVED AND REPLACED HYDRAULIC LINES FROM B-SYSTEM PUMP TO B-SYSTEM CONTROL MODULE & B-SYSTEM PUMP CASE DRAIN TO T-FITTING PER MM.

Part: LENS — MISSING (CABIN) · airframe 43,180 hrs · 42,478 cycles

LENS MISSING AT AFT GALLEY OVERHEAD EMERGENCY EXIT LIGHT. INSTALLED LIGHT LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 42,063 hrs · 41,363 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 749, STRINGER 18L, CRACKED. REPAIRED SKIN PER SRM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 44,576 hrs · 40,864 cycles

DURING SCHEDULED RON, FOUND FWD ENTRY EMERGENCY EXIT LIGHTS RANDOMLY ILLUMINATE. REMOVED AND REPLACED BATTERY PER MM.

Part: SNUBBER — INOPERATIVE (L2 DOOR) · airframe 41,458 hrs · 40,749 cycles

L2 DOOR WILL NOT OPEN. REMOVED AND REPLACED L2 DOOR SNUBBER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 40,295 hrs · 39,633 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR AFT LOWER CUTOUT. REPAIRED SKIN PER SWA EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 40,295 hrs · 39,633 cycles

DURING SCHEDULED 1/4D CHECK, FOUND UPPER MLG W/W BEADED WEB CRACKED AT BS 665, OUTBD OF NR 2 SEAT TRACK. REPAIRED WEB PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 40,295 hrs · 39,633 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 40,294 hrs · 39,632 cycles

DURING SCHEDULED 1/4D CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: FRAME — CRACKED (R1 DOOR) · airframe 40,294 hrs · 39,632 cycles

DURING SCHEDULED 1/4D CHECK, FOUND R1 DOOR LOWER FRAME CRACKED AT STOP FITTING. REPAIRED FRAME PER BAC DRAWING.

Part: LENS — LOOSE (CABIN) · airframe 40,294 hrs · 39,632 cycles

DURING SCHEDULED 1/4D CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. REPAIRED LENS ASSY PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 40,294 hrs · 39,632 cycles

DURING SCHEDULED 1/4D CHECK, FOUND SHEARE TIE CORRODED AT BS 482, LOWER BILGE AREA. REPAIRED SHEAR TIE PER SRM.

Part: SLIDE — UNSERVICEABLE (ENTRY DOOR) · airframe 34,750 hrs · 34,446 cycles

AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 35,422 hrs · 34,138 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND 1.5 INCH SKIN CRACK AT BS 942 ABOVE STR 24L. REPAIRED SKIN PER SRM.

Part: SLIDE — UNSERVICEABLE (SERVICE DOOR) · airframe 32,495 hrs · 32,300 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 32,324 hrs · 32,143 cycles

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

Part: SKIN — CANNING (FUSELAGE) · airframe 32,201 hrs · 32,022 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN OIL CANNED AT BS 1026, BETWEEN STR 27L & 27R. REPAIRED SKIN PER SRM.

Part: CLIP — CRACKED (FUSELAGE) · airframe 32,201 hrs · 32,022 cycles

DURING SCHEDULED D CHECK, FOUND STR CLIP CRACKED AT BS 482, STR 19L. R&R CLIP PER SRM.

Part: BEAM — CORRODED (RH WING) · airframe 32,201 hrs · 32,022 cycles

DURING SCHEDULED D CHECK, FOUND RH MLG STABILIZER BEAM CORRODED AT AFT INBD SIDE. R&R STAB BEAM PER MM.

Part: SPAR — CRACKED (LH WING) · airframe 32,201 hrs · 32,022 cycles

DURING SCHEDULED D CHECK, FOUND LH REAR SPAR UPPER CHORD CRACKED AT WBL 157. R&R REAR SPAR UPPER CHORD SECTION PER BFG ER .

Part: RIB — CRACKED (RT WING) · airframe 32,201 hrs · 32,022 cycles

DURING SCHEDULED D-CHECK, FOUND RT WING RIB LOWER CHORD CRACKED AT STR 2, WBL 135.5. REPAIRED CHORD PER BFG ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,201 hrs · 32,022 cycles

DURING SCHEDULED D CHECK, FOUND FRAME CRACKED AT FWD CARGO DOOR LOWER CUT OUT AT BS 452, RBL 41. R&R FRAME SECTION PER SRM.

Part: CLIP — CRACKED (FUSELAGE) · airframe 32,201 hrs · 32,022 cycles

DURING SCHEDULED D CHECK, FOUND STR CLIP CRACKED AT BS 277, STR 10R. R&R STR CLIP PER SRM.

Part: FITTING — CORRODED (LH WING) · airframe 32,201 hrs · 32,022 cycles

DURING SCHEDULED D CHECK, FOUND LH MLG SUPPORT BEAM AFT HANGER FITTING CORRODED. R&R FITTING PER MM.

Part: SLAT — DELAMINATED (LH WING) · airframe 32,201 hrs · 32,022 cycles

DURING SCHEDULED D CHECK, FOUND # 2 L/E SLAT DELAMINATED AT T/E WEDGE OTBD END. REPAIRED SLAT PER SRM.

Part: BEARING — WORN (RH ELEVATOR) · airframe 32,201 hrs · 32,022 cycles

DURING SCHEDULED D CHECK, FOUND RH ELEVATOR TAB ROD END BEARINGS WORN. R&R ELEVATOR TAB ROD END BEARINGS PER OHM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,201 hrs · 32,022 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED AT STR 8R, BS 400, BS 747, BS 787 & BS 867. REPAIRED FUSELAGE FRAMES PER SRM & BFG ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,201 hrs · 32,022 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED AT STR 8L, BS 400, BS 787 & BS 827. REPAIRED FUSELAGE FRAMES PER SRM & BFG ER.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 32,201 hrs · 32,022 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CRACKED AT BS 277, STR 10R. REPAIRED STR PER SRM.

Part: FITTING — BROKEN (AFT SVC DOOR) · airframe 32,201 hrs · 32,022 cycles

DURING SCHEDULED D CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING ANCHOR NUT BROKEN. R&R GIRT BAR FITTING ANCHOR NUT PER MM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 32,201 hrs · 32,022 cycles

DURING SCHEDULED D CHECK, FOUND CREASE BEAM CRACKED AT BS 520, LBL 59. REPAIRED CREASE BEAM PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 32,198 hrs · 32,021 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 4R. REMOVED STR CLIP PER SRM.

Part: SLIDE — OUT OF ADJ (SERVICE DOOR) · airframe 31,021 hrs · 30,867 cycles

FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. RE-ADJUSTED EVAC SLIDE ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,916 hrs · 30,767 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS INOP AND TRACK COVERS BROKEN/LOOSE IN SEVERAL AREAS. REPAIRED EEPLS AND REMOVED AND REPLACED TRACK COVERS PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 30,746 hrs · 30,601 cycles

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

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 30,746 hrs · 30,601 cycles

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

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 30,314 hrs · 30,169 cycles

DURING SCHEDULED SPECIAL VISIT AT DALFORT, FOUND BS 178 BULKHEAD WEB CRACKED AT RBL 4.7, WL 201. REPAIRED BULKHEAD PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 30,314 hrs · 30,169 cycles

DURING SCHEDULED SPECIAL VISIT AT DALFORT, FOUND BS 178 BULKHEAD VERTICAL CHORD CRACKED AT LBL 5.7, WL 184. REPAIRED VERTICAL CHORD PER SRM.

Part: COVER — LOOSE (CABIN FLOOR) · airframe 30,102 hrs · 29,955 cycles

EEPLS COVER LOOSE AND BROKEN AT ROW 5. REPLACED TRACK COVER AND 1 BULB (P/N 0L3071BPL5GPL).

Part: BULB — INOPERATIVE (CABIN) · airframe 29,981 hrs · 29,838 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS INOP BETWEEN ROWS 3 & 5. REMOVED AND REPLACED BULBS PER MM.

Part: WIRE — EXPOSED (CABIN) · airframe 29,302 hrs · 29,168 cycles

EEPLS WIRES EXPOSED. REPAIRED WIRES PER MM.

Part: COVER — MISSING (CABIN) · airframe 28,327 hrs · 28,200 cycles

EEPLS TRACK COVER MISSING AT MID CABIN. REPLACED TRACK COVERS PER MM.

Part: INDICATOR — DISLODGED (ESCAPE SLIDE) · airframe 28,317 hrs · 28,189 cycles

DURING SCHEDULED C3 CHECK, FOUND FWD SERVICE DOOR EVACUATION SLIDE PRESSURE IND OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM.

Part: COVER — CRACKED (CABIN) · airframe 28,317 hrs · 28,189 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS TRACK COVERS LOOSE AND CRACKED ON ROWS 1, 8, AND 18. REMOVED AND REPLACED TRACK COVERS PER MM.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 27,992 hrs · 27,842 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. R&R BATTERY PACK PER MM.

Part: BLADE — BIRD STRIKE (NR 1 ENGINE) · airframe 27,984 hrs · 27,832 cycles

AIR TURNBACK, BIRD STRIKE IN NR 1 ENGINE INTAKE. COMPLIED WITH BIRD STRIKE BORESCOPE INSP. R&R NR 1 ENGINE FAN BLADE SET AND NR 1 ENGINE PRECOOLER VALVE PER MM.

Part: COMPRESSOR — STALLED (NR 2 ENGINE)

AIR TURNBACK, IN FLIGHT SHUT DOWN, NR 1 ENG COMPRESSOR STALLED AT 27,000 FEET AND THEN AGAIN AT 16,000 FEET FOLLOWED BY OIL PRESS IND DECREASE AND ENG VIBRATION. REMOVED AND REPLACED NR 1 ENG PER MM.

Part: COVER — MISSING (CABIN)

EEPLS TRACK COVER MISSING AT MID CABIN. REPLACED TRACK COVER PER MM.

Part: LIGHT — NOT ALIGNED (BIN 5 RT)

DURING SCHEDULED C1 CHECK, FOUND OVERHEAD BIN (5RT) EMERGENCY LIGHT LENS NEEDS ALIGNED. EMERGENCY LIGHT SECURED PER BOEING MM.

Part: SLIDE — DETACHED (PAX DOOR)

DURING SCHEDULED BC4 CHECK, FOUND SLIDE WAS PULLED OUT OF DOOR BY OPS AGENT. RESECURED PER BOEING MM.

Part: BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK PER BOEING M/M.