N394SW

Part: MOUNT — LOOSE (R2 DOOR) · airframe 71,153 hrs · 56,886 cycles

R2 DOOR EMERGENCY EVAC SLIDE FORWARD UPPER SLIDE MOUNT LOOSE. R&R MOUNT PER SRM.

Part: SLAT — DELAMINATED (RT WING) · airframe 70,265 hrs · 56,293 cycles

RIGHT WING NR 4 SLAT INBD DELAMINATED. R & R NR 4 SLAT IAW AMM.

Part: ACM — LEAKING (AC BAY) · airframe 69,505 hrs · 55,777 cycles

DIVERSION & DECLARED EMER. FUMES IN CABIN ABEAM, BETWEEN ROWS 15 - 19 ON RT SIDE OF THE ACFT. FOUND ACM LEAKED. R & R RT ACM IAW AMM.

Part: ACTUATOR — LEAKING (RT SPOILER) · airframe 69,285 hrs · 55,633 cycles

RIGHT WING NR 6 FLIGHT SPOILER ACTUATOR EXTERNAL HYD LEAKED. R & R ACTUATOR IAW AMM.

Part: ACTUATOR — LEAKING (LT SPOILER) · airframe 69,285 hrs · 55,633 cycles

LEFT WING NR 3 FLIGHT SPOILER ACTUATOR EXTERNAL HYD LEAKED. R & R ACTUATOR IAW AMM.

Part: FITTING — CRACKED (TE FLAP) · airframe 69,285 hrs · 55,633 cycles

RIGHT WING NR 6 FAIRING PYLON INBD FLAP, OTBD TRACK INTERFACE CRACKED. REPAIRED FITTING IAW EA.

Part: RIB — CRACKED (LT WING) · airframe 69,285 hrs · 55,633 cycles

LEFT WING INSPAR RIB WEB CRACKED ON RIB WEB ON WBL 198.60, AT LEVEL OF S 5 FUEL TANK. REPAIRED WEB IAW EA.

Part: PLATE — CRACKED (RT WING) · airframe 69,285 hrs · 55,633 cycles

RIGHT WING SUPPORT PLATE CRACKED ON RSS 237. R & R PLATE IAW SRM & DWG.

Part: SKIN — CRACKED (RT WING) · airframe 69,285 hrs · 55,633 cycles

RIGHT WING SKIN CRACKED IN FASTENER HOLE REAR SPAR AFT ROW ON EXTERNAL SKIN, LOCATED RSS 254 & 12 O'CLOCK. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 69,285 hrs · 55,633 cycles

RIGHT WING IN SPAR UPPER SKIN CRACKED AT RSS 249 & 6 0'CLOCK ORIENTATION. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 69,285 hrs · 55,633 cycles

RIGHT WING IN SPAR UPPER SKIN TE CRACKED AT RSS 230 & 6 O'CLOCK ORIENTATION. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 69,285 hrs · 55,633 cycles

RIGHT WING IN SPAR UPPER SKIN TE CRACKED AT RSS 237 & 12 O'CLOCK ORIENTATION. REPAIRED SKIN IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 69,285 hrs · 55,633 cycles

LEFT WING REAR SPAR WEB AT RSS 158 CRACKED. REPAIRED WEB IAW EA.

Part: PLATE — CRACKED (LT WING) · airframe 69,285 hrs · 55,633 cycles

LEFT WING SUPPORT PLATE CRACKED ON RSS 237. R & R PLATE IAW SRM & DWG.

Part: SKIN — CRACKED (LT WING) · airframe 69,285 hrs · 55,633 cycles

LEFT WING SKIN CRACKED IN FASTENER HOLE REAR SPAR AFT ROW ON EXTERNAL, LOCATED AT RSS 251 & 6 O'CLOCK. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 69,285 hrs · 55,633 cycles

RIGHT WING IN SPAR UPPER SKIN TE CRACKED AT RSS 248.5" & 12 O'CLOCK ORIENTATION. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 69,285 hrs · 55,633 cycles

LEFT WING SKIN CRACKED IN FASTENER HOLE, REAR SPAR AFT ROW ON EXTERNAL, LOCATED AT RSS 249.5" & 6 O'CLOCK. REPAIRED SKIN IAW EA.

Part: BRACKET — CRACKED (TE FLAP) · airframe 69,285 hrs · 55,633 cycles

RIGHT WING NR 6 FAIRING INBD FLAP OTBD TRACK, FWD OTBD BRACKET CRACKED. R & R BRACKET IAW SRM & DWG.

Part: ANGLE — CRACKED (FLAP TRACK) · airframe 69,285 hrs · 55,633 cycles

LEFT WING INBD FLAP, OTBD TRACK NR 3 FAIRING INTERNAL STRUCTURE OF ACCESS PANEL 5735 ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.

Part: SKIN — CRACKED (LT WING) · airframe 69,285 hrs · 55,633 cycles

LEFT WING SKIN TE CRACKED IN FASTENER HOLE REAR SPAR AFT ROW ON EXTERNAL SKIN LOCATED AT RSS 239.25 & 5 O'CLOCK. REPAIRED SKIN IAW EA.

Part: ANGLE — CRACKED (FLAP TRACK) · airframe 69,285 hrs · 55,633 cycles

LEFT WING INBD FLAP, OTBD TRACK 3, FAIRING INTERNAL STRUCTURE OF ACCESS PANEL 5736 ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 69,285 hrs · 55,633 cycles

AFT CARGO COMPARTMENT ANGLE CRACKED AT BS 947.5+10, BETWEEN STRINGER 24L - 26L. R & R ANGLE IAW SRM & DWG.

Part: SPAR — CRACKED (LT WING) · airframe 69,285 hrs · 55,633 cycles

LEFT WING REAR SPAR, UPPER CHORD CRACKED IN OPEN HOLE, LOCATED ON RSS 215.97+5. REPAIRED CHORD IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 69,285 hrs · 55,633 cycles

LEFT WING REAR SPAR, UPPER CHORD CRACKED, LOCATED ON RSS 215.97+6. REPAIRED CHORD IAW EA.

Part: SPAR — CRACKED (RT WING) · airframe 69,285 hrs · 55,633 cycles

RIGHT WING REAR SPAR UPPER CHORD CRACKED AT RSS 221.5 ON TE. REPAIRED CHORD IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 69,285 hrs · 55,633 cycles

LEFT WING REAR SPAR UPPER CHORD CRACKED ON RSS 215.97+4. REPAIRED CHORD IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 69,285 hrs · 55,633 cycles

LEFT WING REAR SPAR WEB & LOWER CHORD ON RSS 224.14 +1", AT 3 O' CLOCK DIRECTION. REPAIRED WEB IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 69,285 hrs · 55,633 cycles

LEFT WING REAR SPAR WEB & LOWER CHORD CRACKED AT RSS 215.97+4, AT 9 O' CLOCK DIRECTION. REPAIRED WEB IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 69,285 hrs · 55,633 cycles

LEFT WING REAR SPAR WEB & LOWER CHORD CRACKED AT RSS 215.97+3, AT 5 & 12 O' CLOCK. REPAIRED WEB IAW EA.

Part: SPAR — CRACKED (RT WING) · airframe 69,285 hrs · 55,633 cycles

RIGHT WING REAR SPAR WEB CRACKED AT RSS 218 ON TE AT 11 O'CLOCK DIRECTION. REPAIRED WEB IAW EA.

Part: SPAR — CRACKED (RT WING) · airframe 69,285 hrs · 55,633 cycles

RIGHT WING UPPER REAR SPAR WEB CRACKED AT RSS 221.5, ON TE AT 5 O' CLOCK DIRECTION. REPAIRED WEB IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 69,285 hrs · 55,633 cycles

LEFT WING REAR SPAR WEB & LOWER CHORD CRACKED AT RSS 215.97+6, AT 2 & 6 O' CLOCK DIRECTIONS. REPAIRED WEB IAW EA.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 69,285 hrs · 55,633 cycles

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

Part: SPAR — CRACKED (LT WING) · airframe 69,285 hrs · 55,633 cycles

LEFT WING REAR SPAR WEB & LOWER CHORD CRACKED AT RSS 215.97+5, AT 11 O' CLOCK DIRECTION. REPAIRED WEB IAW EA.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 69,285 hrs · 55,633 cycles

LEFT WING INBD AFT FLAP DELAMINATED FROM OTBD EDGE UPPER SKIN. REPAIRED AFT FLAP IAW SRM.

Part: SPAR — CRACKED (LT WING) · airframe 69,285 hrs · 55,633 cycles

LEFT WING REAR SPAR UPPER CHORD CRACKED AT RSS 215.97+3. REPAIRED CHORD IAW EA.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 69,285 hrs · 55,633 cycles

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

Part: PLATE — CRACKED (RT WING) · airframe 69,285 hrs · 55,633 cycles

RIGHT WING TE PLATE CRACKED AT LEVEL WBL 180. R & R PLATE IAW SRM & DWG.

Part: ANGLE — CRACKED (RT WING) · airframe 69,285 hrs · 55,633 cycles

RIGHT WING TE ANGLE CRACKED AT WBL 184.53. R & R ANGLE IAW SRM & DWG.

Part: ANGLE — CRACKED (L1 DOOR) · airframe 69,285 hrs · 55,633 cycles

L1 DOOR CLIP ANGLE CRACKED AT BS 348.5, STRINGER 15L. R & R ANGLE IAW SRM & DWG.

Part: ANGLE — CRACKED (RT WING) · airframe 69,285 hrs · 55,633 cycles

RIGHT WING ANGLE CRACKED ON TE LOCATION WBL. 203 LOWER SURFACE. R & R ANGLE IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,285 hrs · 55,633 cycles

LOWER AFT CORNER OF FWD ENTRY DOOR SKIN CRACKED AT BS 344, STRINGER 16L. REPAIRED SKIN IAW SRM.

Part: SUPPORT FITTING — CRACKED (LT WING) · airframe 69,285 hrs · 55,633 cycles

LEFT WING REAR SPAR MLG AFT SUPPORT FITTING CRACKED ON RSS 215.97+6. REPAIRED FITTING IAW EA.

Part: PLATE — CRACKED (LT WING) · airframe 69,285 hrs · 55,633 cycles

LEFT WING TRAILING PLATE EDGE CRACKED, AT WBL 181.15. R & R PLATE IAW SRM & DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,285 hrs · 55,633 cycles

STRINGER CLIP CRACKED AT BS 277, STRINGER 11R. R & R CLIP IAW SRM & DWG.

Part: LINK ASSY — CORRODED (LT MLG) · airframe 69,285 hrs · 55,633 cycles

LEFT MLG SWING LINK LUG CORRODED. REPAIRED SWING LINK ASSEMBLY IAW CMM.

Part: FITTING — CORRODED (LT WING) · airframe 69,285 hrs · 55,633 cycles

LEFT WING NR 4 FLAP TRACK AFT SUPPORT MAIN LINK FITTING CORRODED. REPAIRED FITTING IAW CMM & EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 69,285 hrs · 55,633 cycles

L1 DOOR AFT LOWER CORNER DOOR CUT OUT ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,285 hrs · 55,633 cycles

SKIN CRACKED AT BS 303, STRINGER 7R. REPAIRED SKIN IAW EA.

Part: FLAP TRACK — CORRODED (TE FLAP) · airframe 69,285 hrs · 55,633 cycles

LEFT WING NR 4 FLAP TRACK CORRODED. REPAIRED FLAP TRACK IAW CMM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 69,285 hrs · 55,633 cycles

ZEE ANGLE CORRODED, BETWEEN BS 951 - 1006, STRINGER 17R. R & R ZEE ANGLE IAW SRM & DWG.

Part: LINK ASSY — CORRODED (RT MLG) · airframe 69,285 hrs · 55,633 cycles

RIGHT MLG SWING LINK LUG CORRODED. REPAIRED SWING LINK ASSEMBLY IAW CMM.

Part: SKIN — CRACKED (LT WING) · airframe 69,285 hrs · 55,633 cycles

LEFT WING INBD LEADING EDGE SKIN CRACKED AT 208.00. REPAIRED SKIN IAW EA.

Part: ANGLE — CRACKED (LT WING) · airframe 69,285 hrs · 55,633 cycles

LEFT WING ANGLE CRACKED AT TE STRUCTURE LOWER SURFACE WBL 203.00. R & R ANGLE IAW SRM.

Part: ANGLE — CRACKED (LT WING) · airframe 69,285 hrs · 55,633 cycles

LEFT WING TE ANGLE CRACKED ON WS 537.806. R & R ANGLE IAW SRM & DWG.

Part: GLOWSTRIP — BROKEN (CABIN) · airframe 69,285 hrs · 55,633 cycles

AFT CABIN PHOTO LUMINESCENT FLOOR PROXIMITY LIGHTING STRIP BROKEN. R & R STRIP IAW AMM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 69,285 hrs · 55,633 cycles

SEAT TRACK AT LONGITUDINAL FLOORBEAM CRACKED AT BS 727B, RBL 24.50, AT CTR WING BOX. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 69,285 hrs · 55,633 cycles

SEAT TRACK AT LONGITUDINAL FLOORBEAM CRACKED AT BS 727B, LBL 24.50, AT CTR WING BOX. REPAIRED SEAT TRACK IAW EA.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 69,285 hrs · 55,633 cycles

MAIN WW COMPARTMENT STIFFENER CRACKED, AT BS 663.75, LBL 6.15, ON FWD BULKHEAD. R & R STIFFENER IAW ACO.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 69,285 hrs · 55,633 cycles

STIFFENER CRACKED AT BS 663.75, RBL 6.15. R & R STIFFENER IAW AC.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 69,285 hrs · 55,633 cycles

CENTER WING BOX LONGITUDINAL FLOORBEAM WEB CRACKED, AT BS 705, LBL 0.07. REPAIRED WEB IAW EA.

Part: COVER — LOOSE (CABIN) · airframe 69,162 hrs · 55,558 cycles

RIGHT OVERWING EMER EXIT LIGHT COVER LOOSE. SECURED COVER IAW SIP.

Part: SPOILER — BROKEN (RT WING) · airframe 68,927 hrs · 55,401 cycles

RIGHT WING NR 5 GND SPOILER, OTBD MAIN ATTACH LUG BROKEN. R & R GND SPOILER IAW MM.

Part: SIGN — LOOSE (CABIN) · airframe 68,409 hrs · 55,058 cycles

RIGHT EMER EXIT SIGN LOOSE. SECURED SIGN IAW SIP.

Part: COVER — LOOSE (EXIT SIGN) · airframe 68,224 hrs · 54,931 cycles

RIGHT OVERWING EMER EXIT SIGN LIGHT, COVER LOOSE. SECURED SIGN IAW SIP.

Part: CABLE — MISROUTED (R2 DOOR) · airframe 67,966 hrs · 54,761 cycles

R2 DOOR EMER EVAC SLIDE CABLE MISROUTED. RE-ROUTED CABLE IAW AMM.

Part: POWER SUPPLY — BROKEN (CABIN) · airframe 67,966 hrs · 54,761 cycles

LEFT CTR EMER BATTERY PACK, FWD MOUNTING SCREW, INSERT BROKEN. R & R POWER SUPPLY IAW AMM.

Part: SIGN — LOOSE (CABIN) · airframe 67,922 hrs · 54,729 cycles

RIGHT OVERWING EXIT SIGN LOOSE. SECURED SIGN IAW EA.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 67,814 hrs · 54,649 cycles

RIGHT EMER BULLNOSE LIGHT INOPERATIVE, BETWEEN ROW 12 - 16. R & R BATTERY CHARGER IAW AMM.

Part: SENSOR — FAULTY (LANDING GEAR) · airframe 67,323 hrs · 54,309 cycles

AIR TURN BACK, DECLARED EMER. ON TAKEOFF AFTER LIFTOFF, LOST BOTH FLIGHT DIRECTORS, UNABLE LNAV OR VNAV. COULD NOT SEQUENCE WAY POINTS IN FMC. COULD NOT SET AIRSPEED ABOVE 187 KTS. CLIMBING THRU FL 230 GOT CABIN ALT WARNING HORN & LIGHT. DESCENDED TO 10,000 FT IN MANUAL & REGAINED CABIN. CABIN REACHED 11,000 FT. ACFT APPEARED TO REMAIN IN GND MODE. FOUND GND SAFETY SENSOR WITH HIGH RESISTANCE. R & R SENSOR IAW MM.

Part: LENS — LOOSE (EXIT SIGN) · airframe 67,299 hrs · 54,287 cycles

RIGHT OVERWING EXIT SIGN LOOSE. R & R LENS IAW MM.

Part: HOOK — BROKEN (R1 DOOR) · airframe 67,293 hrs · 54,282 cycles

R1 DOOR EMER EVAC SLIDE GIRT BAR HOOK BROKEN. R & R SLIDE IAW MM & MT.

Part: TAB — DELAMINATED (LT ELEVATOR) · airframe 67,146 hrs · 54,174 cycles

LEFT ELEVATOR TAB DELAMINATED AT TE. R & R TAB IAW MM.

Part: LENS — LOOSE (CABIN) · airframe 67,056 hrs · 54,114 cycles

RIGHT OVERWING EMER EXIT LENS LOOSE. SECURED LENS IAW MM.

Part: HANDLE — LOOSE (R2 DOOR) · airframe 66,870 hrs · 53,984 cycles

R2 DOOR ASSIST HANDLE LOOSE. SECURED HANDLE IAW MM.

Part: GENERATOR — FAULTY (NR 1 ENGINE) · airframe 66,699 hrs · 53,862 cycles

DIVERSION, DURING TAKEOFF EQUIPMENT COOLING LIGHT, OFF, LIGHT CAME ON. FLIGHT ATTENDANT SMELLED A BAD SMELL IN CABIN. R & R NR 1 ENG GEN IAW MM.

Part: SIGN — BROKEN (CABIN) · airframe 65,171 hrs · 52,815 cycles

L1 DOOR EMER EXIT SIGN BROKEN. R & R LIGHT ASSEMBLY IAW MM.

Part: SKIN — CRACKED (L1 DOOR) · airframe 64,513 hrs · 52,323 cycles

L1 DOOR INNER SKIN CRACKED AT LOWER HINGE BOX. REPAIRED SKIN IAW EA 1-352-1548.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,440 hrs · 52,274 cycles

FORWARD ENTRY GALLEY EMER EXIT LIGHT INOPERATIVE. R & R LIGHT IAW AMM.

Part: STIFFENER — CRACKED (TE FLAP) · airframe 64,440 hrs · 52,274 cycles

LEFT WING NR 3 FLAP TRACK FAIRING TE INTERNAL STRUCTURE INBD SIDE LOWER STIFFENER CRACKED AT WBL 188.40. R & R STIFFENER IAW SRM & DWG.

Part: STIFFENER — CRACKED (TE FLAP) · airframe 64,440 hrs · 52,274 cycles

RIGHT WING NR 6 FLAP TRACK FAIRING TE UPPER STIFFENER CRACKED AT WBL 188.40. R & R STIFFENER IAW SRM & DWG.

Part: STIFFENER — CRACKED (LT WING) · airframe 64,440 hrs · 52,274 cycles

LEFT WING NR 3 TE UPPER STIFFENER CRACKED ON WBL 188.40 INBD SIDE. R & R STIFFENER IAW SRM & DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 64,440 hrs · 52,274 cycles

FLOORBEAM WEB CRACKED AT BS 616 LBL 45.5. REPAIRED WEB IAW EA.

Part: DOOR FRAME — CRACKED (R1 DOOR) · airframe 64,440 hrs · 52,274 cycles

R1 DOOR AFT LATERAL FRAME CRACKED. REPAIRED FRAME IAW EA.

Part: FITTING — CORRODED (GIRT BAR) · airframe 64,440 hrs · 52,274 cycles

L2 DOOR EMER EVAC SLIDE GIRT BAR FITTING CORRODED. R & R FITTING IAW AMM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 64,440 hrs · 52,274 cycles

TIE CLIP CRACKED AT BS 380 STRINGER 21L. R & R TIE CLIP IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,440 hrs · 52,274 cycles

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

Part: WEB — CRACKED (FUSELAGE) · airframe 64,440 hrs · 52,274 cycles

WEB CRACKED AT BS 348.2 STRINGER 16L. R & R WEB IAW SRM & DWG.

Part: RIB — CRACKED (RT WING) · airframe 64,440 hrs · 52,274 cycles

RIGHT WING FUEL IN SPAR RIB WEB CRACKED AT WBL 198.60 STRINGER 5 AT REAR SPAR. REPAIRED WEB IAW EO & EA.

Part: STRUCTURE — CRACKED (LT WING) · airframe 64,440 hrs · 52,274 cycles

LEFT WING LOWER CHORD CRACKED AT WBL 135 BETWEEN STRINGER 2 TO 3. REPAIRED CHORD IAW EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 64,440 hrs · 52,274 cycles

TIE CLIP ANGLE CRACKED AT BS 348.2 STRINGER 15L. R & R ANGLE IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 64,440 hrs · 52,274 cycles

TIE CLIP CRACKED AT BS 380 STR 22L. R & R TIE CLIP IAW SRM & DWG.

Part: PLATE — CRACKED (VERTICAL STAB) · airframe 64,440 hrs · 52,274 cycles

VERTICAL STABILIZER ACCESS PANEL 9506R PLATE CRACKED. R & R PLATE IAW SRM & DWG.

Part: RIB — CRACKED (RT WING) · airframe 64,440 hrs · 52,274 cycles

RIGHT WING RIB UPPER CHORD CRACKED AT WBL 114 STRINGER 2. REPAIRED CHORD IAW EO & EA.

Part: BEARING — CRACKED (RT WING) · airframe 64,440 hrs · 52,274 cycles

RIGHT WING NR 8 A FRAME BEARING CRACKED. R & R BEARING IAW CMM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,440 hrs · 52,274 cycles

FRAME CRACKED AT BS 520 BETWEEN STRINGER 20R TO 21R. REPAIRED FRAME IAW EA.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 64,440 hrs · 52,274 cycles

LEFT NLG WW ALONG THE DOUBLER EDGE CRACKED AT BS 259.5, WL 169.1+7.5. REPAIRED DOUBLER IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,440 hrs · 52,274 cycles

FRAME CRACKED AT BS 492 STRINGER 24R. R & R FRAME IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,440 hrs · 52,274 cycles

SKIN CRACKED AT BS 787+12 STRINGER 25R. REPAIRED SKIN IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,440 hrs · 52,274 cycles

FRAME CRACKED AT BS 492 BETWEEN STRINGER 16R TO 28R. R & R FRAME IAW SRM & DWG.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 64,440 hrs · 52,274 cycles

MAIN WW PRESS DECK CRACKED AT BS 663+9 LBL 40.5. REPAIRED DECK IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,440 hrs · 52,274 cycles

FRAME CRACKED AT BS 520 BETWEEN STRINGER 21R TO 22R. REPAIRED FRAME IAW EA.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 64,440 hrs · 52,274 cycles

MAIN WW PRESS DECK CRACKED AT BS 663+2, LBL 39.5. REPAIRED DECK IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,440 hrs · 52,274 cycles

AFT CARGO COMPARTMENT SKIN CUT OUT CRACKED AT BS 787+12 STRINGER 25R. REPAIRED SKIN IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,440 hrs · 52,274 cycles

FRAME CRACKED AT BS 500B BETWEEN STRINGER 20L TO 21L. REPAIRED FRAME IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 64,440 hrs · 52,274 cycles

FLOORBEAM CHORD CRACKED AT BS 663.75+2 LBL 24.5. REPAIRED CHORD IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,440 hrs · 52,274 cycles

FRAME CRACKED AT BS 500B BETWEEN STRINGER 20L TO 21L. REPAIRED FRAME IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,440 hrs · 52,274 cycles

FRAME CRACKED AT BS 500D BETWEEN STRINGER 20L TO 21L. REPAIRED FRAME IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,440 hrs · 52,274 cycles

FRAME CRACKED AT BS 500B BETWEEN STRINGER 20R TO 21R. REPAIRED FRAME IAW EA.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 64,440 hrs · 52,274 cycles

CENTER SECTION UPPER CHORD CRACKED AT BS 672.5 RBL 24.5. REPAIRED CHORD IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,440 hrs · 52,274 cycles

FRAME CRACKED AT BS 500D BETWEEN STRINGER 20L TO 21L. REPAIRED FRAME IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 64,440 hrs · 52,274 cycles

FLOORBEAM UPPER CHORD CRACKED AT BS 663.75+7 LBL 24.5. REPAIRED CHORD IAW EA.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 64,440 hrs · 52,274 cycles

STRINGER SPLICE CORRODED AT BS 907 STRINGER 18L. R & R SPLICE IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,440 hrs · 52,274 cycles

FRAME STUB BEAM WEB CRACKED AT BS 616 WL 208 AT LEVEL OF INNER CHORD LT SIDE. REPAIRED STUB BEAM IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 64,440 hrs · 52,274 cycles

FLOORBEAM CHORD CRACKED AT BS 663.75+6 LBL 24.5. REPAIRED CHORD IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,440 hrs · 52,274 cycles

FRAME CRACKED AT BS 500D BETWEEN STRINGER 20R TO 21R. REPAIRED FRAME IAW SRM.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 64,440 hrs · 52,274 cycles

CHANNEL CRACKED AT BS 540 BETWEEN BL 0 TO LBL 24.5. R & R CHANNEL IAW SRM.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 64,440 hrs · 52,274 cycles

UPPER CHORD CRACKED AT BS 670 RBL 24.5. REPAIRED CHORD IAW EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 64,440 hrs · 52,274 cycles

INTERCOSTAL CRACKED BETWEEN BS 520 TO 540 BL 0. R & R INTERCOSTAL IAW SRM & DWG.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 64,440 hrs · 52,274 cycles

CHANNEL CRACKED AT BS 540 BETWEEN BL 0 TO RBL 24.5. R & R CHANNEL IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,440 hrs · 52,274 cycles

FRAME OTBD FRAME CHORD CRACKED AT BS 727 STRINGER 18A LT SIDE. REPAIRED CHORD IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,440 hrs · 52,274 cycles

FRAME OTBD CHORD CRACKED AT BS 727 STRINGER 18A RT SIDE. REPAIRED CHORD IAW EA.

Part: LENS — LOOSE (CABIN) · airframe 62,949 hrs · 51,222 cycles

LT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. R & R LIGHT ASSEMBLY IAW MM.

Part: LENS — LOOSE (CABIN) · airframe 62,617 hrs · 51,006 cycles

RT EMERGENCY EXIT LENS COVER LOOSE. SECURED COVER IAW AMM.

Part: FLAP — DELAMINATED (RT WING) · airframe 61,768 hrs · 50,378 cycles

RT WING INBD TE DELAMINATED. R&R AFT FLAP IAW MT.

Part: SENSOR — FAULTY (NR 2 ENGINE) · airframe 61,549 hrs · 50,210 cycles

NR 2 ENGINE WILL NOT REDUCE TO NORMAL FLIGHT IDLE WITH THRUST LEVERS REDUCED TO IDLE POSITION FROM TOP OF DESCENT. NR 2 ENGINE N 1 REMAIN AT 50-55% UNTIL APPROXIMATELY FL250 THEN SLOWLY REDUCES TO NORMAL. FLIGHT IDLE IN REMAINDER DESCENT. R&R NR 2 ENGINE T2 TEMPERATURE SENSOR & CIT SENSOR IAW MM.

Part: SUPPORT FITTING — CORRODED (TE FLAP) · airframe 61,306 hrs · 50,028 cycles

RT WING NR 7 FLAP TRACK, AFT TRACK SUPPORT FITTING CORRODED. R&R FITTING IAW SRM.

Part: FITTING — CORRODED (TE FLAP) · airframe 61,306 hrs · 50,028 cycles

LT WING NR 2 FLAP TRACK AFT ATTACH POINT CORRODED. R&R FITTING IAW SRM.

Part: REGULATOR — FAILED (BLEED AIR SYS) · airframe 60,590 hrs · 49,498 cycles

DECLARED EMERGENCY - AT INITIAL DESCENT FM FL350 CABIN ALT WARNING HORN SOUNDED & CABIN ALT LIGHT CAME ON COULD NOT CONTROL ALT IN AUTO OR MANUAL PER QRH. REMOVED AND REPLACED NR 1 ENGINE BLEED AIR REGULATOR, NR 1 ENGINE PRECOOLER CONTROL VALVE, NR 2 ENGINE HIGH STAGE PRESSURE REGULATOR PER AMM.

Part: SLIDE — LOW PRESSURE (L1 DOOR) · airframe 60,369 hrs · 49,348 cycles

L1 DOOR EMERGENCY EXIT SLIDE PRESSURE LOW. REMOVED AND REPLACED SLIDE IAW MT.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 60,031 hrs · 49,132 cycles

R-2 DOOR GIRT NEEDS RE-INSTALLED, TOO LONG. RE-INSTALLED PER M/M R-2 DOOR SLIDE C/W M/T 325-61-06

Part: LIGHT — INOPERATIVE (CABIN) · airframe 59,080 hrs · 48,452 cycles

RIGHT FORWARD LOWER EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 58,375 hrs · 47,900 cycles

STRINGER CLIP CORRODED AT BS 907, STR 27R. REMOVED AND REPLACED CLIP IAW DWG & SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 58,375 hrs · 47,900 cycles

STRINGER CORRODED AT BS 867+10, STR 26R. REPAIRED STRINGER IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 58,375 hrs · 47,900 cycles

RIGHT "Z" ANGLE CORRODED BETWEEN BS 767 TO BS 787. REMOVED AND REPLACED "Z" ANGLE IAW DWG & SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,375 hrs · 47,900 cycles

FRAME CRACKED AT BS 500C, BETWEEN STR 20L TO STR 21L. REPAIRED FRAME IAW EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 58,375 hrs · 47,900 cycles

SHEAR TIE CORRODED AT BS 500 BETWEEN STRINGERS 26R AND 27R. REMOVED AND REPLACED SHEAR TIE IAW SRM AND DWG.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 58,241 hrs · 47,796 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: HOOK — LOOSE (GIRT BAR) · airframe 58,241 hrs · 47,796 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR HOOKS LOOSE. SECURED HOOKS PER M/M.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 58,145 hrs · 47,726 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,628 hrs · 47,344 cycles

SKIN CRACKED AT BS 639, STR 4L. REPAIRED SKIN IAW SI.

Part: LIGHT — LOOSE (CABIN) · airframe 57,610 hrs · 47,328 cycles

L1 DOOR EMERGENCY EXIT COVER LOOSE. REMOVED AND REPLACED LIGHT ASSY PER M/M.

Part: SHEAR WEB — CRACKED (FUSELAGE) · airframe 57,597 hrs · 47,318 cycles

SHEAR WEB CRACKED BETWEEN BS 616 TO BS 635, LBL. REMOVED AND REPLACED SHEAR WEB IAW DWG.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 57,597 hrs · 47,318 cycles

LT CREASE BEAM CHORD CRACKED AT BS 639. REPAIRED CHORD IAW EA.

Part: FLAP — DELAMINATED (RT WING) · airframe 57,446 hrs · 47,207 cycles

RT WING I/B FORE FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER AMM.

Part: SIGN — INOPERATIVE (CABIN) · airframe 56,594 hrs · 46,598 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT OVERWING EMERGENCY EXIT SIGN LIGHT INOP. RELAMPED SIGN IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,902 hrs · 46,082 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE WINDOW SKIN CRACKED AT BS 400+10, UPPER FORWARD CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,902 hrs · 46,082 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE WINDOW SKIN CRACKED AT BS 440+10, UPPER FORWARD CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,902 hrs · 46,082 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE WINDOW SKIN CRACKED AT BS 500A+10, LOWER AFT CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,902 hrs · 46,082 cycles

DURING SCHEDULED SPV CHECK, FOUND LT WINDOW SKIN CRACKED AT 360+10 AT LOWER AFT CORNER. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,902 hrs · 46,082 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE WINDOW SKIN CRACKED AT BS 420+10, LOWER AFT CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,902 hrs · 46,082 cycles

DURING SCHEDULED SPV CHECK, FOUND RT FUSELAGE WINDOW SKIN CRACKED AT BS 360+10 LOWER AFT CORNER. REPAIRED SKIN IAW.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,902 hrs · 46,082 cycles

DURING SCHEDULED SPV CHECK, FOUND LT FUSELAGE WINDOW SKIN CRACKED AT BS 500A+10 UPPER FORWARD CORNER. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,902 hrs · 46,082 cycles

DURING SCHEDULED SPV CHECK, FOUND RT FUSELAGE WINDOW SKIN CRACKED AT BS 360+10 UPPER FORWARD CORNER. REPAIRED SKIN IAW.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,902 hrs · 46,082 cycles

DURING SCHEDULED SPV CHECK, FOUND LT FUSELAGE WINDOW SKIN CRACKED AT BS 500B+10 UPPER FORWARD CORNER. REPAIRED SKIN IAW EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,902 hrs · 46,082 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,092 hrs · 46,082 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 500B+8, STR 1. REMOVED AND REPLACED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,902 hrs · 46,082 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 5R. REMOVED AND REPLACED CLIP IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,766 hrs · 45,976 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED BETWEEN BS 877 TO BS 878, STR 4R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,766 hrs · 45,976 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED BETWEEN BS 753 TO BS 755, STR 4R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,757 hrs · 45,969 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND SKIN CRACKED AT BS 520+6, STR 28R. REPAIRED SKIN PER SRM.

Part: ACTUATOR — FAULTY (RT MLG DWNLCK) · airframe 55,379 hrs · 45,677 cycles

ON APPROACH , RT MAIN LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE. R/H MAIN LANDING GEAR EXTENDED MANUALLY. R&R RT MLG DOWN LOCK ACTUATOR PER MM.

Part: SIGN — LOOSE (CABIN) · airframe 55,176 hrs · 45,521 cycles

RIGHT OVERWING EXIT SIGN LENS LOOSE. REMOVED AND REPLACED SIGN PER MM.

Part: SIGN — LOOSE (CABIN) · airframe 55,166 hrs · 45,513 cycles

LT OVERWING EXIT SIGN LOOSE. SECURE SIGN PER EA.

Part: PUMP — FAULTY (NR 1 ENGINE) · airframe 54,948 hrs · 45,351 cycles

INFLIGHT SHUTDOWN / DIVERSION / DECLARED EMERGENCY. WHILE CRUISING AT FL 350, THE NR 1 ENGINE FLAMED OUT. ALL ENGINE FULE PUMPS WERE ON AT THE TIME AND THE CROSSFEED VALVED WAS CLOSED. DESCENDED TO FL 230 WHERE WINDMILL AIRSTART WAS SUCCESSFUL. REMOVED AND REPLACED NR 1 ENGINE FUEL PUMP, MEC, AND FUEL CROSSFEED VALVE ACTUATOR PER MM.

Part: SIGN — LOOSE (CABIN) · airframe 54,873 hrs · 45,300 cycles

DURING SCHEDULED CV CHECK, FOUND OVERHEAD EMERGENCY EXIT SIGN LOOSE AT ROW 22. SECURED SIGN PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,738 hrs · 45,198 cycles

DURING SCHEDULED MV1 CHECK, FOUND RT EEPLS INOP AT ROW 8. RELAMPED PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,731 hrs · 45,191 cycles

DURING SCHEDULED MV2 CHECK, FOUND OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT INOP AT ROW 16. REMOVED AND REPLACED LIGHT PER MM.

Part: LENS — LOOSE (CABIN) · airframe 54,676 hrs · 45,145 cycles

L1 EMERGENCY LIGHT LENS LOOSE. SECURED EMERGENCY LIGHT LENS PER MM.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 53,969 hrs · 44,597 cycles

DURING SCHEDULED OTS CHECK, FOUND LT MLG PRESSURE DECK WEB CRACKED AT BS 664, LBL 35. REPAIRED WEB PER SRM.

Part: PRESSURE PANEL — CRACKED (LT MLG) · airframe 53,966 hrs · 44,596 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND LT MLG WHEEL WELL PRESSURE DECK WEB CRACKED AT BS 540, LBL 35. REPAIRED WEB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,142 hrs · 43,961 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED AT BS 510C LOWER AFT CORNER OF RT PAX WINDOW. REPAIRED SKIN PER EA.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 53,142 hrs · 43,961 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 795, STR 26R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 53,142 hrs · 43,961 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 747, BETWEEN STR 26L TO STR 27L. REPAIRED FRAME PER SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 53,142 hrs · 43,961 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO CHANNEL CORRODED AT BS 859, LBL 12.50. REPAIRED CHANNEL PER EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 53,142 hrs · 43,961 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO CHANNEL CORRODED BETWEEN BS 727C TO BS 727D, LBL 8.10. REPAIRED CHANNEL.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,142 hrs · 43,961 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED AT BS 390 LT LOWER AFT CORNER OF PAX WINDOW. REPAIRED SKIN PER EO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,142 hrs · 43,961 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 235.8, BETWEEN LBL 20 TO LBL 50. REPAIRED FRAME PER EO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,142 hrs · 43,961 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED AT BS 737.5E, STR 4L. REPAIRED SKIN PER EO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,142 hrs · 43,961 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED AT BS 450 RT UPPER FWD CORNER OF PAX WINDOW. REPAIRED SKIN PER EO.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 53,142 hrs · 43,961 cycles

DURING SCHEDULED 16Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 727B, LBL 45.5. REPAIRED BEAM PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,142 hrs · 43,961 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED AT BS 737 RT UPPER AFT CORNER OF PAX WINDOW. REPAIRED SKIN PER EO.

Part: BEAM — CORRODED (FUSELAGE) · airframe 53,142 hrs · 43,961 cycles

DURING SCHEDULED 16Y CHECK, FOUND BEAM CORRODED AT BS 947, LBL 53.5. REPAIRED BEAM PER EO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,142 hrs · 43,961 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED AT BS 797 LT UPPER AFT CORNER OF PAX WINDOW. REPAIRED SKIN PER EO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,142 hrs · 43,961 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED AT BS 510 RT LOWER AFT CORNER OF PAX WINDOW. REPAIRED SKIN PER EO.

Part: FRAME — CORRODED (FUSELAGE) · airframe 53,142 hrs · 43,961 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 787, BETWEEN STR 26R TO STR 27R. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,142 hrs · 43,961 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED AT BS 510 RT UPPER FWD CORNER OF PAX WINDOW. REPAIRED SKIN PER EO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,142 hrs · 43,961 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED AT BS 450 RT LOWER AFT CORNER OF PAX WINDOW. REPAIRED SKIN PER EO.

Part: FRAME — CORRODED (FUSELAGE) · airframe 53,142 hrs · 43,961 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 807, STR 27L. REPAIRED FRAME PER SRM.

Part: BEAM — CORRODED (FUSELAGE) · airframe 53,142 hrs · 43,961 cycles

DURING SCHEDULED 16Y CHECK, FOUND BEAM CORRODED AT BS 947, BETWEEN RBL 12 TO LBL 12. REPAIRED BEAM PER EO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,142 hrs · 43,961 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED AT BS 857 RT UPPER AFT CORNER OF PAX WINDOW. REPAIRED SKIN PER EO.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 53,142 hrs · 43,961 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO CHANNEL CORRODED AT BS 859, RBL 3. REPAIRED CHANNEL PER EA.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 53,142 hrs · 43,961 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT WING AFT FLAP LOWER SKIN I/B EDGE OF O/B FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 53,142 hrs · 43,961 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER SPLICE CORRODED AT BS 907, STR 25L. REMOVED AND REPLACED SPLICE PER SRM AND BAC DWG.

Part: SKIN — CRACKED (LE SLAT) · airframe 53,142 hrs · 43,961 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING NR 3 SLAT L/E SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,142 hrs · 43,961 cycles

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

Part: CHANNEL — CORRODED (CARGO BAY) · airframe 53,142 hrs · 43,961 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO CHANNEL CORRODED AT BS 927, RBL 8.10. REPAIRED CHANNEL PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,142 hrs · 43,961 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED AT BS 530 RT LOWER FWD CORNER OF PAX WINDOW. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,142 hrs · 43,961 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED AT BS 510C RT UPPER FWD CORNER OF PAX WINDOW. REPAIRED SKIN PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 53,142 hrs · 43,961 cycles

DURING SCHEDULED 16Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 727B, RBL 25.8. REPAIRED BEAM PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,142 hrs · 43,961 cycles

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

Part: CHANNEL — CORRODED (CARGO BAY) · airframe 53,142 hrs · 43,961 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO CHANNEL CORRODED AT BS 927, LBL 12.5. REPAIRED CHANNEL PER SWA EA.

Part: CHANNEL — CORRODED (CARGO BAY) · airframe 53,142 hrs · 43,961 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO CHANNEL CORRODED BETWEEN BS 727 TO BS 727D, RBL 3. REPAIRED CHANNEL PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,142 hrs · 43,961 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 947.5, STR 25R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 53,142 hrs · 43,961 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING NR 2 SLAT O/B EDGE DELAMINATED. REMOVED AND REPLACED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,142 hrs · 43,961 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 21L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 53,142 hrs · 43,961 cycles

DURING SCHEDULED 16Y CHECK, FOUND SUPPORT ANGLE CRACKED AT BS 540, STR 22R. REMOVED AND REPLACED ANGLE PER SRM AND BAD DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,142 hrs · 43,961 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 1121, STR 2L. REMOVED AND REPLACED CLIP PER SRM AND BAD DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 53,142 hrs · 43,961 cycles

DURING SCHEDULED 16Y CHECK, FOUND SUPPORT ANGLE CRACKED AT BS 540, STR 22L. REMOVED AND REPLACED ANGLE PER SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 53,142 hrs · 43,961 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING NR 2 SLAT L/E LOWER SURFACE CRACKED. REPAIRED SLAT PER SRM.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 53,142 hrs · 43,961 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING NR 2 SLAT LOWER SURFACE I/B EDGE DELAMINATED. REPAIRED SLAT PER SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 53,142 hrs · 43,961 cycles

DURING SCHEDULED 16Y CHECK, FOUND SUPPORT ANGLE CRACKED AT BS 706, STR 11R. REMOVED AND REPLACED ANGLE PER SRM AND BAC DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 53,142 hrs · 43,961 cycles

DURING SCHEDULED 16Y CHECK, FOUND VERTICAL SUPPORT ANGLE CRACKED AT BS 693, LBL 25.5. REMOVED AND REPLACED ANGLE PER SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 53,142 hrs · 43,961 cycles

DURING SCHEDULED 16Y CHECK, FOUND VERTICAL SUPPORT ANGLE CRACKED AT BS 639, RBL 45.5. REMOVED AND REPLACED ANGLE PER SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 53,142 hrs · 43,961 cycles

DURING SCHEDULED 16Y CHECK, FOUND VERTICAL SUPPORT ANGLE CRACKED AT BS 693, RBL 25.5. REMOVED AND REPLACED ANGLE PER SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,142 hrs · 43,961 cycles

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

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 53,142 hrs · 43,961 cycles

DURING SCHEDULED 16Y CHECK, FOUND SUPPORT ANGLE CRACKED AT BS 706, STR 13L. REMOVED AND REPLACED ANGLE PER SRM AND BAC DWG.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 53,142 hrs · 43,961 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT WING T/E SUPPORT ANGLE CRACKED AT WBL 85. REMOVED AND REPLACED ANGLE PER SRM AND DWG.

Part: LENS — BROKEN (CABIN) · airframe 53,142 hrs · 43,961 cycles

DURING SCHEDULED 16Y CHECK, FOUND FWD GALLEY EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 53,142 hrs · 43,961 cycles

DURING SCHEDULED 16Y CHECK, FOUND VERTICAL SUPPORT ANGLE CRACKED AT BS 639, LBL 45.5. REMOVED AND REPLACED ANGLE PER SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 53,142 hrs · 43,961 cycles

DURING SCHEDULED 16Y CHECK, FOUND SUPPORT ANGLE CRACKED AT BS 706, STR 13R. REMOVED AND REPLACED ANGLE PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,142 hrs · 43,961 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 10R. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 53,142 hrs · 43,961 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME SUPPORT ANGLE CRACKED AT BS 360, STR 11L. REMOVED AND REPLACED ANGLE PER SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 53,142 hrs · 43,961 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME SUPPORT ANGLE CRACKED AT BS 360, STR 9L. REMOVED AND REPLACED ANGLE PER SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,142 hrs · 43,961 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 21L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,142 hrs · 43,961 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 4L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 53,142 hrs · 43,961 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CRACKED AT BS 727B, STR 6L. REMOVED AND REPLACED STRINGER PER SRM AND BAC DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 53,142 hrs · 43,961 cycles

DURING SCHEDULED 16Y CHECK, FOUND SUPPORT ANGLE CRACKED AT BS 685, STR 13L. REMOVED AND REPLACED ANGLE PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,142 hrs · 43,961 cycles

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

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 53,142 hrs · 43,961 cycles

DURING SCHEDULED 16Y CHECK, FOUND SUPPORT ANGLE CRACKED AT BS 685, STR 11L. REMOVED AND REPLACED ANGLE PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,142 hrs · 43,961 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 26R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,142 hrs · 43,961 cycles

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

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 53,142 hrs · 43,961 cycles

DURING SCHEDULED 16Y CHECK, FOUND CROSS FLOORBEAM CORRODED AT BS 986.5, BETWEEN RBL 52 TO LBL 52. REPAIRED BEAM PER TI.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 53,142 hrs · 43,961 cycles

DURING SCHEDULED 16Y CHECK, FOUND SUPPORT ANGLE CRACKED AT BS 597, STR 11L. REMOVED AND REPLACED ANGLE PER BAC DWG AND SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 53,142 hrs · 43,961 cycles

DURING SCHEDULED 16Y CHECK, FOUND SUPPORT ANGLE CRACKED AT BS 847, BETWEEN STR 2R TO STR 2L. REMOVED AND REPLACED ANGLE PER BAC DWG AND SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,142 hrs · 43,961 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 16L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,142 hrs · 43,961 cycles

DURING SCHEDULED 16Y CHECK, FOUND SUPPORT ANGLE CRACKED AT BS 597, STR 11R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,142 hrs · 43,961 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 667, STR 10R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,142 hrs · 43,961 cycles

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

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 53,142 hrs · 43,961 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CORRODED AT BS 312, BETWEEN BBL 0 TO LBL 21. REPAIRED BEAM PER TI.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 53,142 hrs · 43,961 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CORRODED AT BS 312, RBL 7.5. REPAIRED BEAM PER TI.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 53,142 hrs · 43,961 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CORRODED AT BS 328, LBL 49. REPAIRED BEAM PER TI.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,142 hrs · 43,961 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,782 hrs · 43,685 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 508B, STR 1. REPAIRED SKIN PER SRM.

Part: LENS — LOOSE (CABIN) · airframe 52,582 hrs · 43,531 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT OVERWING EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED EXIT LIGHT HOUSING AND LENS PER MM.

Part: SIGN — LOOSE (CABIN) · airframe 51,818 hrs · 42,960 cycles

L2 DOOR EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 50,821 hrs · 42,243 cycles

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

Part: BEAM — CORRODED (LT MLG) · airframe 50,339 hrs · 41,882 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT MLG SUPPORT BEAM CORRODED. REMOVED AND REPLACED BEAM PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,285 hrs · 41,109 cycles

DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT BS 1004, STR 5R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,801 hrs · 40,064 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 47,572 hrs · 39,892 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT WING O/B AFT FLAP DELAMINATED AT I/B FWD SIDE. REMOVED AND REPLACED FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,572 hrs · 39,892 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,600 hrs · 39,914 cycles

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

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 47,396 hrs · 39,759 cycles

DURING SCHEDULED 14Y CHECK, FOUND FWD CARGO SHEAR TIE CORRODED AT BS 360, LBL 10. REMOVED AND REPLACED TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,396 hrs · 39,759 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 16L. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 47,396 hrs · 39,759 cycles

DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CRACKED AT STA 540, LBL 40, WL 206. REPAIR SHEAR TIME PER SRM.

Part: GLOWSTRIP — WORN (CABIN) · airframe 47,396 hrs · 39,759 cycles

DURING SCHEDULED 14Y CHECK, FOUND EMERGENCY EVACUATION PHOTOLUMINESCENT STRIPS WORN IN CABIN. REMOVED AND REPLACED STRIPS PER AMM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 47,396 hrs · 39,759 cycles

DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 7R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SPOILER — CRACKED (RT WING) · airframe 47,396 hrs · 39,759 cycles

DURING SCHEDULED 14Y CHECK, FOUND RT WING NR 5 SPOILER CRACKED AT OUTBOARD ATTACH FITTING. REMOVED AND REPLACED NR 5 SPOILER PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,396 hrs · 39,759 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,396 hrs · 39,759 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 480 S7R) · airframe 47,396 hrs · 39,759 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 480, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 480 S8R) · airframe 47,396 hrs · 39,759 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 480, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SLAT — DELAMINATED (RT WING) · airframe 46,047 hrs · 38,781 cycles

DURING SCHEDULED HC2 CHECK, FOUND RIGHT WING NR 5 L/E SLAT DELAMINATED AT OUTBOARD T/E. REMOVED AND REPLACED SLAT PER MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 45,904 hrs · 38,678 cycles

RIGHT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD T/E. REMOVED AND REPLACED FLAP PER MM.

Part: LENS — LOOSE (CABIN) · airframe 44,295 hrs · 37,437 cycles

DURING SCHEDULED HC1 CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 44,285 hrs · 37,431 cycles

DURING SCHEDULED HC1 CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 42,783 hrs · 36,226 cycles

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

Part: STRINGER CLIP — CRACKED (BS 360 S11L) · airframe 42,469 hrs · 35,977 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 360 S8L) · airframe 42,469 hrs · 35,977 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 42,151 hrs · 35,731 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR CUTOUT FWD LOWER CORNER. REPAIRED SKIN PER SRM.

Part: GLOWSTRIP — WORN (CABIN) · airframe 42,151 hrs · 35,731 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN BETWEEN ROW 3 DEF AND 5 DEF. REMOVED AND REPLACED STRIP PER MM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 41,023 hrs · 34,874 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD CARGO DOOR CUTOUT AFT FRAME CRAKCED AT NR 5 DOOR STOP. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 41,023 hrs · 34,874 cycles

DURING SCHEDULED SPV CHECK, FOUND AFT CARGO DOOR CUTOUT FWD FRAME CRACKED AT NR 5 DOOR STOP. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: STRINGER — CRACKED (BS 480 S28R) · airframe 41,023 hrs · 34,874 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 28R CRACKED AT BS 480. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 40,748 hrs · 34,641 cycles

DURING SCHEDULED A1 CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT INOP AT ROW 23 DEF. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 38,400 hrs · 32,844 cycles

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

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 38,366 hrs · 32,820 cycles

DURING SCHEDULED C3 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 38,101 hrs · 32,588 cycles

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

Part: SKIN — CRACKED (BS 379) · airframe 37,376 hrs · 32,015 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 379, STR 27L. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 36,442 hrs · 31,232 cycles

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

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 36,205 hrs · 31,027 cycles

L2 DOOR EMERGENCY EXIT SIDE LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: BUTTON — STUCK (ESCAPE ROPE) · airframe 35,301 hrs · 30,299 cycles

CAPTAIN'S EMERGENCY ESCAPE ROPE DOOR BUTTON STUCK. ADJUSTED AND LUBED BUTTON PER MM.

Part: BUTTON — STUCK (ESCAPE ROPE) · airframe 34,919 hrs · 30,021 cycles

CAPTAIN'S EMERGENCY ESCAPE ROPE DOOR BUTTON STUCK. LUBED AND ADJUSTED BUTTON PER MM.

Part: FAN — FAULTY (E&E BAY) · airframe 34,454 hrs · 29,653 cycles

APPROX 8 MINUTES BEFORE LANDING PAX REPORTED SMELLED SMOKE. AFTER ENGINE SHUTDOWN AT THE GATE SMELL GOT WORSE, IT WAS A STRONG ACRID SMELL. REMOVED AND REPLACED GASPER FAN PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,077 hrs · 29,330 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 616, RBL 65, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM, TI-153-018.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 34,077 hrs · 29,330 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 328, LBL 28 TO RBL 36, CORRODED. REMOVED AND REPLACED FLOORBEAM SECTION PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 34,077 hrs · 29,330 cycles

DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB AT BS 465, RBL 70, TO BS 865, RBL 65, BS 817 TO BS 865 LBL 65, CORRODED. REMOVED AND REPLACED CREASE BEAM WEB SECTIONS PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 34,077 hrs · 29,330 cycles

DURING SCHEDULED D-CHECK, FOUND FLOOR WEB AT BS 178 TO BS 196.5, LBL 24 TO LBL 28, CRACKED. REMOVED AND REPLACED FLOOR WEB SECTION PER SRM.

Part: FRAME — CRACKED (BS 787) · airframe 34,077 hrs · 29,330 cycles

DURING SCHEDULED D CHECK, FOUND FRAME AT BS 787, STRINGER 8L, CRACKED. REPAIRED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,077 hrs · 29,330 cycles

DURING SCHEDULED D-CHECK, FOUND FRAMES AT BS 188, RBL 30 AND BS 188, LBL 30, CRACKED. REPAIRED FRAME SECTIONS PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,077 hrs · 29,330 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 747, STRINGERS 8L & 8R, CRACKED. REPAIRED FRAME SECTIONS PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,077 hrs · 29,330 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME SECTION AT BS 727D, STRINGERS 8L & 8R, CRACKED. REPAIRED FRAME SECTIONS PER SRM.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 34,077 hrs · 29,330 cycles

DURING SCHEDULED D-CHECK, FOUND RIGHT HORIZONTAL STAB LOWER RIB CHORD AT STATION 120.30, CRACKED. REMOVED AND REPLACED LOWER RIB CHORD PER SRM, BAC DRAWING.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 24,077 hrs · 29,330 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE LT CREASE BEAM CORRODED AT BS 877. REPAIRED CREASE BEAM PER SRM.

Part: FRAME — CRACKED (L1 DOOR CUTOUT) · airframe 24,077 hrs · 29,330 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 303.9, WL 212, LBL 58. REPAIRED FRAME PER SRM & BOEING S/B.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 34,077 hrs · 29,330 cycles

DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB AT BS 407, RBL 70 CORRODED. REMOVED AND REPLACED CREASE BEAM SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,077 hrs · 29,330 cycles

DURING SCHEDULED D-CHECK, FOUND FRAMES AT BS 480, STRINGERS 8L & 8R, CRACKED. REPAIRED FRAME SECTIONS PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,077 hrs · 29,330 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,077 hrs · 29,330 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 500A, STRINGER 8L, CRACKED. REPAIRED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (BS 400) · airframe 34,077 hrs · 29,330 cycles

DURING SCHEDULED D CHECK, FOUND FRAME AT BS 400 , STRINGER 8L AND STRINGER 8R, CRACKED. REPAIRED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,077 hrs · 29,330 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 616, LBL 65, WL 202, CRACKED. REMOVED AND REPLACED FRAME SECTION PER TI-153-018.

Part: CABLE — MISROUTED (EVAC SLIDE) · airframe 30,166 hrs · 26,243 cycles

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

Part: SLIDE — OUT OF ADJUST (ENTRY DOOR) · airframe 30,166 hrs · 26,243 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (FWD CABIN DOORS) · airframe 29,212 hrs · 25,487 cycles

DURING SCHEDULED C1 CHECK, FOUND BOTH FWD CABIN DOOR EMERGENCY EVAC SLIDE ASSY'S OUT OF ADJUST. ADJUSTED SLIDE ASSY'S PER MM.

Part: CABLE — MISROUTED (AFT ENTRY DOOR) · airframe 28,274 hrs · 24,766 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY CABLE MISROUTED. REROUTED CABLE PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 28,031 hrs · 24,577 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER WHEN OPENING THE DOOR. REMOVED AND REPLACED SLIDE PER MM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 27,365 hrs · 24,033 cycles

DURING SCHEDULED C3 CHECK, FOUND LT HORIZ STAB CRACKED ON LOWER SKIN AT AFT SPAR, 6 FT FROM ROOT. REPAIRED SKIN PER SRM.

Part: HYDRAULIC LINE — LEAKING (HYD SYSTEM) · airframe 26,890 hrs · 23,629 cycles

AIR TURNBACK, B-SYSTEM HYDRAULIC FAILURE AFTER TAKEOFF. REMOVED AND REPLACED HYD PRESS LINE BETWEEN B-ELEC PUMP AND B-SYSTEM MODULE PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 26,522 hrs · 23,320 cycles

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

Part: CONNECTOR — ERRATIC (NR 1 ENG) · airframe 26,188 hrs · 23,051 cycles

AIR TURNBACK, ENG SHUTDOWN, DECLARED EMERGENCY ON TAKEOFF NR 1 ENG EGT INDICATED 1290 DEGREES, COULD NOT STABILIZE ENG, SHUT ENG DOWN. DISCREPANCY WAS DETERMINNED TO BE AN INDICATION PROBLEM. REMOVED AND REPLACED ENG EGT WIRE CONNECTOR PER MM.

Part: FLOORBEAM — CORRODED (AFT CARGO) · airframe 25,760 hrs · 22,726 cycles

DURING SCHEDULED 1/4D CHECK, FOUND LONGITUDINAL FLOORBEAMS CORRODED AT BS 847 AND LBL 8, BS 812 AND RBL 3, BS 847 AND LBL 3. REPAIRED FLOORBEAM PER SWA RA.

Part: ELEVATOR — DELAMINATED (RH ELEVATOR) · airframe 25,760 hrs · 22,726 cycles

DURING SCHEDULED 1/4D CHECK, FOUND RT ELEVATOR DELAMINATED INBD OF T/E. REPAIRED ELEVATOR PER SRM.

Part: LENS — LOOSE (CABIN) · airframe 25,760 hrs · 22,726 cycles

DURING SCHEDULED 1/4D CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT LENS LOOSE IN AFT CABIN. SECURED LENS PER MM.

Part: LENS — LOOSE (CABIN) · airframe 25,760 hrs · 22,726 cycles

DURING SCHEDULED 1/4D CHECK, FOUND EMERGENCY EXIT LIGHT LENS LOOSE AT FWD ENTRY LOWER LAV WALL. REMOVED AND REPLACED LENS PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 25,730 hrs · 22,700 cycles

EEPLS LOOSE AT ROW 15. SECURED EEPLS PER MM.

Part: GIRT BAR — OUT OF ADJ (AFT ENTRY DOOR) · airframe 25,426 hrs · 22,461 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED GIRT ASSY PER MM.

Part: WIRE — DISCONNECTED (CABIN) · airframe 25,356 hrs · 22,405 cycles

EEPLS INOP AT SEVERAL AREAS IN CABIN. RECONNECTED WIRES PER MM.

Part: COVER — LOOSE (CABIN FLOOR) · airframe 25,216 hrs · 22,284 cycles

EEPLS TRACK COVERS LOOSE AT ROWS 13 TO 15. SECURED TRACK COVERS PER MM.

Part: COVER — LOOSE (CABIN) · airframe 25,210 hrs · 22,277 cycles

EEPLS TRACK COVERS LOOSE. REINSTALLED COVERS PER MM.

Part: LIGHT — NOT SEATED (CABIN) · airframe 25,190 hrs · 22,263 cycles

EEPLS INOP FROM ROW 12 AFT. RESEATED LIGHT ASSY'S AND BATTERY PACK. OPS CK GOOD PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 25,190 hrs · 22,263 cycles

EEPLS DIM BETWEEN ROWS 10 TO 14. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,173 hrs · 22,246 cycles

EEPLS INOP AT REAR SECTION. REPAIRED EEPLS PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 25,141 hrs · 22,221 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP AT AFT SECTION. REMOVED AND REPLACED BATTERY POWER SUPPLY PER MM.

Part: WIRE — EXPOSED (CABIN) · airframe 25,073 hrs · 22,166 cycles

EEPLS IS LOOSE AND WIRES EXPOSED AT ROW 15. SECURED EEPLS PER MM.

Part: WIRE — DAMAGED (CABIN) · airframe 24,674 hrs · 21,837 cycles

EEPLS INOP BETWEEN ROWS 13-22. REPAIRED EEPLS WIRING AND RELAMPED PER MM.

Part: COVER — CRACKED (CABIN) · airframe 34,482 hrs · 21,687 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS COVER CRACKED AT ROW 17. R&R EEPLS COVER PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,482 hrs · 21,687 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS INOP AT AFT CABIN. RELAMPED EEPLS PER MM.

Part: WIRE — DISCONNECTED (CABIN) · airframe 23,856 hrs · 21,162 cycles

EEPLS LOOSE AND INOP BETWEEN ROWS 13 TO 23. RECONNECTED WIRES AND SECURED EEPLS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,793 hrs · 21,099 cycles

EEPLS INOP FROM ROW 15 TO ROW 22. REPAIRED EEPLS PER MM.

Part: WIRE — LOOSE (CABIN) · airframe 23,738 hrs · 21,052 cycles

EEPLS WIRES LOOSE. RECONNECTED EEPLS WIRES PER MM.

Part: COVER — MISSING (CABIN) · airframe 23,702 hrs · 21,016 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS COVER MISSING AT ROW 18. INSTALLED EEPLS COVER PER MM.

Part: WIRE — DISCONNECTED (CABIN) · airframe 23,693 hrs · 21,007 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP AT ROWS 12 & 13. RECONNECTED WIRE PER MM.

Part: COVER — MISSING (CABIN FLOOR) · airframe 23,537 hrs · 20,872 cycles

EEPLS COVERS MISSING AT ROW 12 THRU ROW 14. INSTALLED COVERS PER MM.

Part: WIRE — LOOSE (CABIN) · airframe 23,326 hrs · 20,709 cycles

EEPLS WIRES LOOSE AT ROW 17. SECURED EEPLS WIRES PER MM.

Part: WIRE — EXPOSED (CABIN) · airframe 23,326 hrs · 20,709 cycles

EEPLS WIRES EXPOSED AT ROW 17. SECURED EEPLS WIRES PER MM.

Part: SLIDE — LOOSE (SERVICE DOOR) · airframe 22,895 hrs · 20,349 cycles

FWD SVC DOOR EMERGENCY EVAC SLIDE LOOSE. RESECURED EVAC SLIDE CASE TO DOOR PER MM.

Part: COVER — MISSING (CABIN) · airframe 22,722 hrs · 20,223 cycles

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

Part: COVER — LOOSE (CABIN) · airframe 22,617 hrs · 20,129 cycles

EEPLS TRACK COVER LOOSE AT ROW 18. REPAIRED EEPLS WIRING AND SECURED TRACK COVERS PER MM.

Part: COVER — LOOSE (CABIN) · airframe 22,602 hrs · 20,115 cycles

EEPLS LOOSE AT ROW 16. SECURED EEPLS TRACK COVER PER MM.

Part: COVER — MISSING (CABIN) · airframe 22,551 hrs · 20,075 cycles

EEPLS TRACK COVERS MISSING AT ROWS 14 & 15. INSTALLED TRACK COVERS PER MM.

Part: GASPER FAN — DEFECTIVE (CABIN) · airframe 22,341 hrs · 19,896 cycles

SMOKE ODOR IN CABIN. GASPER AND RECIRCULATION FAN TURNED OFF AND ODOR WENT AWAY. ODOR STRONGEST AT MID CABIN. REMOVED AND REPLACED GASPER FAN MOTOR ASSY PER MM.

Part: COVER — MISSING (CABIN FLOOR) · airframe 21,915 hrs · 19,550 cycles

EEPLS TRACK COVER MISSING AT ROW 2. REPLACED TRACK COVER PER MM.

Part: LIGHT — DISCONNECTED (CABIN FLOOR) · airframe 21,857 hrs · 19,500 cycles

EEPLS INOP. CONNECTED EEPLS WIRING. OPS CK GOOD PER MM.

Part: LENS — MISSING (CABIN) · airframe 21,666 hrs · 19,347 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS LENS MISSING AT AFT END OF TRACK. REPLACED TRACK COVER PER MM.

Part: FLOORBEAM — CORRODED (BS 986)

DURING SCHEDULED 1/2D CHECK, FOUND CORROSION ON BS 986 FLOORBEAM, RBL 20 - RBL 40. REPAIRED BEAM PER ER 99-6080 AND SRM.

Part: SKIN — CRACKED (FUSELAGE)

DURING SCHEDULED 1/2D CHECK, FOUND CRACKED FUSELAGE SKIN, FWD SERVICE DOOR LOWER HINGE CUT OUT. REPAIRED SKIN PER ER NR 99-6084A.

Part: FLOORBEAM — CORRODED (BS 947.5)

DURING SCHEDULED 1/2D CHECK, FOUND BS 947.5 UPPER CHORD OF FLOORBEAM CORRODED, LBL 20.75. REPAIRED FLOORBEAM PER SRM.

Part: COVER — MISSING (CABIN)

EEPLS LIGHTS HAS EXPOSED WIRES BY OVERWING EXITS. INSTALLED TRACK COVER PER MM.

Part: CONNECTOR — BROKEN (ROW 11-15)

DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY ESCAPE FLOOR TRACK LIGHT INOP BETWEEN ROWS 11-15. REPAIRED WIRING CONNECTION PER MM.

Part: WHEEL — VIBRATION (NLG)

ON TAKEOFF ROLL FROM PHX AT APPROXIMATELY 130-165 KNTS, SIGNIFICANT LATERAL MOVEMENT FROM CENTER LINE WAS ENCOUNTERED. NO SHIMMY BUT DIRECTIONAL CONTROL WAS VERY DIFFICULT, RAPID AND EXTREME RUDDER INPUTS WERE NECESSARY FOR CONTROL. REMOVED AND REPLACED NOSE TIRE/WHEEL ASSY PER MM.

Part: SLIDE — DETERIORATED (SERVICE DOOR)

DURING SCHEDULED BC3 CHECK, FOUND AFT SERVICE DOOR EVACUATION SLIDE STRAP DETERIORATED. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: TARGET — OUT OF ADJUST (CARGO DOOR)

AIR TURNBACK DUE TO FWD CARGO LIGHT ILLUMINATED ON ROTATION. AIRCRAFT MADE AN UNEVENTFUL LANDING. FOUND TARGET OUT OF ADJUSTMENT, RE-ALIGNED TARGET PER BOEING MM. OPS CHECK OK. (LP 87022)

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY FWD ENTRY SLIDE SINGLE LIGHT INOP. SLIDE (P/N 61620-468) (S/N 0712A) REPAIRED PER BOEING MM.

Part: ENGINE — FAILED (NR 2)

DURING CLIMBOUT THROUGH 6,000 FT, NOTED A STRONG HYD TYPE SMELL IN COCKPIT. SHUT OFF GASPER FAN, BUT ODOR PERSISTED. AIRCRAFT RETURNED TO PHX AND MADE AN UNEVENTFUL LANDING. REPLACED NUMBER 2 ENGINE PER BOEING M/M.

Part: SKIN — DENTED (BS 915)

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE GOUGED AND DENTED AT BS 915 AT STRINGER S21L. REPAIRED PER BOEING SRM.

Part: FAN BLADES — BENT (NR 2 ENGINE)

ON TAKEOFF, EXPERIENCED BIRDSTRIKE TO NR 2 ENGINE CAUSING VIBRATION. AIRCRAFT RETURNED TO SFO AND MADE AN UNEVENTFUL LANDING. PERFORMED BIRDSTRIKE INSPECTION AND FOUND TWO ENGINE FAN BLADES BENT. REPLACED BLADES AND PERFORMED ENGINE POWER ASSURANCE RUN PER BOEING M/M.