N700GS

Part: WEB — CORRODED (FUSELAGE) · airframe 74,366 hrs · 45,407 cycles

FWD CARGO THRESHOLD AREA HAS LARGE AREA OF CORROSION. R&R WEB AT FWD CARGO DOOR CUT OUT AS PER SRM & DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 74,366 hrs · 45,407 cycles

AFT CARGO COMPARTMENT INTERCOSTAL WEB CORRODED AT BS. 727 STR. 27R. R&R INTERCOSTAL IAW SRM AND DWG.

Part: PROXIMITY SENSOR — FAULTY (LE SLAT) · airframe 74,358 hrs · 45,401 cycles

AIR TURNBACK, ON DEPARTURE AND UPON RETRACTING FLAPS LEADING EDGE FLAP TRANIST ILLUMINATED INTERMITTANTLY AND THEN FULL STEADY AFTER APPROXIMATELY 2 MINUTES. ACCOMPANIED BY LEADING EDGE FLAP 2 INDICATING FULL EXTEND. MINIMAL ROLL NOTED INFLIGHT. LEADING EDGE TRANSITON AND LEADING EDGE FLAP 2 INDICATED FULL EXTEND WITH FLAP HANDLE IN UP POSITION AT GATE. R&R #2 K-FLAP PROXIMITY SENSOR PER AMM.

Part: SUPPORT ANGLE — CRACKED (RT WING FAIRING) · airframe 74,038 hrs · 45,193 cycles

AFT R/H WING TO BODY FAIRING PANEL #194 CR-INBOARD VERTICAL SUPPORT ANGLE CRACKED (BS 727A). APPROX. 2.0" LONG. / R&R ANGLE PER SRM.

Part: SIGN — MISSING (CABIN) · airframe 73,011 hrs · 44,548 cycles

L1 DOOR LOWER EXIT SIGN MISSING DIRECTIONAL ARROW. R&R SIGN PER AMM.

Part: COVER — MISSING (EXIT SIGN) · airframe 73,011 hrs · 44,548 cycles

R1 DOOR LOWER EXIT SIGN MISSING DIRECTIONAL ARROW. R&R LIGHT ASSEMBLY PER AMM.

Part: FLAP — DELAMINATED (RT WING) · airframe 71,926 hrs · 43,838 cycles

RT WING OUTBOARD AFT FLAP INBOARD TRAILING EDGE DELAMINATED. REPAIRED AFT FLAP IAW SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 71,926 hrs · 43,838 cycles

RT HORIZONTAL STABILIZER NR 2 INSPAR RIB CRACKED AT STAB STA 101.9, 4TH VERTICAL STIFFENER FROM FRONT. REPAIRED RIB IAW SRM & DWG.

Part: CONTACT — DIRTY (EMERGENCY LIGHT) · airframe 70,708 hrs · 43,058 cycles

L2 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. CLEANED THE LIGHT'S CONTACT. OPS CHECKED GOOD IAW MM.

Part: WIRE — NOT REPORTED (COCKPIT) · airframe 70,386 hrs · 42,850 cycles

COCKPIT EMERGENCY LIGHT INOP. R&R WIRE IAW SWPM & WDM.

Part: TAB — DISLODGED (L1 DOOR SLIDE) · airframe 70,139 hrs · 42,703 cycles

L1 DOOR SLIDE HOOK AND LOOP TAB DISLODGED. SECURED IAW SIP.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 70,090 hrs · 42,675 cycles

R2 DOOR EMERGENCY LIGHT COVER LOOSE. SECURED THE COVER IAW EA.

Part: RETAINER — DAMAGED (L1 GIRT BAR) · airframe 70,024 hrs · 42,638 cycles

L1 DOOR SLIDE AFT GIRT BAR RETAINER HAD A SHEARED RIVET. R & R THE GIRT BAR ASSEMBLY IAW SRM.

Part: ISOLATOR — BROKEN (R2 DOOR SLIDE) · airframe 70,024 hrs · 42,638 cycles

R2 DOOR SLIDE PACK MOUNT ISOLATORS BROKEN. R & R SLIDE IAW SRM.

Part: LIGHT — LOOSE (CABIN) · airframe 68,817 hrs · 41,860 cycles

LT OVERWING EMERGENCY EXIT LIGHT LOOSE. SECURED LIGHT PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 68,443 hrs · 41,613 cycles

LT EXTERNAL EMERGENCY EXIT LIGHT INOP. R&R BATTERY PACK PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 68,443 hrs · 41,613 cycles

LT AFT OVERHEAD BIN EMERGENCY EXIT LIGHT INOP AT ROW 13. R&R BATTERY PACK PER MM.

Part: FLOORBEAM — CRACKED (BS 294) · airframe 68,442 hrs · 41,612 cycles

FLOORBEAM FORWARD UPPER FLANGE CRACKED AT BS 294.5, RBL 52. REPAIRED THE FLOORBEAM FLANGE IAW EA.

Part: HOOK — CORRODED (EMERGENCY EXIT) · airframe 68,442 hrs · 41,612 cycles

LEFT EMERGENCY EXIT HATCH ESCAPE STRAP HOOK CORRODED. R & R STRAP HOOK IAW AMM.

Part: HOOK — CORRODED (CABIN) · airframe 68,442 hrs · 41,612 cycles

RT EMERGENCY EXIT HATCH ESCAPE STRAP HOOK CORRODED. R&R STRAP IAW AMM.

Part: SUPPORT — CORRODED (AFT DRAIN MAST) · airframe 68,442 hrs · 41,612 cycles

AFT DRAIN MAST INTERNAL SUPPORT STRUCTURE CORRODED. R & R STRUCTURE IAW SRM AND EA.

Part: SUPPORT ANGLE — CRACKED (BS 947 BULKHEAD) · airframe 68,442 hrs · 41,612 cycles

AFT CARGO BAY AFT BULKHEAD SUPPORT ANGLE CRACKED AT BS 947, LBL 10. R & R THE SUPPORT ANGLE IAW SRM & DWG.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 68,442 hrs · 41,612 cycles

LEFT HORIZONTAL STABILIZER IN SPAR RIB CRACKED AT HSS 138.70, ON THE SECOND VERTICAL STIFFENER AT THE LOWER END. REPAIRED THE RIB IAW SRM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 68,442 hrs · 41,612 cycles

STRINGER SPLICE CORRODED AT BS 360, STR 28L. R&R SPLICE IAW DWG AND SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 68,442 hrs · 41,612 cycles

EQUIPMENT COOLING EXHAUST DUCT OUTLET INTERNAL SKIN DOUBLER CORRODED BETWEEN BS 360 TO BS 380, BETWEEN STR 28L TO STR 28R. REPAIRED SKIN IAW SRM & DWG.

Part: WEB — CORRODED (DOOR FRAME) · airframe 68,442 hrs · 41,612 cycles

E/E BAY DOOR CUTOUT RT WEB CORRODED BETWEEN BS 328 TO 344. R & R THE WEB IAW SRM AND DWG.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 68,442 hrs · 41,612 cycles

RIGHT HORIZONTAL STABILIZER IN SPAR RIB CRACKED AT HSS 129.50, THIRD VERTICAL STIFFENER AT THE LOWER END. REPAIRED THE RIB IAW SRM.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 68,442 hrs · 41,612 cycles

LEFT HORIZONTAL STABILIZER IN SPAR RIB CRACKED AT HSS 138.70, 4TH VERTICAL STIFFENER AT THE LOWER END. REPAIRED THE RIB IAW SRM.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 68,442 hrs · 41,612 cycles

RIGHT HORIZONTAL STABILIZER IN SPAR RIB CRACKED AT HSS 129.50, SECOND VERTICAL STIFFENER AT THE LOWER END. REPAIRED THE RIB IAW SRM.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 68,442 hrs · 41,612 cycles

LEFT HORIZONTAL STABILIZER IN SPAR RIB CRACKED AT HSS 111.10, 4TH VERTICAL STIFFENER AT THE LOWER END. REPAIRED THE RIB IAW SRM.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 68,442 hrs · 41,612 cycles

LEFT HORIZONTAL STABILIZER IN SPAR RIB CRACKED AT HSS 138.70, THIRD VERTICAL STIFFENER AT THE LOWER END. REPAIRED THE RIB IAW SRM.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 68,442 hrs · 41,612 cycles

LEFT HORIZONTAL STABILIZER IN SPAR RIB CRACKED AT HSS 111.1. REPAIRED THE RIB IAW SRM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 68,442 hrs · 41,612 cycles

SPLICE CORRODED AT BS 370, STR 27L. R&R SPLICE PER DWG.

Part: BULKHEAD — CRACKED (BS 663) · airframe 68,442 hrs · 41,612 cycles

LEFT MAIN WHEEL WELL FORWARD BULKHEAD CRACKED AT BS 663, LBL 32. REPAIRED THE BULKHEAD IAW SRM.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 68,442 hrs · 41,612 cycles

ANGLE SPLICE CORRODED AT BS 365, STR 28L. R&R ANGLE SPLICE IAW SRM AND DWG.

Part: FLOOR SUPPORT — CORRODED (BS 310) · airframe 68,442 hrs · 41,612 cycles

FLOOR SUPPORT CORRODED AT BS 310, RBL 15. REPAIRED THE FLOOR SUPPORT EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 68,442 hrs · 41,612 cycles

STRINGER CORRODED AT BS 375, STR 28L. REPAIRED STRINGER PER SRM.

Part: FRAME — CRACKED (BS 296) · airframe 68,442 hrs · 41,612 cycles

R1 DOOR STUB FRAME CRACKED AT BS 296, STRINGER 17R. REPAIRED STUB FRAME IAW ER AND EA.

Part: WEB — CORRODED (BS 887-905) · airframe 68,442 hrs · 41,612 cycles

CREASE BEAM WEB CORRODED BETWEEN BS 887 TO 905, RBL 64. REPAIRED WEB IAW EA AND ER.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 68,442 hrs · 41,612 cycles

SUPPORT ANGLE CRACKED AT BS 663, BETWEEN RBL 65 TO RBL 70. R&R ANGLE PER DWG.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 68,442 hrs · 41,612 cycles

FLOOR SUPPORT CRACKED AT BS 663, BETWEEN RBL 45 TO RBL 65. R&R FLOOR SUPPORT PER DWG.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 68,442 hrs · 41,612 cycles

UPPER PRESSURE WEB CRACKED AT BS. 663, RBL 40. REPAIRED THE BULKHEAD WEB IAW EA.

Part: SKIN — CRACKED (LT WING LE SLAT) · airframe 68,442 hrs · 41,612 cycles

LEFT WING NR 3 SLAT LOWER NOSE SKIN CRACKED AT ACTUATOR RIB. R & R THE SKIN IAW SRM.

Part: INTERCOSTAL — CRACKED (BS 540) · airframe 68,320 hrs · 41,537 cycles

INTERCOSTAL CRACKED AT BS 540, RT OF CENTER. R&R INTERCOSTAL IAW SRM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 68,320 hrs · 41,537 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1672. R & R THE BATTERY PACK IAW AMM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 68,320 hrs · 41,537 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1673. R & R THE BATTERY PACK IAW AMM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 68,320 hrs · 41,537 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1671. R & R THE BATTERY PACK IAW AMM.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 68,235 hrs · 41,492 cycles

LEFT WHEEL WELL BULKHEAD WEB CRACKED AT BS 663, LBL 33. REPAIRED THE BULKHEAD WEB IAW EA.

Part: LENS — MISSING (CABIN) · airframe 67,300 hrs · 40,934 cycles

EXIT LIGHT LENS MISSING NEXT TO L1 DOOR. INSTALLED LENS PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 66,465 hrs · 40,443 cycles

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

Part: BATTERY PACK — FAILED (CABIN) · airframe 66,263 hrs · 40,311 cycles

EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY TEST AT LOCATION M01672. R&R BATTERY PACK PER DWG.

Part: BATTERY PACK — FAILED (CABIN) · airframe 66,263 hrs · 40,311 cycles

EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY TEST AT LOCATION M01669. R&R BATTERY PACK PER DWG.

Part: ANGLE — CRACKED (VERTICAL STAB) · airframe 66,263 hrs · 40,311 cycles

RT VERTICAL STABILIZER PANEL 223CR LOWER SKATE ANGLE RETAINER CRACKED. R&R ANGLE PER SRM.

Part: SUPPORT BRACKET — CRACKED (VERTICAL STAB) · airframe 66,263 hrs · 40,311 cycles

RT VERTICAL STABILIZER SIDE LOWER PANEL 323CR VERTICAL SUPPORT BRACKET CRACKED. R&R BRACKET IAW SRM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 66,263 hrs · 40,311 cycles

EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY TEST AT LOCATION M01675. R&R BATTERY PACK PER DWG.

Part: BATTERY PACK — FAILED (CABIN) · airframe 66,263 hrs · 40,311 cycles

EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY TEST AT LOCATION M01673. R&R BATTERY PACK PER DWG.

Part: BATTERY PACK — FAILED (CABIN) · airframe 66,263 hrs · 40,311 cycles

EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY TEST AT LOCATION M01670. R&R BATTERY PACK PER DWG.

Part: BATTERY PACK — FAILED (CABIN) · airframe 66,263 hrs · 40,311 cycles

EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY TEST AT LOCATION M01674. R&R BATTERY PACK PER DWG.

Part: LATCH — STIFF (R1 GIRT BAR) · airframe 66,245 hrs · 40,304 cycles

R1 DOOR EMERGENCY SLIDE GIRT BAR STOW LATCHES STIFF. CLEANED THE LATCHES IAW SIP.

Part: LATCH — STIFF (L1 DOOR GIRT BAR) · airframe 66,245 hrs · 40,304 cycles

L1 DOOR SLIDE GIRT BAR STOW LATCHES STIFF. CLEANED THE LATCHES IAW SIP.

Part: PANEL — DELAMINATED (RT WING) · airframe 65,414 hrs · 39,827 cycles

RIGHT WING LEADING EDGE PANEL INBOARD OF FUELING STATION DELAMINATED. REPAIRED THE PANEL IAW SRM AND EA.

Part: COVER — BROKEN (EXIT SIGN) · airframe 62,874 hrs · 38,337 cycles

AFT GALLEY EMER EXT SIGN COVER BROKEN. R & R SIGN ASSEMBLY IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,729 hrs · 38,257 cycles

LEFT EMER EXIT LIGHTS INOPERATIVE, BETWEEN ROW 6 - 9. R & R LIGHT IAW AMM.

Part: LENS — MISSING (CABIN) · airframe 62,729 hrs · 38,257 cycles

LEFT EMER EXIT LIGHT LENS MISSING. R & R LIGHT IAW AMM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 62,729 hrs · 38,257 cycles

AFT CARGO INTERCOSTAL WEB CORRODED, BETWEEN BS 927 - 947, RBL 3. R & R INTERCOSTAL IAW SRM & DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 62,729 hrs · 38,257 cycles

AFT CARGO INTERCOSTAL WEB CORRODED, BETWEEN BS 927 - 947, LBL 3. R & R WEB IAW SRM & DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 62,729 hrs · 38,257 cycles

R1 GALLEY DOOR AREA CREASE BEAM WEB CLIP CRACKED AT BS 290, STRINGER 17R. R & R CLIP IAW SRM & DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 62,729 hrs · 38,257 cycles

RIGHT LOWER CREASE BEAM ANGLE CORRODED, BETWEEN BS 947 - 986. R & R ANGLE IAW EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 62,729 hrs · 38,257 cycles

AFT CARGO PIT FLOORBEAM CORRODED AT BS 927+10, STRINGER 27R. R & R BEAM IAW DWG & MM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 63,381 hrs · 38,616 cycles

AFT CARGO PIT STRINGER CLIP CORRODED AT BS 727D, STRINGER 26R. R & R CLIP IAW SRM & DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 62,729 hrs · 38,257 cycles

AFT CARGO PIT RT Z ANGLE CORRODED, BETWEEN BS 747 - 767. R & R Z ANGLE IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 62,729 hrs · 38,257 cycles

AFT CARGO PIT FLOORBEAM CORRODED, BETWEEN BS 907 - 927+10, STRINGER 27L. R & R BEAM IAW DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 62,729 hrs · 38,257 cycles

AFT CARGO PIT RT Z ANGLE CORRODED, BETWEEN BS 727D+10 - 747. R & R Z ANGLE IAW SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 62,729 hrs · 38,257 cycles

AFT CARGO PIT INTERCOSTAL CORRODED AT BS 767. R & R INTERCOSTAL IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 62,729 hrs · 38,257 cycles

FLOOR SUPPORT CORRODED, BETWEEN BS 947 - 967, LBL 55. R & R SUPPORT IAW DWG & SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 62,729 hrs · 38,257 cycles

FLOOR SUPPORT STRUCTURE CORRODED, BETWEEN BS 312 - 328, LBL 11.50. R & R FLOOR SUPPORT IAW DWG & SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 62,729 hrs · 38,257 cycles

FLOORBEAM CORRODED AT BS 328, BETWEEN RBL 65 TO RBL 45. REPAIRED FLOORBEAM IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 62,729 hrs · 38,257 cycles

FLOORBEAM T CAP UPPER SURF CORRODED AT BS 967, BETWEEN LBL 13 - 37. R & R T CAP IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 62,729 hrs · 38,257 cycles

R2 DOOR CUT OUT THRESHOLD CREASE BEAM CORRODED, BETWEEN BS 947 - 986. R & R CREASE BEAM IAW SRM & DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 62,729 hrs · 38,257 cycles

LEFT FWD CARGO Z ANGLE CORRODED, BETWEEN BS 500+12 - 500+16. R & R Z ANGLE IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 62,729 hrs · 38,257 cycles

L1 DOOR CREASE BEAM CORRODED, BETWEEN BS 312 - 360. R & R BEAM IAW SRM & DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 62,729 hrs · 38,257 cycles

L1 DOOR CREASE BEAM ANGLE CORRODED, BETWEEN BS 298 - 344. R & R ANGLE IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 62,729 hrs · 38,257 cycles

FLOORBEAM UPPER T CAP CORRODED AT BS 987, BETWEEN RBL 0 TO RBL 45. REPAIRED T CHORD IAW SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 62,729 hrs · 38,257 cycles

FLOOR STRUCTURE WEB CORRODED AT BS 1012, RBL 30. R & R WEB IAW DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 62,729 hrs · 38,257 cycles

L2 DOOR CUT OUT THRESHOLD, CREASE BEAM CORRODED. R & R CREASE BEAM IAW SRM & DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 62,729 hrs · 38,257 cycles

R1 DOOR CREASE BEAM TOP & SIDE SURFACES CORRODED, BETWEEN BS 294 - 328. R & R CREASE BEAM IAW DWG & SRM.

Part: TAIL CONE — DELAMINATED (TE FLAP) · airframe 62,729 hrs · 38,257 cycles

NUMBER 6 FLAP SUPPORT AFT ASSEMBLY TAIL CONE 642EB DELAMINATED. REPAIRED TAIL CONE IAW SRM & EA.

Part: NUT PLATE — MISSING (R2 DOOR) · airframe 62,729 hrs · 38,257 cycles

R2 DOOR EMER EVAC SLIDE AFT GIRT BAR FITTING. FWD ATTACHING POINT NUTPLATE MISSING. INSTALLED NUTPLATE IAW WO.

Part: NUT PLATE — MISSING (L2 DOOR) · airframe 62,729 hrs · 38,257 cycles

L2 DOOR EMER EVAC SLIDE AFT GIRT BAR FITTING, FWD ATTACHING POINT NUTPLATE MISSING. INSTALLED NUTPLATE IAW WO.

Part: SLIDE — UNSECURE (L1 DOOR) · airframe 61,869 hrs · 37,787 cycles

L1 DOOR ESCAPE SLIDE FELL OUT, DID NOT DEPLOY & STILL OPERATIONAL. R & R SLIDE IAW MT.

Part: BATTERY — FAILED (CABIN) · airframe 59,739 hrs · 36,578 cycles

FORWARD LT EMER LIGHTING BATTERY PACK FAILED CAPACITY CHECK. R & R BATTERY IAW AMM.

Part: BATTERY — FAILED (CABIN) · airframe 59,739 hrs · 36,578 cycles

CENTER LT EMER LIGHTING BATTERY PACK FAILED CAPACITY CHECK. R & R BATTERY IAW AMM.

Part: BATTERY — FAILED (CABIN) · airframe 59,739 hrs · 36,578 cycles

LEFT EMER LIGHTING BATTERY PACK FAILED CAPACITY CHECK AT ROW 17. R & R BATTERY IAW AMM.

Part: BATTERY — FAILED (CABIN) · airframe 59,739 hrs · 36,578 cycles

AFT RT EMER LIGHTING BATTERY PACK FAILED CAPACITY CHECK. R & R BATTERY IAW AMM.

Part: LENS — BROKEN (CABIN) · airframe 59,056 hrs · 36,172 cycles

LEFT OVERWING EMER EXIT DOOR LOWER FWD EXIT LIGHT LENS BROKEN. R & R LIGHT ASSEMBLY IAW MM.

Part: SLIDE — LOW PRESSURE (L1 DOOR) · airframe 59,037 hrs · 36,160 cycles

L1 DOOR EMER EVAC SLIDE PRESS LOW. R & R SLIDE IAW MT.

Part: LENS — BROKEN (EXIT SIGN) · airframe 57,478 hrs · 35,249 cycles

R1 DOOR EMERGENCY EXIT SIGN LENS BROKEN. R & R LENS IAW MM.

Part: CONNECTOR — DAMAGED (CABIN) · airframe 56,914 hrs · 34,918 cycles

RT OVERWING EXIT LIGHT CONNECTOR D12464 DAMAGED. R & R CONNECTOR IAW WDM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,914 hrs · 34,918 cycles

FRAME CRACKED AT BS 867 STRINGER 8R. REPAIRED FRAME IAW SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,914 hrs · 34,918 cycles

FRAME CRACKED AT BS 400 STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,914 hrs · 34,918 cycles

FRAME CRACKED AT BS 480 STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,914 hrs · 34,918 cycles

FRAME CRACKED AT BS 727D STRINGER 8L. REPAIR FRAME IAW SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,914 hrs · 34,918 cycles

FRAME CRACKED AT BS 440 STRINGER 8R. REPAIRED FRAME IAW SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,914 hrs · 34,918 cycles

FRAME CRACKED AT BS 727B STRINGER 8R. REPAIR FRAME IAW SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,914 hrs · 34,918 cycles

FRAME CRACKED AT BS 440 STRINGER 8L. REPAIRED FRAME IAW EA.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 56,914 hrs · 34,918 cycles

VERTICAL PRESS WEB CRACKED AT BS 663, LBL 40. REPAIRED WEB IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,914 hrs · 34,918 cycles

FRAME CRACKED AT BS 727B STRINGER 8L. REPAIR FRAME IAW SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,914 hrs · 34,918 cycles

FRAME CRACKED AT BS 747, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,914 hrs · 34,918 cycles

FRAME CRACKED AT BS 907, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,914 hrs · 34,918 cycles

FRAME CRACKED AT BS 907, STRINGER 8L. REPAIRED FRAME IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,914 hrs · 34,918 cycles

FUSELAGE SKIN CRACKED AT BS 540, STRINGER 22R. REPAIRED SKIN IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,914 hrs · 34,918 cycles

FRAME CRACKED AT BS 867 STRINGER 8L. REPAIRED FRAME IAW SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,914 hrs · 34,918 cycles

FRAME CRACKED AT BS 827 STRINGER 8R. REPAIRED FRAME IAW SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,914 hrs · 34,918 cycles

FRAME CRACKED AT BS 480 STRINGER 8R. REPAIRED FRAME IAW SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,914 hrs · 34,918 cycles

FRAME CRACKED AT BS 727D STRINGER 8R. REPAIRED FRAME IAW EA.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 56,914 hrs · 34,918 cycles

VERTICAL PRESS WEB CRACKED AT BS 663, LBL 40. REPAIRED WEB IAW SRM.

Part: FITTING — CRACKED (TE FLAP) · airframe 56,914 hrs · 34,918 cycles

RT WING AFT FLAP TRACK FAIRING 643BB FWD INTERNAL FITTING CRACKED ON RT SIDE BELOW BUSHING. R & R FITTING IAW SRM & DRAWING.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,914 hrs · 34,918 cycles

NR 1 LT WINDOW SILL POINT D SPLICE FITTING FASTENER HOLE COMMON TO SKIN FWD FASTENER ROW CTR HOLE 3.5 INCHES BELOW WINDOW CUTOUT CRACKED. REPAIRED SKIN IAW SRM & DRAWING.

Part: ATTACH FITTING — CRACKED (LE SLAT) · airframe 56,914 hrs · 34,918 cycles

LT WING NR 2 SLAT ACTUATOR ATTACH FITTING CRACKED. REPAIRED FITTING IAW SRM.

Part: SUPPORT BRACKET — CRACKED (RT WING) · airframe 56,914 hrs · 34,918 cycles

RT WING UPPER INBD PANEL SUPPORT BRACKET CRACKED. R & R BRACKET IAW DRAWING & SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 56,914 hrs · 34,918 cycles

LT OVERWING EMERGENCY EXIT CUTOUT LOWER PAN INTERCOSTAL CORRODED AT BS 637. R & R INTERCOSTAL IAW SRM & DRAWING.

Part: SLAT — CRACKED (RT WING) · airframe 56,914 hrs · 34,918 cycles

RT WING NR 8 SLAT CRACKED AT ACTUATOR ATTACH FITTING. REPAIRED NR 8 SLAT IAW SRM.

Part: SUPPORT BRACKET — CRACKED (LT WING) · airframe 56,914 hrs · 34,918 cycles

LT WING UPPER INBD PANEL SUPPORT BRACKET CRACKED. R & R BRACKET IAW SRM & DRAWING.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,914 hrs · 34,918 cycles

L1 DOOR EMERGENCY EXIT LIGHT BULBS INOPERATIVE. REPAIRED BULBS IAW AMM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,833 hrs · 34,867 cycles

FRAME CRACKED AT BS 400 STRINGER 8R. REPAIRED FRAME IAW SWA EA.

Part: COVER — MISSING (CABIN) · airframe 56,725 hrs · 34,804 cycles

EMERGENCY LIGHT COVER MISSING AT RT OVERWING EXIT AREA. INSTALLED COVER IAW MM.

Part: MOUNT — CRACKED (LE SLAT) · airframe 55,653 hrs · 34,144 cycles

RT WING NR 5 SLAT INBD AUXILIARY ROLLER MOUNT CRACKED. R&R NR 5 SLAT IAW MM.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 55,156 hrs · 33,860 cycles

RT WING MLG TRUNNION FITTING LUG FACE CORRODED. REPAIRED FITTING IAW EA.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 55,156 hrs · 33,860 cycles

LT WING MLG TRUNNION FITTING LUG FACE CORRODED. REPAIRED FITTING IAW EA.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 55,156 hrs · 33,860 cycles

RT WING MLG TRUNNION FITTING LUG FACE CORRODED. REPAIRED FITTING IAW EA.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 55,156 hrs · 33,860 cycles

LT WING MLG TRUNNION FITTING LUG FACE CORRODED. REPAIRED FITTING IAW EA.

Part: ATTACH BRACKET — MISSING (CABIN) · airframe 55,136 hrs · 33,847 cycles

MID CABIN OVERHEAD EMERGENCY EXIT LIGHT HOUSING ATTACH BRACKET MISSING. R&R LIGHT ASSEMBLY IAW M/M.

Part: HOOK — LOOSE (L1 DOOR) · airframe 54,480 hrs · 33,465 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR HOOK LOOSE. SECURED HOOK PER SRM.

Part: HOOK — LOOSE (R1 DOOR) · airframe 54,480 hrs · 33,465 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR HOOK LOOSE. SECURED HOOK PER SRM.

Part: LIGHT — BROKEN (CABIN) · airframe 54,143 hrs · 33,270 cycles

L2 DOOR EMERGENCY LIGHT INDICATOR ON WALL BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 53,792 hrs · 33,078 cycles

JUST FWD OF LEFT OVERWING EMERGENCY EXIT HATCH, THE EXIT SIGN JUST ABOVE THE FLOOR HAS BURNED OUT LAMPS. REMOVED AND REPLACED EXIT SIGN BULB FORWARD OF LEFT OVERWING EMERGENCY EXIT HATCH JUST ABOVE FLOOR IAW AMM 33-51-01-960-801. OPS CHECK

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 53,792 hrs · 33,078 cycles

CAPTAINS NR 3 WINDOW FRAME. 2ND HOLE FROM BOTTOM OF E-F WINDOW POST, HAS A CRACK INDICATION. CAPTAINS NR 3 WINDOW FRAME, 2ND HOLE FROM BOTTOM OF E-F WINDOW POST HAD CRACK INDICATION. REAMED HOLE TO 0.324" AND PERFORMED HFEC WHICH DETERMINED THAT

Part: FLAP — DELAMINATED (LT WING) · airframe 53,792 hrs · 33,078 cycles

LEFT OUTBOARD AFT FLAP HS DELAMINATED ON THE INBOARD TRAILING EDGE CORNER. REMOVED DAMAGE CLEANED EVALUATED LEFT O/B AFT FLAP DELAMINATED ON I/B TRAILING EDGE CORNER NO MOISTURE NOTED TAP TEST GOOD REPAIR MATERIALS.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 53,792 hrs · 33,078 cycles

JUST AFT OF RIGHT OVERWING EMERGENCY EXIT HATCH, THE EXIT SIGN JUST ABOVE THE FLOOR HAS BURNED OUT LAMPS. REMOVED AND REPLACED EXIXT SIGN BULB AFT OF RIGHT OVERWING EMERGENCY EXIT HATCH IAW AMM 33-51-01-960-801. OPS CHECK GOOD.

Part: SCREW — LOOSE (GIRT BAR) · airframe 53,792 hrs · 33,078 cycles

FWD GALLEY SERVICE DOOR (R1) FORWARD GIRT BAR FITTING LOOSE. TIGHTENED SCREWS OF FWD GALLEY SERVICE DOOR R1 FORWARD GIRT BAR IAW AMM 25-66-02-400-801.

Part: SCUFF PLATE — CORRODED (FUSELAGE) · airframe 53,440 hrs · 32,852 cycles

AFT CARGO COMPARTMENT FWD SCUFF PLATE CORRODED. REMOVED AND REPLACED AFT CARGO COMPARTMENT FWD SCUFF PLATE IAW IPC 25-52-10-02, AMM 25-52-10-400-801 AND BOEING DRAWING 453A2600.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 53,440 hrs · 32,852 cycles

CABIN BS 727B LBL 45.5 O/B SEAT TRACK FASTENER HOLE CRACKED. REMOVED AND REPLACED PLATE IAW EA.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 53,325 hrs · 32,778 cycles

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

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 53,325 hrs · 32,778 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 51,859 hrs · 31,881 cycles

FLIGHT DECK CENTER BEAM BETWEEN CAPTAINS AND F/O WINDOW FRAME CRACKED AT LOWER FORWARD END. REPAIR FRAME IAW EA.

Part: BATTERY — FAILED (CABIN) · airframe 51,555 hrs · 31,714 cycles

LT AFT CABIN EMERGENCY LIGHT BATTERY PACK FAILED TEST. REMOVED AND REPLACED BATTERY PER M/M.

Part: BATTERY — FAILED (CABIN) · airframe 51,555 hrs · 31,714 cycles

RT MID CABIN EMERGENCY LIGHT BATTERY PACK FAILED TEST. REMOVED AND REPLACED BATTERY PER M/M.

Part: FLAP — DELAMINATED (RT WING) · airframe 51,028 hrs · 31,420 cycles

RT WING AFT O/B TRAILING EDGE FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 51,018 hrs · 31,413 cycles

RT WING AFT FLAP O/B TRAILING EDGE I/B AND UPPER SURFACE DELAMINATED. REPAIRED AFT FLAP PER MM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 49,185 hrs · 30,315 cycles

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

Part: HOOK — OUT OF ADJUST (GIRT BAR) · airframe 49,177 hrs · 30,310 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR HOOKS OUT OF ADJUST. ADJUSTED HOOKS PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 48,297 hrs · 29,787 cycles

DURING SCHEDULED MV1 CHECK FOUND, RT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT LOOSE. SECURED LIGHT PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 44,475 hrs · 27,532 cycles

L1 DOOR EVACUATION SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: STIFFENER — CRACKED (BS 727 BULKHEAD) · airframe 43,114 hrs · 26,690 cycles

DURING SCHEDULED 12Y CHECK, FOUND AFT CARGO COMPARTMENT STIFFENER CRACKED AT FWD BULKHEAD BS 727, LBL 12. REMOVED AND REPLACED STIFFENER PER BAC DWG.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 43,114 hrs · 26,690 cycles

DURING SCHEDULED 12Y CHECK, FOUND RT OVERHEAD EMERGENCY EXIT LIGHT INOP AT ROW 13. RELAMPED LIGHT PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 43,114 hrs · 26,690 cycles

DURING SCHEDULED 12Y CHECK, FOUND LT OVERWING EXTERIOR EMERGENCY LIGHT INOP. RELAMPED PER MM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 41,114 hrs · 26,690 cycles

DURING SCHEDULED 12Y CHECK, FOUND CREASE BEAM CORRODED BETWEEN BS 950 TO BS 997, BETWEEN RBL 55 TO RBL 46. REMOVED AND REPLACED BEAM PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 41,114 hrs · 26,690 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM UPPER T-CAP CORRODED AT BS 986.5, BETWEEN LBL 37 TO LBL 46. REMOVED AND REPLACED BEAM PER SRM.

Part: SLAT — DELAMINATED (LE SLAT) · airframe 43,114 hrs · 26,690 cycles

DURING SCHEDULED 12Y CHECK, FOUND NR 7 L/E SLAT WEDGE DELAMINATED. REPAIRED SLAT PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 43,114 hrs · 26,690 cycles

DURING SCHEDULED 12Y CHECK, FOUND CREASE BEAM CHORD CORRODED BETWEEN BS 956 TO BS 986.5, BETWEEN LBL 56 TO LBL 48. REMOVED AND REPLACED BEAM PER SRM.

Part: FITTING — CRACKED (CENTER WING) · airframe 43,114 hrs · 26,690 cycles

DURING SCHEDULED 12Y CHECK, FOUND CENTER WING SECTION SHEAR FITTING CRACKED AT BS 548, RBL 42. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING) · airframe 43,114 hrs · 26,690 cycles

DURING SCHEDULED 12Y CHECK, FOUND CENTER WING SECTION SHEAR FITTING CRACKED AT BS 548, LBL 31. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING) · airframe 43,114 hrs · 26,690 cycles

DURING SCHEDULED 12Y CHECK, FOUND CENTER WING SECTION SHEAR FITTING CRACKED AT BS 548, LBL 42. REMOVED AND REPLACED FITTING PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,114 hrs · 26,690 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 43,114 hrs · 26,690 cycles

DURING SCHEDULED 12Y CHECK, FOUND CREASE BEAM CORRODED BETWEEN BS 312 TO BS 328, LBL 60. REPAIRED BEAM PER SRM.

Part: FITTING — CRACKED (CENTER WING) · airframe 43,114 hrs · 26,690 cycles

DURING SCHEDULED 12Y CHECK, FOUND CENTER WING SECTION SHEAR FITTING CRACKED AT BS 548, LBL 6.5. REMOVED AND REPLACED FITTING PER SRM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 40,786 hrs · 25,247 cycles

DURING SCHEDULED HC1 CHECK, RT EMERGENCY EXIT LIGHT BATTERY PACK FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 40,786 hrs · 25,247 cycles

DURING SCHEDULED HC1 CHECK, LT EMERGENCY EXIT LIGHT BATTERY PACK FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 38,632 hrs · 23,947 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 138. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 38,632 hrs · 23,947 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 120. REPAIRED SKIN PER SRM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 38,191 hrs · 23,689 cycles

FWD CABIN EMERGENCY EXIT SIGN LENS MISSING. INSTALLED LENS PER MM.

Part: SKIN — DELAMINATED (NR 7 SLAT) · airframe 36,209 hrs · 22,514 cycles

DURING SCHEDULED 10Y CHECK, FOUND RT WING NR 7 L/E SLAT T/E DELAMINATED AT INBOARD END. REMOVED AND REPLACED SLAT PER MM.

Part: SKIN — DELAMINATED (NR 6 SLAT) · airframe 36,209 hrs · 22,514 cycles

DURING SCHEDULED 10Y CHECK, FOUND RIGHT WING NR 6 L/E SLAT T/E DELAMINATED AT INBOARD END. REMOVED AND REPLACED SLAT PER MM.

Part: SKIN — DELAMINATED (NR 5 SLAT) · airframe 36,209 hrs · 22,514 cycles

DURING SCHEDULED 10Y CHECK, FOUND RIGHT WING NR 5 L/E SLAT T/E DELAMINATED AT INBOARD END. REMOVED AND REPLACED SLAT PER MM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 36,209 hrs · 22,514 cycles

DURING SCHEDULED HC1 CHECK, FOUND HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STATION 129.50. REPAIRED SKIN PER SWA EA.

Part: WINDOW — MISSING (R1 DOOR SLIDE) · airframe 31,028 hrs · 19,595 cycles

R1 DOOR EMERGENCY EVAC SLIDE PLEXIGLASS WINDOW MISSING. INSTALLED PLEXIGLASS WINDOW PER MM.

Part: LIGHT — WORN (CABIN) · airframe 29,370 hrs · 18,653 cycles

DURING SCHEDULED 8Y CHECK, FOUND CABIN EEPLS STRIPS WORN. REMOVED AND REPLACED STRIPS PER MM & BAC DRAWING.

Part: FLOORBEAM — CORRODED (BS 270) · airframe 29,370 hrs · 18,653 cycles

DURING SCHEDULED 8Y CHECK, FOUND FUSELAGE FLOORBEAM CORRODED AT BS 270, BETWEEN LBL 4 TO RBL 14. REPAIRED FLOORBEAM PER SWA EA.

Part: FLOORBEAM — CORRODED (BS 764) · airframe 29,370 hrs · 18,653 cycles

DURING SCHEDULED 8Y CHECK, FOUND LONGITUDINAL FLOORBEAM CORRODED AT BS 764, LBL 17. REPAIRED FLOORBEAM PER SWA EA.

Part: FLOORBEAM — CORRODED (BS 772) · airframe 29,370 hrs · 18,653 cycles

DURING SCHEDULED 8Y CHECK, FOUND LONGITUDINAL FLOORBEAM CORRODED AT BS 772, LBL 17. REPAIRED FLOORBEAM PER SWA EA.

Part: FLOORBEAM — CORRODED (BS 772) · airframe 29,370 hrs · 18,653 cycles

DURING SCHEDULED 8Y CHECK, FOUND LONGITUDINAL FLOORBEAM CORRODED AT BS 772, LBL 8. REPAIRED FLOORBEAM PER SWA EA.

Part: FLOORBEAM — CORRODED (BS 772) · airframe 29,370 hrs · 18,653 cycles

DURING SCHEDULED 8Y CHECK, FOUND LONGITUDINAL FLOORBEAM CORRODED AT BS 772, LBL 13. REPAIRED FLOORBEAM PER SWA EA.

Part: FLOORBEAM — CORRODED (BS 772) · airframe 29,370 hrs · 18,653 cycles

DURING SCHEDULED 8Y CHECK, FOUND LONGITUDINAL FLOORBEAM CORRODED AT BS 772, RBL 8. REPAIRED FLOORBEAM PER SWA EA.

Part: FLOORBEAM — CORRODED (BS 772) · airframe 29,370 hrs · 18,653 cycles

DURING SCHEDULED 8Y CHECK, FOUND LONGITUDINAL FLOORBEAM CORRODED AT BS 772, LBL 3. REPAIRED FLOORBEAM PER SWA EA.

Part: FLOORBEAM — CORRODED (BS 328) · airframe 29,370 hrs · 18,653 cycles

DURING SCHEDULED 8Y CHECK, FOUND FUSELAGE FLOORBEAM CORRODED AT BS 328, BETWEEN RBL 43 TO RBL 50. REPAIRED FLOORBEAM PER SRM.

Part: FLOORBEAM — CORRODED (BS 772) · airframe 29,370 hrs · 18,653 cycles

DURING SCHEDULED 8Y CHECK, FOUND LONGITUDINAL FLOORBEAM CORRODED AT BS 772, RBL 3. REPAIRED FLOORBEAM PER SWA EA.

Part: CONNECTOR — FAULTY (E/E BAY) · airframe 27,389 hrs · 17,526 cycles

DIVERSION/DECLARED EMERGENCY. RUDDER TRIM FAILED. REMOVED AND REPLACED RUDDER TRIM ACTUATOR CONNECTOR PER MM.

Part: STIFFENER — CRACKED (LT WING K FLAP)

DURING SCHEDULED HC2 CHECK, FOUND LEFT WING NR 1 L/E KRUGER FLAP OUTBOARD STIFFENER, CRACKED. REMOVED AND REPLACED FLAP PER MM. (M)SWAA

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 23,851 hrs · 15,541 cycles

DURING SCHEDULED C3 CHECK, FWD AND MID-AFT EMERGENCY EXIT LIGHTS FAILED TEST. REMOVED AND REPLACED BATTERIES PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 23,119 hrs · 15,166 cycles

DURING SCHEDULED C2 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 22,017 hrs · 14,606 cycles

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

Part: BATTERY — DISCHARGED (CABIN) · airframe 20,102 hrs · 13,531 cycles

DURING SCHEDULED PM CHECK, FOUND FWD ENTRY EEPLS LIGHTS EXTINGUISHED AFTER 1 MINUTE. REMOVED AND REPLACED BATTERY PER MM.

Part: LENS — LOOSE (SLIDE COVER) · airframe 19,521 hrs · 13,205 cycles

DURING SCHEDULED C3 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE COVER LENS LOOSE. SECURED LENS PER MM.

Part: COVER — MISSING (CABIN) · airframe 17,330 hrs · 11,961 cycles

EEPLS COVER MISSING AT ROW NR 16. INSTALLED COVER PER MM.

Part: SLIDE — OUT OF ADJUST (FWD SVC DOOR) · airframe 17,141 hrs · 11,849 cycles

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

Part: PUMP — FAILED (NR 2 ENGINE) · airframe 17,020 hrs · 11,777 cycles

DECLARED EMERGENCY, DURING FLIGHT LOST B HYDRAULIC SYSTEM, QUANTITY ZERO. REMOVED AND REPLACED NR 2 ENGINE DRIVEN HYDRAULIC PUMP AND NR 2 ELECTRIC PUMP PER MM.

Part: COVER — DAMAGED (CABIN) · airframe 16,638 hrs · 11,558 cycles

EEPLS WIRES EXPOSED AT MID CABIN. REPAIRED COVER PER MM.

Part: WIRE — EXPOSED (CABIN) · airframe 16,638 hrs · 11,558 cycles

EEPLS WIRES EXPOSED AT MID CABIN. REPAIRED EEPLS PER MM.

Part: TRIM TAB — VIBRATION (ELEVATOR) · airframe 16,459 hrs · 11,453 cycles

DURING CLIMB AIRCRAFT STARTED A HIGH RATE OF VIBRATION WHICH WAS FELT UNDER PILOT'S SEAT AND FEET, ALSO FELT THROUGH OUT CABIN BY F/A. REMOVED AND REPLACED BOTH LT AND RT ELEVATOR TABS. REMOVED AND REPLACED NR 1 ENG IDG. REMOVED AND REPLACED NR 2 ENG MOUNT HARDWARE. COMPLIED WITH AIRFRAME VIBRATION CONDITION INSP, OPS CHECK GOOD PER MM.

Part: SLIDE — LOOSE (AFT SVC DOOR) · airframe 13,695 hrs · 9,873 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT BAR FLAP LOOSE. ADJUSTED GIRT BAR FLAP.

Part: COVER — BROKEN (CABIN) · airframe 13,054 hrs · 9,477 cycles

EEPLS COVER BROKEN FWD CABIN. INSTALLED COVER PER MM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 12,925 hrs · 9,405 cycles

AFT EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,567 hrs · 9,200 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED GROUNDING BLOCK GD 3802S PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 11,959 hrs · 8,836 cycles

EEPLS TRACK LIGHTING LOOSE AT ROW 8. RESCURED EEPLS LIGHT PER MM.

Part: COVER — LOOSE (CABIN) · airframe 11,835 hrs · 8,772 cycles

EEPLS TRACK COVER LOOSE AT ROW 8. SECURED TRACK COVER PER MM.

Part: LENS — BROKEN (CABIN) · airframe 11,387 hrs · 8,518 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 11,387 hrs · 8,518 cycles

DURING SCHEDULED C4 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: RETAINER — LOOSE (FWD ENTRY) · airframe 11,387 hrs · 8,518 cycles

DURING SCHEDULED C4 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR RETAINER LOOSE. SECURED GIRT RETAINER PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,387 hrs · 8,518 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS INOP AT ROW 21. RELAMPED EEPLS PER MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 11,199 hrs · 8,424 cycles

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

Part: BOTTLE — DISCHARGED (ESCAPE SLIDE) · airframe 10,989 hrs · 8,308 cycles

DURING SCHEDULED RON CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE ASSY PER MM.

Part: FITTING — LOOSE (COCKPIT) · airframe 10,659 hrs · 8,105 cycles

DIVERTED, AIR SPEED DISAGREE LIGHT ILLUMINATED AT ALTITUDE FL370. SECURED LOOSE FITTING AT CAPT PITOT AIR DATA MODULE. OPS CK GOOD PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 10,479 hrs · 7,992 cycles

DURING SCHEDULED SERVICE CHECK, FOUND MID-CABIN EMERGENCY EXIT LIGHTS INOP. R&R BATTERY PACK & CHARGER (P/N 2012-1).

Part: COVER — MISSING (CABIN FLOOR) · airframe 10,418 hrs · 7,958 cycles

DURING SCHEDULED C3 CHECK, FOUND ROW 6 EEPLS LENS MISSING. INSTALLED EEPLS TRACK COVER PER MM.

Part: LENS — BROKEN (CABIN) · airframe 9,655 hrs · 7,499 cycles

AFT SERVICE DOOR EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: BUSHING — FAILED (RT ELEVATOR)

AIRCRAFT VIBRATION AT 295 KNOTS AND ABOVE DURING LEVEL FLIGHT AND NO BANKS. REMOVED AND REPLACED RT ELEVATOR TAB ASSY AND HINGE ATTACH FITTING BUSHINGS PER MM.

Part: LENS — MISSING (GALLEY)

DURING SCHEDULED C2 CHECK, FOUND EMERGENCY EXIT LIGHT LENS MISSING ON FWD GALLEY AREA. REMOVED AND REPLACED LENS PER MM.

Part: BATTERY PACK — DISCHARGED (EMER EXIT)

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

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY EXIT LIGHTS AT FLOOR AND AT OVERHEAD BIN BULLNOSES INTERMITTENT. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LAVATORY — REQD SERVICE (CABIN)

AIRCRAFT DIVERTED TO OKC DUE TO LAV SYSTEM GOING INOP. DRAINED AND RESERVICED SYSTEM PER BOEING M/M.