N121DE

Part: SKIN — CORRODED (LT MLG WW) · airframe 83,104 hrs · 36,355 cycles

FUSELAGE SKIN CORRODED, EXTERNAL SKIN AT LOWER CAVITY POPPET DRAIN. AT AFT END OF LT NLG W/W TUNNEL SKIN EXFOLIATED AND CRACKED. C/W ERA 54226-14, ORIGINAL, REF LP 2286535, 2286537, 2286538, 2286543.

Part: TEE FITTING — CORRODED (NLG WW) · airframe 83,104 hrs · 36,355 cycles

WHILE DRILLING UPPER T CHORD, 141T2938 FOR NOSE W/W REPAIR, DRILLED INTO NOSE GEAR PIVOT FITTING WEB. REPAIRED IAW ERA 542226-14.

Part: SKIN — CORRODED (BS 287) · airframe 83,104 hrs · 36,355 cycles

FUSELAGE, SECTION 41, LT SKIN, STA 287, S-36L, CORROSION. C/W ERA 541993-14.

Part: SKIN — CORRODED (BS 287) · airframe 83,104 hrs · 36,355 cycles

FUSELAGE 41 SECTION SKIN BS 287 S-37L CORROSION.

Part: FUEL TANK — CORRODED (CENTER) · airframe 83,104 hrs · 36,355 cycles

LAV 214 ON THE LT SIDE OF THE AIRPLANE BELOW THE CABIN FLOOR. HAS NUMEROUS AREAS OF CORROSION ON THE OUTER SKIN OF THE CENTER TANK. REPAIRED IAW ERA 541299-14.

Part: SKIN — CORRODED (BS 883) · airframe 83,104 hrs · 36,355 cycles

CENTER WING UPPER SURFACE AT FS 883.5 AND LBL 90 HAS AREA OF CORROSION APPROXIMATELY 2" IN DIAMETER. REPAIRED IAW ERA 541299-14.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 79,650 hrs · 35,351 cycles

FOUND EMERGENCY LIGHTS ON SEATS 19, 31, 32 LT SIDE INOPERATIVE. ROW 38 RT SIDE EMERGENCY LIGHT BRACKET BROKEN. MAINTENANCE FIXED LIGHTS AT 19 AND 32. REPLACED LIGHT COVER ASSY AT 31AB AND BRACKET ON 38 RT SIDE. SYSTEM OPERATION IS NORMAL.

Part: LIGHT — INOPERATIVE (SEAT 28B) · airframe 77,872 hrs · 34,864 cycles

EMERGENCY LIGHTS AT 28B ARE INOPERATIVE. REPLACED SEAT BUMPER ASSEMBLY. SYSTEM OPERATION IS NORMAL, REMOVED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 73,995 hrs · 33,741 cycles

EMERGENCY FLOOR LIGHTS AT SEAT 29B ARE INOPERATIVE. MX FOUND MISSING CLIP NUTS AT BRACKET ASSY AND REPLACED. SYS OPS IS NORMAL.

Part: FITTING — CRACKED (RT UNDERWING) · airframe 72,420 hrs · 33,268 cycles

RT FUSELAGE UNDERWING LONGERON FITTING IS CRACKED AND REPLACED PER EA 01-499898-03 ME-04 REV ORIG.

Part: FITTING — CRACKED (LT UNDERWING) · airframe 72,420 hrs · 33,268 cycles

LT FUSELAGE UNDERWING LONGERON FITTING IS CRACKED AND REPLACED PER EA 01-499898-03 ME-03 REV ORIG.

Part: DOOR FRAME — CORRODED (BS 1461 S32-33L) · airframe 72,420 hrs · 33,268 cycles

CARGO DOOR CUTOUT AFT FRAME WEB CORROSION BETWEEN S32L AND S33L BS 1461. REPAIRED PER ERA 502708-14 REV ORIG.

Part: BOLT — MISINSTALLED (SLATS) · airframe 72,420 hrs · 33,268 cycles

DURING THE SLAT MAIN TRACK DOWN STOP ASSY INSPECTION, STOP BOLTS WERE FOUND TO HAVE INCORRECT THREAD PROTRUSION AT NUTS. BOLTS AND NUTS WERE REPLACED AS PER OPN 2201.

Part: FLOORBEAM — CORRODED (FS 654) · airframe 72,420 hrs · 33,268 cycles

FORWARD CARGO, FS 654+44, RBL 39, FLOORBEAM UPPER CHORD CORRODED. REPAIRED AS PER SRM 53-00-07, REPAIR 4, FIGURE 201, DETAIL VI.

Part: WEDGE — DELAMINATED (RT WING TE FLAP) · airframe 72,420 hrs · 33,268 cycles

RT WING OTBD TRAILING EDGE FLAP, LOWER SURFACE WEDGE DELAMINATED. REPAIRED AS PER SRM 57-53-01, REPAIR 1, TABLE II AND SRM 51-70-07, PAR 5A(1), FIGURE 9.

Part: FAIRING — DELAMINATED (RT WING TE FLAP) · airframe 72,420 hrs · 33,268 cycles

RT WING OTBD TRAILING EDGE FLAP, LEADING EDGE FAIRING DELAMINATED. REPAIRED AS PER SRM 57-53-01, REPAIR 1, TABLE 1 AND SRM 51-70-05 PAR 5A(1), FIGURE 5.

Part: FLOORBEAM — CRACKED (BS 347) · airframe 72,420 hrs · 33,268 cycles

MAIN DECK BS 347 LBL 8 AND RBL 9 FLOORBEAM UPPER FLANGE CRACKED. REPAIRED PER ERA 502703-14 REV ORIG.

Part: FLOORBEAM — CORRODED (BS 287) · airframe 72,420 hrs · 33,268 cycles

FS 278, RBL 62 TO RBL 65 FLOORBEAM UPPER TEE CORROSION. REPAIRED AS PER SRM 53-00-51, REPAIR 1, FIGURE 201.

Part: ACCESS PANEL — DELAMINATED (RT WING TE FLAP) · airframe 72,420 hrs · 33,268 cycles

RT OTBD TRAILING EDGE FLAP UPPER ACCESS PANEL 666KT DELAMINATED. REPAIRED AS PER SRM 57-53-01, REPAIR 1, FIGURE 201, SHEET 3 AND SRM 51-70-10, REPAIR 4, FIGURE 202, SHEET 3.

Part: FAIRING — DELAMINATED (RT WING TE FLAP) · airframe 72,420 hrs · 33,268 cycles

RT WING OTBD TRAILING EDGE FLAP INBOARD LEADING EDGE FAIRING DELAMINATED. REPAIRED PER SRM 57-53-01, REPAIR 1, TABLE 1 AND SRM 51-70-05 PAR 5A(1), FIGURE 5.

Part: FLOORBEAM — CORRODED (BS 325) · airframe 72,420 hrs · 33,268 cycles

FS 325, RBL 17 TO RBL 52, UPPER FLOORBEAM CORROSION. REPAIRED AS PER SRM 53-00-51, REPAIR 1, FIGURE 201.

Part: FLOORBEAM — CRACKED (BS 1000) · airframe 72,420 hrs · 33,268 cycles

FS 1000 WL199 INCH LBL33, FLOORBEAM CRACKED. REPAIRED AS PER SRM 53-00-51 REPAIR 3, FIGURE 201, DETAIL II.

Part: FLOORBEAM — DAMAGED (BS 1219) · airframe 72,420 hrs · 33,268 cycles

AFT CARGO BS 1219 LBL 18 TO RBL 5, FLOORBEAM UPPER TEE AFT FLANGE HAS SCREW HOLES ELONGATED. REPAIRED IAW SRM 53-00-07, REPAIR 4 FIGURE 201 DETAIL VI.

Part: FAILSAFE — CORRODED (BS 955 BULKHEAD) · airframe 72,420 hrs · 33,268 cycles

RT STA 955 BULKHEAD FAILSAFE STRAP REPAIR TEE FITTING CORRODED. REPAIRED PER ERA 502701-14AD REV ORIG.

Part: FAILSAFE — CRACKED (BS 955 BULKHEAD) · airframe 72,420 hrs · 33,268 cycles

BS 955 RT BULKHEAD FAILSAFE STRAP 1 FASTENER HOLE CRACKED. REPAIRED PER ERA 502701-14 REV ORIG.

Part: SEAT TRACK — UNKNOWN (FUSELAGE) · airframe 69,477 hrs · 32,456 cycles

CABIN SEAT TRACK UNDER LT MID LAVATORY LBL 92 STA 845, SEAT TRACK FABRICATED AND INSTALLED PER PRI490882-14 REV.0 DATED 28MAR2011 0914HRS. PRI490882-14 REV.0 COMPARED WITH ER/A490882-14 REV.0 DATED 20MAY2011 1007HRS FOUND IN COMPLIANCE

Part: SKIN — CRACKED (NR 1 PYLON) · airframe 69,477 hrs · 32,456 cycles

NR 1 PYLON OTBD CORE COWL UPP AFT EXTERIOR CRACKED SKIN REPAIRED PER PRI490780-14 REV.0 TO REV.2 DATED 25APR2011 1117HRS. PRI490890-14 REV.0 TO REV.2 COMPARED WITH ER/A490890-14 REV.0 DATED 20MAY2011 1228 HRS FOUND IN COMPLIANCE.

Part: SKIN — CORRODED (FUSELAGE) · airframe 69,477 hrs · 32,456 cycles

CORROSION AT FUSELAGE SKIN AT STA 434 S-37R REPAIRED AS PER PRI 490913-14AD REV.0 DATED 27APR2011 1515HRS, PRI490913-14AD REV.1 DATED 03MAY2011 1015HRS AND COMPLIED WITH ER/A 490913-14AD REV.0 DATED 21MAY2011 1008HRS

Part: SKIN — DAMAGED (FUSELAGE) · airframe 69,477 hrs · 32,456 cycles

SCIBE LINE AT STA1532 S-22L REPAIRED AS PER PRI492328-14AD REV.0 DATED 03MAY2011 1550HRS, PRI492328-14AD REV.1 DATED 06MAY2011 1713HRS, PRI492328-14AD REV.2 DATED 10MAY2011 1124HRSAND COMPLIED WITH ER/A492328-14AD REV.0 DATED 21MAY2011 0942HRS.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 69,477 hrs · 32,456 cycles

FX-LT KEEL BEAM CHORD UPPER SURFACE AT STA 1014, CORRODED SURFACE REPAIRED PER PRI490885-14 REV.0 AND REV.1 DATED 18APR2011 1121HRS. PRI490885-14 REV.0 AND REV.1 COMPARED WITH ER/A490885-14 REV.0 DATED 20MAY2011 1120HRS FOUND IN COMPLIANCE.

Part: SKIN — CORRODED (FUSELAGE) · airframe 69,477 hrs · 32,456 cycles

CORROSION AT FUSELAGE STA 427-434 S-37L, REPAIRED AS PER PRI490913-14AD REV.0 DATED 27APR2011 1515HRS, PRI490913-14AD REV.1 DATED 03MAY2011 1015HRS AND COMPLIED WITH ER/A490913-14AD REV.0 DATED 21MAY2011 0957HRS.

Part: FAILSAFE — CRACKED (FUSELAGE) · airframe 69,477 hrs · 32,456 cycles

DURING ULTRASONIC INSPECTION, CRACK INDICATION FOUND LT SIDE FAILSAFE STRAP OF THE REAR SPAR BULKHEAD AT STA 955. REPAIR CARRIED OUT PER PRI488814-14AD REV.0 DATED 15MAR2011 0817HRS. PRI488814-14AD REV.0 COMPARED WITH ER/A488814-14 REV.0 DATED 20MAY2011 0815HRS FOUND IN COMPLIANCE.

Part: TEE FITTING — UNKNOWN (FUSELAGE) · airframe 69,477 hrs · 32,456 cycles

AROUND BS 955, T-FITTING FABRICATED AND INSTALLED PER PRI490880-14AD REV.0 DATED 25MAR2011 0907HRS, PRI490880-14AD REV.0 COMPARED WITH ER/A490880-14AD REV.0 DATED 20MAY2011 0851HRS FOUND IN COMPLIANCE.

Part: SKIN — UNKNOWN (MEC DOOR) · airframe 69,477 hrs · 32,456 cycles

MEC DOOR SKIN (P/N:141T6301-57) FABRICATED AND INSTALLED PER PRI490906-14 REV.0 DATED 21APR2011, PRI490906-14 REV.0 COMPARED WITH ER/A490906-14 REV.0 DATED 20MAY2011 1237HRS FOUND IN COMPLIANCE.

Part: SKIN PANEL — CORRODED (CENTER WING) · airframe 69,477 hrs · 32,456 cycles

CENTER TANK UPPER EXTERNAL SKIN AT STA 954, CORRODED SKIN REWORKED AND REPAIRED PER PRI490903-14 REV.0 DATED 13APR2011 0803HRS. PRI490903-14 REV.0 COMPARED WITH ER/A490903-14 REV.0 DATED 20MAY2011 1000 HRS FOUND IN COMPLIANCE.

Part: ACCESS PANEL — DAMAGED (NR 1 PYLON) · airframe 69,477 hrs · 32,456 cycles

NR 1 PYLON ACCESS PANEL NR 436AR CUTOUT REPAIRED PER PRI490910-14 REV.0 AND REV.1 DATED 28APR2011 1714HRS. PRI490910-14 REV.0 AND REV.1 COMPARED WITH ER/A490910-14 REV.0 DATED 20MAY2011 1327HRS FOUND IN COMPLIANCE.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 69,477 hrs · 32,456 cycles

FX-LT KEEL BEAM CHORD UPPER SURFACE AT STA 1010, CORRODED SURFACE REPAIRED PER PRI490885-14 REV.0 AND REV.1 DATED 18APR2011 1117HRS, PRI490885-14 REV.0 AND REV.1 COMPARED WITH ER/A490885-14 REV.0 DATED 20MAY2011 1130HRS FOUND IN COMPLIANCE.

Part: SKIN — CORRODED (RT WING) · airframe 69,477 hrs · 32,456 cycles

RT WING T/E REAR SPAR AT APPROX WS 415 UPPER CHORD OF SKIN EXTENSION, CORRODED SKIN REPAIRED PER PRI490875-14 REV.0, REV.1 AND REV.2 DATED 18APR2011 1210HRS. PRI490875-14 REV.0, REV.1 AND REV.2 COMPARED WITH ER/A490875-14 REV.0 DATED 20MAY2011 1146HRS FOUND IN COMPLIANCE.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 69,477 hrs · 32,456 cycles

CORRODED STRINGER AT STA 434 S38R FOUND CORRSION EXCEED LIMIT AS PER SRM 53-00-03 FIG 101 OTIS. REPAIR CARRIED OUT ON STRINGER AT STA 434 S-38R AS PER SRM 53-00-03 FIG 201 REPAIR 2 OTIS.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,477 hrs · 32,456 cycles

CRACKED SKIN AREA AT STA 654+68 S-2R ON THE LOWER SKIN OF THE LAP JOINT REPAIRED AS PER SRM 53-00-01 REPAIR 12 FIG 201 OTIS AND COMPLIED WITH PRI 492492-14AD DATED 10MAY 2011 1210HRS AND ER/A 492492-14AD DATED 20 MAY 2011 1016HRS.

Part: SKIN — CORRODED (CENTER WING) · airframe 69,477 hrs · 32,456 cycles

CENTER WING TANK UPPER SKIN UNDER LT MID LAVATORY AROUND LBL 90 STA 845, CORRODED SURFACE REPAIRED PER PRI488818-14 REV.0 TO REV.6 DATED 12MAY2011 1419HRS. PRI488818-14 REV.0 TO REV.6 COMPARED WITH ER/A488818-14 REV.0 DATED 24MAY2011 0819HRS FOUND IN COMPLIANCE.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 68,487 hrs · 32,062 cycles

DURING SHOP VISIT, SERVICE DAMAGE WAS FOUND ON THE LOWER SKIN OF THE RT WING OUTBOARD MAIN FLAP. THE DAMAGE RESULTED IN A LOWER SKIN CUTOUT OF 33.5 INCH BY 5.8 INCH. REPAIRED PER ERA HAS BEEN IN SHOP FOR SEVERAL YEARS, ONLY REMAINING A/C IN THE FLEET EFFECTIVE FOR THIS FLAP.

Part: GASKET — LEAKING (ENG FUEL LINE) · airframe 67,405 hrs · 31,686 cycles

HAD FUEL IMBALANCE DURING FLIGHT. LEFT SIDE WAS 1300-1400 LBS LOWER THAN RIGHT. AFTER BALANCED TOTAL FUEL WAS LESS THAN CALCULATED. DETERMINED FUEL LEAK WAS POSSIBLE AND DIVERTED TO LAS. FOUND FUEL LINE FROM FCU TO FUEL PUMP LINE GASKET LEAKING. REPLACED SAME. WET MOTOR AND IDLE RAN, NO LEAKS.

Part: SPAR — CORRODED (T/E FLAP) · airframe 66,615 hrs · 31,399 cycles

DURING SHOP VISIT, CORROSION WAS FOUND ON THE REAR SPAR OF THE RT INBOARD MAIN FLAP. THE DAMAGE WAS CUT OUT AND A REPLACEMENT SECTION WAS SPLICED IN. REPAIR WAS COMPLETED PER ERA 467064-14.

Part: KEELBEAM — CORRODED (BS 965-993) · airframe 66,437 hrs · 31,342 cycles

LT KEELBEAM CORRODED ON OUTBD FLANGE BETWEEN FS 965-933. DAMAGE REMVOED AND A REPAIR STRAP WAS INSTALLED.

Part: SKIN — CORRODED (FS 500) · airframe 66,437 hrs · 31,342 cycles

FUSELAGE SKIN CORRODED AT S-36L LAP JOINT NEAR FS 500. DAMAGED SKIN AND TEAR STRAP CUT OUT AND REINFORCED WITH DOUBLERS.

Part: LINK — UNKNOWN (TE FLAP) · airframe 66,437 hrs · 31,342 cycles

LINK REPLACEMENT IAW 01-076248-12. ME07 OUTBOARD LINK REPL-OUTBOARD FLAP-LEFT P/N 113T1321-XX ME08 INBOARD LINK REPL-OUTBOARD FLAP-LEFT P/N 113T1322-XX ME09 OUTBOARD LINK REPL-INBOARD FLAP-LEFT OUTER PINS ME10 INBOARD LINK REPL-OUTBOARD FLAP RIGHT P/N 113T1321-XX ME11 INBOARD LINK REPL-OUTBOARD FLAP RIGHT P/N 113T1322-XX ME12 OUTBOARD LINK REPL-INBOARD FLAP-LEFT OUTER PINS.

Part: FLOORBEAM — MISINSTALLED (BS 880) · airframe 65,640 hrs · 31,036 cycles

DURING AN IFE MOD AT BFM, AN EXISTING FLOORBEAM SPLICE REPAIR WAS FOUND TO BE INSTALLED INCORRECTLY. THE REPAIR WAS REMOVED AND A NEW SPLICE REPAIR WAS INSTALLED.

Part: FRAME — CRACKED (FS 1725 S7R) · airframe 65,259 hrs · 30,909 cycles

FATIGUE CRACKS IN SKIN AND BULKHEAD CHORD STRAP AT FS 1725.5 AND S-7R. CUT OUT CRACKED MATERIAL AND INSTALLED DOUBLERS.

Part: SKIN — DAMAGED (HORIZONTAL STAB) · airframe 65,250 hrs · 30,907 cycles

TOOLING DAMAGE TO UPPER HORIZONTAL STAB SKIN AND FRONT SPAR UPPER CHORD AT SPAR STA 27. DAMAGE WAS CUTOUT AND REPAIR DOUBLER INSTALLED.

Part: SKIN — GOUGED (FS 650 S21R) · airframe 65,250 hrs · 30,907 cycles

SKIN GOUGE AT FS 650 AND STR 21R. CUT OUT DAMAGE AND INSTALLED REPAIR DOUBLER.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 61,629 hrs · 29,577 cycles

ON DOM A CHECK FOUND EMERGENCY LIGHTS BATTERY CHARGER M9010 AT ROW 45FG CAUSING EMERGENCY LIGHTS TO BE DIM FOR THE BACK PART OF THE CABIN ROW 35 AFT. REMOVED AND REPLACED BATTERY CHARGER ASSY PER M/M, CKS GOOD.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,467 hrs · 29,186 cycles

A CRACK WAS FOUND IN THE BS 903.5 FRAMES ON THE LT AND RT SIDES. REPAIR ANGLES WERE INSTALLED.

Part: FITTING — DAMAGED (NR 2 NACELLE) · airframe 60,467 hrs · 29,185 cycles

AN ELONGATED HOLE WAS FOUND ON THE INBOARD MID SPAR FITTING. THE HOLE WAS OVERSIZED TO CLEAN UP THE DAMAGE.

Part: ROD — BENT (SLAT ACTUATOR) · airframe 56,424 hrs · 27,379 cycles

RIGHT WING INBD L/E SLAT OUTBD ACTUATOR ROD BENT DAMAGING L/E PANEL AND CAUSING A SLAT ASSYM. REPLACED ROD WITH NEW. ADJUSTMENT MADE ON OPN 7007. DRIVE ROD INSTALLATION OK /INSP.

Part: TIRE — DAMAGED (NLG) · airframe 55,773 hrs · 27,085 cycles

LEFT NOSE TIRE DAMAGED, MISSING A LARGE PIECE OF RUBBER. REPLACED LEFT NOSE TIRE ASSY.

Part: SKIN — DELAMINATED (HORIZ STAB) · airframe 53,687 hrs · 26,003 cycles

DELAMINATION FOUND ON HORIZONTAL STABILIZER, FWD TORQUE BOX, UPPER SKIN, RT SIDE, IN SECOND RIB BAY OUTBD FROM FUSELAGE. INNER SKIN OF THE ALUM HONEYCOMB PANEL WAS DELAMINATED FROM THE CORE. REPAIRED PER ERA 426746-14.

Part: APU — LEAKING (APU BAY) · airframe 50,275 hrs · 24,344 cycles

AT TOP OF CLIMB AND CRUISE AT 410 HOT PACK ODOR IN COCKPIT NO LIGHTS OR WARNINGS. NO REPORTED ODOR FROM THE CABIN. F/A'S LATER REPORTED HAZE AND LAV SMOKE DETECTOR ALARMS. TURNED RT PACK OFF, SMOKE SEEMED TO ABATE. REMOVED RT PACK BYPASS VALVE AND DUCT HAS OIL . CONTINUED INSPECTION RT ENGINE HIGH PRESSURE DUCT AND LOW PRESSURE DUCT. NO CONTAMINATION NOTED. FOUND OIL LEAKING IN APU BLEED AT APU. APU CHANGE PER TRANS 1T101(453486) PERFORMED DUCT BURNOUT PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,599 hrs · 22,585 cycles

BOLT HOLE HFEC INSPECTION OF FASTENERS COMMON TO THE RT FWD OUTER CHORD OF THE FS 1809.5 BULKHEAD INDICATED SMALL CRACKS IN 3 FASTENER HOLES. THE HOLES ARE COMMON TO THE INSPECTION AREA OF BAC S/B 767-53-0078 AND AD 2001-09-13. THE CRACKED SECTION OF CHORD WAS CUT AND REMOVED AND A NEW SECTION INSTALLED PER THE S/B AND ER/A 381135-14AD.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,599 hrs · 22,585 cycles

BOLT HOLE HFEC INSPECTION OF THE LT FWD OUTER CHORD OF THE FS 1809.5 BULKHEAD REVEALED A SMALL CRACK IN A FASTENER HOLE. THE FASTENER LOCATION IS COMMON TO THE INSPECTION AREA OF BAC S/B 767-53-0078 AND AD 2001-09-13. THE CRACKED SECTION OF CAP WAS CUT AND REMOVED AND A NEW SECTION INSTALLED PER THE S/B AND ER/A 381134-14AD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 46,599 hrs · 22,585 cycles

R-1 DOOR EXTERIOR EMERGENCY LIGHT INOP. REPLACED BULB, OP CK GOOD.

Part: FAN — SMOKE (RECIRCULATION) · airframe 43,044 hrs · 20,849 cycles

RECIR FAN MESSAGE ILLUMINATED IN FLIGHT WITH SMELL OF SMOKE. TURNED OFF RECIR FAN AND PULLED CB. FORWARD TO MCO.

Part: SKIN — CRACKED (BS 434)

FUSELAGE / CROWN SKIN / FS 434 / STRG. 1R : CRACK THE FUSELAGE SKIN WAS FOUND WITH A .25 INCH CRACK EMANATING FROM A FASTENER HOLE I/B OF STRINGER 1R AT THE FS 434 BUTT JOINT (FS 432.5). THE CRACK IS TYPICAL OF THAT NOTED IN B767 S/B 767-53-0081. THE CRACK WAS CUT OUT OF THE SKIN AND REPAIRED WITH AN EXTERNAL DOUBLER PER THE DIRECTIONS IN THE S/B AND DOCUMENTED PER ER/A 369340-14.

Part: HYD HOSE — RUPTURED (CENTER SYST)

DURING TAXI IN LOST CENTER HYDRAULIC SYSTEM FLUID AND PRESS. FOUND ADP PRESSURE LINE LEAKING. REPLACED SAME.

Part: BATTERY PACK — DISCHARGED (CABIN)

LEFT AND RIGHT OVERWING EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK.

Part: SLAT — DELAMINATED (NR 3 LE SLAT)

THE OUTBOARD END OF THE TRAILING EDGE OF THE NR 3 SLAT WAS FOUND TO HAVE THE UPPER SKIN DELAMINATED. THE DELAMINATION IS 6 INCHES BY 8 INCHES. THE DAMAGE WAS REPAIRED PER B767-300 SRM 57-43-02, FIGURE 201.

Part: OUTFLOW VALVE — FAILED (CABIN)

ON CLIMBOUT, CABIN AUTO INOP EICAS WITH CABIN ALT AUTO 2 AND CABIN ALT 1 EICAS STATUS MESSAGE. RETURN TO LAX. REPLACED OUTFLOW VALVE, SYSTEM CHECKS NORMAL.

Part: WIRE — SHORTED (CABIN)

AFT SECTION OF THE AFT COACH CABIN EMERGENCY FLOOR TRACK LIGHTING WAS INOP ON T/S CHECK. FOUND WIRE SHORTED TO GROUND AT SIDE WALL FEED. REPAIRED WIRE AND REPLACED THE BATTERY PWR SUPPLY M9010, SYSTEM NOW OPERATES NORMAL.

Part: WHEEL — FAILED (NOSE GEAR)

ON TAXI OUT FELT AND HEARD LOUD BANG AT NOSE AREA. RETURNED TO GATE, FOUND RT NOSE WHEEL RIM BROKEN AND LEFT WHEEL DAMAGED FROM THE EXPLOSION. INITIAL INSPECTION, INDICATES FAILURE OF WHEEL AT BEAD AREA.