N752AX

Part: ACTUATOR — WORN (LT WING AILERON) · airframe 65,014 hrs · 48,859 cycles

AFTER PUSHBACK AND ENGINES STARTED EICAS MESSAGE AILERON LOCKOUT DISPLAYED, AIRCRAFT RETURNED TO BLOCK. AIRCRAFT WAS GROUNDED. T/S IAW B767 FIM 27-11 FT 804 FAULT CONFIRMED BAD LT AILERON LOCKOUT ACTUATOR. REMOVED AND REPLACED LT AILERON LOCKOUT ACTUATOR, IAW B767 AMM 27-11-44, OPS CK GOOD PER AMM 27-11-44. THIS ACTION CLEARS DI 16933, PLACARDS REMOVED, REACTIVATION PROCEDURES APPLIED.

Part: AILERON SYS — LACK OF LUBE · airframe 64,907 hrs · 48,817 cycles

AILERON'S STIFF AND WILL NOT RETURN TO CENTER. AIRCRAFT WAS GROUNDED. CLEANED AND LUBE ROD BEARING. C/W INSPECTION FOR AILERON PULLEYS, ALL CHECKS NORMAL. LUBED AILERON PULLEYS AS PRECAUTIONARY. C/W OPS CHECK. AILERON ZERO OUT ON BOTH LH AND RH YOLK. REF AMM 27-11-08, 21-11-00

Part: WARNING LIGHT — ILLUMINATED (RUDDER) · airframe 64,700 hrs · 48,703 cycles

RUDDER RATIO LIGHT AND MESSAGE DISPLAYED ON PUSH BACK. THE AIRPLANE WAS GROUNDED.

Part: WARNING MESSAGE — ILLUMINATED (LE SLATS) · airframe 64,812 hrs · 48,757 cycles

EICAS MESSAGE FOR THE LE SLAT ASSYM DURING APPROACH WHEN FLAPS 5 SELECTED. AIRCRAFT WAS GROUNDED.

Part: INTERCOSTAL — CORRODED (LEFT WING) · airframe 62,148 hrs · 47,438 cycles

CORROSION FOUND ON THE LEFT WING TRAILING EDGE INTERCOSTAL ABOVE THE LEFT MAIN LANDING GEAR AFT TRUNNION. THE INTERCOSTAL WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: SUPPORT — CORRODED (LT WING) · airframe 62,148 hrs · 47,438 cycles

CORROSION ON THE LEFT WING UPPER TRAILING EDGE PANEL SUPPORT AT WING STATION 318. THE PANEL SUPPORT RIB WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: BULKHEAD WEB — CANNING (BS 1832) · airframe 62,148 hrs · 47,438 cycles

OIL CANNING ON APU BULKEAD WEB REPAIR AT BS 1832. THE WEB WAS REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: KEELBEAM — CORRODED (BS 964) · airframe 62,148 hrs · 47,438 cycles

CORROSION ON THE KEEL BEAM AT BS 964. THE KEEL BEAM WAS REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: SUPPORT — CORRODED (LT WING) · airframe 62,148 hrs · 47,438 cycles

CORROSION FOUND ON THE LEFT WING FALSE SPAR, UPPER TRAILING EDGE PANEL SUPPORT, WING STATION 360. THE SUPPORT RIB WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: SPAR — CORRODED (LT WING) · airframe 62,148 hrs · 47,438 cycles

CORROSION ON THE LEFT WING LOWER FRONT SPAR WEB AT OUTBOARD FRONT SPAR STATION 865. THE SPAR WAS REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: SKIN — CORRODED (TE FLAP) · corrosion level 2 · airframe 57,843 hrs · 44,992 cycles

LEFT OTBD FLAP UPPER SURFACE AT APPROXIMATELY STATION 367 - 377, HAS CORROSION, BULGING SKIN & ALSO HAS CORRODED SHIMS AT ACCESS 566MT OPENING EDGE. FLAP REPLACED ON NON-ROUTINE 0037. SDR INFO, CORRODED, PN 113T3100-63, PART NAME LT OTBD FLAP, SN 000355, FS & BS LOCATION: FROM OTEF 367 - 377. ACFT WAS GNDED.

Part: SUPPORT — CORRODED (LT WING) · airframe 57,843 hrs · 44,992 cycles

LEFT WING UPPER TE EDGE PANEL SUPPORT TEE CORRODED ALONG ENTIRE LENGTH. VIEWED THROUGH PANELS 561AB & 552HB. REMOVED LT WING UPPER TE PANELS FWD INBD AILERON. REMOVED TE PANEL SUPPORT. REINSTALLED SERVICEABLE SUPPORT TE PN 113T1510-33 & TE PANELS IAW SRM CH 51-40-02. SDR INFO, CORRODED, PN 113T1510-33, PART NAME SUPPORT TEE CHORD, SN NSN, WS LOCATION 289. ACFT WAS GNDED.

Part: SKIN — CRACKED (FUSELAGE) · corrosion level 2 · airframe 57,843 hrs · 44,992 cycles

SKIN UNDER THE FWD ADF ANTENNA HAS A 0.50 IN CRACK AT FS 1125, STRINGER 1L. FABRICATED & INSTALLED REPAIR TRIPLER & DOUBLER FOR SKIN UNDER FWD ADF ANTENNA AT FS 1125, STRINGER IL IAW DWG 146T3110 & SRM 53-00-01. SDR INFO, CRACKED 0.5 INCHES, PN 146T3110, SN NSN, PART NAME FUSELAGE SKIN, FS & BS LOCATION FROM FS 1125 TO 1125.5 & FROM STRINGER 1L - S1L. ACFT WAS GNDED.

Part: BEAM — CORRODED (RT WING) · airframe 57,843 hrs · 44,992 cycles

RIGHT WING LE OSS 1007.5 NOSE BEAM EXFOLIATED AT NUTPLATE AREA. R & R NOSE BEAM SECTION ON RT WING LE OSS 1007.5 IAW SRM 51-40-02. ACCOMPLISHED SB-60 351084. SDR INFO, CORRODED, PN 114T2330, PART NAME NOSE BEAM, SN NSN, STRINGER & WS LOCATION FROM OSS 1007.5 TO OSS 1010.5. ACFT WAS GNDED.

Part: RIB — CRACKED (NR 2 COWLING) · airframe 57,843 hrs · 44,992 cycles

NUMBER 2 INBD CORE COWL NR 3 RIB FROM AFT CRACKED. REMOVED NR 3 RIB & LOWER DOUBLER. WELDED RIB IAW PSM 900-7-2-1 NR 1 REV 50. REINSTALLED IAW SRM 51-40-02. SDR INFO, CRACKED LENGTH 2.5 INCHES, PN 314T1210-17, SN NSN, PART NAME RIB. ACFT WAS GNDED.

Part: BEAM — CORRODED (RT WING) · airframe 57,843 hrs · 44,992 cycles

RIGHT WING LE OSS 695 NOSE BEAM EXFOLIATED AT LE PANEL ATTACH FLANGE. REPLACED RT WING LE 055 695 NOSE BEAM PART 114T2300-292 & NR 10 INBD SLAT CURTAIN. RE-FINISHED NOSE BEAM IAW SRM 51-40-02, SRM 51-20-01 & AMM 27-81-31. SDR INFO, CORRODED, PN 114T2300-292, PART NAME NOSE BEAM, SN NSN, WS LOCATION FROM 695 TO 717. ACFT WAS GNDED.

Part: SWITCH — FAILED (RUNWAY LIGHTS) · airframe 57,728 hrs · 44,928 cycles

INTERMITTENT BURNING RUBBER SMELL DURING FLIGHT. AFTER LANDING, THE RUNWAY TURNOFF LIGHT SWITCH WAS CYCLED & VISIBLE SMOKE & FIRE APPEARED AT OVERHEAD PANEL. RT RUNWAY TURNOFF LIGHT REMAINED ILLUMINATED WITH THE SWITCH IN THE OFF POSITION. PERFORMED VISUAL INSPECTION BEHIND THE FLIGHT COMPARTMENT LT OVERHEAD LIGHTING CONTROL PANEL. VISUALLY INSPECTED LT & RT RUNWAY TURNOFF LIGHTING TRANSFORMERS. REPLACED OVERHEAD FLIGHT COMPARTMENT LIGHT PANEL ASSEMBLY. RT RUNWAY LIGHT SWITCH FAILED.

Part: LEVER — FOD (L1 DOOR SLIDE) · airframe 52,538 hrs · 18,426 cycles

L1 DOOR EVACUATION SLIDE DIFFICULT TO MOVE TO DISARMED POSITION. REMOVED FOREIGN OBJECT FROM L1 DOOR MODE SELECTOR LEVER MECHANISM. OPS CHECKED OK IAW AMM 52-11-00. ACFT WAS GROUNDED.

Part: GPU — MALFUNCTIONED · airframe 55,972 hrs · 44,879 cycles

LEFT ENGINE VERY SLOW TO RESPOND WITH THROTTLE ADVANCEMENT. ON BLOCK IN, LT ENGINE ADVANCED UNCOMMANDED, THROTTLE IN IDLE POSITION, TO APPROXIMATELY 80 PERCENT, N2. PERFORMED ENGINE RUN IAW 74-00-00-2, NO DEFECTS NOTED. AS FAR AS ENGINE GOING TO FLIGHT IDLE AT SHUTDOWN IAW GREW COMMENT, GPU LOST POWER. NORMAL ACTION TO GO TO FLIGHT IDLE WHEN POWER IS LOST. NO DEFECT NOTED.

Part: TEE FITTING — CORRODED (RT WING) · airframe 55,278 hrs · 43,726 cycles

CORROSION ON UPPER RIGHT WING TRAILING EDGE PANEL ATTACH TEE-CAP FROM WING REAR SPAR TO TRAILING EDGE AT WING STA 434. INSTALLED NEW WING CHORD IAW B767 SRM 51-40-02 PARA 4, 7 AND 9. AIRCRAFT WAS GROUNDED.

Part: BATTERY — DEFECTIVE (CABIN) · airframe 54,774 hrs · 43,496 cycles

EMERGENCY LIGHT SPARE BATTERY M736 WILL NOT HOLD A CHARGE. REPLACED EMERGENCY LIGHT SPARE BATTERY (M736) IAW B767 AMM 33-51-07-2, ACFT WAS GROUNDED.

Part: BATTERY — DISCHARGED (CABIN) · airframe 54,774 hrs · 43,496 cycles

EMERGENCY LIGHT SPARE BATTERY M735 WILL NOT HOLD A CHARGE. REPLACED SPARE EMERGENCY LIGHT BATTERY. REPLACED EMERGENCY LIGHT SPARE BATTERY (M735) IAW B767 AMM 33-51-07-2, ACFT WAS GROUNDED.

Part: PLATE — CORRODED (FUSELAGE) · airframe 53,247 hrs · 42,713 cycles

CORROSION ON BULK CARGO DOOR FLOOR PLATE BY AFT DOUBLER UNDER SCUFF PLATE. REMOVED & REPLACED CORRODED FLOOR PLATE IAW B767-200 SRM 51-40-02, AWG.

Part: FITTING — CORRODED (FUSELAGE) · airframe 53,247 hrs · 42,713 cycles

CORROSION ON FITTING AT FORWARD LOWER END OF CARGO DOOR CUTOUT BEHIND SEAL DEPRESSOR. REPAIRED IAW REA B653-595330-MR, AWG.

Part: BRACKET — CRACKED (RT WING) · airframe 53,247 hrs · 42,713 cycles

T-BRACKET CRACKED AT LOWER SUPPORT BRACE FWD OF RT INBD AILERON UNDERNEATH PANEL 661BB. REMOVED AND REPLACED T-BRACKET IN LWR SUPPORT BRACE BELOW PANEL 661BB IAW B767 DWG 113T1944, AWG.

Part: PBE — UNSERVICEABLE (CABIN) · airframe 52,189 hrs · 42,200 cycles

CREW REPORTED VACUUM SEAL ON PBE BROKEN. DEFERRED 68232 IAW B767 SERVICE CHECK AND GMM 07.04 FOR TRACKING MUST BE CLEARED BY 36 HOURS. PLACARD INSTALLED. CODE 15. AIRCRAFT WAS NOT GROUNDED.

Part: WARNING SYSTEM — FALSE ACTIVATION (LE SLAT) · airframe 51,668 hrs · 41,938 cycles

EICAS MESSAGE "L/E SLAT ASYMMETRY" AND L/E DISCRETE LIGHT ILLUMINATED ON APPROACH TO LANDING. EMERGENCY DECLARED. PERFORMED FIM PROCEDURE IAW 27-81-00-1 FIG 107 SYSTEM CHECK'S OK.

Part: SKIN — CRACKED (TE FLAP) · airframe 50,004 hrs · 41,123 cycles

LEFT OUTBOARD FLAP AFT SKIN IS CRACKED AT INBOARD END CAP. REPAIRED DAMAGED AREA IAW 767 SRM 51-70-03.

Part: SUPPORT BEAM — CRACKED (NR 1 PYLON) · airframe 50,004 hrs · 41,123 cycles

NR 1 ENGINE PYLON SUPPORT BEAM IS CRACKED AND HAS LOOSE / MISSING NUT PLATES CON TO PANEL 437ERX. REPAIRED SUPPORT BEAM IAW REA B654-58641-MR.

Part: MEC — MALFUNCTIONED (LT ENGINE) · airframe 49,949 hrs · 41,091 cycles

LEFT ENGINE FLAMED OUT AT APPROXIMATELY 1,000 AGL AFTER VNAV SELECTED. RE-LIGHT OF LEFT ENGINE SUCCESSFUL. (WHEN VNAV IS SELECTED THIS CHANGES THE THRUST PROFILE. FLAME OUT OCCURRED AS THROTTLES CAME BACK.) INSPECTED SUMPS AND FOUND NO WATER. FUEL FILTERS INSPECTED AND CLEAN. IGNITION IS GOOD. MEC WAS REMOVED AND REPLACED PER FIM REF LG ITEM 3. OPS CHECKED ON ENG RUN IAW MM 71-00-00, CHECKED NORMAL.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 46,843 hrs · 39,756 cycles

LOWER RIGHT KEEL BEAM CORD APPROXIMATELY STA 1030 - CORRODED. BLENDED CORROSION ON LOWER RIGHT KEEL BEAM STA 1030 IAW B767 SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 46,843 hrs · 39,756 cycles

LOWER RIGHT KEEL BEAM APPROXIMATELY STA 970 CORRODED. BLENDED CORROSION ON LOWER RIGHT KEEL BEAM STA 970 IAW B767 SRM.

Part: STRAP — CRACKED (RT WING SPAR) · airframe 46,843 hrs · 39,756 cycles

STRAP ON UPPER CAP OF FRONT SPAR WAS CRACKED LES 485. REMOVED AND REPLACED UPPER SPAR CAP STRAP SECTIONS IAW B767 SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 46,843 hrs · 39,756 cycles

R1 DOOR CUTOUT LOWER AFT CORNER INTERIOR DOUBLER HAD A .125 INCH CRACK AT THE FASTENER HOLE. REPLACED R1 DOOR CUTOUT LOWER AFT CORNER IAW REA 13653-57164-MA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,843 hrs · 39,756 cycles

L1 DOOR CUTOUT LOWER AFT CORNER INTERIOR DOUBLER HAD 2 EACH .25 INCH CRACKS AT THE FASTENER HOLE AND THE EXTERIOR SKIN HAD A .125 INCH CRACK AT THE SAME HOLE. REPAIRED L1 DOOR CUTOUT LOWER AFT CORNER IAW REA B653-57165-MR.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,843 hrs · 39,756 cycles

L1 DOOR CUTOUT LOWER AFT CORNER INTERIOR DOUBLER HAD 2 EACH .25 INCH CRACKS AT THE FASTENER HOLE AND THE EXTERIOR SKIN HAD A .125 INCH CRACK AT SAME HOLE. REPAIRED L1 DOOR CUTOUT LOWER AFT CORNER IAW REA B653-57165-MR.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,843 hrs · 39,756 cycles

CRACK IN SKIN APPROXIMATELY 1.375" LONG AT FASTENER FS 1654 AT STRINGER 6 LEFT. REPAIRED AREA IAW B767 SRM 53-80-01.

Part: ACTUATOR — FAILED (STABILIZER) · airframe 45,680 hrs · 39,321 cycles

DURING MAINTENANCE, REF JOB CARD 12-003-C1, STABILIZER TRIM BALL NUT UPPER SEAL APPEARED TO HAVE FAILED - STEP (23) (B) NOTE 2 (BEAVER UNIT). REMOVED AND REPLACED TRIM BALL SCREW ACTUATOR IAW B767 MM 27-41-10.

Part: CONTROL UNIT — MALFUNCTIONED (RT ENGINE) · airframe 44,602 hrs · 38,938 cycles

AS CREW WAS ON FINAL AT ILN, GOING THROUGH 27K, NR 2 ENGINE HAD AN UNCOMMANDED SHUTDOWN. CREW RESTARTED ENGINE WITHOUT ANY FURTHER ISSUES. NO EMERGENCY DECLARED. NO EN ROUTE DELAY. REMOVED AND REPLACED NR 2 ENGINE MAIN ENGINE CONTROL IAW B767 AMM 73-21-01-4, REF WORK PACK 600266182 FOR WORK ACCOMPLISHED.