N709AX

Part: STRINGER — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 77,401 hrs · 20,107 cycles

DURING C-CHECK, FOUND HORIZONTAL STAB STRINGER S2 LWR, CORRODED ON AFT SIDE OF VERTICAL LEG BETWEEN RIB 1L-2L. REPAIRED IAW SRM AND REA B655-59478MR.

Part: STRINGER — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 77,401 hrs · 20,107 cycles

DURING C-CHECK, FOUND HORIZONTAL STAB STRINGER S5 LWR, CORRODED ON AFT SIDE OF VERT FLANGE BETWEEN RIB 1R-2R. REPAIRED IAW SRM AND REA B655-59479MR.

Part: BULKHEAD — CANNING (ZONE 200) · airframe 77,401 hrs · 20,107 cycles

DURING C-CHECK FOUND AFT PRESSURE BULKHEAD OIL CANNED. REPAIRED IAW WITH REA B653-59512MR.

Part: BULKHEAD — DAMAGED (NR 2 NACELLE) · airframe 74,759 hrs · 19,498 cycles

NR 2 PYLON AFT TORQUE BOX BULKHEAD SIDE BRACE ATTACH LUG HAD LOCK FASTENER HEAD SHEARED OFF LEFT SIDE. REPLACED BROKEN AND MISSING HI-LOKS IAW B767 MM 54-51-03, DC9 SRM 51-40-02, AND DWG 311T3180 AS PER RFTS 42887.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 73,639 hrs · 18,988 cycles

EMERGENCY LIGHTS WERE LEFT ON WITH SWITCH IN -ARMED- POSITION. SWAPPED MAIN POWER SUPPLY WITH ALTERNATE POWER SUPPLY IAW B767 AMM 33-51-02. OPS CHECKED GOOD.

Part: RIB — CRACKED (CARGO DOOR) · airframe 73,144 hrs · 18,763 cycles

AFT FORWARD RIB FOR FORWARD LOWER CARGO DOOR CRACKED ON LOWER FLANGE. RIB IS ON AIRCRAFT STRUCTURE. REPAIRED HORIZONTAL LEG OF FORWARD LOWER CARGO DOOR ACTUATOR SUPPORT IAW B767 SRM.

Part: ANGLE — CRACKED (NR 2 NACELLE) · airframe 73,144 hrs · 18,763 cycles

NR 2 ENGINE STRUT CLOSEOUT ANGLE WAS CRACKED JUST AFT OF THE OUTBOARD MID SPAR FITTING (INBOARD FASTENER OF THE CLOSEOUT FITTING ON THE OUTBOARD SIDE). REMOVED AND REPLACED CLOSEOUT FITTING IAW BOEING DWG 311T3150 AND BOEING SRM 51-40-2.

Part: SKIN — DAMAGED (BS 430) · airframe 73,144 hrs · 18,763 cycles

STATIC DISCHARGE MARK ON FUSELAGE EXTERIOR AT FS 430 BETWEEN LONGERON 11 AND 12 RIGHT. REPAIRED IAW B767 SRM 53-00-01.

Part: WINDOW — MISSING (CABIN) · airframe 72,335 hrs · 18,439 cycles

1ST CABIN WINDOW AFT OF OVERWING EMERGENCY EXIT LEFT SIDE WAS MISSING A PIECE OF THE OUTER PANE. REMOVED AND REPLACED BROKEN WINDOW AFT OF LEFT EMERGENCY EXIT DOOR IAW B767 AMM 56-21-01-4.

Part: LAMP — INOPERATIVE (MLG INDICATOR) · airframe 70,613 hrs · 17,800 cycles

LT MAIN GEAR DOWN (GREEN) INDICATION LIGHT INOPERATIVE. LIGHT INOPERATIVE WITH TEST BUTTON PUSHED. CREW PERFORMED A GO AROUND AT EWR. RELAMPED LT MAIN GEAR DOWN GREEN INDICATOR LIGHT AND RT MAIN GEAR DOWN GREEN INDICATOR LIGHT. OPS CHECKED OK.

Part: STOP — BROKEN (COCKPIT DOOR) · airframe 70,061 hrs · 17,604 cycles

COCKPIT ENTRY DOOR CAME OPEN AND THEN JAMMED DURING TAXI AND COULD NOT BE OPENED. COCKPIT DOOR LATCH BROKEN. REPLACED BROKEN DOOR STOP IAW 767 SRM 51-40-2.

Part: FITTING — CRACKED (NR 2 PYLON) · airframe 69,558 hrs · 17,432 cycles

MX INSPECTED O/B PITCH LOAD FITTING LOCATED ON NR 2 ENG PYLON MANDATED BY AD 2001-08-23 & S/B 767-57A0070. HFEC INSPECTION REVEALED A CRACK INDICATION IN FITTING. CRACK WAS LOCATED IN UPPER I/B RADIUS OF FITTING, APPROX 1.25 INCH LONG RUNNING FORWARD AND AFT. HFEC AND FLUORESCENT PENETRANT INSPECTION INDICATED CRACK IS IN INBOARD RADIUS ONLY AND DOES NOT EXTEND ONTO FORWARD FACE OF FITTING OR THROUGH ENTIRE THICKNESS OF FITTING. CRACK WAS BLENDED AND DEFERRED PER REA-B657-49099-MR AND ABX GMM CHAPTER 1, SECTION 07.04 FOR MX TRACKING. A/C INSPECTED AND FOUND TO BE IN SAFE CONDITION FOR FERRY FLT FROM ILN TO GSO FOR PERMANENT REPAIR OR REPLACEMENT OF NR 2 ENG O/B PITCH LOAD FITTING. FERRY PERMIT ISSUED.

Part: FITTING — CRACKED (NR 2 ENGINE) · airframe 69,561 hrs · 17,433 cycles

DURING INSPECTION OF NR 2 ENGINE PYLON OUTBOARD SIDE LOAD FITTING PER AD 2001-08-23 AND SB 767-547A0070, HFEC INSPECTION REVEALED CRACK IN UPPER INBOARD RADIUS. INTERIM REPAIR ON REA B657-49099MR.

Part: ACM — CONTAMINATED (AIR CONDITIONER) · airframe 69,069 hrs · 17,271 cycles

AIR CONDITIONING SYSTEM HAD A STRONG GLUE TYPE ODOR, ESPECIALLY DURING DESCENT. ODOR WAS THERE WITH APU OR ENGINES SUPPLYING AIR. FOUND ODOR TO BE AN OIL TYPE ODOR FROM ACM'S. PERFORMED STEPS TO REMOVE OIL CONTAMINATION FROM AIR CONDITIONING SYSTEM IAW B767 21-00-21-2. NO ODOR DETECTED AFTER PURGING SYSTEM.

Part: BOLT — SHEARED (EMPENNAGE) · airframe 65,066 hrs · 15,948 cycles

THE RIGHT HORIZONTAL STABILIZER REAR SPAR UPPER CHORD ATTACH FITTING HAD A DOME SEALED FASTENER BACKING OFF. MAINTENANCE REPLACED THE FASTENERS IAW B767 SRM 51-40-04.

Part: JACKSCREW — DAMAGED (HORIZ STAB) · airframe 65,064 hrs · 15,946 cycles

THE HORIZONTAL STABILIZER JACKSCREW LOWER GIMBLE STOPS WERE DAMAGED. MAINTENANCE REPLACED THE HORIZONTAL STABILIZER JACKSCREW ASSEMBLY IAW B767 MM 27-41-10. OPERATION CHECKS WERE COMPLETED AND WERE SATISFACTORY.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,594 hrs · 15,785 cycles

DURING ACCOMPLISHMENT OF AD 2001-09-13, INSPECTION REPORTED CRACK INDICATIONS AT 2 FASTENER LOCATIONS, ON THE HORIZONTAL STABILIZER PIVOT BOX, LEFT AND RIGHT CHORDS. THE FASTENERS WERE REMOVED AND THE HOLES WERE REWORKED OVER SIZING THE 2 HOLES BY .016 INCH. THE REWORKED HOLES WERE REINSPECTED AND THE CRACKS WERE VERIFIED AS REMOVED IAW REA B653-41517MR.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,594 hrs · 15,785 cycles

DURING ACCOMPLISHMENT OF AD, INSPECTION REPORTED CRACK INDICATIONS AT 2 FASTENER LOCATIONS ON THE HORIZONTAL STABILIZER PIVOT BOX, LEFT AND RIGHT CHORDS. THE FASTENERS WERE REMOVED AND THE HOLES WERE REWORKED, OVER SIZING THE HOLES BY .016 INCH. THE REWORKED HOLES WERE REINSPECTED AND THE CRACKS WERE VERIFIED AS REMOVED. WHILE ACCOMPLISHING THE REPAIR, MAINTENANCE DISCOVERED 1 ELONGATED FASTENER HOLE IN THE LEFT OUTER CHORD. A HFEC INSPECTION WAS ACCOMPLISHED ON THE HOLE AND NO CRACKS WERE REPORTED IAW REA B653-41539MR.