N785AX

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 53,291 hrs · 39,455 cycles

RIGHT EMERGENCY OVERWING EXIT HAS CORROSION ON FWD INSIDE CUTOUT IN TWO SPOTS, 2.25" X 1.75. COMPLIED WITH REA B653-59974-MR, ACFT WAS GROUNDED.

Part: SPAR CAP — CORRODED (RT WING) · airframe 53,291 hrs · 39,455 cycles

SMALL SPOTS OF CORROSION AROUND NUT PLATES ON UPPER T-CAP ON REAR SPAR TO TRAILING EDGE RIB AT WS 434. REMOVED AND REPLACED CAP IAW B767-200 SRM 51-40-02, RW STA 434, ACFT WAS GROUNDED.

Part: INERTIA REEL — OUT OF POSITION (COCKPIT) · airframe 53,231 hrs · 39,415 cycles

COCKPIT INERTIAL REEL FOUND DISPLAYED. COCKPIT INERTIAL REEL PER AMM 28-61-03-4, ACFT WAS GROUNDED.

Part: INERTIA REEL — MISSING (CABIN) · airframe 50,668 hrs · 41,056 cycles

1 EACH INERTIAL REEL DEVICE MISSING AT SUPERNUMARY AREA POSITION. DEF 68450 CODE 11 DEFERRED 1 EACH INTERTIAL DESCENT DEEVICE PER MEL 25-16-1-1. PLACARD INSTALLED MBCB 4-29-11.

Part: HARNESS — MISSING (CABIN) · airframe 51,670 hrs · 38,468 cycles

ONE DESCENT HARNESS MISSING FROM SUPERNUMERARY AREA. DEFERRED: 68427 DEFERRED IAW MEL 25-61-1-2, CAT C, CODE 11. MBCB 4/25/11. PLACARD CLR DI #68427. REMOVED AND REPLACED NR 6 DESCENT DEVICE P/N 379103C-29 IN FLIGHT COMPARTMENT AREA IAW B767 SF MMS 25-61-03. AIRCRAFT WAS NOT GROUNDED.

Part: UNKNOWN — UNSERVICEABLE (CABIN) · airframe 51,670 hrs · 38,468 cycles

ON S/C FOUND 1 DESCENT DEVICE UNSERVICEABLE (POSITION #6) DEFERRED 68425. DEFERRED IAW MEL 25-61-1-1 CAT C CODE 11. REMOVED AND REPLACED NR 6 DESCENT DEVICE P/N 379103C-29 IN CREW SERVICE AREA IAW B767 SF MMS 25-61-03. AIRCRAFT WAS NOT GROUNDED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 51,366 hrs · 38,288 cycles

CLIP CRACKED AT BS 1582/SIL C/T INTERCOSTAL. REPLACED CLIP IAW B767-200 SRM 51-40-02.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,366 hrs · 38,288 cycles

STRINGER 32L SPLICE FITTING CORRODED AT STA 434. FABRICATED SPLICE FITTING IAW PFEA B655-16019. INSTALLED NEW SPLICE FITTING IAW B767-200 SRM 51-40-02. BOEING SHAL GRANTED.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,366 hrs · 38,288 cycles

THE S39L CORRODED STA 434-456. REPAIRED IAW B767-200 SRM 53-30-03.

Part: FITTING — CRACKED (FUSELAGE) · airframe 51,366 hrs · 38,288 cycles

CLIP CRACKED AT BS 1582/S1R C/T INTERCOSTAL. REPLACED CLIP IAW B767-200 SRM 51-40-02.

Part: SKIN — CORRODED (LT WING) · airframe 51,356 hrs · 38,286 cycles

LEFT WING LOWER SURFACE SPLICE IS CORRODED ON THE UPPER AND LOWER SURFACE IN THE AREA OF THE REFUELING DOOR. REMOVED CORROSION AND REPAIRED AREA IAW REA B657-58923.

Part: TEE FITTING — CORRODED (CARGO DOOR) · airframe 51,356 hrs · 38,286 cycles

FWD LOWER CARGO DOOR 2 BEAM FROM THE TOP HAS SEVERE CORROSION. REMOVED AND REPLACED CARGO DOOR BEAM TEE IAW SRM 51-3-0.

Part: FRAME — CRACKED (PYLON) · airframe 51,356 hrs · 38,286 cycles

INBOARD PYLON NR 1 BELOW 437 BR FRAME CRACKED. REMOVED STRIKER PLATES AND FRAME. RE-INSTALLED STRIKER PLATES AND NEW FRAME PER SRM 51-40-02.

Part: SUPPORT FITTING — CRACKED (LE SLAT) · airframe 51,356 hrs · 38,286 cycles

CRACK IN SUPPORT CLIP ABOVE AND AFT OF SLAT PDU BEHIND NR 6 SLAT. REMOVED AND REPLACED SUPPORT CLIP IAW SRM 51-40-01.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,356 hrs · 38,286 cycles

SHEAR TIE CORRODED ON AFT SIDE OF FLOOR SUPPORT WEB BETWEEN STRINGER 36LT AT AFT SIDE OF STA 742. FABRICATED NEW SHEAR TIE. INSTALLED IAW SRM 51-40-02.

Part: SUPPORT BRACKET — DAMAGED (CARGO DOOR) · airframe 51,356 hrs · 38,286 cycles

AFT LOWER CARGO DOOR INTERNAL LWR ANGLE SUPPORT BRACKET IS BENT AND GOUGED ON LWR SIDE OF DOOR. REMOVED AND REPLACED AFT LOWER CARGO DOOR INTERNAL LOWER ANGLE SUPPORT BRACKET WITH SERVICEABLE UNIT IAW SRM 51-40-02.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 51,356 hrs · 38,286 cycles

CRACK COMING FROM RIVET STA 1654 BETWEEN S4R AND S5R. REPAIRED FUSELAGE AND STRINGER DAMAGE IAW REA B653-58914-MR SRM 53-00-03 FIG 201 AND SRM 53-80-01 FIG 2.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,356 hrs · 38,286 cycles

R1 DOOR LWR AFT CORNER HAS 1.5 INCH CRACK TWO CRACKS FROM DOOR CUTOUT .75 INCH LC RUNNING TO BOLT HOLE. ANOTHER .75 INCH LONG CRACK EMANATES FROM THE OPPOSITE SIDE OF THE SAME BOLT HOLE EXTERNAL SKIN. REPAIRED AFT LOWER DOOR CORNER AT R1 DOOR IAW SRM 53-10-01 FIG 201.

Part: PRESSURE PANEL — CHAFED (FUSELAGE) · airframe 51,356 hrs · 38,286 cycles

PRESSURE DOME CHAFED ON TS6 BETWEEN RS18 AND RS19. BLENDED AREA FOUND TO BE OUT OF LIMITS IAW SRM 53-80-08. REMOVED AND REPLACED TEAR STRAP USING 2024T3 .040 IAW SRM 51-40-02. REMOVED LINER TO GAIN ACCESS TO RIVETS. RE-INSTALLED LINER IAW SRM 51-40-02.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 51,356 hrs · 38,286 cycles

AFT INBOARD END OF STRINGER 39RT CORRODED AT STA 786. SPLICED NEW SECTION OF STRINGER 39 RT IAW SRM 53-3-00.

Part: BEAM — CORRODED (CARGO DOOR) · airframe 51,356 hrs · 38,286 cycles

THE INTERNAL SIDE OF THE AFT LOWER CARGO DOOR HAS SURFACE CORROSION ACROSS THE DOOR STRUCTURES BEAM BELOW VENT DOORS. INSTALLED NEW T CAP AND FASTENERS IAW SRM 51-40-02.

Part: BATTERY PACK — WEAK (EMERGENCY LIGHT) · airframe 43,124 hrs · 35,333 cycles

SPARE BATTERY PACK WOULD NOT OPERATE THE COCKPIT EMERGENCY LIGHTS. REPLACED SPARE EMERGENCY LIGHT BATTERY AND POWER SUPPLY. SYSTEM OPS CHECKED GOOD IAW B767 MM 33-51-00 AND A CHECK (B767-3A) ITEM 3 AND 27.

Part: ENGINE — MALFUNCTIONED (LEFT) · airframe 42,240 hrs · 35,020 cycles

LT ENGINE OIL PRESSURE AND QUANTITY LOSS WITH 5.1 VIBRATION THAT COULD BE FELT THROUGH THE AIRCRAFT AND THE ENGINE SHUT DOWN. REPLACED ENGINE IAW WORK PACK 600178060.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 41,403 hrs · 34,741 cycles

EMERGENCY LIGHT TO RT OF MAIN ENTRY DOOR, INOPERATIVE EMERGENCY LIGHT. REPLAMPED AS REQUIRED. OPS CHECKED GOOD IAW B767 MM.

Part: LINK — WORN (T/E FLAP) · corrosion level 2 · airframe 40,408 hrs · 34,400 cycles

LINK ON INBOARD FITTING OF THE LEFT OUTBOARD FLAP HAD EXCESSIVE MOVEMENT. REPLACED LINK IAW B767 AMM 27-51-27.

Part: ACTUATOR — DEFECTIVE (ONLY) · airframe 40,256 hrs · 34,350 cycles

During flight at all altitudes, rudder appeared to be failed in the faired position. Rudder control tab appeared to work normally. Rudder position indicator on status page had negative movement with full rudder pedal deflection. Rudder trim was inop. Removed rudder panels 324BL and 324EL. Visually inspected aft compartment and tail section, cables, rudder mechanism and associated parts. No defects noted. Ops check of rudder trim system normal IAW B767 FIM 27-21-00, fig. 106/ Checked rudder linkages during ops check. No binding found. Replaced rudder trim actuator and aileron/rudder trim control panel IAW B767 AMM 27-21-11-2 and 27-28-05 as a precaution. Reinstalled panels 324BL and 324EL. Removed rig pins use

Part: FITTING — DEFECTIVE (T/E FLAP) · airframe 39,600 hrs · 34,121 cycles

RIGHT OUTBOARD FLAP, OUTBOARD 3-10 LINK, AFT FITTING, WOULD NOT TAKE GREASE WHILE PERFORMING AD 2002-01-15. REMOVED AND REPLACED FITTING IAW B767 MM 27-51-274.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 38,934 hrs · 33,894 cycles

RIGHT MAIN LANDING GEAR LAMP INOPERATIVE ON GEAR EXTENSION. SWAPPED LEFT LAMP IN AND INDICATED GOOD ON THE RIGHT SIDE. CREW ELECTED TO DO A FLY BY OVER THE TOWER AT PDX. EMERGENCY EQUIPMENT WAS DISPATCHED. NO GEAR RECYCLE WAS ANNOTATED IN THE LOG BOOK. RELAMPED THE RIGHT MAIN LANDING GEAR INDICATION LIGHT. OPS CHECKED GOOD.

Part: HYDRAULIC LINE — LEAKING (NR 1 ENGINE) · airframe 38,630 hrs · 33,799 cycles

NR 1 HYDRAULIC QUANTITY DECREASED TO 0.44 IN FLIGHT. QUANTITY STABLE WITH EDP DEPRESSURIZED AND ACMP OFF. INSPECTED NR 1 ENGINE FOUND ENGINE PUMP PRESSURE HOSE LEAKING. REPLACED THE NR 1 ENGINE PRESSURE HOSE. LEAK CHECKED GOOD IAW B767 AMM.

Part: ENGINE — VIBRATION (RIGHT) · airframe 38,407 hrs · 33,723 cycles

DURING CLIMB, RIGHT ENGINE VIBRATION 2.0 TO 2.2, SOME VIBRATION FELT. DURING ALL OTHER PHASES OF FLIGHT, NO VIBRATION FELT. OPENED COWLING AND CHECKED FOR LOOSE DUCTS, ETC. NO DEFECTS. PERFORMED BITE OF AVM AND EEC, NO DEFECTS NOTED AND NO MAINTENANCE MESSAGES. SYSTEM CHECKED GOOD IAW B767 AMM 77-37-00-5.

Part: TRANSFORMER — FAILED (CARGO BAY) · airframe 37,955 hrs · 33,571 cycles

THE UPPER CARGO COMPARTMENT LIGHTS WERE INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE UPPER CARGO LIGHTS TRANSFORMER AND WIRING IAW B767 MM.

Part: BATTERY PACK — DISCHARGED (COCKPIT) · airframe 36,432 hrs · 33,075 cycles

EMERGENCY EXIT LIGHT WOULD NOT TEST. REPLACED BATTERY PACK.

Part: LIGHT — DEFECTIVE (COCKPIT) · airframe 36,276 hrs · 33,020 cycles

COCKPIT EMERGENCY EXIT LIGHT WAS INOPERATIVE IN THE ON POSITION. REPLACED COCKPIT EMERGENCY LIGHT ASSEMBLY.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 35,642 hrs · 32,821 cycles

CAPTAIN''S WINDSHIELD CRACKED DURING FLIGHT. REPLACED WINDSHIELD.

Part: SUPPORT BRACKET — CORRODED (FUSELAGE) · airframe 35,639 hrs · 32,820 cycles

CORROSION ON SUPPORT BETWEEN STATION 1329 AND 1351 AT RBL 16.5. REPLACED SUPPORTIAW BAC DWG 146T5000.

Part: STIFFENER — CORRODED (BS 610 - 632) · airframe 35,639 hrs · 32,820 cycles

CORROSION ON STIFFENER BETWEEN STATIONS 610-632 AT LBL 6.5 LEFT IN FWD CARGO COMP. REPLACED STRINGER IAW BAC DWG 143T5000.

Part: KEELBEAM — CRACKED (BS 1050 - 1057) · airframe 35,639 hrs · 32,820 cycles

CRACK IN KEEL BEAM WEB BL 0 BETWEEN STATION 1050 AND 1057. REPAIRED IAW ABXREA B653-34320MR.

Part: FLOORBEAM — CRACKED (BS 246) · airframe 35,639 hrs · 32,820 cycles

CRACK IN FLOORBEAM AT RBL 20 AND STATION 246. REPAIRED IAW 767 SRM 51-70-13.

Part: BOLT — BROKEN (LT WING) · airframe 35,639 hrs · 32,820 cycles

LEFT WING LOAD FITTING BOLT BROKEN. (REF: S/B 767-57A064 AND AD 99-19-29). REPLACEDBOLT AND REPAIRED FITTING IAW ABX REA B653-34274MR AND BOEING FAX ABX-ILN-99-00410H.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 35,639 hrs · 32,820 cycles

CRACK ON UPPER SIDE OF STRINGER 18A RIGHT, BETWEEN STATION 412R AND 434R. REPAIREDIAW B767 SRM 53-00-03 AND ABX REA B653-32119MR.