N773AX

Part: BATTERY — WEAK (SMOKE DETECTOR) · airframe 59,851 hrs · 43,709 cycles

THE GALLEY AREA SMOKE DETECTOR ALARMS SOUNDED TWICE WITH NO SMOKE PRESENT. THE SMOKE DETECTOR BATTERY WAS REPLACED.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 59,856 hrs · 43,711 cycles

EMERGENCY LIGHTS IN THE CEILING ON THE LEFT SIDE OF THE SERVICE AREA WERE INOPERATIVE. THE BATTERIES IN THE EMERGENCY LIGHTS' POWER SUPPLIES WERE REPLACED. THE CAUSE OF THE INOPERATIVE EMERGENCY LIGHTS WERE FAULTY BATTERIES.

Part: ACTUATOR — FAILED (LT MLG) · airframe 58,344 hrs · 42,997 cycles

LEFT MAIN GEAR FAILED TO RETRACT WITH ASSOCIATED DOORS AMBER LIGHT , GEAR LIGHT ILLUMINATED. DOORS AMBER LIGHT REMAINED ILLUMINATED WHEN GEAR WAS EXTENDED. THE CORRECTIVE ACTION WAS REPLACING THE LT MLG SIDE BRACE LOCK ACTUATOR. THE CAUSE OF THE LT MAIN GEAR FAILING TO RETRACT WAS THE ROD END SEPARATED FROM THE PISTON OF THE LT MLG SIDE BRACE LOCK ACTUATOR.

Part: SMOKE DETECTOR — FALSE ACTIVATION (CABIN) · airframe 57,709 hrs · 42,682 cycles

GALLEY SMOKE DETECTOR GOES OFF WITH NO SMOKE IN ACFT. REPLACED SMOKE DETECTOR BATTERY.

Part: WINDOW — FAULTY (COCKPIT) · airframe 56,264 hrs · 41,839 cycles

RED GLOWING BURNING NOTED AT BOTTOM EDGE OF LT FWD WINDOW. STOPPED WHEN LT FWD WINDOW HEAT TURNED OFF. REPLACED L1 WINDOW ASSEMBLY. WINDOW ASSEMBLY EXCHANGED WITH NEW ASSEMBLY.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,244 hrs · 41,825 cycles

STATION 977 LBL 9 CORROSION ON INBD FLANGE OF VERTICAL CHORD 2 INCHES UP FROM KEEL PANEL AS SEEN FROM RT WW. R & R VERTICAL T CHORD AT STATION 977 IAW SRM 51-40-02. SDR INFO CORRODED L2, PN 145T8762-1, PART NAME CHORD, SN NA, FS & BS LOCATION FS 977, STRINGER & WS LOCATION LBL 10. ACFT WAS GNDED.

Part: SPLICE PLATE — CORRODED (RT WING) · corrosion level 2 · airframe 56,244 hrs · 41,825 cycles

THE RT WING FRONT SPAR AREA NEAR WS 416.0 IS CORRODED, EXFOLIATED. REPAIRED RT WING LOWER SPLICE PLATE AT FRONT SPAR FROM OFSS 338 TO 450 IAW REA B657-60915. CORRODED L2, PN 114T0222-6, PART NAME SPLICE PLATE, SN NSN, LOCATION STRINGER & WS FROM OFSS 420 RT TO 423 RT. ACFT WAS GNDED.

Part: SKIN PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 56,244 hrs · 41,825 cycles

AFTER REMOVING THE RT WING LOWER SPLICE PLATE, FOUND CORROSION ON THE TOP SIDE OF THE LOWER WING SKIN FROM APPROX LES 416 - 436. REPAIRED RT WING LOWER SKIN PANEL NR 4 FROM WS 403 TO 431 IAW REA B657- 60924-MR. CORRODED L2, PN 113T4101-6, SN NSN, PART NAME SKIN PANEL NR 4. WS LOC 403 RT TO 431 RT. ACFT WAS GNDED.

Part: SPAR — CORRODED (RT WING) · corrosion level 2 · airframe 56,244 hrs · 41,825 cycles

RIGHT WING FRONT SPAR LOWER CHORD AT APPROX WS 416 IS CORRODED. REPAIRED RT WING FRONT SPAR LOWER CHORD FROM OFSS 370 - 460 IAW REA B657-60910-MR. SDR INFO CORRODED L2, PN 112T2005-2, PART NAME FRONT SPAR LOWER CHORD, LOCATION STRINGER & WS FROM OFSS 370 RT TO 460 RT. ACFT WAS GNDED.

Part: FITTING — DAMAGED (RT WING) · airframe 56,244 hrs · 41,825 cycles

THE RT WING INBD SIDE LOAD FITTING HAS A DAMAGED HOLE. REPAIRED HOLE IN INBD SIDE LOAD FITTING IAW REA NR 657-60901-MR. SDR INFO DAMAGED HOLE, PN 112T7004-26, PART NAME SIDE LOAD FITTING, SN NSN, LOCATION BS FROM NAC 237 TO NAC 237 FROM NAC BL 10 TO NAC BL 10. ACFT WAS GNDED.

Part: SKIN PANEL — DAMAGED (RT WING) · airframe 56,244 hrs · 41,825 cycles

RIGHT WING LE LOWER SKIN HAS A FASTENER HOLE THAT IS OBLONG COMMON TO INBD SIDE BRACE FITTING AT APPROX LES 385. REAMED DAMAGED HOLE TO .658 INCHES DIAMETER IAW REA B657-60901-MR. FREEZE PLUG WAS INSTALLED ON NR 0774, REPAIRED DAMAGED HOLE IAW REA B657-60901-MR. SDR INFO DAMAGED HOLE, PN 112T4106-6, PART NAME SKIN PANEL, SN NSN, LOCATION WS FROM NAC BL 10 TO NAC BL 10 FROM 375.8 TO 375.8. ACFT WAS GNDED.

Part: BEAM — CRACKED (NR 1 PYLON) · airframe 56,244 hrs · 41,825 cycles

NR 1 ENG, AFT PYLON SECTION, RT LOWER BEAM IS CHAFED & CRACKED FWD END. R & R BEAM IAW SRM 51-40-02. SDR INFO PN 313T1380-243, SN NSN, PART NAME BEAM, CRACKED 2 INCHES, FS & BS LOCATION NAC STATION 35334. ACFT WAS GNDED.

Part: SKIN PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 56,244 hrs · 41,825 cycles

AFTER REMOVAL OF LOWER LE SPLICE PLATE, FOUND LE OF LOWER WING SKIN CORRODED, UPPER SURFACE AT SS 410 - 418. REPAIRED DAMAGE IAW B657-60879-MR & B65760916. LEVEL 2 CORRODED, PN 112T4101-5, SN NA, PART NAME WING SKIN PANEL NR 4, EXACT STRINGER & WS LOCATION ON ACFT FROM 396 TO 417.5. ACFT WAS GNDED.

Part: SPLICE PLATE — CORRODED (LT WING) · corrosion level 2 · airframe 56,244 hrs · 41,825 cycles

EXFOLIATION LT WING LE LWR SPLICE PLATE LES 416 PNL ACCESS 521AMB. REPAIRED LT WING LE LWR SPLICE PLATE AT LES 416 IAW REA B657-60876. SDR INFO PN 114T0222-5, SN NSN, PART NAME SPLICE PLATE, CORRODED LEVEL 2, EXACT WS LOCATION FROM 410 TO 416. ACFT GNDED.

Part: FITTING — DAMAGED (LT WING) · airframe 56,244 hrs · 41,825 cycles

THE LT WING INBD SIDE LOAD FITTING HAS MULTIPLE DAMAGED HOLES. REPAIRED DAMAGED LT WING INBD SIDE LOAD FITTING IAW REA B657-60871-MR. SIDE LOAD FITTING WILL BE INSTALLED ON NR. PN 112T7004-25, PART NAME SIDE LOAD FITTING, DAMAGED DURING REMOVAL, EXACT WS LOCATION OFSS 420. ACFT WAS GNDED.

Part: RIB — CORRODED (RT WING) · airframe 56,244 hrs · 41,825 cycles

TOP PORTION OF FWD LE RIB STATION 438 IS CORRODED. FABRICATED RIB IAW B657-60875-MR. AIR LOAD RIB WILL BE INSTALLED ON NR 0581 ENTRY NR 9. PN 114T2201-78, PART NAME RIB, CORRODED, CORRODED EXACT WS LOCATION OFSS 438. ACFT WAS GNDED.

Part: BEAM — CHAFED (NR 2 PYLON) · airframe 56,244 hrs · 41,825 cycles

NUMBER 2 AFT PYLON ASSEMBLY, INBD LOWER BEAM IS CHAFED ON FWD END. R & R NR 2 AFT PYLON ASSEMBLY INBD LOWER BEAM PN 313T1380-244 IAW SRM 51-40-02, PN 313T1380-244, PART NAME BEAM. CHAFED DAMAGE BEYOND LIMITS, SN NSN, EXACT FS & BS LOC ON ACFT NAC STATION 308. ACFT WAS GNDED.

Part: DOUBLER — CRACKED (NLG WW) · airframe 56,244 hrs · 41,825 cycles

REMOVE EXISTING REPAIR DOUBLERS ON THE VERTICAL CHORD IN THE NWW AT RBL 25 STATION 287 & INSTALL NEW REPAIR DOUBLERS IAW SRM 51-70-12. REFERENCE JC NEA53130001-001. R & R REPAIR DOUBLERS ON VERTICAL CHORD IN THE NWW AT RBLS STATION 287 IAW 8767 SRM 51-70-12. PN 141T938, SN NSN, PART NAME NWW VERTICAL CHORD, CRACKED LENGTH 1.1 INCHES. EXACT FS & BS LOCATION ON ACFT FROM STATION 287 TO RBL 25. ACFT WAS GNDED.

Part: SUPPORT — CORRODED (LT WING) · corrosion level 2 · airframe 56,244 hrs · 41,825 cycles

LEFT WING STRUCTURE CORRODED AT INBD OF SPOILER NR 6 AT STATION 226. OPENED PANELS 551LT & 552AB FOR ACCESS. REPLACED DOG BONE PANEL SUPPORTS INBD OF SPOILER NR 6. R & R STRUCTURE AT PANEL SUPPORT AFT OF SPOILER. CLOSED PANELS 551LT & 552AB. WORKED IAW SRM 51-40-02. SDR INFO PN 113T1623-131, SN NSN, PART NAME CHORD, UPPER AFT BEAM CORRODED, EXACT STRINGER & WS LOCATION FROM 226, TE T0 226, TE. ACFT WAS GNDED.

Part: SUPPORT ANGLE — CORRODED (NR 2 PYLON) · corrosion level 2 · airframe 56,244 hrs · 41,825 cycles

NUMBER 2 AFT PYLON ASSEMBLY SUPPORT ANGLE BETWEEN LT & RT LWR BEAMS ON FWD END OF PYLON APPEARS TO HAVE CORROSION. BLENDED AREA & FOUND TO BE OUT OF LIMITS IAW DWG 313T1380. INSTALLED NEW SUPPORT ANGLE IAW SRM 51-40-02 SEC 7. CORRODED, PN 313T1380-22, PART NAME CHANNEL, SPAR, ANGLE, SN AUTO-260278, EXACT PYLON LOCATION ON ACFT FROM 308.0 TO 308.0. EXACT WL LOCATION ON AC FROM 130.17 TO 130.17. ACFT WAS GNDED.

Part: ATTACH FITTING — CORRODED (NR 1 PYLON) · corrosion level 2 · airframe 56,244 hrs · 41,825 cycles

NR 1 AFT PYLON ASSEMBLY, APPEARS TO HAVE CORROSION ON THE FRONT STRUCTURE IN BETWEEN THE FWD ENDS, OF THE LWR BEAMS. R & R CORRODED PN 313T1380-22 IAW SRM 51-40-02. HYD BAY FWD LWR BEAM CROSS PIECE ATTACH FITTING. SDR INFO PN 313T1380-22, SN NSN, PART NAME SPAR CHANNEL, EXACT PYLON LOCATION ON ACFT FROM 308.00 TO 308.00, EXACT WL LOCATION ON ACFT FROM 130.17 TO 130.17. ACFT WAS GNDED.

Part: PLATE — CRACKED (NR 2 PYLON) · airframe 56,244 hrs · 41,825 cycles

NUMBER 2 AFT PYLON ASSEMBLY, AFT OTBD STINGER MOUNTING FLANGE IS CRACKED. R & R NR 2 AFT PYLON ASSEMBLY AFT OTBD STRINGER MOUNTING FLANGE IAW DWG 313T3380 SB-47 1-24-14. CRACKED 6 INCHES, PN 313T3380-174, PART NAME PLATE, SN N/S, EXACT PYLON LOCATION ON ACFT FROM 410.50 TO 410.56, WL LOCATION ON ACFT FROM 127.66 TO 160.00. ACFT WAS GNDED.

Part: STRINGER — CRACKED (LT NACELLE) · airframe 56,244 hrs · 41,825 cycles

STRINGER WEB HAS A CRACKED INTERNAL ANGLE INBD SIDE NR 1 ENG AFT PYLON. R & R INTERNAL ANGLE IAW SRM 51-40-02 PAR 7. SDR INFO CRACKED 1.5 INCHES, PN 313T3380-244, PART NAME CHANNEL WS LOCATION ON ACFT FROM WS 433 TO LONGERON 6. ACFT WAS GNDED.

Part: DOUBLER — CRACKED (LT NACELLE) · airframe 56,244 hrs · 41,825 cycles

PANEL 441 AT LATCH DOUBLER CRACKED IN CORNERS OF CUT OUT. REMOVED LATCH, ALIGNMENT BALL & CRACKED CLIP, FABRICATED CLIP, INSTALLED NEW CLIP, ALIGNMENT BALL & LATCH ON PANEL 441AT IAW DWG 313T1100 & AMM 54-52-02. SDR INFO CRACKED 1 INCH, PN 313T1100-65, PART NAME CLIP, EXACT NAC STATION LOCATION ON ACFT FROM 240.31. ACFT WAS GNDED.

Part: INERTIA REEL — OUT OF POSITION (COCKPIT) · airframe 55,057 hrs · 4,115 cycles

ONE INERTIA REEL FELL OUT ON THE FLOOR DURING PRE FLIGHT INSPECTION BY FLIGHT CREW. REMOVED AND DEFERRED NR 4 INERTIA REEL, ACFT WAS GROUNDED.

Part: FAILSAFE — CRACKED (FUSELAGE) · airframe 55,000 hrs · 41,082 cycles

RIGHT FAILSAFE CRACKED VERIFIED WITH HFEC CRACK FOUND ON FREE EDGE (AFT) LOWEST FASTENER OF INSP AREA. PERFORMED RIGHT FAILSAFE TRIM OUT REPAIR PER EA 53500014-003 AND AMES DOCUMENT 47008, ACFT WAS GROUNDED.

Part: SKIN — CORRODED (FUSELAGE) · airframe 55,000 hrs · 41,082 cycles

CORROSION ON SKIN I/B STA 955, S19 RT, AFT OF 955 FRAME (PICKLEFORK). BLENDED CORROSION AND SPOT FACED AROUND THE HOLES IAW B767 SRM 51-10-02. COMPLIED WITH EA 53500014-004 AND REA 47029REA02 AND DOC 47008ORD10, ACFT WAS GROUNDED.

Part: TEE FITTING — CORRODED (FUSELAGE) · airframe 55,000 hrs · 41,082 cycles

CORROSION ON RT TEE FITTING. REF: EA5350014-001. TEE FITTING MATCH DRILLED IAW B767 200 SRM 54-40-05, TEE FITTING INSTALLED ON EA 53500014-003 AMES DOC 47008ORD04 STEP 15, ACFT WILL BE GROUNDED.

Part: TEE FITTING — CORRODED (FUSELAGE) · airframe 55,000 hrs · 41,082 cycles

CORROSION ON LEFT TEE FITTING. REF: EA53500013-001. TEE FITTING MATCH DRILLED IAW B767 200 SRM 54-40-05, P/N TEE FITTING INSTALLED ON EA 53500013-003 AMES DOC 47008ORD03 STEP 15, ACFT WAS GROUNDED.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 55,000 hrs · 41,082 cycles

GUSSET AT UPPER OUTBOARD FWD CORNER OF PRESSURE WEB STA 958 SIDE FRAME FITTING CORRODED. REF: EA53500013-001. FABRICATED GUSSET IAW BOEING DRAWING #125T8752, FROM 2024-T3-.125, PO-0021594, ACFT WAS GROUNDED.

Part: UNKNOWN — OUT OF POSITION (GALLEY) · airframe 54,711 hrs · 40,934 cycles

EMERGENCY DESCENT NR 7 IN GALLEY ONE DROPPED OUT OF BOX. REMOVED AND REPLACED DESCENT DE-ICE NR 7 IN GALLEY WITH B767 AMM 25 61 03 4, ACFT WAS GROUNDED.

Part: UNKNOWN — INOPERATIVE (CABIN) · airframe 53,794 hrs · 40,486 cycles

NR 4 NR 7 ESCAPE DEVICE INOP IN SUPERNUMERARY AREA. DEFERRED IAW B767 MEL 25-61-1-1. PLACARD INSTALLED. 5 ESCAPE DEVICE REEL REMAIN OPERATIONAL. MX PROCEDURE C/W.

Part: INERTIA REEL — DEFECTIVE (CABIN) · airframe 53,065 hrs · 40,060 cycles

WHILE CHECK EMERGENCY ESCAPE REELS AT THE MAIN ENTRY DOOR. NR 1 DEVICE DROPPED ALL THE WAY TO THE FLOOR. DEF DI 68399 CODE 11. REMOVED NR 1 ESCAPE REEL FROM MAIN ENTRY DOOR AREA PER MEL 25-61-1-1. DEFERRED PER MEL 25-61-1-1 PLAC INSTALLED. REPLACED PREVIOUSLY REMOVED DESCENT DEVICE AT SUPERNUMERARY POSITION NR 1 PER AMM 25-61-03. PLACARD REMOVED. AIRCRAFT WAS NOT GROUNDED.

Part: WIRE — SHORTED (APU) · airframe 52,606 hrs · 39,827 cycles

APU GENERATOR INOP. DURING TROUBLESHOOTING FOUND APU GEN PLUS D2648 SHORTED WITH BURNT WIRES. REPAIRED BURNT WIRES W248-202 AT STA 1231 IAW SWPM 20-30-10. OPS CHECK APU GEN IAW 24-21-00. APU GEN OPS CHECK GOOD.

Part: STRUCTURE — CRACKED (NLG WW) · airframe 52,103 hrs · 39,567 cycles

NWW LT VERTICAL CHORD STA 287 LBL 25 HAS A CRACK APPROX 11.5 DOWN, 1.25 LONG. REPAIRED DAMAGED AREA IAW SRM 51-70-12 FIG 1. P/N 141T2938-15.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 51,375 hrs · 39,003 cycles

EMERGENCY LIGHTS ARE INOP. REMOVED AND REPLACED UPPER EMERGENCY LIGHT BATTERY PACK. OPS CHECK GOOD.

Part: BATTERY — DISCHARGED (E&E BAY) · airframe 50,550 hrs · 38,534 cycles

EMERGENCY LIGHT INOPERATIVE. SWAPPED EMERGENCY BATTERY WITH SPARE BATTERY. IAW B767 AMM 33-51-00.

Part: SEAT TRACK — CORRODED (BS 325-347) · airframe 50,498 hrs · 38,495 cycles

TRACK CORRODED AT LT BUTT LINE 7.28, STA 325-347. REMOVED AND REPLACED TRACK IAW B767 SRM. (A)

Part: WEB — CORRODED (BS 624) · airframe 50,498 hrs · 38,495 cycles

WEB CORRODED ON BOTTOM SIDE AT FS 624 AT RIGHT BUTT LINE 38.5. REMOVED AND REPLACED CORRODED WEB IAW B767 SRM. (A)

Part: FLOOR PANEL — CORRODED (BS 412) · airframe 50,498 hrs · 38,495 cycles

UPPER CARGO SUB FLOOR PANEL BENDED BEYOND LIMITS APPROXIMATELY STA 412, RT BUTT LINE 60. REMOVED AND REPLACED PANEL IAW B767 SRM 51-40-02. (A)

Part: SEAT TRACK — CORRODED (BS 424-500) · airframe 50,498 hrs · 38,495 cycles

SEAT TRACK STA 424-500 HAD CORROSION RT BUTT LIVE 18. REPLACED SEAT TRACK BS 325-555, RT BUTT LIVE 18 IAW B767 SRM. (A)

Part: SEAT TRACK — CORRODED (BS 412-423) · airframe 50,498 hrs · 38,495 cycles

SEAT TRACK CORRODED LT BUTT LINE 13.28, STA 412-423. REMOVED AND REPLACED SEAT TRACK IAW B767-200 SRM 51-40-2. (A)

Part: BEAM — CRACKED (BS 287) · airframe 47,407 hrs · 37,363 cycles

NOSE WHEEL VERTICAL BEAM AT STA287 RBL25 HAS A .5 INCH CRACK AT WL173. FOUND CRACK WHILE COMPLETING NEA5313001-001, WO 600251505 NR104. REPAIRED IAW B767 SM 51-70-12.

Part: ODOR — DETECTED (COCKPIT) · airframe 47,288 hrs · 37,307 cycles

STRONG ODOR OF BURNING ELECTRICAL EQUIPMENT FOLLOWED BY INCREASING TEMPERATURE FROM UNDER CAPTAIN'S SEAT AND BACK OF LEGS AND FEET. NO EICAS MESSAGES OR OTHER INDICATIONS OF A FIRE. BOTH FIRE BOTTLES WERE DISCHARGED PRIOR TO EVACUATING AIRCRAFT. INSPECTED COCKPIT MEC AND FORWARD ELECTRICAL COMPARTMENT AND ALL ASSOCIATED WIRING FOR EVIDENCE OF FIRE AND SMOKE DAMAGE. ALL AREAS CHECKED OKAY. APPLIED POWER, CHECKED CAPTAIN'S SEAT FOR EVIDENCE OF FIRE OR SMOKE, ALL OKAY. ALL INSTRUMENT PANEL'S PULLED AND CHECKED FOR WIRING AND INSTRUMENT DAMAGE, NONE FOUND.

Part: FITTING — CRACKED (FUSELAGE) · airframe 47,279 hrs · 37,301 cycles

DURING SCHEDULED LINE INSPECTION, FOUND THE LEFT AFT OUTER CHORD, LEFT HORIZONTAL STABILIZER, STA 1809.5, CRACKED. REPAIRED CHORD IAW B767 SB 53A0078, REV 4, FIG 3 & 4, AND ABX REA B653-5399-MR.

Part: BEARING — SEIZED (RT MLG) · airframe 45,024 hrs · 36,444 cycles

RIGHT MAIN LANDING GEAR INNER BEARING RACE SEIZED TO AXLE. AXLE CHROME MISSING. REMOVED AND REPLACED RIGHT MAIN LANDING GEAR FORWARD AXLE BEARING ASSEMBLY IAW DC-9 MM.

Part: BELLCRANK — CRACKED (RT MLG DOOR) · airframe 43,432 hrs · 35,888 cycles

RIGHT MAIN LANDING GEAR DOOR CENTER HINGE BEAM ASSEMBLY HAD THE LOWER FITTING CRACKED AT THE INBOARD SIDE AT FASTENER. REMOVED AND REPLACED RIGHT MAIN LANDING GEAR DOOR CENTER HINGE BELLCRANK AND OPS CHECKED IAW B767 MM 32-12-01-4 AND 32-12-00-0.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 41,347 hrs · 35,184 cycles

DURING PREDEPARTURE CHECK, FOUND EMERGENCY LIGHTS INOPERATIVE, WOULD NOT TEST. INSTALLED NEW EMERGENCY LIGHT BATTERY PACK IN THE LOWER POSITION. OPS CHECKED GOOD IAW B767 MM.

Part: BOLT — MISINSTALLED (LT FLAP BEAM) · airframe 41,171 hrs · 35,124 cycles

WHILE INSPECTING THE OUTBOARD SUPPORT BEAM FOR THE LEFT FLAP, FOR AD2002-16-05, FOUND GAP AT FORWARD ATTACH BOLT. INSTALLED BOLT IAW EA27510002-002.

Part: COMPUTER — DEFECTIVE (FUEL SYSTEM) · airframe 40,071 hrs · 34,746 cycles

DURING DESCENT, OBSERVED FUEL DISAGREE PROGRAM 2/2 AND VERIFIED FUEL IMBALANCE. LEFT FUEL QUANTITY LOWER THAN THE RIGHT BY APPROXIMATELY 1,400 LBS. ACCOMPLISHED THE QUICK REFERENCE HANDBOOK PROCEDURES AND SECURED THE LEFT ENGINE IAW THE QRH. PERFORMED FIM PROCEDURE 34-61-00, FIG 106, SHEET 1. FUEL INDICATION CHECKED NORMAL. INSTALLED NEW FUEL QUANTITY PROCESSOR IAW B767 MM 28-41-08-04 FOR PRECAUTIONARY PURPOSES. TRANSPOSED FMC'S FOR TROUBLESHOOTING. INSPECTED WINGS AND ENGINES FOR FUEL LEAKS. NONE FOUND.

Part: HANDLE — LACK OF LUBE (COCKPIT DOOR) · airframe 38,542 hrs · 34,255 cycles

THE COCKPIT DOOR WAS DIFFICULT TO OPEN FROM INSIDE THE COCKPIT. DOOR STUCK, HAD TO BE PRIED OPEN. LUBRICATED DOOR HANDLE MECHANISM. MAINTENANCE OPS CHECKED GOOD.

Part: PUMP — FAILED (NR 1 ENGINE) · airframe 38,204 hrs · 34,148 cycles

THE LEFT HYDRAULIC QUANTITY WENT TO ZERO IN FLIGHT. THE LEFT ENGINE PRIMARY HYDRAULIC PRESSURE LIGHT ILLUMINATED. MAINTENANCE INSPECTED AND REPLACED THE NR 1 ENGINE DRIVEN HYDRAULIC PUMP IAW B767 MM 29-11-05.

Part: MECHANISM — LACK OF LUBE (LDG GEAR DOORS)

LANDING GEAR DOORS SLOW TO CLOSE ON GEAR RETRACTION. GEAR DOOR AMBER LIGHT, NO EICAS MESSAGE. FOUND NOSE GEAR DOOR RELEASE MECHANISM NOT LOCKING PROPERLY. LUBRICATED MECHANISM, DOOR OPS CHECKED NORMAL.