N769AX

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 58,094 hrs · 43,760 cycles

EMERGENCY LIGHT SPARE BATTERY PACK M737 IS INOPERATIVE. THE EMERGENCY LIGHT BATTERY PACK M737 WAS REPLACED. THE CAUSE OF THE INOPERATIVE BATTERY PACK WAS A DISCHARGED BATTERY.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 58,085 hrs · 43,757 cycles

CREW SERVICE AREA INTERIOR LIGHTS ARE INOPERATIVE WHEN IN EMERGENCY LIGHTS MODE. THE EMERGENCY LIGHT BATTERY PACK M736 WAS REPLACED. THE CAUSE OF THE INOPERATIVE LIGHTS WAS A DISCHARGED BATTERY.

Part: MODULE — FAULTY (FIRE WARNING) · airframe 56,378 hrs · 42,885 cycles

FIRE WARNING BELL CAME ON CONTINUOUSLY WITH NO OTHER INDICATIONS. TESTED FIRE WARNING, ALL INDICATIONS NORMAL. REPLACED AURAL WARNING MODULE.

Part: UNKNOWN — ODOR (CABIN) · airframe 54,788 hrs · 42,011 cycles

LAVATORY SMOKE DETECTOR WENT OFF DURING CLIMB THROUGH 360 FT, SHORTLY AFTER SELECTING RT PACK ON. STRONG WIRE BURNING ODOR WAS NOTICED IN COCKPIT. NO OTHER INDICATIONS WITH RT PACK ON. TEMP IN FWD & AFT CABIN WILL NOT GO BELOW APPROXIMATELY 22-24 DEGREES. DUCT PRESS INDICATES NR 1, 60 PSI FOR A SHORT TIME WITH PACK OFF. VISUALLY INSPECTED ACFT PACKS, WITH NO FAULTS NOTED. OPERATED ACFT AIR CONDITIONING PACKS FOR 25 MINS ON THE GROUND, WITH NO ODOR NOTED. PACKS CONTROLLED AND OPERATED IAW MM 21-00-00. COMPLIED WITH BITE OF BOTH LT & RT PACKS TEMPERATURE CONTROLLERS WITH NO FAULTS NOTED IAW FIM 21-50-00-1. ALSO C/W BITE CHECK OF THE ZONE TEMP CONTROLLER FIM 21-60-00-1, WITH NO FAULTS FOUND.

Part: STRUCTURE — CORRODED (WING) · corrosion level 2 · airframe 54,564 hrs · 41,885 cycles

UPPER PANEL ATTACH CAP ON RIB FROM REAR SPAR TO T/E AT WS 433 HAS CORROSION UNDER NUTPLATE. FABRICATED NEW CAP IAW DWG 113T1510, HEAT TREATED TO T6 IAW BAC 5602, TABLE 1, PAGE 12 AND 17 NOTE C, INSTALLED NEW CAP IAW SRM 51-40-02 AND AMM 20-11-00D.

Part: FRAME — CRACKED (NR 1 NACELLE) · airframe 54,564 hrs · 41,885 cycles

NR 1 PYLON INBD FRAME BELOW HYD BAY ACCESS DOOR CRACKED AT FWD LATCH FITTING. R & R DEFECTIVE FRAME IAW SRM 51-40-2. ACFT WAS GROUNDED.

Part: ANGLE — CRACKED (VERTICAL STAB) · airframe 54,564 hrs · 41,885 cycles

STRUCTURE INSIDE OF VERTICAL STAB PANEL 324CLX, ON TOP OF FUSELAGE HAS CRACKS IN FWD ANGLE. REMOVED WEB TO FORM IAW SRM 51-40-02, DRILLED AND INSTALLED NEW STIFFENER IAW SRM 51-40-05 AND 51-40-02,

Part: CHANNEL — SPLIT (WING) · airframe 54,564 hrs · 41,885 cycles

T/E PANEL, 661NB LOWER AFT ATTACH CHANNEL AND BRACKET FROM REAR SPAR TO T/E AT WS 1055 SPLIT. R & R AFT LOWER ATTACH BRACKET AND CHANNEL IAW SRM 51-40-02.

Part: SPAR — CORRODED (LT WING) · airframe 54,564 hrs · 41,885 cycles

LEFT WING REAR SPAR APPROX. W.S. 250 AT APU FUEL SHUTOFF VALVE MOUNTING BASE CORRODED. MARKED. REPAIRED REAR SPAR IAW REA B657-60671-MR. REAR WING SPAR, PN: 112T1007-7, SN: NSN, LOC: RSS-250.00, CORRODED; ACFT WAS GROUNDED.

Part: LAMP — UNSECURE (EMERGENCY LIGHT) · airframe 54,401 hrs · 41,793 cycles

ENTRY DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. FOUND LAMP NOT SECURED IN SOCKET. SECURED LAMP IAW AMM 33-51-06-2. LIGHT OPERATES NORMAL, ACFT WAS GROUNDED.

Part: PRESSURE PANEL — CORRODED (LT MLG WW) · airframe 53,878 hrs · 41,422 cycles

LEFT WHEEL WELL PRESSURE DECK PANEL HAS CORROSION AT THE FWD ATTACH HOLES (UPPER SIDE). NEW PANEL FABRICATED PER BOEING DWG 145T8752. ACFT WAS GROUNDED.

Part: FAILSAFE — CRACKED (FUSELAGE) · airframe 53,878 hrs · 41,422 cycles

RIGHT FAILSAFE CRACKED. FAILSAFE STRAP TERMINATING ACTION PERFORMED ON EA 53500014-003, AMES DOCUMENT 47008ORD04, ACFT WAS GROUNDED.

Part: SKIN — CORRODED (FUSELAGE) · airframe 53,878 hrs · 41,422 cycles

STA 955 FOUND CORROSION UNDER FAILSAFE TRIM OUT. CORROSION MIGATES BACK UNDER FAILSAFE AND FUSELAGE SKIN. REPAIRED AREA OF CORROSION IAW REA 47030REA03. ACFT WAS GROUNDED.

Part: FRAME — CORRODED (FUSELAGE) · airframe 53,878 hrs · 41,422 cycles

LEFT SIDE FRAME FITTING NR 10 & 11 HOLES HAVE CORROSION AROUND THEM ON THE FWD FACE. REPAIRED AREAS OF CORROSION AROUND HOLES NR 10 & 11 IN LEFT SIDE FRAME FITTING IAW 47030REA06, ACFT WAS GROUNDED.

Part: LONGERON SPLICE — CORRODED (FUSELAGE) · airframe 53,878 hrs · 41,422 cycles

LEFT LONGERON SPLICE PLATE HAS CORROSION STA 930-943. REPAIR LEFT LONGERON SPLICES PLATE IAW REA 47030REA05, ACFT WAS GROUNDED.

Part: FRAME — CORRODED (FUSELAGE) · airframe 53,878 hrs · 41,422 cycles

LEFT SIDE FRAME FITTING HAS SEVERAL AREAS OF CORROSION ON THE FORWARD FACE ABOVE HOLE 1. CLEANED AREAS OF CORROSION IAW B767-200 SRM 53-50-08. REMOVED CORROSION WITHIN LIMITS .638 REMAINING FROM ORIGINAL THICKNESS OF .700 VERIFIED WITH NDT. PRIMED AND PAINTED SIDE FITTING IAW AMM 51-21-10, ACFT WAS GROUNDED.

Part: TEE FITTING — CORRODED (FUSELAGE) · airframe 53,878 hrs · 41,422 cycles

RIGHT SIDE PRESSURE DECK TEE FITTING CORRODED AT THE FOWARD LOWER HOLE COMMON TO THE FAILSAFE STRAP. REMOVED AND REPLACED TEE FITTING, REF: B767-200 SRM 51-40-05 IAW EA 53500014-003, AMES DOCUMENT 47008ORD04. ACFT WAS GROUNDED.

Part: STRAP — CORRODED (FUSELAGE) · airframe 53,878 hrs · 41,422 cycles

LEFT FAILSAFE STRAP HAS MULTIPLE AREAS OF HEAVY CORROSION. REMOVED AND REPLACED FAILSAFE STRAP IAW B767-200 SRM 51-40-05 ON EA 53500013-008, AMES DOC. 47008ORD11, ACFT WAS GROUNDED.

Part: FAILSAFE — CRACKED (FUSELAGE) · airframe 53,878 hrs · 41,422 cycles

STA 955 LEFT FAILSAFE LOWER HOLE CRACKED AT 2 O`CLOCK POS APPROX .310 LONG MARKED. LEFT FAILSAFE STRAP REPLACED ON EA 53500013-008, AMES DOC. 47008ORD11. ACFT WAS GROUNDED.

Part: FAILSAFE — CORRODED (FUSELAGE) · airframe 53,878 hrs · 41,422 cycles

STA 955 RIGHT FAILSAFE CUTOUT HAS MINOR CORROSION. CLEANED CORROSION IAW B767-200 SRM 51-10-02. SPOTFACED & REPAIRED AREA IAW ABX EA 53500014-004 & AMES DOC 47008ORD10. ACFT WAS GROUNDED, 145T3310.

Part: TEE FITTING — CORRODED (FUSELAGE) · airframe 53,878 hrs · 41,422 cycles

LEFT PRESSURE DECK TEE FITTING CORRODED AT THE FWD LOWER HOLE COMMON TO THE FAILSAFE STRAP REF B767-200 SRM 51-40-05. REMOVED AND REPLACED TEE FITTING IAW EA53500013-008 AND AMES DOCUMENT 47008ORD11. ACFT WAS GROUNDED.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 53,878 hrs · 41,422 cycles

GUSSET FOR LEFT PRESSURE DECK PANEL IS CORRODED AND GOUGED. FABRICATED NEW GUSSET FROM 2024-T3 .125" PO 0020398 IAW B767 DWG 145T8752. ACFT WAS GROUNDED.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 53,878 hrs · 41,422 cycles

GUSSET FOR RT PRESSURE DECK PANEL IS CORRODED, AND HAS PREVIOUS MISDRILLED HOLE. FABRICATED NEW GUSSET FROM 2024-T3 .125" PO 0020398 IAW B767 DWG 145T8752. ACFT WAS GROUNDED.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 52,990 hrs · 40,932 cycles

SUPPORT ANGLE CRACKED ON FWD SIDE OF STA 1087 LBL 26 IN ALC. REPLACED SUPPORT ANGLE STA 1087 LBL 26 PER B767 DRWING 146T8250, AWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 52,990 hrs · 40,932 cycles

SUPPORT ANGLE CRACKED ON FWD SIDE OF STA 1087 RBL 26 IN ALC. REPLACED SUPPORT ANGLE STA 1087 LBL 26 PER B767 DRAWING 146T8250, AWG.

Part: RIB — CORRODED (LT WING) · airframe 52,990 hrs · 40,932 cycles

NR 4 SLAT INBD AUX TRACK OUTBD RIB IS CORRODED AROUND SEVERAL NUT PLATES. INSTALLED NEW STRUT RIB IAW B767 SRM 51-40-02 & BOEING DWG 114T2209, AWG.

Part: RIB — CORRODED (LT WING) · airframe 52,990 hrs · 40,932 cycles

NR 3 SLAT INBD AUX TRACK OUTBD SUPPORT RIB IS CORRODED AROUND NUMEROUS. REMOVED & REPLACED NR 3 SLAT O/B AUX TRACK L/E RIB IAW B767 SRM 51-40-02 AND REA B657-59581. PERFORMED OPS CHECK OF SLAT PROX SWITCH IAW B767 AMM 27-88-01-2, AWG.

Part: RIB — DAMAGED (LT WING) · airframe 52,990 hrs · 40,932 cycles

INBOARD SIDE OF RIB 8 HAS TOOLING MARKS. BLENDED AREAS AND REPAIRED IAW REA B657-59605 MR, AWG.

Part: FITTING — DAMAGED (LT WING) · airframe 52,990 hrs · 40,932 cycles

LEFT WING BACK UP FITTING FOR OUTBOARD SIDE LOAD FITTING HAS SEVERAL TOOLING MARKS. BLENDED AND REPAIRED AREAS IAW REA B657-59607-MR REV A.

Part: RIB — DAMAGED (LT WING) · airframe 52,990 hrs · 40,932 cycles

LEFT WING FWD OUTBOARD SIDE OF RIB 8 HAS TOOLING MARKS. BLENDED AND REPAIRED AREAS IAW REA B657-59606 MR, AWG.

Part: RIB — CORRODED (LT WING) · airframe 52,990 hrs · 40,932 cycles

NR 3 SLAT OUTBD AUX TRACK INBD UPPER LEADING EDGE RIB IS CORRODED AT FWD END. REMOVED & REPLACED NR 3 SLAT O/B AUX TRACK L/E RIB IAW B767 SRM 51-40-02 AND REA B657-59581. PERFORMED OPS CHECK OF SLAT PROX SWITCH IAW B767 AMM 27-88-01-2, OPS CHECK GOOD, AWG.

Part: FITTING — CORRODED (RT WING) · airframe 52,990 hrs · 40,932 cycles

CORROSION ON RT WING, UPPER SURFACE AT WING TO BODY SPLICE FITTING, BS 950 APPROX., UNDER BRACKET. BLENDED CORRODED AREA IAW B767 SRM 57-20-01 FIG 101, AWG.

Part: FITTING — DAMAGED (RT WING) · airframe 52,990 hrs · 40,932 cycles

SIDE LOAD FITTING TO BACK UP FITTING HAS TOOLING MARKS. BLENDED AREA AND REPAIRED IAW REA B657-59598, AWG.

Part: PBE — UNSERVICEABLE (COCKPIT) · airframe 52,002 hrs · 40,356 cycles

COCKPIT PBE LOST VACUUM. REMOVED AND REPLACED COCKPIT PBE IAW B767 AMM 25-60-00-0.

Part: RIB — CORRODED (LT WING) · corrosion level 2 · airframe 50,606 hrs · 39,629 cycles

CORROSION AT FIXED LEADING EDGE RIB LOWER SIDE JUST INBOARD OF OUTBOARD AUX TRACK NR 2 SLAT WS 934. REMOVED AND REPLACED FIXED LEADING EDGE RIB IAW 767 SRM 51-40-02.

Part: FITTING — CORRODED (LT WING) · airframe 50,606 hrs · 39,629 cycles

CORROSION ON FIXED LEADING EDGE LOWER SIDE JUST OUTBOARD OF OUTBOARD SLAT DRIVE UNIT NR 5 SLAT WS 500. REMOVED AND REPLACED LEADING EDGE ANGLE IAW 767 SRM 51-40-02.

Part: STRUCTURE — CRACKED (NLG WW) · airframe 50,606 hrs · 39,629 cycles

NOSE WHEEL WELL VERTICAL CHORD AT LBL 25 STA 287 IS CRACKED IN RADIUS LOCATED 11.5 INCHES BELOW CEILING. CRACK IS APPROX .625 INCH IN LENGTH.

Part: SUPPORT BEAM — CORRODED (LT WING) · corrosion level 2 · airframe 50,606 hrs · 39,629 cycles

CORROSION LT WING WBL 169 T/E STRUCTURE UPPER BONCED PANEL SUPPORT BEAM. REMOVED AND REPLACE SUPPORT BEAM IAW 767 SRM 51-40-02.

Part: RIB — CORRODED (LT WING) · corrosion level 2 · airframe 50,606 hrs · 39,629 cycles

CORROSION AT FIXED LEADING EDGE RIB LOWER SIDE JUST OUTBOARD OF INBOARD AUX TRACK NR 2 SLAT WS 879. REMOVED AND REPLACED RIB IAW 767 SRM 51-40-2.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,606 hrs · 39,629 cycles

DURING CARGO CONVERSION FOUND CORROSION AND 2.5 INCH CRACK ON UPPER CHORD OF FLC FLOORBEAM AT STA 632 RBL 15 TO RBL 20. REPAIRED CHORD IAW B767 SRM 53-00-7.

Part: SUPPORT BEAM — CORRODED (LT WING) · corrosion level 2 · airframe 50,606 hrs · 39,629 cycles

EXFOLIATION CORROSION LT WING TRAILING EDGE UPPER SUPPORT BEAM WBL 289.45 ANGLE I/B APPROX 12 INCH SPAN. REMOVED CORROSION IAW 767 SRM 51-10-00 IS WITHIN LIMITS IAW 767 SRM 57-51-02 FIG 101.

Part: STRUCTURE — CRACKED (NLG WW) · airframe 50,606 hrs · 39,629 cycles

NOSE WHEEL WELL VERTICAL CHORD AT RBL 25 STA 287 IS CRACKED IN RADIUS LOCATED 11.5 INCHES BELOW W/W CEILING. CRACK IS APPROX .437 INCH IN LENGTH. REPAIRED VERTICAL CHORD IAW 767 SRM 51-70-12.

Part: BEAM — CRACKED (RT PYLON) · airframe 50,606 hrs · 39,629 cycles

RIGHT ENGINE PYLON OUTBOARD BEAM THAT RUNS ACROSS LOWER PART OF HYD BAY ACCESS DOOR IS CRACKED AT 3RD NUT PLATE HOLE FROM FWD END. REMOVED DAMAGED SECTION OF RIGHT ENGINE OUTBOARD PYLON BEAM IN LOWER PART OF HYD BAY ACCESS DOOR AND SPLICED. REPAIRED PER REA B654-58712-MR.

Part: RIB — CORRODED (LT WING) · corrosion level 2 · airframe 50,606 hrs · 39,629 cycles

CORROSION AT FIXED LEADING EDGE RIB LOWER SIDE JUST INBOARD OF OUTBOARD AUX TRACK NR 3 SLAT WS 722. REMOVED AND REPLACED RIB IAW 767 SRM 51-40-02.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,606 hrs · 39,629 cycles

INTERCOSTAL AT RBL 16.4 BETWEEN STA 610 AND 632 CORRODED. REMOVED AND REPLACED INTERCOSTAL IAW 767 SRM 51-4-02.

Part: SKIN — CHAFED (NACELLE) · airframe 50,606 hrs · 39,629 cycles

NR 1 NACELLE STRUT FWD TORQUE BOX OUTBOARD SKIN HAS TWO LONG CHAFES AT METAL STRIP FOR T/R SEAL. REPAIRED IAW REA B654-58712-MR.

Part: STRINGER — CRACKED (CENTER WING) · airframe 50,606 hrs · 39,629 cycles

CENTER WING UPPER STRINGER U-1C AFT BAY OF CENTER DRY BAY HAS A 10 INCH CRACK AT LBBL 87 APPROX AT FSS 945. REMOVED AND REPLACED DAMAGED SECTION OF STRINGER U-1C IAW 767 SRM 57-00-03 REPAIR 1 FIGURE 201.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 50,606 hrs · 39,629 cycles

FOUND 2 AREAS OF CORROSION ON STRINGER 38L BETWEEN STA 412 AND 434. REMOVED AND REPLACED FITTING. INSTALLED WITH HI-LOKS IAW 767 SRM 53-02.

Part: SKIN — CHAFED (NACELLE) · airframe 50,606 hrs · 39,629 cycles

NR 1 NACELLE STRUT, FWD TORQUE BOX, OUTBOARD SKIN HAS 2 SMALL CHAFE AREAS JUST BELOW ACCESS PANEL 432AL. REPAIRED IAW REA B654-58718.

Part: RIB — CORRODED (LT WING) · airframe 50,606 hrs · 39,629 cycles

CORROSION AROUND NUT PLATE ON RIB NOSE FOR NR 4 SLAT INBOARD AUX TRACK APPROX. REMOVED AND REPLACED RIB IAW B767 SRM 51-40-02.

Part: SEAT TRACK — CRACKED (COCKPIT) · airframe 48,658 hrs · 38,557 cycles

FIRST OFFICER'S FORWARD OUTBOARD SEAT TRACK CRACKED AT FORWARD STOP FITTING. REMOVED AND REPLACED TRACK ASSEMBLY IAW B767 SRM 51-40-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,658 hrs · 38,557 cycles

FLOORBEAM CORRODED AROUND NUT PLATE AT FS 720, UNDER LEFT OUTER ROLLER TRAY. REPAIRED FLOORBEAM IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,658 hrs · 38,557 cycles

SHEAR TIE CORRODED AT FS 748, BETWEEN STRINGER 37 - STRINGER 38, RIGHT AFT SIDE OF FRAME. REMOVED SHEAR TIE. FABRICATED AND INSTALLED SHEAR TIE IAW SRM 51-40-2.

Part: STRUCTURE — MISREPAIRED (FUSELAGE) · airframe 48,658 hrs · 38,557 cycles

ENGINEERING REQUESTED REMOVE EXISTING DOUBLER LOCATED AT STA 220.5, STRINGER 24 LEFT. REPAIR DID NOT MEET SRM REQUIREMENTS. REMOVED AND REPLACED DOUBLER IAW REA B653-57078-MR.

Part: PANEL — CORRODED (FUSELAGE) · airframe 48,658 hrs · 38,557 cycles

PANEL 221F LEFT BUTT LINE 51 TO LEFT BUTT LINE 86 HAD LEVEL I CORROSION AT CLIP NUTS. REPAIRED IAW REA B653-57098-MR.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 48,658 hrs · 38,557 cycles

CORROSION ON FLOORBEAM AT FS 368, RIGHT BUTT LINE 25. REPAIRED 9G NET STRAP FITTING IAW REA B653-57096-MR.

Part: FITTING — CORRODED (FUSELAGE) · airframe 48,658 hrs · 38,557 cycles

LEVEL I CORROSION ON FITTING AT FS 368, LEFT BUTT LINE 28. REPAIRED IAW REA B653-57097-MR.

Part: BEARING — WORN (LT AILERON) · airframe 48,658 hrs · 38,557 cycles

THE LEFT INBOARD AILERON OUTBOARD PCA SUMMING LINKAGE HAD A WORN BEARING. REPLACED LEFT INBOARD AILERON OUTBOARD PCA IAW B767 AMM 27-11-48-2.

Part: MOUNT FITTING — CRACKED (FLAP ACTUATOR) · airframe 48,658 hrs · 38,557 cycles

KRUEGER FLAP ACTUATOR OUTBOARD MOUNT FITTING CRACKED. REMOVED AND REPLACED FITTING IAW B767 SRM.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 48,658 hrs · 38,557 cycles

R1 DOOR CUTOUT LOWER AFT CORNER INNER DOUBLER HAD A CRACK INDICATION BOTH SIDES OF MARKED HOLE. REPAIRED AREA IAW REA B653-57053-MR.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,658 hrs · 38,557 cycles

FUSELAGE SKIN CRACKED AT FASTENERS FS 1654, STRINGER 3 LEFT. REPAIRED FUSELAGE SKIN AT FS 1654 AND STRINGER 3 LEFT IAW B767 SRM 53-80-01, FIGURE 201.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 47,168 hrs · 37,734 cycles

RT UPPER CABIN WINDOW CRACKED. FIRST WINDOW FORWARD OF THE EMERGENCY EXIT DOOR. REPLACED CABIN WINDOW IAW AMM 56.

Part: FRAME — CRACKED (BS 1809) · airframe 47,075 hrs · 37,689 cycles

WHILE ACCOMPLISHING A REPETITIVE EDDY CURRENT INSPECTION TO THE RIGHT OUTER CHORD AT BULKHEAD STA. 1809, SEVERAL CRACKS WERE CONFIRMED. REPAIRED RIGHT OUTER CHORD PER J.C.'S 53800002-001, 002, 003, AND W/O# 600251128.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 46,762 hrs · 37,580 cycles

L1 DOOR EMERGENCY LIGHTS INTERIOR AND EXTERIOR INOP. SWAPPED BATTERY PACKS FROM M735 & M736 POWER SUPPLIED L1 DOOR EMERGENCY EXIT LIGHTS OPC GOOD IAW ABX 767 AMM 33-51-07. REPLACED M736 POWER SUPPLY BATTERY PACK WITH NEW BATTERY PACK ACQUIRED FROM DELTA OPC GOOD IAW ABX B767 AMM 33-51-07.

Part: SEAT TRACK — CORRODED (AFT CABIN) · airframe 40,303 hrs · 35,286 cycles

CABIN SEAT TRACKS CORRODED STA 1165-1200, LBL 18. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW B767 SRM 53-00-52. DRILLED IAW DWG 96FS667807, INSTALLED TRACK IAW B767 SRM 51-40-02.

Part: CAP — CORRODED (CARGO DOOR) · airframe 40,303 hrs · 35,286 cycles

FORWARD CARGO DOOR TOP T-CAP HAD OUT OF LIMITS CORROSION AT SEVERAL AREAS. FABRICATED T-CAP IAW BOEING DWG 140T2607. INSTALLED T-CAP AND WEBS IAW B767 SRM 51-40-02. INSTALLED CARGO DOOR IAW B767 MM 52-34-01. OPS CHECKED GOOD.

Part: SEAT TRACK — CORRODED (AFT CABIN) · airframe 40,303 hrs · 35,286 cycles

CABIN SEAT TRACKS CORRODED STA 1165-1200, LBL 18. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW B767 SRM 53-00-52. DRILLED IAW DWG 96FS667807, INSTALLED TRACK IAW B767 SRM 51-40-02.

Part: SLAT — CORRODED (RIGHT WING) · airframe 40,313 hrs · 35,286 cycles

RIGHT WING #11 SLAT INBOARD LEADING EDGE ANGLE WAS CORRODED. REMOVED CORROSION OUT OF LIMITS IAW B767 SRM 57-43-02. REPAIRED AREA IAW B657-43913MR.

Part: ODOR — DETECTED (CABIN) · airframe 39,945 hrs · 35,165 cycles

AT TAKEOFF AND THROUGHOUT CLIMB, THERE WAS AN OIL SMELL COMING FROM THE ENVIRONMENTAL SYSTEM. RAN BOTH PACKS ON GROUND, NO SMELL NOTICED. OPS CHECKED GOOD.

Part: SWITCH — WORN (THROTTLE) · airframe 39,410 hrs · 34,970 cycles

DURING TAXI INTO GATE, THE NR 2 THRUST REVERSER DEPLOYED UNCOMMANDED, WOULD NOT STOW. DFDR DATA WAS REVIEWED AND THE DATA SHOWED THAT THE REVERSER DID NOT STOW AFTER LANDING. THE THROTTLE MICROSWITCH PACK WAS FOUND WORN WHICH PREVENTED THE THRUST REVERSER FROM STOWING AFTER LANDING. MICROSWITCH PACK WAS REPLACED IAW DC-9 MM. OPS CHECKED GOOD.

Part: ODOR — DETECTED (COCKPIT) · airframe 39,079 hrs · 34,855 cycles

DURING INITIAL CLIMB AND ENROUTE CLIMB, THE AIR CONDITIONING SYSTEM HAD AN OILY ODOR AND TASTE IN THE COCKPIT AND MAIN CABIN. MAINTENANCE RAN AIR CONDITIONING PACKS AND ENGINE PNEUMATICS AT TAKEOFF POWER. NO ODORS WERE NOTED. OPERATIONAL CHECKS WERE COMPLETED IAW B767 FRM 21, FIG 25A.