N787AX

Part: DOOR — UNSECURE (ESCAPE REEL) · airframe 61,198 hrs · 44,510 cycles

THE FIRST OFFICER'S EMERGENCY ESCAPE ROPE CONTAINER DOOR OPENED DURING LANDING. WHILE THE AIRPLANE WAS REMOVED FROM SERVICE (GROUNDED), THE FIRST OFFICER'S ESCAPE ROPE WAS RE-STOWED INTO THE ROPE'S CONTAINER IN ACCORDANCE WITH THE 767 AMM SO THAT THE ROPE DID NOT APPLY PRESSURE ON THE DOOR. THE CAUSE OF THE DOOR OPENING WAS THE ESCAPE ROPE HAD SHIFTED POSITION INSIDE THE ROPE'S CONTAINER.

Part: CARABINER — MISSING (FORWARD CABIN) · airframe 60,781 hrs · 44,228 cycles

THREE EMERGENCY DESCENT SAFETY HARNESS CARABINERS WERE MISSING FROM THEIR STOWAGE POUCH. WHILE THE AIRPLANE WAS REMOVED FROM SERVICE (GROUNDED), THREE NEW SAFETY HARNESS CARABINERS WERE INSTALLED INTO THE STOWAGE POUCH. THE CAUSE OF THE MISSING CARABINERS IS UNKNOWN.

Part: ESCAPE REEL — DETACHED (COCKPIT) · airframe 60,059 hrs · 43,923 cycles

THREE DESCENT DEVICES WERE FOUND ON THE FLOOR AFTER TAKEOFF. THE AIRPLANE WAS REMOVED FROM SERVICE. REPLACED WITH SERVICEABLE DESCENT DEVICES.

Part: RHEOSTAT — FAILED (COCKPIT) · airframe 59,894 hrs · 43,856 cycles

AFTER ENGINE START WHEN TURNING OFF THE LEFT OVERRIDE LIGHT SWITCH, THE "MAIN PNL FLOOD LT" CIRCUIT BREAKER TRIPPED OPEN. SMOKE AND AN ELECTRICAL ODOR WERE OBSERVED IN THE FORWARD-RIGHT SIDE OF THE FLIGHT DECK. THE AIRPLANE WAS REMOVED FROM SERVICE (GROUNDED) AND THE RIGHT INSTRUMENT PANEL FLOOD LIGHT RHEOSTAT WAS FOUND INOPERATIVE. THE CAUSE FOR THE OPEN CIRCUIT BREAKER WAS THE FAULTY RIGHT INSTRUMENT PANEL FLOOD LIGHT RHEOSTAT.

Part: STRINGER — CRACKED (BS 676-698) · airframe 59,072 hrs · 43,452 cycles

STRINGER 22L CRACKED 6 INCHES, REPAIRED THE STRINGER IAW SRM 53-00-03 REPAIR 2. AIRCRAFT WAS GROUNDED.

Part: SEAT TRACK — CRACKED (BS 883) · airframe 59,072 hrs · 43,452 cycles

CRACK INDICATION DETECTED AT FASTENER HOLE NR 8 ON THE LEFT HAND STUB BEAM AT BS 883.5, LBL89. REMOVED FASTENERS FROM SEAT TRACK FOR ACCESS REAMED NR 8 HOLE UP UNTIL CLEAN AND ROUND. REPAIRED NR 8 HOLE IN CONJUNCTION WITH IAW REA B653-62098, B653-62101-MR AND JOB CARD 53000049-101. AIRCRAFT WAS GROUNDED.

Part: FRAME — CRACKED (BS 883) · airframe 59,072 hrs · 43,452 cycles

UPPER HALF BS 883.5 LBL89 LOWER SIDE FRAME INNER CHORD CRACKED IN RADIUS LOWER END. VERIFIED BY EDDY CURRENT. REMOVED FASTENERS FOR REPAIR AND FOR ACCESS COMPLIED WITH JOB CARD 53D00049-101 AND REA B653-62101-MR. TRACK TO BE INSTALLED ON NR 0338. SDR: CRACKED .250", PART NUMBER: 145T1004-1, PART NAME: INNER CHORD, LOCATION: FS/BS 883.5, STR/WS LBL 89. AIRCRAFT WAS GROUNDED.

Part: STRINGER — CRACKED (BS 676) · airframe 59,072 hrs · 43,452 cycles

STRINGER SPLICE 24L CRACKED BS 676. REMOVED AND REPAIRED THE STRINGER SPLICE BS 676 - 698 IAW SRM 53-00-03 REPAIR 2 DETAIL 3. AIRCRAFT WAS GROUNDED.

Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,072 hrs · 43,452 cycles

CORROSION ON KEEL PANEL EXTENSION STA 793 TO 808 LBL. REMOVED CORRODED AREA OF KEEL. NDT CHECKED SURFACE AND HOLES FOUND TO BE DEFECTIVE. COMPLIED WITH ENGINEERING REPAIR IAW SRM 51-40-02 AND REA NR B653-62113-MR. CORRODED: LEVEL 2, PN 145T8611-1, KEEL, FS/BS LOCATION, STA 800 STR/WS LOCATION. ACFT WAS GROUNDED.

Part: STRINGER — CRACKED (BS 676-698) · airframe 59,072 hrs · 43,452 cycles

STRINGER 21L CRACKED AFT SIDE OF BS 676. REMOVED AND REPAIRED THE DAMAGE IAW SRM 53-00-03 REPAIR 2 DETAIL 4.

Part: ANGLE — CRACKED (NR 1 NACELLE) · airframe 59,072 hrs · 43,452 cycles

BRACKET FOR OUTBOARD ARROWHEAD PANEL SEAL BETWEEN PYLON AND EXHAUST CRACKED. REMOVED AND FABRICATED BRACKET FOR OUTBOARD ARROWHEAD PANEL SEAL BETWEEN PYLON EXHAUST IAW SRM 54-51-71 AND 51-30-01. BRACKET WILL BE INSTALLED ON NON ROUTINE 0232.

Part: BRACKET — CRACKED (LT PYLON) · airframe 59,072 hrs · 43,452 cycles

UPPER T/E BRACKET FOR INBD ARROWHEAD PANEL SEAL BETWEEN PYLON AND EXHAUST NOZZLE CRACKED. FABRICATED REPAIR ANGLE IAW SRM 51-30-01, FIG 2 ID 1 AND 00838880 TAS 1580875 AND HEAT TREATED IAW BAC 5602, REV AF 20, AVG 2001. CRACKED LENGTH: 1.5", PN 313T3380-236, ANGLE, EXACT FS/BS LOCATION ON ACFT, FROM NAC 308 TO NAC 353. ACFT WAS GROUNDED.

Part: SUPPORT BEAM — CRACKED (LT WING) · airframe 59,072 hrs · 43,452 cycles

LEFT WING T/E UPPER PANEL SUPPORT BEAM FORWARD OF INBD AILERON AT WING STA 431-WING STA 468 IS CRACKED AT THE LNBD END. REMOVED PANEL SUPPORT BEAM. FABRICATED NEW BEAM IAW AIR REA 62094. INSTALLED NEW SUPPORT BEAM IAW SRM 51-40-02, PAR 7D. CRACKED LENGTH: 0.5", PN: 113T1944-49, SUPPORT, EXACT STR/WING STA LOCATION ON ACFT FROM WING STA 431 TO WING STA 468. ACFT WAS GROUNDED.

Part: BUSHING — GALLED (RT MLG) · airframe 59,072 hrs · 43,452 cycles

RT MLG SIDE BRACE AFT OTBD BUSHING HAS GALLING MARKS ON THE INSIDE RACE. REMOVED AND INSTALLED A NEW RT MLG SIDE BRACE AFT OTBD BUSHING IAW REA 62096. LENGTH: GAUGE 1.0", PN: 113T1110-2, SWIVEL SUPPORT BUSHING, SIDE STRUT RT MLG, SN:ABXV050. ACFT WAS GROUNDED.

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,072 hrs · 43,452 cycles

LEFT STA 859.5, LBL89 LOWER LT SIDE FRAME INNER CHORD CRACKED IN RADIUS ON LOWER END, VERIFIED BY EDDY CURRENT. REMOVED FASTENERS, COMPLIED WITH EA 53000047-101. REMOVED FASTENERS WERE REPLACED WITH NEW IAW EA53000047-101. CRACKED LENGTH .250", PN: 145T1052-1, INNER CHORD, FS/BS LOCATION: 859.5, STR WING STA: LBL89. ACFT WAS GROUNDED.

Part: BEAM — CORRODED (TE FLAP) · corrosion level 2 · airframe 56,527 hrs · 42,209 cycles

LEFT FLAP 9 - 10 BEAM 4 AFT ATTACHMENT & 2 FWD ATTACHMENT HOLES ARE CORRODED. REMOVED & RE-ROUTE 9 - 10 BEAM TO COMPONENT SERVICES FOR REPAIR IAW REA C057-61249-MR. REINSTALLED BEAM IAW REA C057-61249-MR. CORRODED L2, PN 113T1266-25, SN NSN, PART NAME LT INBD FLAP 9 - 10 BEAM, LOCATION WS 564.2 TO 668.2. ACFT WAS GNDED.

Part: SUPPORT — CORRODED (RT WING) · corrosion level 2 · airframe 56,527 hrs · 42,209 cycles

RIGHT WING PANEL 661NB AFT PANEL SUPPORT EXFOLIATED. R & R PANEL SUPPORT IAW B657-61286. CORRODED L2, PN 113T1912-29, PART NAME BEAM, SN NSN, STRINGER & WS LOCATION WS 1079.95. ACFT WAS GNDED.

Part: BEAM — CORRODED (TE FLAP) · corrosion level 2 · airframe 56,527 hrs · 42,209 cycles

RIGHT FLAP 9 - 10 BEAM FWD 4 & AFT 2 ATTACHMENT HOLES ARE CORRODED. REMOVED & RE-ROUTE 9 - 10 BEAM TO COMPONENT SERVICES FOR WORK IAW REA C057-61250-MR. REINSTALLED 9 - 10 BEAM & NEW FASTENERS IAW REA C057-6150-MR. CORRODED L2, PN 113T1226-26, SN NSN, PART NAME RT INBD FLAP 9 - 10 BEAM, LOCATION WS 564.2 TO 668.2. ACFT WAS GNDED.

Part: SUPPORT FITTING — CRACKED (SPOILER) · airframe 56,527 hrs · 42,209 cycles

SPOILER ACTUATOR SUPPORT BRACKET CRACKED IN TWO AT RT WING STATION 700. LOCATED JUST FWD OF FLAP TORQUE TUBE SUPPORT. REMOVED & INSTALLED SERVICEABLE FITTING IAW DWG 113T1421. CRACKED 2 INCHES, PN 113T1566-26, SN NSN, PART NAME FITTING, WING SPAR WINGS, STRINGER & WS LOCATION 700 TO 700. ACFT WAS GNDED.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 56,527 hrs · 42,209 cycles

RIGHT 1809 CHORD CRACKED AREA 2 FWD LOWER LE. FWD LOWER FASTENER OF AREA 1 NEEDS REMOVED TO VERIFY DEFECT INDICATION IAW STEP 11 OF TASK CARD NEA53800003-001. REPAIRED CHORD IAW SB 767-53A0078. CRACKED, LENGTH .5, PN 015T1059-4, PART NAME CHORD, SN NSN, FS & BS LOCATION FROM 1809 - 1809 STRINGER & WS LOCATION FROM STRINGER 12R TO 14R. ACFT WAS GNDED.

Part: SPLICE PLATE — CORRODED (RT WING) · corrosion level 2 · airframe 56,527 hrs · 42,209 cycles

FRONT SPAR UPPER CHORD CORRODED ABOVE NR 8 SLAT TAI TELESCOPING DUCT. REPAIRED CORROSION ON UPPER SPLICE PLATE IAW REA B657-61236. L2 CORROSION, PN 114T023-20, PART NAME SKIN SPLICE, SN NSN, LOCATION WS 450 TO 464. ACFT WAS GNDED.

Part: RIB — CRACKED (RT WING) · airframe 56,527 hrs · 42,209 cycles

RIGHT OTBD FLAP NR 7 SUPPORT INBD FLANGE ACTUATOR HOLE AT 1:00 LOOKING INBD HAS A DEFECT INDICATION WITH HFEC ROTARY SCAN, ALSO OTBD FLANGE HOLE AT 12:00 HAS AN INDICATION WITH ROTARY SCAN. REAMED & RE-BUSHINGED HOLE LAW SRM 51-70-16 NDT HOLE NO DAMAGE FOUND. CRACKED 1/64, PN 113T1345-26, PART NAME OTBD FLAP SUPPORT RIB RT WING NR 7 SN NSN, WS LOCATION 617.0. ACFT WAS GNDED.

Part: SPLICE PLATE — CRACKED (NR 1 PYLON) · airframe 56,527 hrs · 42,209 cycles

NUMBER 1 PYLON AT INBD LOWER BEAM HYD BAY DOOR AT AFT END STRUCTURE IS CRACKED ABOVE & BELOW THE BEAM. R & R SPLICE PLATE IAW SRM 51-10-2. CRACKED 2.O INCHES, PN 313T3380-59, PART NAME SPLICE PLATE, SN NSN, STRINGER & WS LOCATION 318.50 TO 318.50. ACFT WAS GNDED.

Part: SPLICE PLATE — CORRODED (RT WING) · corrosion level 2 · airframe 56,537 hrs · 42,209 cycles

FRONT SPAR UPPER CHORD CORRODED AT LES 464. REMOVED CORROSION FOUND TO BE OUT OF LIMITS WILL BE REPAIRED ON REA B657-61236. CORRODED L2, PN 114T023-20, SN NSN, PART NAME UPPER SPLICE PLATE, STRINGER & WS LOCATION LES 464. ACFT WAS GNDED.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,527 hrs · 42,209 cycles

LEFT 1809 CHORD TENSION FITTING AREA 1 UPPER AFT HOLE ELONGATED. PERFORMED PERMANENT REPAIR OF THE FWD CHORD IAW SB 767-53A0078. CORRODED L2, PN 0157T1059-7, 148T904441, 015T1059-3148T2512-7, PART NAME CHORD SPLICE FITTING, TENSION FITTING. CHORD SPLICE, LOCATION FROM 1809.5 TO LH 1809. ACFT WAS GNDED.

Part: RIB — CRACKED (RT WING) · airframe 56,527 hrs · 42,209 cycles

RIGHT WING NR 8 ACTUATOR SUPPORT INBD FLANGE 1 EACH HOLE OVERSIZE, 1 EACH OTBD HOLE. REPAIRED HOLES IAW REA B657-61258-MR, RFTS NR E-46238. CRACKED .0625 INCHES, PN 113T1345-22, PART NAME FLAP SUPPORT RIB NR 8, SN NSN, STRINGER & WS LOCATION WS 798.2. ACFT WAS GNDED.

Part: RIB — CRACKED (LT WING) · airframe 56,527 hrs · 42,209 cycles

LEFT OTBD FLAP NR 2 SUPPORT INBD FLANGE 2 ACTUATOR HOLES AT 12:00 HAVE DEFECT INDICATIONS WITH HFEC ROTARY SCAN. OTBD FLAP NR 2 SUPPORT INBD FLANGE 2 ACTUATOR HOLES AT 12:00 ARE REPAIRED ON REA B657-61257. CRACKED .01562 INCHES, PN 113T1345-25, PART NAME LT WING OTBD FLAP SUPPORT RIB NR 2, SN NSN, LOCATION LT WING OTBD FLAP SUPPORT RIB NR 2.

Part: RIB — CRACKED (LT WING) · airframe 56,527 hrs · 42,209 cycles

FLANGE ACTUATOR HOLE AT 12:00 HAS A DEFECT INDICATION WITH HFEC ROTARY SCAN. CLEANED OUT HOLES LAW AMM 20-10-22 SEE REA 657-61238-MR. CRACKED 1/64, PN 113T1345-19, PART NAME LT WING OTBD FLAP SUPPORT RIB NR 1, SN NSN, STRINGER & WS LOCATION WS 798.2. ACFT WAS GNDED.

Part: STRAP — CRACKED (NR 2 NACELLE) · airframe 56,527 hrs · 42,209 cycles

INSIDE ACCESS PANEL 447BR NR 2 STRUT AFT VERTICAL ROW OF FASTENERS FOR ARROWHEAD PANEL STRUCTURE IS CRACKED. R & R DOUBLER LAW SRM 51-40-02 PER 7. CRACKED 3 INCHES, PN 313T3380-245, PART NAME STRAP, SN N/A, EXACT NACELLE STATION 400, EXACT STRINGER & WS FROM WS 344. ACFT WAS GNDED.

Part: FITTING — CRACKED (NR 2 COWLING) · airframe 56,527 hrs · 42,209 cycles

NUMBER 2 ENG OTBD CORE COWL NR 4 LATCH FITTING CRACKED INSIDE OF POCKET & LOCK FASTENERS ARE DAMAGED. REMOVED OLD LATCH FITTING & DRILLED NEW FITTING IAW SRM 51-40-5 & SRM 51-40-0. INSTALLED NEW FITTING IAW SRM 51-40-02. CRACKED .500, PN 314T1223, PART NAME LATCH FITTING, SN N/A, RT NAC 300. ACFT WAS GNDED.

Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,527 hrs · 42,209 cycles

CENTER BEAM IN LT WW BS 997, LBL 8, WL 115 IS CORRODED. CORRODED AREA WAS BLENDED, FOUND TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-50-12. REPAIRED IAW REA B653-61253-MR & SRM 51-40-02. CORRODED L2, PN 145T8612-1, PART NAME WEB, KEEL BEAM, SN NSN, EXACT FS & BS LOCATION ON ACFT FS 997 TO LBL 8. ACFT WAS GNDED.

Part: BEAM — CRACKED (NR 2 NACELLE) · airframe 56,527 hrs · 42,209 cycles

NUMBER 2 STRUT OTBD LOWER BEAM IS CRACKED AT FWD END. R & R OTBD LOWER STRUT BEAM INSTALLED IAW SRM 51-40-02. INSTALLED BRACKETS IAW SRM-51-40-02. PN 313T1380-242, PART NAME OTBD BEAM, CRACKED 1.75 INCHES, SN N/A, EXACT STRINGER & WS LOCATION ON MC 310 TO 314 LT OTBD FLAP NR 1 SUPPORT OTBD. ACFT WAS GNDED.

Part: SUPPORT — CORRODED (RT WING) · corrosion level 2 · airframe 56,527 hrs · 42,209 cycles

RIGHT WING UPPER PANEL SUPPORT TEE INBD END OF 651MT EXFOLIATED NEAR AFT END OF TEE. R & R UPPER CLAMP LAW SRM 51-40-2. CORRODED L2, PN 113T1623-158, PART NAME CHORD, SN NSN, EXACT STRINGER & WS LOCATION ON NC 273WS TO 275WS. ACFT WAS GNDED.

Part: UNKNOWN — ODOR (CABIN) · airframe 56,308 hrs · 42,098 cycles

NOTICED STRONG ELEC ODOR WITH HOT CUP ON AFTER TWO MINUTES. TURNED OFF & SMELL WENT AWAY. RAN HOT CUP FOR SEVERAL MINUTES, CHECKED GOOD. NO ELEC SMELL NOTICED. CAUSE UNKNOWN.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 54,939 hrs · 41,418 cycles

SUPER NUMERARY EMERGENCY LIGHT INOPERATIVE. TROUBLESHOT IAW AMM 33-50-00-00, AND FOUND M736 POWER SUPPLY INOPERATIVE. R & R BATTERY ASSY. ALL EMERGENCY LIGHTS OK, ACFT WAS GROUNDED.

Part: ANGLE — CRACKED (WING) · airframe 54,118 hrs · 40,990 cycles

ANGLE PIECE AT TOP OF FRONT SPAR TO LEADING EDGE CRACKED AT BOTTOM LOCATED AFT AND ABOVE SLAT PDU BEHIND NUMBER 6 SLAT. REMOVED & REPLACED ANGLE IAW B767-200 SRM 51-40-02, ACFT WAS GROUNDED.

Part: STRUCTURE — CRACKED (NLG WW) · airframe 54,118 hrs · 40,990 cycles

RIGHT NOSE LANDING GEAR VERTICAL CHORD HAS DEFECT INDICATION 11.25 INCHES IN FROM TOP. REPAIRED AREA IAW B767-200 SRM 51-70-12 PG 1 FIG 1, ACFT WAS GROUNDED.

Part: TEE FITTING — CORRODED (RT WING) · airframe 54,118 hrs · 40,990 cycles

RIGHT WING LOWER FORWARD STRUCTURE AT WING STATION 735 HAS CORROSION ON PANEL BRACE TEE CLIP STRUCTURE. REMOVED FWD BEAM AT STA 735, REMOVED TEE CLIP, FABRICATED NEW BEAM FROM 7075-T6 .063 PO 000975, FABRICATED NEW TEE CLIP FROM EXTRUSION BAC 1505-100609-7015-T6511 PO 0032344. TREATED, PRIMED AND PAINTED AND INSTALLED NEW FABRICATED PART IAW BOEING DWG 114T2300 IAW B767 SRM 51-20-01, 51-40-02, ACFT WAS GROUNDED.

Part: SHIM — CORRODED (LT WING) · airframe 54,118 hrs · 40,990 cycles

SHIM PACK UNDER DOUBLER AT LEADING EDGE PANEL ATTACH ANGLE 20 INCHES OUTBOARD OF LEFT WING NUMBER 3 SLAT INBOARD AUX TRACK CORRODED. REMOVED FWD BEAM AT STA 735, REMOVED TEE CLIP, FABRICATED NEW BEAM FROM 7075-T6 .063 PO 000975, FABRICATED NEW TEE CLIP FROM EXTRUSION BAC 1505-100609-7015-T6511 PO 0032344. TREATED, PRIMED, PAINTED AND INSTALLED NEW FABRICTED PART IAW BOEING DWG 114T2300, 114T2210, B767 SRM 51-20-01, 51-40-02, ACFT WAS GROUNDED.

Part: STRUCTURE — CRACKED (NLG WW) · airframe 54,118 hrs · 40,990 cycles

LEFT NOSE LANDING GEAR VERTICAL CHORD HAS DEFECT INDICATION 11 INCHES FROM TOP. INSTALLED REPAIR ON LEFT NOSE LANDING GEAR VERTICAL CHORD IAW B767-200 SRM 51-70-12, ACFT WAS GROUNDED.

Part: SKIN — DENTED (FUSELAGE) · airframe 54,118 hrs · 40,990 cycles

FORWARD LEFT FUSELAGE STA 526 S30L-31L HAS UNMARKED DENT. REPAIRED DENT IAW B767-200 SRM 53-00-01 FIG 201 REPAIR 14, ACFT WAS GROUNDED.

Part: BEAM — CRACKED (FUSELAGE) · airframe 54,118 hrs · 40,990 cycles

OUTBOARD HYDRAULIC BAY DOOR LATCH PLATE ATTACH BEAM CRACKED AT FORWARD END. REMOVED AND REPLACED BEAM IAW B767-200 SRM 51-40-02, ACFT WAS GROUNDED.

Part: BATTERY — DISCHARGED (CABIN) · airframe 56,007 hrs · 41,618 cycles

WHEN EMERGENCY LIGHT, (FLT DECK) TESTED; IT WOULD ILLUMINATE BRIEFLY AND THEN FADE OUT (OVER FLT DECK DOOR). REMOVED & REPLACED BATTERY FOR EMERGENCY LIGHTING AS PER B767 AMM 33- 51-00-2. OPS CHECK OF SYSTEM GOOD, ACFT WAS GROUNDED.

Part: WEB — CRACKED (NR 1 PYLON) · airframe 52,593 hrs · 40,183 cycles

NR 1 PYLON T/E WEB CRACKED AT LOWER O/B CORNER JUST FWD OF PNL 437DB. REPLACED NR 1 PYLON T/E WEB IAW B767 SRM 51-40-02 AWG.

Part: TEE FITTING — CORRODED (FUSELAGE) · airframe 52,593 hrs · 40,183 cycles

LT FAILSAFE STRAP "T" FITTING IS DEEPLY CORRODED AND ONE OF THE FASTENER HOLES HAS INSUFFICIENT. REMOVED AND REPLACED "T" FITTING IAW REA B653-59439-MR, AWG.

Part: SKIN PANEL — CRACKED (FUSELAGE) · airframe 52,593 hrs · 40,183 cycles

SKIN PANEL COMMON TO LT FAILSAFE STRAP "T" FITTING CORRODED. REPAIRED SKIN IAW REA B653-59477-MR, AWG., CRACK AREA: 2" X 6".

Part: SKIN PANEL — CORRODED (FUSELAGE) · airframe 52,593 hrs · 40,183 cycles

SKIN PANEL COMMON TO RT FAILSAFE STRAP "T" FITTING CORRODED. REPAIRED SKIN IAW REA B653-59476-MR, AWG. CRACK AREA: 2" X 5".

Part: FAILSAFE — CRACKED (FUSELAGE) · airframe 52,593 hrs · 40,183 cycles

LEFT FAILSAFE STRAP FS 955 LEFT WHEEL WELL IS CRACKED AT THE 1:00 CLOCK POSITION, CRACK EXTENDS TO .160 FROM RADIUS. DAMAGED REMOVED IAW B767 SB 767-53A0100.

Part: FAILSAFE — CRACKED (FUSELAGE) · airframe 52,593 hrs · 40,183 cycles

LOWER BOLT HOLE OF RT FAILSAFE STRAP IS CRACKED. CRACK IS AT THE 11:00 POSITION ON HOLE AS VIEWED FROM WHEEL WELL. CRACK IS .25 INCH LONG AND .5 INCH FROM FAILSAFE STRAP RADIUS. CUT OUT FAILSAFE IAW REA B653-59436-MR, AWG.

Part: FAILSAFE — CORRODED (FUSELAGE) · airframe 52,593 hrs · 40,183 cycles

CTR FUSELAGE RT FAILSAFE STRAP 'T' FITTING HAS AREA OF DEEP CORROSION (3" AREA). REMOVED AND REPLACED TEE FITTING IAW REA B653-59436-MR, AWG.

Part: SKIN — CORRODED (HORIZ STAB) · airframe 52,593 hrs · 40,183 cycles

CORROSION ON LT HORIZ LWR SKIN O/B RIB 26L FWD STRING S6LWR AT STRING TO SKIN SEAM. PERFORMED CLEAN-UP OF CORROSION IAW 767 SRM 55-10-01 AND REA B655-59480 AWG.

Part: RIB — CORRODED (LT WING) · airframe 52,593 hrs · 40,183 cycles

L/E RIB LEFT WING WS 450 CORRODED. REMOVED AND REPLACED P/N 114T2202-7AX L/E-RIB INSTALLED WITH HI-LOKS AND RIVETS IAW 767 SRM 51-40-02 AWG.

Part: BEAR STRAP — DAMAGED (FUSELAGE) · airframe 52,593 hrs · 40,183 cycles

C/W REA B653-59457MR, REPAIR FUSELAGE SKIN & BEAR STRAP, STA 1350, S31R. C/W REA B653-59457MR, REPAIR FUSELAGE SKIN & BEAR STRAP, AWG. ALSO SEE SDR CONTROL ABXA2011080287 FOR BEAR STRAP/SKIN DETAIL.

Part: BEAM — CORRODED (LT WING) · airframe 52,593 hrs · 40,183 cycles

LT LEADING EDGE RIB GUSSET (BEAM) AT LES 446.10 HAS AREA OF CORROSION. REMOVED AND REPLACED NOSE BEAM IAW 767 SRM 51-40-02 AWG.

Part: WEB — CRACKED (ZONE 500) · airframe 52,593 hrs · 40,183 cycles

LT WING L/E WEB AT WS 475 AT NR 5 SLAT AREA HAS CRACKED INBD UPPER CORNER. REMOVED L/E WEB. REPAIRED IAW SRM CH 51-70-11 AND INSTALLED IAW SRM CH 51-40-2 AWG.

Part: CHANNEL — CRACKED (NR 1 PYLON) · airframe 52,593 hrs · 40,183 cycles

NR 1 PYLON LOWER T/E "U" CHANNEL IS CRACKED. JUST FWD OF PANEL 437. REMOVED AND REPLACED NR 1 PYLON LOWER TRAILING EDGE "U" CHANNEL IAW B767 SRM 51-40-02.

Part: SUPPORT ANGLE — CRACKED (NR 1 PYLON) · airframe 52,593 hrs · 40,183 cycles

NR 1 PYLON UPPER T/E SUPPORT ANGLE CRACKED JUST FWD OF PNL 437DB. REMOVED AND REPLACED NR 1 PYLON UPPER TRAILING EDGE SUPPORT ANGLE IAW B767 SRM 51-40-02.

Part: RIB — CORRODED (LT WING) · airframe 52,593 hrs · 40,183 cycles

NR 4 SLAT INBD AUX TRACK OUTBD LOWER PANEL ATTACH RIB CORRODED AROUND FORWARD NUT PLATE AND ATTACH FITTING SHIM PACK CORRODED ON OUTBD SIDE. REMOVED AND REPLACED RIB AND SHIM INSTALLED WITH HILOKS IAW 767 SRM 51-40-02 AWG.

Part: STIFFENER — CRACKED (RT PYLON) · airframe 52,593 hrs · 40,183 cycles

RIGHT PYLON STIFFENER CRACKED OUTBD SIDE ABOVE EXHAUST NOZZLE UNDER PNL 446 CR. REMOVED & REPLACED STIFFENER WITH NEW PART WORKED IAW 767 SRM 51-40-02. ENGINE WAS REMOVED AND AWG.

Part: BEAM — CRACKED (NR 2 PYLON) · airframe 52,593 hrs · 40,183 cycles

INSIDE NUMBER 2 PYLON UNDER 447BL ACCESS A LWR SUPPORT CHANNEL (BEAM PER DRAWING 313T1380) THE WAS FOUND CRACKED AT THE FWD END. REMOVED & REPLACED LOWER INBD CHANNEL & STRIKER PLATES. REMOVED & INSTALLED NEW FASTENERS IAW 767 SRM 51-40-2 AWG.

Part: BEAR STRAP — DAMAGED (FUSELAGE) · airframe 52,593 hrs · 40,183 cycles

FUSELAGE REPAIR EXTNL SKIN/INTRNL BEAR STRAP INSTALL ACCOMPLISHED JOB CARD REAB653-59457-MR DUE TO DUE TO PREVIOUS LINE DAMAGE INTERIM REPAIR ABX REA B65-58940-MR; DAMAGE CUTOUT 1.375 INCH AFT OF DOOR CUTOUT AND 1.50 INCH TALL, AIRCRAFT WAS GROUNDED.

Part: SILL — CORRODED (FUSELAGE) · airframe 52,593 hrs · 40,183 cycles

ALC DOOR SURROUND, MAIN SILL INNER CORD IS CORRODED AT FS 1346. REPAIRED ALC DOOR SURROUND SILL AS REQUIRED, IAW REA B653-59449 AWG.

Part: FAILSAFE — CRACKED (FUSELAGE) · airframe 52,593 hrs · 40,183 cycles

TERMINATING ACTION ON RT FAIL SAFE STRAP AT ST 955. COMPLIED WITH REA B653-59436-MR.

Part: GASKET — DAMAGED (RT ENGINE) · airframe 52,335 hrs · 40,020 cycles

FUEL LEAK RIGHT ENGINE. FOUND DAMAGED GASKET ON FUEL TUBE AT ENGINE DRIVEN FUEL PUMP. REPLACED GASKET IAW AMM 73-11-06-6 AND PERFORMED ENGINE T/O POWER AND LEAK CHECK IAW AMM 71-00-00-5 TEST 4. FOUND NO LEAKS AT THIS TIME. AIRCRAFT WAS GROUNDED.

Part: INERTIA REEL — UNSERVICEABLE (CABIN) · airframe 52,313 hrs · 40,010 cycles

DURING S/C FOUND NR 2 INERTIAL REEL UNSERVICEABLE. DEFERRED 68428. DEFERRED IAW MEL 15-61-1-1, CAT C, CODE 11.

Part: HARNESS — MISSING (CABIN) · airframe 52,313 hrs · 40,010 cycles

ONE DESCENT HARNESS MISSING FROM SUPERNUMERARY AREA. DEFERRED IAW MEL 25-61-1-2 CODE 11, CAT C. PLACARD MSG 4/25/11. AIRCRAFT WAS NOT GROUNDED.

Part: ESCAPE REEL — OUT OF POSITION (NR 1) · airframe 52,229 hrs · 39,976 cycles

NR 1 SUPERNUMERARY INERTIA ESCAPE REEL FELL FROM STORAGE CONTAINER. BLUE SEAL BROKEN, REMOVED NR 1 REEL P/N 379103C-29 S/N 11557. DEF NR 68300 CODE 11 DEFERRED NR 1 SUPERNUMERARY INERTIAL ESCAPE REEL IAW ABX 767 MEL 25-61-1-1 P/N 379103C-29 S/N 11557 MBCB 4/7/11. REMOVED NR 1 REEL. AIRCRAFT WAS NOT GROUNDED.

Part: WIRE — BURNED (CABIN) · airframe 51,862 hrs · 39,762 cycles

EICAS MESSAGE CABIN ALT AUTO 2. FOUND WIRES BURNT AT D6314J AND P WDM 21-31-11 GOES TO OUTFLOW VALVE ACTUATOR.

Part: SKIN — CORRODED (RT WING) · airframe 50,803 hrs · 39,135 cycles

DISCOVERED CORROSION ON WING SKIN UNDER RIGHT WING PANEL P/N 113T1655-22 APPROX RT WING WS 916.75. REPAIRED AREA IAW REA'S B657-58728, B657-58729 AND B657-58730.

Part: WARNING SYSTEM — MALFUNCTIONED (CARGO DOOR) · airframe 50,551 hrs · 38,975 cycles

CLIMBING OUT OF FL 180 MAIN CARGO DOOR LIGHT ILLUMINATED ACCOMPLISHED NON NORMAL PROCEDURE. DEFERRED MAIN DECK CARGO DOOR IAW ABX AIR MEL 52-71-1-2 MAINT PROCEDURE COMPLIED WITHIN 2-52-71-1-10 AND 52-71-1. MBCB 01-06-10 CAT C CODE 11 PLACARD INSTALLED (MUST INSPECT EACH FLIGHT BEFORE).

Part: WARNING SYSTEM — MALFUNCTIONED (CARGO DOOR) · airframe 50,550 hrs · 38,974 cycles

MAIN CARGO DOOR LIGHT ON OUT OF FL280 PERFORMED NON NORMAL PROCEDURE. INSPECTED MAIN CARGO DOOR, NO DEFECTS NOTED OPERATED MAIN CARGO DOOR SEVERAL TIMES, SYSTEM CHECKS NORMAL.

Part: SWITCH — OUT OF ADJUST (CARGO DOOR) · airframe 50,423 hrs · 38,884 cycles

MAIN CARGO DOOR LIGHT ILLUMINATED W/SIREN AT 29000 FT MSL. ACCOMPLISHED ABNORMAL. PRESSURIZATION NORMAL. LIGHT EXTINGUISHED AT 15000 FT MSL. ADJUSTED DOOR DOWN SWITCHES S9019 AND S9020 IAW B767 AMM 52-71-09. DOOR WARNING CHECKS GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (CARGO DOOR) · airframe 50,422 hrs · 38,883 cycles

LEAVING CRUISE ALTITUDE "MAIN CARGO DOOR" LIGHT W/SIREN COME ON. PRESSURIZATION NORMAL. ACCOMPLISHED ABNORMAL PROCEDURE. LIGHT WENT OUT AT 12000FT MSL. PERFORMED INSPECTION MAIN CARGO DOOR INDICATION SYSTEM IAW B767MM 52-71-09-2. SYSTEM CHECKS NORMAL.

Part: SWITCH — OUT OF ADJUST (CARGO DOOR) · airframe 50,423 hrs · 38,884 cycles

MAIN CARGO DOOR LIGHT ILLUMINATED W/SIREN AT 29000 FT MSL. ACCOMPLISHED ABNORMAL. PRESSURIZATION NORMAL. LIGHT EXTINGUISHED AT 15000 FT MSL. ADJUSTED DOOR DOWN SWITCHES S9019 AND S9020 IAW B767 AMM 52-71-09. DOOR WARNING CHECKS GOOD.

Part: PROBE — OBSTRUCTED (PITOT/STATIC SYS) · airframe 50,313 hrs · 5,337 cycles

F/O'S AIRSPEED INDICATED 0, CAPT'S WAS READING 80 ON TAKEOFF, (ABORTED) AT 90 KNOTS CAPT'S AIRSPEED. F/O READS APPROX 65 KNOTS. REMOVED F/O'S PITOT STATIC PROBE, FOUND SMALL OBSTRUCTION, CLEANED PER 767 AMM 34-11-01-7. REINSTALLED F/O'S PITOT STATIC PROBE PER 767 AMM 34-11-01-4. A/S INDICATOR TESTS NORMAL AT THE P61 PANEL.

Part: ENGINE — MALFUNCTIONED (RIGHT) · airframe 50,087 hrs · 38,636 cycles

RECEIVED "R OIL FILTER", COMPLIED WITH PROCEDURE. AT IDLE THRUST, MESSAGE STILL ILLUMINATED, SHUT DOWN ENGINE. EN ROUTE FROM DFW, FLIGHT 402 AIR DIVERTED TO CVG DUE TO RIGHT OIL FILTER MESSAGE. SECURED ENGINE AND LANDED AT CVG WITH NO FURTHER INCIDENT. NR 2 ENGINE REMOVED AND REPLACED IN WORKPACK WO 600304804.

Part: PUMP — BROKEN (HYDRAULIC SYS) · airframe 50,087 hrs · 38,636 cycles

EDP HYD LOW PRESS LIGHT ILLUM EICAS MSG DISPLAYED R HYD PRIMARY PUMP. RIGHT ENG DRIVEN HYD PUMP LEAKING EXTERNAL FROM DRAIN LINE NR 3. REMOVED & REPLACED R EDP IAW ABX AIR B767 MM 29-11-05-4. NO LEAKS NOTED.

Part: STRUCTURE — CORRODED (RT WING TE FLAP) · airframe 48,855 hrs · 38,035 cycles

RIGHT WING OUTBOARD FLAP HAD CORROSION UNDERNEATH THE OUTBOARD SUPPORT BEAM. REMOVED AND REPLACED RIGHT OUTBOARD FLAP IAW B767 MM 27-51-20-4-10.

Part: SKIN — MISREPAIRED (BS 276) · airframe 48,855 hrs · 38,035 cycles

COMPLY WITH REA B653-56867-MR FOR FORWARD FUSELAGE, STA 276, STRINGER 26 RIGHT SKIN REPAIR. REPAIRED FUSELAGE SKIN IAW B767 SRM 53-00-01, FIGURE 201, REPAIR 12 AND REA B653-56867-MR.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,855 hrs · 38,035 cycles

R1 DOOR AFT LOWER CORNER SKIN HAD OUTER SKIN CRACKED. REPAIRED R1 DOOR AT AFT LOWER CORNER IAW B767 SRM.

Part: SKIN — CORRODED (BS 780 S39R) · airframe 48,855 hrs · 38,035 cycles

CORROSION UNDER SKIN CENTER WING FUSELAGE STRINGER 39 RIGHT, STA 780. REPAIRED AREA IAW REA 653-56928-MR.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,855 hrs · 38,035 cycles

R1 DOOR AFT LOWER CORNER INNER SKIN CRACKED. REPAIRED R1 DOOR AT AFT LOWER CORNER IAW B767 SRM.

Part: FLOORBEAM — CRACKED (BS 1092) · airframe 48,855 hrs · 38,035 cycles

FLOORBEAM ANGLE AT RIGHT BUTT LINE 25, STA 1092 WAS CRACKED AT UPPER END. REMOVED AND REPLACED ANGLE IAW B767 SRM 51-40-02 AND 53-60-07.

Part: BEAM — CORRODED (CARGO DOOR) · airframe 48,855 hrs · 38,035 cycles

FORWARD LOWER CARGO DOOR BEAM HAD EXFOLIATED CORROSION AT SEVERAL NUT-PLATE AREAS. REMOVED AND REPLACED BEAM ON FORWARD LOWER CARGO DOOR IAW B767 SRM.

Part: SKIN — CRACKED (BS 1832) · airframe 48,855 hrs · 38,035 cycles

AFT FUSELAGE SKIN CRACKED FORWARD OF RIGHT APU DOOR APPROXIMATELY STA 1832. REPAIRED CRACK IAW B767 SRM 53-00-01, FIGURE 207.

Part: SKIN — CORRODED (NR 2 SLAT) · airframe 48,855 hrs · 38,035 cycles

NR 2 SLAT HAD A LARGE CORROSION BULGE ON THE LOWER SURFACE OF LEADING EDGE, NEAR THE INBOARD END. REMOVED, REPAIRED AND REINSTALLED NR 2 SLAT ON SHOP TRAVELER ST-2279-01 AND PWS15, AND IAW B767 AMM 27-81-02-4.

Part: BULKHEAD — DENTED (FUSELAGE) · airframe 46,441 hrs · 37,129 cycles

DENT IN AFT PRESSURE BULKHEAD (NEA53800006-787AX1) WAS OUT OF LIMITS IAW B767 SRM 53-80-08. REPAIRED DENT IN AFT PRESSURE BULKHEAD IAW B767 SRM 53-80-08. WORK ACCOMPLISHED ON JC 2024 T-3. CUT OUT 1 INCH PO 408452415. 24 EA BACR15BB5 FASTENERS.

Part: SPAR — CORRODED (RIGHT WING) · airframe 46,441 hrs · 37,129 cycles

RIGHT WING REAR SPAR AREA HAD PANEL STRUCTURE WITH CORROSION UNDER NUT PLATES. AREA WAS PREVIOUSLY BLENDED AT WBL 280 NEAR INBOARD AILERON. REPAIRED CORRODED AREA OF SPAR IAW B767 SRM 57-51-02.

Part: ATTACH ANGLE — CRACKED (RT WING SLAT) · airframe 46,441 hrs · 37,129 cycles

TWO EA NOSE RIB TO LEADING EDGE ATTACH ANGLES CRACKED AT NR 8 SLAT OUTBOARD DRIVE CUTOUT. REMOVED AND REPLACED RIB IAW B767 SRM 51-40-02.

Part: SELECTOR VALVE — BINDING (MLG) · airframe 45,264 hrs · 36,671 cycles

INBOUND TO ILN DID A GEAR RECYCLE. GEAR DISAGREE LIGHT WITH THREE GREEN. FOUND SHAFT ON MAIN LANDING SELECTOR VALVE BINDING. REMOVED AND REPLACED MAIN LANDING GEAR SELECTOR VALVE IAW B767 AMM 32-31-02-4. OPS AND LEAK CHECKED GOOD.

Part: MODULE — DEFECTIVE (MLG) · airframe 45,211 hrs · 36,655 cycles

WITH GEAR HANDLE DOWN, 3 GREEN LIGHTS. GEAR DISAGREE ILLUMINATED AND GEAR DISAGREE MESSAGE. GEAR RECYCLED. LANDING GEAR HANDLE MODULE WAS REMOVED AND REPLACED IAW BOEING MM.

Part: BUSHING — DIRTY (MLG) · airframe 44,544 hrs · 36,419 cycles

WHEN LOWERED, THE GEAR HAD 3 GREEN LIGHTS WITH A GEAR DISAGREE LIGHT. LANDED WITH GEAR DISAGREE LIGHT, STAYED ON UNTIL PARKED. SWUNG GEAR AND VERIFIED GEAR DISAGREE LIGHT REMAINED ON WITH GEAR DOWN AND LOCKED. ISOLATED PROBLEM TO DIRTY GEAR LEVER BUSHING. CLEANED GEAR LEVER ROD OF OLD LUBE AND DIRT. BUSHING DID NOT REQUIRE LUBE. SWUNG GEAR AGAIN. PERFORMED SYSTEM TEST IAW B767 AMM 32-32-00. NO FAULTS NOTED. GEAR LEVER WORKED WITHOUT BINDING.

Part: CONTROL VALVE — FAILED (A/C PACK) · airframe 43,791 hrs · 36,141 cycles

INBOUND CREW REPORTED ODOR DURING RIGHT AC PACK OPERATION AND ERRATIC OPERATION OF IT'S CONTROL SYSTEM. FOUND SEVERAL ELECTRICAL CONNECTORS LOOSE ON THE RT AC PACK FLOW CONTROL VALVE. RESEATED AND TIGHTENED CONNECTORS. RAN PACK, OPS CHECKED GOOD.

Part: CHANNEL — CORRODED (C2 DOOR) · airframe 40,469 hrs · 34,990 cycles

"T" CHANNEL CORRODED, C2 BAG BIN DOOR, BELOW DOOR VENT CUTOUTS. REPLACED "T" CHANNEL IAW BOEING SRM.

Part: MOTOR — LEAKING (L/E SLAT) · airframe 38,726 hrs · 34,413 cycles

AN OIL ODOR WAS DETECTED IN THE AIR CONDITIONING SYSTEM DURING TAKEOFF. RAN UP PACKS WITH APU. SUSPECT ODOR FROM THE RIGHT PACK. FOUND EVIDENCE OF HYDRAULIC LEAK. SKYDROL AROUND THE PNEUMATIC DUCT CONNECTION IN THE KEEL AREA, RIGHT SIDE OF AIRCRAFT. REPLACED LEAKING INBOARD SLAT DRIVE HYDRAULIC MOTOR IAW B767 MM 27-81-11-4. OPS AND LEAK CHECKED GOOD. PERFORMED AIR CONDITIONING SYSTEM OIL CONTAMINATION REMOVAL IAW B767 MM 21-00-21-2 FOR THE RIGHT AC PACK.

Part: SEAL — WORN (NLG WHEEL WELL) · airframe 38,293 hrs · 34,259 cycles

A MEDIUM FREQUENCY LOUD TONE ACCOMPANIED BY AIRFRAME VIBRATION WAS FELT IN THE YOKE AND RUDDER PEDALS, WHILE CLIMBING THROUGH 12000 ACCELERATING TO 280 KNOTS. THE TONE CONTINUED UNTIL FL310. THE TONE CEASED UPON LEVAL OFF AT FL350. MAINTENANCE INSPECTED THE LEFT AND RIGHT FORWARD GEAR DOORS AND LINKAGES. THE DOORS WERE DEFERRED PER ABX REA B652-42367. LATER, THE NOSE LANDING GEAR SEALS WERE REPLACED, IAW B767 MM32-22-02 AND THE DEFERRAL WAS REMOVED.

Part: INDICATOR — MALFUNCTIONED (COCKPIT) · airframe 38,293 hrs · 34,259 cycles

BOTH LEFT AND RIGHT GLIDE SLOPES WERE FLAGGED. MAINTENANCE PERFORMED B767 FIM 22-00-02, FIG 113. A CAT III EVALUATION APPROACH WAS COMPLETED WITH SATISFACTORY RESULTS.

Part: DOOR — OUT OF ADJ (NLG) · airframe 38,150 hrs · 34,210 cycles

DURING CLIMB, THERE WAS A LOUD NOISE AND AIRFRAME VIBRATION AT SPEEDS ABOVE 280 KTS BETWEEN 15,000 TO 20,000 FEET. NO LOUD NOISE OR VIBRATION DURING CRUISE OR DESCENT. VISUALLY INSPECTED UPPER AND LOWER FUSELAGE AND ALL CONTROL SURFACES. NO DEFECTS NOTED. FOUND THE LEFT AFT NLG DOOR LEADING EDGE OUT OF TOLERANCE. ADJUSTED IAW 767 AMM 32-22-04-4. OPS CHECKED GOOD ON GEAR SWING. FUNCTIONAL CHECK FLIGHT EVALUATION WAS SATISFACTORY.

Part: STRUCTURE — VIBRATION (FUSELAGE) · airframe 38,148 hrs · 34,208 cycles

THERE WAS A LOUD NOISE ON BOTH SIDES OF THE COCKPIT AND AIRFRAME VIBRATION AT AIRSPEEDS ABOVE 310 AT 10,000 TO 20,000 FOOT ALTITUDES. INSPECTED FLAPS, GEAR WELL AREAS, FLIGHT CONTROLS. RAN FLIGHT CONTROLS THRU. PRESSURIZED AIRCRAFT TO 6 PSI. INSPECTED MEC AREA AND DOOR SEAL. INSPECTED FORWARD EQUIPMENT AREA DOOR SEAL. NO DEFECTS FOUND.

Part: ODOR — DETECTED (CABIN) · airframe 37,944 hrs · 34,136 cycles

THERE WAS AN OIL SMELL FROM THE ENVIRONMENTAL SYSTEM ON TAKEOFF. REMOVED LEFT AND RIGHT CHECK VALVES (ENGINE SUPPLY) AND INSPECTED FOR OIL CONTAMINATION, NONE FOUND. REINSTALLED VALVES IAW B767 MM 36-20. RAN BOTH PACKS ON ENGINE PNEUMATICS, FULL HOT AND COLD AND AT VARIOUS POWER SETTINGS. NO ODOR NOTED. ENGINES RUN IAW B767-10A. OPERATED BOTH PACKS WITH APU AND EXTERNAL PNEUMATIC SUPPLIES. NO ODOR NOTED. REMOVED APU BLEED AIR DUCT AT APU AND APU BLEED AIR VALVE. NO VISIBLE OIL CONTAMINATION FOUND. REINSTALLED BLEED AIR DUCT AND BLEED AIR VALVE. LEAK AND OPS CHECKED GOOD.

Part: ISOLATION VALVE — MALFUNCTIONED (BLEED AIR) · airframe 37,763 hrs · 34,073 cycles

DURING CLIMBOUT OF KDAL, THERE WAS A BAD OIL ODOR. DISSIPATED AT HIGH ALTITUDE AND WHEN RIGHT PACK WAS TURNED OFF. PASSING 13,000 FEET, ODOR RETURNED. CREW DONNED OXYGEN MASKS DUE TO ODOR. CHECKED NR 1 AND NR 2 INLETS AND EXHAUST, NR 1 AND NR 2 ENGINE 8TH AND 14TH STAGE OUTLET DUCTS. REPLACED RIGHT ISOLATION VALVE. CHECKED LEFT AND RIGHT ACM TURBINE OUTLET DUCTS. NO DEFECTS NOTED ON NR 1 OR NR 2 ENGINES. COMPLIED WITH ENGINE RUN, NR 1 AND NR 2 AT VARIOUS POWERS AND PNEUMATIC SETTINGS WITH NO ABNORMAL ODORS NOTED IAW B767 MM 71-00.

Part: PSEU — MALFUNCTIONED (COCKPIT) · airframe 37,684 hrs · 34,039 cycles

EICAS MESSAGE LANDING GEAR MONITOR DISPLAYED WITH LANDING GEAR UP AND LOCKED. REPLACED PSEU PER B767 MM 32-09-03. OPS CHECKED GOOD.