N764CK
Registered owner: KALITTA AIR LLC, MI (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
LEFT ENG FIRE LP1 STATUS MESSAGE INTERMITTENTLY. ITEM PLACED ON MEL 26-11-1-1 PLACARD INSTALLED MBCB 07/10/2026 A/C REMAINS NO ETOPS. A/C RETURNED TO SERVICE.
DURING CREW PREFLIGHT, L ENG FIRE LP 2 STATUS MESSAGE ILLUMINATED. MTX DEFERRED IAW ABX B767 MEL 26-11-1-1. PLACARDS INSTALLED. MX PROCEDURES C/W. MBCB 07/09/26. A/C REMAINS NO ETOPS. RETURNED A/C TO SERVICE.
ON PREFLIGHT HAD A STATUS LEVEL L ENG FIRE LP1 THRT WOULD NOT CLEAR. MTX GROUNDED A/C AND PERFORMED OPS CHECK OF FIRE OVHT. MSG CLEARED. AIRCRAFT REMAINS NO ETOPS IAW B767 AMM 26-11-00. OPS CHECK GOOD. MTX RETURNED A/C TO SERVICE.
LEFT ENG FIRE LOOP LP1 STATUS MSG MTX GROUNDED AC AND DEFERRED LH ENGINE LOOP LP1 FOR DEPARTURE IAW MEL ABX-26-11-1-1. AND RETURNED ACFT TO SERVICE .
INTERMITTENT ENG #1 LP1 STATUS MESSAGE MTX REMOVED AND REPLACED M681 FIRE DET CARD PER AMM 26-10-01. OPS CK GOOD NO DEFECTS NOTED. ACFT REMAINS NO ETOPS. RETURNED TO SERVICE
DURING CREW PREFLIGHT, STATUS MSG LEFT ENG FIRE LP 2. MTC DEFERRED STATUS MSG L ENG FIRE LP 2 IAW MEL 26-11-1-1, MBCB 06/06/26, PLACARD INSTALLED, NO DEACTIVATION REQUIRED, A/C REMAINS NO ETOPS. A/C RETURNED TO SERVICE.
AFTER ENG STARTS AND TAXI OUT, NOTICED LEFT ENGINE EGT INOP. NOTE: EGT LEFT ENGINE 72C RH 369C. CREW RETURNED TO THE GATE (BTB). MTC REMOVED AND REPLACED THERMOCOUPLE JUNCTION BOX IAW 767 300 AMM 77-21-03 UP TO STEP 4 EGT INDICATING SYSTEM OPS TEST AND FOUND PROBE #8 DAMAGED. REMOVED AND REPLACED LH ENG #8 THERMOCOUPLE PROBE IAW B767 AMM 77-21-01. OPS TEST GOOD. EGT INDICATION NORMAL. ENG RUN PERFORMED BY J.C. IAW B767 AMM 71-00-00. A/C REMAINS NO ETOPS. A/C RETURNED TO SERVICE.
DURING PUSHBACK, FIRE/OVHT SYS EICAS MSG. CREW ACCOMPLISHED QRH 8.35. MSG CLEARED THEN REAPPEARED ON FINAL. MTC SWAPPED LT ENG LP2 FIRE DETECTION CARD (M682) AND R/H ENG LP2 FIRE DETECTION CARD (M684) IAW B767 AMM 26-10-01. OPS CHECK GOOD. A/C REMAINS NO ETOPS. A/C RETURNED TO SERVICE.
DURING INSP/MTC, L ENGINE FIRE LOOP 1 INOPERATIVE. DEFERRED L ENGINE FIRE LP 1 INOP IAW MEL 26-11-1-1. ALL MX PROCDURES CW PLACARD INSTALLED. MBCB 05/28/26 AC REMAINS NO ETOPS. A/C RETURNED TO SERVICE.
DURING APPROACH, CREW RECEIVED FIRE/OVHT STS EICAS MESSSAGE ON FINAL UNTIL ENGINE SHUTDOWN. MTC PERFORMED GVI OF LH ENG DUCTING -IAW B767 AMM 71-00-00 AND B767 FIM 26-11 FT 804. NO DAMAGE NOTED RAN LH ENG FOR 5 MIN WITH NO ABNORMAL INDICATIONS IAW B767 AMM 71-00-00. PERR MXC, SWAPPED CARDS M683 AND M681 IAW B767 AMM 26-10-01. OPS CHECK GOOD. AC REMAINS NO ETOPS. A/C RETURNED TO SERVICE.
DURING MAINTENANCE INSPECTION, L ENG FIRE LP 2 STATUS MSG. MAINTENANCE PERFORMED FIRE DET TEST IAS AMM 26-11-00. TESTED GOOD. MESSAGE CLEARED. AIRCRAFT RETURNED TO SERVICE.
CREW REPORTED L ENG FIRE LP 2 STATUS MSG. MAINTENANCE PERFORMED AFOLTS TEST IAW AMM 26-10-00. OPS CHECK PASSED MESSAGE CLEARED. PERFORMED ENGINE FIRE DETECTION OPS TEST IAW B767 AMM 26-11-00. OPS TEST PASSED A/C REMAINS "NO ETOPS". AIRCRAFT RETURNED TO SERVICE.
ON CPF L ENG FIRE LP1 STAUS MSG ON MTX PERFORMED A RESET OF LH FIRE LOOP 1 ON THE MTP-OPS NORMAL IAW AMM 26-11-0 AIRCRAFT NO ETOPS AND RETURNED AC TO SERVICE .
ON TAXI OUT, AFTER CROSS BLEED ENGINE START, HAD LEFT BLEED INOP AND LEFT PACK INOP INDICATIONS. AIRCRAFT RETURNED TO BLOCKS (BTB). PERFORMED OPS CHECK OF LT ENG BLEED AIR. OPS CK GOOD IAW B767 AM 36-11-00. AIRCRAFT REMAINS NO ETOPS. AIRCRAFT RETURNED TO SERVICE.
DURING TAXI OUT, APU SHUT ITSELF DOWN ATTEMPTED RESTART AND FAULTED AGAIN. AIRCRAFT RETURNED TO BLOCKS (BTB). DEFERRED IAW MEL 29-11-1A CAT I PLAC INSTALLED MAINT. PRECED. C/W. A/C REMAINS NON-ETOPS. REF LP 39222-59/1. AIRCRAFT RETURNED TO SERVICE.
DURING TAXI OUT, LE SLAT ASYM EICAS MESSAGE ILLUMINATED. A/C RETURNED TO BLOCKS (BTB). MEG CHECKED AND VERIFIED INDUCTANCE OF PROX SWITCH S305.. ADUSTED GAP TO TARGETS REF B767 AMM 27-22-01. SLAT FUNCTIONS AND INDICATIONS NORMAL, REF B767 AMM 27-22-01. AIRCRAFT RETURNED TO SERVICE.
FOUND LT ENG FIRE LOOP 1 ON EICAS DURING S/CÂ MTX GROUNDED A/C AND TROUBLSHOT PER W.D. 26-11-11 FOUND RESISTANCE FLUCTUATION DURING WIRE SHAKE INSPECTION ON TS681 WIRE W5334-00R-16, FOUND WIRE DAMAGED ABOUT 1/8 INCH FROM TERMINAL LUG. REPAIRED WIRE INSTALLING NEW TERMINAL LUG PER SWPM 20-30-11 SHAKE INSPECTION GOOD. OPS CK PER AMM 26-11-00 GOOD. A/C REMAIN NO ETOPS.MTX RETURNED A/C TO SERVICE
DURING MAINTENANCE CHECK PORTABLE ELT FAIL OPERATIONAL TEST CODE FAULTED 3+2 FLASHES INDICATING LOW RF POWER .MTX REPLACED KANNARD ELT. PERFORMED OPS CHECK PER TASK CARD ABX-ALR-25-013 OPS CHECK GOOD RETURNED A/C TO SERVICE
WHILE TAXING IN AT DFW, RIGHT SIDE INBOARD AFT BRAKE OVERHEAT, TEMP AT '7". WHEN BRAKE ROSE TO UNAFE LIMIT DISCONTINUED TAXI. REFERRED TO QRH AND CALLED OPS. CREW REQUESTED FIRE AND RESCUE TO MEET A/C. FIRE AND RESCUE VISUALLY INSPECTED THE BRAKE AND LANDING GEAR ASSY. BRAKE WAS INTACT, APPEARED NORMAL. MAINTENANCE FOUND #7 MLG WHEEL RUBBING #7 MLG BRAKE. REMOVED AND REPLACED #7 BRAKE PER KAC AMM 32-41-08. OPS NORMAL NO DRAGGING. HOT BRAKE INSPECTION COMPLIED WITH 05-51-14, ALL STEPS COMPLETE. AIRCRAFT RETURNED TO SERVICE.
EICAS FIRE / OVRHT SYS LIGHT ILLUMINATED WHILE TURNING FINAL UNTIL BOTH ENGINES SHUT DOWN.. MAINTENANCE PERFORMED FIRE / OVHT SYSTEM 6 TC CHECK IAW FIM 26-11 FT 804. NO FAULTS NOTED AT THIS TIME. A/C REMAINS NO ETOPS. PERFORMED GVI OF LOOPS ON NR 1 ENGINE AND PERFORMED MSG CHECK OF #1 ENG LOOPS. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
MAIN DECK CARGO DOOR WARNING ON DEPARTURE .ACFT RETURNED TO FIELD (ATB) AND MTX GROUNDED AC, MTX THEN DEFERRED MAIN DECK CARGO DOOR INDICATION IAW MEL ABX52-71-1-2. AND RETURNED AC TO SERVICE.
DURING C4 CHECK .IN OSCODA MICHIGAN (OSC), KALITTA MAINTENANCE FOUND CRACK WITH EDDY CURRENT INSPECTION AS MARKED ON INNER CHORED STA 903.5, LBL89. REPAIRED IAW ABX-EA-5300-0051 .REFERENCE W.O. 976402921 FOR CORRECTIVE ACTION.
DURING AIRCRAFT N764CK C4-CHECK IN OSCODA MICHIGAN (OSC), KALITTA MAINTENANCE DISCOVERED AFT CARGO FRAME WEB AT STA 1395 RBL 5 DAMAGED ,BLENDED AND FOUND TO BE OUT OF LIMITS . ACCOMPLISHED REPAIR AT STA 1395 RBL5 ON FRAME WEB IAW ABX-REA-5360-65922-00 & FVC INC. EO# 25166-4.
"DURING AIRCRAFT N764CK C4-CHECK IN OSCODA MICHIGAN (OSC), KALITTA MAINTENANCE DISCOVERED FUSELAGE SKIN CORROSION UNDER STRINGER S-38L AT STA 1395 WHILE PERFORMING A STRINGER SPLICE. THE CORROSION WAS BLENDED IAW B767-300 SRM AND FOUND TO BE OUT OF LIMITS AND NO APPLICABLE REPAIR WAS IDENTIFIED WITHIN THE SRM. FVCI WAS CONTACTED TO GENERATE A REPAIR EO (REF /A/) AND PROVIDE FAA FORM 8110-3 APPROVAL UPON COMPLETION. THE PURPOSE OF THIS REA IS TO AUTHORIZE AND DOCUMENT ACCOMPLISHMENT OF REF /A/. FUSELAGE SKIN BETWEEN STA 132.5-1843 IS CONSIDERED FCBS STRUCTURE PER B767-300 SRM 51-00-04 TABLE 1. THIS REPAIR IS CONSIDERED MAJOR AND WILL REQUIRE FAA FORM 8110-3 APPROVAL. REPAIRED IAW ABX-REA-5360-65895-00_0001 AND FVCI EO 25166-2A"
DURING AIRCRAFT N764CK C4-CHECK IN OSCODA MICHIGAN (OSC), KALITTA MAINTENANCE DISCOVERED ,EVIDENCE OF CORROSION FOUND ON STRINGER 32 AT STA. 697 AND REPAIRED STRINGER 32R AT REPAIR STA 682 TO REPAIR STA 713 IAW B767-300 SRM 53-00-02 REPAIR 2..
DURING AIRCRAFT N764CK C4-CHECK IN OSCODA MICHIGAN (OSC), KALITTA MAINTENANCE DISCOVERED CORROSION DAMAGE AT APPROXIMATELY STA 555 AND STA 610 ON THE OUTER CHORD OF THE FORWARD LOWER CARGO DOOR LOWER SILL. THE CORROSION WAS BLENDED IAW B767-300 SRM AND FOUND TO BE OUT OF LIMITS. FVCI WAS CONTACTED TO GENERATE A REPAIR EO (REF /A/) AND PROVIDE FAA FORM 8110-3 APPROVAL UPON COMPLETION. THE PURPOSE OF THIS REA IS TO AUTHORIZE AND DOCUMENT ACCOMPLISHMENT OF REF /A/. REPAIRED IAW ABX-REA-5330-65886-00 AND FVCI EO 25166-1A.
WHILE 764CK WAS UNDERGOING C 4 -CHECK IN OSC, CORROSION WAS FOUND ON THE INNER SURFACE OF THE INNER SKIN AT STA 1177 ALONG THE S-36L LAP JOINT. SEE FIGURE 1. THE CORROSION WAS REMOVED BY BLENDING AND THE BLEND WAS BEYOND THE ALLOWABLE LIMIT GIVEN IN B767 SRM 53-00-01, AD1, FIG 101. SINCE THIS DAMAGE IS UNDER THE WING-TO-BODY FAIRING, THERE IS NO REPAIR GIVEN FOR IT IN THE SRM. FLIGHT VEHICLES CONSULTING, INC. WAS CONTACTED FOR AN FAA-DER APPROVED REPAIR. THE PURPOSE OF THIS REA IS TO AUTHORIZE AND DOCUMENT ACCOMPLISHMENT OF FVCI EO 25166-3, WHICH IS AN FAA-DER APPROVED REPAIR.COMPLIED WITH ABX-REA-5365-65899-00 AND FVCI EO 25166-3.
DURING C 4 IN OSCODA MICHIGAN (OSC), KALITTA MAINTENANCE FOUND EVIDENCE OF CORROSION ON UPPER CHORD IN AFT CARGO COMPARTMENT AT BS 1373 RBL 8 JM-44..FOUND TO BE OUT OF LIMITS. ACCOMPLISHED REPAIR OF UPPER CHORD AT BS 1373 RBL8 IAW B767-300 SRM 53-00-07 REPAIR 4..
DURING C 4 CHECK IN OSCODA MICHIGAN (OSC), KALITTA MAINTENANCE FOUND CRACK INDICATION FOUND DURING HFEC INSPECTION OF R1 LOWER DOOR CUTOUT. INDICATION IS LOCATED ON R1 DOOR CUTOUT ON AFT LOWER CORNER AS MARKED FOUND TO BE OUT OF LIMITS . ACCOMPLISHED REPAIR ON R1 DOOR LOWER AFT CORNER AS REQUIRED IAW B767-300 SRM 53-10-01 REPAIR 1.
DURING C 4 CHECK IN OSCODA MICHIGAN (OSC), KALITTA MAINTENANCE FOUND AFT CARGO COMPARTMENT HAS EVIDENCE OF CORROSION BETWEEN STATION 1351-1395 AT STRINGER L39. GB6.FOUND TO BE OUT OF LIMITS.ACCOMPLISHED REPAIR ON AFT CARGO STR39L AT REPAIR STA 1354 TO REPAIR STA 1405 IAW B767-300 SRM 53-00-03 REPAIR 2.
DURING C 4 CHECK IN OSCODA MICHIGAN (OSC), KALITTA MAINTENANCE FOUND AFT LWR CARGO COMPARTMENT HAS EVIDENCE OF CORROSION AT STRINGER 39R AT STA 1307. GB5.FOUND TO BE OUT OF LIMITS REMOVED AND REPLACED AFT LWR CARGO STR39R AT FACTORY SPLICE STA 1219 TO FACTORY SPLICE STA 1307 IAW B767-300 SRM 51-40-02.
DURING C 4 CHECK IN OSCODA MICHIGAN (OSC), KALITTA MAINTENANCE FOUND R/H HORZ STAB LOWER SKIN HAS AREA OF DELAMINATION AT AUX SPAR STA 243 JM-30.FOUND TO BE OUT OF LIMITS REMOVED AND REPLACED LOWER SKIN PANEL IAW B767-300 SRM 51-40-02.
DURING C 4 CKECK IN OSCODA MICHIGAN (OSC), KALITTA MAINTENANCE FOUND FWD CARGO AT APPROX STA 654+44 ON INNER CHORD NUT PLATE HAS EVIDENCE OF CORROSION TB56 FOUND TO BE OUT OF LIMITS AND ACCOMPLISHED REPAIR AT STA 654+44 ON INNER CHORD IAW B767-300 SRM 53-00-07 REPAIR 4.
DURING AIRCRAFT N764CK C4-CHECK IN OSCODA MICHIGAN (OSC), KALITTA MAINTENANCE DISCOVERED CORROSION DAMAGE AT APPROXIMATELY STA 555 AND STA 610 ON THE OUTER CHORD OF THE FORWARD LOWER CARGO DOOR LOWER SILL. THE CORROSION WAS BLENDED IAW B767-300 SRM AND FOUND TO BE OUT OF LIMITS. FVCI WAS CONTACTED TO GENERATE A REPAIR EO (REF /A/) AND PROVIDE FAA FORM 8110-3 APPROVAL UPON COMPLETION. REPAIRED IAW ABX-REA-5330-65886-00 (REPAIR-FORWARD LOWER CARGO DOOR, LOWER SILL, OUTER CHORD, STA 555 & STA 610,AND FVCI EO 25166-1A
DURING 4C IN OSCODA MICHIGAN (OSC), KALITTA MAINTENANCE FOUND FWD CARGO COMPARTMENT R/H AT APPROX STA 610-544 RBL 36.70 WEB IN FRONT OF DOOR CORRODED TB76. FOUND TO BE OUT OF LIMITS . REMOVED AND REPLACED WEB FROM STA 610 - 544 RBL 36.70 IAW B767-300 SRM 51-40-02..
DURING C-4 CHECK IN OSCALA, MI., MAINTENANCE FOUND AFT LOWER CARGO SMOKE DETECTOR ZONE FIALED LEAK CHECK. REMOVED AND REPLACED TUBE ASSY, TEE HOSE, AND SILICON HOSE IAW BOEING PROPRIETARY BAC5014 REV (L) 10JUNE2024 STEP 8.3.3. LEAK CHECK GOOD IAW IAI B767-300 SMM 26-14-00. TUBE, SMOKE SAMPLING SILICONE PN: 368-26-10-91273-211 SN: UNK TUBE ASSY, CARGO SMOKE DET HEATER PN: 371-26-00-C1347-101 SN: UNK.
STATUS MSG: L ENG FIRE LP 2. MAINTENANCE DEFERRED IAW MEL C ABX-26-11-1-1. REFERENCE B767 WDM 26-11-11. FOUND WIRE W53/6-002 R-16 SHORTED TO PNEUMATIC DUCT. TEMPORARILY WRAPPED WITH TAPE. BD SPOT ON I/B SIDE UNDER THRUST REVERSER. DI AND PLACARD REMAIN. AIRCRAFT REMAINS NO ETOPS AND RETURNED TO SERVICE.
AIR TURN BACK DUE TO RH HYD QTY LOSS DUE TO RH EDP AND CASE DRAIN FILTER MODULE FILTER BOWL BROKEN - LEAK CODE: 440-5-C AFTER LANDING MTX GROUNDED A/C AND INSPECTED , FOUND RH EDP PRESSURE CASE DRAIN FILTER MODULE BLEW OFF PRESSURE FILTER BOWL. NO DPIS POPPED. REMOVED AND REPLACED RH EDP MODULE ASSY PER KAC AMM 29-11-17. REPLACED 12 GAL HYDRO FLUID PER KAC AMM 12-12-01. NO LEAKS NOTED. OPS CHECKS NORMAL MTX RETURNED A/C TO SERVICE ..
DURING TAXI OUT STAB TRIM INDICATION DIFFERENCE OF 1 DEG. BEFORE TAKEOFF CHECKLIST, A/C RETURNED TO THE GATE (BTB) AND MTX GROUNDED A/C.MTX THEN DEFERRED RH STAB INDICATOR IAW MEL ABX-27-48-1 . AND RETURNED THE A/C TO SERVICE.
RIGHT FWD WINDOW ARCHED AND CRACKED IN FLIGHT AT FL 340 CREW DECLARED EMERGENCY AND DEVERTED TO TULSA AND LANDED . MTX GROUNDED AC AND MTX REPLACED R1 WINDOW ASSEMBLY IAW B 767 AMM 56-11-01 WINDOW HEAT OPS CHECK GOOD . AND MTX RETURNED AC TO SERVICE.
TMSP IS INOP (N1 DISPLAY BOTH ENGINES). PERFORMED AUTO FL AND TMC C/B'S RESET AND MCDP GND 05 IAW 22-03-00/201. THE SYSTEM OK. TMSP WORKS NORMAL. DEFERRED. RALM STATUS DOWNGRADED TO CAT I PENDING 30/40 TEST.
AFTER ENGINE START RT ENG BLEED WILL NOT TURN ON AC RETURNED TO GATE AND MAINTENANCE GROUNDED AC. AND DEFERRED RH ENGINE BLEED FOR DEPARTURE IAW MEL ABX-36-11-1-2A-1. RETURNED AC TO SERVICE AND AC DEPARTED .RE ACT PRSOV AND FAN AIR VALVE SWAPPED LEFT AND RIGHT AIR SUPPLY CONTROL CARDS RAN ENG NO HELP REINSTALLED ORIG POSITION MANUALLY CYCLED PRSOV SMOOTH PERFORMED HPSOV THUMB TEST PER AMM 36-00-21 TEST GOOD HPSOV RETURNED TO NORMAL C/W MPM 36-11-1-2A-1 AND 36-12-2 .THEN REMOVED AND REPLACED R ENG PRSOV PER AMM 36-11-09, C/W RE-ACTIVATION PROCEDURES PER MEL MPM 36-11-1-2A-1 & 36-12-2 OP'S CHECK OK, DUCT PRESSURE NORMAL. THIS ACTION CLEARS DI 50024, A/C REMAINS NO ETOPS, PLACARD REMOVED.
AFTER TAKEOFF ; FLAP HANDLE UP,FLAP INDICATION BETWEEN UP AND 1 ;LE SLAT ASYM CAUTION ON EICAS .AC RETURENED TO FIELD AND MAINTENANCE GROUNDED AC. MAINTENANCE VERIFIED RESISTANCE AND INDUCTANCE OF ALL LEADING EDGE SENSORS.VISUALLY INSPECTED ALL SENSORS ,FOUND"S280" #5 SLAT OUTBOARD SENSOR TARGET OUT OF TOLERANCE. PSEU SHOWED "S280" BITE FAULT. ADJUSTED TARGET, REF.B767 AMM 27-88-01 ALL OPS NORMAL. AC RETURNED TO SERVICE
DURING CLIMB LE SLAT ASYM EICAS MSG APPEARED AC RETURNED TO FIELD AND MAINTENANCE GROUNDED AC .AND FLIGHT WAS SWAPPED MAINTENANCE CONTINUED TO WORK . REMOVED AND REPLACED C FSPM PER AMM 27-58-01 OPS CHECK NORMAL. ALSO PERFORMED -63 FSEU READOUT OF SENSORS/RVDT'S REF AMM 27-51-26 FLAPS AND SLATS OPERATE NORMALLY NO DEFECTS PER AMM 27-51-00 AC RETURNED TO SERVICE.
DURING TAXI FWD CABIN TEMP EICAS MSG FWD CABIN LIGHT INOP ILUMINATED AC RETURNED TO GATE AND GROUNDED BY MAINTENANCE. MAINTENANCE DEFERRED FWD CABIN TEMP IAW MEL ABX-21-61-1-2.RETURNED TO SERVICE AND AC DEPARTED .
GEAR DISAGREE TAILSKID AND MASTER CAUTION ILLUNINATED ON TURN TO FINAL. RAN QRH 14.17 WHICH CLEARED GEAR DISAGREE AND TAILSKID GEAR DOORS ILLUMINATED. CREW DECLARED AN EMERGENCY. AIRCRAFT LANDED WITH OUT FURTHER INCIDENT. AIRCRAFT WAS GRPONDED BY MAINTENANCE. MAINTENANCE DEFERREDNTHE LANDING GEAR RETRACT SYSTEM IAW MEL 32-30-1. MAINTENANCE PROCEDURES COMPLIED WITH. PLACARD INSTALLED. AIRCRAFT WAS RELOCATED TO CVG FOR FURTHER MAINTENANCE. MLG GEAR CONTROL LEVER MODULE REPLACEMENT PERFORMED MULTIPLE GEAR SWINGS PER B767 AMM 32-34-00 AND 32-32-00. COMPLETED RII FORMS 32-01-1 AND 32-02-1. THIS CLEARS DI 43898. MEL MTC PROCEDURES C/W DI AND PLACARD REMOVED. AIRCRAFT RETURNED TO SERVICE.
TAKE OFF CONFIG WARNING FOR FLAPS & PARKING BRAKE CAME ON DURING BOTH ENGINE STARTS. LEFT AND RIGHT EEC MESSAGE DISPLAYED. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE DEFERRED LEFT AND RIGHT EEC'S PER MEL 73-21-1-1A. AIRCRAFT RETURNED TO SERVICE.
L ISLN VALVE SWITCH STUCK IN OPEN POSITION. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE DEFERRED THE LEFT ISOLATION VALVE SWITCH IAW MWL 36-11-6. MAINTENANCE PROCEDURES COMPLIED WITH AND PLACARD INSTALLED. AIRCRAFT RETURNED TO SERVICE.
EMERGENCY DOORS LIGHT INTERMITTENT IN FLIGHT NO ENGINE INDICATING AND CREW ALERTING SYSTEM. CHECKED IAW SUPPLEMENTAL MAINTENANCE MANUAL 52-09-03, IAW SUPPLEMENTAL MAINTENANCE MANUAL 52-71-00, AMM 05-41-08 AND AMM 33-16-00. NO DEFECTS NOTED.
FORWARD EQUIPMENT OVERHEAT EICAS IN CRUISE. RAN QUICK REFERENCE HANDBOOK. PLACED EQUIPMENT COOLING TO STANDBY. MESSAGE REAPPEARED. THEN PLACED SELECTOR TO OVERRIDE. MESSAGE REAPPEARED IN DECENT. CABIN ALTITUDE WARNING IN CRUISE POSSIBLY DUE TO EQUIPMENT OVERHEAT ISSUE. RAN MEMORY LINES AND QUICK REFERENCE HANDBOOK. DECLARED EMERGENCY. FORWARD EQUIPMENT COOLING IN DECENT. MESSAGE DISAPPEARED BY 10,000 FEET. TROUBLESHOT IAW B767-300 FAULT ISOLATION MANUAL 21-58 FAULT TREE 901 AND FAULT ISOLATION MANUAL 910. NO DEFECTS FOUND. FOUND DUCT DISCONNECTED BETWEEN PACK OUTLET DUCT, MIX MANIFOLD AND CONDITIONED AIR GROUND CONNECTION. REFERENCE WORKORDER 76425312 FOR DUCT ASSEMBLY REPLACEMENT. REMOVED CONDITIONED AIR GROUND CONNECTION TO FACILITATE OTHER MAINTENANCE. REPLACED CONDITIONED AIR GROUND CONNECTION DUCT FLAPPER NOT SEALING IAW B767 AMM 21-21-02. ALL CHECKED GOOD
L/H MLG SUPPORT BEAM AFT TRUNION BEARING DAMAGED (NOTE: SUPPORT BEAM FOUND TO BE CORRODED IN BEARING BORE)
LHMLG FWD TRUNION REAR SPAR IB ATTACH FITTING FOR TRUNION HOUSING LOWER BUSHING HAS EVIDENCE OF CORROSION
LHMLG FWD TRUNION REAR SPAR IB ATTACH FITTING FOR TRUNION HOUSING UPPER BUSHING HAS EVIDENCE OF CORROSION
EVIDENCE OF CORROSION ON FRAME INNER CHORD AT STA 1241 LBL 44
FIRST OFFICER'S FWD INBD SEAT TRACK HAS EVIDENCE OF CORROSION
FIRST OFFICER'S AFT O/B SEAT TRACK HAS EVIDENCE OF CORROSION.
INBOARD FORWARD FLAP MISSING TWO RIVETS ON LOWER SURFACE APPROXIMATELY 15 INCHES INBOARD OF THE #3 FLAP TRACK (NOTE: FURTHER INVESTIGATION REVEALED CORROSION PER SIGN OFF)
EVIDENCE OF CORROSION ON FRAME INNER CHORD AT STA 1219 LBL 44
INNER CHORD @ STA 1131 SHOWS EVIDENCE OF CORROSION
INNER CHORD @ STA 1153 SHOWS EVIDENCE OF CORROSION.
EVIDENCE OF CORROSION ON FRAME INNER CHORD AT STA 1197 + 88 LBL 44
EVIDENCE OF CORROSION ON FRAME UPPER CHORD AT STA 1197 RBL 20
CAPTAIN'S FWD O/B SEAT TRACK HAS EVIDENCE OF CORROSION
CAPTAIN'S FWD I/B SEAT TRACK IS CRACKED
CAPTAIN'S AFT I/B SEAT TRACK IS CRACKED
CORR. ON CARGO COMPARTMENT STRUCTURE WEB AT STA 612, APPROX LBL 15
R/H #2 DEACTIVATED SERVICE DOOR LWR AFT CORNER (FRAME WEB) AROUND RETAINING PIN HOLE HAS EVIDENCE OF CORROSION
L/H #2 DEACTIVATED SERVICE DOOR AFT CORNER (FRAME WEB) AROUND RETAINING PIN HOLE HAS EVIDENCE OF CORROSION
MAIN CARGO DOOR LIGHT ILLUMINATED DURING CRUISE. ADJUSTED THE CARGO DOOR LOCK SWITCH IAW SMM 52-71-09. ALL CHECKED GOOD.
WING T/E FLAP SUPPORT MECHANISM, 1, 2, & 3 BEAMS. NR 1 POSITION. HAD ONE FASTENER HOLE WITH A CRACK INDICATION.
CORROSION ON LOWER SURFACE OF RT INBD MAIN FLAP JUST AFT OF OUTBOARD HINGE ASSY
AFT PIT FORWARD BULKHEAD HORIZONTAL STIFFENER HAS EVIDENCE OF CORROSION STA 1065 WL 167 LBL 61.
AFT PIT BETWEEN STA 1285 & STA 1263 TORQUE BOX COVER HAS EVIDENCE OF CORROSION BETWEEN S 35L & S 34L
AFT PIT BULK CARGO DOOR APPROX STA 1432 STR 29L HAS AREA OF CORROSION ON INNER CHORD.
AFT PIT FWD BULKHEAD WEB HAS EVIDENCE OF CORROSION STA 1065 WL 170 LBL 24.
AFT CARGO COMPARTMENT RT TORQUE BOX ACCESS PANEL AT BS 1263 TO 1285 HAS EVIDENCE OF CORROSION.
TORQUE BOX HAS CORROSION IN FWD PIT AT STA 544 - 566 LBL 55.
STRINGER CLIP CORRODED AT STA 742 STR 35R.
AFT PIT SHEAR TIE BETWEEN S 39R & S 38R AT STA 1263 HAS EVIDENCE OF CORROSION.
AFT PIT AT STA 1263 BETWEEN S 36L & S 35L SHEAR TIE HAS EVIDENCE OF CORROSION.
AFT PIT SHEAR TIE BETWEEN S 38L & S 37L AT STA 1263 HAS EVIDENCE OF CORROSION.
AFT PIT SHEAR TIE BETWEEN S 39L & S 39R AT STA 1263 HAS EVIDENCE OF CORROSION.
AFT PIT SHEAR TIE BETWEEN S 37L & S 36L AT STA 1263 HAS EVIDENCE OF CORROSION.
HORIZ STAB RT SIDE UPPER SURFACE STA 107 S-11 HAS AREA OF CORROSION.
CORROSION IN I/B FLAP MOUNTING HOLES ON AFT END OF NR 3 FLAP SUPPORT BEAM.
CORROSION IN I/B FLAP MOUNTING HOLES ON AFT END OF RT NR 3 FLAP SUPPORT BEAM.
EVIDENCE OF CORROSION ON AFT PIT TORQUE BOX WEB STA 1329-1351 APPROX RBL 40.
EVIDENCE OF CORROSION ON AFT PIT TORQUE BOX INTERCOSTAL STA 1329-1351 APPROX RBL 20.
EVIDENCE OF CORROSION ON AFT PIT WEB AT STA 1280 RBL 20.
SHEAR TIE BETWEEN S 39R & S 39L AT STA 1329 HAS EVIDENCE OF CORROSION.
SHEAR TIE BETWEEN S 39L & S 38L AT STA 1329 HAS EVIDENCE OF CORROSION.
SHEAR TIE BETWEEN S 38L & S 37L AT STA 1329 HAS EVIDENCE OF CORROSION.
SHEAR TIE BETWEEN S 37L & S 36L AT STA 1329 HAS EVIDENCE OF CORROSION.
EVIDENCE OF CORROSION ON UPPER TORQUE BOX PANEL STA 1263 - 1285 LBL 6 - 33.
AFT PIT DOOR SURROUND MAIN SILL WEB AT APPROX STA 1285 HAS CORROSION.
BULK CARGO DOOR CUTOUT LOWER SILL UPPER SURFACE HAS EVIDENCE OF CORROSION.
EVIDENCE OF CORROSION ON STRINGER 3 LOWER, INSIDE OF HORIZONTAL STAB CENTER BOX.
AFT PIT FLOORBEAM STATION 1197 +22 RBL APPROX 40 HAS CORROSION AROUND NUT PLATE.
BULKHEAD FITTING ON FORWARD AFT PIT BULKHEAD FOR APU BLEED AIR DUCT HAS CORROSION ON FITTING, BULKHEAD, AND HORIZONTAL STIFFENER.
AFT PIT FLOORBEAM STATION 1197 +88 RBL APPROX 40 HAS CORROSION AROUND NUT PLATE.
AFT PIT FLOORBEAM STATION 1197 +44 RBL APPROX 40 HAS CORROSION AROUND NUT PLATE.
AFT PIT FLOORBEAM STATION 1197 +66 RBL APPROX 32-37 HAS AREAS OF CORROSION AROUND NUT PLATES.
AFT PIT FLOORBEAM STATION 1197 +44 RBL APPROX 22 HAS CORROSION AROUND NUT PLATE.
AFT PIT FLOORBEAM STATION 1197 +66 LBL APPROX 28-40 HAS CORROSION AROUND NUT PLATE.
AFT PIT BULK CARGO DOOR APPROX STA 1448 STR 29L HAS AREA OFF CORR ON INNER CHORD.
AFT PIT FORWARD BULKHEAD HORIZONTAL STIFFENER HAS EVIDENCE OF CORROSION LBL 13 WL 177.
AFT PIT FORWARD BULKHEAD HORIZONTAL STIFFENER HAS EVIDENCE OF CORROSION LBL 26-47 WL 184.
AFT PIT FORWARD BULKHEAD HORIZONTAL STIFFENER HAS EVIDENCE OF CORROSION LBL 40 WL 177.
AFT PIT FORWARD BULKHEAD HORIZONTAL STIFFENER HAS EVIDENCE OF CORROSION LBL 53 WL 177.
AFT PIT FORWARD BULKHEAD HORIZONTAL STIFFENER HAS EVIDENCE OF CORROSION LBL 27-53 WL 150.
AFT PIT FORWARD BULKHEAD WEB HAS EVIDENCE OF CORROSION LBL 50 WL 153.
TORQUE BOX ACCESS PANEL AT STA 1329 - 1351 HAS EVIDENCE OF CORROSION ON CORNER.
TORQUE BOX ACCESS PANEL AT STA 1153 THRU 1175 HAS EVIDENCE OF CORROSION @ STA 1153 LBL 7.
AFT PIT APPROX STA 1343 RBL 7 UPPER TORQUE BOX WEB HAS PREVIOUS TEMP REPAIR WITH BLIND FASTENERS. (NOTE: OUT OF LIMITS CORROSION FOUND AT STA 1339 RBL 13 DURING ACCESS FOR REPAIR)
FWD CARGO AT STA 742 SHEAR TIE AT S 36R HAS EVIDENCE OF CORROSION.
FWD CARGO AT STA 742 SHEAR TIE AT S 35R HAS EVIDENCE OF CORROSION.
FWD CARGO AT STA 742 SHEAR TIE AT S 34R HAS EVIDENCE OF CORROSION.
LT I/B AFT FLAP HAS A DELAM ON THE T/E WEDGE ON I/B END 18" O/B FROM I/B END.
RIGHT PYLON INBD SIDE, AFT UPPER AREA OF OPENING FOR ACCESS PANEL 442AL. PYLON SKIN CRACKED.
FWD CARGO AT STA 742 SHEAR TIE AT S 37R HAS EVIDENCE OF CORROSION.
FUSELAGE SKIN AT BS 1554 BETWEEN STRINGERS 24L & 25L AT VACUUM OUTFLOW NOZZLE THE SKIN IS CORRODED.
FUSELAGE SKIN AT BS 1574 BETWEEN STRINGERS 24L & 25L AT VACUUM OUTFLOW NOZZLE THE SKIN IS CORRODED.