N219CY

Part: BEARING — CORRODED (AILERON) · airframe 97,893 hrs · 25,923 cycles

ON TAXI OUT, CONTROL CHECK ON AILERON DID NOT PASS CHECK. CAME BACK TO GATE FOR HELP WITH MAINTENANCE. (BTB). FOUND AILERON CENTERING MECHANISM CENTERING CAM FOLLOWER BEARING CORRODED. REMOVED AND REPLACED BEARING IAW B767 AMM 20-11-00. FURTHER T/S REQUIRED. FOUND AILERON FEEL, CENTERING, AND TRIM MECHANISM IN SPRING OUT OF TENSION LIMIT LOW. CORRECTED IAW CMM 27-11-23. FOUND AILERON AFT POWER BUS CABLES OUT OF TENSION LIMITS AND ADJUSTMENT. ADJUSTED IAW AMM 27-11-00 AND RII FORM 27-03. OPS TEST GOOD PER AMM 27-11-00. AIRCRAFT RETURNED TO SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (SLAT SYS) · airframe 97,891 hrs · 25,922 cycles

LE SLAT DISAGREE CAUTION MESSAGE ON SHORT FINAL , AFTER LANDING MTX .PERFOMED L.E.S OPERATIONAL CHECK WITH HYDS. AND ELECTRCAL POWER IAW AMM 27-81-00. ALL FOUND NORMAL AT THIS TIME. MTX RETURNED AC TO SERVICE

Part: PITOT HEAD — DEFECTIVE (ZONE 200) · airframe 97,869 hrs · 25,912 cycles

AFTER ENGINE START, "CAPT PITOT" EICAS MGS AND "CAPT PITOT" OVERHEAD LIGHT ILLUMINATED. AIRCRAFT RETURNED TO BLOCKS (BTB). MAINTENANCE REMOVED AND REPLACED THE UPPER LEFT PITOT PROBE REF B767 AMM 34-11-01. LEAK AND OPS CHECK NORMAL. PROBE HEAT REF B767 AMM 30-31-00. AIRCRAFT REMAINS RYSM COMPLIANT. AIRCRAFT RETURNED TO SERVICE.

Part: WARNING MESSAGE — ILLUMINATED (AILERON SYS) · airframe 97,624 hrs · 25,809 cycles

AILERON LOCKOUT EICAS WHEN SLOWED TO 250 KTS. AFTER AC LANED MTX GROUNDD ACFT AND TOUBLESHOT IAW FIM 27-11 FT 804, FOUND FAULT BULB ON LT SAM. SWAPPED SAM P/N 285T001S-117 / S/N. 000276 WITH SAM S/N D01364 / P/N 285ST001S-116. NO HELP. ORIGINAL SAM REINSTALLED. CHKD LT LOCKOUT AILERON IAW AMM 27-11-44. NO DEFECTS NOTED. FURTHER T/S REQUIRED. TRANSFER TO DI 67284 IAW MEL 27-11-2. (M) PROCEDURE COMPLIED WITH PLACARD INSTALLED. CAT C MBCB 11.02.25. MTX REURED AC TO SERVICE.

Part: ANTI-SKID SYS — FAULTED (ZONE 700) · airframe 97,286 hrs · 25,677 cycles

ON FINAL FOR 10L INTO KORD, GEAR DISAGREE AND TAILSKID EICAS RAN CHECKLIST AFTER GO AROUND. ABORTED APPROACH. (AAP) CAME BACK AFTER CALLING MX CONTROL AND RUNNING QRH. IN ORD, CONFIRMED TAIL SKID DID NOT DEPLOY. ABOUT 10 MINUTES AFTER BLOCK IN THE TAIL SKID DROPPED ON ITS OWN. LANDING GEAR LEVER CONTROL MODULE WAS CLEANED AND LUBED PER B767 AMM 32-31-01, OPS CHECK GOOD. FIM TASK 32-71 F/T 803 C/O. SYSTEM FUNCTION WAS NORMAL. NO FAULTS FOUND. AIRCRAFT RETURNED TO SERVICE.

Part: TRANSPONDER — INOPERATIVE (ZONE 100) · airframe 97,268 hrs · 25,656 cycles

ON TAXI OUT, ATC TRANSPONDER INOP. AIRCRAFT RETURNED TO BLOCKS. (BTB). MAINTENANCE PERFORMED OPS TEST OF TRANSPONDER IAW AMM 34-53-03. OPS TEST GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SPRING — OUT OF TOLERANCE (ZONE 800) · airframe 97,267 hrs · 25,665 cycles

LT FWD ENTRY DOOR OPENED ON LANDING WITH EICAS MESSAGE. UPON LANDING OBSERVED PSEU PROX SENSOR S195 TARGET WAS FLAGGED RESET TARGET FOUND GAP BETWEEN LOCK PIN AND PROX SENSOR S195 AT .059 IN. REMOVED DOORWAY LINING AND FOUND SPRING HYD SNUBBER OUT OF TOLERANCE AT +.25 IN. ADJUSTED SPRING HYD SNUBBER IAW B767 AMM 52-12-31. REINSTALLED DOOR LINING. PROC TARGET CAP AT S195 WITHIN TOLERANCE PRESSURIZED. OPS CK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: WINDOW — DEFECTIVE (ZONE 200) · airframe 96,493 hrs · 13,391 cycles

ON DESCENT PASSING FL320 WE NOTICED A FAINT ELECTRICAL SMOKE SMELL ON PILOT SIDE IN FRONT INSTRUMENTS. REMOVED AND REPLACED LH 41 WINDOW IAW AMM 56-11-01. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 97,222 hrs · 25,618 cycles

ELECT ODOR DURING CLIMB. AIR TURNBACK. DECLARED EMERG & DONNED O2 MASK. PERF AFOLTS TEST PER AMM 26-10-00. PERF ENG FIRE DETECT TEST PER AMM 26-11-00. PERF MAIN CARGO SMOKE DETECT TEST PER AMM 26-14-00. PERF LWR CARGO SMOKE DETECT TEST PER AMM 26-16-00. PERF APU FIRE DETECT TEST PER AMM 26-15-00. PERF SMOKE OR FUMES IN CABIN INSP PER AMM 05-51-56 & AMM 21-00-21. PERF LT & RT ENGINE IDLE RUNS IAW AMM 71-00-00. OPS PACKS, HYDS, FUEL PUMPS, ALL COCKPIT LIGHTS, CARGO HEAT. PERF DVI &THERMAL CHKS OF C/B PANELS, E&E SHELVES, E8 RACKS, LT & RT ENG CABLES, APU CABLES, COCKPIT OVERHEAD & INST PANELS, MAIN CARGO, FWD CARGO, AFT CARGO PER AMM 20-10-75 NO SMOKE, FUMES, CONTAMS, OR HOTSPOTS DETECTED. ACFT RTS.

Part: CONTROLLER — DEFECTIVE (ZONE 100) · airframe 96,894 hrs · 25,481 cycles

DURING TAXI AFT CABIN TEMP FWD CABINE TEMP FLT DECK TEMP EICAS MESSAGE APPEARED, AC RETURNED TO GATE (BTB), MTX GROUNDED AC. T/S SYSTEM, FOUND CABIN ZONE TEMP CONTROLLER FAULTED. REMOVED AND REPLACED CABIN ZONE TEMP CONTROLLER IAW B767 AMM 21-61-03. SYSTEM OPS CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. AIRCRAFT REMAINS NON-ETOPS.

Part: GENERATOR — FAULTED (LEFT) · airframe 96,780 hrs · 25,417 cycles

ON TAKEOFF ROLL LT UTILITY BUS, RT UTILITY BUS, AND LT GEN ILLUMINATED. ABORTED TAKEOFF AT 30-40KTS, BRAKE ENERGY WAS A MAX OF 3. A/C RETURNED TO BLOCKS (BTB).  DEFERRED LT GENERATOR IAW MEL ABX-24-00-1-2. A/C REMAINS NO ETOPS. A/C RETURNED TO SERVICE.

Part: OIL SYSTEM — WARNING MESSAGE (RT ENGINE) · airframe 96,749 hrs · 25,402 cycles

DURING TAXI WHILE STARTING RH ENGINE ,OIL DROPPED TO 11QTS AFTER START, A/C RETURNED TO GATE (BTB) AND MTX GROUNDED A/C .CONFIRMED OIL LEVEL AND MTX DEFERRED RH OIL QTY INDICATION IAW MEL ABX-79-31-1-1 PLACARD INSTALLED AND RETURNED A/C TO SERVICE .AC REMAINS ETOPS 180.

Part: TRANSPONDER — FAULTED · airframe 96,560 hrs · 25,319 cycles

DURING TAXIOUT  ATC NOT RECEIVING TRANSPONDER. AC RETURNED TO GATE (BTB) RESET CONTROL HEAD AND PERFORMED OPS CHECK OF BOTH SYSTEMS IAW B767 AMM 34-45-00 OPS CHECK GOOD. MTX RETURNED AC TO SERVICE

Part: ANTENNA — FAULTED (WX RADAR) · airframe 96,413 hrs · 25,264 cycles

BOTH LEFT AND RIGHT RADAR SYSTEMS FAILED IN FLIGHT TESTED OK ON GROUND PRIOR TO DEPARTURE FLIGHT WAS TO BOGATA WITH KNOWN HEAVY THUNDERSTORMS ENROUTE, RETURNED TO KMIA (ATB) AND LANDED MTX GROUNDED AC AND BEGAN TROUBLESHOOTING .MTX REMOVED WEATHER RADAR ANTENNA IN REF WITH B767 AMM 34-43-05 AF. REPLACED WEATHER RADAR ANTENNA, INSTALLATION IAW AMM 34-43-05/401. INSTALLATION TEST GOOD. OPS CHECK NORMAL IAW AMM 21-51-00/501. AIRCRAFTS REAMINS ETOPS 180 RETUNRED TO SERVICE

Part: START VALVE — MALFUNCTIONED (ZONE 500) · airframe 95,980 hrs · 25,063 cycles

DURING TAXI WHILE STARTING LH ENGINE LEFT ENG DID NOT START, STARTVALVE LIGHT ILLUMINATED ,AC RETURNED TO GATE , MTX GROUNDED AC AND DEFERRED THE START VALVE IAW MEL-ABX-80-00-2-1 , RETURNED AC TO SERVICE AND MANUALLY STARTED ENGINE ,AC DEPARTED . REMOVED AND REPLACED LEFT ENG STARTER CONTROL VALVE IAW B767 AMM 80-11-02. OPS CHECK GOOD. THIS CLEARS DI NUMBER 54790. PLACARDS REMOVED. NO MX PROCEDURES REQUIRED. A/C REMAINS ETOPS 180. PLACARD ROTATED. REF LP 38946-63/1

Part: CONTROL PANEL — MALFUNCTIONED (ZONE 200) · airframe 95,702 hrs · 24,945 cycles

DURING TAXI OUT LEFT AND RIGHT TRANSPONDER INOP . A/C RETURNED TO GATE AND MTX GROUNDED A/C .MTX PERF L AND R ATC TXPNR BITE CHECKS PER AMM 34-53-01, NO DEFECTS NOTED. REMOVED AND REPLACED ATC CONTROL PANEL PER AMM 34-53-02, A/C RELEASED RVSM COMPLIANT RETURNED A/C TO SERVICE

Part: START VALVE — MALFUNCTIONED (LT ENGINE) · airframe 95,592 hrs · 24,897 cycles

"DURING TAXI WHILE STARTING LH ENGINE L START CUTOUT EICAS AFTER ENGINE START SEQUENCE WAS NORMAL WITH START SWITCH, SWITCHING TO AUTO POSITION AT 50% N2 AC RETURNED TO GATE AND MTX GROUNDED AC .AND DEFERRED LH START CUTOUT IAW MEL ABX-80-00-2-1 . AND RETURNED AC TO SERVICE . AND DEPARTED . NEXT LEG REPLACED L START VALVE REF: L/P 38632-27/2 AND AMM 80-11-02. OPS TEST OK. THIS CLEARS DI 53104. PLACARD REMOVED. A/C VERIFIED ETOPS 180. REF LP 38632-28/1"

Part: STARTER — FAULTED (LT ENGINE) · airframe 95,568 hrs · 24,886 cycles

DURING TAXI WHILE STARTING LH ENGINE ,LEFT STARTER CUTOUT EICAS MESG AFTER ENGINE START. AC RETURNED TO THE GATE AND MTX GROUNDED AC AND DEFERRED,STARTER SWITCH HOLDING /CUTOUTSYSTEM , IAW MEL ABX-80-11-2 FOR DEPARTURE AND RETURUN AC TO SERVICE, AND DEPARTED.

Part: HOSE — LEAKING (HYD SYSTEM) · airframe 95,424 hrs · 24,824 cycles

RIGHT HYDRAULIC SYSTEM FAILED - NO PRESSURE, QUANTITY 0 ON TAXI OUT. AC RETURED TO GATE AND MAINTENANCE GROUNDED AC . FOUND HYDRAULIC LINE FLEX LINE AS117-08K0165 (HOSE ASSY, SECT 31 ENG HYD) LEAKING AT THE RH ACMP. .REPLACED WITH FLEX LINE AND DERERRED FOR TACKING IAW AMM 20-10-04 AND GMM 07.04 . SERVICED HYDRAULICS TO FULL . LEAK CHECK GOOD .AC RETURNED TO SERVICE. NEXT LEG REMOVED & REPLACED R/H HYD ACMP TEMPORARY LINE WITH THE CORRECT FLEX LINE IAW B767 AMM 29-11-01 OK FOR SERVICE THIS CLOSES DI52279 PLACARDS REMOVED A/C REMAINS NO ETOPS LP 38850-44/2.

Part: SWITCH — MALFUNCTIONED (CABIN PRESSURE) · airframe 95,420 hrs · 24,822 cycles

CABIN ALTITUDE EICAS MESSAGE & WARNING ILLUM IN CRUISE AT FL370, EMERGENCY DESCENT CABIN ALTITUDE DESCENDED TO 7,000' AT FL240. IN CRUISE FLT AT FL240 CABIN ALTITUDE CONTINUED TO DESCEND TO 4,000'.  REMAINDER OF FLT UNEVENTFUL WITH CABIN STABLE AT 4,000'. ACFT GROUNDED & PRESSURIZED TO 4/5 PSI & CHKD FUSELAGE, WW & 48 SECT FOR LEAKS, NO DEFECTS. PACKS OPS NORM, NO LEAKS. REPLACED CABIN ALTITUDE WARNING SWITCH IAW AMM 21-33-00. FOUND ORIGINAL HAD HIGH RESISTANCE & DIDN'T OPEN & CLOSE ELECT. CABIN PRESSURE CONTROLLERS CHECK GOOD IAW AMM 21-31-02. ACFT NO ETOPS. ACFT WORKED BEFORE ANOTHER FLT, & FOUND LT FCV WAS NOT WORKING. REPLACED LT FCV IAW AMM 21-54-01. PERFORMED TEST FLT ABOVE FL370, GOOD.

Part: VALVE — WARNING MESSAGE (EQUIP COOLING) · airframe 95,413 hrs · 24,817 cycles

EQUIP COOLING VALVE MESSAGE DURING TAXI . AC RETURNED TO THE GATE. AND MAINTENANCE DEFERRED THE FWD COOLING IAW MEL ABX-21-58-7-2-1 AND AIRCRAFT DEPARTED.

Part: SHUTOFF VALVE — MALFUNCTIONED (CABIN PRESSURE) · airframe 95,408 hrs · 24,813 cycles

DURING CRUISE MASTER WARNING ILLUMINATED AT FL400 AND CABIN ALTITUDE WARNING EICAS DISPLAYED WITH SIREN , RAN QRH TO COMPLETION . CABIN ALT MODE SELECTOR IN AUTO 2. CREW DECLARED EMERGENCY PERFORMED EMERGENCY DECENT TO 10,000 AND FINISHED FLIGHT INTO CVG. AFTER LANDING MAINTENANCE GROUND AC AND TROUBLESHOT FINDING AIR DRIVEN PUMP SHUT OFF VALVE PARTIALLY OPEN WHEN OFF,AUTO,OR ON. REPLACE VALVE IAW 29-11-30 OPS CHECK GOOD,ALSO PERFORMED OPS CHECKS ON LH AND RH PACKS BOTH OPERATING NORMALLY IAW B767 AMM 21-51-00 . AC RETURNED TO SERVICE .

Part: TERMINAL — BROKEN (VALVE) · airframe 95,071 hrs · 24,678 cycles

AFTER ENGINE START, RIGHT ENGINE PRV STATUS MESSAGE. PERFORMED PRV VALVE INSPECTION AND FOUND THE TERMINAL LUG BROKEN FROM WIRE #2,. REPLACED TERMINAL LUG AS REQUIRED IAW SWPM 20-30-11 WDM 36-11-52. OPS CHECK NORMAL WITH ENGINE RUN-UP IAW AMM 71-00-00. A/C REMAINS NO ETOPS

Part: CONTROL PANEL — INOPERATIVE (ATC) · airframe 95,021 hrs · 24,655 cycles

ATC COULD NOT READ XPONDER, NEITHER L NOR R. AC RETURNED TO GATE. MAINTENANCE PERFORMED TROUBLESHOOTING RESULTING IN REPLACEMENT OF THE ATC CONTROL PANEL IAW AMM 34-53-02. OPS TEST OF BOTH TRANSPONDERS GOOD. AC RVSM COMPLIANT. AC DEPARTED.

Part: TRANSPONDER — UNKNOWN (LEFT) · airframe 94,879 hrs · 24,592 cycles

ATC REPORTED ONLY PRIMARY ON THE L XPDR SWAPPED TO R NO CHANGED AC RETURENED TO GATE AND MAINTENANCE GROUNDED AC. MAITENANCE PERFORMED ATC TEST IAW B767 AMM 34-53-01 NO FAULT FOUND TEST PASSED AC REMAIN CAT IIIB. AND RETURND AC TO SERVICE . AND AC DEPARTED .

Part: SENSOR — MALFUNCTIONED (CABIN TEMP) · airframe 94,791 hrs · 24,550 cycles

L PACK TEMP SHOWS INOP DURING TAXI AC RETURENED TO GATE AND MAINTENANCE GROUNDED AC .AND DEFERRED PACK FOR DEPARTURE IAW MEL ABX-21-51-3-1 AND RETURNED AC TO SERVICE.AC DEPARTED T/S SYSTEM FOUND BAD COMPRESSER OUTLET TEMP SENSOR FOR LH PACK R/R TEMP SENSOR WITH NEW IAW B767 AMM 21-52-01. SYSTEM WAS RAN AND OPERATION IS NORMAL. THIS CLEARS DI 48896. PLACARDS REMOVED. ACFT REMAINS NON ETOPS

Part: WARNING LIGHT — FALSE ACTIVATION (ANTI-SKID SYS) · airframe 94,755 hrs · 24,534 cycles

AFTER PUSH BACK & ENG START WHEN BRAKES WERE RELEASED ANTISKID OFF EICAS & DISCRETE LIGHT CAME ON, AND PARKING BRAKE DISCRETE LIGHT STAYED ON AC RETURNED TO THE GATE AND MAINTENANCE GROUNDED THE AC. OPERATED PARKING BRAKE VALVE NUMEROUS TIMES. PERFORMED BITE TEST AND RESET OF ANTI-SKID VALVE. SYSTEM CHECKS GOOD AS PER AMM 32-44-11.RETURNED AC TO SERVICE

Part: VALVE — MALFUNCTIONED (ZONE 100) · airframe 94,701 hrs · 24,513 cycles

DURING TAXI FWD CARGO AIR INOP .DEFERRED SYSTEM FOR DEPARTURE IAW MEL -ABX-21-28-1.RETURNED AC TO SERVICE FOR FLIGHT. T/S PER FIM 21-28 FAULT TREE 810. NO FAULTS NOTED ON ZONE TEMP BITE TEST. "COND CARGO VALVE" MSG REMAINS AFTER RESET. LEADS TO BLOCK 42, (REPLACE FWD CARGO A/C SHUT OFF VALVE). DEACTIVATED SYSTEM PER MEL 21-28-1. DI REMAINS OPEN. R&R FWD CARGO VLV SHUTOFF VLV PER MM 21-28-01 OPS CHKD OK PERFORMED REACTIVATION PROCEDURES PER MEL MPM 21-28-1 PLACARD REMOVED AND DI CLEARED.

Part: INDICATOR — INOPERATIVE (ZONE 200) · airframe 94,438 hrs · 24,384 cycles

LOWER EICAS DISPLAY FLASHING WHILE HOLDING SHORT AT RUNWAY / WENT BLANK + CAME BACK ON AC RETURENED TO GATE MAINTENANCE GROUNDED AC . DEFERRED LOWER EICAS DISPLAY IAW ABX-31-41-1-1 AC RETURNED TO SERVICE. AT NEXT MAINTENACE BASE REMOVED AND REPLACED LOWER EICAS DISPLAY UNIT IAW B767 AMM 31-41-01 OPS CHECK GOOD. DI CLEARED, PLACARD REMOVED. A/C RELEASED BACK TO ETOPS 180. PLACARD ROTATED. REF LP 38548-80/3

Part: SHUTOFF VALVE — MALFUNCTIONED (ZONE 500) · airframe 94,342 hrs · 24,340 cycles

DURING TAXI LH. ENGINE BLEED VALVE STUCK CLOSED AFTER ENGINE START. AC RETURNED TO BLOCK AND GROUNDED BY MAINTENACE .REMOVED AND REPLACED LEFT ENGINE PRSOV IAW B767 AMM 36-11-09 OPS CHECKS GOOD AFTER ENGINE RUNS..AC RETURNED TO SERVICE.

Part: OXYGEN MASK — MALFUNCTIONED (ZONE 200) · airframe 94,335 hrs · 24,336 cycles

HOT MIC ON F/O'S 02 MASK . REURNED TO GATE GROUNDED BY MAINTENANCE SWAPPED F/O'S AND 1ST OBS O2 MASK ASSY IAW AMM 35-11-51. OPS CHECK GOOD AIRCRAFT RETURNED TO SERVICE

Part: CIRCUIT BOARD — DEFECTIVE (ZONE 100) · airframe 94,194 hrs · 24,270 cycles

"LH ENG BLEED OFF LIGHT. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE REMOVED + REPLACED LH PRSOV PER AMM 36-11-09 AFTER ENG START NO BLEED LH ENG STATUS MSG + 0 DUCT PRESS C/W HPSOV THUM TEST REF AMM 36-11-07 AND PRV THUMB TEST REF AMM 36-11-18 NO DEFECTS NOTED ON BOTH LH ENG VALVE (HPSOV + PRV) PERFORMED ENG RUN AT IDLE POWER STILL NO BLEED AVAILABLE SWAPPED AIR SUPPLY CAR LH WITH RH (LH M859 P/N 285T1115-15 S/N D00660) (R/H P/N 285T1115-15 S/N D01862) ENG RUN UP SUCCESSFUL PLACED AIR SUPPLY PLACED AIR SUPPLY CARDS BACK TO ORIGINAL CONFIGURATION REMOVED AND REPLACED LH AIR SUPPLY CONTROL CARD PER AMM 36-12-00 OPS CHECK GOOD LH ENG BLEED PRESSURE OK CONTROL CARDS READ AS FOLLOW LH P/N 285T1115-15 S/N D01340 R/H P/N 285T115-15 S/N D01862 A/C OK FOR SERVICING A/C REMAINS NO ETOPS PRSOV OPS AND LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: PRESSURE VALVE — FAULTY (LEFT ENGINE) · airframe 94,183 hrs · 24,265 cycles

AT FL340 CABIN ALT EICAS MESSAGE AND DISCRETE LIGHT ILLUMINATED AND STAYED ON UNTIL DESCENT TO 13,000. CREW DECLARED AN EMERGENCY AND OXYGEN MASKS WERE USED. AIRCRAFT RETURNED TO DEPARTURE AIRPORT WITHOUT FURTHER INCIDENT. MAINTENANCE GROUNDED AIRCRAFT. MAINTENANCE FOUND LEFT BLEED OUTPUT VERY LOW. REMOVED AND REPLACED THE LEFT, PRV IAW AMM 36-11-10 PRV CONT. IAW AMM 36-11-19 AND THE LEFT PRSOV IAW AMM 36-10-09 ALL 3 COMPONENTS OPS NORMAL AIRCRAFT REMAINS ETOPS 180. AIRCRAFT RETURNED TO SERVICE

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 94,176 hrs · 24,260 cycles

CABIN ALT WARNING AT FL340 CABIN WAS AT 10,000 ZERO RATE OF CLIMB, DIFFERENTIAL AT 6 PSI. RT PACK INDICATED 27 PSI- LEFT 0 PSI. DESCENDS TO FL300 CABIN INDICATED 9500 FT. ALL OTHER INDICATIONS DID NOT CHANGE. IT TOOK APPROX 45 MINUTES FOR DIFF TO CLIMB TO 7 PSI CABIN TO DESCEND TO 6500FT RT PACK STILL INDICATED 27 PSI LEFT PACK 10 PSI. AIRCRAFT LANDED WITHOUT FURTHER INCIDENCE. AIRCRAFT WAS GROUNDED BY MAINTENANCE. MAINTENANCE PERFORMED OUTFLOW VALVE TEST AND VISUAL INSP. IAW B767 AMM 21-31-03. TEST AND GEN CONDITION GOOD. THUMB TESTED AND VISUALLY INSPECTED HPV/ HPSOV EWIS & GEN. COND IAW B767 AMM 36-11-07 & 36-11-18. TEST & GEN COND. GOOD. VISUALLY INSP. LEFT PACK IAW B767 AMM 21-51-00. GENERAL COND. GOOD. ELIMINATED LEAK FOUND AT L ISL VALVE IAW B767 AMM 36-1-04. BITE TEST CABIN PRESS CONT UNIT/ AIR SUPPLY MODULE IAW B767 AMM 36-23-00/21-31-00. NO FAULTS. CABIN PRESS LEAK TEST WITH BOTH ENG RUNNING IAW AMM 05-51-24/B767-10A. COULD NOT DUPLICATE PROBLEM AFTER MULTIPLE ATTEMPTS. SYS OPERATES NORMAL. LEFT PACK PLACED ON DEFERRAL PER MEL 21-51-1, PLACARD INSTALLED. MAINTENANCE PROCEDURES COMPLIED WITH. AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 94,106 hrs · 24,228 cycles

AIRCRAFT BLOCKED OUT AND DURING TAXI THE FLIGHT CREW WAS NOTIFIED THAT THE LOG BOOK HAD AN OPEN ENTRY FOR THE MAIN CARGO DOOR REINSPECT. THE AIRCRAFT RETURNED TO BLOCK AND MAINTENANCE PERFORMED MAIN CARGO DOOR REINSPECT AND VERIFIED THE DOOR WAS CLOSED AND LOCKED PER MEL 52-71-1-2. LOG BOOK ENTRY COMPLETE. D.I. REMAINS OPEN. AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 94,101 hrs · 24,224 cycles

INFLIGHT MAIN CARGO DOOR INDICATION ILLUMINATED DURING CLIMB OUT OF CVG. FLIGHT CREW ELECTED TO RETURN TO CVG. AIRCRAFT LANDED WITH OUT FURTHER INCIDENT. AIRCRAFT WAS GROUNDED BY MAINTENANCE. MAINTENANCE PLACED ON D.I. IAW MEL 52-71-1-2 MBCB 8-14-23 PLACARD INSTALLED C/W MX PROCEDURES TO VERIFY DOOR IS LATCHED AND LOCKED. AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 94,095 hrs · 24,221 cycles

AIRCRAFT DEPARTED SKBO. AT ABOUT 2000Z AT FL240 WE GOT A MASTER WARNING ASSOCIATED WITH A “MN CARGO DOOR” DISCRETE LIGHT. WE RAN THE QRH AND RETURNED TO BOG. THE CABIN PRESSURIZATION GAVE NO INDICATION OF AN OPEN DOOR AND THE DISCRETE LIGHT WENT OUT ON APPROACH INTO BOG. WE ELECTED TO LAND OVERWEIGHT AT 325,800LBS RATHER THAN A CIRCLE ABOVE 12,000’ AND UNABLE TO DESCEND DUE TO HIGH TERRAIN. WE DECLARED AN EMERGENCY AND ENTERED OVERWEIGHT LANDING IN THE LOGBOOK AS WELL AS THE WRITE UP FOR THE MAIN CARGO DOOR ANNUNCIATION. AIRCRAFT WAS GROUNDED BY MAINTENANCE. MAINTENANCE PERFORMED INSPECTION TO VERIFY DOOR WAS CLOSED. DOOR INDICATION WAS DEFERRED IAW MEL 52-71-2. AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 94,072 hrs · 24,208 cycles

BLEED ISLN VALVE EICAS MSG AFTER PUSH-BACK. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE FOUND LH ISOL VALVE LOCKOUT PIN IN THE LOCKED DETENTS. ROTATED LOCK PIN TO UNLOCK DETAIN AND FOUND SYSTEM TO OPERATE NORMAL IAW B767 AMM 36-11-04. AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 93,851 hrs · 24,121 cycles

CABIN HEAT FWD/AFT/CABIN INOP CAME ON AFTER ENGINE START. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE BITE CHECKED ZONE TEMP CONTROLLER IAW B767 21-61-00 NO MESSAGES PRESENT. ALL FAULTS ON EICAS CLEARED. A/C REMAINS ETOPS 180. AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 93,840 hrs · 24,113 cycles

NOTICED A L ENG EGT OVERTEMP OF 657 DURING PUSHBACK PRIOR TO ENGINE START. CONTACTED MAINTENANCE CONTROL AND ADVISED TO RETURN TO GATE. AICRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE RESET INDICATION PER FIM 71-05 FAULT TREE 810. OKAY TO CONTINUE. A/C REMAINS NO ETOPS. AIRCRAFT RETURNED TO SERVICE.

Part: WEB — CRACKED (ZONE 500) · airframe 93,657 hrs · 24,053 cycles

DURING C21 MAINTENANCE CHECK AT HAECO AMERICAS, MAINTENANCE REPORTED LH WING L/E BULLNOSE WEB (BEAM) AT APPROX. OSS 679.82 (AT FUEL PANEL) IS CRACKED. THE B767-300 SRM 57-41-13 FIG. 201 REPAIR 3 IS FOR THIS SPECIFIC AREA. THE REFERENCED SRM REPAIR IS FOR THE CRACK DAMAGE CONTAINED WITHIN THE RADIUS AND ON THE FLANGE ONLY. HOWEVER, A 2ND CRACK WAS REPORTED ON THE VERTICAL WEB. THE REFERENCE SRM REPAIR IS LIMITED ON THE DAMAGED FLANGE. THE NEW TRIM OUT INCLUDES FLANGE AND WEB OF THE BULL NOSE WEB. REPAIRED PER ABX-REA-5741-64991-00.

Part: NOSE COWL — WORN (RIGHT ENGINE) · airframe 93,657 hrs · 24,053 cycles

DURING C21 MAINTENANCE CHECK AT HAECO AMERICAS, MAINTENANCE FOUND THAT NO. 2 INLET, (BULKHEAD ASSY.) LOWER CHORD (314T4013-17) HAVE WEAR MARK ON THE INBOARD AND OUTBOARD SIDE (AT THE GROOVE). THE INBOARD SIDE HAS MATERIAL LOSS OF 0.015” AND OUTBOARD SIDE HAS MATERIAL LOSS OF 0.027” FROM INITIAL THICKNESS OF 0.110 INCHES (BAC1506-3111). BOTH ARE OUT OF LIMITS PER SRM 54-13-02 ALD1, FIGURE 101, DETAIL III OF 10%. THE LENGTH OF DAMAGES IS BOTH 2.40 INCHES. REPAIRED PER ABX-REA-7110-64999-00

Part: PIVOT — CORRODED (ZONE 300) · airframe 93,657 hrs · 24,053 cycles

DURING C21 IN HAECO AMERICAS C21 MAINTENANCE CHECK. DURING ACCOMPLISHMENT OF T/C ABX-55-552-00-01, MAINTENANCE DISCOVERED CORROSION DAMAGE AT TWO FASTENER HOLES COMMON TO THE RIGHT HAND AFT HORIZONTAL STABILIZER PIVOT FITTING AND SPLICE STRAP. SUBJECT HOLES WERE REAMED TO CLEAN, ROUND AND FINAL HOLE DIAMETER OF 0.4351-INCH. THE HORIZONTAL STABILIZER SPLICE STRAP AND PIVOT FITTINGS ARE CLASSIFIED AS PRIMARY STRUCTURE, A PSE, AN AWL, AND FCBS (NOTE 1) PER 767-300 SRM 51-00-04 STRUCTURAL CLASSIFICATION. REPAIRED PER ABX-REA-5551-64995-00.

Part: SUPPORT — CORRODED (ZONE 500) · corrosion level 2 · airframe 93,657 hrs · 24,053 cycles

DURING C21 IN HAECO AMERICAS C21 MAINTENANCE CHECK. HAECO NR 22798 - LH HAND REAR SPAR HYD LINE SUPPORT FOR CLAMP BLOCK IS CORRODED.REMOVED AND REPLACED -13 BRKT IAW BAC DWG 272T1338 REV "A". SUPPORT FABRICATED PER BAC DWG 272T1338 REV "A"

Part: VAPOR BARRIER — DAMAGED (LEFT PYLON) · airframe 93,657 hrs · 24,053 cycles

DURING C21 MAINTENANCE CHECK AT HAECO AMERICAS, MAINTENANCE FOUND NO. 1 PYLON OUTBOARD VAPOR BARRIER WEB APPROXIMATELY AT NAC STA. 230 DAMAGED AT THE D4044J MOUNT (CUTOUT). THE D4044J MOUNT WAS PULLED-OUT FROM THE WEB. THE SUBJECT BARRIER IS SUBJECT TO SB-767-54-0080-02 (AD 2004-16-12). REPAIRED PER ABX-REA-5400-64998-00

Part: PIN — FAILED INSP (MAIN CARGO DOOR) · airframe 93,657 hrs · 24,053 cycles

DURING C21 IN HAECO AMERICAS C21 MAINTENANCE CHECK WHILE PERFORMING JOB CARD FOR MCD PIN INSPECTION IT WAS DICOVERED THAT PINS #1,3.6 AND 7 FAILED DIMENSIONAL CHECK.. REMOVED AND REPLACED MCD LATCH CAM PINS OPS CHECKED GOOD, NO FURTHER DEFECTS NOTED PER B767-300 IAI AMM 52-32-11.

Part: ELEVATOR — DAMAGED (ZONE 300) · airframe 93,657 hrs · 24,053 cycles

DURING C21 MAINTENANCE CHECK AT HAECO AMERICAS, MAINTENANCE REPORTED R/H TRAILING EDGE ELAVATOR HAS DAMGE DUE TO IMPACT TO LIFT. REPAIRED IMPACT DAMGE ON R/H ELEVATOR O/B T/E WITH 350 DEGREE CARBON GRAPHITE DOUBLER WITH CORE REPAIR IAW B767-300 51-40-02, 55-20-01, 51-70-04 B767 NDTM PT 1 51-01-01, BAC DWG 113T3001 REV C, WEIGHT AND BALANCED ELEVATOR IAW B767-300 SRM 51-60-02.

Part: PANEL — DAMAGED (RIGHT PYLON) · airframe 93,657 hrs · 24,053 cycles

DURING C21 MAINTENANCE CHECK AT HAECO AMERICAS, MAINTENANCE REPORTED THAT THE NO. 2 PYLON AFT HYDRAULIC BAY CLOSE UP PANEL (313T3381-212) HAS NUMEROUS DAMAGES. SINCE THERE ARE AREAS HAVE MULTIPLE AND HEAT DAMAGES, MAINTENANCE OPTED TO REPLACE THE OUTER SKIN AND DOUBLERS. THE DRAWING 313T3381-212 IS BONDED /MANUFACTURED PER BAC5514-570 (DRAWING FL 1). MAINTENANCE "CANNOT ACCOMPLISH" THE BAC5514 ENTIRETY AND REQUESTED TO REPLACEMENT PARTS AND BOND PER B767-300 SRM 51-70-10 (SRM 54-53-70). REPAIRED PER ABX-REA-5450-64997-00.

Part: SPLICE PLATE — CORRODED (ZONE 500) · corrosion level 2 · airframe 93,657 hrs · 24,053 cycles

DURING C21 MAINTENANCE CHECK AT HAECO AMERICAS, MAINTENANCE REPORTED CORROSION DAMAGE ON THE LH WING OUTBOARD UPPER SPLICE PLATE (114T0223-19), APPROXIMATELY AT OSS 630.945. (2) RIVETS WERE REMOVED PER B767-300 SRM 51-40-02. THE DAMAGE WAS BLENDED PER SRM 51-20-01 WITH MINIMUM MATERIAL REMAINING OF 0.052 INCHES (LOSS 0.028”) FROM INITIAL THICKNESS OF 0.080 INCHES. THE MATERIAL LOSS FOUND TO BE OUT OF LIMITS PER SRM 51-41-01, ALLOWABLE DAMAGE 2. HOWEVER, MISCOMMUNICATION BETWEEN MAINTENANCE AND ENGINEERING, INADVERTENTLY CUT THE SUBJECT SPLICE PLATE.REPAIRED PER ABX-REA-5741-65023-00

Part: SKIN — CORRODED (LT WING TE FLAP) · airframe 93,657 hrs · 24,053 cycles

DURING C21 MAINTENANCE CHECK AT HAECO AMERICAS, AIRCRAFT MAINTENANCE DISCOVERED (2 EA.) AREAS OF CORROSION ON THE LOWER OUTER SKIN PANEL (P/N 113T3143-3) OF THE LEFTWING OUTBOARD FLAP ASSEMBLY (P/N 113T3100-77, S/N 000664) CURRENTLY INSTALLED ON AIRCRAFT N219CY. THE FIRST AREA, DAMAGE 2 (OPS 22352) IS LOCATED APPROXIMATELY 100” FROM THE INBOARD EDGE AS SHOWN IN FIGURE 3. THE CORROSION WAS REMOVED BY BLENDING PER 767-300 SRM 57-53-01, FIGURE 101, AD 1 AND AFTER EVALUATION, THE REWORKED AREA WAS FOUND TO EXCEED PUBLISHED LIMITS (0.065” REMAINING MATERIAL THICKNESS AT THE THINNEST LOCATION FROM 0.100” (NOMINAL) (35% MATERIAL LOSS). THE SECOND AREA, DAMAGE 1 (OPS 22351) IS LOCATED APPROXIMATELY 108” FROM THE INBOARD EDGE AS SHOWN IN FIGURE 3. THE CORROSION WAS REMOVED BY BLENDING PER 767-300 SRM 57-53-01, FIGURE 101, AD 1 AND AFTER EVALUATION, THE REWORKED AREA WAS FOUND TO EXCEED PUBLISHED LIMITS (0.076” REMAINING MATERIAL THICKNESS AT THE THINNEST LOCATION FROM 0.100” (NOMINAL) (24% MATERIAL LOSS). PER 767-300 SRM 57-53-01, REPAIR 1, THE DAMAGE CAN BE REPAIRED PER 767-300 SRM 51-70-10 EXCEPT PER TABLE A, AN INITIAL SKIN THICKNESS IS LIMITED TO 0.080” COMPARED TO THE 0.100” OUTER SKIN THICKNESS REPORTED AT EACH DAMAGE LOCATION. REPAIRED PER ABX-REA-5750-64994-00.

Part: CONTROLLER — FAULTED (CABIN TEMP) · airframe 92,396 hrs · 23,724 cycles

CABIN TEMP CONTROLLERS INDICATED INOP ON EICAS FOR "FWD" , "AFT", AND "FLT DK" ON OVHD PANEL. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE RESET CABIN TEMP ZONE CONTROLLER REF AMM 21-61-00 OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE.

Part: NONE — NONE · airframe 92,117 hrs · 23,649 cycles

STARTING LEFT ENGINE STATUS MESSAGE "L ENG PRV" AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE PERFORMED OPS CHECK OF BITE AIR SUPPLY CONTROLLER IAW AMM 36-23-00 OPS CHECK GOOD. NO FAULTS AT THIS TIME. A/C REMAINS ETOPS 180. AIRCRAFT RETURNED TO SERVICE.

Part: CABIN PRESSURE — FAILED · airframe 92,059 hrs · 23,629 cycles

DURING CRUISE FLIGHT AT 28000, THE MASTER WARNING HORN / LITES AND EICAS MESSAGE, CABIN ALT WAS ON. CABIN ALT WAS 11,000. WE SWITCHED FROM CONTROLLER 2 TO 1. HAD A STATUS MESSAGE "CABIN ALT AUTO2/CAB. CREW DESCENDED TO 10,000 FEET AND DECLARED AN EMERGENCY. AIRCRAFT DIVERTED INTO PTY. MAINTENANCE GROUNDED AIRCRAFT. MAINTENANCE BITE BOTH PRESSURE CONTROLLERS NO FAULTS NOTED INSPECTED PRESSURE RELIELF VALVES NO DISCREPANCIES NOTED AT THISE TIME. REPLACED OUTFLOW VALVE ASSY OPS CHECK AND PRESSURIZED AT 5PSI. NO DEFECTS IAW AMM 21-31-03, 21-31-00, 21-32-00. AIRCRAFT RETURNED TO SERVICE.

Part: NONE — NONE · airframe 91,637 hrs · 23,528 cycles

CARGO FIRE "B" INDICATOR LIGHTS "6" & "8" AMBER ILLUMINATED. CREWMEMBER VISUALLY INSPECTED CARGO COMPARTMENT AND VERIFIED NO SMOKE OR FIRE. THE CREW DECIDED TO DIVERT AND LAND AT NEAREST AIRPORT (CYYR) AN EMERGENCY WAS DECLARED AND AIRCRAFT LANDED OVERWEIGHT WITH OUT FURTHER INCIDENT. AIRCRAFT WAS GROUNDED UNTIL MAINTENANCE PERSONNEL ARRIVED. MAINTENANCE DEFERRED CARGO FIRE SYSTEM IAW MEL 26-16-2-2. AICRAFT RETURNED TO SERVICE.

Part: NONE — NONE · airframe 90,367 hrs · 23,211 cycles

APU BLEED VALVE CYCLED CLOSED AND REMAINED IN THE COLSED POSITION WHEN AC PACKS WERE TURNED OFF ON ENGINE START CHECKLIST, APU BLEED POWER CONTROL C/B OPENED. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE RESET APU BLEED CONTROL C/B SATIS. IAW AMM 49-53-01 AIRCRAFT REMAINS ETOPS 180. AIRCRAFT RETURNED TI SERVICE.

Part: FLOOR SUPPORT — CORRODED (FWD CARGO) · airframe 88,203 hrs · 22,587 cycles

DURING C-CHECK AMES TAMPA FACILITY, FWD CARGO FLOOR DECK SUPPORT ANGLE UNDER FLOOR WEB AT I/B SIDE OF POWER DRIVE 6R CORRODED. REMOVED INTERCOSTAL. FOUND ORIG MAT .100", MAT LOSS .018", MAT REMAINING .082". AREA FOUND TO BE OUT OF LIMIT. LOCATED AND DRILLED NEW INTERCOSTAL IAW B767-300 DWG 143T5019-31AND SRM 51-40-03. FABRICATED NEW INTERCOSTAL IAW B767-300 SRM 51-40-02

Part: FLOORBEAM — CORRODED (BS 654) · airframe 88,203 hrs · 22,587 cycles

DURING C-CHECK, CORROSION ON FWD CARGO STA 654 FLOOR BEAM UPPER CAP BOTTOM SIDE ARPOUND NUT PLATES LBL 10. REMOVED CORROSION AT FWD CARGO STA 654 FLOOR BEAM UPPER CAP IAW B767-300 SRM 51-10-02. EVALUATED DAMAGE, ORIGINAL MATERIAL THICKNESS IS .102, MAT LOSS IS .037, MAT REMAINING IS .065. FOUND TO BE OUT OF LIMITS IAW B767-300 SRM 53-00-07. REMOVED AND REPLACED FLOOR BEAM UPPER CAP IAW B767-300 SRM 51-40-02.

Part: START VALVE — BINDING (RT ENGINE) · airframe 87,984 hrs · 22,504 cycles

RIGHT ENGINE START VALVE WILL NOT OPEN. AIRCRAFT BTB AND GROUNDED. R & R RT ENGINE START VALVE, IAW B-767 AMM 80-11-02. OPERATIONS GOOD. AIRCRAFT RELEASED.

Part: PRESSURE SWITCH — INTERMITTENT (RT OIL PRESSURE) · airframe 87,785 hrs · 22,423 cycles

DURING ENGINE START RIGHT ENGINE OIL PRESSURE DISCRETE LIGHT INTERMITTENT, AICRAFT RETURNED TO GATE WHERE MAINTENANCE GROUNDED AIRCRAFT UNTIL REPAIRED. REMOVED AND REPLACED RT ENGINE LOW OIL PRESSURE WARING SWITCH, PER AMM 79-33-01. OPERATIONAL TEST C/W NO DEFECTS NOTED. ENGINE RUN UP C/W FOR 5 MIN IN IDLE POWER RT ENGINE LOW OIL PRESS LIGHT WORKING FINE. A/C RELEASED REMAINS ETOPS 180.

Part: WARNING LIGHT — ILLUMINATED (MASTER) · airframe 87,186 hrs · 22,190 cycles

MASTER WARNING LIGHT ILLUMINATES DURING CRUISE FLIGHT, NO OTHER INDICATIONS OR EICAS MESSAGES NOTED. AIRCRAFT WAS GROUNDED.

Part: LATCH — UNSECURE (ENTRY DOOR) · airframe 87,176 hrs · 22,186 cycles

ENTRY DOOR SAFETY LATCH POPPED IN FLIGHT CAUSING A FORWARD ENTRY DOOR EICAS MESSAGE. UNABLE TO RE-SECURE LATCH IN FLIGHT. AIRCRAFT WAS GROUNDED.

Part: WARNING LIGHT — ILLUMINATED (BRAKES) · airframe 87,139 hrs · 22,174 cycles

WHEN RTO SELECTED AUTO BRAKE EICAS MSG AND BRAKE DISCRETE LIGHT ILLUMINATED W/RTO SWITCH ENGAGED. AIRCRAFT WAS GROUNDED.

Part: NOSE RIB — CRACKED (RT WING) · airframe 84,469 hrs · 21,115 cycles

A 1.5 INCH CRACK IN THE NOSE RIB ANGLE AT RIGHT WING LEADING EDGE STATION 488. THE NOSE RIB ANGLE WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: STRUCTURE — CORRODED (RT WING) · corrosion level 2 · airframe 84,469 hrs · 21,115 cycles

CORROSION ON THE RIGHT WING TRAILING EDGE LOWER CHORD BETWEEN WING STATIONS 344 AND 433. THE CHORD WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: HANDLE — DIRTY (DOOR ARMING) · airframe 82,692 hrs · 20,363 cycles

THE LEFT FORWARD ENTRY DOOR WAS EXTREMELY HARD TO ARM. THE ACFT WAS GROUNDED AND THE DOOR LATCH AND LOCK MECHANISM WAS INSPECTED INTERNALLY AND EXTERNALLY IAW AMM 52-12-25. THE ASSEMBLY WAS CLEANED AND A SATISFACTORY OPERATIONAL CHECK OF THE DOOR LATCH AND LOCK WAS PERFORMED. THE CAUSE OF THE STIFF ARMING HANDLE IS UNKNOWN.

Part: HANDLE — MALFUNCTIONED (PAX DOOR) · airframe 82,323 hrs · 20,178 cycles

THE LEFT FORWARD ENTRY DOOR ARMING HANDLE WOULD NOT SEAT AFTER THE DOOR WAS CLOSED. THE AIRPLANE WAS REMOVED FROM SERVICE AND THE EXTERNAL EMERGENCY RELEASE HANDLE WAS RESET, ALLOWING THE INTERIOR ARMING HANDLE TO SEAT. THE CAUSE OF THE ARMING HANDLE NOT SEATING IS UNKNOWN.

Part: COMPUTER — MALFUNCTIONED (AUTOPILOT SYS) · airframe 77,177 hrs · 18,386 cycles

FUMES IN COCKPIT AFTER LOSS OF AUTOPILOT. REPLACED FAULTY CTR FLIGHT CONTROL COMPUTER.

Part: CHANNEL — CORRODED (RT HORIZ STAB) · corrosion level 2 · airframe 76,862 hrs · 18,256 cycles

THE RIGHT HORIZONTAL STABILIZER OTBD TE WEDGE REAR SPAR HAS MULTIPLE DOUBLE DRILLED HOLES & CORROSION. REMOVED DAMAGED SECTION OF RT OTBD TE WEDGE. FABRICATED NEW SECTION & REPAIRED DOUBLED IAW SRM 51-70-11. SDR INFO, CORRODED, LEVEL 2, PN 183T1141-6, PART NAME CHANNEL, SN NSN, FS & BS LOCATION FROM HSBL 357 TO HSBL 366. ACFT WAS GNDED.

Part: STRUCTURE — CRACKED (RT WING) · airframe 76,862 hrs · 18,256 cycles

RIGHT WING LE SUPPORT, STATION LES 525 CRACKED. R & R RT WING LE LOWER CHORD IAW SRM 51-40-02. SDR INFO, CRACKED, LENGTH: 0.75" PN 114T2206-6, PART NAME CHORD, SN NSN, STRINGER & WS LOCATION: LES 525. ACFT WAS GNDED.

Part: REPAIR — CRACKED (RT WING) · airframe 76,862 hrs · 18,256 cycles

FOUND A CRACK ON RT WING LE STATION 651 ON A PREVIOUS REPAIR OF A STRUT RIB. R & R AIR LOAD RIB LOWER CHORD AT STATION 651 IAW SRM 51-40-02 & DWG 114T2212. SDR INFO, CRACKED, LENGTH 1.2", PN 114T2212-6, PART NAME CHORD, SN N/A, STRINGER & WC LOCATION WS 651. ACFT WAS GNDED.

Part: SKIN — CORRODED (FUSELAGE) · airframe 74,610 hrs · 17,344 cycles

LOWER FUSELAGE SKIN AT FWD MIDDLE MOUNTING AREA WHERE RADIO ALTIMETER ANTENNA IS SECURED HAS CORROSION. REMOVED CORROSION AT FUSELAGE SKIN REPAIR DOUBLER UNDER FWD MIDDLE RADIO ALTIMETER ANTENNA IAW SRM 51-40-02, AND INSTALLED A NEW REPAIR DOUBLER IAW SRM 53-00-01 FIG 201. ACFT WAS GROUNDED.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 74,610 hrs · 17,344 cycles

CORROSION ON LT UPPER WING SURFACE LOCATED AT REAR SPAR APPROX WBL 710. REMOVED CORROSION IAW SRM 57-20-01, DETAIL I AREA WAS REPAIRED ON ABX REA NR B657-60562-MR; ACFT WAS GROUNDED.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 74,610 hrs · 17,344 cycles

CORROSION ON UPPER WING SURFACE ALONG SKIN T/E ABOVE REAR SPAR FROM INBD EDGE OF OTBD AILERON TO APPROX WS 990.5. REMOVED CORROSION IAW SRM 57-20-01, DETAIL I. WS LOCATION FROM 912 TO 1008; ACFT WAS GROUNDED.

Part: SKIN — CORRODED (ZONE 500) · airframe 74,610 hrs · 17,344 cycles

CORROSION AT FASTENERS AND AFT SKIN EDGE OF LT WING UPPER SKIN WS 798. REMOVED CORROSION IAW SRM 57-20-01, DETAIL I AREA WAS REPAIRED ON REA NR B657-60562.

Part: SKIN — GOUGED (FUSELAGE) · airframe 74,610 hrs · 17,344 cycles

FORWARD UPPER TCAS ANTENNA MOUNTING AREA HAS SCRATCHES AND GOUGES IN THE FUSELAGE. R & R DOUBLER IAW REA B653-60557-MR, ACFT WAS GROUNDED.

Part: SKIN — DENTED (FUSELAGE) · airframe 74,610 hrs · 17,344 cycles

OUTWARD DENT, STA 1654-1678, S32R-S33R. DENT IS OUT OF LIMITS, REPAIRED IAW SRM 53-00-01, FIG 201, REPAIR 6; ACFT WAS OUT OF LIMITS AND GROUNDED.

Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 74,610 hrs · 17,344 cycles

R1 DOOR FWD CUTOUT SILL HAS CORROSION. R & R R1 DOOR FWD CUTOUT SILL STIFFENER IAW SRM 51-40-02 AND DWG 141T8313. CORR LEVEL 2. ON ACFT: FROM DOOR STA 79 TO DOOR STA 86; ACFT WAS GROUNDED.

Part: SKIN — DENTED (FUSELAGE) · airframe 74,610 hrs · 17,344 cycles

OUTWARD DENT STA 1654-1678 ABOVE S36L. DENT IS OUT OF LIMITS, REPAIRED IAW SRM 53-00-01 FIG 201, REPAIR 6, ACFT WAS GROUNDED.

Part: SPLICE PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 74,610 hrs · 17,344 cycles

STRINGER 39, SPLICE PLATE HAS SURFACE CORROSION AT END. REMOVED DAMAGE AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-03, FABRICATED NEW SPLICE IAW SRM 53-00-03. ACFT WAS GROUNDED.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 74,610 hrs · 17,344 cycles

FLOOR WEB PANEL CORRODED AROUND SCREW HOLES. FABRICATED NEW WEB IAW ENGINEERING DWG 143T5010. ACFT WAS GROUNDED.

Part: SUPPORT CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 74,610 hrs · 17,344 cycles

R1 DOOR CUTOUT CENTER LOWER SILL HAS CORROSION IN SEVERAL PLACES. R & R R1 DOOR CUTOUT CENTER LOWER SILL SUPPORT CHANNEL IAW SRM 51-40-02 AND DWG 141T8313. CORROSION LEVEL 2, ACFT WAS GROUNDED.

Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 74,610 hrs · 17,344 cycles

LOWER CARGO STRESS PANEL STA 1129-1351 HAS CORROSION AT 2 SPOTS AT EDGE. BLENDED AND CHECKED LIMITS (OUT OF LIMIT) FABRICATED NEW PANEL, TREATED, PRIMED, PAINTED, AND REASSEMBLED IAW SRM 53-60-53, DETAIL III, B767-300 PRINT, SRM 51-20-01, SRM 51-40-02 LBL20 LBL36, ACFT WAS GROUNDED.

Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 74,610 hrs · 17,344 cycles

R1 DOOR AFT LOWER CUTOUT SILL HAS CORROSION. R & R STIFFENER IAW SRM 51-40-02 FROM DOOR STA 121 TO DOOR STA 130, ACFT WAS GROUNDED.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 74,610 hrs · 17,344 cycles

LOWER CARGO, BULK CARGO AREA, BS 1480-1502, MOST RT BULK CARGO FLOOR SUPPORT HAS SURFACE CORROSION AT MARKED NUTCLIP HOLES. REPAIRED RIGHT FLOOR SUPPORT AT FS 1480-1502 IAW SRM 51-70-11, FIG. 1; ACFT WAS GROUNDED.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 74,610 hrs · 17,344 cycles

UPPER CARGO RT SIDE STA 1219 AT S-18 HAS CORROSION ON FRAME. FRAME AT STA 1219 S-18 RT WAS FOUND TO BE OUT OF LIMITS, AND REPAIRED IAW SRM 53-00-07, FIG 201; ACFT WAS GROUNDED.

Part: FAIRING — CORRODED (APU) · airframe 74,610 hrs · 17,344 cycles

APU INLET HAS AREA OF CORROSION ON LOWER FLANGE. REMOVED CORROSION, PERFORM UTI, FOUND FLANGE OUT OF LIMITS, FABRICATED NEW FLANGE, TREATED, PRIMED AND INSTALLED IAW SRM 51-10-2 & 51-40-02, NDT MANUAL 51-00-10 AND DWG 353T0115, ACFT WAS GROUNDED.

Part: FIRE DETECTOR — FAULTY (CARGO BAY) · airframe 73,089 hrs · 16,973 cycles

CARGO FIRE A3 AMBER LIGHT DISPLAYED. REMOVED AND REPLACED CARGO FIRE DETECTOR A3 IAW AMM 26 14 00 OPS CHECK GOOD, ACFT WAS GROUNDED.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 72,021 hrs · 16,792 cycles

BOTH SHIPS FLASHLIGHTS INOP. REMOVED AND REPLACED BATTERIES IN BOTH EMERGENCY FLASHLIGHTS IAW 767 MM 25-60-00. OPS CHECK GOOD, ACFT WAS GROUNDED.

Part: HANDLE — LACK OF LUBE (ENTRY DOOR) · airframe 70,848 hrs · 16,644 cycles

52 71 X1 01 L FWD ENTRY DOOR ARMING HANDLE REQUIRED EXTERNAL HANDLE TO BE PUSHED FLUSH TO ARM. LUBRICATED AND OPS CHECK DOOR IAW B767 AMM 52 11 00, OPS CHECK GOOD AT THIS TIME, AWG.

Part: STIFFENER — CRACKED (BS 287) · airframe 69,673 hrs · 16,494 cycles

NOSE WHEEL WELL STIFFENER BS 287 LBL 25 IS CRACKED. CUT & REMOVED PORTION OF EXTRUSION. FABRICATED REPAIR PLATES. REPAIRED DAMAGE IAW SRM 51-70-12 FIG 1.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 69,673 hrs · 16,494 cycles

NOSE WHEEL WELL CHORD STA 287 RBL 25 IS CRACKED. REPAIRED NOSE WHEEL WELL CHORD STA 287 RBL 25 IAW B767 SRM 51-70-12 FIG 1 AWG.