N362CM

Part: CHARGER — FAULTED (ZONE 100) · airframe 117,518 hrs · 34,942 cycles

DURING TAXI OUT, MAIN BATTERY DISCHARGE STATUS MESSAGE ILLUMINATED. AIRCRAFT RETURNED TO BLOCKS. (BTB). MAINTENANCE REMOVED AND REPLACED MAIN BATTERY CHARGER. OPS CHECKED GOOD IAW AMM 24-31-01-4. ACFT RFEMAINS ETOPS 180. AIRCRAFT RETURNED TO SERVICE.

Part: TRANSFER SYS — MALFUNCTIONED (ZONE 100) · airframe 117,495 hrs · 34,932 cycles

UNWANTED FUEL TRANSFER FROM RIGHT TANK INTO CENTER TANK DURING CRUISE. SECOND WRITE UP FOR SAME ISSUE ON 9/11/2025 GB 845. ONLY APPARENT ON FLIGHTS LONGER THAN ONE HOUR.  PRESSURIZED FW+AFT R/H FUEL PUMPS FOR 1HR PER FIM 28-21 F/T 821 NO FUEL TRANSFERRED OBSERVED. SYSTEM CONSIDERED OK AT THIS TIME. AIRCRAFT RETURNED TO SERVICE.

Part: TRANSFER SYS — MALFUNCTIONED (ZONE 100) · airframe 117,467 hrs · 34,917 cycles

DURING CRUISE, UNWANTED FUEL TRANSFER FROM RIGHT MAIN TANK TO CENTER TANK DURING CRUISE. PROBLEM PERSISTED THROUGHOUT THE ENTIRE FLIGHT. PRESSURIZED FWD & AFT RH FUEL PUMPS FOR 1 HOUR PER FIM 28-21 F/T 821. NO FUEL TRANSFER OBSERVED. SYSTEM IS CONSIDERED OK AT THIS TIME.

Part: SMOKE GOGGLES — DAMAGED (ZONE 200) · airframe 117,019 hrs · 34,717 cycles

MAINTENANCE FOUND RH SUPERNUMERARY SEAT SMOKE GOGGLES HEADBAND HAS NO ELASTICITY. DEFERRED THE RH SUPERNUMERARY SEAT PER MEL 25-25-3. PLACARD INSTALLED, MX PROCEDURE C/W MBCB 10/16/2025. SEAT MUST NOT BE OCCUPIED. L/P: 38866-47/2. REMOVED AND REPLACED RH SUPERNUMERARY SEAT SMOKE GOGGLES IAW AMM 25-64-00. THIS CLEARS DI 63376. PLACARD REMOVED. AIRCRAFT RETURNED TO SERVICE.

Part: PLACARD — MISMARKED (ZONE 200) · airframe 117,002 hrs · 34,698 cycles

DURING SERVICE CHECK FOUND NBR 5 ESCAP REEL EXP DATE 26APR25 MTX GROUNDED A/C . DEFERRED THE ESCAPE REEL FOR DEPARTURE IAW MEL ABX-25-61-1-1 DUE TO INCORRECT DATE ON PLACARD.RETURNED A/C TO SERVICE . DI CLEARED BY INSTALLING NEW ESCAPE REEL IAW AMM 25-61-03 CHECKS GOOD . RETURNED A/C TO SERVICE.

Part: START VALVE — MALFUNCTIONED (LT ENGINE) · airframe 116,600 hrs · 34,511 cycles

DURING TAXI, LEFT ENGINE START VALVE FAILED TO OPEN.  VALVE LIGHT ON OVERHEAD ILLUMINATED "LEFT ENGINE STARTER" EICAS MESSAGE. A/C RETURNED TO GATE. (BTB) A/C DEFERRED LH ENGINE START VALVE FOR DEPARTURE IAW MEL ABX-80-00-2-1. MTX RETURNED A/C TO SERVICE.

Part: START VALVE — FAULTED (LT ENGINE) · airframe 116,532 hrs · 34,471 cycles

DURING TAXI STARTING LH ENGINE THERE WAS NO ROTATION ON LH ENGINE , A/C RETURNED TO THE GATE (BTB) AND MTX GROUNDED A/C . MTX DEFERRED LH ENGINE START VALVE IAW MEL ABX-80-00-2-1 . AND RETURNED A/C TO SERVICE .AC REMAINS NO ETOPS

Part: TARGET — OUT OF ADJUST · airframe 116,522 hrs · 34,463 cycles

DURING A/C EVAL FLIGHT ,AT CLIMBOUT LE SLAT ASYM ON EICAS AND LEADING EDGE DESCREET LIGHT , RAN CHECKLIST AND DECLARED AN EMERGENCY PERFORMED (ATB) AND RETURNED TO FIELD.MTX GROUNDED AC AND TROUBLE SHOT AND . ADJUSTED GAP ON LEADING EDGE SLAT TARGET PROX SENSOR ON #8 SLAT. ADJUSTED IAW B767 AMM 27-81-04. OPS CHECK GOOD. MTX RETURNED AC TO SERVICE.

Part: DUCT — DAMAGED (ZONE 600) · airframe 116,501 hrs · 34,450 cycles

DURING TAXI RIGHT ENG "BLEED OFF"APPEARED WITH NO DUCT PRESSURE AC RETURNED TO GAT (BTB)AND MTX GROUNDED AC .MTX TROUBLE SHOT AND FOUND COOLING DUCT DAMAGED ON RH ENGINE AND REPLACED SAME IAW B767 AMM 75-00-00 LEAK CHECK GOOD MTX RETURNED AC TO SERVICE

Part: YAW DAMPER — FAULTED (ZONE 300) · airframe 116,500 hrs · 34,449 cycles

DURING TAXI OUT R YAW DAMPER INOP CAME ON , AC RETURNED TO GATE(BTB) AND MTX GROUNDED AC , MTX DEFERRED R YAW DAMPER FOR DEPARTURE IAW MEL ABX-22-21-1 .AND RETURNED AC TO SERVICE .

Part: WARNING LIGHT — FALSE ACTIVATION · airframe 116,484 hrs · 34,442 cycles

RIGHT BLEED OFF DISCRETE LIGHT ILLUMINATED DURING TAXI.AC RETURNED TO GATE (BTB) AND MTX GROUNDED AC .PERFORMED ENGINE RUN IAW AMM 71-00-00 VALUE OPERATED NORMALLY WITH PACKS ON AIRCRAFT REMAINS NON-ETOPS + CATIIIA. AND RETURNED AC TO SERVICE

Part: WARNING LIGHT — ILLUMINATED (RT ENGINE OIL) · airframe 116,480 hrs · 34,438 cycles

RIGHT ENGINE OIL PRESSURE LIGHT ON AFTER TAXI, OIL PRESSURE NORMAL AT 28 PSI. AC RETURNED TO GATE (BTB) AND MTX GROUNDED AC . MTX DEFERRED RH ENGINE OIL PRESSURE LIGHT INDICATION IAW MEL ABX-79-33-1-1 . AC REMAINS NO ETOPS . MTX RETURNED AC TO SERVICE.

Part: PIN — BROKEN · airframe 116,177 hrs · 34,231 cycles

TOW BAR STEERING PIN BROKE DURING, PUSH LOUD BANG HEARD IN COCKPIT. REPAIRED TOWBAR AND RETURN AC TO GATE . MTX GROUNDED AC AND PERFORMED MAX LOAD CONDITIONAL INSPECTION (PHASE I INSP) IAW B767 AMM 05-51-29. NO DEFCTS NOTED. AC WAS RETURNED TO SERVICE.

Part: FMC — MALFUNCTIONED (LEFT) · airframe 115,981 hrs · 34,092 cycles

DURING TAXI IN L FMC WENT BLACK (AT SAME TIME AS SOUND AND SMOKE APPEARED AFTER AC WAS BLOCKED IN MAINTENANCE GROUNDED AC AND ACCOMPLISHED FMC INTERFACE CHECK AND WIRING CHECK MORMAL LH FMC INOP .CONTACTED ENG. RECEIVED REA 3400-65418-00 TO PULL AND COLLAR BREAKER C609. SWAPPED LH TO RH AFTER POWER UP AND VERIFY NO SMOKE THEY DEFERRED THE RH FOR DEPARTURE IAW MEL 34-61-1-1A. AND RETURES TO SERVICE .AFTER ARIVAL IN CVG . RELACED RH FMC CDU OPS CHECK GOOD IAW AMM 34-61-02 PLACARDS REMOVED THE CLEARS DI 52779.

Part: PNEUMATIC SYSTEM — FAILED (APU) · airframe 115,744 hrs · 33,976 cycles

AFTER PUSH BACK APU AIR PRESSURE LOW ON ENGIN START, WILL NOPEN START VALVE AC RETURNED TO GATE MAINTENANCE DEEFERRED THE APU PNEUMATICS IAW ABX-MEL-49-11-1-1 AND RETURNED AC TO SERVICE .

Part: CONTROL UNIT — MALFUNCTIONED (SLAT SYSTEM) · airframe 115,682 hrs · 33,950 cycles

AFTER TAKE OFF EICAS MESSAGE LEADING EDGE SLAT DISAGREE. LEADING EDGE SLAT DISPLAYED BETWEEN UP AND 1. AC PERFORMED ATB AND LANDED , MAINTENANCE GROUNDED AC AND TROUBLESHOT REPLACING FSEU IAW B767 AMM 27-51-01. LEADING EDGE SLATS AND FLAPS CHECK GOOD AS PER AMM 27-51-01 AIRCRAFT REMAINS ETOPS 180 + CAT IIIB. REURNED AC TO SERVICE .

Part: SHUTOFF VALVE — FAULTED (HYD SYSTEM) · airframe 115,454 hrs · 33,848 cycles

LEFT WING HYD VALVE MESSAGE CAME ON DURING PUSH BACK, AC RETURENED TO GATE AND MAINTENANCE GROUNDED AC , MAINTENANCE DEFERRED LEFT WING LATERAL CONTROL HYD SHUTOFF VALVE IAW MEL ABX-27-03-1 RETURNED AC TO SERVICE AND DEPARTED .

Part: PUMP — WARNING LIGHT (RT) · airframe 115,394 hrs · 33,820 cycles

DURING TAXI R FWD FUEL PUMP INOP INDICATION ,AC RETURNED TO GATE AND MAINTENANCE GROUNDED AC . MAINTENANCE DEFERRED THE PUMP IAW MEL ABX-28-22-1. AND RETURNED AC TO SERVICE AND AC DEPARTED .

Part: BATTERY — UNSERVICEABLE (MASTER) · airframe 115,324 hrs · 33,787 cycles

DURING TAXI MAIN BAT CHGR STATUS MESSAGE IS DISPLAYED AFTER ENGINE START. AC RETURED TO GATE AND GROUNDED BY MAINTENANCE. TROUBLE SHOT AND REMOVED AND REPLACED MAIN BATTRY ASSY. IAW 24-31-01 OPS CHECK GOOD AND AC RETURNED TO SERVICE AND DEPARTED.

Part: GENERATOR — MALFUNCTIONED (LEFT) · airframe 115,319 hrs · 33,785 cycles

L GEN OFF EICAS DURING TAXI AC RETURENED TO GATE AND GROUNDED BY MAINTENANCE ,DEFERRED LH IDG IAW ABX-24-00-1-1. AND AC REURNED TO SERVICE AND DEPARTED. AC FLEW TO CVG AND LH IDG WAS REPLACEDIAW B767 AMM 24-11-01. PERFORMED OPS CHECK IAW B767 AMM 24-11-00. OPS CHECK LEAK CHECK GOOD. THIS CLEARS DI# 49271 LEFT GEN INOP PLACARD REMOVED. A/C REMAINS ETOPS 120.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 114,821 hrs · 33,568 cycles

AIRCRAFT RETURNED TO THE GATE DUE TO RT FLAP INDICATOR STUCK AT 1 DEGREE DURING CHECK LIST. AC GROUNDED BY MAINTENANCE PERFORMED OPERATIONAL CHECK IAW B767 AMM 27-51-00. BOTH LT AND RT FLAPS OPERATES NORMAL PHYSICALLY BUT RT FLAP INDICATION STUCK AT 1 DEGREE. DI 43644 REMAINS OPEN. NO DEACTIVATION PROCEDURES APPLIED. MBCB 11/10/23 AC RETURNED TO SERVICE

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 114,137 hrs · 33,270 cycles

MAIN CARGO DOOR OPEN INDICATION ON PUSH BACK. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE DEFERRED MAIN CARGO DOOR INDICATION IAW ABX MEL 52-71-1-2. AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 113,801 hrs · 33,157 cycles

AFTER PUSHBACK AND ENGINE START L ENG EEC AND R ENG EEC EICAS MESSAGES AND EEC INOP LIGHTS. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE RESET EEC TEST SWITCH. RAN BOTH ENGINES. ALL EEC FUNCTIONS AND INDICATIONS NORMAL, REF B767 AMM 73-23-00. A/C REMAINS "ETOPS 180". AIRCRAFT RETURNED TO SERVICE

Part: BEAM — CRACKED (ZONE 500) · airframe 113,526 hrs · 33,048 cycles

DURING AIRCRAFT C22 CHECK, 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 REPAIR IS FOR THE CRACK DAMAGE CONTAINED WITHIN THE RADIUS AND ON THE FLANGE ONLY, HOWEVER, A 2ND CRACK COMING IS EVIDENT ON THE VERTICAL WEB. THE REFERENCE SRM CUTOUT IS ALSO LIMITED ON THE FLANGE ONLY. SEE FIGURE 2 FOR DETAILS. CPZ AND ABX ENGINEERING CONTACTED FLIGHT VEHICLES CONSULTING INC. REQUESTING AN APPROVED REPAIR SOLUTION FOR THE DAMAGE REPORTED ABOVE. REPAIR WAS COMPLETED PER FVCI EO#23020-4. VENDOR DID NOT REPORT REPAIR TO ABX AIR. THIS WAS DICOVERED BY AN FAA AUDIT OF THE VENDOR.

Part: FRAME — DENTED (WING TO BODY FAI) · airframe 113,526 hrs · 33,048 cycles

DURING THE MAINTENANCE AIRCRAFT INSPECTION, A DENT DAMAGE WAS FOUND ON THE WTB UNDERWING STRUCTURE FAIRING FRAME (19T7300-5) APPROXIMATELY AT BS 779. THE DENT DAMAGE IS ON AREA WHERE NO DAMAGE IS ALLOWED. FOR DENT DETAILS SEE FIGURE 2 AND FIGURE 3. CPZ AND ABX ENGINEERING CONTACTED FLIGHT VEHICLES CONSULTING INC. REQUESTING AN APPROVED REPAIR SOLUTION FOR THE DAMAGE REPORTED ABOVE. REPAIR WAS COMPLETED PER FVCI EO#23020-3. VENDOR DID NOT REPORT REPAIR TO ABX AIR. THIS WAS DICOVERED BY AN FAA AUDIT OF THE VENDOR.

Part: UNKNOWN — CORRODED · corrosion level 2 · airframe 113,526 hrs · 33,048 cycles

DURING C22 MAINTENANCE CHECK AT HAECO AMERICAS, MAINTENANCE REPORTED SEVERE CORROSION DAMAGES ON THE FWD. CARGO LOWER SILL OUTER CHORD (143T8205-3). MAINTENANCE AND CUSTOMER OPTED TO REPLACE THE SUBJECT CHORD AND REQUIRED A SUBSTANTIAL WORK (FASTENERS AND PARTS REMOVAL) FROM BS 412 TO BS 654+44. DUE TO AMOUNT AND SIZE OF STRUCTURES TO BE REMOVED, THE AIRCRAFT REQUIRED TO BE JACK AND SHORED. HAECO AND BOEING ENGINEERING WERE CONSULTED ON REPAIR PROCEDURE. REPAIRED PER ABX-REA-5330-64885-00. VENDOR DID NOT REPORT REPAIR TO ABX AIR. THIS WAS DICOVERED BY AN FAA AUDIT OF THE VENDOR.

Part: SKIN — CORRODED · airframe 113,514 hrs · 33,043 cycles

DURING C22 MAINTENANCE CHECK AT HAECO AMERICAS, WHILE ACCOMPLISHMENT OF SRM 53-00-01, FIGURE 201, REPAIR 12, MAINTENANCE STATED THAT FASTENERS (AT FRAME/SHEAR-TIE LOCATIONS, STA. 1395 AND STA. 1417) ON THE LOWER SKIN IS TOO CLOSE TO THE EDGE OF THE UPPER SKIN MAKING HOLES ON REFERENCED SRM (-3) FILLER TO HAVE NO EDGE MARGINS ON THE HOLES. THE SRM REQUIRES A MINIMUM OF 2D EDGE MARGIN. REFERENCE PARA. SRM 2.F. STATED TO HAVE A MINIMUM OF 2D EDGE MARGINS ON “ALL” REPAIR PARTS. ALSO, SRM PARA. 2.D., STATED 4D-6D SPACING. REPAIR WAS COMPLETED PER ABX-REA-5360-64927-00.

Part: CAM — CORRODED (ZONE 800) · airframe 113,526 hrs · 33,048 cycles

DURING C CHECK IT WAS DISCOVERED THAT MAIN CARGO DOOR LATCH CAMS #1,2,6,11 AND 12 HAVE PITTING CORROSION. CORROSION WAS CLEANED UP IAW B767 SRM 51-10-02. ALL LATCH CAMS WERE FOUND TO BE IN LIMITS PER IAI SERVICE BULLETIN 368-53-049. LATCH CAMS 3,7,8 AND 9 FAILED DIMENSIONAL CHECK AND WERE REPLACED.

Part: SKIN — CORRODED (ZONE 600) · corrosion level 2 · airframe 113,514 hrs · 33,043 cycles

DURING C22 MAINTENANCE CHECK AT HAECO AMERICAS, MAINTENANCE FOUND CORROSION DAMAGE ON THE RH WING LOWER SKIN PANEL NO. 3 APPROX., INBOARD OF WS 176.69 BETWEEN STR 11 AND STR 12. THE CORROSION DAMAGE WAS REMOVED BY BLENDING AFFECTED AREA WITH MINIMUM REMAINING MATERIAL OF 0.478” INCHES FROM INITIAL THICKNESS (CLOSEST TO DAMAGE WITHOUT BLEND) OF 0.545” INCHES, WITH MATERIAL LOSS OF 0.067” INCHES 12.3% MATERIAL REMOVED. THE MATERIAL LOSS OF 0.067” INCHES IS FOUND TO BE OUT OF LIMITS PER SRM 57-20-01. THERE IS NO APPLICABLE REPAIR IN SRM. FCVI WAS CONTACTED FOR REPAIR EVALUATION. REPAIR COMPLETED PER ABX-REA-5725-64884-00

Part: SKIN — CORRODED (ZONE 100) · airframe 113,514 hrs · 33,043 cycles

DURING C22 MAINTENANCE CHECK AT HAECO AMERICAS, MAINTENANCE FOUND GOUGE DAMAGE ON THE FUSELAGE SKIN THAT EXTENDS ONTO AN EXISTING SKIN REPAIR WHICH WAS INSTALLED PER ABX REA B653-61017-MR. THE EXISTING REPAIR WAS REMOVED, DAMAGES ON THE SKIN WERE REMOVED AND FOUND WITHIN LIMITS PER SRM 53-00-01, ALLOWABLE DAMAGE 1. THE EXISTING DAMAGE WAS REPAIRED PER ABX REA B653-61017-MR

Part: SKIN — CORRODED (HORIZONTAL STAB) · corrosion level 3 · airframe 113,144 hrs · 32,917 cycles

WHILE AIRCRAFT WAS IN FOR SCHEDULED PAINT. CORROSION WAS DISCOVERED ON UPPER L/H HORIZONTAL STABILIZER. CORROSION ON LH HORIZONTAL INNER SPAR, TOP SURFACE, TRAILING EDGE IS APPROX. SIX FEET IN FROM OUTBD EDGE OF ELEVATOR, CORROSION IS APPROX. 6" TO 10" IN LENGTH. CORROSION WAS FOUND TO BE OUT OF LIMITS. AIRCRAFT WAS REPAIRED IAW ABX-REA-5510-64771-00 AND RETURNED TO SERVICE.

Part: ACTUATOR — LEAKING (SPOILER) · airframe 113,097 hrs · 32,898 cycles

HYDRAULIC FLUID QUANTITY INDICATING SYSTEM READS ZERO. HYD QTY LIGHT ON. EICAS MESSAGE DISPLAYED C HYD QUANTITY. LOW PRESSURE LIGHT IS ON. AIRCRAFT DIVERTED TO JFK AND LANDED WITHOUT FURTHER INCIDENCE. AIRCRAFT WAS GROUNDED BY MAINTENANCE. MAINTENANCE FOUND SPOILER PCA NO.10 LEAKING, R&R'D NO.10 PCA PER AMM 27-61-02. OPS CHK NORMAL. SERVICED HYD SYSTEM PER AMM 12-12-01. OPERATED ALL FLIGHT CONTROLS OK, NO LEAKS NOTED. A/C REMAINS ETOPS 180. AICRAFT RETURNED TO SERVICE.

Part: O-RING — FAILED (SPOILER PCU) · airframe 113,050 hrs · 32,882 cycles

AFTER ENG START C HYD QTY EICAS ILLUMINATED AND THE HYD QTY DECREASED TO .11 ON CENTER SYSTEM. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE FOUND #10 SPOILER PCA FILTER HOUSING O-RING BLOWN, REMOVED AND REPLACED FILTER HOUSING O-RINGS IAW B767 AMM 27-61-02-434-060. LEAK CHECK GOOD CODE 600-4-D OPS CHECKS GOOD CENTER HYD SERVICED TO FULL IAW B767 MM 12-12-01. AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — VIBRATION (MLG) · airframe 113,025 hrs · 32,873 cycles

BAD VIBRATION ON TAXI AND TAKEOFF, ABORTED TAKEOFF.PERFORMED VISUAL INSPECTION OF NOSE AND MAIN TIRES, NO FLAT SPOTS NOTICED PERFORMED INSPECTION OF BRAKES NO PUCK DAMAGE NO LEAKS WERE NOTICED. PERFORMED OPERATIONAL TEST OF BRAKES WITH CENTER AND RIGHT HYDRAULIC SYSTEM FOUND NORMAL. PERFORMED ANTI SKID AUTO BRAKE TEST IAW AMM 32-41-00 CKD NORMAL ALL VISUAL INSP WERE GUIDED PER AMM 32-45-00. AIRCRAFT RETURNED TO SERVICE.

Part: CONTROLLER — FAULTED (CABIN PRESSURE) · airframe 113,001 hrs · 32,873 cycles

CABIN ALT WARNING EICAS @ 330.AIRCRAFT TURNED BACK TO MIAMI AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE GROUNDED AIRCRAFT. MAINTENANCE REMOVED AND REPLACED AUTOMATIC CABIN PRESSURE CONTROLLER IAW B767 AMM 21-31-02. BITE TEST NORMAL. (CONTROLLER #2) PART EFFECTIVITY VERIFIED. A/C REMAINS ETOPS 180. AIRCRAFT RETURNED TO SERVICE

Part: WIRE — BROKEN (ACCUMULATOR) · airframe 112,830 hrs · 32,814 cycles

LEFT HYD SYS PRESSURES EICAS, L HYD SYSTEM PRESSURE SYS LIGHT AND L PRIMARY ENGINE CAUTION LIGHT ON, STRONG ELECTRICAL SMELL FOLLOWED. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE FOUND A BROKEN WIRE IN LEFT PYLON GOING TO ACMP. REPAIRED BROKEN WIRE FOR L/H ACMP IAW B767 SWPM 20-30-13. REPOSITION HARNESS IAW B767 SWPM 20-10-11 PERFORMED OPS CHECK OF L/H ACMP IAW B767 AMM 29-11-00 OPS CHECK GOOD NO DEFECTS NOTED REPAIRED WIRE IS W290-008-6/AL

Part: CONTROLLER — INOPERATIVE (RT A/C PACK) · airframe 112,800 hrs · 32,804 cycles

R PACK INOP LIGHT EICAS MSG AND OVERHEAD. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE FOUND PRV CONTROLLER INOP. PRV CONTROLLER REPLACED IAW AMM 36-11-19/401 TESTED OK ENGINE RUN PERFORMED NO LEAK FOUND AIRCRAFT RELEASED ETOPS 180, AIRCRAFT RETURNED TO SERVICE.

Part: NONE — NONE (ZONE 100) · airframe 111,572 hrs · 32,461 cycles

AFTER ENGINE START: R AUX PITOT EICAS MESSAGE, AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE REMOVED AND REPLACED R/H AUX PITOT PROBE IAW B767 AMM 34-11-01 OPS AND LEAK CHECK GOOD. REMOVED AND REPLACED K243 IAW WDM 30-31-13. OPS CHECK GOOD. A/C REMAINS RVSM COMPLIANT. AIRCRAFT RETURNED TO SERVICE.

Part: NOT REPORTED — NOT REPORTED · airframe 111,514 hrs · 32,440 cycles

NO IGNITION DURING ENGINE START ON RIGHT ENGINE. PERFORMED ADVERTED STARTED AND 2ND ATTEMPT PROCEDURE WITH NO IGNITION. AIRCRAFT BACK TO BLOCK AND GROUNCED BY MAINTENANCE. MAINTENANCE RAN #2 ENG USING IGNITION #2. ENG RUN NORMAL PER AMM 74-00-00. PLACED RT ENG #1 IGNITION ON DI. PER MEL 74-00-1B CATC PLACARD INSTALLED. MBCB 3/4/22, A/C REMAINS NO ETOPS. AIRCRAFT RETURNED TO SERVICE.

Part: EXCITER — FAULTY (RIGHT ENGINE) · airframe 111,483 hrs · 32,432 cycles

NO LIGHT OFF ENGINE 2, ACCOMPLISHED ABORTED ENGINE START CHECKLIST. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE REMOVED AND REPLACED THE RIGHT ENGINE #1 EXCITER, REF B767 AMM 74-11-01, CONDUCTED ENGINE START WITH #1 IGNITION. START SUCCESSFUL PER ABX ERU/TAXI CHECKLIST. AIRCRAFT RETURNED TO SERVICE.

Part: HOSE — LEAKING (ZONE 700) · airframe 111,360 hrs · 32,385 cycles

RT HYD SYS PRESS EICAS MSG DURING TAXI OUT. RETURNED TO GATE AND WAS GROUNDED BY MAINTENANCE. MAINTENANCE FOUND #3 BRAKE HOSE LEAKING.REMOVED AND REPLACED #3 BRAKE HOSE IAW AMM 32-41-15 NO LEAKS NOTICED. INSTALLED TEMPORALLY LINE FROM HYDRAULIC KIT P/N 24600100360. AIRCRAFT RETURNED TO SERVICE.

Part: SHUTOFF VALVE — STUCK (TE FLAP SYSTEM) · airframe 110,948 hrs · 32,257 cycles

ON TAKE OFF, TRAILING EDGE FLAP DISAGREE EICAS MSG WHILE MOVING FLAPS FROM 5 TO 1. FOLLOWED QRH PROCEDURE. FLAP WORKED FINE ELECTRICALLY. AIR TURNBACK. LANDED WITHOUT FURTHER INCIDENCE. AIRCRAFT GROUNDED BY MAINTENANCE. MAINTENANCE FOUND THE FLAP/SLAT SHUTOFF VALVE STICKING DURING OPERATION. REMOVED AND REPLACED FLAP/SLAT SHUT OF FVALVE IAW B767 AMM 27-57-48. OPS CHECK GOOD. VERIFIED FLAP/SLAT MOVEMENT MULTIPLE TIMES. MOVED FLAP HANDLE ONE DETENT AT A TIME AND FROM 0 TO 30. NO ISSUE PRESENT. RAN FLAPS ELECTRICALLY WITH NO ISSUES. NO LEAKS NOTED. A/C RELEASED CAT I PENDING MCDP 30/40 TEST. THE AIRCRAFT WAS RETURNED TO SERVICE FOLLOWING A SUCCESSFUL TEST FLIGHT.

Part: CIRCUIT BREAKER — TRIPPED (SPEED BRAKE) · airframe 110,483 hrs · 32,085 cycles

AUTO SPEED BRAKE CAUTION AFTER ENGINE START. C/B POPPED. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE PERFORMED OPERATIONAL TEST OF THE AUTO-SPEED BRAKE SYSTEM IAW AMM 27-62-00, OPS NORMAL, AIRCRAFT RELEASED FOR FLIGHT.

Part: SENSOR — OUT OF TOLERANCE (RT A/C PACK) · airframe 109,516 hrs · 31,797 cycles

RIGHT PACK TEMP EICAS MESSAGE ILLUMINATED, AICRAFT BACK TO GATE AND TAKEN OUT OF SERVICE BY MAINTENANCE. REPLACED TEMP SENSOR TS199 IAW AMM 21-58-08 POST INSTALLATION TEST NORMAL R PACK TEMP CONTROL OPS CHECK OK IAW AMM 21-51-00/501 A/C UPGRADED TO ETOPS 180 PLACARD REMOVED

Part: MODULE — INTERMITTENT (ZONE 100) · airframe 109,450 hrs · 31,778 cycles

AILERON LOCK-OUT EICAS MSG AFTER LEAVING BLOCKS. BACK TO BLOCK AND AIRCRAFT WAS GROUNDED. MAINTENANCE REMOVED AND REPLACED RH SAM.AIRCRAFT IAW B767 AMM 27-11-02 WAS RETURNED BACK TO SERVICE.

Part: BLEED VALVE — RUPTURED (RT ENGINE) · airframe 109,120 hrs · 31,681 cycles

RIGHT ENGINE BLEED VALVE WON’T OPEN, NO AIRFLOW, "RT ENG BLEED" LIGHT ILLUMINATED, AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. FOUND RIGHT ENGINE PRV STUCK IN THE CLOSED POSITION, FAILED THUMB TEST. SWAPPED RT PRV AND HPSOV IAW B767 AMM 36-11-18. TRANSFERRED RT ENGINE PRV SYSTEMS IN THE INOPERATIVE OPEN POSITION TO DI IAW MEL 36-11-8-1-1A. ACCOMPLISHED MEL PM 36-11-8-3,78-31-1,36-12-2 AND 36-11-2. A/C RELEASED CAT IIIA, REALM PLACARD ROTATED. A/C DOWNGRADES TO ETOPS 120. LP 38152-07/1

Part: HYDRAULIC LINE — LEAKING · airframe 109,090 hrs · 31,674 cycles

UPON A CAT 3 LANDING , AT LEIPZIG, LOSS OF CENTER HYDRAULIC QUANTITY. ABLE TO EXIT AT A4. SLUGGISH RESPONSE TO BRAKES AND NOSE WHEEL STEERING ELECTED NOT TO FURTHER TAXI, HELD SHORT OF TAXIWAY C. AIRCRAFT TOWED BACK TO GATE. MAINTENANCE FOUND TAIL SKID HYDRAULIC LEAK. AIRCRAFT WAS GROUNDED. REA FOR LEAK REPAIR WAS ISSUED, AIRCRAFT WAS RELEASED.

Part: PRESSURE SWITCH — INTERMITTENT (RT YAW DAMPER) · airframe 108,983 hrs · 31,647 cycles

RUDDER RATIO LIGHT AND EICAS MESSAGE AFTER ENGINE START. BTB AND GROUNDED. RIGHT YAW DAMPER MODULE FAULTED LEFT HYD SWITCH. REMOVED AND REPLACED S27 HYD PRESS SWITCH, IAW B767 AMM 27-11-17. OPERATIONS AND LEAK CHECK GOOD. RAN ENGINE, IAW B767-10A. NO DEFECTS NOTED.

Part: SWITCH — STICKING (RUDDER) · airframe 108,983 hrs · 31,647 cycles

RUDDER RATIO EICAS MESSAGE AND LIGHT. AIRCRAFT BTB. AND GROUNDED. FOUND PCA FAULT ON BOTH MODULES. DISCOVERED TAIL HYDRAULIC CUT OFF SWITCH KORRY SWITCH UNLATCHED. REPLACED KORRY LENS MODULE, IAW B767 SWPM 20-84-14. RUDDER RATIO RESET AND PASSES TEST, AS PER B767 FIM 27-21 FT 804.

Part: SKIN — DENTED (LT WING SLAT) · airframe 108,756 hrs · 31,582 cycles

NR 1 SLAT DAMAGED BY BOARDING STAND ON TAXI OUT. DAMAGE WAS OBSERVED BY GROUND CREW. THEY CALLED MANAGEMENT AND MANAGEMENT NOTIFIED TOWER. TOWER NOTIFIED FLIGHT CREW AND THE CREW PERFORMED AIR TURN BACK INTO CVG. MAINTENANCE OBSERVED DAMAGE TO NR 1 SLAT AND SLAT FAIRING PANELS. THE AIRCRAFT WAS GROUNDED. MAINTENANCE REPLACED NR 1 SLAT, IAW AMM 27-81-02 AND THE SLAT FAIRINGS WERE REPAIRED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — GOUGED (RT WING TE FLAP) · airframe 108,467 hrs · 31,467 cycles

DURING AIRCRAFT C-CHECK AT TAMPA, MAINTENANCE DISCOVERED A GOUGE ON THE UPPER OUTER SKIN (P/N 113T3140-5) OF THE RT WING OUTBOARD FLAP AT OTEF STA 83.72. THE GOUGE WAS REMOVED BY LOCALIZED BLENDING, PER 767-300 SRM 57-53-01, EXCEEDING PUBLISH LIMITS. ALL FASTENERS COMMON TO THE REWORKED AREA, AS REQUIRED, WERE REMOVED. HFEC OPEN-HOLE AND SURFACE SCAN INSPECTIONS WERE ACCOMPLISHED, PER 767 NTM MANUAL PART 6, WITH NO DEFECTS REPORTED. AN ULTRASONIC (UT) INSPECTION WAS ACCOMPLISHED TO DETERMINE THE MINIMAL REMAINING MATERIAL THICKNESS, AND RESULTS WERE RECORDED IN A 0.50 X 0.50 GRID PATTERN AS SHOWN IN FIGURE 2. THE UPPER OUTER SKIN IS FABRICATED FROM 0.125 THICK 7075-T6 ALUMINUM SHEET, PER QQ-A-250/12. THIS REA ACCOMPLISHES THE PERMANENT REPAIR OF THE UPPER OUTER SKIN, REF ABX-REA-2750-64104-00 AND FAA FORM 8110-3 ABX-REA-2750-64104-00.

Part: WARNING MESSAGE — FALSE ACTIVATION (SPOILERS) · airframe 108,182 hrs · 31,354 cycles

SPOILER EICAS MESSAGE APPEARED AND SPOILER DISCREET LIGHT ILLUMINATED AIRCRAFT WAS GROUNDED. PERFORMED FIM TASK 27-09 FT 809. RESET SPOILER MODULE 1 LEFT AND MESSAGE AND LIGHT CLEARED. SPOILERS OPS CHECK OKAY.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 107,658 hrs · 31,123 cycles

RIGHT SIDE BRACE EICAS. GEAR HANDLE DOWN, NO RIGHT GREEN LIGHT AND GEAR DISCREET LIGHT. CONFIGURATION AND GEAR NOT DOWN EICAS MESSAGE. AIRCRAFT WAS GROUNDED.

Part: UNKNOWN — ODOR · airframe 107,294 hrs · 30,952 cycles

STRONG SMELL OF ELECTRICAL ODOR (SMOKE LIKE IN NATURE). THAT LASTED APPROX. 2 MINUTES AT THE TIME THE AUTO-PILOT DISCONNECTED. THE AIRPLANE WAS GROUNDED. CAUSE OF ODOR IS UNKNOWN.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 105,907 hrs · 30,322 cycles

DURING THE DESCENT INTO HRL, THE CREW SMELLED A STRONG ELECTRICAL ODOR WHICH LASTED ABOUT FIVE MINUTES. THE AIRPLANE WAS REMOVED FROM SERVICE (GROUNDED) AND THE MAIN EQUIPMENT CENTER, MAIN CARGO COMPARTMENT, FLIGHT DECK, AND GALLEY WERE INSPECTED. NO ABNORMALITIES WERE FOUND. THE CAUSE OF THE ODOR IS UNKNOWN.

Part: SKIN — DENTED (RT WING SPOILER) · airframe 104,399 hrs · 29,680 cycles

DENT ON THE RIGHT WING NUMBER 8 SPOILER, LOWER SURFACE SKIN. THE SKIN WAS REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: STIFFENER — CORRODED (BS 1065) · airframe 104,399 hrs · 29,680 cycles

CORROSION ON THE WHEEL WELL BULKHEAD HORIZONTAL STIFFENER NUMBER 7 AT FUSELAGE STATION 1065. THE STIFFENER WAS REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: SKIN — CORRODED (BS 1490) · airframe 104,399 hrs · 29,680 cycles

CORROSION ON THE FUSELAGE SKIN AT STATION 1490 UNDER THE BULK CARGO EXTERIOR FLOODLIGHT HOUSING. THE SKIN WAS REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: SKIN — CRACKED (LT WING SLAT) · airframe 104,399 hrs · 29,680 cycles

CRACK AND CORROSION ON THE LEFT WING NUMBER 2 LEADING EDGE SLAT, OUTBOARD LOWER SKIN. THE SKIN WAS REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: SKIN — CORRODED (RT WING SLAT) · airframe 104,399 hrs · 29,680 cycles

CORROSION ON THE RIGHT WING NUMBER 9 SLAT LEADING EDGE SKIN. THE SKIN WAS REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: SKIN — CRACKED (BS 347) · airframe 104,399 hrs · 29,680 cycles

R1 DOOR SILL, FUSELAGE SKIN AT LOWER AFT EXTERIOR CORNER HAS CRACK INDICATION. THE SKIN WAS REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: MODULE — ODOR (GALLEY) · airframe 104,305 hrs · 29,638 cycles

DURING TAXI TO THE RUNWAY, THE CREW SMELLED A SULFUR/WOOD SMOKE IN THE FLIGHT DECK. THE AIRPLANE WAS REMOVED FROM SERVICE (GROUNDED) AND THE MAINTENANCE TECHNICIAN NOTICED AN ODOR IN THE GALLEY. THE OVEN/HOT CUP MODULE WAS REPLACED. THE CAUSE FOR THE ODOR WAS A FAULTY OVEN/HOT CUP MODULE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 100,605 hrs · 27,972 cycles

THE FLIGHT CREW REPORTED A STRONG HOT METAL TYPE OF ODOR DURING TAKEOFF AND CRUISE. THE ODOR WOULD LAST A MINUTE OR TWO, THEN DISSIPATE. NO SMOKE WAS OBSERVED. THE AIRPLANE WAS REMOVED FROM SERVICE AND THE MAIN EQUIPMENT CENTER WAS INSPECTED. THERE WAS NO EVIDENCE OF BURNT COMPONENTS. THE COOLING PACK SYSTEM WAS RUN WITH NO ODORS OBSERVED. THE CAUSE OF THE ODOR WAS NOT FOUND.

Part: BULKHEAD WEB — CRACKED (BS 995) · airframe 100,498 hrs · 27,925 cycles

CANTED PRESSURE WEB IS CRACKED AT STATION 995 IN MAIN CABIN UNDER FLOOR. REPAIRED MAIN CABIN FLOOR PRESSURE WEB AT STATION 995 IN ACCORDANCE WITH REO G20250 REV 8 AND ABX REA B653-62043MR. SDR INFO: CRACKED, 11", PART NUMBER: 145T8755-19, SERIAL NUMBER: NSN, PART NAME: WEB, LOCATION: STA 995. AIRCRAFT WAS GROUNDED.

Part: TRANSFORMER — DEFECTIVE (CARGO BAY) · airframe 100,450 hrs · 27,900 cycles

5 OUT OF 6 FORWARD LOWER CARGO DOOR SILL AREA LIGHTS DO NOT ILLUMINATE DURING CARGO LOADING OPERATIONS. AT THE FORWARD UPPER SILL LIGHT POSITION, SMOKE WAS FOUND AT A BURNED WIRE. THE FORWARD UPPER LIGHT ASSEMBLY WAS REMOVED AND FOUND 4 WIRES BURNED, 2 SHORTED TOGETHER, AND 2 TERMINAL ENDS WERE BURNED OFF. ALSO, FOUND CIRCUIT BREAKER C21, TERMINAL 2 BURNED. THE CORRECTIVE ACTION ACCOMPLISHED WAS REMOVING & REPAIRING THE BURNED WIRING, REPLACING THE TERMINALS, AND REPLACING THE FORWARD CARGO COMPARTMENT LIGHTS TRANSFORMER T148. THE SUSPECTED CAUSE OF THE INOPERATIVE LIGHTS AND BURNED WIRING IS A FAULTY TRANSFORMER T148.

Part: SKIN — DAMAGED (HORIZONTAL STAB) · airframe 100,115 hrs · 27,758 cycles

LOWER HORIZONTAL SKIN DAMAGED. AIRCRAFT WAS GROUNDED. REPAIRED AREA IAW SRM 51-70-10 AND REA-8655-62114-MR.

Part: SKIN — DAMAGED (HORIZONTAL STAB) · airframe 100,115 hrs · 27,758 cycles

LOWER HORIZONTAL STAB HAS SKIN DAMAGE. AIRCRAFT WAS GROUNDED. REMOVED DAMAGE AND REPAIRED AREA IAW SRM 51-70-10 & REA-8655-62114-MR.

Part: SKIN — DAMAGED (HORIZONTAL STAB) · airframe 100,115 hrs · 27,758 cycles

LOWER HORIZONTAL SKIN DAMAGED. AIRCRAFT WAS GROUNDED. REPAIRED THE AREA IAW SRM 51-70-10 & REA-8655-62114-MR. RESTORED FINISH IAW AMM 51-21-10.

Part: SUPPORT — CORRODED (RT WING) · corrosion level 2 · airframe 97,593 hrs · 26,822 cycles

NUMBER 7 FLAP SUPPORT 1-2-3 BEAM HAS 5 HOLES WITH DEFECT INDICATIONS & 1 HOLE WITH DEFECT INDICATION & IS OUT OF ROUND, FOUND ON HFEC ROTARY SCAN. REAMED DISCREPANT HOLES ROUND & TONE, PERFORMED HFEC WITH NO INDICATION. REA NR C057-61559-MR WAS ISSUED, ALL DISCREPANT HOLES WERE REWORKED IAW REA C057-61559 WORK STEPS 1-7. SDR INFO, CORRODED LEVEL 2, PN 113T1499-12, SN ABX W028, PART NAME NR 7 FLAP SUPPORT 1-2-3 BEAM, WS LOCATION FROM 600 RT. ACFT WAS GNDED.

Part: SUPPORT — CORRODED (RT WING) · corrosion level 2 · airframe 97,593 hrs · 26,822 cycles

DISCREPANT HOLE REAMED TO 0.499" FROM INITIAL 0.438", PERFORMED HFEC WITH NO FURTHER DEFECT INDICATIONS. REA NR C057-61570-MR ISSUED TO FABRICATION REPAIR OF BUSHING & WASHERS. WORK STEPS 1-11 OF REA COMPLIED WITH. FOR DETAILS REF SRM 51-40-05 FOR REAMING OF DISCREPANT HOLE. SDR INFO, CORRODED LEVEL 2, PN 113T1498-8, SN ABX W03, PART NAME NR 8 FLAP SUPPORT 1-2-3 BEAM, WS LOCATION FROM WS 798 RT. ACFT WAS GNDED.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 97,593 hrs · 26,822 cycles

FUSELAGE SKIN AT LOWER VHF ANTENNA LOCATION HAS A SCRIBE LINE THE ENTIRE PERIPHERY OF THE ANTENNA. REPAIRED FUSELAGE SKIN AT LOWER VHF ANTENNA IAW SRM 53-60-01 REPAIR & REA B-653-61554-MR. SDR INFO, PN 146T3261-1, PART NAME SKIN, SN NSN, FS LOCATION FROM 1197 & 95, STRINGER LOCATION 39L - 39R. ACFT WAS GNDED.

Part: SUPPORT RIB — CORRODED (LT WING) · corrosion level 2 · airframe 97,593 hrs · 26,822 cycles

NUMBER 1 FLAP SUPPORT 1-2-3 BEAM HAS 7 HOLES WITH DEFECT INDICATIONS ON HFEC ROTARY SCAN. HOLES REPAIRED FOR REA C057-61565-MR. SDR INFO, LEVEL 2, PN 113T1498-7, PART NAME NR 1 FLAP SUPPORT 1-2-3 BEAM, SN ABX V965, WS LOCATION FROM WS 798 LT. ACFT WAS GNDED.

Part: SUPPORT — CORRODED (LT WING) · corrosion level 2 · airframe 97,593 hrs · 26,822 cycles

NUMBER 2 FLAP SUPPORT 1-2-3 BEAM HAS 2 HOLES WITH DEFECT INDICATIONS WITH HFEC ROTARY SCAN. HOLES FOR NR 2 FLAP SUPPORT 1-2-3 BEAM REPAIRED IAW REA C057-61571-MR AS REQUIRED. SDR INFO, LEVEL 2, PN 113T1499-11, PART NAME NR 2 FLAP SUPPORT 1-2-3 BEAM, SN ABX V974, WS LOCATION FROM WS 600 LT. ACFT WAS GNDED.

Part: SUPPORT RIB — CORRODED (LT WING) · corrosion level 2 · airframe 97,593 hrs · 26,822 cycles

NUMBER 1 FLAP SUPPORT INBD FLANGE HAS 2 ROTARY ACTUATOR HOLES WITH DEFECT INDICATIONS ON HFEC ROTARY SCAN, HOLES ARE AT 10:00 AND 10:30 LOCATIONS LOOKING OTBD. AFTER CLEANING & RE-CANNING DISCREPANT HOLE AT 10:00 POSITION, NO FURTHER DEFECTS NOTED. REA B 657-61551 ISSUED FOR DISCREPANT HOLE AT THE 10:30 POSITION. REAMED HOLE RE-SCANNED WITH NO DEFECTS NOTED. INSTALLED FREEZE PLUG REAMED TO 0.4425" IAW REA WORK STEPS. SDR, CORROSION LEVEL 2, PN 113T1323-35, PART NAME SUPPORT RIB, SN NSN, LOCATION: AT WS 798.2. ACFT WAS GNDED.

Part: SUPPORT RIB — CORRODED (LT WING) · corrosion level 2 · airframe 97,593 hrs · 26,822 cycles

NUMBER 2 FLAP OTBD SUPPORT HAS 1 ROTARY ACTUATOR HOLE WITH A DEFECT INDICATION ON HFEC ROTARY SCAN, HOLE IS LOCATED AT 2:00 LOOKING OTBD. REA B657-61551 ISSUED, REMOVED DISCREPANT HOLE, RE-SCANNED, NO DEFECTS NOTED. INSTALLED FREEZE PLUG & REAMED TO 1.380" IAW REA WORK STEPS. SDR, CORRODED LEVEL 2, PN 113T1324-29, PART NAME SUPPORT RIB, SN NSN, LOCATION: AT WS 616.2. ACFT WAS GNDED.

Part: SKIN — CRACKED (FUSELAGE) · airframe 97,593 hrs · 26,822 cycles

ELT ANTENNA LOCATION, SKIN HAS HFEC CRACK INDICATION AT MID OTBD ANTENNA MOUNT HOLE. REPAIRED ELT ANTENNA SKIN AT MID OTBD ANTENNA MOUNT HOLE IAW EWO NR 57133-0000-0005 & SRM 53-00-01 REPAIR 14. SDR INFO, PN 146T1331-1, PART NAME SKIN, SN NSN, CRACKED .200, EXACT FS LOC ON ACFT FS 1510 - 1511, EXACT STRINGER LOC ON ACFT STRINGER 2L - 3L. ACFT WAS GNDED.

Part: SKIN — CHAFED (FUSELAGE) · corrosion level 2 · airframe 97,593 hrs · 26,822 cycles

VERTICAL STABILIZER ACCESS 324AL FUSELAGE MOUNTED FWD & AFT FLANGE COMMON TO PANEL MATING SURFACE CHAFED. R & R SKIN FAIRING IAW SRM 51-40-05 & 51-40-02. APPLIED PROTECTIVE COATINGS IAW SRM 51-20-01. APPLIED TOP COAT IAW AMM 51-21-10. SDR INFO, CORRODED PN 148T7501417, PART NAME SKIN FAIRING, LOCATION 1740 - 1746, STRINGER LOCATION 1L TO 1L. ACFT WAS GNDED.

Part: SKIN — CRACKED (FUSELAGE) · airframe 97,593 hrs · 26,822 cycles

RIGHT FUSELAGE EXTERNAL SKIN CRACKED AROUND TWO FASTENERS IN SECTION 48B, STATION 654.5 BETWEEN STRINGER 3R & 4R. REPAIRED CRACKED SKIN ON EXTERNAL FUSELAGE AT STATION 1654 IAW SRM 53-00-01. SDR INFO, PN 148T3121, PART NAME FUSELAGE SKIN, SN NSN, CRACKED LENGTH .500". ACFT WAS GNDED.

Part: SKIN — PUNCTURED (FUSELAGE) · airframe 95,194 hrs · 25,885 cycles

THREE INCH SQUARE PUNCTURE THROUGH FUSELAGE SKIN BETWEEN FUSELAGE STATIONS 1373 & 1395 BETWEEN STRINGERS 26R & 27R. REPAIRED IAW SRM 53-00-01, REPAIR 12 WITH SLIGHT DEVIATIONS DUE TO DAMAGE BEING NEAR AN EXTERNAL LIGHT & A BUTT JOINT. .

Part: ENGINE — BIRD INGESTION (RIGHT) · airframe 95,093 hrs · 25,845 cycles

ON TAKEOFF, BIRD STRIKE TO THE RT ENG. HIGH EGT, 1025 DEGREES FOR 2 SECONDS. RT ENG SHUT DOWN, AIR TURN BACK.

Part: WARNING MESSAGE — FALSE ACTIVATION (RT ENG FIRE) · airframe 93,595 hrs · 25,359 cycles

AFTER BLOCKOUT, EICAS MESSAGE RT ENGINE FIRE LP1. PERFORMED RT ENGINE FIRE LP1 OPS CHECKED IAW AMM 23-11-00. EICAS ERASE PROCEDURE IAW AMM 31-41-00-2. NO FURTHER FAULTS NOTED. OPS CHECKED NORMAL.

Part: SKIN — CRACKED (BS 500) · airframe 93,110 hrs · 25,178 cycles

DENT BS 500 S17-18L. SKIN DETERMINED CRACKED. REPAIRED SKIN IAW SRM 53-00-01. REMOVED AND REINSTALLED SIDEWALL PANELS AND KICK PANEL IAW AMM 75-27-09-4 AND REA B653-60595-MR, ACFT WAS GROUNDED.

Part: BEAM — CHAFED (NACELLE) · airframe 93,110 hrs · 25,178 cycles

THREE CHAFED AREAS ON LOWER BEAM AFT OF SECOND PANEL LATCH FOR 437BR. R & R HYD BAY ACCESS DOOR LOWER BEAM IAW SRM 51-40-02. PYLON BEAM INBD.

Part: ATTACH FITTING — CRACKED (VERTICAL STAB) · airframe 93,110 hrs · 25,178 cycles

VERTICAL STABILIZER TO FUSELAGE ATTACHMENT STRUCTURE BETWEEN STAB REAR SPAR AND T/E IS CRACKED ON FWD RT FLANGE ACCESS THROUGH PANEL 324CLX FS 1746. R & R ATTACHED STRUCTURE ANGLE IAW SRM-300 51-40-02. ACFT WAS GROUNDED.

Part: PIN — MISINSTALLED (BRAKE) · airframe 92,800 hrs · 25,055 cycles

LOSS OF NR 2 BRAKE ROD PIN ALLOWED BRAKE ROD TO ROTATE INTO A POSITION THAT PREVENTED LEFT MAIN LANDING GEAR FULL RETRACTION INTO WHEEL WELL. ON LANDING, BRAKE ROTATED WITH WHEEL ASSEMBLY CAUSING FIELD REPAIRABLE DAMAGE TO LEFT MAIN LANDING GEAR. BRAKE ROD PIN LOSS WAS CAUSED BY INCORRECT INSTALLATION OF PIN ASSEMBLY FOR INSTALLED BRAKE CONFIGURATION. AIRCRAFT GROUNDED.

Part: CONTROL PANEL — FAULTY (COCKPIT) · airframe 92,800 hrs · 25,055 cycles

FLIGHT MANAGEMENT COMPUTER SYSTEMS "CDU" FIRST OFFICER, DISPLAY BLANK. SELECTING ALT FMC DID NOT CORRECT FAULT. FIRST OFFICERS FMCS CDU CIRCUIT BREAKER POPPED AND ELECTRIC BURNING SMELL ALSO NOTED. REMOVED AND REPLACED FLIGHT MANAGEMENT PANEL PER AMM 34-61-02. OPS CHECKED GOOD, ACFT WAS GROUNDED.

Part: SMOKE DETECTOR — DEFECTIVE (CARGO BAY) · airframe 91,194 hrs · 24,499 cycles

NR 5A CARGO SMOKE DETECTOR LIGHT IS AMBER. REMOVED AND REPLACED NR 5A SMOKE DETECTOR IAW MM 26-14-01. OPS CHECK GOOD. OPS CHECK GOOD PER AMM 26-14-01, ACFT WAS GROUNDED.

Part: WIRE — ARCED (ZONE 100) · airframe 90,297 hrs · 24,302 cycles

DURING INSPECTION FOUND WIRE W9021-015-16 SHOWING SIGNS OF ARCING. R & R AFFECTED WIRE IAW SWPM.