N760CK

Part: A/C PACK — LOW (ZONE 100) · airframe 94,357 hrs · 27,443 cycles

ON TAXI OUT, NO DUCT PRESSURE WITH BOTH PACKS ON. AIRCRAFT RETURNED TO BLOCKS. MAINTENANCE DEFERRED IAW ABX-49-11-1-1. AIRCRAFT RETURNED TO SERVICE.

Part: WARNING MESSAGE — ILLUMINATED (AILERONS) · airframe 94,271 hrs · 27,403 cycles

ON CLIMB OUT, RECEIVED AILERON LOCKOUT EICAS MESSAGE. AFTER LANDING, MTX DEFERRED AILERON LOCKOUT SYSTEM IAW MEL ABX 27-11-2 PLACARD INSTALED MX PROCEDURES ACCOMPLISHED. AIRCRAFT RETURNED TO SERVICE.

Part: START VALVE — FAULTED (LT ENGINE) · airframe 94,050 hrs · 27,274 cycles

ON TAXI OUT STARTING LH ENGINE LEFT ENGINE START VALVE WOULD NOT OPEN AC RETURNED TO GATE (BTB) MTX GROUNDED AC. MTC CYCLED LT ENG START VALVE OPS NORMAL IAW B767 AMM 80-11-02 A/C REMAINS NO ETOPS AND RETURNED AC TO SERVICE.

Part: CONTROLLER — INOPERATIVE (ZONE 400) · airframe 93,994 hrs · 27,241 cycles

DURING TAXI OUT, NO AIR OFF OF RIGHT ENGINE AFTER ENGINE START,.A/C RETURNED TO GATE (BTB). MTX GROUNDED A/C MTX PERFORMED FIM 36-11 TREE 837, REMOVED AND REPLACED PRC/PRVC IAW B767 AMM 36-11-19 OPS TEST GOOD A/C RELEASED NO ETOPS. AND RETURNED A/C TO SERVICE.

Part: INDICATION SYS — MALFUNCTIONED (FUEL QTY) · airframe 93,885 hrs · 27,184 cycles

FUEL QUANTITY CHANNEL STATUS MSG ON TAXI OUT A/C RETURNED TO THE GATE (BTB) MTX GROUNDED AC AND DEFERRED FUEL QTY FOR DEPARTURE IAW MEL ABX-28-41-1-3-1. MTX RETURNED AC TO SERVICE.

Part: ELEVATOR SYSTEM — FAULTED · airframe 93,885 hrs · 27,184 cycles

DRUING TAXI OUT, LEFT SIDE ELEVATOR DID NOT MOVE ON STATUS PAGE. ACFT RETURNED TO THE GATE. MTX GROUNDED ACFT AND DEFERRED ELEVATOR INDICATION FOR DEPARTURE IAW MEL ABX-27-08-01. MTX RETURNED AC TO SERVICE.

Part: HYDRAULIC SYSTEM — LOW · airframe 93,783 hrs · 27,144 cycles

AFTER ENG START RIGHT HYD QTY DROPPED TO 0.73 WITH RF.AC THEN RETURNED TO THE GATE (BTB) AND MAINTENANCE GROUNDED AC . MTX THEN SERVICED R HYD SYS TO 1.00 IAW AMM 12-12-01. PERFORMED ENGINE RUN ON RIGHT ENGINE RUN ON RIGHT ENGINE IAW AMM 71-00-00. OPS CHECK GOOD NO LEAKS DETECTED. A/C REMAINS NO ETOPS.AND RETURNED AC TO SERVICE .

Part: ELEVATOR SYSTEM — MALFUNCTIONED · airframe 93,772 hrs · 27,141 cycles

DURING TAXI, L ELEVATOR SHOWING NO MOVEMENT DURING BEFORE TAKEOFF CHECKLIST. AIRCRAFT RETURNED TO BLOCKS. (BTB) DEFERRED IAW MEL C ABX-27-08-1. AIRCRAFT RETURNED TO SERVICE.

Part: INDICATOR — MALFUNCTIONED (ELEVATOR) · airframe 93,602 hrs · 27,051 cycles

DURING TAXI OUT, LEFT ELEVATOR INDICATION DOES NOT FOLLOW FLIGHT CONTROL INPUTS. AIRCRAFT RETURNED TO BLOCKS (BTB). DEFERRED IAW MEL 27-08-1. MTX PROCEDURES C/W. PLACARD INSTALLED. MAINTENANCE GAINED ACCESS TO LT ELEVATOR TRANSMITTER, FOUND BIRD NEST. CLEANED AND REMOVED AS NEEDED. CLEANED CANNON PLUG D1858 ON TRANSMITTER IAW SWPM 20-60-01. INDICATION OPS CHECK GOOD AT THIS TIME. DI CLEARED. PLACARD REMOVED. AIRCRAFT RETURNED TO SERVICE.

Part: ELT — MALFUNCTIONED (ZONE 200) · airframe 93,581 hrs · 27,042 cycles

DURING INSPECTION, FROM W/O# 14829897, ELT CHECK FAILED TEST. FOUND 3 AND 2 LOW RF POWER, ELT P/N S1823502-03. KANNAD 406 A5. DEFERRED IAW MEL D ABX-23-24-1-1. C/;W THE REMOVAL AND REPLACEMENT OF THE ELT IAW ABX AIR W/O# 14829897. OPS CHECK GOOD. DI CLEARED. PLACARDS REMOVED. A/C REMAINS NO ETOPS. A/C RETURNED TO SERVICE.

Part: APU — FAULTED (ZONE 100) · airframe 93,508 hrs · 27,008 cycles

ON TAXI OUT, NO DUCT PRESSURE FROM APU. AIRCRAFT RETURNED TO BLOCKS (BTB). MAINTENANCE DEFERRED SYSTEM IAW MEL C ABX-49-11-1-1. RETURNED AIRCRAFT TO SERVICE.

Part: START VALVE — MALFUNCTIONED (ZONE 400) · airframe 93,505 hrs · 27,006 cycles

AFTER PUSH BACK, RH ENGINE NOT STARTING - VALVE LIGHT RH ON ALL THE TIME. A/C RETURNED TO BLOCKS (BTB) AND MTX GROUND A/C. MTX DEFERRED THE RH START VALVE FOR DEPARTURE IAW MEL ABX-80-00-2-1 AND RETURNED A/C TO SERVICE.

Part: START VALVE — FAULTED (RT ENGINE) · airframe 93,492 hrs · 27,001 cycles

DURING TAXI OUT WHILE STARTING RH ENGINE R START VALVE ANNUN ILL WITH ENG START(RH) IN GND THE VALVE LIGHT WILL EXT W/ SWITCH IN AUTO. A/C RETURNED TO GATE (BTB) AND MTX GROUNDED A/C . AND DEFERRED RH START VALVE FOR DEPARTURE AND IAW MEL ABX -80-10-2-1 FOR DEPARTURE AND RETURNED A/C TO SERVICE

Part: WARNING MESSAGE — FALSE INDICATION (SLATS) · airframe 93,238 hrs · 26,840 cycles

DURING FLIGHT CONTROL CHECK ON TAXI L/E SLAT DISAGREE INDICATOR ILLUMINATED WHEN FLAPS 5 WAS SELECTED. THE CREW RETURNED TO BLOCKS. MAINTENANCE GROUNDED THE AIRCRAFT. MAINTENANCE PERFORMED FSEU BITE PROCEDURE WITH NO FAULTS NOTED. PSEU BITE CHECKED AND RESET. FLAPS/SLATS OPERATED SEVERAL TIMES WITH NO FAULTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE IAW FIM 27-51 FT 808.

Part: WARNING MESSAGE — FALSE ACTIVATION (APU) · airframe 93,155 hrs · 26,800 cycles

DURING TAXI CREW REPORTED ,APU DOOR STATUS MESSAGE APPEARED AFTER TAXI A/C RETURNED TO GATE (BTB) AND MTX GROUNDED A/C. MTX PERFORMED TROUBLESHOT IAW FIM 49-11 FAULT TREE 988. NO DEFECTS NOTED. OPS CHECK GOOD.MTX REURED A/C TO SERVICE .

Part: NOT REPORTED — NOT REPORTED (NOT REPORTED) · airframe 92,999 hrs · 26,730 cycles

MCD CLOSED AND LATCHED AND LOCKED BEFORE EACH DEPARTURE. ACFT LEFT BLOCKS WITH NO INSPECTION AND RETURNED TO SATISFY REINSPECT. BEFORE FLIGHT (BTB) VERIFIED MCD CLOSED, LATCHED AND LOCKED IAW B767 ABX REA - 5230-65623-01. DI REMAINS OPEN. AC RETURNED TO SERVICE

Part: BEAR STRAP — GOUGED (ZONE 100) · airframe 84,099 hrs · 21,386 cycles

NN-24:AFTCARGO CONTROL PANEL UPPER BEARSTRAP HAS MARKED GOUGES . DURING AIRCRAFT MAJOR MAINTENANCE VISIT IN OSCODA-WURTSMITH AIRPORT, CORROSION DAMAGE WAS FOUND ON THE INNER SIDE OF AFT CARGO CONTROL PANEL CUTOUT BEARSTRAP AT BSTA 1263 AND BETWEEN STRINGERS S-22R AND S-26R. THE DAMAGE WAS REMOVED BY BLEND OUT TECHNIQUES AND LOWEST BLENDED POINT IS 0.120". THE BLEND OUT IS OUT OF THE _ALLOWABLE SRM LIMITS DUE TO BLEND OUT REMOVED MATERIAL DEPTH ..REPAIR- AFT CARGO CONTROL PANEL BEARSTRAP CUTOUT CORROSION AT STA 1263 BETWEEN STRINGERS S22 AND S26R ACCOMPLISED REPAIR IAW FLIGHT VEHICLES CONSULTING INC. EO.CONTROL # 24159-1 REV.A

Part: SKIN — DAMAGED (ZONE 200) · airframe 92,824 hrs · 26,233 cycles

"DURING CK C5 AT KALITTA EVIDENCE OF LIGHTNING STRIKE ON UPPER HALF FUSELAGE EXTERIOR LEFT APPROX STA 300 AND S-1, TD34 FUSELAGE SKIN PAMAGE AT STRAP WE ARE SEEKING REPAIR OR RELIEF ON THE UPPER FUSELAGE SKIN JUST FORWARD OF STATION 368, WE HAVE TWO BELNDOUTS THAT ARE OUT OF LIMITS BETWEEN STRINGER LR AND 2R THERE IS A REINFORCEMENT STRAP AT STATION 368 AND A LAP SPLICE AT 2R. ACCOMPLISHED REPAIR ON CANTED STA 303 TO 325 BETWEEN STR 2R AND STR 3R IAW FVCI EO CONTROL #24159-3 REV A AND TA# 105547."

Part: SKIN — DAMAGED (ZONE 200) · airframe 92,824 hrs · 26,233 cycles

DURING CK C5 AT KALITTA EVIDENCE OF LIGHTNING STRIKE ON UPPER HALF FUSELAGE EXTERIOR RIGHT APPROX STA 300 AND S-2, TD35 REPAIR - FUSELAGE SKIN (SECTION 41 ), FULLELAGE SKIN REPAIR BETWEEN CANTED STA 303 AND CANTED STA 325, BETWEEN STRINGERS STR-2R AND STR-3R, 8767. ACCOMPLISHED REPAIR OF FUSELAGE SKIN AT CANTED STA 303 BETWEEN STR 1L AND 1R IAW FVCI EO CONTROL# 24159-4 REV IR.

Part: SKIN — DAMAGED (ZONE 200) · airframe 92,824 hrs · 26,233 cycles

DURING CK C5 AT KALITTA EVIDENCE OF LIGHTNING STRIKE ON UPPER HALF FUSELAGE EXTERIOR LEFT APPROX STA 654+110 AND S-1, TD18 WE NEED A REPAIR FOR DAMAGE TO THE UPPER SKIN AND TEAR STRAP. WE CUTOUT DAMAGE ON A SKIN AND TEARSTRAP AT STATION 654+110 BETWEEN STRINGER LR AND 2R FOR REPAIR, AND REQUIRE ENGINEERING DUE TO CLOSENESS TO A LAP SPLICE AND THE CUTTING OF THE TEAR STRAP. THE HOLE CUTOUT IS 1" AND HAS BEEN SURFACE SCANNED AND. IS FREE OF DAMAGE. ALSO WE HAVE A CUTOUT BETWEEN STRINGER LL AND 2L AT APPROXIMATELY STATION 654+93. ACCOMPLISED REPAIR OF UPPER SKIN AT STA 654+110 STR 1L IAW FVCI EO CONTROL # 24159-2 REV IR

Part: RIB — CORRODED (ZONE 600) · airframe 92,824 hrs · 26,233 cycles

"KALITTA AIR FOUND ON THE RH WING FIXED LIE AT ISS 337 .60 SEAL RIB DAMAGED WITH A HOLE IN THE OUTBOARD SIDE OF THE RIB . .THE HOLE IS LOCATED JUST BELOW STIFFENER 114T6120-97. THE SIZE .OF THE HOLE IS 0.450"" BY 0.300"". THICKNESS OF THE RIB AT THE HOLE IS 0.096"".KALITTA AIR HAS ADDED DWG.114T6210 FOR THE INSTALL AT ISS 337.60. KALITTA AIR IS UNABLE TO OBTAIN BOEING PART DWG.114T6211 FOR THE RIB. THIS RIB IS LOCATED JUST I/B OF THE #3 PYLON. REPAIRED IAW FVCI EO CONTROL# 24159-6 REV A STEPS 1 THRU 15 AND 16 THRU 20."

Part: CONTROL PANEL — UNSERVICEABLE (ZONE 200) · airframe 92,735 hrs · 26,586 cycles

DURING TAXI OUT LEFT HYD PRESS LIGHT AND SYS PRESS LIGHT ILLUMINATED ,A/C RETURNED TO GATE AND MTX GROUNDED THE A/C REMOVED AND REPLACED OVERHEAD CONTROL PANEL IAW AMM 29-11-40 OPS CHECK GOOD . A/C WAS RETURNED TO SERVICE .

Part: HYDRAULIC SYSTEM — LOW (RIGHT) · airframe 92,713 hrs · 26,572 cycles

DURING TAXI OUT STOPPED AND  AFTER SETTING BRAKE FOR CROSSBLEED START "RF" APPEARED NEAR RIGHT HYD QUANTITY INDICATOR ON LOWER EICAS A/C RETURNED TO GATE AND MTX GROUNDED A/C . INSPECTED AND VERIFIED NO EXTERNAL HYDRAULIC LEAKS IAW AMM 29-11-00 AND SERVICED RIGHT HAND SYSTEM TO FULL . IAW B 767 AMM 12-12-01 AND A/C DEPARTED.

Part: WARNING MESSAGE — ILLUMINATED (LT ENG STARTER) · airframe 92,652 hrs · 26,545 cycles

DURING LT ENGINE START, STARTER EICAS MSG AND NO N2 ROTATION ON #1 ENGINE. ACCOMPLISHED QRH 7.40. MTX ENTERED THE FLGHT DECK AND THEN EXERCISED VALVE AND OPERATION WAS NORMAL IAW B767 AMM 80-11-00.ENGINE STARTS NORMAMALLY IAW AMM 71-00-00 AC TRURNED TO SERVICE AND DEPARTED .

Part: UNKNOWN — MULTIPLE FAIL (COCKPIT) · airframe 92,375 hrs · 26,355 cycles

DURING TAXI OUT, THE FOLLOWING ABNORMALITIES OCCURRED; BOTH CAPTAIN & FO PFDS & MAP DISPLAYS WENT BLANK, STAND BY HORIZON WENT BLANK, BOTH FMCS WENT BLANK, A FULL DISPLAY OF EICAS MESSAGES ASSOCIATED WITH LOSS OF AFFECTED SYS APPEARED THEY DISAPPEARED WITHIN APPROXMATELY 15 SECS.  ALL SYSTEMS RESTORED THEMSELVES RESEMBLING NORMAL OPS AS IF NOTHING HAPPENED   ACFT RTB , BPLU HAD NO FAULTS, MCDP HAD NO PREVIOUS FLT FAULTS. FPDS SELF TEST OKAY IAW SMM 34-22-00. ATT DISAGREE EICAS MESSAGE STAYED ILLUMINATED LONG ENOUGH TO READ IT. ACCOMPLISHED IRS BITE CHECK IAW FIM 34-21 FT 818. INDS OF YAW DAMPER TEST MATCHED CREW. CONTINUITY & MEGGER CHECKED YAW DAMPER TEST WIRING FROM D1022 PIN 2 TO D1261B PIN G7 IAW WDM 22-21-21 & D10224 PIN 12 TO D1259B PIN G7 IAW WDM 22-21-11, NO DEFECTS. DAR CHECKED GOOD. R & R M10398 TEST PANEL IAW AMM 24-22-06, & LT & RT YAW DAMPER MODULES IAW AMM 22-21-04. BITE & OPS CHECKED GOOD. IRS BITE CHECKED GOOD IAW FIM 31-21-FT 818. ARS.

Part: COMPUTER — FAULTED · airframe 92,261 hrs · 26,304 cycles

AIRCRAFT DOWNGRADED TO CAT I. PERFORMED MCDP TEST 30/40 AUTOLAND IAW AMM 22-00-02. NO DISCREPANCIES NOTED. AIRCRAFT RELEASED TO CAT IIIB OPERATIONAL. PLACARD TURNED TO CAT IIIB. DI STICKER REMOVED.

Part: ENGINE — VIBRATES (LEFT) · airframe 92,052 hrs · 26,167 cycles

ON T/O AT APPROX 90 KIAS LOUD BANG,AC SWERVED TO THE LEFT AND VIBRATION IN SEAT. ABBORTED T/O. AC RETURNED TO GATE AND MAINTENCE GROUNDED AC. CONDUCTED T/S PER FIM 71-05 FT 848 AND STALL INSPECTION PER AMM 72-00-00/601. METAL DEBRIS FOUND IN TURBINE EXHAUST, PER FIM AND AMM, LH ENGINE REPLACEMENT REQUIRED. SEE L/P 38704-73 FOR FURTHER ACTION. A/C VERIFIED NO ETOPS. A BORESCOPE WAS ACCOMPLISHED AND ENGINE WAS DAMAGED BEYOND LIMITS AND REQUIRES AN ENGINE CHANGE, IT IS SCHDULED FOR 1/14/24 IN MEM . AN AMENDED REPORT WILL BE SENT AFTER THE CORRECTIVE ACTION IS ACCOMPLISHED .

Part: ENGINE — DAMAGED (ZONE 500) · airframe 92,052 hrs · 26,167 cycles

THIS IS AN AMENDED REPORT // ON T/O AT APPROX 90 KIAS LOUD BANG,AC SWERVED TO THE LEFT AND VIBRATION IN SEAT. ABBORTED T/O. AC RETURNED TO GATE AND MAINTENCE GROUNDED AC. CONDUCTED T/S PER FIM 71-05 FT 848 AND STALL INSPECTION PER AMM 72-00-00/601. METAL DEBRIS FOUND IN TURBINE EXHAUST, PER FIM AND AMM, L ENGINE REPLACEMENT REQUIRED. SEE L/P 38704-73 FOR FURTHER ACTION. A/C VERIFIED NO ETOPS. A BORESCOPE WAS ACCOMPLISHED AND ENGINE WAS DAMAGED BEYOND LIMITS AND REQUIRES AN ENGINE CHANGE, IT IS SCHDULED FOR 1/14/24 IN MEM . AN AMENDED REPORT WILL BE SENT AFTER THE CORRECTIVE ACTION IS ACCOMPLISHED . REMOVED AND REPLACED #1 ENGINE DUE TO DAMGE OPS CHECK GOOD AC RETURNED TO SERVICE.

Part: ACTUATOR — UNSERVICEABLE (RUDDER) · airframe 92,013 hrs · 26,138 cycles

RUDDER RATIO EICAS MSG AND C/B POPPING . AC RETURNED TO GATE,MAINTENACE GROUNDED A/C. FOUND RUDDER RATIO CB POPPING. FIM 27-09 FT 814 DIRECTS TO REMOVE AND REPLACE RRCA. REMOVED AND REPLACED RRCA IWA KAC AMM 27-21-15. FOUND PLUG D231 NEEDS REPLACED. REMOVED AND REPLACED D231 PLUG IAW SWPM 20-61-11. RRCA TEST GOOD. RII FORM 27-08-01 COMPLIED WITH. LEAK CK GOOD.RETURNED A/C TO SERVICE.

Part: START VALVE — FAULTED (ZONE 500) · airframe 91,914 hrs · 26,068 cycles

L ENG START VALVE LIGHT ILLUMINATED ON ENGINE START AC RETURNED TO GATE AFTER LEFT ENGINE WOULD NOT START . AC GROUNDED BY MAINTENANCE. DEFERRED LH STARTER IAW ABX MEL 80-00-2-1 AND RETURNED AC TO SERVICE AND PERFORMED MANUAL ENGINE START.AT NEXT BASE, MAINTENANCE REMOVED AND REPLACED L ENG START VALVE PER B767-300 AMM 80-11-02 CHECKS GOOD. THIS CLEARS DI 46691 PLACARDS REMOVED AC REMAINS NO ETOPS.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 91,910 hrs · 26,064 cycles

RUDDER RATIO EICAS MESSAGE AND DISCRETE LIGHT ILLUMINATED AC RETURNED TO GATE AND GROUNDED BY MAINTENANCE PERFORMED BIT TEST BOX "RUDDER RATIO" IAW ABX B767 FIM 27-21 FT 804, OPS CHECK. MESSAGE CLEARED.AC RETURNED TO SERVICE .

Part: ACTUATOR — INOPERATIVE (ZONE 300) · airframe 91,879 hrs · 26,040 cycles

RUDDER RATIO EICAS MSG ON TAXI OUT. A/C RETURNED TO BLOCK GROUNDED BY MAINTENANCE .REMOVED AND REPLACED RUDDER RATIO CHANGER REF AMM 27-71-13. NO FAULTS NOTED, C/W RII 27-08 STEPS 5, 6. A/C RETURNED TO SERVICE .

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 91,742 hrs · 25,948 cycles

AFT CABIN TEMP. FWD CABIN TEMP. "FLT DECK TEMP." EICAS MESSAGE AND TEMP SELECTOR FAULT LIGHTS ALL ILLUMINATED AFTER ENGINE START. AIICRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE DETERMINED APU PWR TRANSFER ISSUES FIM CHECKED GOOD ON SYSTEM IAW FIM 21-61-1-1 REF TABLE 803. OPS CHECK NORMAL AT THIS TIME. AIRCRAFT REMAINS NO ETOPS. AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 91,004 hrs · 25,574 cycles

PUSHED AND STARTED ENGINES. RUDDER RATIO LIGHT WAS ON WHEN WE DID THE AFTER START CHECKLIST. CAME BACK TO GATE AFTER MAINT ADVISED. AIRCRAFT GROUNDED BY MAINTENANCE. MAINTENANCE RESET RUDDER RATIO MODULE L AND R PER FIM 27-09 F7 803. NO MSG OR LIGHTS DISPLAYED. AIRCRAFT RETURNED TO SERVICE.

Part: NONE — NONE · airframe 90,822 hrs · 25,491 cycles

L ENG. STARTER EICAS MSG APPEARED APPROX 35 SECONDS INTO START SEQUENCE ON #1 ENGINE. AICRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE ACCOMPLISHED OPERATIONAL TEST OF LEFT ENG START VALVE IAW AMM 80-11-02. NO FAULTS NOTED. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (RUDDER RATIO) · airframe 90,494 hrs · 25,334 cycles

RUDDER RATIO EICAS MESSAGE IN VIEW WITH ASSOCIATED LIGHT ON OVERHEAD PANEL AFTER ENGINE START. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE PERFORMED FIM 27-09 FT 803 + FIM 27-09 FT 814 FOR RUDDER RATIO CHANGER BITE PROCEDURE. ALL TEST PASSED NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: CIRCUIT BREAKER — TRIPPED (RUDDER RATIO) · airframe 90,363 hrs · 25,272 cycles

RUDDER RATIO LIGHT ILLUM AFTER ENG START ON BLOCK OUT. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE RESET RUDDER RATIO CIRCUIT BREAKER- MAGIC 8 AND RESET BOXES IN E & E IAW FIM 27-21 MAP FAULT TREE 804, OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CIRCUIT BREAKER — FAULTED · airframe 90,338 hrs · 25,261 cycles

EICAS MESSAGE RUDDER RATIO DISPLAYED. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE CYCLED CB G10 RUDDER RATIO IAW AMM 20-60-01 AND CLEARED FAULT BALLS IAW FIM 27-09. MESSAGE CLEARED. AIRCRAFT RETURNED TO SERVICE.

Part: TERMINAL — DIRTY (MASTER BATTERY) · airframe 90,306 hrs · 25,247 cycles

STATUS MSG MAIN BAT. CHGR. ON EICAS DISPLAY. AIRCRAFT RETURNED TO BLOCK AND WAS GROUNDED BY MAINTENANCE. MAINTENANCE INSPECTED AND CLEANED DC GROUND TERMINAL M10212 IAW B767 WDM 24-34-11. OPS CHECK GOOD AT THIS TIME. NO PRESENT MESSAGES. AIRCRAFT RETURNED TO SERVICE.

Part: STRINGER — CORRODED (BS 511 S39L) · corrosion level 2 · airframe 90,244 hrs · 25,214 cycles

STRINGER 39L AT STA. 511 SHOWS EVIDENCE OF CORROSION.

Part: SKIN — CRACKED · airframe 90,244 hrs · 25,214 cycles

#1 PYLON HAS CRACK AT UPPER AFT CORNER OF ACCESS PANEL HOLE 432AL.

Part: INTERCOSTAL — CRACKED · airframe 90,244 hrs · 25,214 cycles

INTERCOSTAL JUST AFT OF THE L\H AFT ENTRY DOOR IS CRACKED AT STA. 1540 STR 14L.  MARKED FA-3

Part: SKIN — CORRODED · corrosion level 2 · airframe 90,244 hrs · 25,214 cycles

EVIDENCE OF CORROSION ON L/H STABALIZER UPPER SKIN APROX. STA. 1750 HSBL 42

Part: INTERCOSTAL — DAMAGED · airframe 90,244 hrs · 25,214 cycles

IN RIGHT WING DRY BAY, BETWEEN RIB AT W. S. 375.8 & BULKHEAD AT W. S. 404.4, DAMAGED INTERCOSTAL, IMMEDIATELY FWD OF AFT BULKHEAD, ATTACHED TO LOWER SKIN.   MARKED  TT  101

Part: STRINGER — CRACKED · airframe 90,244 hrs · 25,214 cycles

SUPPLEMENTAL INFORMATION: 7.(C) CRACK LENGTH SHOULD BE .375 AND 7.(D) NUMBER OF CRACKS SHOULD BE 1

Part: SHEAR TIE — CORRODED · corrosion level 2 · airframe 90,244 hrs · 25,214 cycles

SHEAR TIE AT STA 1395 BETWEEN STR 35L-36L HAS EVIDENCE OF CORROSION

Part: LIGHT — NO TEST (COCKPIT) · airframe 90,244 hrs · 25,214 cycles

EMERGENCY LAMP ON RIGHT SIDE OF FLIGHT DECK FAILED TO ILLUMINATE.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 88,462 hrs · 24,427 cycles

TRAILING EDGE OF L/H LOWER TRAILING WING SKIN APPROX STA 798.2 SHOWS SIGNS OF CORROSION

Part: DOOR SILL — CORRODED (BS 1440) · corrosion level 2 · airframe 88,462 hrs · 24,427 cycles

EVIDENCE OF CORROSION ON UPPER CHORD OF BULK PIT LOWER SILL PLATE

Part: SEAT TRACK — CRACKED (COCKPIT) · airframe 88,462 hrs · 24,427 cycles

CAPTAINS AFT OUTBD SEAT TRACK IS CRACKED

Part: ATTACH FITTING — DAMAGED (RT ELEVATOR) · airframe 88,462 hrs · 24,427 cycles

R/H ELEVATOR CENTER PCA ATTACH LUG IS DAMAGED

Part: SEAT TRACK — DAMAGED (COCKPIT) · airframe 88,462 hrs · 24,427 cycles

FIRST OFFICERS FWD INBD SEAT TRACK HAS UPPER SURFACE DAMAGE AND 1 EA DAMAGED HOLE

Part: STRUCTURE — CORRODED (AFT CARGO DOOR) · corrosion level 2 · airframe 88,462 hrs · 24,427 cycles

AFT CARGO DOOR UPPER AFT SECTION HAS EVIDENCE OF CORROSION

Part: PIN — NO TEST (DOOR LATCH) · airframe 88,462 hrs · 24,427 cycles

MDCD LATCH PINS #2, #5, #9 AND #12 FAIL NDT INSP

Part: SEAT TRACK — BROKEN (COCKPIT) · airframe 88,462 hrs · 24,427 cycles

CAPTAINS AFT INBD SEAT TRACK HAS LARGE MISSING PIECE ON FWD EDGE

Part: SEAT TRACK — CRACKED (COCKPIT) · airframe 88,462 hrs · 24,427 cycles

CAPTAINS FWD INBD SEAT TRACK IS CRACKED

Part: SEAT TRACK — CRACKED (COCKPIT) · airframe 88,462 hrs · 24,427 cycles

FIRST OFFICERS AFT INBD SEAT TRACK IS CRACKED

Part: SEAT TRACK — CRACKED (COCKPIT) · airframe 88,462 hrs · 24,427 cycles

CAPTAINS FWD OUTBD SEAT TRACK IS CRACKED

Part: SUPPORT — CORRODED (BS 610-632) · corrosion level 2 · airframe 87,024 hrs · 23,521 cycles

FWD CARGO AUX SILL CHORD HAS CORROSION AT STA 610 - 632

Part: ANGLE — CRACKED (BS 534-625) · airframe 87,024 hrs · 23,521 cycles

CRACKED ANGLE JUST I/B OF FWD CARGO DOOR LOWER SILL STA 625 AND 534 RBL 41

Part: SUPPORT — DAMAGED (BS 610) · airframe 87,024 hrs · 23,521 cycles

BALLMAT SUPPORT AT FWD CARGO DOOR AT STA 610 DAMAGED

Part: SPLICE PLATE — CORRODED (WING) · corrosion level 2 · airframe 87,024 hrs · 23,521 cycles

WS 610 JUST FWD OF FRONT SPAR AROUND FASTENER HAS INTERGRANULAR CORROSION FOUND WITH UT THICKNESS.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 87,024 hrs · 23,521 cycles

FWD PIT INTERCOSTAL HAS EVIDENCE OF CORROSION AT STA 595 RBL 33.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 87,024 hrs · 23,521 cycles

FWD PIT INTERCOSTAL HAS EVIDENCE OF CORROSION AT STA 605 RBL 27.

Part: FITTING — CORRODED (LT MLG) · corrosion level 2 · airframe 87,024 hrs · 23,521 cycles

LT MLG KICK FITTING HAS CORROSION SEVERAL AREAS.

Part: ANGLE — CRACKED (NLG WW) · airframe 87,024 hrs · 23,521 cycles

CRACK INDICATION IN THE NWW LT AFT VERTICAL ANGLE (CHORD) ABOUT 12" FROM THE TOP ABOUT 3" LONG AT STA 287.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 87,024 hrs · 23,521 cycles

EVIDENCE OF CORROSION FUSELAGE EXTERNAL STRINGER 33 L STA 658 - 676.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 87,024 hrs · 23,521 cycles

EVIDENCE OF CORROSION FUSELAGE EXTERNAL STRINGER 34 L STA 657 - 670.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 87,024 hrs · 23,521 cycles

FWD CARGO FRAME AT STA 632 RBL 18 - 23 UPPER CORD HAS CORROSION.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 87,024 hrs · 23,521 cycles

FUSELAGE SKIN INNNER SURFACE HAS EVIDENCE OF CORROSION AT STA 654+11 S-34L.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 87,024 hrs · 23,521 cycles

FUSELAGE SKIN INNNER SURFACE HAS EVIDENCE OF CORROSION AT STA 654+11 S-33L.

Part: SKIN — CRACKED (RT PYLON) · airframe 87,024 hrs · 23,521 cycles

RIGHT PYLON INBD SIDE AFT UPPER CORNER OF ACCESS PANEL 442AL, PYLON SKIN HAS POSSIBLE CRACK.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 87,024 hrs · 23,521 cycles

FWD PIT UPPER CHORD FLOORBEAM HAS EVIDENCE OF CORROSION STA 434 LBL 50.

Part: STRAP — CRACKED (FUSELAGE) · airframe 87,024 hrs · 23,521 cycles

LT SIDE BS 955 BULKHEAD FITTING FAIL SAFE STRAP REQUIRES CLEANING DUE TO CRACK INDICATION.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 87,024 hrs · 23,521 cycles

FWD CARGO DOOR LWR MAIN SILL HAS EVIDENCE OF CORROSION STA 528 ON INNER CHORD.

Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 87,024 hrs · 23,521 cycles

BOTTOM OF RT KEEL BEAM HAS EVIDENCE OF CORROSION IN MULTIPLE SPOTS APPROX STA 967 TO 1008 RBL 9.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 87,024 hrs · 23,521 cycles

FWD CARGO DOOR LWR MAIN SILL HAS EVIDENCE OF CORROSION ON FAIL-SAFE STRAP AT STA 567.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 87,024 hrs · 23,521 cycles

FWD CARGO DOOR LWR MAIN SILL HAS EVIDENCE OF CORROSION ON INNER CHORD AT STA 566.

Part: LIGHT — NO TEST (CABIN) · airframe 87,024 hrs · 23,521 cycles

DURING EMERGENCY LIGHT OPS TEST, EMERGENCY EXIT AND R/H EMERGENCY FLOOD LIGHT FAIL TO ILLUMINATE

Part: SHUTOFF VALVE — STICKING (CABIN PRESSURE) · airframe 85,799 hrs · 22,500 cycles

CABIN ALTITUDE MASTER WARNING WITH RAPID DESCENT, CLIMBING THROUGH FLIGHT LEVEL 280. ACCOMPLISHED CONDITIONAL INSPECTION FOR EXCESSIVE CABIN PRESSURE LEAK IAW AMM 05-51-24. FOUND E/E ACCESS DOOR SEAL IMPROPERLY INSTALLED. REINSTALLED THE SEAL IAW AMM 52-09-04. CABIN PRESSURE AND LEAK CHECKED, DECAY CHECKED GOOD IAW AMM 05-51-24. NO OTHER DEFECTS FOUND AT THIS TIME. REMOVED AND REPLACED THE NR 2 ENGINE PRSOV IAW AMM 36-11-09. OPS CHECKED GOOD, LEAK CHECKED GOOD.

Part: CONTROL VALVE — FAILED (APU) · airframe 85,799 hrs · 22,501 cycles

CABIN ALTITUDE MASTER WARNING WITH RAPID DESCENT, CLIMBING THROUGH FLIGHT LEVEL 280. REMOVED AND REPLACED APU SURGE CONTROL VALVE IAW AMM 49-53-01. ALL CHECKED GOOD.

Part: CONTROL VALVE — MALFUNCTIONED (APU) · airframe 85,799 hrs · 22,500 cycles

CABIN ALTITUDE MASTER WARNING WITH EICAS MESSAGE, LOST CABIN PRESSURE AT 27,000 FEET, PERFORMED AN EMERGENCY DESCENT. REMOVED AND REPLACED APU SURGE CONTROL VALVE IAW AMM 49-53-01. ALL CHECKED GOOD.

Part: STRINGER — CORRODED (BS 1809.5) · corrosion level 2 · airframe 85,795 hrs · 22,496 cycles

CORROSION ON STRINGER 36R, BS 1809.5

Part: BULKHEAD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,795 hrs · 22,496 cycles

STA 1809 BULKHEAD LOWER CHORD HAS CORROSION AT RBL 4.

Part: PLACARD — BROKEN (L1 DOOR SLIDE) · airframe 85,565 hrs · 22,313 cycles

L1 DOOR ESCAPE SLIDE PLACARD BROKEN OFF. REMOVED AND REPLACED L1 DOOR ESCAPE SLIDE PLACARD IAW MM 52-11-02 AND SRM 51-40-02.

Part: LAMP — INOPERATIVE (ANNUNCIATOR) · airframe 84,890 hrs · 21,834 cycles

EMERGENCY LIGHTS "UNARMED" ANNUNCIATOR LIGHT OUT. REPLACED THE LAMPS IN THE ANNUNCIATOR IAW MM 33-16-02. OPS CHECKED NORMAL.