N740AX

Part: ELECTRONIC UNIT — FAILED (RT ENGINE) · airframe 94,002 hrs · 44,528 cycles

ON TAXI OUT N1 ON RT ENG FAILED. INDICATED ZERO. STBY ALSO, ALL OTHER INDICATIONS NORMAL. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE REPLACED RT. EEC OPS CHECK GOOD IAW 73-21-07. AIRCRAFT RETURNED TO SERVICE

Part: MEC — FAULTED (RIGHT ENGINE) · airframe 93,439 hrs · 44,325 cycles

AFTER ENGINE START, RIGHT ENGINE SURGE AND EGT NOT GOING OVER 500. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE REMOVED AND REPLACED MAIN ENGINE CONTROL (MEC) IAW AMM 73-21-01 . REF. FIM TASK 73-11-FT 812,811 PERFORMED ENGINE RUNS IAW AMM 71-00-00. OPS CHECK GOOD. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: WARNING MESSAGE — ILLUMINATED (LT STARTER) · airframe 93,439 hrs · 44,325 cycles

AFTER PUSH BACK DOING CROSS BLEED START THE LEFT ENGINE STARTER EICAS MSG ILLUM. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE DEFERRED THE LEFT START CONTROL VALVE IAW MEL 80-00-2-1. AIRCRAFT RETURNED TO SERVICE.

Part: CIRCUIT CARD — FAULTED (STALL WARNING) · airframe 93,297 hrs · 44,277 cycles

RIGHT STICK SHAKER SOUNDED CONTINUESLY AFTER DEPARTURE. AIRCRAFT EXECUTED AN AIR TURNBACK WITHOUT FURTHER INCIDENT. AIRCRAFT WAS GROUNDED AT CVG. MAINTENANCE REMOVED AND REPLACED STALL WARNING CARD IAW B767 27-32-01. AND RESET WEU AS WELL OPS CHECK GOOD. NO FAULTS PRESENT. AIRCRAFT RETURNED TO SERVICE.

Part: NONE — FAULTED (ZONE 100) · airframe 92,848 hrs · 44,114 cycles

DURING PUSHBACK, SPOILERS EICAS ADVISORY MESSAGE ILLUMINATED. AIRCRAFT BTB AND GROUNDED BY MAINTENANCE. MAINTENANCE REMOVED AND REPLACED SPOILER CONTROL MODULE ASSY 3 LEFT IAW AMM 27-09-00. OP CHECK GOOD. AICRAFT RETURNED TO SERVICE.

Part: NONE — FAULTY (ZONE 100) · airframe 92,818 hrs · 44,098 cycles

FWD WINDOW HEAT INOP LIGHT ILLUMINATED L FWD WINDOW EICAS MESSAGE. AIRCRAFT RETURNED TO BLOCK AND WAS GROUNDED BY MAINTENANCE. MAINTENANCE REMOVED AND REPLACED LEFT WINDOW HEAT CONTROLLER PER AMM 30-41-01. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE

Part: SKIN — CRACKED (ZONE 100) · airframe 91,509 hrs · 43,495 cycles

DURING AIRCRAFT C-CHECK, MAINTENANCE DISCOVERED A CRACK ON THE FUSELAGE SKIN (SECTION 46) LOCATED AT STATION 1541 AND STRINGER S29L.  THE DAMAGE WAS EVALUATED PER 767-200 SRM 53-00-01, FIGURE 101 AND FOUND TO EXCEED ALLOWABLE LIMITS, REQUIRING A REPAIR.  THE DAMAGE CAN BE REPAIRED PER 767-200 SRM 53-00-01, FIGURE 201, REPAIR 1 EXCEPT THE PROPOSED REPAIR WILL FALL WITHIN 22” OF THE OUTFLOW VALVE CUT OUT (SKIN EOP), REQUIRING SPECIFIC APPROVAL.  THE SKIN PANEL (P/N 146T3231-1) IS FABRICATED FROM 2024-T3 X 0.200” ALUMINUM CLAD SHEET (QQ-A-250/5) CHEM. MILLED DOWN TO 0.056” MINIMUM (0.108” AT THE DAMAGE/REPAIR LOCATION).  AIRBORNE MAINTENANCE AND ENGINEERING SERVICES CONTACTED FLIGHT VEHICLES CONSULTING INC. WITH A PROPOSED REPAIR FOR EVALUATION AND APPROVAL. REPAIR COMPLETED PER ABX-REA-5365-64368-00

Part: STRINGER — CORRODED (BS 783 S38L) · airframe 91,509 hrs · 43,495 cycles

DURING AIRCRAFT C-CHECK, MAINTENANCE DISCOVERED CORROSION ON STRINGER S38L LOCATED IN THE FORWARD LOWER CARGO COMPARTMENT AT APPROXIMATE STATION 783.00.  THE DAMAGE WAS EVALUATED PER 767-200 SRM 53-00-03, FIGURE 101 AND FOUND TO EXCEED LIMITS REQUIRING A SPLICE SECTION REPAIR. THIS ENGINEERING ORDER PROVIDES REPAIR INSTRUCTIONS TO THE DAMAGED STRINGER PER 767-200 SRM 53-00-03, FIGURE 201, REPAIR 2. REPAIR COMPLETED PER ABX-REA-5330-64382-00

Part: SHEAR TIE — CORRODED (BS 764 S38-39R) · airframe 91,509 hrs · 43,495 cycles

DURING AIRCRAFT C-CHECK, MAINTENANCE DISCOVERED CORROSION ON A SHEAR TIE LOCATED BETWEEN S38R AND S39R AT STATION 764.  AFTER EVALUATION, THE DAMAGE WAS DETERMINED TO BE BEYOND ECONOMICAL REPAIR, WARRANTING REPLACEMENT.  THE SHEAR TIE, P/N 140T2103-213, WAS UNAVAILABLE FOR PURCHASE AND A SPARES MATERIALS AGREEMENT LICENSE (SMAL) WAS OBTAINED FROM BOEING FOR APPROVAL TO FABRICATE THE PART.  THIS ENGINEERING ORDER PROVIDES DETAILED INSTRUCTIONS TO FABRICATE A REPLACEMENT SHEAR TIE (FORMER) TO BE CONSUMED DURING THIS MAINTENANCE VISIT. FABRICATED AND INSTALLED SHEAR TIE PER ABX-REA-5330-64403-00

Part: BATTERY — LOW VOLTAGE (ZONE 100) · airframe 91,319 hrs · 43,410 cycles

MAIN BATTERY CHARGER STATUS MSG AFTER BLOCKOUT. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. INSTALLED NEW BATTERY AND CHARGER IAW B767 AMM 24-31-01 AND 24-31-02, NO STATUS MESSAGE. AIRCRAFT RELEASED.

Part: WARNING MESSAGE — ILLUMINATED (AFT BOOST PUMP) · airframe 91,263 hrs · 43,378 cycles

LEFT AFT FUEL PUMP EICAS MSG ILLUMINATED AFTER BLOCKOUT. AIRCRAFT BTB AND GROUNDED BY MAINTENANCE. FUEL PUMP WAS DEFERRED IAW MEL 28-22-1 AND AIRCRAFT RELEASED.

Part: DOOR — ABNORMAL (FWD CARGO) · airframe 91,186 hrs · 43,342 cycles

AFTER TAKEOFF AND DURING CLIMB THROUGH APPROXIMATELY 11,500 FEET. RED CABIN ALTITUDE LIGHT ILLUMINATED. FOLLOWED QRH BUT CABIN ALTITUDE COULD NOT BE CONTROLLED. AIRCRAFT COMPLETED AIR TURNBACK AND GROUNDED BY MAINTENANCE. FORWARD LOWER CARGO DOOR WAS FOUND NOT TO BE CLOSED. MAINTENANCE CLOSED DOOR AND AIRCRAFT WAS RELEASED.

Part: PRESSURE SWITCH — OUT OF TOLERANCE (HYD SYSTEM) · airframe 90,933 hrs · 43,203 cycles

C HYD PRIM 1 EICAS MESSAGE. AIRCRAFT BACK TO BLOCK AND GROUNDED. REMOVED OLD, THEN INSTALLED NEW C1 PRESSURE SWITCH, IAW B767 AMM 29-11-10. OPERATIONS CHECK OK, AIRCRAFT RELEASED FOR FLIGHT.

Part: CONTROL PANEL — SHORTED (FIRE DETECTION) · airframe 90,930 hrs · 43,201 cycles

DURING LEFT ENGINE START "LT ENGINE FUEL VALVE" AND "ENGINE VALVE" LIGHT ILLUMINATED 0.0 FUEL FLOW NO LIGHT OFF. AIRCRAFT BACK TO BLOCK AND GROUNDED. FOUND ENGINE FIRE CONTROL PANEL SHORTING-REMOVED AND REPLACED ENGINE FIRE CONTROL PANEL ASSEMBY, IAW 767 AMM 26-21-02. OPERATIONS CHECK GOOD. AIRCRAFT RELEASED.

Part: IDG — INTERMITTENT (RIGHT) · airframe 90,910 hrs · 43,187 cycles

RIGHT GENERATOR DRIVE LIGHT CAME ON INTERMITTENTLY ON TAXI. AIRCRAFT RETURNED TO GATE AND WAS GROUNDED BY MAINTENANCE. REMOVED AND REPLACED RT GEN, IAW B767 AMM 24-11-01. AIRCRAFT WAS RETURNED TO SERVICE.

Part: SHUTOFF VALVE — FAILED (CABIN AIR) · airframe 90,909 hrs · 43,187 cycles

DURING TAKE OFF, RT PACK OFF AND RT ENGINE BLEED OFF LIGHTS ILLUMINTAED WITH PACK SELECTED TO AUTO. DUCT PRESSURE GAUGE READS 5-10 PSI ON RIGHT. AIRCRAFT DIVERTED, AIRCRAFT WAS GROUNDED. CONDUCTED T/S, PER B767 FIM 36-20 FT 805, RT PRSOV FAULT INDICATED. REMOVED OLD, THEN INSTALLED NEW RT PRSOV, IAW AMM 36-11-09, TEST OK. RIGHT ENGINE RUN CONDUCTED, PER ERU AND TAXI CHECKLIST, DUCT PRESSURE RIGHT SIDE 40 PSI, BLEED SHIFT OK. RIGHT PACK OFF CAUSED BY NO DUCT PRESSURE. AIRCRAFT RELEASED.

Part: WINDSHIELD — CRACKED (LEFT) · airframe 90,875 hrs · 43,175 cycles

LT FWD WINDOW IN CRUISE CAPT WINDSHIELD SHATTERED AT FL360 CRUISE OUTER PANE. MX ADV RETURN TO CVG. AIRCRAFT WAS GROUNDED AND WINDSHIELD REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: GCU — INTERMITTENT (APU GENERATOR) · airframe 90,785 hrs · 43,131 cycles

APU GENERATOR FAILED IN FLIGHT DURING APPROACH. THE LEFT IDG WAS ON DEFERRAL, THE AIRCRAFT DECLARED AN EMERGENCY BECAUSE THE AIRCRAFT ONLY HAD (1) OPERATING ELECTRICAL POWER SOURCE. AIRCRAFT LANDED AND WAS GROUNDED BY MAINTENANCE. MAINTENANCE REPLACED THE APU GENERATOR CONTROL PANEL. AIRCRAFT WAS RELEASED.

Part: GENERATOR — FAILED (APU) · airframe 90,785 hrs · 43,131 cycles

ON TAXI OUT APU GENERATOR QUIT, AIRCRAFT BACK TO BLOCK. AIRCRAFT GROUNDED BY MAINTENANCE. REMOVED AND REPLACED APU GENERATOR, IAW AMM 24-21-01. AIRCRAFT RELEASED FOR FLIGHT.

Part: STRINGER — CORRODED (BS 1582) · airframe 89,832 hrs · 42,669 cycles

CORROSION ON STRINGER 31R END FITTING AT FUSELAGE STATION 1582. THE STRINGER END FITTING WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: STRINGER — CORRODED (BS 1582) · airframe 89,832 hrs · 42,669 cycles

CORROSION ON STRINGER 30R END FITTING AT FUSELAGE STATION 1582. THE STRINGER END FITTING WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: STRINGER — CORRODED (BS 1582) · airframe 89,832 hrs · 42,669 cycles

CORROSION ON STRINGER 37L END FITTING AT FUSELAGE STATION 1582. THE STRINGER END FITTING WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: FLOOR SUPPORT — CORRODED (BS 1572-1582) · corrosion level 2 · airframe 89,832 hrs · 42,669 cycles

CORROSION ON FLOOR SUPPORT AT FUSELAGE STATION 1582 TO 1572, STRINGER 20R. THE FLOOR SUPPORT WAS REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: STRINGER — CORRODED (BS 1582) · airframe 89,832 hrs · 42,669 cycles

CORROSION ON STRINGER 33L END FITTING AT FUSELAGE STATION 1582. THE STRINGER END FITTING WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: STRINGER — CORRODED (BS 1582) · airframe 89,832 hrs · 42,669 cycles

CORROSION ON STRINGER 8R END FITTING AT FUSELAGE STATION 1582. THE STRINGER END FITTING WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: STRINGER — CORRODED (BS 1582) · airframe 89,832 hrs · 42,669 cycles

CORROSION ON STRINGER 29R END FITTING AT FUSELAGE STATION 1582. THE STRINGER END FITTING WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: STRINGER — CORRODED (BS 1582) · airframe 89,832 hrs · 42,669 cycles

CORROSION ON STRINGER 4R END FITTING AT FUSELAGE STATION 1582. THE STRINGER END FITTING WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: STRINGER — CORRODED (BS 1582) · airframe 89,832 hrs

CORROSION ON STRINGER 34L END FITTING AT FUSELAGE STATION 1582. THE STRINGER END FITTING WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: STRINGER — CORRODED (BS 1582) · airframe 89,832 hrs · 42,669 cycles

CORROSION ON STRINGER 27R END FITTING AT FUSELAGE STATION 1582. THE STRINGER END FITTING WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: STRINGER — CORRODED (BS 1582) · airframe 89,832 hrs · 42,669 cycles

CORROSION ON STRINGER 22R END FITTING AT FUSELAGE STATION 1582. THE STRINGER END FITTING WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: STRINGER — CORRODED (BS 1582) · airframe 89,832 hrs · 42,669 cycles

CORROSION ON STRINGER 38L END FITTING AT FUSELAGE STATION 1582. THE STRINGER END FITTING WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: STRINGER — CORRODED (BS 1582) · airframe 89,832 hrs · 42,669 cycles

CORROSION ON STRINGER 39R END FITTING AT FUSELAGE STATION 1582. THE STRINGER END FITTING WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: STRINGER — CORRODED (BS 1582) · airframe 89,832 hrs · 42,669 cycles

CORROSION ON STRINGER 38R END FITTING AT FUSELAGE STATION 1582. THE STRINGER END FITTING WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: STRINGER — CORRODED (BS 1582) · airframe 89,832 hrs · 42,669 cycles

CORROSION ON STRINGER 35L END FITTING AT FUSELAGE STATION 1582. THE STRINGER END FITTING WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: STRINGER — CORRODED (BS 1582) · airframe 89,832 hrs · 42,669 cycles

CORROSION ON STRINGER 9R END FITTING AT FUSELAGE STATION 1582. THE STRINGER END FITTING WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: STRINGER — CORRODED (BS 1582) · airframe 89,832 hrs · 42,669 cycles

CORROSION ON STRINGER 39L END FITTING AT FUSELAGE STATION 1582. THE STRINGER END FITTING WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: STRINGER — CORRODED (BS 1582) · airframe 89,832 hrs · 42,669 cycles

CORROSION ON STRINGER 2R END FITTING AT FUSELAGE STATION 1582. THE STRINGER END FITTING WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: STRINGER — CORRODED (BS 1582) · airframe 89,832 hrs · 42,669 cycles

CORROSION ON STRINGER 1R END FITTING AT FUSELAGE STATION 1582. THE STRINGER END FITTING WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: SLEEVE — NOT SEATED (FUEL SYSTEM) · airframe 89,261 hrs · 42,429 cycles

WHILE THE AIRPLANE WAS OUT OF SERVICE (GROUNDED) AND THE LEFT AFT FUEL BOOST PUMP IN THE LEFT WING WAS BEING REMOVED, FUEL STARTED TO FLOW OUT OF THE FUEL TANK. THE PUMP COULD NOT BE RE-INSERTED UNTIL THE FUEL STOPPED FLOWING OUT OF THE TANK. AFTER THE FUEL WAS CLEANED OFF THE RAMP BY HAZMAT TECHNICIANS, A SERVICEABLE LEFT AFT FUEL BOOST PUMP WAS INSTALLED. THE CAUSE OF THE FUEL SPILL WAS AN UNSEATED FUEL BOOST PUMP SHUTOFF SLEEVE.

Part: SKIN — DAMAGED (BS 539) · airframe 89,181 hrs · 42,392 cycles

DAMAGE IN THE SKIN AT THE FORWARD LOWER CARGO DOOR FRAME AT FUSELAGE STATION 539, STRINGER 30R. THE DAMAGE IS MEASURED 3.5" BY 0.5". THE SKIN WAS REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: SMOKE DETECTOR — DIRTY (SUPERNUMERARY) · airframe 89,120 hrs · 42,364 cycles

THE SUPERNUMERARY AREA SMOKE DETECTOR'S ALARM SOUNDED WITH NO SMOKE PRESENT AFTER OPENING THE COMPARTMENT’S DOOR. THE AIRPLANE WAS REMOVED FROM SERVICE (GROUNDED) AND THE SMOKE DETECTOR WAS CLEANED. THE CAUSE OF THE SMOKE DETECTOR'S ALARM WAS DUST IN THE SMOKE DETECTOR.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 89,115 hrs · 42,359 cycles

CRACK IN STRINGER 25L AT FUSELAGE STATION 676 AT THE SUPPLEMENTAL TYPE CERTIFICATE SPLICE. THE STRINGER WAS REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: FAILSAFE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 89,115 hrs · 42,359 cycles

CORROSION ON THE FAIL-SAFE CHORD AT FUSELAGE STATION 1562, BETWEEN STRINGERS 35L AND 37R. THE CHORD WAS REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 89,115 hrs · 42,359 cycles

CORROSION AND CRACK IN SHEAR TIE BETWEEN STRINGERS 35R AND 36R AT FUSELAGE STATION 1439. THE SHEAR TIE WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 89,115 hrs · 42,359 cycles

CRACK IN STRINGER 19L AT FUSELAGE STATION 676 AT THE SUPPLEMENTAL TYPE CERTIFICATE SPLICE. THE STRINGER WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: STRUT — CORRODED (LT WING) · corrosion level 2 · airframe 89,115 hrs · 42,359 cycles

CORROSION ON THE LEFT WING #4 SLAT INBOARD AUXILIARY TRACK, OUTBOARD LOWER STRUT. THE STRUT WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 89,115 hrs · 42,359 cycles

CORROSION AND CRACK IN STRINGER 30R AT FUSELAGE STATIONS 1540 AND 1554. THE STRINGER WAS REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: FLOORBEAM — CORRODED (BS 1219) · corrosion level 2 · airframe 89,115 hrs · 42,359 cycles

CORROSION ON UPPER T-CHORD OF AFT LOWER COMPARTMENT FLOOR FRAME AT FUSELAGE STATION 1219. THE T-CHORD WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: FITTING — CORRODED (BS 434) · corrosion level 2 · airframe 89,115 hrs · 42,359 cycles

CORROSION ON STRINGER 39L SPLICE FITTING AT FUSELAGE STATION 434. THE SPLICE FITTING PART NUMBER 140T0115-16 AND STRINGER PART NUMBER 141T3001-1 WERE REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 89,115 hrs · 42,359 cycles

CORROSION ON THE SHEAR TIE AT FUSELAGE STATION 742 BETWEEN STRINGERS 35R AND 36R. THE SHEAR TIE WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 89,115 hrs · 42,359 cycles

CORROSION ON STRINGER 33R AT FUSELAGE STATION 1470. THE STRINGER WAS REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: SHEAR TIE — CORRODED (BS 1502) · corrosion level 2 · airframe 89,115 hrs · 42,359 cycles

CORROSION ON THE SHEAR TIE AT FUSELAGE STATION 1502 BETWEEN STRINGERS 39L AND 38L. THE SHEAR TIE WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: DOUBLER — DAMAGED (FUSELAGE) · airframe 89,115 hrs · 42,359 cycles

GOUGES ON DOUBLER FOR DUMP VALVE PAN SPACER AT FUSELAGE STATION 1571, STRINGER 38L. THE DOUBLER WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 89,115 hrs · 42,359 cycles

CORROSION ON THE LOWER SURFACE OF THE HORIZONTAL WEB PAD UP AREA OF THE KEEL BEAM IN TWO AREAS AT BUTT LINE 0 AND AT LEFT BUTT LINE 7 BETWEEN BODY STATIONS 1013 AND 1020. THE HORIZONTAL WEB WAS REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 89,115 hrs · 42,359 cycles

CORROSION AND A PUNCTURE IN THE WASTE WATER PAN SUPPORT INTERCOSTAL BETWEEN FUSELAGE STATIONS 1562 AND 1582 AT STRINGER 38L. THE INTERCOSTAL WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: STRINGER — CORRODED (BS 1395) · corrosion level 2 · airframe 89,115 hrs · 42,359 cycles

CORROSION ON STRINGER 32R AT FUSELAGE STATION 1395. THE STRINGER WAS REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 89,115 hrs · 42,359 cycles

CORROSION ON STRINGER 35L AT FUSELAGE STATION 420. THE STRINGER WAS REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 89,115 hrs · 42,359 cycles

CORROSION ON STRINGER 34L AT FUSELAGE STATION 1562. THE STRINGER WAS REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 89,115 hrs · 42,359 cycles

CORROSION ON UPPER T-CAP IN FRAME AT FUSELAGE STATION 1351. THE T-CAP WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 89,115 hrs · 42,359 cycles

CRACK IN THE SHEAR TIE AT FUSELAGE STATION 1641 BETWEEN STRINGERS 33R AND 32R. THE SHEAR TIE WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: STRUT — CORRODED (LT WING) · corrosion level 2 · airframe 89,115 hrs · 42,359 cycles

CORROSION ON THE LEFT WING #2 SLAT OUTBOARD AUXILIARY TRACK, INBOARD LOWER STRUT. THE STRUT WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 89,115 hrs · 42,359 cycles

CORROSION ON STRINGER 36L AT FUSELAGE STATION 420. THE STRINGER WAS REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 89,115 hrs · 42,359 cycles

CORROSION ON STRINGER 38R AT FUSELAGE STATION 423. THE STRINGER WAS REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 89,115 hrs · 42,359 cycles

CORROSION ON THE SHEAR TIE AT FUSELAGE STATION 1307, STRINGER 34L. THE SHEAR TIE WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 89,115 hrs · 42,359 cycles

CORROSION ON THE RIGHT KEEL BEAM CHORD IN SEVERAL AREAS FROM STA 925 TO STA 1028. THE CHORD WAS REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 89,115 hrs · 42,359 cycles

CRACK AND CORROSION IN STRINGER 33L AT FUSELAGE STATION 445. THE STRINGER WAS REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: STRINGER — CORRODED (BS 1540) · corrosion level 2 · airframe 89,115 hrs · 42,359 cycles

CORROSION ON STRINGER 35L AT FUSELAGE STATION 1540. THE STRINGER WAS REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 89,115 hrs · 42,359 cycles

CRACK IN STRINGER 1L AT FUSELAGE STATION 676. THE STRINGER WAS REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: SPLICE PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 89,115 hrs · 42,359 cycles

CORROSION ON THE SPLICE PLATE BETWEEN FUSELAGE STATIONS 1034 AND 1040, LEFT BUTT LINE 97. THE SPLICE PLATE WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 89,115 hrs · 42,359 cycles

CRACK IN STRINGER 37L AT FUSELAGE STATION 1558. THE STRINGER WAS REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 89,115 hrs · 42,359 cycles

CORROSION ON THE BULK CARGO DOOR SILL FLOOR PLATE ATTACH STIFFENER AT STRINGER 22L BETWEEN FUSELAGE STATIONS 1417 AND 1461. THE STIFFENER WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: RIB — CORRODED (RT WING) · corrosion level 2 · airframe 89,115 hrs · 42,359 cycles

CORROSION ON THE AIR LOAD RIB AT THE #10 SLAT, OUTBOARD AUXILIARY TRACK. THE RIB WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 89,115 hrs · 42,359 cycles

CRACK IN STRINGER 21L AT FUSELAGE STATION 676 AT THE SUPPLEMENTAL TYPE CERTIFICATE SPLICE. THE STRINGER WAS REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 89,115 hrs · 42,359 cycles

CRACKS IN STRINGER 32R AT FUSELAGE STATION 1407, 1500, AND 1546 AND 1562. THE STRINGER WAS REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: STRINGER — CORRODED (BS 1263) · corrosion level 2 · airframe 89,115 hrs · 42,359 cycles

CORROSION ON STRINGER 39L AT FUSELAGE STATION 1263. THE STRINGER WAS REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: SHEAR TIE — CORRODED (BS 1502) · airframe 89,115 hrs · 42,359 cycles

CORROSION ON THE SHEAR TIE AT FUSELAGE STATION 1502 BETWEEN STRINGERS 37R AND 36R. THE SHEAR TIE WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: RIB — CORRODED (RT WING) · corrosion level 2 · airframe 89,115 hrs · 42,359 cycles

CORROSION ON THE AIR LOAD RIB AT THE #10 SLAT, INBOARD AUXILIARY TRACK. THE RIB WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 89,115 hrs · 42,359 cycles

CORROSION ON STRINGER 38L AT FUSELAGE STATION 420. THE STRINGER WAS REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 89,115 hrs · 42,359 cycles

CORROSION ON INTERCOSTAL IN THE AFT LOWER COMPARTMENT AT FUSELAGE STATION 1274, LBL 33. THE INTERCOSTAL WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 89,115 hrs · 42,359 cycles

CORROSION ON THE FRAME WEB LOCATED AT FUSELAGE STATION 1562, BETWEEN STRINGERS 26L AND 32R. THE WEB WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 89,115 hrs · 42,359 cycles

CORROSION ON STIFFENER AT FUSELAGE STATION 1414 STRINGER 22L. THE STIFFENER WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: SPAR — CORRODED (LT WING) · corrosion level 2 · airframe 89,115 hrs · 42,359 cycles

CORROSION ON THE LEFT WING TRAILING EDGE AUXILIARY SPAR UPPER CHORD UNDER THE #6 SPOILER. THE CHORD WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 89,115 hrs · 42,359 cycles

CRACK IN STRINGER 22L AT FUSELAGE STATION 676 AT THE SUPPLEMENTAL TYPE CERTIFICATE SPLICE. THE STRINGER WAS REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: STRINGER — CORRODED (BS 1263) · corrosion level 2 · airframe 89,115 hrs · 42,359 cycles

CORROSION ON STRINGER 39R AT FUSELAGE STATION 1263. THE STRINGER WAS REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 89,115 hrs · 42,359 cycles

CORROSION ON THE SHEAR TIE AT FUSELAGE STATION 1351 BETWEEN STRINGERS 36L AND 37L. THE SHEAR TIE WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 89,115 hrs · 42,359 cycles

CRACK IN STRINGER 17L AT FUSELAGE STATION 676 AT THE SUPPLEMENTAL TYPE CERTIFICATE SPLICE. THE STRINGER WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 89,115 hrs · 42,359 cycles

CORROSION ON THE UPPER CHORD OF THE FLOORBEAM AT FUSELAGE STATION 1540, STRINGER 33L. THE CHORD WAS REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 89,115 hrs · 42,359 cycles

CORROSION ON THE LEFT KEEL BEAM CHORD IN SEVERAL AREAS FROM STA 860 TO STA 1034. THE CHORD WAS REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 89,115 hrs · 42,359 cycles

CORROSION ON THE SHEAR TIE AT FUSELAGE STATION 742 BETWEEN STRINGERS 37R AND 36R. THE SHEAR TIE WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 89,115 hrs · 42,359 cycles

CORROSION ON STRINGER 39L AT FUSELAGE STATION 1555. THE STRINGER WAS REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 89,115 hrs · 42,359 cycles

CORROSION ON THE SHEAR TIE AT FUSELAGE STATION 1329 BETWEEN STRINGERS 38R AND 39R. THE SHEAR TIE WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 89,115 hrs · 42,359 cycles

CORROSION ON STRINGER 34L AT FUSELAGE STATION 1307. THE STRINGER WAS REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: FAILSAFE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 89,115 hrs · 42,359 cycles

CORROSION ON THE UPPER SURFACE OF THE FAIL-SAFE STRAP COMMON TO THE FORWARD FRAME OF THE FORWARD LOWER CARGO DOOR JAMB. THE FAIL-SAFE STRAP WAS REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: SKIN — CRACKED (FUSELAGE) · airframe 89,115 hrs · 42,359 cycles

CRACK IN SKIN AT FUSELAGE STATION 757 BETWEEN STRINGERS 35R AND 36R. THE SKIN WAS REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: KEELBEAM — DEFECTIVE (FUSELAGE) · airframe 89,115 hrs · 42,359 cycles

DEFECT INDICATION IN THE LOWER FASTENER HOLE COMMON TO THE RIGHT KEEL BEAM CHORD PART NUMBER 145T8611-2 AND STIFFENER PART NUMBER 111T1005-2 AT FUSELAGE STATION 955, RBL 10. THE HOLE WAS REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 89,115 hrs · 42,359 cycles

CORROSION ON STRINGER 25R AND ITS SPLICE CHANNEL AT FUSELAGE STATION 1395. THE STRINGER AND SPLICE CHANNEL WERE REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: FLOORBEAM — CORRODED (BS 1263) · corrosion level 2 · airframe 89,115 hrs · 42,359 cycles

CORROSION ON UPPER T-CHORD OF AFT LOWER COMPARTMENT FLOOR FRAME AT FUSELAGE STATION 1263. THE T-CHORD WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 89,115 hrs · 42,359 cycles

CORROSION ON STRINGER 30R AT FUSELAGE STATION 1480. THE STRINGER WAS REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: FITTING — CORRODED (BS 1582) · corrosion level 2 · airframe 89,115 hrs · 42,359 cycles

CORROSION ON STRINGER 27R END FITTING AT FUSELAGE STATION 1582. THE STRINGER END FITTING WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 89,115 hrs · 42,359 cycles

CORROSION IN STRINGER 38L SPLICE AT FUSELAGE STATION 434. THE STRINGER SPLICE WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 89,115 hrs · 42,359 cycles

CORROSION ON INTERCOSTAL IN THE AFT LOWER COMPARTMENT AT FUSELAGE STATION 1274, LBL 6. THE INTERCOSTAL WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 89,115 hrs · 42,359 cycles

CORROSION ON STRINGER 39R AT FUSELAGE STATION 1555. THE STRINGER WAS REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: STRINGER — CORRODED (BS 1241) · corrosion level 2 · airframe 89,115 hrs · 42,359 cycles

CORROSION ON STRINGER 36R AT FUSELAGE STATION 1241. THE STRINGER WAS REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 89,115 hrs · 42,359 cycles

CORROSION AND A PUNCTURE IN THE WASTE WATER PAN SUPPORT INTERCOSTAL BETWEEN FUSELAGE STATIONS 1562 AND 1582 AT STRINGER 38R. THE INTERCOSTAL WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 89,115 hrs · 42,359 cycles

CORROSION ON THE SHEAR TIE AT FUSELAGE STATION 1351 BETWEEN STRINGERS 35L AND 36L. THE SHEAR TIE WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 89,115 hrs · 42,359 cycles

CORROSION ON THE RIGHT WING LOWER SKIN INBOARD OF LEADING EDGE STATION 160, FORWARD OF THE JACK PAD AREA. THE SKIN WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 89,115 hrs · 42,359 cycles

CRACK IN STRINGER 37R AT FUSELAGE STATION 1307. THE STRINGER WAS REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: STRUCTURE — CORRODED (RT WING) · corrosion level 2 · airframe 89,115 hrs · 42,359 cycles

CORROSION ON THE RIGHT WING REAR SPAR TO LOWER TRAILING EDGE PANEL CHORD AT WING STATION 932. THE CHORD WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 89,115 hrs · 42,359 cycles

CORROSION ON THE FUSELAGE SKIN AT STRINGERS 38L AND 39L AT FUSELAGE STATION 420. THE SKIN WAS REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 89,115 hrs · 42,359 cycles

CORROSION ON STRINGER 33L AT FUSELAGE STATION 1263. THE STRINGER WAS REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: SHEAR TIE — CRACKED (BS 1417) · corrosion level 2 · airframe 89,115 hrs · 42,359 cycles

CRACK AND CORROSION ON THE SHEAR TIE AT FUSELAGE STATION 1417 BETWEEN STRINGERS 35R AND 36R. THE SHEAR TIE WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 89,115 hrs · 42,359 cycles

CORROSION ON INTERCOSTAL IN THE AFT LOWER COMPARTMENT AT FUSELAGE STATION 1274, LBL 22.5. THE INTERCOSTAL WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 89,115 hrs · 42,359 cycles

CORROSION ON THE REAR SPAR BULKHEAD TENSION FITTING LOCATED AT FUSELAGE STATION 950, LBL 88. THE TENSION FITTING WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: RIB — CORRODED (RT WING) · corrosion level 2 · airframe 89,115 hrs · 42,359 cycles

CORROSION ON THE AIR LOAD RIB AT THE #9 SLAT, INBOARD AUXILIARY TRACK. THE RIB WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: SUPPORT — CORRODED (RT WING) · corrosion level 2 · airframe 89,115 hrs · 42,359 cycles

CORROSION ON THE LOWER PANEL SUPPORT AT THE #10 SLAT, RIGHT WING STATION 682. THE SUPPORT WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: STRINGER SPLICE — DAMAGED (BS 434) · airframe 89,115 hrs · 42,359 cycles

HOLE IN STRINGER 37L SPLICE AT FUSELAGE STATION 434. THE STRINGER SPLICE WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: FITTING — CORRODED (BS 1582) · corrosion level 2 · airframe 89,115 hrs · 42,359 cycles

CORROSION ON THE END FITTINGS OF STRINGERS 30R AND 32R AT FUSELAGE STATION 1582. THE STRINGERS END FITTINGS WERE REPLACED. THE AIRPLANE WAS GROUNDED.

Part: STRINGER — CRACKED (FUSELAGE) · corrosion level 2 · airframe 89,115 hrs · 42,359 cycles

CORROSION, CRACK, AND GOUGE IN STRINGER 29R AT FUSELAGE STATIONS 1480 AND 1496. THE STRINGER WAS REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: STRINGER SPLICE — DAMAGED (BS 434) · airframe 89,115 hrs · 42,359 cycles

CRACK AND GOUGES IN STRINGER 36L SPICE AT FUSELAGE STATION 434. THE SPLICE WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: STRAP — CORRODED (BS 1240-1380) · corrosion level 2 · airframe 89,115 hrs · 42,359 cycles

CORROSION ON THE LOWER MAIN SILL FAIL-SAFE STRAP LOCATED IN THE AFT LOWER COMPARTMENT FROM FUSELAGE STATION 1240 TO FUSELAGE STATION 1380, RBL 44.92, WL 124.43. THE FAIL-SAFE STRAP WAS REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 89,115 hrs · 42,359 cycles

CORROSION AND CRACK IN STRINGER 31R AT FUSELAGE STATION 1412. THE STRINGER WAS REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 89,115 hrs · 42,359 cycles

CORROSION ON THE SHEAR TIE AT FUSELAGE STATION 1373 BETWEEN STRINGERS 36L AND 37L. THE SHEAR TIE WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: STRUCTURE — CORRODED (RT WING) · corrosion level 2 · airframe 89,115 hrs · 42,359 cycles

CORROSION ON THE RIGHT WING REAR SPAR TO LOWER TRAILING EDGE PANEL CHORD AT WING STATION 1054. THE CHORD WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: SHEAR TIE — DAMAGED (FUSELAGE) · airframe 89,115 hrs · 42,359 cycles

DAMAGE ON THE SHEAR TIE AT FUSELAGE STATION 1396 BETWEEN STRINGERS 26L AND 27L. THE SHEAR TIE WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: STRINGER — CORRODED (BS 1219) · corrosion level 2 · airframe 89,115 hrs · 42,359 cycles

CORROSION ON STRINGER 39L AT FUSELAGE STATION 1219. THE STRINGER WAS REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: SPAR — CORRODED (LT WING) · corrosion level 2 · airframe 89,115 hrs · 42,359 cycles

CORROSION ON THE LEFT WING TRAILING EDGE AUXILIARY SPAR LOWER CHORD UNDER THE #6 SPOILER. THE CHORD WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 89,115 hrs · 42,359 cycles

CORROSION ON THE UPPER SURFACE OF THE AFT LOWER CARGO DOOR LOWER SILL BEAM AROUND FORWARD LOWER CORNER ROLLER FITTING AND DOOR FITTING AT FUSELAGE STATION 1285. THE ASSOCIATED CHORD WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: STRINGER — CORRODED (HORIZ STAB) · corrosion level 2 · airframe 89,115 hrs · 42,359 cycles

CORROSION ON THE OUTER SURFACE OF THE LOWER HORIZONTAL LEG OF THE #3 UPPER STRINGER, LOCATED AT BL 0 IN THE HORIZONTAL STABILIZER CENTER SECTION. THE STRINGER WAS REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 89,115 hrs · 42,359 cycles

CORROSION ON THE SHEAR TIE AT FUSELAGE STATION 1219 BETWEEN STRINGERS 37L AND 38L. THE SHEAR TIE WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: FLAP — CORRODED (RT WING) · corrosion level 2 · airframe 89,115 hrs · 42,359 cycles

CORROSION ON THE RIGHT WING OUTBOARD TRAILING EDGE FLAP. THE FLAP WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: STRINGER SPLICE — CORRODED (BS 434) · corrosion level 2 · airframe 89,115 hrs · 42,359 cycles

CORROSION IN STRINGER 33L SPLICE AT FUSELAGE STATION 434. THE STRINGER SPLICE WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 89,115 hrs · 42,359 cycles

CORROSION ON STRINGER 37L AT FUSELAGE STATION 420. THE STRINGER WAS REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: SHEAR TIE — CORRODED (BS 742) · corrosion level 2 · airframe 89,115 hrs · 42,359 cycles

CORROSION ON THE SHEAR TIE AT FUSELAGE STATION 742 BETWEEN STRINGERS 34R AND 33R. THE SHEAR TIE WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: RIB — CRACKED (LT WING) · airframe 89,115 hrs · 42,359 cycles

CRACK IN THE LEFT WING RIB CHORD AT WING STATION 416 FORWARD OF THE FRONT SPAR. THE CHORD WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: STRINGER — CRACKED (BS 1461) · airframe 89,115 hrs · 42,359 cycles

CRACK IN STRINGER 39R AT FUSELAGE STATION 1461. THE STRINGER WAS REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: INTERCOSTAL — CORRODED (BS 1274) · corrosion level 2 · airframe 89,115 hrs · 42,359 cycles

CORROSION ON INTERCOSTAL IN THE AFT LOWER COMPARTMENT AT FUSELAGE STATION 1274, LBL 22.5. THE INTERCOSTAL WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: STRINGER — CORRODED (BS 434-445) · corrosion level 2 · airframe 89,115 hrs · 42,359 cycles

CORROSION ON STRINGER 37L AT FUSELAGE STATIONS 434 THROUGH 445. THE STRINGER WAS REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 89,115 hrs · 42,359 cycles

CORROSION ON THE BOTTOM SURFACE OF THE RIGHT WING UPPER SKIN AT THE REAR SPAR BETWEEN WING STATIONS 856 AND 879. THE SKIN WAS REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: SPAR WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 89,115 hrs · 42,359 cycles

CORROSION ON THE CENTER WING REAR SPAR WEB, AT FUSELAGE STATION 955.10, RIGHT BODY BUTT LINE 75, JUST BELOW THE UPPER CHORD. THE WEB WAS REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: STRINGER — CORRODED (BS 1351-1439) · corrosion level 2 · airframe 89,115 hrs · 42,359 cycles

CORROSION ON STRINGER 26R AT FUSELAGE STATIONS 1351, 1417, AND 1439. THE STRINGER WAS REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 89,115 hrs · 42,359 cycles

DAMAGE IN STRINGER 35R AT FUSELAGE STATION 1375. THE STRINGER WAS REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: SKIN — CRACKED (BS 757.3) · airframe 89,068 hrs · 42,326 cycles

CRACK IN THE FUSELAGE SKIN AT BODY STATION 757.3 AND BETWEEN STRINGERS 25R AND 26R. THE SKIN WAS REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 88,896 hrs · 42,229 cycles

CORROSION ON KEELBEAM LOWER OUTBOARD FLANGE BETWEEN BODY STATIONS 795 AND 1045 AND THE LOWER INBOARD FLANGE BETWEEN BODY STATIONS 966 AND 917. THE KEEL BEAM FLANGES WERE REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: SKIN — CORRODED (FUSELAGE) · airframe 88,887 hrs · 42,224 cycles

CORROSION, CRACKED, AND POPPED FASTENER HEADS IN FUSELAGE SKIN AT BODY STATION 1502 BETWEEN STRINGERS 32R AND 33R. THE SKIN WAS REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: ESCAPE ROPE — OUT OF POSITION (NR 7) · airframe 85,990 hrs · 40,965 cycles

NR 7 DESCENT DEVICE AND ESCAPE ROPES WERE FOUND OUT OF POSITION. THE AIRPLANE WAS GROUNDED. REPAIRED IAW AMM 25-61-03-2.

Part: SOFTWARE — DEFECTIVE (COCKPIT) · airframe 84,374 hrs · 40,256 cycles

THE LT & RT PRIMARY FLIGHT DISPLAYS FLASHED NUMEROUS TIMES THEN BOTH FAILED. THE LT & RT NAVIGATIONAL DISPLAYS FLASHED & FAILED INTERMITTENTLY. REPLACED THE CTR & RT DATA CONCENTRATOR UNITS. THE CAUSE OF THE DISPLAY UNITS FLASHING & FAILING WAS INCOMPATIBLE SOFTWARE AMONG THE FOUR DISPLAY ASSEMBLIES & THE THREE DATA CONCENTRATOR UNITS. THIS AIRPLANE IS EQUIPPED WITH A FLAT PANEL DISPLAY SYS THAT WAS INSTALLED IAW STC ST02165NY.

Part: SKIN — SCRATCHED (FUSELAGE) · airframe 82,950 hrs · 39,572 cycles

APPROXIMATELY STATION 434R TO 676R, STRINGER 2R MULTIPLE SCRATCHES. REQUEST ENGINEERING EVALUATION. MEASURED ALL SCRATCHES, SEE PARTIAL WORK ON BACK FOR EXACT MEASUREMENTS. REPAIRED SCRATCHES IAW 53-30-71 & REA B653-61512-MR. SDR INFO, PN 143T3120, PART NAME, SKIN, EXACT FS & BS LOCATION ON ACFT 552 - 571. EXACT STRINGER & WS LOCATION ON ACFT STRINGER 2R. ACFT WAS GNDED.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 82,950 hrs · 39,572 cycles

STATION 425R, STRINGER 17R DAMAGE ON LAP SEAM. COMPLETED M 287, SEE REA B653-61513-MR FOR REPAIR. DAMAGE WAS REMOVED & REPAIRED IAW REA B653-61513-MR. SDR INFO, PN 141T3330, SN, NA, PART NAME, FUSELAGE SKIN, FS & BS LOCATION FROM 425 - 419, STRINGER & WS LOCATION FROM STRINGER 17R TO N/A. ACFT WAS GNDED.

Part: SKIN — SCRATCHED (FUSELAGE) · airframe 82,950 hrs · 39,572 cycles

STATION 217R, STRINGER 21R VERTICAL SCRATCH ON LAPSEAM. NON-ROUTINE WAS COMPLIED WITH ON REA B653-61516-MR & REA B653-61516 MR. DAMAGE WAS R & R REA'S B653-61516-MR & B653-61517. SDR INFO, PN141T3211, PART NAME: SKIN, FS LOCATION 217 - 218, STRINGER LOCATION 21R -21R. ACFT WAS GNDED.

Part: SKIN — SCRATCHED (FUSELAGE) · airframe 82,950 hrs · 39,572 cycles

STATION 317L, STRINGER 36L DAMAGE MARKED IN LAP SEAM. REPAIRED IAW REA B653-61514-MR. SDR INFO, SCRATCH, PN 141T3230, SN NSN, PART NAME, FUSELAGE SKIN, FROM FS 317 - 317, FROM STRINGER 37L - 36L. ACFT WAS GNDED.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 82,950 hrs · 39,572 cycles

EXTERIOR SKIN CORRODED & BLOWN OUT AT STATION 1307 STRINGER 37L. REQUEST ENGINEERING ASSISTANCE FOR REPAIR. REMOVED BALL MAT, VHF ANTENNA, TRAY, POWER STEP, ROLLER, WEB & GUSSET. REPAIRED AREA IAW REA B653-61463-MR HOLE & EDGE SCANS OF DAMAGED AREA COMPLIED WITH. REINSTALLED BALL MAT, VHF ANTENNA TRAY, POWER STEP, TRAY, WEB & GUSSET. OPERATIONS CHECKED OK VHF ANTENNA GOOD. SDR INFO CORRODED, PN 146T3203-1, PART NAME FUSELAGE SKIN, FS & BS LOCATION, 1300 TO 1330, STRINGER & WS LOCATION, STRINGER 38R - 36L. ACFT WAS GNDED.

Part: RIB — CORRODED (RT WING) · corrosion level 2 · airframe 82,950 hrs · 39,572 cycles

NUMBER 8 FLAP SUPPORT 3 & 4 TENSION BOLT HOLES HAVE DEFECT INDICATIONS WITH ROTARY SCAN, POSSIBLE CORROSION. NR 8 SUPPORT HOLES REAMED IAW REA-B657-61484-MR. SDR INFO, PN 113T1345-44, PART NAME, NR 8 RIB, CORRODED LEVEL 2, FROM NR 8 FLAP SUPPORT. ACFT WAS GNDED.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 82,950 hrs · 39,572 cycles

STATION 1562L FOUND CORROSION ABOVE OUTFLOW VLV ON STRINGER. R & R STRINGER 31 LT AT STATION 1540 IAW SRM 53-00-03. SDR INFO, PN 146T3008, PART NAME, STRINGER, SN, NSN, CORRODED: LEVEL 2, EXACT FS & BS LOCATION ON ACFT 1540.00 TO 1543.00. EXACT STRINGER & WS LOCATION ACFT, STRINGER 31L TO 31L. ACFT WAS GNDED.

Part: SUPPORT — CORRODED (TE FLAP) · corrosion level 2 · airframe 82,950 hrs · 39,572 cycles

NUMBER 7 FLAP SUPPORT NR 3 HOLE HAS DEFECT INDICATION WITH ROTARY SCAN, POSSIBLE CORROSION. NR 7 SUPPORT HOLES REAMED IAW REA-B657-61484-MR. SDR INFO, PN A13T1345-48, PART NAME NR 7 FLAP SUPPORT, CORRODED LEVEL 2, FROM NR 7 FLAP SUPPORT. ACFT WAS GNDED.

Part: SUPPORT — CORRODED (TE FLAP) · corrosion level 2 · airframe 82,950 hrs · 39,572 cycles

NUMBER 1 FLAP SUPPORT NR 1, 2 & 4 HOLES HAVE DEFECT INDICATION WITH ROTARY SCAN, POSSIBLE CORROSION. NR 1 SUPPORT HOLES REAMED IAW REA-B657-61484-MR. SDR INFO, PN 113T1345-43, PART NAME, NR 1 FLAP SUPPORT, CORRODED LEVEL 2, FROM NR 1 FLAP SUPPORT. ACFT WAS GNDED.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 82,950 hrs · 39,572 cycles

AFT LOWER CARGO STRINGER SPLICE AT STATION 1307, STRINGER 37L IS EXFOLIATED AT AFT SIDE OF SPLICE. SPLICED NEW SECTION AT STRINGER 37L FROM FS 1275 - 1337 IAW SRM 53-00-03. SDR INFO, CORRODED, PN 46T3003, PART NAME, STRINGER, FS & BS LOCATION 1275 TO 1337, STRINGER & WS LOCATION: STRINGER 37L TO NA. ACFT WAS GRNDED.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 82,950 hrs · 39,572 cycles

AFT LOWER CARGO STRINGER SPLICE AT STATION 1307, STRINGER 36L IS EXFOLIATED ON THE FWD SIDE OF SPLICE. SPLICED NEW STRINGER SECTION AT FS 1275 TO 1307 IAW SRM 53-00-03. SDR INFO, CORRODED, PN 146T3003, PART NAME STRINGER 36L, FS & BS LOCATION ON ACFT 1275 TO 1307, STRINGERS & WS LOCATION ON ACFT 36L TO N/A. ACFT WAS GNDED.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 82,950 hrs · 39,572 cycles

STATION 676, STRINGER 7L FOUND CRACKED. DAMAGED STRINGER WAS REPAIRED IAW SRM 53-00-03. SDR, CRACK 1, 1.5", PART NAME, STRINGER, PN BAC 1498-20-6, SN N/A, FS LOCATION, 676 TO 678, STRINGER LOCATION 7L TO 7L. ACFT WAS GNDED.

Part: SKIN — GOUGED (FUSELAGE) · airframe 82,950 hrs · 39,572 cycles

STATION 676 LT BETWEEN STRINGER 20L & 21L, REPAIR COVERS AFT ROW OF MDCD SURROUND SKIN CIRCUMFERENTIAL SPLICE. JC S53-30-F27-DB STEP 03 NOTE STATES THIS TO BE A DISCREPANCY. HFEC CANNOT BE COMPLETED AT LOCATION INDICATED, CONTACT ENGINEERING FOR DISPOSITION. REMOVED & REPAIRED DOUBLER & FILLER. NEW REPAIR TO BE COMPLIED WITH ON REA -B652-61472-MR. SDR INFO, PN 143T3320-1, PART NAME, SKIN ASSEMBLY, SN, N/A, FS LOCATION: 676 - 676, STRINGER LOCATION: 20L - 21L. ACFT WAS GNDED.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 82,950 hrs · 39,572 cycles

STATION 412 - 434, STRINGER 13R CRACKED OVER RIVET HEAD. R & R DAMAGED STRINGER 13 LIGHT AT STATION 412 - 434 IAW SRM 300-03. SDR, CRACK 1, 0.5", 2, 2", PN BAC 1498 - 207, PART NAME, STRINGER, SN N/A, FS LOCATION 412, 434 TO 411, 436. STRINGER LOCATION, 13R TO 13R. ACFT WAS GNDED.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 82,950 hrs · 39,572 cycles

INSTALLED NEW STRINGER, SPLICE PLATES & STRINGER BRACKETS IAW SRM 53-00-03. SDR, CRACKED 1, 1/4 INCHES, 2, .5 INCHES. FS LOCATION 681 TO 685, STRINGER LOCATION L13 TO L13. ACFT WAS GNDED.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 82,950 hrs · 39,572 cycles

STATION 676, STRINGER 11L FOUND CRACKED. R & R CRACKED SECTION OF STRINGER IAW SRM 53-00-03. SDR INFO, PN BAC 1498-142, PART NAME, STRINGER, CRACKED 3 INCHES, EXACT FS & BS LOCATION ON ACFT 676 TO 679, EXACT STRINGER & WS LOCATION ON ACFT 11L. ACFT WAS GNDED.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 82,950 hrs · 39,572 cycles

SKIN IS BULGED UP & FASTENER HEAD IS SHEARED & ROTATED AT FS STATION 440, STRINGER 39L. REMOVED SKIN CORROSION, REPLACED STRINGER 39L IAW SRM 53-00-01 & SRM 51-40-02. SDR INFO, PN BAC 1498-205, PART NAME, STRINGER 39L, CORRODED, EXACT FS & BS LOCATION ON ACFT, FS 434 TO FS 456, EXACT STRINGER & WS LOCATION ON ACFT STRINGER 39L. ACFT WAS GNDED.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 82,950 hrs · 39,572 cycles

STATION 676, STRINGER 12L FOUND CRACKED. R & R DAMAGED STRINGER IAW SRM 53-00-03. SDR, CRACKED 1.5 INCHES, PN BAC 1498 - 207, PART NAME, STRINGER, FS LOCATION FROM 681 TO 682.5, STRINGER LOCATION, L12, SN 1334400 & 1334764. ACFT WAS GNDED.

Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 82,950 hrs · 39,572 cycles

CORROSION FOUND ON LT KEEL BEAM UPPER SURFACE, VIEWED FROM WW STATION 955 - 1015. REMOVED CORROSION & REPAIRED IAW REA B653-61465-MR. SDR INFO, CORRODED, PN 145T8611-1, PART NAME, KEEL BEAM, EXACT FS 966 - 1014, EXACT STRINGER & WS LBL 10 LBL 10. ACFT WAS GNDED.

Part: SKIN — CRACKED (FUSELAGE) · airframe 82,950 hrs · 39,572 cycles

FUSELAGE EXTERNAL SKIN HAS 3 CRACKS 3/4", 1 3/4" & 1/2" AT STATION 1659 - 1662, APPROX STRINGER 13R. REPAIRED FUSELAGE EXTERNAL SKIN IAW SRM 53-80-01 REPAIR 7. SDR INFO, PN 148T3131, SN NSN, CRACKED 3", EXACT FS & BS LOCATION ON ACFT 1659 - 1662, EXACT STRINGER & WS LOCATION ON ACFT 13R TO 13R. ACFT WAS GNDED.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 82,950 hrs · 39,572 cycles

STATION 676 STRINGER 1R FOUND CRACKED. R & R DAMAGED STRINGER AT STAB 676, STATION 1 IAW SPM 53-00-03. OPERATIONS CHECK FOR VHF ANTENNA STATION 715, STATION 1 RT & 1 LT TO BE COMPLETED ON NR 0960. SDR, CRACKED 1/4", PN BAC 1498-203, PART NAME, CHANNEL HAT SECTION, SN NA, FS LOCATION 676 TO 680. ACFT WAS GNDED.

Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 82,950 hrs · 39,572 cycles

KEEL BEAM LOWER CHORD CORRODED AT STATION 820, RBL 10. CORROSION WAS REMOVED, EVALUATED & REPAIRED IAW SRM 53-50-12. SDR INFO, CORROSION, PN 145T8700, PART NAME, KEEL BEAM, LOCATION 820 - 822, RBL10 TO RBL10. ACFT WAS GNDED.

Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 82,950 hrs · 39,572 cycles

KEEL BEAM, LOWER CHORD CORRODED AT STATION 805 LBL 10. CORROSION WAS REMOVED, EVALUATED & REPAIRED IAW SRM 53-50-12. SDR INFO, CORRODED, PN 145T8700, PART NAME, KEEL BEAM, LOCATION FS & BS FROM: 805 TO 806, LOCATION STRINGER & WS, FROM: LBL10 TO LBL I0. ACFT WAS GNDED.

Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 82,950 hrs · 39,572 cycles

KEEL BEAM, LOWER CHORD CORRODED AT STATION 795, LBL 10 UPPER & LOWER SIDE. CORROSION WAS REMOVED, EVALUATED & REPAIRED IAW SRM 53-50-12. SDR INFO, CORROSION, PN 145T8700, PART NAME, KEEL BEAM, LOCATION FROM 796 TO 796, LBL10 TO LBL10. ACFT WAS GNDED.

Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 82,950 hrs · 39,572 cycles

KEEL BEEM LOWER CHORD CORRODED AT STATION 816, RBL 10. CORROSION WAS REMOVED, EVALUATED & REPAIRED IAW SRM 53-50-12. SDR INFO, CORRODED, PN 145T8700, PART NAME, KEEL BEAM, FS & BS LOCATION, 816 TO 817, STRINGER & WS LOCATION, RBL10 TO RBL10. ACFT WAS GNDED.

Part: SWITCH — OUT OF ADJUST (CARGO DOOR) · airframe 82,863 hrs · 39,522 cycles

MAIN CARGO DOOR WARNING LIGHT ILLUMINATED DURING CLIMB THROUGH FL290. CABIN WAS PRESSURIZED NORMALLY. DEPRESSURIZED & DESCENDED TO 10,000 FEET. LIGHT EXTINGUISHED. INDICATION SWITCHES GAP ADJUSTED TO TOLERANCE. WORN DOOR MECHANISM CAUSING SWITCH GAP TO FALL OUT OF TOLERANCE.

Part: STRINGER — CORRODED (ZONE 100) · airframe 80,953 hrs · 38,437 cycles

FUSELAGE SKIN CORRODED AND SKIN DAMAGED AT BS 1351-1373. REPAIRED IAW SRM 53-00-03, FIG 201, REPAIR NR 2, ACFT GROUNDED.

Part: WEB — CORRODED (ZONE 100) · airframe 80,953 hrs · 38,437 cycles

CORROSION ON WEB AT BS 1395. R & R IAW SRM 51-40-02, ACFT WAS GROUNDED.

Part: STRINGER — CRACKED (ZONE 100) · airframe 80,953 hrs · 38,437 cycles

STRINGER 31R CRACKED AT BS 1087. REMOVED CRACKED SECTION OF STRINGER AND REPAIRED IAW SRM 53-00-03, REPAIR 2, ACFT GROUNDED.

Part: STRINGER — CRACKED (ZONE 200) · airframe 80,953 hrs · 38,437 cycles

BS 1307, STRINGER S2R CRACKED. REPAIRED DAMAGED STRINGER 2R IAW SRM 53-00-63 AND 51-40-02. SHEET NR 80. ACFT GROUNDED.

Part: CHANNEL — CRACKED (ZONE 200) · airframe 80,953 hrs · 38,437 cycles

BS 1367, OVERTOP OF AIRBOX INBETWEEN STRINGER 2R-3R, FOUND CRACKED. FABRICATED AND INSTALLED HAT SECTION, 2 ANGLES AND 1 CHANNEL IAW SRM 53-00-03, FIG 1, DETAIL I III, SRM 51-40-02. ACFT WAS GROUNDED.

Part: STRINGER — CRACKED (ZONE 100) · airframe 80,953 hrs · 38,437 cycles

STRINGER 33R CRACKED AT BS 1087, ACFT GROUNDED. REPAIRED STRINGER IAW SRM 53-00-03, REPAIR 2.

Part: SKIN — DENTED (ZONE 100) · airframe 80,593 hrs · 38,437 cycles

FUSELAGE SKIN DENTED AND SCRATCHED. ACFT WAS GROUNDED. INSTALLED REPAIR FILLERS AND DOUBLER IAW REA B653-60582-MR.

Part: KEELBEAM — CORRODED (ZONE 100) · airframe 80,953 hrs · 38,437 cycles

CORROSION AT LEFT KEELBEAM OTBD LOWER FLANGE AT FS 792. BLENDED CORROSION FOUND OUT OF LIMITS. HFEC FOUND NO FURTHER DEFECT. REPAIRED FLANGE IAW REA-B653-60568-MR, ACFT WAS GROUNDED.

Part: KEELBEAM — CORRODED (BS 876) · airframe 80,953 hrs · 38,437 cycles

KEEL BEAM RT SIDE LOWER FLANGE FS 876 CORRODED. ACFT GROUNDED, BLENDED AREA IAW SRM 53-50-12, FIG 101. AREA IS WITHIN LIMITS .

Part: SKIN — CORRODED (ZONE 500) · airframe 80,953 hrs · 38,437 cycles

CORROSION ON LT WING T/E UPPER WING SKIN (SURFACE) WS 805. ACFT GROUNDED. REMOVED FASTENERS, BLENDED OUT CORROSION AND REINSTALLED FASTENERS IAW SRM 51-40-02 AND REA B657-60572-MR,

Part: SPAR — CORRODED (ZONE 500) · airframe 80,953 hrs · 38,437 cycles

LEFT WING AT UPPER REAR SPAR WS 975 JUST AFT OF OTBD AILERON FOUND WITH CORROSION UNDER COMPOSITE PANEL JUST FWD OF OTBD AILERON, BLENDED CORRODED AREA FOUND TO BE OUT OF LIMITS. REPAIRED AREA IAW REA B657-60579-MR AND IAW SRM 51-40-02. ACFT WAS GROUNDED.

Part: BEAM — CORRODED (ZONE 100) · airframe 80,953 hrs · 38,437 cycles

LEFT WHEEL WELL TRANSVERSE BEAM BS 1021 HAS CORROSION ON OTBD LOWER TEE. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED SECTION AND REPAIRED IAW SRM 51-70-12, FIG 1, ACFT WAS GROUNDED.

Part: BEAM — CRACKED (NR 2 PYLON) · airframe 80,953 hrs · 38,437 cycles

AREA JUST BELOW PANEL 437ERX OF NR 2 OTBD PYLON IS CRACKED IN TWO PLACES AT THE PERIMETER OF FASTENER HOLES NEAR THE FLOATING NUT PLATES. R & R OTBD BEAM ON NR 2 PYLON IAW SRM 51-40-02. ACFT WAS GROUNDED.

Part: INTERCOSTAL — CORRODED (ZONE 100) · airframe 80,953 hrs · 38,437 cycles

INTERCOSTAL AFT AND INBD OF AFT DOOR ACTUATOR BENT AND CORRODED. INTERCOSTAL AFT AND INBD OF AFT CARGO DOOR WAS REMOVED AN REPLACED IAW SRM 51-40-02, ACFT WAS GROUNDED.

Part: FLOOR SUPPORT — CORRODED (BS 858) · airframe 80,953 hrs · 38,437 cycles

WING CENTER SECTION HAS AN AREA OF CORROSION UNDER FLOOR PANEL 241J, BS 858, LBL 70 UNDER SUPPORT, ACFT WAS GROUNDED.

Part: STRINGER — CRACKED (ZONE 200) · airframe 80,953 hrs · 38,437 cycles

FORWARD OF BS 456 RT STRINGER 10 CRACKED. REMOVED DAMAGED SECTION OF STRINGER BS 434 TO 466 AND INSTALLED REPAIR SECTION IAW SRM 53-00-03. ACFT WAS GROUNDED.

Part: WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 80,953 hrs · 38,437 cycles

CORROSION NOTED AT BULK CARGO DOOR LOWER SILL CUTOUT STRUCTURE BS 1440. R & R CORRODED WEB IAW SRM 51-40-02. GROUNDED.

Part: CHANNEL — CRACKED (ZONE 600) · airframe 80,953 hrs · 38,437 cycles

RIGHT INBD HYD BAY ACCESS LOWER CHANNEL FOUND CRACKED AT AFT UPPER FASTENER. ACFT GROUNDED. R & R CHANNEL. REMOVED AND REINSTALLED HYD DRAIN LINE IAW SRM 51-40-02.

Part: PROXIMITY SWITCH — OUT OF ADJUST (ENTRY DOOR) · airframe 80,170 hrs · 37,672 cycles

L FWD ENT DOOR EICAS MESSAGE ILLUMINATED AFTER ENGINE START AND EXTERIOR EMERGENCY EXIT LIGHT ON. ADJUSTED 1 PROX SW S194, AWG.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 79,988 hrs · 37,603 cycles

EMERGENCY LIGHTS AT DOOR CUTOUT R1 AND L1 INOP. REMOVED AND REPLACED POWER SUPPLY OPS CHECK OK. REF M/M 32-51-07-2, AIRCRAFT WAS NOT GROUNDED.

Part: TEE FITTING — CORRODED (FUSELAGE) · airframe 79,758 hrs · 37,509 cycles

RIGHT FAIL SAFE STRAP T-FITTING IS CORRODED. REMOVED AND REPLACE T-FITTING IAW REA B653-59375 MR.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 79,758 hrs · 37,509 cycles

CRACK AND CORROSION ON SKIN AT STA 1307 S37L-S38L. FABRICATED DOUBLER IAW REA B653-5982-MR.

Part: FAILSAFE — CORRODED (FUSELAGE) · airframe 79,758 hrs · 37,509 cycles

RT FAILSAFE STRAP CORRODED. REMOVED AND REPLACED RT FAILSAFE STRAP IAW REA B653-59389-MR.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 79,758 hrs · 37,509 cycles

STRINGER S11L AT STA 676 CRACKED. REMOVED AND REPLACED STRINGER STA 676 TO 703 IAW REA B653-59379-MR.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 79,758 hrs · 37,509 cycles

STRINGER S8L HAS 5 INCH CRACK IN END CAP RADIUS. REMOVED AND REPLACED STRINGER S8L AT STA 676 TO 705 IAW REA B653-5976-MR REV IR 07-05-2011.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 79,758 hrs · 37,509 cycles

STRINGER S9L AT STA 676 CRACKED. REMOVED AND REPLACED STRINGER STA 676 TO 703 IAW REA B653-59377-MR REV IR 07-05-2011.

Part: FAILSAFE — CORRODED (FUSELAGE) · airframe 79,758 hrs · 37,509 cycles

LT FAILSAFE STRAP AND "T" FITTING CORRODED. REMOVED AND REPLACED FAILSAFE STRAP AND "T" FITTING IAW REAB693-59386-MR.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 79,758 hrs · 37,509 cycles

CRACK IN LOWER RADIUS OF BOEING PRODUCTION STRINGER S11L AT STATION 676. SPLICED IN REPLACEMENT STRINGER SECTION AT 680 AREA IAW REA B653-5979-MR.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 79,758 hrs · 37,509 cycles

STRINGER S10L AT STA 676 CRACKED. REMOVED AND REPLACED STRINGER AT STA 676 TO 703 IAW REA B653-59378-MR REV JR 07-05-2011.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 79,758 hrs · 37,509 cycles

CRACK IN UPPER RADIUS OF BOEING PRODUCTION STRINGER S10L AT STATION 676. SPLICED IN REPLACEMENT STRINGER SECTION AT 680 AREA IAW REA B653-59378-MR.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 79,758 hrs · 37,509 cycles

CRACK IN LOWER RADIUS OF BOEING PRODUCTION STRINGER S9L AT STATION 676. SPLICED IN REPLACEMENT STRINGER SECTION AT 680 AREA IAW REA B653-59377-MR.

Part: PRESSURE DECK — DAMAGED (FUSELAGE) · airframe 79,758 hrs · 37,508 cycles

LEFT PICKLE FORK PRESSURE DECK WEB REQUIRES REPLACEMENT DUE TO FASTENERS INSTALLED DOUBLE FLUSH AND TRIM OUTS AT EXISTING FASTENERS. REMOVED LT PRESSURE WEB. INSTALLED NEW PRESSURE DECK WEB PER REA NR B653-59386-MR AND IAW SRM B767-200 51-40-02, AWG.

Part: FAILSAFE — CRACKED (FUSELAGE) · airframe 79,758 hrs · 37,509 cycles

RT FAILSAFE STRAP CRACKED. REMOVED AND REPLACED RT FAILSAFE STRAP IAW REA B653-59411-MR, REA B653-59428-MR.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 79,758 hrs · 37,509 cycles

CRACK IN UPPER RADIUS OF BOEING PRODUCTION STRINGER S8L AT STATION 676. SPLICED IN REPLACEMENT STRINGER SECTION AT 680 AREA IAW REA B653-59376-MR.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 78,776 hrs · 37,128 cycles

EMERGENCY EXIT LIGHTS POWER SUPPLY M734 PARTIALLY INOP (SOME LIGHTS IN CIRCUIT DO NOT ILLUMINATE). REMOVED AND REPLACED M734 IAW B767 AMM 33-51-07. OPS CHECK GOOD.

Part: WIRE — DAMAGED (APU) · airframe 77,464 hrs · 36,432 cycles

AFTER APU TURNED OFF DURING AFTER START CHECKLIST, APU GEN OFF EICAS MESSAGE WITH APU RUN LIGHT ILLUMINATED. APU GEN OFF LIGHT ILLUMINATED APU GEN FIELD LIGHT NOT ILLUMINATED. REMOVED AND REPLACED APU ECU AS PRECAUTIONARY MEASURE IAW 767 AMM 49-61-05-4, NO HELP. ISOLATED PROBLEM THROUGH D5874P - PIN (6) TO TB26 (G23 BLOCK) FOUND MULTIPLE WIRES DAMAGED (BURNED) IN WIRE BUNDLE W030 BETWEEN E6 RACK AND CONNECTOR D5874P. ITEM REMAINS ON DI.

Part: WARNING LIGHT — FALSE ACTIVATION (CARGO DOOR) · airframe 772,111 hrs · 36,372 cycles

MAIN CARGO DOOR LIGHT ILLUMINATED DURING INITIAL CLIMB. PRESSURIZATION WAS NORMAL. LIGHT EXTINGUISHED AFTER CRUISE FLIGHT AT 10000 FL. OPERATED SEVERAL TIMES MAIN CARGO DOOR AND ALL INDICATION NORMAL IAW AMM 52-32-00-2. VISUALLY INSPECTED DOOR LATCH AND SENSOR. NO DEFECT NOTED. DOOR CLOSE PROPERLY.

Part: PINION GEAR — BROKEN (COCKPIT SEAT) · airframe 76,926 hrs · 36,298 cycles

WHILE RAISING HEIGHT ON F/O'S SEAT, HEARD LOUD SNAP, WENT DOWN AND VERTICAL ADJUSTMENT BECAME INOP BOTH MANUAL AND ELECTRIC. FOUND DRIVE PINION GEAR BROKEN, REPLACED WITH SERVICEABLE PART IAW WEBER AIRCRAFT CMM. OPS CHECKS GOOD.

Part: HINGE FITTING — CRACKED (FUSELAGE) · airframe 76,768 hrs · 36,249 cycles

RT BODY DOOR CTR HINGE AFT FITTING HAS CRACK INDICATION AT LWR O/B HI-LOK HOLE (APPROX 1.5 INCH LONG). REMOVED AND REPLACED RT BODY DOOR CTR HINGE FITTING ASSY 149T6902-6 IAW B76 DWG 149T6902 AND 767 SRM 51-40-02.

Part: DOUBLER — DAMAGED (FUSELAGE) · airframe 76,768 hrs · 36,249 cycles

FUSELAGE SKIN REPAIR IS NICKED AND GOUGED ON FWD EDGE AT AFT LOWER CARGO DOOR CUTOUT LOWER AFT EDGE. PREVIOUS REPAIR DATA TAG INFO AC1011 NRC 7 12-19-96. REMOVED AND REINSTALLED NEW REPAIR DOUBLER IAW B767 SRM 53-00, 51-40-02 ATA 53 P/N 146T3531-1 2024-T3 .080.

Part: MODULE — BROKEN (HYD SYSTEM) · airframe 75,106 hrs · 35,809 cycles

CENTER HYD QTY DECREASED TO ZERO AND SYS PRESS AND QUANTITY LIGHTS ILLUM. EICAS MSG "HYD SYS PRESS AND C HYD QTY." DISPLAYED. AFTER INSP, FOUND RAT CHECKOUT MODULE LEAKING DUE TO CHECK VALVE BROKEN. REMOVED AND REPLACED CHECK OUT MODULE IAW 29-21-11. HYDR SYS "C" REFILLED TO FULL, OP TEST SATISFACTORY.

Part: SKIN — CRACKED (LEFT WING) · airframe 73,184 hrs · 35,077 cycles

LEFT WING LEADING EDGE STRUCTURE HAD A BROKEN FASTENER AND TWO CRACKED MEMBERS AT LEADING EDGE SLAT 160. INSTALLED NEW SKIN IAW B767 SRM 51-40-01.

Part: SKIN — CRACKED (LEFT WING) · airframe 73,184 hrs · 35,077 cycles

LEFT WING LEADING EDGE STRUCTURE HAD A BROKEN FASTENER AND TWO CRACKED MEMBERS AT LEADING EDGE SLAT 160. INSTALLED NEW SKIN IAW B767 SRM 51-40-1.

Part: STRUT — CRACKED (LT ENGINE) · airframe 73,184 hrs · 35,077 cycles

NR 1 ENGINE STRUT INBOARD AFT BEAM INSIDE HYDRAULIC BAY CRACKED AT FORWARD END OF BEAM. INSTALLED NEW BEAM IAW B767 SRM 51-40-2.

Part: SKIN — CRACKED (BS 1767 S4R) · airframe 73,184 hrs · 35,077 cycles

SKIN CRACKED STRINGER 4 RIGHT FS 1767. REPAIRED AREA RIGHT AFT FS 1767 IAW REA B653-56945.

Part: STRINGER — CRACKED (BS 566-588) · airframe 73,184 hrs · 35,077 cycles

STRINGER 36 RIGHT CRACKED BELOW SPLICE REPAIR, BETWEEN FS 566 AND 588. REPAIRED LONGERON 36 RIGHT IAW B767 SRM 53-00-03, FIGURE 201 AND SRM 51-40-1.

Part: SKIN — CRACKED (BS 1654 S4-8L) · airframe 73,184 hrs · 35,077 cycles

SEVERAL FUSELAGE SKIN CRACKS FS 1654.5, STRINGER 4 LEFT, STRINGER 8 LEFT. REPAIRED AREA IAW B767 SRM 53-80-01.

Part: SKIN — CRACKED (BS 1654 S5-6R) · airframe 73,184 hrs · 35,077 cycles

FUSELAGE SKIN CRACKED FS 1654.5 BETWEEN STRINGER 5 AND 6 RIGHT. REPAIRED CRACKED AREA IAW B767 SRM 53-80-01, FIGURE 201.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,184 hrs · 35,077 cycles

SKIN CRACKED AT SERVICE DOOR ENTRY AFT LOWER CORNER INNER SKIN. REPAIRED SERVICE DOOR AFT LOWER CORNER.

Part: FLANGE — LOOSE (LT ENGINE) · airframe 71,464 hrs · 34,387 cycles

ON CLIMBOUT, EICAS MESSAGE LEFT ENGINE OVERHEAT DISPLAYED WITH ENGINE OVERHEAT LIGHT ILLUMINATED. LIGHT REMAINED ILLUMINATED AFTER THRUST REDUCTION. ENGINE WAS SHUTDOWN. DID AIR TURNBACK TO STA SAL. OPENED NR 1 ENGINE COWL, INSPECTED BLEED AIR DUCTING. FOUND LOOSE DUCT FLANGE NEAR TURBINE LOOSE. TIGHTENED FLANGE HARDWARE. RUN-UP NR 1 ENGINE TO 60 - 80 PERCENT N2 LIGHTS AND EICAS MESSAGE REMAINED OUT. ALSO REPLACED FIRE DETECTION CARD IAW DC9 MM 26-10-01. OVERHEAT LOOPS 1 & 2 SYSTEM OPS CHECKED GOOD.

Part: WIRE — OUT OF POSITION (CONNECTOR) · airframe 71,316 hrs · 34,325 cycles

DOOR 1 LEFT EMERGENCY EXIT SIGN INOPERATIVE. FOUND WIRE M748-033-14, MIS-PINNED IN PIN 13 OF CONNECTOR D1084, REPOSITIONED TO PIN 9 OF CONNECTOR D1084. OPS CHECKED GOOD IAW B767 MM 33-51-00-715-801.

Part: WIRE — DAMAGED (CABIN) · airframe 71,213 hrs · 34,295 cycles

L1 EXTERIOR EMERGENCY LIGHTING AT STA 305, 315, & 317 IN SUPERNUMERARY AREA INOPERATIVE. REPAIRED WIRING AT PIN 9 OF CONNECTOR J0984. TEST GOOD IAW B767 MM 33-51-00-5.

Part: FITTING — BROKEN (HYDRAULIC SYS) · airframe 70,841 hrs · 34,144 cycles

LOST CENTER SYSTEM HYDRAULICS ON LANDING INTO GDL. REPLACED BROKEN QUICK DISCONNECT FITTING ON ADP PRESSURE LINKAGE. OPS AND LEAK CHECKED GOOD.