N763CK

Part: FIRE LOOP — FAULTED (ZONE 100) · airframe 92,914 hrs · 29,855 cycles

CARGO FIRE B ROW YELLOW LIGHTS ON,MTX,DEFERRED FOR DEPARTURE IAW MEL 26-16-2-2 MX ACTIONS C/W PLACARDS INSTALLED. AC REMAINS NO ETOPS. REPETITIVE ITEM REQUIRES INSPECTION AFTER EACH FLIGHT. MBCB 12/22/25. LP 38985-25/1 AND RETURNED A/C TO SERVICE.

Part: AUTOTHROTTLE SYS — MALFUNCTIONED · airframe 92,860 hrs · 29,829 cycles

THE AUTO-THROTTLE WOULD NOT ENGAGE DURING THE TAKEOFF ROLL. PERFORMED A LOW SPEED REJECTED TAKEOFF (<30 KNOTS). CLEARED RUNWAY TO TROUBLE SHOOT. FOLLOWED GUIDANCE IN THE MECHANICAL DISCREPANCY FLOW CHART. PERFORMED A FLIGHT CREW DEFERRAL IAW MEL 22-30-1-1 IN CONFERENCE WITH FLIGHT CONTROL AND MAINTENANCE CONTROL. REST OF FLIGHT WAS UNEVENTFUL (NO AUTO-THROTTLE).

Part: FRAME — CORRODED (ZONE 100) · airframe 92,277 hrs · 29,512 cycles

DURING 763CK'S C4 CHECK AT OSC KALITTA, CORROSION WAS FOUND ON THE STA 1153 FRAME ASSEMBLY INNER CHORD (P/N 146T1060-2) IN THE LOWER CARGO COMPARTMENT. THE CHORD HAD TO BE REPLACED DUE TO THE EXTENT OF CORROSION. UPON REMOVAL OF THE CHORD, AN UNDOCUMENTED TRIM OUT OF THE FRAME WEB (P/N 146T1204-3) WAS FOUND AT RBL 6.5. IT WAS DETERMINED THAT THE FRAME WEB COULD NOT BE REPAIRED PER ANY OF THE REPAIRS GIVEN IN THE B767 SRM, SO FLIGHT VEHICLES CONSULTING, INC., WAS CONTACTED TO PROVIDE AN FAA-DER APPROVED REPAIR. THE PURPOSE OF THIS REA IS TO AUTHORIZE AND DOCUMENT ACCOMPLISHMENT OF REF /A/, WHICH IS AN FAA-DER APPROVED REPAIR.ANALYSIS:THE FRAME WEB IS CONSIDERED FCS STRUCTURE PER SRM 51-00-04, 767-FCBS-53-008, NOTE 1. THIS REPAIR IS CLASSIFIED AS MAJOR .ACCOMPLISHED REPAIR ON FRAME WEB STA 1153 RBL 6.5 AS REQUIRED IAW FVCI E.O. 25089-4 REV A.

Part: BEAM — CORRODED (ZONE 100) · airframe 92,277 hrs · 29,512 cycles

DURING 763CK'S C4 CHECK IN OSC, KALITTA MAINTENANCE CORROSION FOUND NOSE WHEEL WELL BEAM STA: 266.5 RIGHT HAND E&E BAY TUNNEL REPAIRED DAMAGED BEAM IAW B767-300 SRM 51-70-12.

Part: FRAME — CRACKED (ZONE 200) · airframe 92,277 hrs · 29,512 cycles

DURING 763CK'S C4 CHECK IN OSC, KALITTA MAINTENANCE FOUND CRACK R1 DOOR THRESHOLD LOWER AFT CORNER MARKED CRACK ACCOMPLISHED REPAIR OF R1 DOOR AFT CORNER IAW B767-300 SRM 53-10-01 REPAIR 1.

Part: SKIN PANEL — DAMAGED (ZONE 500 ELEV) · airframe 92,277 hrs · 29,512 cycles

WHILE 763CK WAS UNDERGOING C-CHECK IN OSC, DAMAGE WAS FOUND ON THE LH INBOARD ELEVATOR (P/N 183T2001-29; S/N 000518).  THE DAMAGE WAS ON THE OUTBOARD EDGE NEAR THE TRAILING EDGE.  SEE FIGURE 1.  REF /A/ DOES NOT PROVIDE LIMITS FOR DAMAGE IN THIS AREA SINCE IT IS CONSIDERED A CRITICAL AREA, AND NO SRM REPAIR IS PROVIDED.  FLIGHT VEHICLES CONSULTING, INC. WAS CONTACTED FOR AN FAA-DER APPROVED REPAIR.  THE PURPOSE OF THIS REA IS TO AUTHORIZE AND DOCUMENT ACCOMPLISHMENT OF REF /B/, WHICH IS AN FAA-DER APPROVED REPAIR.ANALYSIS: THE INBOARD ELEVATOR IS PRIMARY STRUCTURE, AND THE SKIN PANELS ARE PSE. THE SKIN PANELS ARE ALSO NOTE 3A FCS. THIS REPAIR IS CLASSIFIED AS MAJOR. REPAIRED AREA ON L/H INBOARD ELEVATOR TRAILING EDGE APPROX. ELEVATOR STA 138 IAW B767-300 SRM 51-70-17 AND F.V.C.I ENGINEERING ORDER# 25089-1 REV. IR, REFERENCE COMPOSITE HOT BOND REPAIR FORM AND ENGINEERING ORDER FOR STEPS ACCOMPLISHED AND ORIGINAL SIGNATURES.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 92,277 hrs · 29,512 cycles

WHILE 763CK WAS UNDERGOING C-CHECK IN OSC, CORROSION WAS FOUND ON THE UPPER CHORD OF THE STA 228.5 TRANSVERSAL FLOOR BEAM. (P/N 141T5810). THE CORROSION WAS REMOVED BY BLENDING. SOME AREAS WERE BLENDED BEYOND ALLOWABLE LIMITS PER REF /A/ AND NO SRM REPAIR IS PROVIDED. FLIGHT VEHICLES CONSULTING, INC. WAS CONTACTED FOR AN FAA-DER APPROVED REPAIR. THE PURPOSE OF THIS REA IS TO AUTHORIZE AND DOCUMENT ACCOMPLISHMENT OF REF /B/, WHICH IS AN FAA-DER APPROVED REPAIR ANALYSIS: THE TRANSVERSAL FLOOR BEAM AT STA 228.5 IS CONSIDERED MAIN DECK FLOOR STRUCTURE, WHICH IS PRIMARY STRUCTURE. THIS BEAM WAS REINFORCED BY IAI AND IS CONSIDERED FCS. THIS REPAIR IS CLASSIFIED AS MAJOR. ACCOMPLISHED REPAIR ON COCKPIT FLOOR STRUCTURE APPROX STA 212 - 228 APPROX LBL24 IAW FVCI EO 25089-2.

Part: STRINGER — CORRODED (ZONE 100) · airframe 92,277 hrs · 29,512 cycles

DURING 763CK'S C4 CHECK IN OSC, KALITTA MAINTENANCE CORROSION FOUND ON STRINGER 39L AT STA. 1285-1263.ACCOMPLISHED REPAIR OF STRINGER 39L IAW B767-300 SRM 53-00-03 REPAIR 2.

Part: STRINGER — CORRODED (ZONE 100) · airframe 92,277 hrs · 29,512 cycles

DURING 763CK'S C4 CHECK IN OSC, KALITTA MAINTENANCE FOUND BULK CARGO STRINGER AT STA.1540 STR39R HAS EVIDENCE OF CORROSION .REPAIRED STRINGER AT STA 1540 SR39R IAW B767-300 SRM 53-00-03 REPAIR 2.

Part: SKIN PANEL — CORRODED (ZONE 500) · airframe 92,277 hrs · 29,512 cycles

DURING 763CK'S C4 CHECK IN OSC, KALITTA MAINTENANCE FOUND CORROSION ON THE UPPER SKIN PANEL #1 (P/N 112T3301-1) UNDER PANEL #9 (P/N 113T1609-1), AFT OF THE REAR SPAR, WSTA 349.7 - 359. THE CORROSION WAS BLENDED AND FOUND OUT OF LIMITS PER SRM 57-20-01, ALLOWABLE DAMAGE. IT WAS DETERMINED THAT NO SRM REPAIRS COVER THIS AREA. ABX HAS CONTACTED FVCI TO PROVIDE A FAA-DER APPROVED REPAIR. THE PURPOSE OF THIS REA IS TO AUTHORIZE AND DOCUMENT THE ACCOMPLISHMENT OF REF/A/, APPROVED REPAIR.ANALYSIS: WING UPPER SKIN PANEL #1 IS CONSIDERED FCS STRUCTURE PER SRM 51-00-04, GENERAL, TABLE 4, 767-FCBS-57-021. MAJOR REPAIR. ACCOMPLISHED REPAIR AT LT WING UPPER SKIN APPROX WS 314 IAW FVCI EO 25089-5.

Part: SKIN PANEL — CORRODED (ZONE 500) · airframe 92,277 hrs · 29,512 cycles

DURING 763CK'S C4 CHECK AT KALITTA, CORROSION WAS FOUND ON THE LH WING, LOWER SKIN PANEL #3 BETWEEN WING STATION 668.2 - 694.2, RIB 19 - 20 AND A BLENDOUT WAS ACCOMPLISHED. BLENDOUT WAS BEYOND ALLOWABLE LIMITS STATED IN REF /A/. FVCI WAS CONTACTED TO PROVIDE AN FAA-DER APPROVED REPAIR. THE PURPOSE OF THIS REA IS TO AUTHORIZE AND DOCUMENT ACCOMPLISHMENT OF REF /B/, WHICH IS AN FAA-DER APPROVED REPAIR. ANALYSIS:WING SKIN IS CONSIDERED PRIMARY STRUCTURE AND FCBS PER 767-300 SRM 51-00-04 GENERAL, 767-FCBS-57-024. THIS REPAIR IS CLASSIFIED AS MAJOR.ACCOMPLISHED REPAIR AT LEFT WING SKIN LOWER SURFACE LEADING EDGE AT WS 630.2 IAW FLIGHT VEHICLES CONSULTING EO 25089-3 REV B.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 92,277 hrs · 29,512 cycles

DURING 763CK'S C4 CHECK IN OSC, KALITTA MAINTENANCE FOUND SEAT TRACK HAS DAMAGE IN CENTER CHANNEL @ LBL 11, STA 1263-1274 TT41 .ACCOPLISHED REPAIR ON SEAT TRACK AT STA 1274-1209 IAW IAI SRM 53-00-52 REPAIR 3.

Part: FRAME — CRACKED (ZONE 200) · airframe 92,277 hrs · 29,512 cycles

DURING 763CK'S C4 CHECK IN OSC, KALITTA MAINTENANCE CRACK IN STA 903.5, RBL 89, FRAME INNER CHORD FOUND DURING ACCOMP OF ABX-NEA-5300-0050. RPR'D PER ABX-EA-5300-0052. ABX-NEA-5300-0056 WILL INSP REPAIR. NO DTI REQ'D REFERENCE O.O.# 976303244 FOR CORRECTIVE ACTION..

Part: SHUTOFF VALVE — FROZEN (RT ENGINE) · airframe 92,219 hrs · 29,481 cycles

DURING TAXI OUT, RT ENG PRV ON TAKEOFF. ABORTED TAKEOFF ABOUT 120 KTS. RIGHT BRAKES UP TO 9 ON TEMP. REUTRNED TO BLOCKS (BTB). REMOVED AND REPLACED RT ENGINE PRESSURE REGULATING VALVR PER B767 AMM 36-11-18. OPS AND LEAK CK GOOD. A/C REMAINS NO ETOPS. REF LP 38815-81/2 FOR BRAKE CONDITIONAL INSP. PERFORMED HIGH ENERGY STOP INSPECTION PER AMM 05-51-14. NO DEFECTS NOTED.

Part: WARNING LIGHT — FALSE ACTIVATION (HYD SYS) · airframe 92,032 hrs · 29,381 cycles

DURING AFTER START CHECK LIST, C HYD SYS PRESS DISCRETE LIGHT AND EICAS MSG DISPLAYED. QRH PROCEDURE DID NOT FIX THE ISSUE.AC/ REURNED TO THE GATE (BTB) AND MTX GROUNDED A/C, MTX THEN PERFORMED OPS TEST PER AMM 29-11-00, OPS TEST GOOD .MTX THEN RETURNED A/C TO SERVICE AND A/C DEPARTED.

Part: START VALVE — MALFUNCTIONED · airframe 91,944 hrs · 29,315 cycles

DURING TAXI OUT WHILE STARTING RH ENGINE ,RH ENGINE STARTER WILL NOT ENGAGE AFTER START SWITHCH TO GROUND VALVE LIGHT STAYS ON , AC RETURNED TO GATE (BTB) AND MTX GROUNDED AC . MTX DEFERRED RH START VALVE IAW MEL ABX -80-00-2-1 AND RETURNED AC TO SERVICE .

Part: START VALVE — FAULTED (ZONE 400) · airframe 91,918 hrs · 29,294 cycles

DURING TAXI WHILE STARTING RH ENGINE ,RIGHT STARTER CUTOUT EICAS MESSAGE APPEARED AC RETURNED TO GATE (BTB) AND MTX GROUNDED AC MTX DEFERRED RH START VALVE FOR DEPARTURE IAW MEL ABX-80-00-2-1 AND RETURNED AC TO SERVICE

Part: WARNING MESSAGE — FALSE INDICATION · airframe 91,626 hrs · 29,165 cycles

DURING TAXI OUT FLAP/SLAT ELEC. MSG. APPEARED, AC RETURNED TO THE GATE AND MTX GROUNDED THE AC . MTX PERFORMED BITE TEST OF FSEU IAW FIM 27-51-50-00, NO DEFECTS WERE FOUND . RAN BOTH ENGINES AND OPERATED FLAPS AND SLATS HYDRAULICALLY AND ELECTRICALLY NO MEASAGES OR FAULTS FOUND IAW B767 AMM 71-00-00 . MTX RETURNED AC TO SERVICE AND AC DEPARTED .

Part: WARNING MESSAGE — FALSE ACTIVATION (MLG) · airframe 90,922 hrs · 28,822 cycles

DURING TAXI AIR GROUND DISAGREE STATIS MEASEAGE APPEARED AC RETURNED TO GATE AND MAINTENANCE GROUNDED AC . VERIFIED SENSOR 244 CHECKS NORMAL IAW AMM 32-09-08 , VERIFIED LOADING OUT OF LIMITS READJUSTED FRIEGHT. AND RETURNED TO SERVICE

Part: TRANSPONDER — MALFUNCTIONED · airframe 90,807 hrs · 28,769 cycles

DURING TAXI OUT ATC NOT RECEIVING INFO FROM EITHER XPDR . NO EICAS MSG. AC RETURNED TO THE GATE AND MAINTENANCE GROUNDED AC AND PERFORMED OPS CHECK IAW B767 AMM 34-5302 AND ATC WAS PICKING UP SIGNAL NOW AND WAS OPERATING NORMALLY. MAINTENANCE RETURED AC TO SERVICE AND DEPARTED .

Part: SKIN — CRACKED (BS 1654 S15R) · airframe 90,746 hrs · 28,736 cycles

DURING ROUTINE LINE OPERATIONS IN MIA, MAINTENANCE DISCOVERED TWO CRACKS AT THE RH EMPENNAGE SECTION AT STA. 1654.5. AT APPROXIMATELY STRINGER 15R. BOTH CRACKS MEASURE APPROXIMATELY 2¿¿ IN LENGTH. MIA INDICATED THAT THERE WAS NO DENT ASSOCIATED WITH THE CRACK. DUE TO PARTS AVAILABILITY AND THE AIRCRAFT SCHEDULE, ABX AIR MAINTENANCE CONTROL CONTACTED AMES ENGINEERING FOR ANALYSIS AND DISPOSITION.ANALYSIS: THE FUSELAGE SKIN AFT OF STA 1582 IS UNPRESSURIZED BUT IS CONSIDERED PRIMARY, PSE, FCBS STRUCTURE PER 767 SRM 51-00-04. THE SUBJECT AREA OF SKIN IS NOT CONSIDERED A CRITICAL AREA WHERE A HIGH DEGREE OF AERODYNAMIC SMOOTHNESS IS REQUIRED. THE DAMAGED AREA WILL BE INSPECTED TO ENSURE NO FURTHER DAMAGE EXISTS, AND THE SKIN WILL HAVE SPEED TAPE APPLIED TO PREVENT MOISTURE INTRUSION. THIS REA ABX-REA-5300-65396-00 PREPARES N763CK FOR A SINGLE, EMPTY FLIGHT FROM MIA TO CVG FOR FURTHER MAINTENANCE. THIS REPAIR IS CONSIDERED MINOR AND TEMPORARY .REA ISSUED - DMI ISSUED FOR 1 FLIGHT TO CVG. WHILE IN CVG REPAIRED CRACKS IAW B767 SRM 53-80-01, REPAIR 7, DETAIL V. D.I. CLEARED PLACARD REMOVED. NO REACTIVATION PROCEDURE REQUIRED.

Part: ENGINE — UNKNOWN (RIGHT) · airframe 90,695 hrs · 28,705 cycles

ON TAXI OUT RT ENGINE DID NOT STABILIZE AFTER START ON 1ST ATTEMPT .AC RETURNED TO GATE AND MAINTENANCE GROUNDED AC . MAINTENANCE PERFORMED RH ENG RUN PER AMM 71-00-00. AFTER 5 MIN RH ENG VALUES STABLE ( N1& N2 ). RH ENG OPERATES NORMAL. A/C REMAINS NO ETOPS. AC WAS RETURNED TO SERVICE

Part: PITOT HEAD — MALFUNCTIONED (FIRST OFFICER'S) · airframe 90,428 hrs · 28,577 cycles

DURING TAXI F/O PITOT FAILED AFTER ENGINE START . AC RETURNED TO GATE AND MAINTENACE GROUNDED AC . TROUBLE SHOT AND REMOVED AND REPLACED F/O PITOT-STATIC PROBE(THIRD) IAW B767 AMM 34-11-01, OPS CHECK GOOD. HIGH RANGE LEAK GOOD IAW 34-11-00. MAINTENANCE RETURNED AC TO SERVICE .

Part: WARNING LIGHT — ILLUMINATED (ADP) · airframe 90,329 hrs · 28,529 cycles

AFTER BOTH ENG'S STARTED ADP PRESS LGT ILLUMINATED PRESS LGT STAYS ILUMINATED WITH SELECTOR SWITCH IN ON POSTION .AC RETURNED TO THE GATE , MAINTENACE GROUNDED AC DEFERRED ADP FOR DEPARTURE IAW MEL ABX-29-11-3. RETURENED AC TO SERVICE AND DEPARTED. WILL AMEND AFTER REPAIR

Part: CIRCUIT CARD — MALFUNCTIONED (HYD PUMP) · airframe 90,329 hrs · 28,529 cycles

AMENDED:.AFTER BOTH ENG'S STARTED ADP PRESS LGT ILLUMINATED PRESS LGT STAYS ILUMINATED WITH SELECTOR SWITCH IN ON POSTION .AC RETURNED TO THE GATE , MAINTENACE GROUNDED AC DEFERRED ADP FOR DEPARTURE IAW MEL ABX-29-11-3. RETURENED AC TO SERVICE AND DEPARTED. REMOVED AND REPLACED ADP O/S CARD IAW B767 AMM 29-11-69 AND HYD SYS OVHD PANEL ASSY IAW AMM 29-11-40. OPS CHK GOOD. NO MESSAGE PRESENT.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 89,541 hrs · 28,134 cycles

AILERON LOCKOUT MESSAGE DISPLAYED. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE DEFERRED AILERON LOCKOUT SYSTEM PER MEL 27-11-2. AIRCRAFT RETURNED TO SERVICE

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 89,499 hrs · 28,114 cycles

DURING PUSH BACK MAINTENANCE NOTED TOILET DOOR SERVICE SNAPPED. REALLIGHNMENT HINGE SPRINGS AND SECURED DOOR CLOSED IAW AMM 52-49-07

Part: STARTER — FAILED (RT ENGINE) · airframe 89,370 hrs · 28,010 cycles

#2 ENGINE DID NOT ROTATE WHEN SELECTED TO START. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE REMOVED AND REPLACED RH STARTER, REF AMM 80-11-01 OPS CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — UNKNOWN (UKNOWN) · airframe 89,081 hrs · 27,858 cycles

AFTER PUSHBACK NOSE A/G SYS EICAS ADVISORY AND NOSE A/G DISAGREE STATUS MESSAGE APPEARED. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE PERFORMED BITE OF PSEU NO DEFECTS PER B767 AMM 32-09-11 NO STORED FAULTS OR ACTIVE FAULTS. AIRCRAFT RETURNED TO SERVICE.

Part: RIB — GOUGED (ZONE 600) · airframe 89,055 hrs · 27,833 cycles

WHILE IN C-CHECK AT KALITTA IN OSC. IT WAS FOUND THAT RIGHT WING LEADING EDGE BULL NOSE PANEL GOUGED AT APPROX LES 500.10, TD10. AFTER BLENDING IT WAS FOUND TO BE BEYOND ALLOWABLE LIMITS. ENGINEERING WAS CONTACTEDFOR A REPAIR. AN FAA-DER APPROVED AND REPAIR WAS COMPLETED ON ABX-REA-5740-64985-00.

Part: THRUST REVERSER — NOT CLOSED (RIGHT) · airframe 88,752 hrs · 27,670 cycles

ON PUSH OUT, NOTICED R/H I/B TR NOT STOWED FULLY. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE PROPERLY DEFERRED R/H T/R IAW ABX MEL 78-31-1A. DI REMAINS OPEN. AC REMAINS CAT 3A. AIRCRAFT RETURNED TO SERVICE.

Part: NONE — UNKNOWN (CAPTAIN'S SEAT) · airframe 88,530 hrs · 27,520 cycles

CAPTAIN'S SIDE EMERGENCY FLASHLIGHT INOP REMOVED AND REPALCED CAPTAIN'S SIDE EMERGENCY FLASHLIGHT BATTERY IAW B767-300 AMM 25-54-02 OPERATIONS CHECK GOOD NO DEFECTS NOTED

Part: STRUCTURE — DAMAGED (RT AILERON) · airframe 86,282 hrs · 26,591 cycles

R/H INBD AILERON OTBD FACE DAMAGED NEAR HINGE

Part: SEAT TRACK — CRACKED (COCKPIT) · airframe 86,282 hrs · 26,591 cycles

CAPTAINS INBOARD AFT SEAT TRACK P/N 1A097-0105 CRACKED

Part: SEAT TRACK — CRACKED (COCKPIT) · airframe 86,282 hrs · 26,591 cycles

FIRST OFFICERS OUTBOARD AFT SEAT TRACK P/N 1A097-0508 CRACKED

Part: SEAT TRACK — CRACKED (COCKPIT) · airframe 86,282 hrs · 26,591 cycles

CAPTAINS INBOARD SEAT TRACK P/N 1A098-0181 CRACKED

Part: SEAT TRACK — CRACKED (COCKPIT) · airframe 86,282 hrs · 26,591 cycles

CAPTAINS OUTBOARD FWD SEAT TRACK P/N 1A098-0183 CRACKED

Part: SEAT TRACK — CRACKED (COCKPIT) · airframe 86,282 hrs · 26,591 cycles

FIRST OFFICERS FWD INBOARD SEAT TRACK P/N 1A098-0182 CRACKED

Part: SEAT TRACK — CRACKED (COCKPIT) · airframe 86,282 hrs · 26,591 cycles

FIRST OFFICERS AFT INBOARD SEAT TRACK P/N 1A097-0106 CRACKED

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 86,282 hrs · 26,591 cycles

EMERGENCY LIGHT BATTERY M735 FAILS CAPACITY TEST

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 86,282 hrs · 26,591 cycles

EMERGENCY LIGHT BATTERY M736 FAILS CAPACITY TEST

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 84,414 hrs · 25,523 cycles

EMERGENCY LIGHTS ARE ON WHEN AIRCRAFT POWER IS OFF.

Part: CHANNEL — CORRODED (BS 552) · corrosion level 2 · airframe 84,414 hrs · 25,523 cycles

FWD PIT; CORROSION ON "Z" CHANNEL FLOOR SUPPORT @ STA 552 LBL 43

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 84,414 hrs · 25,523 cycles

FWD PIT LWR FRAME UPPER CHORD HAS EVIDENCE OF CORROSION AT STA 654 +110 RBL 21.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 84,414 hrs · 25,523 cycles

FWD PIT FLOOR WEB CORRODED AT STA 654 +70 RBL 20.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 84,414 hrs · 25,523 cycles

FWD PIT LWR FRAME UPPER CHORD HAS EVIDENCE OF CORROSION AT STA 676 RBL 21.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 84,414 hrs · 25,523 cycles

WEB BENEATH ROLLER TRAY IN FWD PIT STATION 654 +88, LBL APPRX 6 IS CORRODED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 84,414 hrs · 25,523 cycles

UPPER CHORD FLOORBEAM STA 654 +121 LBL 8 HAS AREA OF CORROSION.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 84,414 hrs · 25,523 cycles

UPPER CHORD FLOORBEAM STA 720 LBL 8 HAS AREA OF CORROSION.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 84,414 hrs · 25,523 cycles

FWD PIT LOWER FRAME UPPER CHORD HAS EVIDENCE OF CORROSION @ STA 698 RBL 8 TO RBL 14.

Part: TORQUE BOX — CORRODED (FUSELAGE) · corrosion level 2 · airframe 83,230 hrs · 24,485 cycles

FWD PIT STA 478 RBL 36 TORQUE BOX UPPER SKIN HAS EVIDENCE OF CORROSION.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 83,230 hrs · 24,485 cycles

CORROSION ON LOWER SURFACE OF INTERCOSTAL REMOVED FROM STA 478 TO STA 500 AT APPROX RBL 34.

Part: SUPPORT CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 83,230 hrs · 24,485 cycles

FLOOR SUPPORT CHANNEL FROM STA 478 TO STA 500 AT APPROX RBL 32 HAS CORROSION ON LOWER SIDE.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 83,230 hrs · 24,485 cycles

STATION 1809.5 BULKHEAD OUTER CHORD LT SIDE HAS A TIME LIMITED REPAIR INSTALLED. CRACK INDICATION DURING OPEN HOLE INSPECTION.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 83,230 hrs · 24,485 cycles

INVESTIGATE REPAIR AND CUTOUT RADII ON PREVIOUS REPAIR LOCATED IN THE AFT PIT AT APPROX BS 1451 AT STRINGER 38L. CORROSION FOUND UNDER REPAIR.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 83,230 hrs · 24,485 cycles

INTERCOSTAL CORRODED AROUND FASTENER HOLE ON LOWER SIDE AT STA 496 APPROX RBL 25.

Part: WEB — CORRODED (BS 478-537) · corrosion level 2 · airframe 83,230 hrs · 24,485 cycles

WEB AT BS 478 - 537, RBL 32 CORRODED.

Part: FRAME — CORRODED (BS 520) · corrosion level 2 · airframe 83,230 hrs · 24,485 cycles

BS 520 FRAME UPPER ANGLE CORRODED AROUND FASTENER HOLE ON THE LOWER SIDE AT RBL 39.

Part: FLOORBEAM — CORRODED (BS 478) · corrosion level 2 · airframe 83,230 hrs · 24,485 cycles

THE FLOORBEAM AT BS 478, RBL 39, IN THE FWD CARGO BAY HAS EVIDENCE OF CORROSION ON UPPER TEE.

Part: FRAME — CORRODED (BS 513) · corrosion level 2 · airframe 83,230 hrs · 24,485 cycles

FRAME UPPER ANGLE CORRODED AROUND FASTENER HOLE ON THE LOWER SURFACE AT BS 513, RBL 30.

Part: STIFFENER — CRACKED (BS 246) · airframe 83,230 hrs · 24,485 cycles

MAIN DECK FLOORBEAM AT BS 246, LBL 40 HAS TWO CRACKED STIFFENERS

Part: STRAP — CRACKED (FUSELAGE) · airframe 83,230 hrs · 24,485 cycles

CRACK DETECTED ON BULKHEAD OUTER CHORD STRAP STA 1727 STR - 7R.

Part: WEB — CORRODED (BS 1417) · corrosion level 2 · airframe 83,230 hrs · 24,485 cycles

CORROSION FOUND AT BS 1417, LBL 42. ON SILL WEB.

Part: STRINGER — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 83,230 hrs · 24,485 cycles

STRINGER 8, RBL 6 UPPER SURFACE WEB HAS AREA OF CORROSION IN THE HORIZONTAL STABILIZER CENTER SECTION.

Part: SUPPORT — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 83,230 hrs · 24,485 cycles

HORIZONTAL STAB CENTER SECTION LOWER ZEE SUPPORT 11 @ LBL 1 HAS SMALL AREA OF CORROSION

Part: SUPPORT — CORRODED (BS 1067) · corrosion level 2 · airframe 83,230 hrs · 24,485 cycles

SUPPORT BETWEEN RBL 47 & LBL 26.10 HAS EVIDENCE OF CORROSION. IN THE AFT CARGO BAY BS 1067.

Part: RIB — CORRODED (BS 993) · corrosion level 2 · airframe 83,230 hrs · 24,485 cycles

FUSELAGE UPPER LOBE INTERIOR STRUCTURE, LEFT SIDE MAIN DECK INTERIOR EVIDENCE OF CORROSION ON RIB BS 933 & WL 200

Part: DOOR SILL — CORRODED (BS 1417) · corrosion level 2 · airframe 83,230 hrs · 24,485 cycles

CORROSION ON LOWER SIDE OF BULK CARGO DOOR CUTOUT MAIN SILL AT BS 1417

Part: DOOR FRAME — CORRODED (BS 480) · corrosion level 2 · airframe 83,230 hrs · 24,485 cycles

FWD LOWER CARGO DOOR SURROUND STRUCTURE SHOWS EVIDENCE OF CORROSION AT BS 480, RBL 44 ON UPPER SUFACE.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 83,230 hrs · 24,485 cycles

FUSELAGE UPPER LOBE INTERIOR STRUCTURE FWD LT SIDE ESCAPE HATCH LWR SILL (A/C SIDE) HAS EVIDENCE OF CORROSION.

Part: FRAME — CRACKED (FUSELAGE) · airframe 83,230 hrs · 24,485 cycles

BS 903.5 LBL 89 APPROX WL196 FRAME INNER CHORD CRACKED AT LOWER END TRANSITION RADIUS.

Part: FRAME — CORRODED (BS 1480) · corrosion level 2 · airframe 83,218 hrs · 24,480 cycles

CORROSION ON FUSELAGE FRAME AT BS 1480, STRINGER 30L.

Part: WEB — CORRODED (BS 1480-1502) · corrosion level 2 · airframe 83,218 hrs · 24,480 cycles

WEB AT STRINGER 30L SHOWS SIGNS OF CORROSION FROM BS 1480 TO 1502.

Part: FRAME — CORRODED (BS 1502) · corrosion level 2 · airframe 83,218 hrs · 24,480 cycles

FUSELAGE FRAME AT BS 1502, STRINGER 30L SHOWS EVIDENCE OF CORROSION ON THE FORWARD SIDE

Part: STRINGER — CORRODED (BS 1480) · corrosion level 2 · airframe 83,218 hrs · 24,480 cycles

STRINGER 25L IS CORRODED AT STATION 1480

Part: FRAME SPLICE — CORRODED (BS 1480) · corrosion level 2 · airframe 83,218 hrs · 24,480 cycles

FUSELAGE FRAME AT BS 1480, FACTORY SPLICE AREA, IS CORRODED AT STRINGER 25L

Part: STRINGER — CORRODED (BS 1480) · corrosion level 2 · airframe 83,218 hrs · 24,480 cycles

STRINGER 30L HAT CHANNEL IS CORRODED AT STATION 1480.

Part: FRAME SPLICE — CORRODED (BS 1502) · corrosion level 2 · airframe 83,218 hrs · 24,480 cycles

FUSELAGE FRAME AT BS 1502, FACTORY SPLICE AREA, IS CORRODED AT STRINGER 25L

Part: SHEAR TIE — CORRODED (BS 1540) · corrosion level 2 · airframe 83,218 hrs · 24,480 cycles

SHEAR TIE AT BS 1540 BETWEEN STRINGERS 33L & 34L IS CORRODED

Part: SHEAR TIE — CORRODED (BS 1540) · corrosion level 2 · airframe 83,218 hrs · 24,480 cycles

SHEAR TIE AT BS 1540 BETWEEN STRINGERS 32L & 33L IS CORRODED

Part: SHEAR TIE — CORRODED (BS 1540) · corrosion level 2 · airframe 83,218 hrs · 24,480 cycles

SHEAR TIE AT BS 1540 BETWEEN STRINGERS 34L & 35L IS CORRODED

Part: SHEAR TIE — CORRODED (BS 1540) · corrosion level 2 · airframe 83,218 hrs · 24,480 cycles

SHEAR TIE AT BS 1540 BETWEEN STRINGERS 35L & 36L IS CORRODED.

Part: STRINGER CLIP — CORRODED (BS 1540) · corrosion level 2 · airframe 83,218 hrs · 24,480 cycles

STRINGER CLIP AT BS 1540 STRINGER 33L IS CORRODED