N761CX
Registered owner: CARGO AIRCRAFT MANAGEMENT INC, OH (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
RIGHT ENGINE REVERSER UNLOCKED AT FLIGHT LEVEL 380. GREEN, AMBER, GREEN, AMBER NO YAW. NO CONTROL PROBLEM. LIGHT EXTINGUISHED FOR THE REMAINDER OF THE FLT. NO ABNORMAL INDS ON LANDING ROLL WITH THRUST REVERSER DEPLOYED. AIR TRAFFIC CONTROL DECLARED EMERGENCY FOR CREW. NO ABNORMAL INDICATIONS ON LANDING. AIRCRAFT WAS GROUNDED. REPAIRED WIRES W330-01TR-20, W330-015-18, W330-016-18, AND W330-02TB-20 AND CLEANED D4192P IN ACCORDANCE WITH B767 SWPM 20-10-15 AND B767 SWPM 20-61-00. ALL OPERATIONAL CHECKS GOOD. AIRCRAFT RELEASED FOR SERVICE.
SPARE LIFE VEST MISSING FROM SUPERNUMERARY STORAGE CUPBOARD BY L1 DOOR. MINIMUM EQUIPMENT LIST ATI-25-62-01-01 CATEGORY D. DUE 04 OCTOBER 2026. INSTALED LIFE VEST IAW AMM 25-11-01.
COCKPIT DOOR LATCH MISSING. PLACED ON NON-ESSENTIAL FURNISHINGS DEFERRAL 70898 ATI-25-20-01-01-N3011. REMOVED AND REPLACED COCKPIT DOOR HOLD OPEN LATCH IN ACCORDANCE WITH B767 SRM 51-40-02. OPERATIONAL CHECK GOOD. DEFERRAL 70898 CLEARED.
PORTABLE FIRE EXTINGUISHER MOUNTING BRACKET WILL NOT HOLD, FIRE EXTINGUISHER FALLS OFF. PLACED ON DEFERRAL 70338 MINIMUM EQUIPMENT LIST ATI-26-26-01-01 CATEGORY D. REMOVED AND REPLACED FIRE EXTINGUISHER MOUNTING BRACKET IN ACCORDANCE WITH B767 SRM 51-40-02.
EMERGENCY EXIT LIGHT OVERHEAD SWITCH GUARD WILL NOT ARM LIGHTS WHEN CLOSED. REMOVED AND REPLACED SWITCH GUARD IN ACCORDANCE WITH B767 MAINTENANCE MANUAL 33-51-00. OPERATIONAL CHECK GOOD.
EMERGENCY LIGHT A/C EXTERIOR NEXT TO L1 DOOR INOPERATIVE. EMERGENCY LIGHT NEXT TO L1 DOOR REMOVED AND REPLACED PER BOEING 767 AIRCRAFT MAINTENANCE MANUAL 33-51-03. OPERATIONAL CHECK GOOD.
RT HORIZ STAB PIVOT PIN FITTING CORRODED
#1 ENGINE I/B CORE COWL L/E INTERNAL RUB STRIP WORN AND PEELED BACK AT LOWER END
#1 PYLON BRACKET HAS SUPPORTING WEB CRACKED AROUND TIA DUCT SUPPORT
BRACKET ASSY. - PYLON HOLD OPEN ROD.
PANEL 446CR HAS ELONGATED HOLES
NUMBER 2 ENGINE I/B CORE COWL HAS APPROX 6 INCH CRACK ON UPPER AFT. CORNER OF EXTERIOR SKIN
LEFT WING PANEL SUPPORT IN LWW UPPER CHORD IS CORRODED.
UPPER CARGO FLOOR PANEL SUPPORT AT APPPROX STA 670 LBL O HAS CORROSION AROUND FASTENER HOLE.
#1 PYLON ACCESS 436AL CUTOUT KNIFE EDGED AFT LWR
WHILW PERFORMING OK TO CLOSE ON ALC DOOR LINER, FOUND THE DOUBLER LINER HOLE AND THE NEXT THREE HOLES GOING FORWARD TO BE CORRODED.
R1 DOOR CUTOUT LOWER AFT CORNOR STA 335 JUST ABOVE STRINGER 20R LOWER FASTERNER HOLE HAS CRACK INDICATION IN SKIN ONLY.
FUSELAGE STRINGER 1R IS CRACKED IN THE RADIUS STA 676 COMMON TO THE IAI SPLICE
RIGHT WING FIXED LEADING EDGE STRUCTURE CRACKED @ OFSS 410.00.
L-1 ENTRY DOOR AFT LOWER CORNER HAS CRACK INDICATION IN BEAR STRAP AT LOWER HOLE
#1 ENG OTBD T/R UPPER V BAND TAB CHAFFING IN THE FAN CASE AT THE 12:00 POSITION (
FIRE PROTECTION MOUNT BRACKET CORRODED UPPER CARGO STA 654 LBL 3
NUMBER 2 ENGINE I/B T/R HAS A CRACK AT LOWER AFT CORNER
453T2622-8 BRACKET AT STA 654 LBL 3 NEEDS REPLACED.
453T2622-7 BRACKET AT STA 654 LBL3 NEEDS REPLACED.
UPPER CARGO FLOOR INTERCOSTAL FROM APPROX STA 572 TO STA 592 RBL 80 HAS CORROSION ON FLANGE.
CORROSION FOUND ON THE TOP FLANGE OF MAIN CARGO FLOOR FRAME
CORROSION FOUND ON THE TEE ASSEMBLY COMMON TO THE RACEWAY SUPPORT ASSEMBLY ON THE TRAILING EDGE WING IN THE LMLG WW
#1 ENG TURBINE CASE COOLING COMPOSITE RAM AIR SCOOP IS CRACKED. LOCATED ON THE AFT SIDE OF THE FAN CASE BETWEEN THE 1:00 AND 2:00 POSITION
R/H 1809.5 BULKHEAD FWD OUTER CHORD INBOARD FLANGE IS CRACKED AT FASTENER HOLE JUST ABOVE HORIZ STAB PIVOT PIN FITTING
WHILE CLIMBING THROUGH 31,000 FEET CREW REPORTED A LOUD BANG SUSPECT FROM RH ENGINE FOLLOWED BY A VIBRATION, RISE IN EGT AND LOSS OF ENGINE POWER. FOLLOWING ATI QUICK REFERENCE HANDBOOK COMPLIANCE, THE CREW SECURED RIGHT ENGINE, DECLARED AN EMERGENCY LANDING WITH AIR TRAFFIC CONTROL AND DIVERTED TO KTUL. LANDING WAS UNEVENTFUL WITH NO ADDITIONAL PRECAUTIONARY ACTIONS NOTED. SUPPLEMENTAL INFORMATION TO PREVIOUS SUBMITTAL IXXA20240915064 ON 15 SEPTEMBER 2024 AT KILN, RIGHT ENGINE REMOVED AND REPLACED IAW TASK CARDS ATI-24-003-00-01, ATI-26-000-01-01 ATI-36-005-00-02, ATI-71-602-00-02 AND ATI-71-999-03-01. ALL POWERPLANT TESTS AND LEAK CHECKS GOOD. NO ADDITIONAL FAULTS NOTED.
POST FLIGHT CREW REPORTED SUBSEQUENT TO HARD LANDING, INERTIAL REELS IN SUPERNUMERARY DEPLOYED. NO ADDITIONAL FAULTS NOTED. CONDITIONAL INSPECTIONS PHASE 1A AND 1B HARD LANDING INSPECTIONS SATISFACTORY PER BOEING 767 AIRCRAFT MAINTENANCE MANUAL 05-51-30. DEFERRAL MAINTENANCE ITEM 51964 INITIATED FOR 3 EACH INERTIAL ESCAPE REELS DEPLOYED IAW ATI BOEING 767 MINIMUM EQUIPMENT LIST 25-61-01-01. CORRECTIVE ACTIONS DUE 3 JUNE 2024. SUPPLEMENTAL INFORMATION TO PREVIOUS SUBMITTAL ON 28 MAY 2024 AT KILN. DESCENT DEVICES POSITIONS 3, 4, AND 5 REMOVED AND REPLACED PER BOEING 767 AIRCRAFT MAINTENANCE MANUAL 25-61-03. DEFERRAL MAINTENANCE ITEM 51964 CLEARED. .
POST FLIGHT CREW REPORTED SUBSEQUENT TO HARD LANDING, INERTIAL REELS IN SUPERNUMERARY DEPLOYED. NO ADDITIONAL FAULTS NOTED. CONDITIONAL INSPECTIONS PHASE 1A AND 1B HARD LANDING INSPECTIONS SATISFACTORY PER BOEING 767 AIRCRAFT MAINTENANCE MANUAL 05-51-30. DEFERRAL MAINTENANCE ITEM 51964 INITIATED FOR 3 EACH INERTIAL ESCAPE REELS DEPLOYED IAW ATI BOEING 767 MINIMUM EQUIPMENT LIST 25-61-01-01. CORRECTIVE ACTIONS DUE 3 JUNE 2024. SUPPLEMENTAL INFORMATION TO PREVIOUS SUBMITTAL ON 28 MAY 2024 AT KILN. DESCENT DEVICES POSITIONS 3, 4, AND 5 REMOVED AND REPLACED PER BOEING 767 AIRCRAFT MAINTENANCE MANUAL 25-61-03. DEFERRAL MAINTENANCE ITEM 51964 CLEARED.
POST FLIGHT CREW REPORTED SUBSEQUENT TO HARD LANDING, INERTIAL REELS IN SUPERNUMERARY DEPLOYED. NO ADDITIONAL FAULTS NOTED. CONDITIONAL INSPECTIONS PHASE 1A AND 1B HARD LANDING INSPECTIONS SATISFACTORY PER BOEING 767 AIRCRAFT MAINTENANCE MANUAL 05-51-30. DEFERRAL MAINTENANCE ITEM 51964 INITIATED FOR 3 EACH INERTIAL ESCAPE REELS DEPLOYED IAW ATI BOEING 767 MINIMUM EQUIPMENT LIST 25-61-01-01. CORRECTIVE ACTIONS DUE 3 JUNE 2024. SUPPLEMENTAL INFORMATION TO PREVIOUS SUBMITTAL ON 28 MAY 2024 AT KILN. DESCENT DEVICES POSITIONS 3, 4, AND 5 REMOVED AND REPLACED PER BOEING 767 AIRCRAFT MAINTENANCE MANUAL 25-61-03. DEFERRAL MAINTENANCE ITEM 51964 CLEARED.
AFTER TAKE OFF, CREW REPORTED A LOUD POP FOLLOWED BY A RUSH OF AIR AND BODY DUCT LEAK EICAS MESSAGE DISPLAY. THE APU BLEED VALVE WAS TURNED OFF. ALTERNATIVELY, THE CENTER ISOLATION VALVE WOULD NOT CLOSE AND THE DUCT LEAK INDICATION FAILED TO CLEAR. ADDITIONAL ATI QUICK REFERENCE HANDBOOK PROCEDURES WERE COMPLIED WITH, THE LEFT BLEED AND LEFT PACK WERE TURNED OFF. CONVERSELY, THE FAULT LIGHT PERSISTED. AFTER LEVELING OFF IN CRUISE, LOSS OF CABIN PRESSURE. CREW ELECTED FOR DIVERSION TO KPHX WITH AN EMERGENCY DECLARATION. LANDING WAS WITHOUT INCIDENT AND ON ARRIVAL THE AIRCRAFT WAS GROUNDED FOR MAINTENANCE. DURING INSPECTION, FAULT ISOLATED TO APU AIR SUPPLY DUCT SEPARATED AT WELD IN LEFT WHEEL WELL. SUPPLEMENTAL INFORMATION TO PREVIOUS SUBMITTAL IXXA20231031079 ON 31 OCTOBER 2023 AT KILN. DURING AIRCRAFT INSPECTION, LINE MAINTENANCE IDENTIFIED APU AIR SUPPLY DUCT AT LEFT WHEEL WELL DAMAGED AND SEPARATED AT WELD. ADDITIONALLY, SHRAPNEL FROM THE DUCT DAMAGED FLOORBOARD PANEL ASSEMBLY SECTION 45 AT STATION 977 AND LEFT WHEEL WELL WIRING HARNESS ASSEMBLIES W922 OF CENTER AIR SUPPLY ISOLATION VALVE, W930 OF WHEEL WELL LIGHTS, W626 OF LEFT DUCT LEAK DETECTOR, W1326 AND W1330 OF THE HYDRAULIC MOTOR GENERATOR AND W533 OF ACCELEROMETER. REPAIRED DAMAGED PRESSURE DECK PANEL AT STA 977 LEFT WHEEL WELL IAW B767 STRUCTURAL REPAIR MANUAL 53-50-51. HFEC AND BOLT HOLE INSPECTION ON REPAIRED AREA AT THE LEFT SIDE WHEEL WELL PRESSURE DECK PER B767 NONDESTRUCTIVE TEST MANUAL PART 6-51-00-1 AND 51-00-19 GOOD. NO RELEVANT INDICATIONS NOTED. COMPLIED WITH WIRING REPAIRS OF ASSEMBLIES W922, W930, W626, W1326, W1330, AND W533 PER B767 WIRING DIAGRAM MANUAL (WDM) CHAPTERS 36-11-31, 33-31-11, 26-18-31, 24-25-12, 31-31-13, AND B767 STANDARD WIRING PRACTICES MANUAL (SWPM) 20-10-13. REMOVED AND REPLACED TS220 DUCT LEAK DETECTOR IAW B767 AIRCRAFT MAINTENANCE MANUAL (AMM) 26-18-01. SYSTEM OPERATIONAL CHECKS AFFECTED BY DUCT DAMAGE COMPLIED WITH. CENTER AIR SUPPLY ISOLATION VALVE, WHEEL WELL LIGHTS, HYDRAULIC MOTOR GENERATOR, FLIGHT DATA RECORDER, WHEEL WELL DUCT LEAK DETECTION AND WHEEL WELL FIRE DETECTION SYSTEM OPERATIONAL CHECKS GOOD PER B767 AMM CHAPTERS 36-11-00, 33-31-00, 24-25-00, 31-31-00, 26-18-00, AND 26-17-00 RESPECTIVELY. NO FAULTS NOTED. DURING STRUCTURE REPAIRS, MAINTENANCE IDENTIFIED APU FUEL DRAIN TUBE DAMAGED. APU WING CAVITY TUBE REPLACED IAW B767 AMM 28-22-07. OPERATIONAL CHECK GOOD. REMOVED AND REPLACED INITIALLY REPORTED APU AIR DUCT DAMAGED AT WELD AND TWO ADDITIONAL APU AIR DUCTS IN THE LEFT WHEEL WELL PER B767 AMM 36-11-01. LEAK CHECKS GOOD. CARGO COMPARTMENT FLOOR PANEL LOCATED FROM STA 900 TO STA 1025 AND BLL 12 TO BLL 30 REINSTALLED PER B767 IAI SUPPLEMENTAL MAINTENANCE MANUAL. CABIN PRESSURIZATION GROUND TEST SATISFACTORY. DIFFERENTIAL PRESSURE PSI NORMAL. CABIN PRESSURIZATION OPERATIONAL CHECK GOOD IAW B767 AMM 21-31-00. NO ADDITIONAL FAULTS FOUND. AIRCRAFT RELEASED TO SERVICE.
AFTER TAKE OFF, CREW REPORTED A LOUD POP FOLLOWED BY A RUSH OF AIR AND BODY DUCT LEAK EICAS MESSAGE DISPLAY. THE APU BLEED VALVE WAS TURNED OFF. ALTERNATIVELY, THE CENTER ISOLATION VALVE WOULD NOT CLOSE AND THE DUCT LEAK INDICATION FAILED TO CLEAR. ADDITIONAL ATI QUICK REFERENCE HANDBOOK PROCEDURES WERE COMPLIED WITH, THE LEFT BLEED AND LEFT PACK WERE TURNED OFF. CONVERSELY, THE FAULT LIGHT PERSISTED. AFTER LEVELING OFF IN CRUISE, LOSS OF CABIN PRESSURE. CREW ELECTED FOR DIVERSION TO KPHX WITH AN EMERGENCY DECLARATION. LANDING WAS WITHOUT INCIDENT AND ON ARRIVAL THE AIRCRAFT WAS GROUNDED FOR MAINTENANCE. DURING INSPECTION, FAULT ISOLATED TO APU AIR SUPPLY DUCT SEPARATED AT WELD IN LEFT WHEEL WELL. WORK IN PROGRESS.
POST FLIGHT WALKAROUND, ATI QC IDENTIFIED CRACK ON LEFT WING AFT OF SLAT UNDER SLAT FAIRING INBOARD. REMOVED AND REPLACED INBOARD WING LEADING EDGE SKIN PLATE AT LEFT WING AFT OF INBOARD SLAT UNDER SLAT FAIRING INBOARD IAW B767 SRM 51-40-02.
RIGHT ENGINE OIL FILTER EICAS MESSAGE DISPLAYED DURING CLIMB OUT FROM DEPARTURE STATION KRIV. PER ATI-QUICK REFERENCE HANDBOOK, CREW ELECTED TO SHUT DOWN RIGHT ENGINE. AIR TURN BACK WITH EMERGENCY DECLARATION. LANDING WAS WITHOUT INCIDENT AND NO ADDITIONAL PRECAUTIONARY ACTIONS. ON ARRIVAL, AIRCRAFT GROUNDED FOR INSPECTIONS AND FAULT ISOLATION. POWERPLANT ENGINEERING HAS REQUESTED QAR DATA DOWNLOAD. CREW REPORTED RH ENGINE WINDMILLED FOR APPROX 10 MINUTES. NO LOSS OF OIL PRESSURE, OIL QUANTITY OR VIBRATION INDICATIONS PRESENTED. POST FLIGHT, DFDR REMOVED FOR ANALYSIS IAW B767 AMM 31-31-01 AND TELEDYNE CMM 0G2243800-300. PER B767 FIM 79-21 FAULT TREE 802, REMOVED AND REPLACED SCAVENGE OIL FILTER PER B767 AMM 79-21-04. NO LEAKS DETECTED. SAMPLES FOR OIL SPECTRUM ANALYSIS COLLECTED AND FORWARDED FOR EVALUATION. COMPLIED WITH CONTAMINATION "SUPPLEMENTAL" INSPECTION IAW B767 AMM 72-00-00. DRAINED AND SERVICED RH ENGINE OIL TO 20 QUARTS IAW B767 AMM 79-11-00. PERFORMED IDLE RUNS IAW B767AMM 71-00-00. REMOVED AND REPLACEDOIL FILTER DIFFERENTIAL PRESSURE SWITCHIAW B767 AMM 79-35-01. PER B767 AMM71-00-00 POWERPLANT TEST 2, LEAK CHECKGOOD. NO FAULT MESSAGES ON EICASPRESENT. MAX POWER ENGINE RUNS IAW B767 AMM 71-00-00 SATISFACTORY. ALL PARAMETERS WITHIN RANGE IAW B767 AMM 71-01-02. OK FOR SERVICE. PER B767 FIM 79-21-03, RH ENGINE MAGNETIC CHIP DETECTORS CHECK GOOD IAW B767 AMM 72-00-00. NO DEFECTS NOTED. LOW OILPRESSURE CHECK IAW B767 FIM 71-05-FAULT TREE 820 AND NO OIL INSPECTIONIAW B767 AMM 72-00-00 SATISFACTORY.NO FAULTS FOUND. OIL SPECTROGRAPHICANALYSIS GOOD AND NO ADDITIONAL CORRECTIVE ACTIONS RECOMMENDED. RH ENGINE OIL SAMPLES SCHEDULED AT 25-50 AND 75-100 FLIGHT HOURS. AIRCRAFT RELEASED TO SERVICE.
RIGHT ENGINE OIL FILTER EICAS MESSAGE DISPLAYED DURING CLIMB OUT FROM DEPARTURE STATION KRIV. PER ATI-QUICK REFERENCE HANDBOOK, CREW ELECTED TO SHUT DOWN RT ENGINE. AIR TURN BACK WITH EMERGENCY DECLARATION. LANDING WAS WITHOUT INCIDENT AND NO ADDITIONAL PRECAUTIONARY ACTIONS. ON ARRIVAL, AIRCRAFT GROUNDED FOR INSPECTIONS AND FAULT ISOLATION. POWERPLANT ENGINEERING HAS REQUESTED QAR DATA DOWNLOAD. OPEN
BRACKET ABOVE DENSITOMETER IN L/H MAIN TANK, RIB 4 FOUND TO BE CRACKED.
LEFT WHEEL WELL FITTING CORRODED
SEAL RETAINER CORRODED
PYLON PANEL 441AT RUB STRIP BENT
VERTICAL STAB LH AFT TE PANEL SUPPORT CORRODED
AUTFLOW VALVE CAGE CORRODED
FAIRING SUPPORT FRAME CRACKED
FLAP CORROSION
LW #1 PYLON AFT STINGER FAIRING 437DB I/B AFT WING TO FAIRING SUPPORT ANGLE T/E CRACKED
#2 ENGINE, AFT SIDE OF I/B REVERSER, BELOW AND, AFT OF IDG ACCESS DOOR. WHERE LOWER SIDE CORE COWLING SITS ON THRUST REVERSER. RUB STRIP IS CRACKED ABOUT 3 INCHES AND, HAS DENT IN TRAILING EDGE.
LEFT MLG BODY HAS DELAMINATION
LEFT WHEEL WELL UPPER SURFACE OFF REAR SPAR FITTING WHERE THE DOG BONE FITTING ATTACHES TO REAR SPAR FITTING CORROSION UNDER HARDWARE BOLT.
AT FL 300, FWD EQPT VALVE EICAS MESSAGE DISPLAYED. CREW COMPLIED WITH ATI QRH CHECKLIST, AND LIGHT REMAINED ANNUNCIATED. AFTER SEVERAL MINUTES CREW NOTED A LOSS PRESSURIZATION AND EQUIPMENT COOLING CB POPPED OVRD DURING DESCENT. DIVERSION TO KILN WITH A DECLARED EMERGENCY. LANDING WAS UNEVENTFUL WITH NO ADDITIONAL PRECAUTIONARY ACTIONS. ON ARRIVAL AIRCRAFT GROUNDED FOR UNSCHEDULED MAINTENANCE. WORK IN PROGRESS
IN CRUISE VIA AIRLINK, CREW REPORTS POSSIBLE FUEL LEAK FROM LEFT MAIN TANK, UNABLE TO COMPENSATE, FUEL LEAK IS NOT INTERNAL, 2900LBS FUEL IN-BALANCE, UNABLE TO CONTROL WITH CROSSFEED. AS A PRECAUTIONARY MEASURE, AIR TURN BACK TO KPHX WITH AN EMERGENCY DECLARATION TO ATC. AIRCRAFT GROUNDED FOR UNSCHEDULED MAINTENANCE. DETAILED VISUAL INSPECTION OF SYSTEM IN ADDITION TO MULTIPLE FUEL TRANSFER CHECKS SATISFACTORY WITH NO LEAKS NOTED. ENGINE RUNS WITH FUEL FLOW AND FEED NORMAL. FAULT NOT DUPLICATED. NO DEFECTS NOTED. AIRCRAFT RELEASED TO SERVICE.
CREW REPORTED THE MAIN CARGO DOOR LIGHT AND WARNING HORN SOUND ANNUNICATED AS AIRCRAFT PASSED THROUGH 19,000 FT. CREW DECLARED AN EMERGENCY. QRA PROCEDURE. NO LOSS OF CABIN PRESSURIZATION. AIR TURN BACK. INSPECTION AFTER LANDING NOTED MAIN CARGO DOOR WAS CLOSED AND VERIFIED LOCKED AFTER LANDING. REMOVED AND REPLACED THE LOCK TORQUE TUBE. MAIN DECK CARGO DOOR ADJUSTMENT TEST AND PRESSURIZATION TEST SATISFACTORY. MAIN DECK CARGO DOOR WARNING LIGHT AND HORN DID NOT ANNUNCIATE. NO FURTHER DEFECTS NOTED. AIRCRAFT RELEASED TO SERVICE.
RRCA HYDRAULIC HOSE INSIDE VERTICAL STABILIZER STRINGER 3R DAMAGED IN TWO PLACES. REPAIRED VERTICAL STABILIZER STRINGER IAW SRM 65-30-03. ACFT GROUNDED.
ANGLE AT BS 1843 AFT SIDE OF FIRE WALL HAS SEVERAL CRACKS AT LBL 10 AND RBL 10. REMOVED AND REPLACED ANGLE IAW SRM 51-70-11. ACFT GROUNDED.
LEFT WING TRAILING EDGE UPPER AFT PANEL SUPPORT AT BS 400 CORRODED. REMOVED AND REPLACED THE SUPPORT IAW SRM 51-40-02. AIRCRAFT GROUNDED
AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. APU FIRE WALL FORWARD SIDE HAS SEVERAL CRACKS AT VERTICAL STIFFENERS, ACCESS 313AL. APU FIREWALL FORWARD SIDE WEB CRACKS REPAIRED IAW SRM 53-80-30, FIG 201, REPAIR 1, DWG 353T0400, IAW 47233REA01.
AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. NR 1 AFT STRUT TOP ANGLE JUST FORWARD OF MOUNTING FLANGE 437DB IS CRACKED. R & R TOP ANGLE JUST FORWARD OF MOUNT FLANGE 437 DB.
AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. AFT FUSELAGE EXTERNAL SKIN HAS A DENT AT STA 1794, S37R. REPAIRED AFT FUSELAGE EXTERNAL SKIN AT STATION 1794 IAW 47233, REA 04 & SRM 53-00-01.
CORROSION ON THE LEFT WING TRAILING EDGE SUPPORT STRUCTURE UPPER CHORD JUST FORWARD OF THE NR 6 SPOILER IN BOARD FORWARD CORNER. CORROSION ON THE LEFT WIN TRAILING EDGE SUPPORT STRUCTURE UPPER CHORD FOUND TO BE OUT OF LIMITS IN ACCORDANCE WITH SRM 57-51-02. NEW TOP CHORD WAS FABRICATED AND INSTALLED IN ACCORDANCE WITH AMEN DOCUMENT 47233FAB01.
ACFT GROUNDED FOR HEAVY MAINTENANCE. FUSELAGE STA 1046-1049, & 1055, RT BUTT LINE 95 ON TOP OF OVER WING LONGERON IS CORRODED. REMOVED ANGLE AND FASTENERS, BLENDED, CORROSION REA 47233, REA 02, COMPLETED IN AREA BLENDED. REINSTALLED ANGLE AND FASTENERS IAW SRM 51-40-02.
AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. NR 1 PYLON UNDER 431AT FORWARD CORNERS ON SKIN CHAFED. R & R FORWARD CORNER GUSSETS ON NR 1 PYLON UNDER 431AT IAW SRM 51-40-02, PARA 5 AND 7.
AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. NR 1 PYLON OTBD HYDRAULIC BAY LOWER BEAM IS CHAFED VERY THIN AT FORWARD END. R & R LOWER BEAM IN NR 1 OTBD HYDRAULIC BAY IAW SRM 51-40-02, SECTION 5, PARA B AND SECTION 7, PARA D.
CORROSION LT UPPER WING AT STATION 1075.2, TEMPORARY REPAIR OF LT WING SKIN AT STATION 1090 IAW 46971REA28. PERMANENT REPAIR TO BE ACCOMPLISHED AT NEXT C CHECK IAW 46971REA28 STEP 9 REFERENCE ATI COI 47257.
NUMBER 5 EMER DESCENT DEVICE EXTENDED & UNSERVICEABLE. R & R NR 5 EMER DESCENT DEVICE IAW AMM 25-61-03.
NUMBER 4 EMER DESCENT DEVICE EXTENDED & UNSERVICEABLE. R & R NR 4 EMER DESCENT DEVICE IAW AMM 25-61-03.
LEFT HORIZONTAL STAB CORROSION ON TOP SURFACE AT REAR SPAR 16, 108 INCHES FROM FUSELAGE, RS STATION 24 - 26.15 & 127.25 - 129.5 ABOVE REAR SPA. REPAIRED IAW REPAIR EO 47120REA08. INBOUND BLEND ACCOMPLISHED IAW EO 47120REA08.
UPPER TE PANEL ATTACH CHORD CORRODED AROUND NUTPLATE AS SEEN THRU PANEL 652CB OPENING. R & R TE CHORD IAW SRM 51-40-02.
REAR SPAR TO TE PANEL ATTACH BEAM AT WS 285 UPPER CHORD CORRODED AROUND NUTPLATES. UPPER PANEL ATTACH CHORD WAS FABRICATED REA 47120REA03 & REPLACED IAW SRM 51-40-02.
PANEL 652HB REAR SPAR TO TE RIB UPPER & LOWER CHORDS CORRODED AROUND NUTPLATES. R & R LOWER CHORD IAW SRM 51-40-02.
PANEL 661AB REAR SPAR TO TE ATTACH RIB UPPER CHORD CORRODED AROUND NUTPLATE WS 435. R & R TE UPPER RIB CHORD IAW SRM 51-40-02 & REA 47120REA04.
HINGED PANEL 651XB HAS CORROSION AROUND NUTPLATE. REMOVED CORROSION BEYOND LIMITS. NEW INTERCOSTAL FABRICATED. INSTALLED TO PANEL 651XB IAW SRM 51-40-02.
PANEL 652CB AFT ATTACH CHORD SPLIT ON EDGE. R & R AFT ATTACH CHORD AT PANEL 652GB IAW SRM 51-40-2.
TRAILING EDGE PANEL 652EB ATTACH FITTING CORRODED AROUND NUTPLATE. R & R TE PANEL 652EB ATTACH FITTING IAW SRM 51-40-02.
HINGED PANEL 651TB REAR SPAR TO TE OTBD ATTACH CHANNEL SPLIT ON EDGE. R & R ATTACH CHANNEL FOR HINGED PANEL 651TB REAR SPAR TO TE OTBD IAW SRM 51-40-02.
AFT UPPER WING PANEL ATTACH CHANNEL CORRODED AROUND NUTPLATES AS SEEN THRU PANEL 651TB. R & R WING PANEL ATTACH CHANNEL IAW SRM 51-40-02 & REA 47120REA02.
LOWER PANEL DIAGONAL ATTACH CHANNEL INBD OF H BLOCK AT WS 289 SPLIT ON EDGE. R & R IAW SRM 51-40-02.
NOSE WHEEL BULKHEAD FWD FACE WL 170, RBL 25 CHORD CRACKED. REMOVED DAMAGE SECTION OF CHORD & REPAIRED AREA IAW SRM 51-70-12.
NOSE WHEEL BULKHEAD FWD FACE WL 170, LBL 25 CHORD CRACKED. REMOVED DAMAGE SECTION OF CHORD & REPAIRED AREA IAW SRM 51-70-12.
PANEL 661AB REAR SPAR TO TE ATTACH RIB LOWER CHORD SPLIT ON EDGE WS 435. LOWER CHORD R & R IAW SRM 51-40-02.
NUMBER 2 DESCENT DEVICE CABLE IS EXTENDED, NEEDS REPLACED. IAW MM 25-61-03 R & R NR 2 EMERGENCY DESCENT DEVICE, NO DEFECTS NOTED.
AT SERVICE CHECK RT SIDE EMERGENCY EXIT LIGHT INOPERABLE. R & R EMERGENCY BATTERY PACK AT M736. OPERATIONAL CHECK SATISFACTORY IAW MM SUPP 33-51-00.
LEFT FWD CABIN ENTRY DOOR EMERGENCY EXIT LIGHT INOPERATIVE. EMERGENCY LIGHT POWER SUPPLY M735 AT FAULT, ACFT WAS GNDED.
DURING CLIMB RECEIVED EICAS MESSAGE RT BLEED DUCT LEAK AND APPROXIMATELY ONE MINUTE LATER RT AC BUSS POWER FAILURE. BUSS OFF LIGHT ILLUMINATED. RETURNED TO ORIGINATING STATION. INSPECTION FOUND RIGHT BLEED CROSSOVER DUCT RUPTURED. RIGHT HAND ISOLATION VALVE CONNECTOR DAMAGED. RIGHT HAND WING TO BODY ISOLATION DUCT DAMAGED. RIGHT HAND VAPOR BARRIER DAMAGED. REMOVED AND REPLACED DAMAGED BLEED CROSSOVER DUCT IAW AMM 36-11-01. LEAK CHECKED GOOD. REMOVED AND REPLACED ISOLATION VALVE CONNECTOR IAW SWPM 20-50-01. REMOVED AND REPLACED RIGHT HAND WING TO BODY ISOLATION DUCT IAW AMM 36-11-01. ACCOMPLISHED INTERIM REPAIR TO THE RIGHT HAND VAPOR BARRIER IAW EO 53-767-4960.
AFT LOWER CARGO DOOR LINER HOLES CORRODED BELOW AFT CONTROL ARM ATTACHMENT POINT ON DOOR. REPLACED INNER TEE CHORD IAW SRM 51-40-02.
AFT LOWER CARGO FLOOR FRAME IS CORRODED AT STATION 1197, RBL 20. R & R CORRODED SECTION OF FLOORBEAM INNER CHORD IAW SRM 51-40-02.
RT TEE FITTING IS CORRODED AT LOWER FASTENER HOLE COMMON TO FAILSAFE STRAP. R & R WITH NEW TEE FITTING IAW SRM 51-40-05.
LEFT WING T/E PANEL SUPPORT IS CORRODED AT WS 355. REPAIRED PANEL SUPPORT BEAM IAW SRM 51-70-12.
LEFT WING T/E PANEL SUPPORT IS CORRODED BETWEEN WS 330 AND 355. REPAIRED PANEL SUPPORT BEAM IAW SRM 51-70-12.
UPPER SKIN OF RT HORIZONTAL STAB IS CORRODED IN 3 PLACES FWD OF OTBD ELEVATOR. REPAIRED RT HORIZONTAL STAB AT STA 258-270, STA 288-300, STA 311-326 IAW SRM 55-10-01, FIG 201 REPAIR 7.
FUSELAGE TO VERTICLE WEB SUPPORT ANGLE HAS A 1.00" CRACK AT STATION 1746 ON THE LT AND RT ENDS OF THE ANGLE. COMMON TO PANELS 324AR AND 324AL. REPLACED FUSELAGE TO VERTICLE WEB SUPPORT ANGLE IAW SRM 51-40-02, 51-21-04, AND 51-21-10.
NR 1 PYLON INBD CHANNEL ABOVE ARROWHEAD PANEL HAS A 2.00" CRACK. REPLACED INBD CHANNEL ON NR 1 PYLON IAW SRM 57-40-02.
FLOORBEAM WEB IS DENTED WITH A 1.1250" CRACK AT RBL 30 STA 303. REMOVED DAMAGED SECTION OF FLOORBEAM AND REPAIRED IAW SRM 51-70-11, FIG 1.
RIGHT PRESSURE DECK WEB IS CORRODED AND HAS PREVIOUS DRILL STARTS. FABRICATED REPAIR WEB IAW DWG 145T8752 AND INSTALLED WEB IAW ENGINEERING DOCUMENT 47008ORD04.
RIGHT FAILSAFE STRAP HAS A 0.450" CRACKED AT THE LOWER HOLE IN INSPECTION AREA. THE CRACK WAS REMOVED DURING THE FAILSAFE TRIM OUT PROCEDURE THAT WAS PERFORMED IAW AMES ENGINEERING DOCUMENT 47008ORD04. REF SB 767-53A0100, REV 3, DATED FEB 06, 2012 AND SB 767-53-0116, DATED JULY 18, 2012 AS MANDATED BY AD 2012-09-04.
AFTER THE FAIL SAFE TRIM OUT PROCEDURE, THE INTERNAL SURFACE OF THE RT SIDE FUSELAGE SKIN WAS FOUND TO BE CORRODED AT FAILSAFE TRIM OUT AREA. THE CORROSION WAS REMOVED, AREAS SPOT FACED AND FILLERS INSTALLED IAW ENGINEERING DOCUMENT 47008ORD10. REF SB767-53A0100, REV 3 AND SB767-53-0116 AS MANDATED BY AD 2012-09-04.
LEFT T-FITTING IS CORRODED AT LOWER FASTENER HOLE COMMON TO FAILSAFE STRAP. INSTALLED NEW T-FITTING IAW SRM 51-40-05.
AFT LOWER CARGO FLOORBEAM IS CORRODED AT BS 1153, LBL 6 TO LBL 44. R & R CORRODED SECTION OF FLOORBEAM INNER CHORD IAW SRM 51-40-02.
RT WING INBD MAIN FLAP T/E UPPER SURFACE CORRODED. REPLACED INBD MAIN FLAP IAW AMM 27-51-03.
RT WING INBD MAIN FLAP UPPER SKIN CORRODED AT WS 205. REPLACED INBD MAIN FLAP IAW AMM 27-51-03.
FAULT CODE 34-45-XA-01/02, NAV DISPLAY "TCAS FAIL" WAS DISPLAYED ON BOTH CAPTAIN'S AND F/O DISPLAY. ACFT RETURNED TO STATION. R & R TCAS SYS COMPUTER IAW AMM 34-45-01. OPS CHECK GOOD ON GROUND.
FAULT CODE 71-05-XG-01, LT ENGINE WOULD NOT SPOOL TO N1 COMMAND AT 70 PERCENT, AFTER ENGAGING N1, LARGE THROTTLE SPLIT. REJECTED TAKEOFF AT LOW SPEED, LESS THAN 40 KNOTS. NO BRAKING REQUIRED. COMPLIED WITH BORESCOPE INSPECTION IAW AMM 72-00-00/601 AND JOB CARD 767-70.06-1. ENGINE FOUND TO BE IN SERVICEABLE CONDITION. R & R MEC IAW AMM 73-21-01. PERFORMED ENGINE RUN IAW ERH AND COMPLIED WITH TESTS NR5, NR6 AND NR12 IAW AMM 71-00-00, POWER ASSURANCE. NR 1 ENGINE OPS AND LEAK CHECKED GOOD.
DURING CRUISE THE LT ENGINE OIL TEMP STEADILY CLIMB OUT OF LIMITS, OIL TEMP 190, AND OIL PRESSURE 58. THE CREW SHUTDOWN THE LT ENGINE AND RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX TROUBLESHOT THE OIL TEMP WIRING CIRCUIT AND FOUND PROTECTIVE COATING ON GROUND WIRE DAMAGED AT GROUND STUD. CLEANED GROUND STUD AND REPAIRED GROUND WIRE IAW MM STANDARD WIRING PRACTICES CH 20-10-13. RAN ENGINES AT TAKEOFF POWER IAW MM 71-00-00. OPS CHECKED GOOD.
LT ENGINE SHUTDOWN IN-FLIGHT DUE TO HIGH OIL TEMP - ENGINE OIL TEMP INDICATED 175 DEGREES CELSIUS, OIL PRESSURE WAS 58 PSI. MX R & R NR 1 ENGINE OIL TEMP BULB IAW MM 79-34-00, BLOCK 1 AND 79-34-99, FIG 101, PG 101 & 102, STEPS 1 THRU 10. VERIFED, ACFT RELEASED TO ETOPS 180.
DURING ROUTINE C-CHECK INSPECTION, FOUND STRINGER 1 LT CRACKED AT STA 676 - 698. REMOVED CRACKED STRINGER. INSTALLED NEW STRINGER SEGMENT IAW SRM 53-00-03, FIGURE 201.
AFTER TAKEOFF, THE CREW PERFORMED A PACKS OFF TAKEOFF, THE AIR CONDITIONING PACKS WOULD NOT TURN ON AND THE ACFT WOULD NOT PRESSURIZE. THE CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX ACCOMPLISHED FIM PROCEDURES 21-31-00, FIG 104 AND BIT STEPS 1, 2, 22, 23A, 24, 25, 26 AND 46. TEST CHECKED GOOD IAW FIM 21-31-00 FIGURE 103. ACFT WAS RETURNED TO SERVICE.
DURING TOW INTO HANGER ACFT STRUCK WORK STAND AND DENTED L/E OF RT SIDE HORIZ STABILIZER. REPAIRED IAW SRM 51-70-10, FIG 209, REV ATI 03 AND MM 55-15-01.
DURING TOW INTO HANGER ACFT STRUCK WORK STAND AND DENTED L/E OF LT SIDE HORIZ STABILIZER. REPAIRED IAW SRM 51-70-10, FIG 209, REV ATI 03 AND MM 55-15-01.
DURING VISUAL INSP FOUND CORROSION IN AFT WASTE SERVICE PAN AREA AT STA 1582 STRINGER 39 LT AND 39 RT. REPAIR WAS ACCOMPLISHED IAW SRM 51-30-01, DWG 146T3248, SRM 51-40-02, SRM 53-00-03, MM 38-32-03-01 AND MM 05-51-24/201.
AFTER UNLOADING ACFT, FOUND PANEL BELOW LOCK/GUIDE TORN AND THE PANEL SUPPORT INTERCOSTAL BROKEN. REPLACED DAMAGED INTERCOSTAL AND WEB SECTION IAW SRM 767-200 51-10-02, 51-30-01, 51-70-13 AND 51-40-02 REV 2. AIRCRAFT WAS RETURNED TO SERVICE.
DURING TAKEOFF FROM ELECTRONICS BAY ACCESS DOOR WARNING ILLUMINATED. THE CREW ABORTED TAKEOFF AND RETURNED TO BLOCKS. MX CLEANED AND ADJUSTED PROXIMITY SWITCH. OPS CHECK GOOD IAW BAMM 52-71-00/501. ACFT WAS RETURNED TO SERVICE.
DURING ROUTINE C CHECK INSP FOUND SCRATCHES AT AFT CARGO DOOR AREA UPPER FWD CORNER AND UPPER AFT CORNER ON RT AFT FUSELAGE. BLENDED OUT SCRATCHES. FOUND TO BE WITHIN LIMITS. PERFORMED NDT INSP, NO CRACKS OR CORROSION NOTED. CLEANED, TREATED, PRIMED AND PAINTED IAW SRM 51-10-01, 51-20-01 REV101, 52-30-01 FIGURE 101 REV 101, NDT D634T301 REV93 PART6 SUB 51-11-19 AND MM 11-00-00 REV97.
DURING ROUTINE C CHECK INSP FOUND NR 1 ENGINE OTBD PYLON DENTED JUST AFT OF HYD ACCESS DOOR. BLENDED OUT DENTS. FOUND TO BE WITHIN LIMITS. PERFORMED NDT INSP, NO CRACKS OR CORROSION NOTED. CLEANED, TREATED, PRIMED AND PAINTED IAW SRM 51-10-01, 51-20-01 REV101, 54-51-10 FIGURE 101 REV101, AND NDT D634T301 REV93 PART6 SUB 51-11-19.
DURING ROUTINE C CHECK INSP FOUND LT LWR KEELBEAM INBD FLANGE CORRODED AT STA 844. REMOVED CORROSION. FOUND TO BE WITHIN LIMITS. CLEANED, TREATED, PRIMED AND PAINTED IAW SRM 767 51-10-01 REV101, 53-50-12-FIGURE 101 REV 101, AND SOPM 20-10-03 REV36.
DURING ROUTINE C CHECK INSP, FOUND A DENT 15 FWD OF AFT ACCESSORY DOOR AT STA 1788. BLENDED OUT DENT. FOUND TO BE WITHIN LIMITS. PERFORMED NDT INSP, NO CRACKS OR CORROSION NOTED. CLEANED, TREATED, PRIMED AND PAINTED IAW SRM 51-10-01, 51-20-01 REV101, 5300-01 FIGURE 101 REV101, NDT D634T301 REV 93 PART 6 SUB 51-00-19 AND MM 11-00-00-REV 97.
DURING ROUTINE C-CHECK INSP FOUND SCRATCHES ON FUSELAGE FWD AND BELOW FWD CARGO DOOR CONTROL. BLENDED OUT SCRATCHES. FOUND TO BE WITHIN LIMITS. PERFORMED NDT INSPECTION, NO CRACKS OR CORROSION NOTED. CLEANED, TREATED, PRIMED AND PAINTED IAW SRM 51-10-01, 51-20-01, 53-00-01 FIGURE 101 REV101, NDT D634T301 REV 93 PART 6 SUB 51-00-19 AND MM 11-00-00 REV97.
DURING ROUTINE C CHECK INSP FOUND BULK CARGO DOOR FWD SILL DENTED. REMOVED DAMAGED AREA. FOUND TO BE WITHIN LIMITS. PERFORMED NDT INSPECTION, NO CRACKS OR CORROSION NOTED. CLEANED, TREATED, PRIMED AND PAINTED IAW SRM 51-10-01, 51-20-01 REV101, 53-00-01 FIGURE 101 REV101, NDT D634T301 REV93 PART6 SUB 51-11-19 AND MM 11-00-00 REV 97.
DURING ROUTINE C-CHECK INSP, FOUND SCRATCHES ON AFT OF BULK CARGO DOOR AT STA 1461 BETWEEN STR 33 LT AND 39 LT. BLENDED SCRATCHES OUT. FOUND TO BE WITHIN LIMITS. PERFORMED NDT INSP, NO CRACKS OR CORROSION NOTED. CLEANED, TREATED, PRIMED AND PAINTED IAW SRM 51-10-01, 51-20-01 REV101, 53-00-01 FIGURE 101 REV101, NDT D634T301 REV 93 PART6 SUB 51-11-19 AND MM 11-00-00 REV97.
DURING ROUTINE C-CHECK INSP FOUND DENT AFT EDGE OF BULK CARGO DOOR OPENING. BLENDED OUT DENT. FOUND TO BE WITHIN LIMITS. PERFORMED NDT INSP, NO CRACKS OR CORROSION NOTED. CLEANED, TREATED, PRIMED AND PAINTED IAW SRM 51-10-01, 51-20-01 REV101, 53-00-01 FIGURE 101 REV101, NDT D634T301 REV93 PART6 SUB 51-11-19 AND MM 11-00-00 REV 97.
DURING ROUTINE C CHECK INSP FOUND KEEL BEAM LT INBD FLANGE CORRODED BETWEEN STA 815-839. REMOVED CORROSION. FOUND TO BE WITHIN LIMITS. CLEANED, TREATED PRIMED IAW SRM 51-10-02 REV 101 , 53-50-12 FIGURE 101, REV 101, AND 20-10-13 REV36.
DURING ROUTINE C CHECK INSP FOUND GOUGES AT AFT END OF CARGO DOOR AT 28R. BLENDED OUT GOUGES. FOUND TO BE WITHIN LIMITS. PERFORMED NDT, NO CRACKS OR CORROSION NOTED. CLEANED, TREATED, PRIMED AND PAINTED IAW SRM 51-10-01, 51-20-01, 53-00-01 FIGURE 101 REV 101, NDT D634T301 REV93 PART6 SUB 51-00-19 AND MM 11-00-00 REV 97.
DURING ROUTINE C CHECK INSP FOUND LWR KEELBEAM CORRODED AT STA 1010. REMOVED CORROSION. FOUND TO BE WITHIN LIMITS. CLEANED, TREATED, PRIMED AND PAINTED IAW SRM 51-10-02 REV 101, 53-50-12 FIGURE 101 REV101, AND SOPM 20-10-03 REV 36.
DURING ROUTINE C-CHECK INSP, FOUND SCRATCHES BELOW FORWARD CARGO DOOR CONTROL PANEL. BLENDED OUT SCRATCHES. FOUND TO BE WITHIN LIMITS. PERFORMED NDT INSP, NO CRACKS OR CORROSION NOTED. CLEANED, TREATED, PRIMED AND PAINTED IAW SRM 55-00-01 FIGURE 101 REV 101, 51-20-01 REV 101, NDT D634T301 REV93 PART 6 SUB 51-00-19, AND MM 11-00-00, REV97.
DURING ROUTINE C CHECK INSP FOUND CORROSION ON LOWER KEELBEAM RT INBD FLANGE AT STA 808. REMOVED CORROSION. FOUND WITHIN LIMITS. CLEANED, TREATED, PRIMED AND PAINTED IAW SRM 53-50-12 FIGURE 101 REV 101, 20-10-03 REV 036, AND 51-20-01 REV 101.
DURING ROUTINE C CHECK INSP, FOUND DENTS IN SKIN AT STA 1372 30R. BLENDED OUT DENTS. FOUND TO BE WITHIN LIMITS. PERFORMED NDT INSP, NO CRACKS OR CORROSION NOTED. CLEANED, TREATED, PRIMED AND PAINTED IAW SRM 51-10-01, 51-20-01 REV 101, 53-00-01 FIGURE 101 REV 101, NDT D634T301 REV 93 PART6 SUB 51-11-19 AND MM 11-00-00 REV 97.
DURING ROUTINE C CHECK INSP, FOUND SCRATCHES ON L/E OF LT STABILIZER. BLENDED OUT SCRATCHES. FOUND TO BE WITHIN LIMITS. PERFORMED NDT INSP, NO CRACKS OR CORROSION NOTED. CLEANED, TREATED, PRIMED AND PAINTED IAW SRM 51-10-01, 51-20-01 REV 101, 55-10-01 FIGURE 101 REV 101, NDT D634T301 REV 93 PART 6 SUB 51-00-19 AND MM 11-00-00 REV 97.
DURING ROUTINE C CHECK INSP FOUND GOUGES AT LWR FWD CORNER IN FRONT OF AFT CARGO DOOR. BLENDED OUT GOUGES. FOUND TO BE WITHIN LIMITS. PERFORMED NDT, NO CRACKS OR CORROSION NOTED. CLEANED, TREATED, PRIMED AND PAINTED IAW SRM 51-10-01, 51-20-01, 53-00-01 FIGURE 101 REV 101, NDT D634T301 REV93 PART6 SUB 51-00-19 AND MM 11-00-00 REV 97.
DURING ROUTINE C CHECK INSP FOUND LWR KEELBEAM LT INBD FLANGE CORRODED AT STA 889. REMOVED CORROSION. FOUND TO BE WITHIN LIMITS. CLEANED, TREATED, PRIMED AND PAINTED IAW SRM 51-10-02 REV 101, 53-50-12 FIGURE 101 REV101, AND SOPM 20-10-03 REV36.
DURING ROUTINE C CHECK INSP FOUND LWR KEELBEAM LT INBD FLANGE CORRODED AT STA 856. REMOVED CORROSION. FOUND TO BE WITHIN LIMITS. CLEANED, TREATED, PRIMED AND PAINTED IAW SRM 51-10-02 REV 101, 53-50-12 FIGURE 101 REV101, AND SOPM 20-10-03 REV36.
DURING ROUTINE C CHECK INSP FOUND DENTS IN RT VERTICAL STABILIZER BETWEEN STA FSS 245 AND FSS 92. BLENDED OUT DENTS. FOUND TO BE WITHIN LIMITS. PERFORMED NDT INSP, NO CRACKS OR CORROSION NOTED. CLEANED, TREATED, PRIMED AND PAINTED IAW SRM 51-10-01, 51-20-01 REV101, 55-30-00 FIGURE 101 REV 101, NDT D634T301 REV 93 PART 6 SUB 51-00-19, AND MM 11-00-00 REV 97.
DURING ROUTINE C-CHECK INSP FOUND LWR KEELBEAM CORRODED AT STA 990. REMOVED CORROSION. FOUND TO BE WITHIN LIMITS. CLEANED, TREATED, PRIMED AND PAINTED IAW SRM 51-10-02 REV 101, 53-50-12 FIGURE 101 REV101, AND SOPM 20-10-03 REV36.
DURING ROUTINE C CHECK INSP FOUND LWR KEELBEAM LT INBD FLANGE CORRODED AT STA 914. REMOVED CORROSION. FOUND TO BE WITHIN LIMITS. CLEANED, TREATED, PRIMED AND PAINTED IAW SRM 51-10-02 REV 101, 53-50-12 FIGURE 101 REV 101, AND SOPM 20-10-03 REV 36.
DURING ROUTINE C CHECK INSP FOUND GOUGE ON LWR FUSELAGE LT OF CTR LINE AT STATION 1619. BLENDED OUT GOUGE. FOUND TO BE WITHIN LIMITS. PERFORMED NDT INSP, NO CRACKS OR CORROSION NOTED. CLEANED, TREATED, PRIMED AND PAINTED IAW SRM 51-10-01, 51-20-01, 53-00-01 FIGURE 101 REV 101, NDT 634T301 REV 93 PART 6 SUB 51-00-19 AND MM 11-00-00 REV 97.
DURING ROUTINE C-CHECK INSP, FOUND DENTS ON L/E RT SIDE OF VERTICAL STABILIZER. BLENDED OUT DENTS. FOUND TO BE WITHIN LIMITS. PERFORMED NDT INSP, NO CRACKS OR CORROSION NOTED. CLEANED, TREATED, PRIMED AND PAINTED IAW SRM 51-10-01, 51-20-01, 55-30-01 FIGURE 101 REV 101, NDT 634T301 REV93 PART6 SUB 51-00-19 AND MM 11-00-00 REV 97.
DURING ROUTINE C CHECK INSP FOUND SCRATCHES ON LT FUSELAGE AFT BODY FAIRING BY T/E. BLENDED OUT SCRATCHES. PERFORMED NDT INSP, NO CRACKS OR CORROSION NOTED. CLEANED, TREATED, PRIMED AND PAINTED IAW SRM 51-10-01, 51-20-01, 53-00-01 FIGURE101 REV 101, NDT D634T301 REV 93 PART6 SUD 51-00-19 AND MM 11-00-00, REV 97.
DURING ROUTINE C CHECK INSP, FOUND L/E SURFACE LT HORIZONTAL STABILIZER GOUGED 1â FROM ROOT. BLENDED OUT GOUGE. PERFORMED NDT INSP, NO CRACK OR CORROSION NOTED. CLEANED, TREATED AND PRIMED IAW SRM 51-10-01, 51-20-01, 55-10-01 FIGURE 101 REV101 AND NDT 634T301 REV93 PART6 SUB 51-00-19.
DURING ROUTINE C CHECK INSP FOUND GOUGES IN SKIN AT AFT CARGO DOOR AT 27R E58 3417771. BLENDED OUT GOUGES. FOUND TO BE WITHIN LIMITS. PERFORMED NDT INSP, NO CRACKS OR CORROSION NOTED. CLEANED, TREATED, PRIMED AND PAINTED IAW SRM 51-10-01, 51-20-01 REV101, 52-30-01 FIGURE 101 REV 101, NDT D634T301 REV93 PART6 SUB 51-11-19 AND MM 11-00-00 REV 97.
DURING ROUTINE C CHECK INSP, FOUND DENTS IN TAIL CONE ACCESS DOOR RT SIDE. REMOVED DENTS. FOUND TO BE WITHIN LIMITS. PERFORMED NDT INSP. NO CRACK OR CORROSION NOTED. CLEANED, TREATED, PRIMED AND PAINTED IAW SRM 51-10-01, 51-20-01 REV101, 52-40-01 FIGURE 101 REV 101, D634T301 REV 93 PART 6 SUB 51-00-01, AND MM 11-00-00 REV97.
DURING ROUTINE C-CHECK INSP FOUND CORROSION ON LOWER KEELBEAM RT AT STA 975.5. REMOVED CORROSION. FOUND WITHIN LIMITS. CLEANED, TREATED, PRIMED AND PAINTED IAW SRM 53-50-12 FIGURE 101, REV 101, 20-10-03 REV 036, AND 51-20-01 REV 101.
DURING ROUTINE C CHECK INSP FOUND CORROSION ON LOWER KEELBEAM RT AT STA 1003. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED KEELBEAM. PERFORMED NDT INSP. NO CRACK OR CORROSION. FABRICATED NEW KEELBEAM. ACCOMPLISHED HEAT TREATMENT TO REPAIR PART. CLEANED, TREATED, PRIMED AREA AND REPAIR PART. INSTALLED REPAIR PART IAW SRM 53-50-12, FIG 101, REV 101, 53-50-12, FIGURE 201 REV 101, NDT P634T301 REV 93 PART 6 51-00-19, 20-42-05, 51-20-01-REV 101, AND 20-10-03 REV 036.
DURING ROUTINE C-CHECK INSP FOUND DENTS IN UPPER AREA OF BULK CARGO DOOR. REMOVED DENTS. FOUND TO BE WITHIN LIMITS. PERFORMED NDT INSP. NO CRACK OR CORROSION NOTED. CLEANED, TREATED, PRIMED AND PAINTED IAW SRM 51-10-01, 51-20-01 REV101, 53-00-01 FIGURE 101 REV101, NDT D634T301 REV 93 PART 6 SUB 51-00-19, AND MM 11-00-00, REV 97.
DURING ROUTINE C-CHECK INSP FOUND CORROSION ON LOWER KEELBEAM LT INBD FLANGE BETWEEN STA 801-803. REMOVED CORROSION. FOUND WITHIN LIMITS. CLEANED, TREATED, PRIMED AND PAINTED IAW SRM 53-50-12 FIGURE 101 REV 101, 20-10-03 REV 036, AND 51-20-01 REV 101.
DURING ROUTINE C-CHECK INSP FOUND CORROSION ON LOWER KEELBEAM RT INBD FLANGE BETWEEN STA 905-925. REMOVED CORROSION. FOUND WITHIN LIMITS. CLEANED, TREATED, PRIMED AND PAINTED IAW SRM 53-50-12, FIGURE 101, REV 101, 20-10-03 REV 036, AND 51-20-01 REV 101.
DURING ROUTINE C CHECK INSP FOUND CORROSION ON LOWER KEELBEAM RT INBD FLANGE BETWEEN STA 876-901. REMOVED CORROSION. FOUND WITHIN LIMITS. CLEANED, TREATED, PRIMED AND PAINTED IAW SRM 53-50-12 FIGURE 101 REV 101, 20-10-03 REV 036, AND 51-20-01 REV 101.
DURING ROUTINE C CHECK INSP FOUND CORROSION ON LOWER KEELBEAM RT INBD FLANGE BETWEEN STA 843-854. REMOVED CORROSION. FOUND WITHIN LIMITS. CLEANED, TREATED, PRIMED AND PAINTED IAW SRM 53-50-12 FIGURE 101 REV 101, 20-10-03 REV 036, AND 51-20-01 REV 101.
DURING ROUTINE C CHECK INSP FOUND CORROSION ON LOWER KEELBEAM RT INBD FLANGE BETWEEN STA 825-839. REMOVED CORROSION. FOUND WITHIN LIMITS. CLEANED, TREATED, PRIMED AND PAINTED IAW IAW SRM 53-50-12, FIGURE 101, REV 101, 20-10-03 REV 036, AND 51-20-01 REV 101.
DURING ROUTINE C-CHECK INSP, FOUND DENTS IN VERTICAL STABILIZER AT STA FSS118. REMOVED DENTS. FOUND TO BE WITHIN LIMITS. PERFORMED NDT INSP. NO CRACK OR CORROSION NOTED. CLEANED, TREATED, PRIMED AND PAINTED IAW SRM 51-10-01REV 101, SRM 51-20-01 REV 101, 55-30-01 FIGURE 101 REV 101, NDT D634T301 REV 93 PART 6 51-00-19, AND MM 11-00-00-REV 97.
DURING ROUTINE C CHECK INSP FOUND FWD CARGO COMPARTMENT FLOORBOARD PUNCTURED AT STA 455 BOTTOM LINE 0. APPLIED GLASS CLOTH AND RESIN TO FILL PUNCTURE FLOOR. CLEANED, TREATED, PAINTED AREA IAW SRM 53-00-50 REV 101 AND 51-21-10 REV 97.
DURING ROUTINE C-CHECK INSP FOUND LT FUSELAGE BODY FAIRING PANEL NR 193PL EDGE DAMAGED. APPLIED GLASS CLOTH AND RESIN. CLEANED, TREATED, PRIMED AND PAINTED IAW SRM 51-70-06 REV 101 AND MM 51-21-10 REV 97.
DURING ROUTINE C CHECK INSP, FOUND CORROSION ON LWR KEELBEAM BETWEEN STATION 786 - 815 LT STRINGER 38. REMOVED CORROSION. FOUND TO BE WITHIN LIMITâS. CLEAN, TREATED, PRIMED AND PAINTED IAW SRM 53-50-12 FIGURE 101 REV 101, 20-10-03 REV 36, AND 51-20-01 REV 101.
DURING ROUTINE C CHECK INSP FOUND CORROSION ON LOWER KEELBEAM RIGHT BETWEEN STA 925-936, STR 38. REMOVED CORROSION. FOUND TO BE WITHIN LIMITâS. CLEAN, TREATED, PRIMED AND PAINTED IAW SRM 53-50-12 FIGURE 101, REV 101, 20-10-03 REV 36, AND 51-20-01 REV101.
DURING ROUTINE C-CHECK INSP, FOUND LT OTBD ELEVATOR UPPER SKIN AFT INBD SIDE HAS DELAMINATED. REMOVED DELAMINATED PART. APPLIED GRAPHITE FABRIC AND RESIN TO PART. CLEANED, TREATED, PRIMED AND PAINTED. ACCOMPLISHED WEIGHT AND BALANCE PROCEDURES IAW SRM 51-70-03 REV 101, 51-21-10 REV 97 AND 51-60-02 REV101.
DURING ROUTINE C-CHECK INSP, FOUND CORROSION ON LOWER KEEL BEAM LT BETWEEN STA 982-993, STR 38. REMOVED CORROSION. FOUND TO BE WITHIN LIMITâS. CLEAN, TREATED, PRIMED AND PAINTED IAW SRM 53-50-12 FIGURE 101 REV 101, 20-10-03 REV 36, AND 51-20-01 REV101.
DURING ROUTINE C-CHECK INSP, FOUND CORROSION ON LOWER KEEL BEAM LT BETWEEN STATION 839-854 STR 38. REMOVED CORROSION. FOUND TO BE WITHIN LIMITâS. CLEAN, TREATED, PRIMED AND PAINTED IAW SRM 53-50-12 FIGURE 101 REV 101, 20-10-03 REV 36, AND 51-20-01 REV101.
DURING ROUTINE C-CHECK INSP FOUND NICKS ON LT HORIZONTAL STABILIZER REMOVABLE L/E NR 332DL. BLENDED OUT NICKS. PERFORMED NDT INSP. NO CRACKS INDICATED. CLEANED, TREATED, PRIMED PART IAW SRM 55-10-01 FIGURE 101 REV 101 AND NDT D634T301, REV 93, PART 6 51-00-19.
DURING ROUTINE C CHECK INSPECTION FOUND NICKS ON LEFT HAND HORIZONTAL STABILIZER REMOVABLE LEADING EDGE NUMBER 332CL. BLENDED OUT NICKS. PERFORMED NDT INSPECTION. NO CRACKS INDICATED. CLEANED, TREATED, PRIMED PART IAW SRM 55-10-01 FIGURE 101, REV 101 AND NDT D634T301, REV 93, PART 6 51-00-19.
DURING ROUTINE C-CHECK INSP FOUND NICKS ON LT HORIZONTAL STABILIZER REMOVABLE L/E NR 332BL. BLENDED OUT NICKS. PERFORMED NDT INSP. NO CRACKS INDICATED. CLEANED, TREATED, PRIMED PART IAW SRM 55-10-01 FIGURE 101, REV 101 AND NDT D634T301 REV 93, PART 6 51-00-19.
DURING ROUTINE C-CHECK INSP, FOUND LT HORIZ STAB REMOVABLE L/E NR 332BL CRACKED. REMOVED CRACKED L/E PANEL. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO CRACK NOTED. FABRICATED REPAIR DOUBLER. CLEANED, TREATED, PRIMED AREA AND REPAIR PART. INSTALLED REPAIR PART IAW AMM 20-11-00 REV 97, SRM 51-70-10 FIGURE 204 REPAIR 4 REV 101, ATI 767 NDT D634T301 REV 93 PART 6 51-00-19, MFG DWG 184T1006, AND SRM 51-20-01 REV101.
DURING ROUTINE C CHECK INSP FOUND LT HORIZ STABILIZER EXTERIOR UPPER SURFACE AFT STRIP PANEL NR 335UT ERODED. APPLIED RESIN FOR PROTECTION. CLEANED, TREATED, PRIMED AND PAINTED IAW SRM 51-70-06 REV 101 AND MM 51-21-10 REV 97.
DURING ROUTINE C-CHECK INSP FOUND IMPROPER REPAIR ON RT OTBD ELEVATOR UPPER SURFACE. REMOVED DAMAGED AREA. APPLIED RESIN. CLEANED, TREATED, PRIMED AND PAINTED IAW SRM 51-70-06 REV 101 AND 51-21-10 REV 97.
DURING ROUTINE C CHECK INSP FOUND DELAMINATING ON VERTICAL STABILIZER RT SIDE SKIN. ACCOMPLISHED REPAIR IAW SRM 51-70-03 REV 101, SRM 51-21-10 REV 97.
DURING ROUTINE C-CHECK INSP, FOUND VERTICAL STABILIZER L/E PANEL NR 321E ERODED. ACCOMPLISHED REPAIR IAW SRM 51-70-06 REV101 AND 51-20-10 REV 97.
DURING ROUTINE C-CHECK INSP FOUND NR 2 PYLON V-FAIRING 447DB FWD EDGE OTBD ATTACH SUPPORT CHANNEL CRACKED. REMOVED FASTENERâS AS NEEDED TO PERFORM REPAIR. REMOVED CRACKED CHANNEL. INSTALLED NEW FASTENERâS AND CHANNEL IAW SRM 51-40-02 REV101 AND SRM 54-40-05 REV 101.
DURING ROUTINE C-CHECK INSP FOUND NR 2 PYLON V-FAIRING 447DB FWD EDGE INBD ATTACH SUPPORT CHANNEL CRACKED. REMOVED FASTENERâS AS NEEDED TO PERFORM REPAIR. REMOVED CRACKED CHANNEL. INSTALLED NEW FASTENERâS AND CHANNEL IAW SRM 51-40-02 REV101 AND SRM 54-40-05 REV 101.
DURING ROUTINE C-CHECK INSP FOUND CORROSION ON NR 2 PYLON PANEL 447CR. REMOVED CORROSION. FOUND TO BE WITHIN LIMITâS. CLEANED, TREATED, PRIMED AND PAINTED AREA IAW SRM 51-10-02 REV 101, SRM 54-51-70 FIGURE 101 REV 101, AND SRM 51-20-01 REV 101.
DURING ROUTINE C-CHECK INSP FOUND CORROSION ON RT WING LOWER SURFACE L/E PANEL 621AFB SUPPORT FRAME AT STATION LES1070. REMOVED FASTENERâS AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOUND TO BE WITHIN LIMITâS. CLEANED, TREATED, PRIMED AND PAINTED AREA. REINSTALLED FASTENERâS IAW SRM 51-40-02 REV 101, SRM 51-20-01 REV 101, AND SRM 57-41-09 FIGURE 101, REV 101.
DURING ROUTINE C-CHECK INSP FOUND SCRATCH MARKS ON FUSELAGE SKIN BETWEEN STATIONS 1241, 1263 AND STRINGER 25-26. REMOVED SCRATCH MARKâS. FOUND TO BE WITHIN LIMITâS. PERFORMED NDT INSP. NO CRACKâS OR CORROSION. CLEANED, TREATED, PRIMED AND PAINTED AREA IAW SRM 51-10-02 REV 101, SRM 53-00-01 FIGURE 101 REV 101, SRM 51-20-01 REV 101, AND NDTM D634T301 REV93 PART 6 SUB 51-00-19.
DURING ROUTINE C-CHECK INSP FOUND NR 2 PYLON V-FAIRING 447DB FWD AREA DELAMINATED. ACCOMPLISHED REPAIR IAW SRM 51-70-17, REV 101 AND SRM 51-21-10, REV 101.
DURING ROUTINE C-CHECK INSP, FOUND FLOOR PANEL PUNCTURED IN AFT CARGO COMPARTMENT AT STA 1227, RT BOTTOM LINE 12. ACCOMPLISHED REPAIR IAW SRM 53-00-50 REV 101 AND MM 51-21-10 REV 97.
DURING ROUTINE C-CHECK INSP FOUND FLOOR PANEL PUNCTURED IN AFT CARGO COMPARTMENT AT STA 1272 LT BOTTOM LINE 12. ACCOMPLISHED REPAIR IAW SRM 53-00-50 REV 101 AND MM 51-21-10 REV 97.
DURING ROUTINE C-CHECK INSP FOUND CORROSION ON RT WING LOWER SURFACE L/E PANEL 621AFB SUPPORT FRAME AT STATION LES1076. REMOVED FASTENERâS AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOUND TO BE WITHIN LIMITâS. CLEANED, TREATED, PRIMED AND PAINTED AREA. REINSTALLED FASTENERâS IAW SRM 51-40-02 REV 101, SRM 51-20-01 REV 101, AND SRM 57-41-09 FIGURE 101, REV 101.
DURING ROUTINE C-CHECK INSP FOUND CORROSION ON LOWER DRAIN VALVE SURROUNDING STRUCTURE AT STATION 1542. REMOVED CORROSION. FOUND TO BE WITHIN LIMITS. CLEANED, TREATED, PRIMED AND PAINTED AREA IAW SRM 53-00-01 FIGURE 101 REV 101, AND SRM 51-20-01 REV 101.
DURING ROUTINE C-CHECK INSP FOUND NR 2 PYLON V-FAIRING 447DB FWD EDGE INBD ATTACH SUPPORT FRAME CRACKED. REMOVED FASTENERâS AS NEEDED TO PERFORM REPAIR. REMOVED CRACKED FRAME. INSTALLED EXISTING FASTENERâS AND NEW FRAME IAW AMM 20-11-00 REV97, SRM 51-40-02 REV 101, AND SRM 51-40-05 REV 101.
DURING ROUTINE C-CHECK INSP FOUND RT WING INBD FLAP OTBD AFT FLAP SUPPORT FAIRING DELAMINATED. ACCOMPLISHED REPAIR IAW SRM 51-70-17 REV 101 AND MM 51-20-10 REV 97.
DURING ROUTINE C-CHECK INSP FOUND RT WING T/E PANEL NR 651WB CRACKED. ACCOMPLISHED REPAIR IAW MM 20-11-00 REV 79, AND SRM 51-70-06 REV 101, 51-21-10 REV 97, 51-40-05 REV 101.
DURING ROUTINE C-CHECK INSP FOUND LT WING INBD T/E FLAP OTBD FLAP SUPPORT FAIRING FWD FAIRING ERODED. ACCOMPLISHED REPAIR IAW SRM 51-70-06 REV 101 AND MM 51-20-10 REV 97.
DURING ROUTINE C-CHECK INSP, FOUND LT WING OTBD T/E FLAP SUPPORT FAIRING FWD FAIRING EXTERIOR SURFACE ERODED. ACCOMPLISHED REPAIR IAW SRM 51-70-06 REV 101 AND MM 51-21-10-REV 97.
DURING ROUTINE C-CHECK INSP FOUND CORROSION ON NR 1 PYLON LT AND RT UPPER HINGE FAIRING SUPPORT. REMOVED CORROSION. FOUND TO BE WITHIN LIMITâS. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-10-02 REV 101, AND SRM 51-20-01 REV 101.
DURING ROUTINE C CHECK INSP, FOUND EROSION ON THE LT WING OTBD T/E FLAP INBD FLAP SUPPORT FAIRING FORWARD AND MID FAIRING EXTERIOR SURFACE. ACCOMPLISHED REPAIR IAW SRM 51-70-06 REV 101, AND MM 51-21-10 REV 97.
DURING ROUTINE C-CHECK INSP, FOUND RT WING FUEL PUMP ACCESS PANEL NR 631AB CRACKED. REMOVED CRACKED ACCESS PANEL. INSTALLED NEW PANEL IAW MM 20-11-000 REV 97.
DURING ROUTINE C-CHECK INSP FOUND RT WING OTBD FLAP SUPPORT FAIRING DELAMINATED. ACCOMPLISHED REPAIR IAW SRM 51-70-17 REV 101 AND 51-21-10 REV 97.
DURING ROUTINE C-CHECK INSP, FOUND CORRODED FASTENERS ON RT WING BETWEEN STATION WS404- WS538. REMOVED CORRODED FASTENERS. INSTALLED NEW FASTENERS IAW SRM 51-40-02 REV 101 AND SRM 51-20-01 REV 101.
DURING ROUTINE C-CHECK INSP FOUND CORROSION ON RT WING ACCESS PANEL NR 633AB, 642AB, 642BB AND 642CB. REMOVED CORROSION. FOUND TO BE WITHIN LIMITâS. PERFORMED NDT. NO CRACKâS OR CORROSION. CLEANED, TREATED AND PRIMED AREA IAW SRM 57-20-01 FIGURE 201 REV 101, NDT D634T301 PART 6 51-00-19 REV 93, SRM 20-10-03 REV 036 AND SRM 51-20-01 REV 101.
DURING CRUISE, THE CREW NOTICED AN ABNORMAL VIBRATION FROM THE NR 2 ENG, THEN A LOSS OF OIL PRESSURE AND OIL QUANTITY. SHUTDOWN NR 2 ENG AND RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT.
OUTWARD DENT STA 544, STRINGER 31-30 LT REQUIRES REPAIR. REPAIRED AREA IAW B767 SRM 53-00-01, FIGURE 201. (S)
APPROX 6 INCH CREASE AT STA 1510, LONGERON STRINGER 36-35 LT, BELOW BULK CARGO DOOR IS OUT OF LIMITS. REPAIRED SKIN IAW B767-200 SRM 53-60-1. (S)
SCREW AND COUNTERSINK WASHER INSTALLED IN FUSELAGE SKIN OVER PREVIOUSLY BLENDED AREA AT APPROX STA 615 LONGERON STRINGER 34 RT. DAMAGED AREA COMPLIED WITH ON PREVIOUS REPAIR. (S)