N752CX
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
CORROSION ON THE LOWER SURFACE OF THE RIGHT WING LOWER SKIN
LEFT WHEEL WELL ON THE H BEAM IS A HYDRAULIC LINE B NUT THATS SITTING RIGHT IN FRONT OF THE CUSHION CLAMP AND BRACKET, AND THE BRACKET IS CORRODED.
CORROSION AROUND SUPPORT FITTING FASTENER AT STA 1180 RBL 28
CORROSION ON SUPPORT ANGLE IN LWW FOR STRUT DOOR CUTOUT
WHILE SERVICING MAIN LANDING GEAR STRUTS, THE AIRCRAFT TILTED TO THE LEFT CAUSING LEFT MAIN GEAR JACK TO COME INTO CONTACT LOWER WING AT JACKING PAD.
WHILE DRILLING OUT FASTENER IN THE LEFT-WING JACK PAD DOUBLER, THE DRILL CONTACTED THE OUTER PERIMETER OF HOLE IN THE WING SKIN
CORROSION AT THE HYD TUBING PASS THRU AT THE KEEL WALL IN THE LWW BS 1171-1180.
LEFT WING UPPER FIXED WING SKIN PANEL SUPPORT BEAM CORRODED IN SEVERAL PLACES
LEFT WING T/E INBD. OF DEFUEL VALVE HAS CABLE GUIDE BRACKET CORRODED
SEAL RETAINER SUPPORT STRUCTURE BROKEN IN RWW MLG DOOR CUTOUT
FOUND SKIN CORROSION COMMON TO RT FILLET PANEL @ STA 793, 805, 825 ALL ON SKIN PANEL 143N3561-4
NR 1 ENGINE COMPRESSOR BOOST FRAME FLANGE BRACKET BENT AND CRACKED AT THE ENGINE 11 O'CLOCK POSITION.
REPAIRED CORRODED LEFT WING REAR SPAR UPPER PANEL SUPPORT LIP AND SKIN.
FUSELAGE SKIN IS CORRODED AT LOWER FWD WING TO BODY ATTACHMENT. STA 740-781, S18L- 18R. OTHER PN +143N3521-9,143N359-1/2
FUSEELAGE LEFT SIDE STA 785-855 LEVEL 2 CORROSION2 BODY TO WING PANELS
RIGHT FUSELAGE CLOSEOUT FAIRING PANEL AFT OF MAIN CARGO DOOR FOUND CORROSION AT UPPER AND LOWER DOOR CORNERS NO PART NUMBERS FOUND ON REMOVE PANEL. FABRICATED NEW CLOSEOUT FAIRING PANEL, ASSIGNED NEW P/N 47696FAB01
NR 1 ENGINE REMOVED AND REPAIRED HP2 VALVE CASE BRACKET DUE TO BROKEN SUPPORT BRACKET NR 187303-0400-0178, AND AMES 47170REA622
REAR SPAR HYD BLOCK CLAMP SUPPORT BRACKET CORRODED.PN 271N6114-22
RIGHT WHEEL WELL PRESSURE DECK CORRODED STA1160 RBL3 P/N 144N8142-10
LW FUEL BOOST PUMP CUTOUT CORROSION IRSS 183
LEADING EDGE JUST ABOVE PYLON HAS CORROSION AROUND NUT PLATE
LEFT LANDING GEAR ELECTICAL CONNECTOR BRACKET CORRODED
RIGHT MLG DOOR IS GOUGED NEAR NO STEP PLACARD.
REAR SPAR FUEL BOOST PUMP CUTOUT TO BE CORRRODED
CORROSION ON PANEL SUPPORT ATTACHED TO THE AFT WALL IN THE LWW, FROM LBL7 TO LBL34
CORROSION ON THE UPPER EXTERIOR SURFACE OF THE RIGHT WING UPPER SKIN, LOCATED FWD OF THE RIGHT AILERON.
CORROSION ON THE KEEL WEB, AROUND THE HYD. TUBE FEEDTHROUGH, AT STA.1111, 47 INCHES UP FROM THE KEEL BEAM, IN THE LWW
DURING REPAIR ON NR 187303-0100-0192 IT WAS DISCOVERED THAT THERE IS A SCRIBE JUST FWD OF THE REPAIR AREA AT STA 740 STR 19L COMMON TO THE SKIN LAP.
FOUND AREA OF LW LOWER SKIN CORRODED JUST O/B OF BBL 70.50, JUST FWD OF STR L-10 ON THE EXTERNAL SURFACE
L1 FWD DOOR STOP FITTING DAMAGE WAS REMOVED BY BLEND. THIS DAMAGE EXCEEDS ALLOWABLE LIMITS.
LOWER FUSELAGE WING TO BODY PANEL SUPPORT BRACKET HAS CORROSION AT WIRING CLAMP HOOKUP BETWEEN LEFT WHEEL WELL AND GEAR
LEFT WING T/E FRONT SECTION OF LANDING GEAR SUPPORT BEAM HAS CORRODED PANEL SUPPORT BRACKET
EDIT (NEW CONTROL NUMBER) FROM DUPLIACATE CONTROL NUMBER IXXA20260111001 - FOUND CORROSION ON THE BLOCK SUPPORT TUBING IN THE OUTBOARD UPPER AREA OF THE LEFT WHEEL WELL OUTBOARD OF THE ANTISKID VALVES.
FOUND CORROSION ON THE BLOCK SUPPORT TUBING IN THE OUTBOARD UPPER AREA OF THE LEFT WHEEL WELL OUTBOARD OF THE ANTISKID VALVES.
GALLING, LIGHT CORROSION AND GOUGE AROUND BEARING FACE
RMLG STRUT DOOR SUPPORT BEAM IS CORRODED IN MULTIPLE AREAS
CORROSION ON THE INSIDE OF THE U CHANNEL THAT SUPPORTS THE HYD ISOLATION VALVE, LOCATED ON THE BACK WALL IN THE LEFT WHEEL WELL STA 1180
.CORROSION OF THE UPPER EXTERIOR SURFACE OFTHE RIGHT WING UPPER SKIN FWD OF THE AILERON
RIGHT WING INBD FLAP T/E FAIRING 671BB HAD A CRACKED RUB BLOCK AT FAIRING AFT ATTACH ARM.
REMOVED FOR ACCESS THE RW SIDE LINK ATTACH FITTING "MICKEY MOUSE FITTING" FOR SIDE LOAD FITTING ALIGHNMENT. DURING REMOVAL FOUND DAMAGED FREEZE PLUG/BUSHING IN HOLE.
RH AFT LOWER WING TO BODY FAIRING FRAME BS 1037 IS CORRODED
LEFT WING UNDER PANEL 551 AT SEVERAL AREA AROUND NUTPLATES ARE CORRODED.
RIGHT MLG STRUT DOOR SUPPORT BEAM IS HEAVILY WORN ALONG THE EDGE JUST FWD OF DRAG STRUT.
LEFT MLG DOOR GOUGED.
RH AFT WING TO BODY FAIRING ATTACH FRAME AT STA 1220 IS CORRODED.
RH AFT LOWER WING TO BODY FAIRING FRAME STA 1050 IS CORRODED.
FUSELAGE EXTERNAL SKIN IS CORRODED AT LAP SEAM S-20L BS 1718.
LEFT LOWER WING - BODY FAIRING SUPPORT BRACKET STA 958 IS CORRODED.
RIGHT WING LOWER SURFACE (INSPAR) IS CORRODED AROUND FASTENER AND RUNS UNDER PYLON RIGHT AT I/B SIDE OF PYLON APROX 5 INCHES AFT OF FWD SPAR AT STRINGER 14.
FOUND L1 DOOR ACTUATOR EMERGENCY RESERVIOIR UNSERVICABLE. REMOVED AND REPLACED L1 DOOR ACTUATOR EMERGENCY RESERVOIR IN ACCORDANCE WITH BOEING 757 AIRCRAFT MAINTENANCE MANUAL 52-11-30.
PRIOR TO ETOPS ENTRY POINT CREW REPORTED, BOTH FLIGHT MANAGEMENT COMPUTER DISPLAYS BLANK. ADDITIONALLY, AIR TRAFFIC CONTROL REPORTED NO ADS-B DATA RECEIVED. AIRCRAFT WAS IN IMC, ALTERNATIVELY, NO LIGHTING WAS SIGHTED. WITH COMPONENT FAULTS PRESENTING, FLIGHT COULD NOT CONTINUE AS SCHEDULED ETOPS ROUTE. AIR TURN BACK TO DEPARTURE STATION FJDG. CREW DECLARED AN EMERGENCY DESCENT. LANDING WAS UNEVENTFUL AND NO ADDITIONAL PRECAUTIONARY ACTIONS WERE NOTED. ON ARRIVAL, THE AIRCRAFT WAS GROUNDED FOR MAINTENANCE. SUBSEQUENT TO FLIGHT MANAGEMENT COMPUTER BUILT IN TEST EQUIPMENT CHECK AND ADDITIONAL TROUBLESHOOTING PER BOEING 757-200 (B757) FAULT ISOLATION MANUAL 34-61-FAULT TREE 802, 22-02-FAULT TREE 828, AND 34-61-FAULT TREE 818, LINE MAINTENANCE REPORTED LEFT CONTROL DISPLAY UNIT FAULTY. LEFT MULTI-PURPOSE DISPLAY UNIT REMOVED AND REPLACED IAW B757-200 AIRCRAFT MAINTENANCE MANUAL 34-61-02. OPERATIONAL CHECK GOOD. PER B757-200 FAULT ISOLATION MANUAL 34-45-FAULT TREE 810 AND AIRCRAFT MAINTENANCE MANUAL 34-45-00, TRAFFIC ALERT AND COLLISION/AIR DATA COMPUTING SYSTEM OPERATIONAL TEST SATISFACTORY. NO FAULTS FOUND. LIGHTNING STRIKE AND WATER INTRUSION IN E/E BAY CONDITIONAL INSPECTIONS IAW B757-200 AIRCRAFT MAINTENANCE MANUAL 05-51-19 AND 05-51-13 GOOD. NO EVIDENCE OF LIGHTNING STRIKE OR WATER INTRUSION IN E/E BAY. AIRCRAFT RETURNED TO SERVICE.
LH WING, WING SIDE OF BODY SPLICE, UPPER SPLICE EVIDENCE OF CORRION BS 900 TO BS 940.
CORROSION ON NOSE LANDING GEAR WHEEL WELL RIGHT HAND T-CHORD.
MULTIPLE TIMES DURING FLIGHT, R EMER DOOR EICAS MESSAGE DISPLAYED. FLIGHT CONTINUED UNAFFECTED. NO ADDITIONAL FAULTS NOTED. IAW B757 FAULT ISOLATION MANUAL 52-71-FAULT TREE 805, CLEARED DEBRIS AND VERIFIED SECURITY AND INTEGRITY OF DOOR SILL AREA. DOOR FOUND TO BE FAIRED WITH THE FUSELAGE. RIGHT NO 3 EMERGENCY EXIT DOOR OPERATIONAL TEST GOOD PER B757 AIRCRAFT MAINTENANCE MANUAL 52-21-01. NO FAULTS FOUND.
POST FLIGHT LINE MAINTENANCE IDENTIFIED, L4 DOOR EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED L4 EMERGENCY FLASHLIGHT BATTERY PER B757 AMM 25-64-00. OPERATIONAL CHECK GOOD.
POST FLIGHT LINE MAINTENANCE REPORTED, R4 EMERGENCY FLASHLIGHT INOPERTIVE. REMOVED AND REPLACED EMERGENCY FLASH LIGHT BATTERY IAW 757 AMM 25-64-00. OPERATIONAL CHECK GOOD.
DURING ROUTINE MAINTENANCE DISCOVERED L3 UPPER AND LOWER EMERGENCY LIGHTS, UPPER R3 DOOR LIGHTS AND LIGHTS AT ROW 4L INOPERATIVE. REMOVED AND REPLACED L3 DOOR EMERGENCY BATTERY PACK IAW B757 AMM 33-51-07. SYSTEM OPERATIONAL CHECK GOOD.
RIGHT OB LOWER MAIN AFT FLAP CORROSION ON LOWER SURFACE.
RIGHT OB LOWER MAIN AFT FLAP CORROSION ON LOWER SURFACE
RIGHT WING LOWER SURFACE TRAILING EDGE FROM WING TIP TO OUTBOARD FLAP HINGE NUMEROUS SPOTS OF CORROSION.
UPON REMOVAL OF # 2 PYLON INBOARD BATHTUB FITTING FOUND TO BE DAMAGED.
# 2 PYLON ANGLE CHANNEL COVER WORN SEVERAL AREAS.
RIGHT WHEEL WELL FS 1148 UPPER PRESSURE DECK RBL 3 CORROSION ON DOUBLER AROUND HYDRAULIC FITTING.
LEFT WHEEL WELL FS 1060 10 INCHS OUTBOARD OF KEEL WEB TOP SIDE OF WHEEL WELL HYDRAULIC LINE ISOLATOR GROMMET KEEPER CORRODED HARDWARE AND CORROSION ON ANCHORING ANGLE.
RIGHT WING TRAILING EDGE SUPPORT BRACKET ATTACHING TO FUSELAGE FOR PANEL HAS CORROSION BL. 70.50 STATION 1158.
RIGHT WHEEL WELL RBL 0 STATION 1096 HAS CORROSION ON INTER VERTICAL WEB AT MULTIPLE LOCATIONS.
THREE AREAS OF CORROSION ON EXTERNAL LOWER SURFACE OF LEFT WING SKIN ON STRINGER L6 AT WS 150.50 TO 177.50.
CORROSION ON UPPER SURFACE LEFT WING ABOVE PYLON AREA 3 SPOTS.
LEFT WING LOWER SURFACE CORROSION AROUND FUEL STICK 7 PANEL STATION 606.
RIGHT WING SKIN LOWER SURFACE CORRODED AT WS 663 REAR SPAR.
CORROSION ON EXTERNAL SIDE OFM LEFT WING LOWER SKIN AT WS 21.00 AND AFT FUEL PANEL 531CB CUTOUT.
PREVIOUS REPAIR ON LEFT WING UPPER SKIN AT WS 150.5 THRU WS 204.5 NEEDS REACCOMPLISHED PER AMES REA 47508REA41 AND FVCI ENGINEERING ORDER 22082-22 REV C.
#2 PYLON ACCESS THRU PANEL 443HL LOWER FORWARD CORNER STRUCTURE INTERNALLY HAS CORROSION.
AFT LOWER CARGO COMPARTMENT STA 1412 BELLY OF FRAME APPROX 29L STRINGER END HAS BAD CORROSION ON EAR OF STRINGER.
NUMBER 2 PYLON THRU ACCESS PANEL 443AR INTERNAL SKIN LWR SECTION AROUND OPENING HAS CORROSION.
#2 PYLON THRU ACCESS PANEL 443CR INTERNAL SKIN HAS CORROSION FWD AND BELOW CUTOUT.
#2 PYLON LEADING EDGE PANEL CORRODED SEVERAL SPOTS ON REPAIR RACK.
# 7 SLAT HAS COMPOSITE DAMAGE MARKED LOWER TRAI;ING EDGE.
#7 SLAT HAS COMPOSITE DAMAGE MARKED LOWER TRAILING EDGE.
RIGHT WING SKIN LOWER SURFACE IS CORRODED AT WS 742.
# 2 PYLON ACCESS THRU PANEL 433GL INTERNAL SKIN LOWER SECTION AROUND PANEL HAS CORROSION.
RIGHT WING TRAILING EDGE AROUND BBL. 70.50 BRACKET HAS CORROSION.
RIGHT WING UPPER TRAILING EDGE SKIN HAS CORROSION IN MULTIPLE AREAS ON BOTH SIDES (UPPER/LOWER) APPROXIMATELY AT WS. 188 TO WS. 216.
RIGHT WING TRAILING EDGE AROUND WS. 177.50 AFT OF STABILIZING LINK( IN BETWEEN LANDING GEAR AND WHEEL WELL) BRACKET HAS CORROSION.
RIGHT WING TRAILING EDGE AROUND BBL 70.50 HAS CORROSION.
RIGHT WING LOWER SKIN (PANEL #1) WS 663 HAS CORROSION.
RIGHT WING TRAILING EDGE UPPER SUPPORT BRACKET FOR WIRING HAS CORROSION AT WS 168 - WS 181.
RIGHT WING UPPER TRAILING EDGE SKIN HAS CORROSION IN MULTIPLE AREAS ON BOTH SIDES (UPPER/LOWER) APPROXIMATELY AT W.S. 188 TO W.S. 216.
RIGHT WING TRAILING EDGE AROUND W.S.177.50 AFT OF STABILIZING LINK 9IN-BETWEEN LANDING GEAR AND WHEEL WELL.SUPPORT BEAM
LOWER CHORD HAS CORROSION AT STA 1180 - 1242.
RIGHT WING SKIN LOWER SURFACE IS CORRODED AT W.S. 736 REAR SPAR.
# 1 PYLON OUTBOARD SIDE SKIN AROUND 433BL HAS CORROSION INTERNALLY IN MULTIPLE AREAS.
UPPER CARGO ROLLER AT RBL 30.0 IS CUT.
LEFT WING LOWER T/E EXTERNAL SKIN HAS CORROSION AT W.S. 656.
LEFT WING LOWER T/E EXTERNAL SKIN HAS CORROSION AT W.S.708.
# 1 PYLON INBOARD SIDE INTERNAL SKIN AROUND PANEL 433LR HAS CORROSION IN MULTIPLE AREAS.
NUMBER 1 PYLON INBOARD SIDE FORWARD EXTERNAL SKIN REQUIRES REMOVAL FOR CORROSION.
RIGHT WHEEL WEEL PRESSURE DECK WEB CORRODED AT STA 1159, RBL 4 AND STA 1153, RBL 6.
CORROSION ON UPPER SURFACE LEFT WING 48" FROM FUSELAGE 50" FROM LEADING EDGE.
CORROSION ON UPPER SURFACE LEFT WING 48" FROM FUSELAGE 50" FROM LEADING EDGE.
CORROSION BETWEEN SKIN AND PYLON STRUCTURE IN TWO PLACES FWD AND AFT SIDE INSIDE #1 PYLON OUTBOARD PANEL 433AL.
RIGHT WHEEL WELL PRESSURE DECK WEB CORRODED AT STA 1139.819, BL 0 - RBL 8.20
LEFT WING TRAILING EDGE WS 832 OUTBOARD OF THE AILERON AREAS OF CORROSION AROUND NUT-PLATES.
RIGHT WING SKIN LOWER SURFACE IS CORRODED AT W.S. 761 REAR SPAR.
RIGHT WING SKIN LOWER SURFACE IS CORRODED AT W.S. 751 REAR SPAR.
RIGHT WING SKIN LOWER SURFACE IS CORRODED AT W.S. 698 REAR SPAR.
LEFT WING INBD MAIN FLAP HAS 3 DAMAGED AREAS ON THE UPPER SKIN PANEL.
RIGHT WING UPPER SURFACE PANEL ABOVE LANDING GEAR ACTUATOR OUTBOARD BOLT CORROSION UNDER NUMEROUS NUT-PLATES.
RIGHT WING LOWER SURFACE IS CORRODED AT W.S. 646, REAR SPAR.
RIGHT WING CLECO POINT ATTACHMENT CORRODED APPROX WING STATION 223.
RIGHT WING UPPER T/E BONDED PANEL, BONDED SHIM STACK IS CORRODED
RIGHT WING T/E PANEL SUPPORT BEAM HAS CORROSION ON TOP APPROX W.S. 216.
# 2 PYLON ACCESS THRU PANEL 443HL LOWER FORWARD CORNER STRUCTURE INTERNALLY HAS CORROSION.
LOWER KEEL FITTING STA 1140 RIGHT WHEEL WELL REMOVED FOR REPLACEMENT BECAUSE REA REPAIR SHIFTING HOLE ATTACH POINTS.
LEFT WING CORROSION ON LOWER SURFACE OF SKIN AT FSS 580 10'' AFT OF L/E.
RIGHT WHEEL WELL 1040 HOT EXHAUST FRAME INBD ANGLE CORROSION UNDER NUT PLATES.
THE HEAT SHIELD ON THE AFT STRUT FAIRING HAS BULGED AREA ON THE INBOARD SIDE.
ANGLE IN THE LEFT WHEEL WELL SHOWS SIGNS OF CORROSION FOR THE PRESSURE SENSITIVE FLOW LIMITER ABOVE THE TRANSFER CYLINDER ACCUMALATOR ON THE KEEL WEB.
RIGHT WING T/E UPPER SUPPORT BEAM FWD ATTACH LINKS CORRODED APPROX W.S. 216 OR WBL 130.
#2 PYLON THRU ACCESS PANEL 443CR, INTERNAL SKIN HAS CORROSION FWD, AFT AND BELOW CUTOUT.
BRACKET IN THE RIGHT WHEEL WELL AT STA 1086 RBL4 HAS CORROSION.
KEEL WEB IN LEFT WHEEL WELL SHOWS SIGNS OF CORROSION AT STA 1146.
LEFT MLG BODY DOOR EXTENSION TRAILING EDGE IS CRACKED/DIS-BONDED.
RIGHT WHEEL WELL PRESSURE DECK WEB STA1160, RBL 8.20 - 16.50 CORRODED.
RIGHT WHEEL WELL PRESSURE DECK WEB STA 1159, RBL 4 AND STA 1153, RBL 6 CORRODED.
CORROSION ON WEB STA. 1100.
RIGHT WHEEL WELL PRESSURE DECK WEB STA 1139.819, BL 0, RBL- 8.20 CORRODED.
RT WHEEL WELL PRESSURE DECK SHOWS SIGNS OF CORROSION STA 1130 - 1154 RBL 0-12.
RW SKIN LOWER SURFACE CORRODED, RT WING STATION 676.
FWD ATTACH ANGLE AT PANEL 198JR IS CRACKED(RT FILLET AREA) REF AMES N/R 147534-0100-0281
BRACKET CORRODED
RWW PRESSURE DECK CORRODED
#7 SLAT COMPOSITE DAMAGE
LWW SUPPORT ANGLE CORRODED
RWW UPPER PRESSURE DECK STIFFENER CORRODED
LEFT WING LOWER SKIN PANEL CORRODED.
RWW STIFFENER CORRODED
CORROSION UPPER SURFACE LW
LMLG DOOR FORWARD LOWER ANGLE CORRODED
ANGLE CORRODED LWW
LWW ANGLE CORRODED
LW LOWER SURFACE IS CORRODED
PANEL 117BL CORRODED
RIGHT WHEEL WELL PRESSURE DECK CORRODED
RIGHT WHEEL WELL PRESSURE PANEL CORRODED
RIGHT WING TRAILING EDGE SUPPORT BRACKET CORRODED.
LW L/E RIB LWR STRAP AT WS 285.65 CORRODED
LT WING PANEL 551CT CORRODED
LEFT WING LOWER WING PNL STA. 822-829 IS CORRODED AT FUEL PNL
LWW UPPER WEB STIFFENER AT STA 1144 LBL 16.5 CORRODED
REF AMES NR 147534-0100-0150 LWW FS1180 35" OTBD KEEL CENTER WEB AT CEILING ISOLATION VALVE STAND OFF MOUNTING WEB CORROSION ON AFT SIDE.
FOUND CRACK IN THE RIGHT O/B AFT FLAP T/E LOWER SURFACE BY THE O/B SUPPORT FITTING
LEFT WING UPPER SURFACE L/E CORRODED
LEFT WING TE EXTERNAL SKIN CORRODED AT WS 717.5 TO 775.5
LONGITUDINAL STIFFENER IN LEFT WHEEL WELL AT LWS 38 FROM STA 1100-1110 CORRODED
KEEL WEB IN LEFT WHEEL WELL AT STA 1175 SHOWS SIGNS CORROSION AROUND HYDRAULIC LINES
LEFT WING LOWER SKIN CORRODED FROM WS 150-177.5 AT AFT SPAR
REF AMES NR 147534-0100-0077 AFT SIDE OF STA 900 WEB IS CORRODED AROUND PNEUMATIC DUCT AND HYDRAULIC LINE RBL 12
RT WEHEEL WELL PRESSURE DECK CORRODED STA 1100 RBL 64-58
LOWER FLANGE OF ANGLE IN THE KEEL AREA AT STA 1168 CORRODED
RT WHEEL WELL PRESSUER DECK CORRODED STA 100 RBL 49
RT WHEEL WELL PRESSURE DECK CORRDED STA 1094 RBL 47
RT WHEEL WELL PRESSURE DECK CORRODED
CORROSION ON UPPER SURFACE LWING 60" FROM FUSELAGE 18" FROM L/E. REF AMES NR 147534-0500-0030
LT WHEEL WELL PRESSURE DECK CORRODED
LT WHEEL WELL PRESSURE DECK CORRODED
UPPER SURFACE LEFT WING ABOVE PYLON AREA CORRODED
CORROSION ON EXTERNAL SURFACE OF LEFT WING LOWER SKIN AT WS 74.5 AND APPROXIMATELY SIX INCHES AFT OF STRINGER L8 REF AMES NR 147534-0500-0018
LEFT WING EXTERNAL LOWER SURFACE SKIN STR L6 AT WS 150.5 TO 177.5 CORRODED
CORROSION ON EXTERNAL SIDE OF RIGHT WING REAR SPAR LOWER CHORD IN RIGHT WHEEL WELL WHERE SPAR ATTACHES TO CENTER WING BOX
UPPER CARGO ROLLER TRAY AT RBL 30.0 IS CUT REF AMES N/R 147534-0200-0042
AIRCRAFT GROUNDED FOR UNSCHEDULED POWER PLANT MAINTENANCE, IDENTIFIED R1 DOOR EMERGENCY EXIT DOORS LIGHT INOPERATIVE. REMOVED AND REPLACED REMOVED AND REPLACED R1 EMERGENCY EXIT LIGHTS POWER SUPPLY IAW AMM 33-51-07. OPERATIONAL CHECK SATISFACTORY. NO FURTHER DEFECTS NOTED.
DURING EMERGENCY LIGHT OPS CHECKS MULTIPLE LIGHTS FAILED TO COME ON. REMOVED AND REPLACED TWO BATTERY PACKS AT M736 AND M737 IAW AMM 33-51-07. REMOVED AND REPLACED 5 AMP FUSE IAW AMM 33-51-07. PERFORMED OPS CHECK OF EMERGENCY LIGHTS IAW 33-51-00 OPS CHECK GOOD. REMOVED AND REPLACED EMERGENCY LIGHT SWITCH IAW B757-SWPM 20-83-11 OPS CHECK GOOD.
DURING EMERGENCY LIGHT OPS CHECKS MULTIPLE LIGHTS FAILED TO COME ON. REMOVED AND REPLACED TWO BATTERY PACKS AT M736 AND M737 IAW AMM 33-51-07. REMOVED AND REPLACED 5 AMP FUSE IAW AMM 33-51-07. PERFORMED OPS CHECK OF EMERGENCY LIGHTS IAW AMM 33-51-00. OPS CHECK GOOD. REMOVED AND REPLACED EMERGENCY LIGHT SWITCH IAW SWPM 20-83-11 OPS CHECK GOOD.
RIGHT WING STA 718 STRINGER U12 WAS CORRODED. REMOVED AND ELVAUATED CORROSION, ORIGNAL MATERIAL .100 IN., MATERIAL LOSS .068 IN., MATERIAL REMAINING .022., MATERIAL LOSS ALLOWABLE 10%. FOUND TO BE OUT OF LIMITS. REMOVED DAMAGE AND PERFORMED STRINGER REPAIR IAW SRM. 57-00-03 DET.III., REPAIR 1 FIGURE 201, 53-20-03 AND ER RES 15213.
NR 2 NACELLE STRUT DOOR (443LL) HAS CORROSION ON FWD BOTTOM CORNER ON DOOR LANDING. ACCOMPLISHED REPAIR IAW ENGINEERING ORDER CONTROL 20191, TITLED REPAIR-DOUBLER, INBOARD NACELLE SIDE SKIN PANEL ASSEMBLY NR 2 ENG, PPS 176.25.
NON-ROUTINE 2832N248 DISCREPANCY. LMWW, CORROSION ON FWD LOWER FLANGE OF LT MAIN GEAR DOOR ACTUATOR SUPPORT BEAM STA 1120. CORRECTIVE ACTION, LT WHEEL WELL MAIN GEAR DOOR ACTUATOR SUPPORT REPAIRED IAW FVCI EO CONTROL 20184.
AIRBORNE/PEMCO NON-ROUTINE 2832N241 DISCREPANCY: CORROSION ON KEEL BEAM LOWER SURFACE NLEFT CHORD AT STA 1170 CORRECTIVE ACTION: REPAIRED PER FVCI E.O. #20174
FWD WET AREA, FLOOR SUPPORT BETWEEN BS 324 AND 345 CORRODED AT RBL 40. ACCOMPLISHED EO 20215, REPAIR OF SEC. 41 WITHOUT ANY DEVIATIONS.
NR 2 NACELLE STRUT DOOR (443LL) HAS CORROSION ON FWD BOTTOM CORNER ON DOOR LANDING. ACCOMPLISHED REPAIR IAW ENGINEERING ORDER CONTROL 20191, TITLED REPAIR-DOUBLER, INBOARD NACELLE SIDE SKIN PANEL ASSEMBLY NR 2 ENG, PPS. 176.25.
NON-ROUTINE 2832N258 DISCREPANCY. RMWW, CORROSION ON KEEL BEAM RIGHT CHORD UPPER SURFACE IN RADIUS OF TAB THAT ATTACHES TO STA 1120 GEAR DOOR ACTUATOR SUPPORT BEAM. CORROSION RUNS UNDER SUPPORT BEAM. CORRECTIVE ACTION. REMOVED CORROSION ON RT KEEL BEAM CHORD UPPER SURFACE AT STA 1120, RBL 7.5, MINIMUM REMAINING THICKNESS 0.187", REMOVED 0.063", ORIGINAL THICKNESS 0.250". REWORK SUBSTANTIATED AND REPAIRED IAW ENGINEERING ORDER CONTROL NR 20178.
FWD LAV SVC PANEL INSIDE ALL FASTENER ARE CORRODED AND 2EA COVER PLATES HAVE CORROSION. REMOVED AND REPLACED FASTENERS AND FABRICATED 2EA COVER PLATES ON 2832N1011, ACCOMPLISHED EO 20195 ON N/R 2832N245 WITHOUT ANY DEVIATIONS.
NON-ROUTINE 2832N283, NR 1 ENG ZONE 433 NACELLE STRUT MID STRUCTURE O/B PANEL, LWR AFT CORNER; FOUND EXCESSIVE CORROSION. REPAIRED NR 1 ENGINE NACELLE STRUT MID STRUCTURE O/B PANEL, ACCOMPLISHED REPAIR ON ENGINEERING ORDER 20192, WITHOUT ANY DEVIATIONS.
NWW LOWER CHORD HAS CORROSION BETWEEN RT AFT GEAR DOOR AND HINGE FITTINGS. REMOVED CORROSION ON NWW LWR CHORD RT AFT AREA IAW-B757-200-SRM-53-10-14. GRID MAP LWR CHORD AREA 2 EA AREA ON LWR CHORD, IAW- PRELIMINARY-E.O. CONTROL 20613. HFEC ACCOMPLISHED IAW-NTM-PT6-51-00-19 AND ROTO PROBE ACCOMPLISHED, IAW-NTM-PT6-51-00-16. ACCOMPLISHED EO CONTROL 20163.
NON-ROUTINE 2832N271 DISCREPANCY, NWW, STA 263 BLKHD AFT FACE, LOWER CHORD HAS CORROSION FROM STR 26L TO STR 26R. CORRECTIVE ACTION: REPAIRED NWW STA 263 BULKHEAD LOWR CHORD PER EO CONTROL 20172 + 20181.
CORRODED UPPER AFT SPAR CAP AT LEFT WS 180. REPAIRED THE SPAR CAP IAW 47313REA05.
PANEL SUPPORT BEAM INBD OF PANEL 197BL IS CORRODED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-04. REMOVED AND REPLACED IAW DWG 149N7550, AND SRM 51-40-02, PARA 7. AIRCRAFT GROUNDED
RIGHT MLG WW BS 1040 BULKHEAD ABOVE ECS DUCT,STIFFENER IS CORRODED AT FASTENER. REMOVED & REPLACED THE CHANNEL STIFFENER IAW SRM 51-40-02 & 58-757-35-0024.
NR 1 PYLON AFT MOUNT BARREL NUT FWD GUIDE TUBE IS CRACKED, LANYARDS ARE NOT SECURE. REPAIRED THE MOUNT BARREL NUT FWD GUIDE TUBE IAW AMES 47313REA01 AND SECURED THE LANYARDS IAW AMM 71-21-03.
RT OTBD FORE FLAP LOWER SURFACE HAS 2 SMALL AREAS OF CORROSION OTBD OF THE OTBD SUPPORT MECHANISM. REPAIRED THE AREAS OF CORROSION ON THE RT WING OTBD FORE FLAP LOWER SURFACE IAW SRM 57-53-01, REPAIR 5, FIG 201. AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE.
LWR KEEL WEB HAS AREA OF CORROSION AROUND HYD LINE BULKHEAD FITTING JUST FWD AND ABOVE LANDING GEAR DOOR ACTUATOR. REPAIRED THE VERTICAL LWR KEEL WEB IAW REA47313 REA 03.REINSTALLED ABOVE THE GEAR DOOR ACTUATOR. LEAK CHECKED IAW IAW AMM 29-11-00. ACFT GROUNDED.
L4 INBOUND FLASHLIGHT BATTERY DEAD. REMOVED AND REPLACED THE BATTERY IAW AMM 25-60-00.
CAPTAIN'S EMERGENCY FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED THE FLASHLIGHT BATTERIES IAW AMM 25-64-00. OPS CHECKED SATISFACTORY. AIRCRAFT RELEASED TO SERVICE.
IN FLIGHT EMERGENCY DECLARATION. AIR TURN BACK. 5 COMPRESSOR STALLS/SURGES WITH ENGINE EXCEEDANCE VALUES RECORDED. INDICATIONS RETURNED TO NORMAL THEREAFTER AND PRIOR TO LANDING. AIRCRAFT GROUNDED FOR BORESCOPE INSPECTION AND FURTHER ANALYSIS. WORK IN PROGRESS. REMOVED AND REPLACED VALVE ASSY. REMOVED AND REPLACED RIGHT ENGINE. OPERATIONAL CHECKS SATISFACTORY. ENGINE RUNS SATISFACTORY. FAULT NOT DUPLICATED. NO FURTHER DEFECTS NOTED. AIRCRAFT RELEASED TO SERVICE ETOPS 180.
SKIN DENTED BETWEEN BS 1701 AND 1720, STRINGER 11 TO 16L. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01, FIGURE 101. REPAIRED THE AREA IAW ENGINEERING DOCUMENT 47255REA01.
L3 AND R3 EMERGENCY EXIT DOOR LIGHTS INOPERATIVE. R & R BATTERY POWER PACK AT MID/AFT IAW AMM 33-51-07. OPS CHECK SATISFACTORY. ADDITIONAL FAULTS NOT NOTED. ACFT RELEASED TO SERVICE.
R4 DOOR WILL NOT DISARM. RETRACTABLE DOOR MECHANISM STICKING DUE TO EXCESSIVE CONTACT WITH DOOR LINERS. TRIMMED DOOR LINER ON L4 DOOR. OPERATIONAL CHECKED SATISFACTORY IAW AMM 52-11-20. ACFT RELEASED TO SERVICE.
L4 DOOR WILL NOT DISARM. UPON TROUBLESHOOTING FOUND RETRACTABLE DOOR MECHANISM STICKING DUE TO EXCESSIVE CONTACT WITH DOOR LINERS. TRIMMED DOOR LINER ON L4 DOOR. OPERATIONAL CHECK SATISFACTORY. ACFT RELEASED TO SERVICE ETOPS 180.
L4 DOOR HARD TO CLOSE. DOOR SEAL WILL NOT REMAIN SECURE IN SEAL RETAINER. REMOVED L4 DOOR. R & R L4 DOOR GUIDE ARM ASSEMBLY IAW AMM 52-11-04. ADJUSTED LATCH ROLLER IAW AMM 52-11-00 2G STEP 2. OPERATIONAL CHECKED SATISFACTORY. PRESS LEAK CHECKED IAW AMM 05-51-24 SATISFACTORY. FAULT NOT DUPLICATED. NO ADDITIONAL FAULTS NOTED. ACFT RELEASED TO SERVICE.
L4 EXTERIOR DOOR HANDLE DOES NOT OPERATE PROPERLY. R & R WORN BEARING SLEEVE ON L4 DOOR EXTERIOR HANDLE & ADJUSTED IAW AMM 52-11-25. OPERATIONAL CHECKED SATISFACTORY IAW AMM 52-11-00. ACFT RELEASED TO SERVICE.
L4 DOOR DIFFICULT TO CLOSE FROM INSIDE. DOOR SEAL WILL NOT STAY IN TRACK. RE-INSTALLED SEAL IN RETAINER TRACK IAW AMM 52-09-01. VERIFIED INTEGRITY OF SEAL WITH OPERATIONAL CHECK. NO ADDITIONAL FAULTS NOTED. SEAL REMAINED IN TRACK. ACFT RELEASED TO SERVICE.
R4 PAX & CREW DOOR HARD TO CLOSE. DETAILED VISUAL INSPECTION, NOTED NO FAULTS ATTRIBUTING TO REPORTED DIFFICULTY. LUBRICATED R4 DOOR LATCH CRANK ROLLERS MECHANISM IAW AMM 12-21-18. OPERATIONAL CHECK VERIFIED INTEGRITY OF R4 DOOR. ACFT RELEASED TO SERVICE.
R1 EXTERIOR EMER LIGHT INOPERATIVE. DOES NOT ILLUMINATE. UPON TROUBLESHOOTING NOTED THE POWER SUPPLY HAS NO POWER. R & R THE BATTERY EMER POWER SUPPLY IAW AMM 33-51-07. OPERATIONAL CHECKED SATISFACTORY. NO FURTHER DEFAULTS NOTED. ACFT RELEASED TO SERVICE.
L1 INTERIOR EMER SIGN INOPERATIVE, DOES NOT ILLUMINATE. REPAIRED WIRE 23532-0011-22 AT CONNECTOR D4532 IAW SWPM 20-10-13. OPERATIONAL CHECK SATISFACTORY IAW AMM 33-51-01. NO ADDITIONAL FAULTS NOTED. ACFT RELEASED TO SERVICE.
ENGINE RUN, AFTER ENG SHUTDOWN L1 DOOR SLIDE DEPLOYED. R & R L1 SLIDE & L1 DOOR ASSIST RESERVOIR IAW AMM 25-66-01 & 52-11-30 RESPECTIVELY. DOOR ASSIST PRESS CHECKS SATISFACTORY IAW DOOR ASSIST. L2 DOOR OPERATIONAL CHECKED SATISFACTORY, NO FAULTS NOTED. ACFT RELEASED TO SERVICE.
ROW 2 RT OVERHEAD BIN, PAX CABIN MEGA PHONE INOPERATIVE. DEFERRED IAW MEL 25-63-01-01. CAT D, NO FLY DATE 09 11 2015. PART REQUISITIONED, WORK IN PROGRESS.
ROW 6 LT SIDE LIGHT STRIP MISSING RED DOT. ROW 2 REPOSITIONED, PHOTO LUMINESCENT STRIP AT ROW 2 LT SIDE TO REVEAL RED EXIT LOCATOR SQUARE IAW AMM 33-51-00. ACFT RELEASED TO SERVICE.
NOSE LANDING GEAR INDICATOR INOPERATIVE DURING APPROACH & LANDING. AFTER 2ND CYCLE OF LG LIGHT WITH 1/2 ILLUMINATION OCCURRED. EMER DECLARED AT DESTINATION STATION. NO ISSUES WITH LANDING. GND PERSONNEL ADVISED OF ALL THREE LG DOWN INDICATION. NO EICAS MX MSGS WERE NOTED. PERFORMED PSEU TEST IAW MM 32-09-04. NO INFLIGHT MSGS PRESENT. FOUND DIODE CARD IN NLG POSITION INDICATOR LOOSE. RESEATED INTO SOCKET & RELAMPED IAW MM 33-13-00. LG POSITION INDICATION SYS TESTED SATISFACTORY IAW AMM 32-61-00. ACFT RELEASED TO SERVICE.
RIGHT FWD EMER EXIT AISLE LIGHT INOPERATIVE. COMPLIED WITH FIM 33-51 FT 802. REPAIRED WIRING AT RT FWD AISLE LIGHT SOCKET IAW SWPM 20-10-11 & RELAMPED IAW AMM 33-51-05. SYSTEMS OPERATIONAL CHECKED SATISFACTORY IAW AMM 33-51-00.
L3 DOOR, R3 DOOR & LT FWD AISLE EMER EXIT LIGHTS INOPERATIVE. COMPLIED WITH FIM 33-51 FT 802. R & R L3 DOOR EMER EXIT LIGHTS BATTERY POWER SUPPLY ASSEMBLY IAW AMM 33-51-07. SYS OPERATIONS CHECKED NORMAL IAW AMM 33-51-00.
R4 DOOR EMER EXIT LIGHTED SIGNS INOPERATIVE. R & R R4 DOOR EMER LIGHTS POWER SUPPLY BATTERY PACK IAW AMM 33-51-07. SYSTEMS OPERATIONAL CHECKED SATISFACTORY IAW AMM 33-51-00.
R4 DOOR EMER EXIT SIGN INOPERATIVE. RESEATED R4 DOOR EMER EXIT LIGHTS POWER PACK BATTERY IAW AMM 33-51-07. OPERATIONS CHECKED NORMAL IAW AMM 33-51-00.
L1 DOOR RESERVOIR DEPLOYED. FAULT ISOLATED TO DOOR ASSIST BOTTLE DIAPHRAGM. REMOVED, REPAIRED, SERVICED & INSTALLED L1 RESERVOIR IAW AMM 52-61-3 & AMM 12-15-10. LEAK & OPERATION CHECK SATISFACTORY.
L4 AFT GIRT BAR COVERS NOT ATTACHED. AFT GIRT BAR COVERS REMOVED. DMI 45243 INITIATED. CAT A NO CONDITIONS NFD 10/15/2014.
L4 DOOR FWD GIRT BAR COVERS NOT ATTACHED. FWD AFT COVERS REMOVED. DMI 45243 INITIATED IAW MEL 25-20-01-01. CAT A NO SPECIAL CONDITIONS NO FLY DATE 10/15/2014.
LEFT RAM AIR DOOR WORN BEYOND LIMITS IAW AMM 21-53-01. R & R LT RAM AIR DOOR. OPERATIONAL CHECK SATIS IAW AMM 21-53-01.
EICAS MSG DISPLAYED LT EMER ADJUSTED LT EMER INDICATION SENSOR IAW AMM 52-71-00. OPERATIONAL CHECK SATISFACTORY.
EICAS MESSAGE TE FLAP DISAGREE DISPLAYED. FLAPS 30 SELECTED & FAILED TO POSITION WITH AIR, AIR SPEED LESS THAN 165. CYCLED FLAPS 3 TIMES & INSPECTED SLATS. CHECKED FSGU & DVI OF FLAP PDU XMT FOUND LOOSE CONNECTOR. CLEANED & SECURED CONNECTOR. RECYCLED FLAPS AGAIN, NO DEFECTS NOTED. IAW BSWPM 20-60-06 SECURITY & CONDITION OF TE FLAP PDU DISCONNECT D01806 WERE INSPECTED. NO DEFECTS WERE NOTED WITH PINS OR WIRING IAW BWDM 27-51-11. NO MSG ON FSEU. ACFT VERIFIED ETOPS 180.
FORWARD CABIN EMERGENCY LIGHTS WILL NOT ILLUMINATE. REPAIRED WIRE ON L1 DOOR OVERHEAD LIGHT IAW B767 AMM 33-51-00, SWPM 20-30. OPERATIONS CHECKED GOOD, ACFT WAS GNDED.
PASSENGER COMPARTMENT, LT SIDE POSITION NR 4 EMERGENCY LIGHT INOPERATIVE. ACFT GROUNDED. REPLACED LEFT POWER SUPPLY. OPS CHECKED GOOD IAW AMM 33-51-07.
PASSENGER COMPARTMENT, RT SIDE EMERGENCY LIGHTS INOPERATIVE. R & R EMERGENCY LIGHTING BATTERY PACK IAW AMM 33-51-07. OPS CHECKED GOOD IAW AMM 33-51-00.
L1 DOOR ESCAPE SLIDE GIRT BAR ENGAGEMENT LIGHT INOPERATIVE. DURING TROUBLESHOOTING, EMERGENCY DOOR ASSIST BOTTLE WAS USED AND ESCAPE SLIDE FELL OFF L1 DOOR. SLIDE DID NOT DEPLOY. R & R L1 DOOR EMERGENCY POWER ASSIST RESERVOIR BOTTLE IAW AMM 52-11-30. INSPECTED L1 ESCAPE SLIDE ASSY IAW AMM 25-66-01. NO DEFECTS NOTED. REINSTALLED SLIDE ASSY TO L1 DOOR IAW AMM 25-66-01. REINSTALLED SLIDE COVER ASSY IAW AMM 52-11-02. L1 DOOR OPS CHECKED GOOD. R & R THE FWD GIRT BAR PROXIMITY SENSOR IAW AMM 25-66-11. L1 DOOR GIRT BAR ENGAGEMENT LIGHT, OPS CHECKED GOOD.
CAPTAIN'S OXYGEN MASK HARNESS IS LEAKING. R & R CAPTAINS OXYGEN MASK IAW AMM 35-11-51. OPS CHECKED GOOD.
DURING DITCHING EXERCISE, FOUND 2 FLASHLIGHTS FROM SURVIVAL KIT INOPERATIVE. R & R SURVIVAL KIT IAW AMM 25-64-00.