N745AX
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
AFTER PUSHBACK, FLAP/SLAT ELEC STATUS MSG. REPLACED FLAP/SLAT SHUTOFF VALVE MODULE PER B767 AMM 27-51-48 LEAK & OPS CK GOOD AT THIS TIME A/C RELEASED CAT I PENDING 30/40 TEST PLACARD ROTATED. A/C RETURNED TO SERVICE.
ON LANDING, CREW RECEIVED FLAP/SLAT ELEC WARN STATUS MSG. PERFORMED FIM 27-51 FT 836. FOUND PREV FAULT # 27810047. CHECKED FLAP/SLAT SHUTOFF VALVE CONDITION IAW AMM 27-51-48. OPS CHECK GOOD. NO FAULTS NOTED. A/C RETURNED TO SERVICE.
DURING SERVICE CHECK INSPECTION FOUND EMERGENCY LIGHT BY L1 DOOR INOP MTX REMOVED AND REPLACED EMERGENCY BATTERY M735 AND OPS CHECK GOOD IAW AMM 33-51-07. AND RETURNED A/C TO SERVICE
WHILE DESCENDING THRU FL 280 AND BELOW, GEAR NOT DOWN EICAS WARNING AND CONFIG LIGHT CAME ON WHEN THRUST LEVERS ARE AT IDLE. REMOVED AND REPLACED LH RA RCVR AND XMTR ANTENNAS IAW 767 AMM 34-33-02. OPS CHECK GOOD. A/C DOWNGRADED CAT I PENDING 30/40 TESTS REF LP 39538-48/3 FOR RALM STATUS. RALM PLACARDS ROTATED. PLACARDS REMOVED. NO REACTIVATION PROCEDURES REQ. REF LP 39538-48/1. A/C RETURNED TO SERVICE.
DURING INSPECTION, FOUND NR 1 DESCENT DEVICE INOPERATIVE. REMOVED AND REPLACED NR 1 DESENT DEVICE IAW 25-61-03. ACFT RETURNED TO SERVICE.
DURING SERVICE CHECK FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP, MTX GROUNDED A/C AND ATTEMPTED TO REMOVE & REPLACE, FOUND BROKEN WIRE PUT BACK TO ORIGINAL IAW AMM 33-51-01 REPAIRED THE WIRE IAW SWPM 20-30-00 OPS CHECKED GOOD. RETURNED A/C TO SERVICE
DURING TAXI, CTR R FUEL PUMP EICAS MESSAGE ILLUMINATED AFTER PUSHBACK. T/S IAW FIM 28-22 FT 805. FOUND UFI INDICATION. RESET UFI IAW SUP AMM 28-23-00. OPS CHECK GOOD. ACFT REMAINS NO ETOPS. ACFT RETURNED TO SERVICE.
ON CREW PREFLIGHT, FOUND FIRE DET SYS INDICATION B# LINE WAS YELLOW (AMBER). MAINTENANCE RESECURED ELEC CONNECTOR ON CARGO FIRE PANEL IAW B767 AMM 26-11-00 AND PERFORMED AFOLTS TEST IAW B767 AMM 26-10-00. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
FWD EQUIP VALVE EICAS MESSAGE AFTER BLOCK OUT. NO OTHER LIGHTS OBSERVED. AIRCRAFT RETURNED TO BLOCKS (BTB). REPLACED MANIFOLD INTERCONNECT VALVE IAW AMM 21-58-01. LEAK CHECK GOOD. OPS CHECKED GOOD.
ON TAXI OUT, FWD EQPT VALVE MESSAGE ILLUMINATED. AIRCRAFT RETURNED TO BLOCKS (BTB). MAINTENANCE PERFORMED FIM 21-58, TASK 805. MSG CLEARED, A/C OK FOR SERVICE.
DURING TAXI OUT, FWD EQUIP VALVE MSG ILLUMINATED. AIRCRAFT RETURNED TO BLOCKS (BTB). REMOVED & REPLACED EQUIP COOLING INDICATION CARD I.A.W AMM 21-58-24 OPS CHECK GOOD I.A.W AMM 21-58-00 MESSAGE CLEARED, A/C NO ETOPS. AIRCRAFT RETURNED TO SERVICE.
DURING TAXI OUT C HYD DEM PUMP PRESSURE WHEN FLAPS ARE IN TRANSITION , ACFT RETURNED TO GATE (BTB) AND MTX GROUNDED ACFT . DEFERRED ADP MTX TRANSFERRED TO DI# 69856 IAW MEL 29-11-3, MBCB 01/27/26, PULLED AND COLLARED C/B, MX PROCEDURES C/W, PLACARD INSTALLED, AND RETUENED ACFT TO SERVICE.
DURING MAINTENANCE INSPECTION, A1 SMOKE DETECTOR FAILED INDICATION ON CARGO FIRE PANEL. REMOVED AND REPLACED A1 MCD SMOKE DETECTOR IAW IAI SUPP AMM 26-14-01. OPS CECK GOOD. AIRCRAFT RETURNED TO SERVICE.
DURING CREW PRE-FLIGHT, 1B MCD CARGO DECK SMOKE DETECTOR FAILED. MAINTENANCE DEFERRED DI# 67028 IAW MEL 26-16-2-2. AIRCRAFT RETURNED TO SERVICE.
DURING MAINTENANCE INSPECTION, EMERGENCY LIGHTS NOT ILLUMINATING. RE-SEATED CANNON PLUGS IAW FIM 33-51 FT 803. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
ON TAKE OFF, LT ENGINE EGT FLUCTUATED. AIRCRAFT ABORTED TAKE OFF AND RETURNED TO BLOCKS. (BTB). MAINTENANCE C/W HIGH ENERGY STOP INSPECTION IAW AMM 05-51-14. NO DISCREPANCIES NOTED AT THIS TIME. REMOVED AND REPLACED D4208P AND D4208J (PYLON CONNECTORS), D932 (AT THE JUNCTION BOX) AND THE WIRING IN BETWEEN IAW SWPM 20-63-00, 20-10-11, AND WDM 77-21-11. FOR OPS CHECKS SEE LP 39328-82/2. ALL OPS CK GOOD. PERFORMED ENGINES HIGH POWER RUNS IAW AMM 71-00-00. LT ENGINE EGT DID NOT FLUCTUATE. ACFT REMAINS NO ETOPS. AIRCRAFT RETURNED TO SERVICE.
DURING THROUGH FLIGHT, MAIN CARGO FIRE DETECTION AMBER LIGHT IN SECTION 3B. MAINTENANCE DEFERRED IAW 26-16-2-1 MEL MAINTENANCE PROCEDURES C/W PLACARD INSTALLED MBCB 9/27/25 REPETITIVE INSPECTION REQUIRED BEFORE EACH DEPARTURE 26-16-2-1 IAW MEL 26-16-2-1. AIRCRAFT RETURNED TO SERVICE.
DURING MAINTENANCE INSPECTION, FOUND FLIGHT DECK EMERGENCY EXIT SIGN LIGHT INOP. CLEANED AND REINSTALLED CONNECTOR FOR POWER SUPPLY. LIGHT OPS CHECKS GOOD IAW AMM 33-51-00. AIRCRAFT RETURNED TO SERVICE.
DURING MAINTENANCE INSPECTION, FOUND L1 DOOR EMERGENCY EXIT SIGN LIGHT INOP. CLEANED AND REINSTALLED CONNECTOR FOR POWER SUPPLY. LIGHT OPS CHECKS GOOD IAW AMM 31-51-00. AIRCRAFT RETURNED TO SERVICE.
DURING INSPECTION, EMERGENCY LIGHTS POWER SUPPLY BATTERY M737 INOP BATTERY M735 ALSO INOP. FOUND CONNECTORS D170 AND D1088 NOT SEATED CORRECTLY FER WDM 33-51-01 AND AMM 33-51-00 ALL LIGHTS OPERATE NORMALLY. AIRCRAFT RETURNED TO SERVICE.
COMPLIED WITH DETAILED INSPECTION OF SURFACE OF SKIN AT STATION 955 FAIL-SAFE CUT OUT. FOUND CORROSION & MINOR TOOLING MARKS. REMOVED & SPOT FACED SKIN CORROSION IAW REA B653-61707-MR & 47008ORD10. SDR INFO CORRODED, PN 145T3420, SN NSN, PART NAME RT SKIN, FROM STATION 955. ACFT WAS GNDED.
LEFT PRESS DECK FWD DOUBLER IS CORRODED BEYOND LIMITS. REFERENCE DWG 145T8752. NEW FWD LT PRESS DECK FWD DOUBLER, PN 145T8754-33 INSTALLED ON JC 53500013-003 & DOCUMENT 47008ORD03, TAG 1409197. SDR INFO CORRODED, PN 14578754-33, PART NAME DOUBLER, SN NSN, FROM STATION 955, FROM LBL 85. ACFT WAS GNDED.
LEFT PRESS DECK WEB IS CORRODED BEYOND LIMITS IAW DWG 145T8752. FABRICATED NEW WEB FROM 2024-T3 .125" PO 0057631. MACHINED EDGES ANODIZED, PRIMED & PAINTED IAW DWG 145T8752 & MIL-A-8625 TYPE I CLASS 1 & SRM 51-40-05. SDR INFO CORRODED L2, PN 14578752-235, PART NAME WEB, SN NSN, FROM 955, LBL 85. ACFT WAS GNDED.
LEFT FWD I BEAM STRINGER AT LBL 85.90 IS CORRODED BEYOND LIMITS. REFERENCE DWG 145T8752. FABRICATED NEW SECTION OF I BEAM FROM BAC 1518-751 2024-73511, PO 0037419 IAW REA B653-61698. SDR INFO CORRODED, PN 14578752-37, SN NSN, PART NAME STRINGER, FROM STATION 955 FROM LBL 85. ACFT WAS GNDED.
FOUND FWD LT BILGE PANEL, AFT MOUNT ANGLE CORRODED & NUTPLATES CORRODED. R & R UPPER CHORD ASSEMBLY AT STATION 544 IAW SRM 51-40-02 PAR 4B 1-5 & SRM 51-40-02 PARA 4 & PARA 7, SOPM 20-50-01, AMM 25-53-03 4, THROUGH COMP AMM 53-01-05 3C 3 TO 3C 4 & AMM 25-53-01. SDR, CORRODED LEVEL 2, PN BAC1506-3400, PART NAM CHORD, FS & BS FROM ONLY STATION 522 - 544, LBL 16 - 24. ACFT WAS GNDED.
FLOOR WEBBING AT FS 550, RBL 36 HAS A HOLE CORRODED THROUGH WEB, WEB IS APPROX 5 FEET IN LENGTH. R & R FLOOR WEB AT FS 550, RBL 36 IN FLC IAW SRM 51-40-02. SDR INFO CORRODED LEVEL 2, PN 451T2504-17, NAME PANEL, FS & BS FS 522 - 642, EXACT STRINGER & WS RBL 36 - 44. ACFT WAS GNDED.
DURING ROTARY HOLE SCAN, FOUND 2 CRACKS IN HOLES COMMON TO THE FAIL SAFE STRAP. ACCOMPLISHED TRIM OUT IAW EA5350013-003 & DOCUMENT 47008ORD03. CRACKED 1/4", PN 145T2524, PART NAME, LEFT FAIL SAFE STRAP, SN NSN, FS & BS LOCATION STATION 955. ACFT WAS GNDED.
DURING DETAILED VISUAL INSPECTION OBSERVED CORROSION & CRACKS AROUND HOLES COMMON TO FAILSAFE STRAP & T FITTING. PREVIOUSLY MENTIONED ON NON-ROUTINE 1369. TRIMMED OUT CRACKED & CORRODED AREA OF FAILSAFE STRAP AS WRITTEN IAW EA 53500013-003 & DOCUMENT 47008ORD03. SDR INFO CRACKED 1/4", CORRODED LEVEL 2, PN 14372524, PART NAME, LEFT FAILSAFE STRAP, SN NSN, FS & BS LOCATION STATION 955. ACFT WAS GNDED.
DURING HFEC SURFACE SCAN FOUND END OF CRACKS MENTIONED ON NON-ROUTINE 1369 & MARKED END OF CRACK LOCATIONS WITHIN TRIM OUT LIMITS. ACCOMPLISHED TRIM OUT OF FAIL-SAFE IAW EA 53500013-003 & DOCUMENT 47008ORD03. SDR INFO 1/4" CRACKED, PN 145T2524, PART NAME, LEFT FAIL-SAFE STRAP, SN NSN, FS & BS LOCATION STATION 955. ACFT WAS GNDED.
SKIN HAS A LARGE CREASE GOING THROUGH LAP SPLICE AT LT FS 1395, STRINGER 36L. REPAIRED LAP SPLICE CREASE IAW REA B653-61583-MR & SRM 53-00-21. SDR INFO, PN 146T3240 & 146T3230, SN N/A, PART NAME FUSELAGE SKINS, FS & BS LOCATION ON ACFT FS 1395 TO 1417, STRINGER LOCATION ON ACFT, 38L - 35L. ACFT WAS GNDED.
DDR ITEM NR 21, REINFORCED REPAIR DOUBLER FOUND ON LT FUSELAGE, STATION 1654, STRINGER 33L - 34L. REPAIRED DAMAGED SKIN IAW SRM 53-00-01 REPAIR 29. SDR, CORRODED, PN 148T3211, PART NAME SKIN, SN NSN, FS & BS LOCATION 1651 TO 1661, STRINGER & WS LOCATION, STRINGER 33L - 34L. ACFT WAS GNDED.
DDR ITEM NR 8, REINFORCED DOUBLER REPAIR FOUND ON LT FUSELAGE, STATION 441 - 451, STRINGER 32L. DDR NR 8 DOC REPAIR LT FUSELAGE HAS BEEN COMPLIED WITH IAW REA B653-61674-MR. CORRODED LEVEL 2, PN 143T3210-1, PART NAME SKIN, SN N/A, FS & BS FROM 442 TO 453, STRINGER & WS 32L. ACFT WAS GNDED.
ANGLE FOUND CORRODED, AFT LOWER CARGO APPROX STATION 1263, RBL 42.0. R & R ANGLE IAW SRM 51-40-02 PARA 7D & E. CORRODED L2, PN 146T5050-84, PART NAME ANGLE, SN N/A, FS & BS FROM 1263 TO 1280, STRINGER & WS FROM STRINGER 33R, RBL 42. ACFT WAS GNDED.
BEAM UNDER OTBD ROTARY ACTUATOR FOR INBD FLAP HAS AREA OF EXFOLIATION AT OTBD END OF BEAM. R & R RT WING CHORD PANEL SUPPORT T AT OTBD ROTARY ACTUATOR IAW SRM 51-40-2. SDR CORRODED L2, PN 113T1407-6, PART NAME CHORD, SN NSN, STRINGER & WS RT WING STATION 226.3 - 284.7. ACFT WAS GNDED.
MULTIPLE SPOTS OF CORROSION ALONG THE STRINGER 37L LAP JOINT FROM LFS 412 - 434. COMPLIED WITH REA B653-61659-MR TO REPAIR FUSELAGE SKIN CORROSION. CORRODED L2, PN 141T3230, PART NAME SKIN, EXACT FS & BS LOCATION ON ACFT STATION 412 - 434, EXACT STRINGER & WS LOCATION ON ACFT STRINGER 37L - 38L. ACFT WAS GNDED.
AFT PYLON FIRE SEAL IS CRACKED AT MARKED LOCATION. REMOVED, FABRICATED, HEAT TREATED & INSTALLED AFT NR 1 PYLON FIRE SEAL IAW DWG 313T1380. SDR INFO, CRACKED LENGTH 1/4", PN 313T1380, PART NAME HEAT SHIELD, NAC LOCATION NR 1 NACELLE, STATION 308.5. ACFT WAS GNDED.
LEFT WING INBD TE PANEL SUPPORT BEAM ON LWW CEILING, NEAR WS 249, IS CORRODED NEAR FWD END. R & R LT WING CEILING INBD TE PANEL SUPPORT BEAM WS 249 IAW SRM 51-40-2. FABRICATED PARA TO REA B757-61588. SDR INFO, CORRODED L2, PN 113T1622-110, PART NAME CHORD, SN NSN, STRINGER & WS LOCATION, LT WING STATION 249. ACFT WAS GNDED.
LARGE DENT ON DOUBLER AT LOWER FUSELAGE 390, STRINGER 20L. REPAIRED DENT IAW REA B653-61656-MR. SDR INFO PN 368-53-11-90699-287, SN NSN, PART NAME REINFORCING STRAP, FS & BS LOCATION ON ACFT 390L STRINGER & WS LOCATION ON ACFT STRINGER 20L. ACFT WAS GNDED.
WHEN INSTALLING THE ARROWHEAD PANEL, FOUND STRUT DOOR LOWER SEAL RETAINER MOUNT, Z ANGLE, CRACKED ON AFT END. R & R Z ANGLE IAW SRM 51-40-02. SDR INFO, CRACKED 3", PN 313T1380-111, SN 1389552, PART NAME NR 2 PYLON, STATION 880 - 883. ACFT WAS GNDED.
NUMBER 2 ENG OTBD CORE COWL LOWER FRAME CRACKED BY NR 3 LATCH. REMOVED & REINSTALLED NR 3 LATCH & LOWER FRAME IAW SRM 51-40-02 D. WELD REPAIR LOWER FRAME IAW PROCESS STANDARDS MANUAL CH 900-7-2-1. PRIMED & PAINTED LOWER FRAME IAW AMM 51-21-02 & 51-21-10. COMPLETED SDR INFORMATION PN 314T1210-200, PART NAME LONGERON, SN NA, CRACKED 1.5 INCH, EXACT FS & BS LOCATION ON ACFT NR 2 NACELLE, STATION 301. ACFT WAS GNDED.
NUMBER 1 FLAP SUPPORT 1 - 3, BEAM HAS 7 HOLES WITH DEFECT INDICATIONS WITH HFEC ROTARY SCAN. REPAIRED FLAP SUPPORT 1-3 BEAM IAW REA CO57-61601-MR. SDR INFO CRACK UNKNOWN, PN 113T1313-7, PART NAME 1 - 3 BEAM, SN ABXT883, LOCATION STRINGER & WS FROM LWS 798.2. ACFT WAS GNDED.
TWO STRINGER CLIPS & SHEAR TIE AT FS 1329, BETWEEN STRINGER 33L & 34L CORRODED. FABRICATED & INSTALLED 452T2706-4 ANGLES IAW DWG 452T27006. SDR INFO, CORRODED L2, PN 452T2706-4, SN NA, PART NAME ANGLE, FS & BS ON ACFT 1280L & 1324L, STRINGER LOCATION ON ACFT STRINGER 34L. ACFT WAS GNDED.
NUMBER 2 FLAP SUPPORT 1 - 3, BEAM HAS A WORN BUSHING AT JOINT 1. REPLACED NR 1 JOINT BUSHING ON THE NR 2 FLAP SUPPORT 1B BEAM IAW REA C057-61596-MR ITEM 18. CRACK UNKNOWN LENGTH, PN BACBZBAP, PART NAME BUSHING, SN NSN, LT WING. ACFT WAS GNDED.
NUMBER 2 FLAP SUPPORT 1 - 3, BEAM HAS 5 HOLES WITH DEFECT INDICATIONS & 1 HOLE WITH DEFECT INDICATION & CORROSION AROUND OUTSIDE OF HOLE, FOUND WITH HFEC ROTARY SCAN. REMOVED DEFECTS FROM NR 2 FLAP SUPPORT 1 - 3, BEAM IN 5 LOCATIONS HFEC ROTARY SCAN FOUND NO DEFECTS IAW NDT MAN PART 6 51-00-16, REA C057-61596-MR. SDR CRACK UNKNOWN LENGTH, PN 113T1314-15, PART NAME LT WING 1 - 3 BEAM, SN ABXT892. ACFT WAS GNDED.
NUMBER 8 FLAP SUPPORT, 1 - 3 BEAM HAS 4 HOLES WITH DEFECT INDICATION WITH ROTARY SCAN. REMOVED DAMAGE TO 4 HOLES ON NR 8 FLAP SUPPORT, 1 - 3 BEAM. HFEC ROTARY SCANNED HOLES & FOUND NO DEFECTS IAW NDT MAN PART 6 51-00-16. COMPLIED WITH C057-61597-MR. SDR INFO CRACK, PN 113T1313-8, SN ABXT954, PART NAME FLAP SUPPORT NR 8, RT WING STATION 616.0. ACFT WAS GNDED.
AFT FUSELAGE EXTERNAL SKIN IS CRACKED, AT STATION 1735 FWD OF LT LOWER STAB FAIRING, SEEN FROM INSIDE. REMOVED SKIN PANELS 148T7321-1 & 148T7320-17. INSTALLED NEW SKIN PIECES. SDR INFO, CRACKED 1.5", PN 148T7321-1, SN N/A, PART NAME SKIN PANEL, FS LOCATION ON ACFT, LT FUSELAGE STATION 1737. ACFT WAS GNDED.
STRINGER 7L LOWER LEG, IS CRACKED APPROX. 2.5" AT APPROX FS 680. STRINGER WAS R & R IAW SRM 53-00-03 & SKETCH ES02821, MATERIAL PO 0064680 & PO 0037419. APPLIED PROTECTIVE COATINGS IAW SRM 51-20-01. SDR INFO, CRACKED 3", PN BAC1498-207, SN NONE, PART NAME STRINGER, FS LOCATION ON ACFT 680 TO 683, STRINGER LOCATION ON ACFT 7L. ACFT WAS GNDED.
LEFT WING LE RIB, CORRODED ON OTBD SIDE AT LES 454, IN SEVERAL PLACES. R & R LT WING LE AT LES 454 IAW SRM 51-40-02. SDR INFO, CORRODED L2, PN 114T2202-23, SN NSN, PART NAME RIB, STRINGER & WS LOCATION ON ACFT, FROM LT WING STATION WS 454. ACFT WAS GNDED.
SKIN ON THE FWD OF THE ANTENNA AT STATION 392, STRINGER 39R HAS .125" CRACK, VERIFIED WITH HFEC. REPAIRED SMALL CRACK IAW SRM 53-00-01 REPAIR 8 FIG 201 SECTION I STEPS 1 - 3. REPAIR RECORD SUBMITTED. SDR INFO CRACKED .125, PN 141T0118, SN NSN, PART NAME FUSELAGE SKIN, FS & BS LOCATION ON ACFT FS 392, STRINGER & WS LOCATION ON ACFT STRINGER 39R - 38R. ACFT WAS GNDED.
RIGHT WING OTBD INTERNAL LE AIR LOAD STRUT HAS CORROSION, AT FWD END & ON WIRE CLAMP STANDOFF, AT APPROX LES 612, INBD OF NR 9 SLAT, OTBD AUXILIARY TRACK. R & R AIR LOAD STRUT IAW SRM 51-40-02. SDR CORRODED, LEVEL 2, PN 114T2210-16, PART NAME RIB, SN NSN, EXACT STRINGER & WS LOCATION, FROM RT WING STATION 612. ACFT WAS GNDED.
DEFECT FIRST OFFICER'S PRIMARY FLIGHT DISPLAY & NAVIGATION DISPLAY BLANKED OUT. REPLACED DATA CONCENTRATOR UNIT. NO OTHER ACTION TAKEN & NO FURTHER FAULTS OCCURRED REGARDING THE BLANKING OF THE FIRST OFFICER'S PRIMARY FLIGHT DISPLAY & NAVIGATION DISPLAY.
RIGHT HAND STATION 1809 FWD CHORD AT STRINGER 12R HAS AN ELONGATED HOLE. IAW NEA53800003-001 S. CHORD REPAIRED IAW EA53800002-002 & 003. REMOVED TWO EACH FASTENERS, FOUND ELONGATED HOLE, CRACK INDICATION FOUND. REAMED HOLE TO 310, REPLACED FASTENERS, TREAT, PRIMED & PAINTED DOUBLER, INSTALLED PANEL 314CRX, IAW SRM 51-40-02, 51-21-01, AMM 55-10-02 & NDT MANUAL PART 6 51-00-16. SDR INFO PN 148T2740-10, NSN, CHORD, CRACKED, ELONGATED HOLE 0.01 INCH, STATION 1809-5, STRINGER 12R. ACFT WAS GROUNDED.
FAN EXIT CASE INNER SKIN CORRODED AT NR 7 FAN FRAME STRUT. BLENDED AREA IAW GECF6-80A ESM 70-42-00. REPAIRED AREA IAW ABX AIR REA-C072- 60864 RFTS NR E-46177 REVISION DATE 2-11-14. SDR INFO PN 9295M34G15, SN 3HY20080, AFT FAN CASE, CORRODED, RT, NAC 160.0. ACFT WAS GROUNDED.
FORWARD LOWER CARGO DOOR FWD LOWER SEAL DEPRESSOR IS CRACKED. R & R SEAL DEPRESSOR IAW DWG 143T6201, 51-40-2, SEE PARTIAL WORK ACCOMPLISHED FOR WORK COMPLETED. CRACK LENGTH: .250", PN: 143T6201-27, PART NAME SEAL DEPRESSOR, LOC: 550 TO 550.
AFT LOWER CARGO CEILING PANEL ATTACH INTERCOSTAL CORRODED AT NUTPLATE BS 1410. R & R ATTACH INTERCOSTAL IAW SRM 51-40-02,
CORROSION ON TOP SURFACE OF KEEL BEAM, FROM BL 0 TO LBL 11, BS 977 TO 1080. BLENDED CORRODED AREAS FOUND TO BE OUT OF LIMITS IAW SRM 53-50-12, FIG 101. REPAIRED IAW REA B653-60727-MR, PN: 145T8612-1, KEEL BEAM HORIZONTAL WEB CORRODED, 999 TO 1065 BLO TO LBL10. ACFT WAS GROUNDED.
RIGHT WING UPPER L/E SKIN AT APPROXIMATELY RWS 837 HAS HEAVY CORROSION. REPAIRED IAW REA B657-60709 MR. AFT WAS GROUNDED.
UPPER CARGO BELOW FLOOR PANELS BETWEEN BS-1197 & BS-1605 , S88L-S88R CORROSION ON NUMEROUS CLIP NUTS AT UPPER CHORDS. FLOOR LOCK PLATES, FLOOR PANEL FASTENER LOCATIONS. R & R CORRODED CLIP NUTS IAW SRM 51-40-02. R & R CORRODED FLOOR LOCK PLATES AND SEAT TRACK BEAM AT STA 1480-1520, LBL 70 IAW SRM 51-40-02, CORRODED LEVEL 2, PN: 3658-53-00-90518 SEAT TRACK BEAM, LOC: 1480 TO 1520 LBL70. ACFT WAS GROUNDED.
LEFT WING UPPER T/E SURFACE HAS CORROSION AT LWS 1018. REMOVED CORROSION IAW SRM 57-20-01, FIG 101. REPAIRED IAW REA B657-60708. ACFT WAS GROUNDED.
UPPER DECK CARGO TRACK IS CORRODED AT LBL 11, BETWEEN BS 1461- 1605. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. R & R CARGO TRACK IAW SRM 51-40-02. ACFT WAS GROUNDED.
NR 2 NACELLE PANEL AFT OF THE NR 2 HYD BAY DOOR, OTBD, HAS SEVERAL SMALL AREAS OF CORROSION, REPLACED PANEL WITH NEW PN 313T3381-84 REINSTALLED IAW AMM 20-11-00-2 AND SRM 51-40-02, PART 7. SDR: PN: 313T3381 PYLON PANEL ASSY AFT RT CORRODED, LEVEL 2 LOC: NAC STA 353, NAC STA 380, NAC WL 420 TO NAC WL 160. ACFT WAS GROUNDED.
UPPER DECK CARGO TRACK AT LBL 33 BETWEEN BS 1461-1605 IS CORRODED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. R & R CARGO TRACK IAW SRM 51-40-02. ACFT WAS GROUNDED.
UPPER CARGO AFT WALL FLOOR DRAIN STRUCTURE BELOW FLOOR PANELS BS 1605 , S88L-S88R HAS CORROSION ON UPPER SURFACE. REMOVED DRAIN AND DRAIN LINES AT STA 1605, REMOVED LT AFT WALL. R & R LT AND RT OTBD FLOOR BRACES AT STA 1580 TO 1605, PICKED UP FLOOR PANEL HOLES IN OTBD FLOOR BRACES REINSTALLED AFT WALL, AND DRAIN AND DRAIN LINES. IAW SRA 51-40-02.53-00-51, 51-40-05 AND AMM 51-41-00. CORRODED LEVEL 2, PN: ANGLE SEC 46 FLOOR PANEL 368-53-16-94490-201 AND LOC: 1580 TO 1605 20R TO 20L. ACFT WAS GROUNDED.
RT WING UPPER T/E SKIN HAS CORROSION AT APPROXIMATELY RT WING STA 746.2. REPAIRED RT WING UPPER T/E SKIN AT APPROX RT WING STA 746.2 IAW REA B657-60709-MR. ACFT WAS GROUNDED.
RT WING UPPER T/E SKIN HAS CORROSION AT APPROX 772.2. REPAIRED RT WING UPPER T/E SKIN AT APPROXIMATELY RT WING 772.2 IAW REA B657-60709-MR. ACFT WAS GROUNDED.
CORRODED FLOORBEAM AT DOOR CUTOUT AT BS 1329. R & R FLOORBEAM IAW DWG 146T1212.
SHEAR TIE AT FS 1329 BETWEEN STRINGER 39 LT AND 39 RT AFT LOWER CARGO HAS SURFACE CORROSION, MARKED. R & R SHEAR TIE AS REQUIRED IAW DWG 146T1212 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07. FABRICATED PART IAW DWG 146T1212 & SRM 51-20, 51-40-02. ACFT WAS GROUNDED.
NR 2 PYLON AFT "V" WEB IN FRONT OF THE STINGER INTERNALLY IS CRACKED. R & R CRACKED CHANNEL IAW SRM 51-40-02. PN 313T3380-244, CHANNEL, CRACKED, LENGTH 1.5" FS /BS LOC ON ACFT: NAC 410.59. ACFT WAS ON GROUND.
REMOVED CORROSION ON LT WING UPPER T/E WS 1006 IAW SRM 57-20-01, FIG 101. REPAIRED AREA IAW REA B657-60708-MR. ACFT WAS GROUNDED.
WHERE THE LOWER TCAS OMNI DIRECTIONAL ANTENNA MOUNTS IT HAS LIGHT CORROSION ON SKIN. R & R EXTERNAL TCAS DOUBLER IAW SRM 51-40-02 AND SB 767-34-0087, REV 4, DATED AUG 5 1993. PN 141T0112U31, PARTNAME: ANTENNA DOUBLE CORRODED LEVEL 2 FS/BS 399 STR/WS 538. ACFT WAS GROUNDED.
LEFT WING LOWER T/E PANEL SUPPORT BEAM FOR PANEL 551XBX IS CORRODED. REMOVED CORROSION FOUND LOWER CHORD TO BE OUT OF LIMITS. REPAIRED AREA IAW SRM 57-51-02 REPAIR 2. ACFT WAS GROUNDED.
CORROSION ON ANGLE ON KEEL BEAM TO UPRIGHT AT BS 1043, BL0 TO LBL 11. R & R ANGLE IAW DWG 145T8610,
ANTENNA BLANKING PLATE AT BS 731 S34-35L CRACKED. REPAIRED IAW SRM 53-00-01, FIG 101ACFT WAS GROUNDED.
ANTENNA BLANKING PLATE AT BS 731 S34-35R CRACKED. REPAIRED WITH SRM REPAIR IAW SRM 53-00-01, FIG 101. ACFT GROUNDED.
FUSELAGE SKIN COMMON TO RT LOWER HORSE COLLAR PANEL 314CRX IS CRACKED AT APPROX STA 1746. R & R SKIN SECTION 148T7321-4 IAW SRM 51-40-02 PAR 4 PG 2. REAR SDR INFORMATION: CRACKED PN 148T7321-4. PARTNAME SKIN PANEL-STAB FAIRING EXACT FS/BS LOCATION ON ACFT FROM 1746 TO 1809 EXACT STR/WS LOCATION ON A/C FROM 21R TO 22R. ACFT WAS GROUNDED.
BULK CARGO, BS 1461, FLOOR SUPPORT CRACKED. R & R FLOOR SUPPORT BS 1420-1540. INSTALLED IAW SRM 51-40-02. ACFT WAS GROUNDED.
AFT LOWER CARGO BULK CARGO FLOOR AREA,BETWEEN BS 1417 & 1439, STRINGER 39L IS CORRODED. REMOVED 8.1 INCH SECTION OF STRINGER. LOCATED, DRILLED, AND INSTALLED REPAIR SHIM, CHANNEL, ANGLES, AND STRINGER FILLER ALONG WITH FAYE SEALING IAW SRM 53-00-03, FOG 201 DETAIL IV AND SRM 51-20-05. ACFT WAS GROUNDED.
FORWARD LOWER CARGO BS 434 , STRINGER SPLICE 30L CRACKED. SPLICE REMOVED AND INSTALLED NEW SPLICE IAW SRM 51-40-02. SDR CRACKED 1" PN 140T0115-14, STRINGER SPLICE EXACT FS/BS LOCATION ON AC 434 TO 438 AND 30L TO 30L. ACFT WAS GROUNDED.
AFT LOWER CARGO BS 1100 LT FLOORBEAM HAS CORROSION UNDER ROLLER ASSY. INSTALLED LT AND RT OTBD ROLLER TRAYS IAW CMM 25-50-25. ACFT WAS GROUNDED.
RT WING UPPER T/E SKIN HAS HEAVY CORROSION AT RWS 790. REMOVED CORROSION, ROTO PEENED REINSTALLED FASTENERS AND RESTORED FINISH IAW EA B657-60709 MR. ACFT WAS GROUNDED.
FLOORBEAM AT BS 1087 HAS SEVERAL CORRODED NUTPLATES. REMOVED CORROSION IAW SRM 53-00-07. ACFT WAS GROUNDED.
KEEL BEAM PANEL ATTACH CROSSMEMBER AT STA. 1013 CORRODED AROUND NUTPLATE ON UPPER SURFACE. REMOVED AND REPLACED CROSSMEMBER IAW B767-200 SRM 51-40-02. PART NUMBER: 145T8629-3, PARTNAME: SPLICE TEE, FS/BS LOC: 1008 TO 1008, STR/WS: B/L9L TO B/L9R, CORRODED, LEVEL 2. ACFT WAS GROUNDED.
CRACKED BRACKET ON LOWER FWD END OF THE E6 RACK. R & R AND INSTALLED BRACKET ON LOWER FWD END OF E6 RACK IAW DWG 453T12B2 FOR WORK COMPLETED. ACCOMPLISHED. ACFT WAS GROUNDED.
ATTACH PLATE FOR AFT END OF NR 1 CORE COWL OTBD SKIRT FAIRING IS CRACKED. REPAIRED CRACKED PLATE, INSTALLED NEW NUTPLATE AND INSTALLED PLATE ONTO PYLON IAW DWG 311T1570 AND SRM 51-40-02, PN: 311T1570-55 NAME: RIB, NACELLE 269.5. ACFT WAS GROUNDED.
KEEL PANEL 194AL FORWARD ATTACH CROSSMEMBER CORRODED AROUND NUTPLATE ON UPPER SURFACE. R & R CROSSMEMBER IAW SRM 51-40-02. SDR INFO - PN: 145T8629-3, SPLICE TEE FS/BS LOC: 962 TO 962, STR/WS LOC: B/L9L TO B/L9R, CORRODED, LEVEL 2. ACFT WAS GROUNDED.
NR 1 NACELLE ANGLE BRACKET JUST FWD OF THE OTBD ARROW HEAD PANEL, ABOVE THE EXHAUST SEAL IS CRACKED. REPAIRED CRACKED ANGLE IAW SRM 51-40-02 AND ABX PROCESS STANDARDS MANUAL. ACFT WAS GROUNDED.
CORROSION ON UNDER SIDE OF ANGLES FOR ROLLER TRAY MOUNT AT LT SIDE AT STA 1417. REMOVED ROLLER TRAY MOUNT ANGLE SUPPORTS AND REPLACED WITH NEW PARTS INSTALLED IAW SRM 51-40-02. ACFT WAS GROUNDED.
UPPER CARGO BS 1065-1197, UNDER FLOOR PANELS, SEAT TRACK CORRODED ON AND AROUND SEVERAL NUT CLIPS. CLEANED AREAS UNDER FLOOR PANELS, AND FOUND AREA BS 1145, LBL34 TO BE OUT OF LIMITS IAW SRM 53-00-52. REPAIR FABRICATED AND INSTALLED IAW REA B653-60704-MR. ACFT WAS GROUNDED.
NR 2 NACELLE ANGLE BRACE CRACKED AT OTBD AREA JUST FORWARD OF THE ARROWHEAD PANEL. R & R AFT FIRE SEAL IAW SRM 51-40-02. ACFT WAS GROUNDED.
UPPER CARGO LOADING SYSTEM, LT SIDE AFT WALL CARGO TRACK CRACKED. REMOVED UPPER CARGO LOADING SYS CRACKED WALL RAIL AND REPLACED WITH A NEW CARGO TRACK IAW CMM 25-50-0288. ACFT WAS GROUNDED.
AFT LOWER CARGO, BULK CARGO FLOOR AREA BS 1439 ABOVE STRINGER 38R FLOOR SUPPORT VERTICLE STIFFENER IS CRACKED IN TWO PLACES. REMOVED, LOCATED, DRILLED AND INSTALLED REPLACEMENT STIFFNER IAW DWG 146T1217. ACFT WAS GROUNDED.
NR 2 ENGINE LT SIDE OF AFT MOUNT HAS MINOR CORROSION AND LT SIDE LINK HAS PITTING. R & R NR 2 ENGINE AFT MOUNT AS REQUIRED, WITH A NEW ENGINE MOUNT, IAW AMM 71-21-02-4. CORROSION, PN: 310T1020-3, MOUNT, AFT ENG, SN: 48. NAC 308.50. ACFT WAS GROUNDED.
CEILING PANEL ATTACH ANGLE CORROSION AT BS 1351. R & R CEILING SUPPORT ANGLES IAW SRM 51-40-02. ACFT WAS GROUNDED.
CEILING PANEL ATTACH ANGLES CORRODED AT STA 1263. R & R ANGLES LBL27-RBL40 IAW SRM 51-40-02 CLEANED TREATED AND PRIMED CORROSION ON ANGLE RBL 40 & RBL 66 IAW SRM 53-00-51, FIG 101. FOUND TO BE WITHIN LIMITS. ACFT WAS GROUNDED.
PASSING 5500 FT, WHEEL WELL FIRE WARNING INDICATED. PERFORMED WW AREA INSPECTION ACC FIM 26-17-09-00 FOR DAMAGE. NO PNEUMATIC LEAK EVIDENCE. NO OBVIOUS DAMAGE AND NO SENSOR DEFECTS NOTED. APPLIED FIM 26-17-09-1 FIRE WARNING TEST. ALL STEPS WERE VERIFIED. BITE TEST SUCCESSFUL. FOLLOW UP ACTION RESULTED IN R & R WHEEL WELL FIRE DETECTOR ELEMENT IAW AMM 26-17-01-4. OPS CHECKED NORMAL, ACFT GROUNDED.
ON TAKEOFF ROLL LOUD POP HEARD, AFTER TAKEOFF SEVERAL STATUS MESSAGE CAME ON; BODY OVERHEAT ON, ADP PRESSURE LIGHT ON, AND CABIN ALT AUTO ON. DUCT LEAK NOTICED. FOUND PNEUMATIC DUCT BLOWN AT STA 1249, ALONG WITH SMOKE DETECTOR TUBING DAMAGED, BODY OVERHEAT DETECTION CLAMPS DAMAGED, SMOKE CURTAIN AND SIDE WALL LINING DAMAGED. CREW REPORTED SMOKE BUT MAY HAVE BEEN RELATED TO RAPID PRESSURE LOSS (FOGGING). AIRCRAFT FERRIED TO MIA FOR REPAIR PER PER REA B636-60549. AND DI 74874. MBCB 05-13-13. CODE 27, ACFT WAS GROUNDED.
WHEEL WELL FIRE EICAS INDICATION DURING CLIMBOUT. RAN NON-NORMAL, EICAS WARNING EXTINGUISHED. FOLLOWED FIM PROCEDURE 26-17-00-1 AND ALL CHECKS AND REQUIREMENTS ACCOMPLISHED. ALSO INTERROGATED BRAKE TEMPERATURE MONITOR AND PHYSICALLY CHECKED BRAKE UNITS FOR OVER TEMPERATURE EVIDENCE. REPEATED FIRE DETECTOR TEST AND ALL INDICATIONS NORMAL, ACFT WAS GROUNDED.
LEFT OVERWING ESCAPE SLIDE DOOR OPEN. UPON INSPECTION FOUND THAT THE INTERLOCK CONTROL ROD LATCH MECHANISM WAS IN THE DOWN POSITON (OPEN). LOCKED THE ROD LATCH MECHANISM BACK INTO THE CLOSED POSITION IAW AMM 25-65-09-4. ACFT WAS GROUNDED.
STRINGER 22 LT CRACKED JUST AFT OF BS 676, AIRCRAFT GROUNDED. REPAIRED IAW REA B653-59624-MR.
FUSELAGE SKIN HAS 2.5 IN CRACK, STA 785 S35L. INSTALLED PNL 193FL IAW B767 AMM 20-11-00. REPAIRED FUSELAGE SKIN IAW B767 SRM 53-00-01, FIG 201.
STRINGER CLIP IS CRACK AT STA 720 STR 37L. INSTALLED NEW STRINGER CLIP P/N 140T2101-413 AT STA 720 STR 37L IAW THE B767-200 SRM 51-40-02. AIRCRAFT WAS GROUNDED.
STRINGER CLIP IS CRACK AT STA 720 STR 39L. INSTALLED NEW STRINGER CLIP PN 140T2101-413 AT STA 720 STR 39L IAW THE BOEING 767-200 SRM 51-40-02. AIRCRAFT WAS GROUNDED.
WEB PANEL (FLOOR) CORRODED AT SCREWS STA 527 RBL 22. FABRICATED NEW FLOOR WEB PER SAMPLE IAW B767 SRM 53-30-53 FIG 1. AIRCRAFT WAS GROUNDED.
WEB STA 588 TO 566 HAS TORN FASTENER HOLES. REPLACED FLC FLOOR WEB AT STA 566 TO 588 WITH NEWLY FABRICATED ONE PER SAMPLE IAW B767 SRM 51-40-02 AND BOEING DWG 143T500. AIRCRAFT WAS GROUNDED.
STRINGER 34L HAS EXFOLIATION CORROSION BETWEEN FS 522 AND 544.0. REPLACED CORRODED SECTION OF STRINGER 34L IAW B767-200 SRM 53-00-03 FIG 201. AIRCRAFT WAS GROUNDED.
CORROSION FS 742 UPPER SIDE OF STRINGER 35L ON SKIN DOUBLER. REMOVED AND REPLACED TEAR STRAP PN 143T3222-11 IAW DWG 143T3220 & SRM 51-40-02. AIRCRAFT WAS GROUNDED.
FLOOR PANEL SUPPORT BRACKET ON WEB AT STA 522-544 RT BL 22 CORRODED. FABRICATED ANGLE PER SAMPLE AND INSTALLED THEM TO WEB PANEL IAW B767 SRM 51-04-02 AND BOEING DWG 143T5000. AIRCRAFT WAS GROUNDED.
FLOOR WEB ATTACH "Z" INTERCOSTAL CORRODED AT STA 610 RBL 22. REMOVED AND REPLACED INTERCOSTAL P/N 143T5000-36 IAW B767 SRM 51-40-02. AIRCRAFT WAS GROUNDED.
BOX BEAM PANEL STA 610-632 FLC HAS CORRODED L ANGLE AND SKIN PANEL. WEB AND L ANGLE FABRICATED IAW BOEING DWG 143T5000. AIRCRAFT WAS GROUNDED.
BOX BEAM PANEL STA 610-632 FLC HAS CORRODED L ANGLE AND SKIN PANEL. WEB AND L ANGLE FABRICATED IAW BOEING DWG 143T5000. AIRCRAFT WAS GROUNDED.
BOX BEAM UPPER CAP FITTING CORRODED BETWEEN STA. 522 AND 544 AT LBL 38. REMOVED AND REPLACED BOX BEAM UPPER CAP FITTING P/N 143T5000-18 BETWEEN STA 522 TO 544 AT LBL 38 IAW B767-200 SRM 51-40-02. AIRCRAFT WAS GROUNDED.
STA 566 BELLY TEAR STRAP HAS CORROSION. FABRICATED PER SAMPLE AND INSTALLED NEW TEAR STRAP P/N 143T3222-6 IAW B767 SRM 51-40-02 AND BOEING DWG 14332220. AIRCRAFT WAS GROUNDED.
LOWER FUSELAGE SKIN NEEDS REMOVED FROM BS 434 TO BS 786 DUE TO INTERNAL CORROSION. REMOVED AND RE-INSTALLED CENTER BELLY SKIN STA 434-785.9 S36L - 36R IAW BOEING DWG 143T3220 AND B767 SRM 51-40-02. AIRCRAFT WAS GROUNDED.
STA 544 TEAR STRAP HAS CORROSION. FABRICATED SAMPLE AND INSTALLED NEW TEAR STRAP P/N 143T3222-5 IAW B767 SRM 51-40-02 AND BOEING DWG 143T3220. AIRCRAFT WAS GROUNDED.
STA 610 TEAR STRAP HAS CORROSION. FABRICATED PER SAMPLE AND INSTALLED NEW TEAR STRAP P/N 143T3222-5 IAW B767 SRM 51-40-02 AND BOEING DWG 14332220. AIRCRAFT WAS GROUNDED.
TEAR STRAP AT STA 632 S-36L CORRODED. FABRICATED PER SAMPLE AND INSTALLED NEW TEAR STRAP P/N 143T3222-8 IAW B767 SRM 51-40-02 AND BOEING DWG 14332220. AIRCRAFT WAS GROUNDED.
FUSELAGE SKIN DOUBLER CORRODED. REMOVED FUSELAGE SKIN DOUBLER FABRICATED NEW AND INSTALLED IAW B767 SRM 51-40-02 AND DWG 143T3220, AWG.
CORROSION AT FS 742 UPPER SIDE OF STRINGER 34L ON TEAR STRAP. REMOVED TEAR STAP, FABRICATED AND INSTALLED NEW TEAR STRAP IAW B767 SRM 51-40-02 AND BOEING DWG, AWG.
CORROSION FS 742 UPPER SIDE OF STRINGER 36L ON SKIN DOUBLER. INSTALLED NEW TEAR STRAP IAW B767 SRM 51-40-02 AND BOEING DWG 143T32220. AIRCRAFT WAS GROUNDED.
TEAR STRAP AT FS 654 BETWEEN STRINGERS 35L AND 36L CORRODED. REMOVED, FABRICATED NEW, AND INSTALLED TEAR STRAP IAW B767 SRM 51-40-02 AND DWG 143T3220, ACFT WAS GROUNDED.
RT WING L/E EDGE RIB WS 433.1 INBD OF THE TAI DUCT IS CORRODED ON THE OUTBD SIDE. REPLACED RIB AT STA 433.1 IAW B767-200 SRM 51-40-02. REPLACED RIB AT STA 433.11. CORROSION REMOVED & REPLACED RIB AT STA 433.11.
STA 478 S36-37L TEAR STRAP HAS CORROSION. REMOVED, FABRICATED NEW AND INSTALLED TEAR STRAP IAW B767 SRM 51-40-02 AND DWG 143T3220. AIRCRAFT WAS GROUNDED.
STA 456 TEAR STRAP HAS CORROSION. REMOVED, FABRICATED NEW AND INSTALLED TEAR STRAP IAW B767 SRM51-40-02 AND DWG 143T3220. AIRCRAFT WAS GROUNDED.
INBOARD RIB, ADJACENT TO NR 5 SLAT OUTBOARD AUXILARY TRACK CORRODED AROUND NUT PLATE, AIRCRAFT GROUNDED. REMOVED & REPLACED RIB IAW REA B767-59641.
FUSELAGE SKIN CORRODED FS 620 UPPER SIDE OF STRINGER 36L. REPAIRED DAMAGED AREA OF SKIN P/N 143T3210 IAW ABX REA B653-59660-MR, ACFT WAS GROUNDED.
SKIN TEAR STRAP CORRODED. REPLACED TEAR STRAP IAW B767 SRM 51-40-02 AND DWG 143T3220.
TEAR STRAP AT STA 434 BETWEEN S-39L AND S-38L HAS CORROSION. FABRICATED NEW AND INSTALLED TEAR STRAP IAW B767 SRM51-40-02 AND DWG 143T3220. AIRCRAFT WAS GROUNDED.
STA 676 TEAR STRAP HAS CORROSION. FABRICATED PER SAMPLE AND INSTALLED NEW TEAR STRAP P/N 143T3222-1 IAW B767 SRM 51-40-02 AND BOEING DRAWING 143T3220. AIRCRAFT WAS GROUNDED.
STA 522 TEAR STRAP HAS CORROSION. SEE PARTIAL WORK ON BACK. REMOVED, FABRICATED NEW AND INSTALLED TEAR STRAP IAW B767 SRM51-40-02 AND DWG 143T3220. AIRCRAFT WAS GROUNDED.
TERMINAL BLOCK HEAVILY CORRODED AT STA 588-610 - S32L. REMOVED AND INSTALLED NEW GROUND BLOCK TO STRINGER IAW B767 SRM 51-40-02, ACFT WAS GROUNDED.
STA 500 TEAR STRAP HAS CORROSION. REMOVED, FABRICATED NEW AND INSTALLED TEAR STRAP IAW B767 SRM51-40-02 AND DWG 143T3220. AIRCRAFT WAS GROUNDED.
WEB ATTACHMENT FITTING TO STRINGER 38L IS CORRODED. INSTALLED NEW ATTACH ANGLE IAW B767 SRM 51-40-02. AIRCRAFT WAS GROUNDED.
STA 786 CTR DOUBLER TEAR STRAP HAS CORROSION. FABRICATED AND INSTALLED NEW CENTER TEAR STRAP, IAW B767 SRM 51-40-02, BOEING DWG 143T3220. AIRCRAFT WAS GROUNDED.
DRAIN MAST SUPPORT STRUCTURE BETWEEN STRINGERS 34L AND 35L & FS 632AND 654 CORRODED. REMOVED & REPLACED DRAIN MAST SUPPORT STRUCTURE IAW B767-200 SRM 51-40-02.
DRAIN MAST SUPPORT STRUCTURE BETWEEN STRINGERS 34L AND 35L & FS 632 AND 654 CORRODED. REMOVED & REPLACED DRAIN MAST SUPPORT STRUCTURE IAW B767-200 SRM 51-40-02, ACFT WAS GROUNDED.
DRAIN MAST SUPPORT STRUCTURE BETWEEN STRINGERS 34L AND 35L & FS 632 AND 654 CORRODED. REMOVED & REPLACED DRAIN MAST SUPPORT STRUCTURE IAW B767-200 SRM 51-40-02, ACFT WAS GROUNDED.
BELLY SKIN INT CORRODED FS 676-698, 36L. REPAIRED DAMAGE SKIN AREA AT STA 676 S36L LOWER SKIN P/N 143T3220 IAW B767-200 SRM 53-00-01 FIG 201 REPAIR 12. REPAIR IS A CAT B REPAIR SEE 53-00-01 FIG 201 REPAIR 12 TABLE III FOR REINSP REQUIREMENTS. AIRCRAFT WAS GROUNDED.
NR 1 PYLON PNL 437ELX LWR ATTACH FLANGE INSIDE PYLON STRUCTURE CHAFED THROUGH. REMOVED AND REPLACED ATTACH FLANGE IAW B767-200 SRM 51-40-02 & B. DWG #311T1380. #3 FITTING TO BE INSTALLED ON NR 0961.
STRINGER 35L CORRODED STA 578 TO 558. INSTALLED NEW SECTION OF STRINGER IAW B767 SRM 51-40-02 AND 53-00-03. AIRCRAFT WAS GROUNDED.
STRINGER 38L BETWEEN FS 720 AND 742 CORRODED. INSTALL NEW KEEL CHORD P/N 143T3223-1 IAW B767 SRM 51-40-02 BOEING DWG 143T3220 AND 140T0822. AIRCRAFT WAS GROUNDED.
CORROSION ON FLC FLOORBEAM WEB FS 720 LT. REPAIRED FLOORBEAM WEB IAW B767 SRM 53-00-07 REPAIR 3. AIRCRAFT WAS GROUNDED.
STRINGER 35L CORROSED AT STA 544. INSTALLED NEW SECTION OF STRINGER IAW B767 SRM 51-40-02 AND 53-00-03. AIRCRAFT WAS GROUNDED.
STRINGER 35L CORRODED STA 598 TO 578. INSTALLED NEW SECTION OF STRINGER IAW B767 SRM 51-40-02 AND 53-00-03. AIRCRAFT WAS GROUNDED.
STRINGER 35L CORRODED STA 598 TO 610. INSTALLED NEW SECTION OF STRINGER IAW B767 SRM 51-40-02 AND 53-00-03. AIRCRAFT WAS GROUNDED.
SHEAR TIE AT STA 610 S36-37R CORRODED. REPLACED SHEAR TIE AT STA 610 S36R-S37R IAW B767 SRM 51-40-02. AIRCRAFT WAS GROUNDED.
STRINGER 39L CORRODED AND DAMAGED FS 434-456. REPLACE STRINGER SECTION AT STA 434-456 STR 39 IAW B767 SRM 51-40-02. AIRCRAFT WAS GROUNDED.
STRINGER 39L BETWEEN STATION 500 TO STA 478 HAS CORROSION/CRACKS ON FWD END. FABRICATED NEW STRINGER PN 143T3001-72 IAW B767 SRM 53-30-03. RE-INSTALLED STRINGER IAW B767 SRM 51-40-02, 53-00-03 FIG 201 STA 456-632 S39L. AIRCRAFT WAS GROUNDED.
TOP FLANGE ON S-35L AT STA 434 IS CORRODED. REMOVED AND REPLACED STRINGER S-35L CHANNEL SPLICE IAW B767 SRM 51-40-02. AIRCRAFT WAS GROUNDED.
STRINGER 39L BETWEEN STA 500 AND STA 522 HAS HOLE IN THE AFT END. FABRICATED NEW STRINGER SECTION P/N 143T3001-72 IAW B767 SRM 53-30-03. INSTALLED STRINGER IAW B767 SRM 51-40-02, 53-00-03 FIG 201. REF BAC1498-202. AIRCRAFT WAS GROUNDED.
STA 434 S36L STRINGER SPLICE CHANNEL CORRODED AND BENT. REMOVED AND REPLACED S36 LEFT STRINGER SPLICE CHANNEL IAW B767 SRM 51-40-02. AIRCRAFT WAS GROUNDED.
STRINGER SPLICE AT FS 434, 39L CORRODED AND DAMAGED. REPLACE STRINGER SPLICE IAW B767 SRM 51-40-02. AIRCRAFT WAS GROUNDED.
STRINGER S39L CORRODED AT FS 777.0. SPLICED IN NEW SECTION OF STRINGER 39L AT STA 788 TO 752. IAW WITH B767-200 SRM 51-40-02. AIRCRAFT WAS GROUNDED.
S37L STA 478 TO 522 CORRODED. REMOVED & REPLACED CORRODED STRINGER 37L FROM STA 522 TO 478 IAW B767-200 SRM 53-00-03 FIG 201 REPAIR 2. AIRCRAFT WAS GROUNDED.
STRINGER 36 LEFT CORRODED BETWEEN STA. 522 TO 544. REPLACED 36L STRINGER FROM STA 522 TO 54 IAW B767 SRM 51-40-02. AIRCRAFT WAS GROUNDED.
STRINGER S-37L DAMAGED BETWEEN STA 522L AND STA 544L. REMOVED AND REPLACED DAMAGED SECTION OF STRINGER IAW B767-200 SRM 53-00-03 FIG 201 REPAIR 2. AIRCRAFT WAS GROUNDED.
STRINGER 36L FS 584 CORRODED. STRINGER AT STA 484, 36L REPLACED IAW B767 SRM 51-40-02, AND BOEING DWG 143T3220. AIRCRAFT WAS GROUNDED.
S37L CRACKED AT STA 464 AT PREVIOUS SPLICE/REPAIR. REMOVED AND REPLACED DAMAGED SECTION OF S37L FROM STA 434 TO 478 IAW B767-200 SRM 53-00-03 FIG 201 REPAIR 2, ACFT WAS GROUNDED.
FAIL SAFE STRAP AT STA 588, STRINGER 36L TO 36R HAS A HOLE IN IT FROM CORROSION. FABRICATED PER SAMPLE AND INSTALLED NEW TEAR STRAP P/N 143T3222-6 IAW B767 SRM 51-40-02 AND BOEING DWG 143T3220. AIRCRAFT WAS GROUNDED.
SHEAR TIE AT STA 500 BETWEEN S-33L AND S-32L IS CORRODED. INSTALLED NEW SHEAR TIE IAW B767 SRM 51-40-02 & BOEING DWG 140T2102. AIRCRAFT WAS GROUNDED.
S38L STA 786 PRESSURE CAP OUTBOARD SIDE IS CRACKED AND CORRODED. FABRICATED PER SAMPLE & BOEING DWG NEW PRESSURE CAP (SEAL PAN) PN 111T2031-7 IAW BOEING DWG 140T0100. MATERIAL IS 2024T-3 .050 PO 0002736. AIRCRAFT WAS GROUNDED.
SHEAR TIE AT STA 412 BETWEEN S-35L AND S-36L IS CORRODED. REPLACED SHEAR TIE PER BOEING DRAWING 140T2102 AND SRM 51-40-02. PN 140T2102-275. AIRCRAFT WAS GROUNDED.
STRINGER 35L CORRODED AND CRACKED BETWEEN FS 632 AND 654. REMOVED STRINGER AND SPLICED IN NEW SECTION AT S35L IAW B767 SRM 53-00-03 FIG 201 REPAIR 2, ACFT WAS GROUNDED.
FUSELAGE STRINGER 32L CORRODED BETWEEN STA 500 AND 478. SPLICED IN NEW SECTION OF S32L STA 460-575 IAW B767 SRM 51-40-02 AND 53-00-03 FIG 201. AIRCRAFT WAS GROUNDED.
FLOOR SUPPORT STA 544 TO 566 LBL 30 HAS CORRODED ANGLE AT NUT PLATE INSIDE OF CHANNEL. REMOVED AND REPLACED NUT PLATE ANGLE IAW B767 SRM 51-40-02. PRIMED AND PAINTED CHANNEL IAW B767 AMM 51-21-10. AIRCRAFT WAS GROUNDED.
FUSELAGE S33L AT STA 522 TO 544 HAS CORROSION AND CORRODED FASTENERS. REMOVED AND REPLACED STRINGER SECTION FROM STA 510 TO 522 IAW B767 SRM 53-00-03 DETAIL 3. AIRCRAFT WAS GROUNDED.
SHEAR TIE CORRODED BETWEEN S33L AND S34L. REPLACED SHEAR TIE PER BOEING DRAWING 140T2102 & SRM 51-40-02. AIRCRAFT WAS GROUNDED.
SHEAR TIE (2 EA) CORRODED AT STA 434 BETWEN S-36L AND S-37L. REPLACED SHEAR TIE (2 EA) PER BOEING DWG 140T2102 & SRM 51-40-02. AIRCRAFT WAS GROUNDED.
SHEAR TIE 610 S36-37L HAS MATERIAL MISSING. REPLACED SHEAR TIE PER BOEING DWG 140T2102 & SRM 51-40-02. AIRCRAFT WAS GROUNDED.
SHEAR TIE CORRODED. REPLACED SHEAR TIE PER BOEING DWG 140T2102 & SRM 51-40-02, A/W/G.
SHEAR TIE CORRODED. REMOVED AND REPLACED SHEAR TIE PER BOEING DWG 140T2102 & SRM 51-40-02, A/W/G.
FUSELAGE SHEAR TIE CORRODED. REMOVED AND REPLACED SHEAR TIE PER BOEING DWG 140T2102 & SRM 51-40-02, A/W/G.
DAMAGE ON AIRCRAFT RIGHT SIDE MAIN LANDING GEAR SUPPORT BEAM LOWER SIDE (AFT BEAM HALF MEASURE) 1.7"" LONG X .600"" WIDE X .060"" DEEP. BLENDED AREA IAW B767 SRM 57-51-14, IAW ABX REA B657-59650-MR. AIRCRAFT WAS GROUNDED.
DAMAGE ON AIRCRAFT LEFT SIDE MAIN LANDING GEAR SUPPORT BEAM (AFT BEAM HALF MEASURED) 1.700" LONG X .500" WIDE X .027" WIDE BLENDED AREA IAW B767 SRM 57-51-14, IAW ABX REA B657-59651-MR. AIRCRAFT WAS GROUNDED.
SHEAR TIE CORRODED AT STA 544 BETWEEN S-37L AND S-36L. REPLACED SHEAR TIE PER BOEING DWG 140T2102 & SRM 51-40-02. AIRCRAFT WAS GROUNDED.
SHEAR TIE CORRODED AT STA 676 BETWEEN S-37L AND S-38L. REPLACED SHEAR TIE PER BOEING DWG 140T2102 & SRM 51-40-02. AIRCRAFT WAS GROUNDED.
STA 434 S39R-39L SHEAR TIE CORRODED. REPLACED SHEAR TIE PER BOEING DWG 140T2102 & SRM 51-40-02. AIRCRAFT WAS GROUNDED.
SHEAR TIE AT STATION 478 LB LINE BETWEEN STRINGER 38-37 CORROSION FOUND. REPLACED SHEAR TIE PER BOEING DWG 140T2102 & SRM 51-40-02. AIRCRAFT WAS GROUNDED.
SHEAR TIE FROM STA 720 39L-38L HAS MISS DRILLED HOLE. REMOVED AND REPLACED SHEAR TIE PER BOEING DWG 140T2102 & SRM 51-40-02, ACFT WAS GROUNDED.
SHEAR TIE AT STA 566 BETWEEN S-39L AND S-39R IS CORRODED. REPLACED SHEAR TIE PER BOEING DWG 140T2102 & SRM 51-40-02. AIRCRAFT WAS GROUNDED.
SHEAR TIE AT STA 434 BETWEEN S-35L AND S-34L IS CORRODED. REPLACED SHEAR TIE PER BOEING DWG 140T2102 & SRM 51-40-02. AIRCRAFT WAS GROUNDED.
SHEAR TIE AT STA 500 BETWEEN S-39L AND S-38L IS CORRODED. REPLACED SHEAR TIE PER BOEING DWG 140T2102 & SRM 51-40-02. AIRCRAFT WAS GROUNDED.
SHEAR TIE CORRODED FS 566.0 BETWEEN S38L AND 39L. REPLACED SHEAR TIE PER BOEING DWG 140T2102 & SRM 51-40-02. AIRCRAFT WAS GROUNDED.
SHEAR TIE AT STA 434 BETWEEN S-39L AND S-38L HAS CORROSION. REPLACED SHEAR TIE PER BOEING DRAWING 140T2102 & SRM 51-40-02. AIRCRAFT WAS GROUNDED.
SHEAR TIE AT STATION 478 BETWEEN STRINGER 35-34 CORROSION FOUND. REPLACED SHEAR TIE PER BOEING DWG 140T2102 & SRM 51-40-02. AIRCRAFT WAS GROUNDED.
SHEAR TIE AT STATION 478 BETWEEN STRINGER 34-33 CORROSION FOUND. REPLACED SHEAR TIE PER BOEING DRAWING 140T2102 & SRM 51-40-02. AIRCRAFT WAS GROUNDED.
SHEAR TIE AT STA 742 BETWEEN S-39R IS CORRODED, MKD. REPLACED SHEAR TIE PER BOEING DWG 140T2102 & SRM 51-40-02. AIRCRAFT WAS GROUNDED.
STA 478 S35-36L SHEAR TIE CORRODED. REPLACED SHEAR TIE PER BOEING DRAWING 140T2102 & SRM 51-40-02. AIRCRAFT WAS GROUNDED.
STA 456 S35 - 36L SHEAR TIE CORRODED. REPLACED SHEAR TIE PER BOEING DWG 140T2102 & SRM 51-40-02. AIRCRAFT WAS GROUNDED.
SHEAR TIE CORRODED FS 544.0 BETWEEN STRINGERS 33 AND 34. REPLACED SHEAR TIE PER BOEING DRAWING 140T2102 & SRM 51-40-02. AIRCRAFT WAS GROUNDED.
SHEAR TIE CORRODED FS 544 BETWEEN STRINGERS 34 AND 35. REPLACED SHEAR TIE PER BOEING DWG 140T2102 & SRM 51-40-02. AIRCRAFT WAS GROUNDED.
STA 434 S38-39L SHEAR TIE CORRODED. REPLACED SHEAR TIE PER BOEING DWG 140T2102 & SRM 51-40-02. AIRCRAFT WAS GROUNDED.
TOOLING MARKS ON TEAR STRAP FROM STATION 764 ALSO HAS COROSION ON BOTTOM END. FABRICATED PER SAMPLE AND INSTALLED NEW TEAR STRAP P/N 143T3222-12 IAW B767 SRM 51-40-02 AND BOEING DWG 14332220. AIRCRAFT WAS GROUNDED.
DAMAGE ON AIRCRAFT RIGHT SIDE MAIN LANDING GEAR SUPPORT BEAM LOWER SIDE (FORWARD BEAM HALF MEASURE) 2.700" LONG X .800" WIDE X .087"DEEP, BLENDED AREA IAW B767 SRM 57-51-14, AND ABX REA B657-59650-MR, ACFT WAS GROUNDED.
DAMAGE ON AIRCRAFT LEFT SIDE MAIN LANDING GEAR SUPPORT BEAM (FORWARD BEAM HALF MEASURED) 2.200" LONG X 1.100" WIDE X .098" DEEP. BLENDED AREA IAW B767 SRM 57-51-14, AND ABX REA B657-59651-MR, ACFT WAS GROUNDED.
STR 38 CORRODED AT STA 440 AND CRACKED AT FWD END STA 434. REPLACED SECTION OF STR 38R P/N 143T3001 BY SPLICING NEW SECTION OF P/N 143T3001 FROM STA 434 TO STA 464 USING PN BAC1498-203 REPAIR MATERIAL IAW BOEING B767-200 SRM 53-00-03 & BOEING DWG 143T3220. AIRCRAFT WAS GROUNDED.
TEAR STRAP FS 632 BETWEEN STRINGERS 34L AND 35L CORRODED. REMOVED AND REPLACED TEAR STRAP PER BOEING DRAWING 143T3222 & SRM 51-40-02, ACFT WAS GROUNDED.
STRINGER 37R BETWEEN STA 500 AND STA 522 HAS HOLE IN THE AFT END. REPAIRED DAMAGE AREA OF STRINGER IAW B767 SRM 53-00-03 FIG 101. AIRCRAFT WAS GROUNDED.
SHEAR TIE BETWEEN STRINGERS CORRODED. REMOVED SHEAR TIE. FABRICATED NEW SHEAR TIE IAW BDWG 140T2102 MATERIAL ID 7075-T6 .050 PO#0001081. INSTALLED NEW FABRICATED SHEAR TIE IAW B767 SRM 51-40-02.
SHEAR TIE AT FS 632 BETWEEN STRINGERS 35L AND 36L CORRODED. REMOVED SHEAR TIE AT FS 632 BETWEEN STRINGERS 35L AND 36L. INSTALLED NEW FABRICATED SHEAR TIE IAW B767 SRM 51-40-02, ACFT WAS GROUNDED.
SHEAR TIE FS 610 BETWEEN STRINGERS 38L AND 39L CORRODED. REMOVED AND INSTALLED NEW SHEAR TIE IAW B767 SRM 51-40-02 & BOEING DWG 140T2102, ACFT WAS GROUNDED.
SHEAR TIE FS 610 BETWEEN STRINGERS 37L AND 38L CORRODED. FABRICATED AND INSTALLED NEW SHEAR TIE IAW B767 SRM 51-40-02 & BOEING DWG 140T2102, ACFT WAS GROUNDED.
SHEAR TIE BETWEEN STRINGERS 36L AND 37L AT FS 610 CORRODED. REMOVED AND INSTALLED NEW SHEAR TIE IAW B767 SRM 51-40-02 & BOEING DWG 140T2102, ACFT WAS GROUNDED.
SHEAR TIE CORRODED FS 676. FABRICATED AND INSTALLED NEW SHEAR TIE IAW SRM 51-40-02 AND DWG, AWG.
SHEAR TIE FS 610 BETWEEN STRINGERS 35L AND 36L CORRODED. REMOVED AND INSTALLED NEW SHEAR TIE IAW B767 SRM 51-40-02 & BOEING DWG 140T2102, ACFT WAS GROUNDED.
STRINGER 39R BETWEEN STA 500 AND STA 522 HAS HOLE IN THE AFT END. REPAIRED DAMAGE AREA OF STRINGER IAW B767 SRM 53-00-03 FIG 101. AIRCRAFT WAS GROUNDED.
SHEAR TIE CORRODED FS 522.0 BETWEEN STRINGERS 33 AND 39. REPLACED SHEAR TIE PER BOEING DRAWING 140T2102 & SRM 51-40-02. AIRCRAFT WAS GROUNDED.
TEAR STRAP AT STA 588 S-36L CORRODED. REMOVED TEAR STRAP AT STA 588 S36L TO S26L. FABRICATED NEW TEAR STRAP PER SAMPLE AND B767 SRM 53-30-01 FIG 1 AND BOEING DWG 143T3212. INSTALLED NEW FABRICATED TEAR STRAP IW B767 SRM 51-40-02. AIRCRAFT WAS GROUNDED.
SHEAR TIE CORRODED FS 522.0 BETWEEN STRINGERS 36 AND 37. REPLACED SHEAR TIE PER BOEING DRAWING 140T2102 & SRM 51-40-02. AIRCRAFT WAS GROUNDED.
SHEER TIE CORRODED FS 478.0. BETWEEN STRINGERS 36 AND 37. REPLACED SHEAR TIE PER BOEING DRAWING 140T2102 & SRM 51-40-02. AIRCRAFT WAS GROUNDED.
SHEAR TIE FS 545 BETWEEN STRINGERS 35L AND 36L CORRODED. REPLACED SHEAR TIE PER SRM 51-40-02 & BOEING DRAWING 140T2102. AIRCRAFT WAS GROUNDED.
SHEAR TIE FS 566 BETWEEN STRINGERS 37L AND 38L CORRODED. REPLACED SHEAR TIE PER SRM 51-40-02 & BOEING DRAWING 140T2102. AIRCRAFT WAS GROUNDED.
SHEAR TIE FS 566 BETWEEN STRINGERS 35L AND 36L CORRODED. REPLACED SHEAR TIE PER SRM 51-40-02 & BOEING DRAWING 140T2102. AIRCRAFT WAS GROUNDED.
SHEAR TIE FS 588 BETWEEN STRINGERS 35L AND 36L CORRODED. REMOVED AND REPLACED SHEAR TIE PER BOEING DRAWING 140T2102& SRM 51-40-02, ACFT WAS GROUNDED.
SHEAR TIE FS 632 BETWEEN STRINGERS 37L AND 38L CORRODED. REMOVED AND REPLACED SHEAR TIE PER BOEING DRAWING 140T2102 & SRM 51-40-02, ACFT WAS GROUNDED.
SHEAR TIE FS 632 BETWEEN STRINGERS 36L AND 37L CORRODED. REMOVED AND REPLACED SHEAR TIE PER BOEING DRAWING 140T2102 & SRM 51-40-02, ACFT WAS GROUNDED.
SHEAR TIE FS 632 BETWEEN STRINGERS 34L AND 35L CORRODED. REPLACED SHEAR TIE PER BOEING DRAWING 140T2102 & SRM 51-40-02, ACFT WAS GROUNDED.
CORROSION ON SHEAR TIE AT FS 720 BETWEEN STRINGERS 36L AND 37L. REPLACED SHEAR TIE PER BOEING DRAWING 140T2102 & SRM 51-40-02. AIRCRAFT WAS GROUNDED.
CORROSION FS 742 ON SHEAR TIE BETWEEN STRINGERS 36L AND 37L. REPLACED SHEAR TIE PER BOEING DRAWING 140T2102 & SRM 51-40-02. AIRCRAFT WAS GROUNDED.
SHEAR TIE CORRODED FS 500.0 BETWEEN STRINGERS 36. REPLACED SHEAR TIE PER BOEING DRAWING 140T2102 & SRM 51-40-02. AIRCRAFT WAS GROUNDED.
CORROSION ON SHEAR TIE. REPLACED SHEAR TIE PER BOEING DRAWING 140T2102 & SRM 51-40-0, A/W/G.
"SHEAR TIE FS 588 BETWEEN STRINGERS 37L AND 38L CORRODED. REPLACED SHEAR TIE PER SRM 51-40-02 & BOEING DRAWING 140T2102 & SRM 51-40-02. AIRCRAFT WAS GROUNDED.
"SHEAR TIE FS 588 BETWEEN STRINGERS 36L AND 37L CORRODED. REPLACED SHEAR TIE PER BOEING DRAWING 140T2102 & SRM 51-40-02. AIRCRAFT WAS GROUNDED.
TEAR STRAP AT STA 434 BETWEEN S-35L AND S-34L IS CORRODED. REMOVED AND REPLACED CORRODED TEAR STRAP IAW B767-200 SRM 51-40-02 AND BOEING DWG 140T0110. AIRCRAFT WAS GROUNDED.
STRINGER S11L IS CRACKED JUST AFT OF STA 676. REPAIRED STRINGER S11L AT STATION 676 IAW REA B653-59623-MR, AIRCRAFT WAS GROUNDED.
FAILSAFE CORD CORRODED AT FS 120.0 BETWEEN S37L AND S39L. BLENDED CORD. REMOVED TOTAL OF .003" FOUND TO BE WITHIN LIMITS IAW B767 SRM 53-00-07, ACFT WAS GROUNDED.
SHEAR TIE CORRODED FS 456.0 BETWEEN S38L AND S39L. REMOVED CORROSION ON SHEAR TIE AND TREATED PER SRM 53-00-07. AIRCRAFT WAS GROUNDED.
CORROSION ON SHEAR TIE FS 742 BETWEEN STRINGERS 34L AND 35L. REPLACED SHEAR TIE PER BOEING DRAWING 140T2102 & SRM 51-40-02. AIRCRAFT WAS GROUNDED.
CORROSION ON SHEAR TIE BETWEEN STRINGERS 35L AND 36L FS 742. REPLACED SHEAR TIE PER BOEING DRAWING 140T2102 & SRM 51-40-02. AIRCRAFT WAS GROUNDED.
EICAS MESSAGE "GEAR DISAGREE" & "DOOR MSG", MLG DOOR LIGHT ILLUMINATED. CYCLED GEAR, NO HELP. WHEN GEAR HANDLE IN DOWN POSITION MESSAGE EXTINGUISHES & GEAR IN NORMAL CONFIGURATION. CREW DECLARED EMERGENCY AS PRECAUTION. ACFT GROUNDED. BITE CHECK OF PSEU FAULTED S262 R SIDE BRACE DOWN TARGET. INSPECTED MLG, ACTUATORS & SYSTEM HYD LINES, NO PROBLEMS FOUND. SWUNG MLG & FOUND RT MLG FAILED TO RETRACT. FOUND HYD FUSE NOT ALLOWING FLUID TO SIDE BRACE ACTUATOR. VERIFIED BAD BY SWAPPING TO LT SIDE. AFTER SEVERAL CYCLES OF MLG, PROBLEM FOLLOWED. REMOVED AND REPLACED LT MLG FUSE IAW 32-32-19. OPS CHECKED NORMAL.
LAV WON'T FLUSH. FOUND DAMAGED LAVATORY WASTE WIRING. CAP & STOW WIRING. DEFERRED LAV SYSTTEM PER MEL 38-30-1A. (BURNT WIRING BUNDLE)
EVIDENCE OF LIGHTNING DISCHARGE ON LOWER AFT FUSELAGE AT STA 1373 LEFT SIDE. CUT OUT DAMAGED ITEM NR 4 REPAIRED IAW B767 SRM 53-00-01 FIG 201.
CRACK IN LOWER SECTION OF S10L AFT OF STA 676. REPLACED CRACKED SECTION OF S10L IAW REA B653-59011-MR
STRINGER 34L STA 434-466 REMOVED DUE TO CORROSION. REPLACED STRINGER WITH P/N BAC1498-207 IAW B767 SRM 51-40-02. REPAIRED IAW B767 SRM 53-00-03 FIG 201 REPAIR 2.
STRINGER 33L STA 434-466 REMOVED DUE TO CORROSION. REPLACED STRINGER SECTION WITH P/N BAC1497-207 IAW B767 SRM 51-40-02. REPAIRED IAW B767 SRM 53-00-03 REPAIR 2 FIG 201.
STRINGER 32 L STA 434-466 REMOVED DUE TO CORROSION. REPLACED STRINGER SECTION WITH P/N BAC 1498-207. REPAIRED IAW B767 SRM 53-00-03. REPAIR NR 2 FIG 201 AND B767 SRM 51-40-02.
THE RIGHT WING UPPER SURFACE IS EXFOLIATED, PLUS A LARGE AREA OF BUBBLED PAINT ABOVE WING REAR SPAR AT WS 798. BLENDED AREA IAW B767 SRM 57-10-2. REWORKED AREA ON REA B657-58785MR.
BULK CARGO LOWER DOOR JAMB FWD I/B CORNER AT WEB HAS SPOT OF CORROSION ON UPPER SURFACE AND EVIDENCE OF CORROSION ON LOWER SIDE BETWEEN DOUBLER AND ANGLE. REPAIRED CORRODED AREA OF BULK CARGO DOOR LOWER DOOR JAM IAW B767 SRM 51-7-13. CORROSION 2.6 L X 1.2 W INCHES.
FLOOR SUPPORT CRACKED IN 2 PLACES STA 1434 AND 1442 LBL 22 IN BULK CARGO COMPARTMENT. SPLICED IN NEW SECTION OF FLOOR SUPPORT.
THE RT NWW CHORD AT RBL 25 IS CRACKED LOCATED 11.5 INCHES BELOW THE UPPER PRESSURE PANEL. REPAIRED CRACKED CHORD IAW B767 SRM 51-70-12 FIG 1.
THE LT NWW CHORD AT LBL 25, IS CRACKED LOCATED 11.5 INCHES BELOW THE UPPER PRESSURE PANEL. REPAIRED THE LT NWW CHORD AT LBL 25.
RT FUSELAGE SKIN HAS A 2.5 INCH CRACK AROUND STA 666 JUST ABOVE S33R. CRACK VERIFIED IAW BOEING 767 NDT MANUAL PART 6 CHAP 51-00-11 PAGE 2-3. REPAIRED DAMAGED AREA IAW 767 SRM 53-00-01 FIG 201.
RUDDER TRIM FAILED TO TRIM IN RT DIRECTION.
AFT MAIN CARGO COMPT FILLS WITH ACRID MIST UPON T/O & LANDING. FOUND HYDRAULIC LINE TO SLAT LEAKING ONTO RT PACK CAUSING SMELL. REPAIRED LINE. REPLACED LEAKING HYDRAULIC LINE AT LOWER FWD CARGO COMPT BULKHEAD AND RT WING ROOT OPERATED FLAPS & SLATS AS PER B767 AMM 20-11-00 & 27-81-00 & 29-00-00, NO LEAKS NOTED.
CAUSTIC FUMES IN THE AIRCRAFT AFTER LANDING AND LEFT DOOR OPEN. CHECKED ENGINE FOR EVIDENCE OF OIL CONTAMINATION, NONE FOUND. RAN PACKS AND AILERON SYSTEM FOR 3 HOURS, NO CAUSTIC ODORS NOTED. CHECKED LOWER CARGO COMPTS, E/E AND FWD E/E, CHECKED FOR FUMES WITH GEAR UP HANDLE IN UP POSITION, CHECKED EXHAUST FANS, NO LEAKS OR CAUSTIC ODORS NOTED IN AIRCRAFT. ACCOMPLISHED CLEANING OF AIRCRAFT INTERIOR. THERE HAVE BEEN NO FURTHER REPORTS OF ODORS REPORTED.
AFTER T/O, LOADMASTER REPORTED UNUSUAL SMELL IN THE CARGO AREA. RETURNED FOR LANDING. FIRE DEPT TESTED AIR AND FOUND OK. LOADMASTER INSPECTED THE FREIGHT AND FOUND NO DAMAGE. UPPER CARGO COMPARTMENT IS CLEAR AT THIS TIME. NO FREIGHT WAS IN BELLY.
UPPER LONGERON ABOVE HORIZONTAL BOX WEB CRACKED AND DAMAGED STA 1734 LT SIDE. REPAIRED IAW REA B653-57691. (S)
L1 DOOR LOWER AFT CORNER HAD CRACK STARTING FROM FASTENER HOLE, CRACK WAS .125 INCHES LONG. REPAIRED L1 DOOR LOWER AFT CORNER, IAW B767 SRM. (S)
FOUND CRACK AT NR 3 SLAT OUTBOARD TRACK CUTOUT ON LEADING EDGE OF LT WING. REPAIRED SPLICE PLATE IAW REA B65757685. (S)
LEFT STA 1654.5 SEVERAL FUSELAGE SKIN CRACKS STRINGERS 3-6. REPAIRED SKIN CRACKS AT STRINGERS 3-6 IAW B767 SRM. (S)
RT STA 1654 SEVERAL FUSELAGE SKIN CRACKS, STRINGERS 3-5. REPAIRED FUSELAGE SKIN IAW B767 SRM 53-80-01. (S)
LT STA 1654.5, 2 EACH SKIN CRACKS STRINGER 13 LT. REPAIRED LT STA 1654.5 AT STRINGER 13 LT ON REA B653-57700. (S)
STA: ILN, ON CREW PREFLIGHT, SMOKE DETECTED IN COCKPIT. ALSO EICAS SCREEN AND LEFT FMC BLANK. REMOVED UPPER EICAS DISPLAY UNIT AND LEFT FMC DISPLAY UNIT. INSPECTED WIRING AND CONNECTORS, NO DEFECTS NOTED. REMOVED AND REPLACED EICAS DISPLAY UNIT AND LEFT FMC. BOTH UNITS CHECK GOOD IAW B767 MM. LEFT FMC REMOVED: P/N: 4038170-905, S/N: 84040157, TSSV: 1001, CSSV: 243.
EMERGENCY EGRESS HANDLE WAS MISSING FROM THE L2 WINDOW. INSTALLED EMERGENCY EGRESS HANDLE AS REQUIRED IAW B767 AMM 56-11-04. CHECKED GOOD.
RIGHT WING SLAT ANTI-ICE DUCT PANEL MISSING. REPLACED RIGHT WING ANTI-ICE DUCT SEAL DOOR IAW BOEING S/B 767-57-0045 AND AMM 57-41-58.
LEFT OUTBOARD AILERON SKIN PEELED BACK/DELAMINATED. REPLACED LEFT OUTBOARD AILERON IAW B767 AMM 27-11-02-4.
ATTACH ANGLE AT LONGERON 3 RIGHT, STA 1654.5 WAS CRACKED. REMOVED AND REPLACED BRACKET IAW B767 SRM 51-40-02.
ATTACH ANGLE AT LONGERON 3 LEFT, STA 1654.5 WAS CRACKED. REMOVED AND REPLACED BRACKET IAW B767 SRM 51-40-02.
ATTACH ANGLE LONGERON 312 AT STA 1678 WAS CRACKED. REMOVED AND REPLACED ATTACH ANGLE BRACKET LONGERON 3 RIGHT, STA 1678 IAW B767 SRM 51-40-02.
ATTACH ANGLE AT LONGERON 312, STA 1702 WAS CRACKED. REMOVED AND REPLACED ATTACH ANGLE IAW B767 SRM 51-40-02.
INTERNAL SKIN CRACKED AT FS 1734 AND STRINGER 18 RIGHT. REMOVED AND REPLACED SKIN AT FS 1734 IAW REA B653-53996 AND DWG 148T7320.