N747AX
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
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
77 reports on file, 2006-11-28 – 2014-05-27.
Part: DOOR FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,828 hrs · 34,173 cycles
FORWARD LOWER CARGO FUSELAGE STATION 549 INSIDE LOWER SEAL, FWD PART OF DOOR JAMB IS CORRODED. NEW OUTER CHORD PN 143T8004-1, INSTALLED ON NR 1071. SDR INFO CORRODED L2, PN 143T8004-1, SN NSN, PART NAME CHORD, FS & BS LOCATION ON ACFT 549 TO 593, STRINGER & WS LOCATION ON ACFT 33R. ACFT WAS GNDED.
Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,828 hrs · 34,173 cycles
FORWARD LOWER CARGO FUSELAGE STATION 544 AT FWD CORNER OF DOOR JAMB. UNDER THE THRESHOLD ARE TWO SPOTS OF CORROSION. REPLACE CORRODED ANGLE WITH A NEW PART PN 143T4003-3, INSTALL IAW SRM 51-40-02. CORRODED L2, PN 143T5003-3, SN NSN, PART NAME ANGLE, FS & BS LOCATION ACFT FS 544, STRINGER & WS LOCATION ON ACFT RBL 48. ACFT WAS GNDED.
Part: STRINGER — CRACKED (FUSELAGE) · airframe 72,828 hrs · 34,173 cycles
NEW STRINGER 24L PN 146T3002-55 NEEDS INSTALLED FROM FS 1307 - 1417. OLD STRINGER WAS REMOVED ON WORK ORDER 600324529 NR 0511. REMOVED STRINGER 24L AT FS 1307 - 1417. FABRICATED NEW STRINGER IAW REA 653-61024- MR. INSTALLED NEW STRINGER 24L AT FS 1307 - 1417 IAW SRM 51-40-02 PARA 7 D & PARA 4 B REA B653-61024-MR. SDR INFO CRACKED 17 INCHES PN 146T3002-55, SN NSN, PART NAME STRINGER, FS & BS LOCATION ON ACFT FS 1307 TO 1417, STRINGER LOCATION ON ACFT STRINGER 24L, PART NAME STRINGER, FS & BS LOCATION ON ACFT 1307 TO 1417, STRINGER & WS LOCATION ON ACFT 24L. ACFT WAS GNDED.
Part: STRINGER — CRACKED (FUSELAGE) · airframe 72,828 hrs · 34,173 cycles
NEW STRINGER 26L PN 146T3002-57 NEEDS INSTALLED FROM FS 1307 - 1417. THE OLD STRINGER WAS REMOVED ON WORK ORDER 600324529 NON-ROUTINE 0510. FABRICATED NEW STRINGER 26L IAW REA B653-61024-MR. R & R STRINGER 26L AT FS 1307 - 1417 IAW B767 SRM 51-40-02 PARA 7 D & PARA 4. CRACKED 42 INCHES PN 146T3002-51, SN NSN, PART NAME STRINGER, FS & BS LOCATION ON ACFT FS 1307 TO FS 1417, STRINGER & WS LOCATION ON ACFT STRINGER 26L. ACFT WAS GNDED.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,828 hrs · 34,173 cycles
AFT LOWER CARGO RT SIDE ABOVE STRINGER 35R BETWEEN STATION 1285 & 1307 UNDERNEATH THE PDU, THE FLOOR & SUPPORT IS CORRODED. R & R INTERCOSTAL ABOVE STRINGER 35R BETWEEN STATION 1285 & 1307 IAW 51-40-02 SRM. CORRODED L2, PN 146T5000-146, SN NSN, PART NAME: SUPPORT CARGO CONTAINER, FS & BS LOCATION ACFT 1285 TO 1307 STRINGER & WS LOCATION ON ACFT STRINGER 35R. ACFT WAS GNDED.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,828 hrs · 34,173 cycles
AFT LOWER CARGO CTR BILGE AREA RT STATION 1263 AT STRINGER 35R AREA THERE IS CORROSION AT THE FLOORBEAM UPPER CHORD NUTPLATES. R & R UPPER CHORD IAW 51-40-02. CORRODED LEVEL 2, PN 146T1209-5146T5000-15 & 16, PART NAME INNER CHORD & SUPPORT, CARGO CONTAINER ABOVE 35L & 36L AT STATION 1263, SN NSN, FS & BS LOCATION STATION 1263 TO 1285, STRINGER & WS LOCATION STRINGER 34L TO 34R. ACFT WAS GNDED.
Part: STIFFENER — CRACKED (FUSELAGE) · airframe 72,828 hrs · 34,173 cycles
VERTICAL STIFFENER ON FRAME AT FS 1480 ABOVE STRINGER 38R CRACKED AT UPPER ATTACHING HOLE. REMOVED DAMAGED STIFFENER AT STATION 1480 STRINGER 38R & INSTALLED NEW STIFFENER AT SAME LOCATION PN 146T1261-4 IAW SRM 51-40-02, SN N/A, PART NAME STIFFENER, CRACKED .400, FS & BS LOCATION ON ACFT 1480 TO 1480, STRINGER & WS LOCATION ON ACFT 38R TO 38R. ACFT WAS GNDED.
Part: STIFFENER — CRACKED (FUSELAGE) · airframe 72,828 hrs · 34,173 cycles
FRAME VERTICAL STIFFENER AT FS 1480 ABOVE STRINGER 38L CRACKED AT UPPER HOLE. REMOVED DAMAGED STIFFENER AT STATION 1480 STRINGER 38L & INSTALLED NEW STIFFENER AT SAME LOCATION. PN 146T1261-3 IAW SRM 51-40-02 SN NA, PART NAME STIFFENER, CRACKED .340, FS & BS LOCATION ON ACFT 1480 TO 1480, EXACT STRINGER & WS LOCATION ON ACFT 38L TO 38L. ACFT WAS GNDED.
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,828 hrs · 34,173 cycles
BULK CARGO, CORROSION AT STRINGER 35L BETWEEN STATION 1480 & 1502. REMOVED DAMAGED SECTION OF STRINGER 35L FROM STATION 1447 - 1526 & INSTALLED STRINGER REPAIR IN SAME LOCATION IAW SRM 53-00-03 FIG 201 REPAIR 2. PN 146T3003, SN NSN, PART NAME STRINGER, CORRODED, EXACT FS & BS LOCATION ON ACFT 1447 TO 1526, EXACT STRINGER & WS LOCATION ON ACFT STRINGER 35L TO STRINGER 35L. ACFT WAS GNDED.
Part: SKIN — DENTED (FUSELAGE) · airframe 72,828 hrs · 34,173 cycles
FUSELAGE EXTERNAL SKIN BETWEEN BS 610 - BS 620, STRINGER 31R - STRINGER 32R HAS SEVERAL DENTS BETWEEN DOOR CUT OUT & EXTERNAL REPAIR DOUBLERS NOT RECORDED ON ACFT OPEN DENT REPORT. REPAIR DENT IN FUSELAGE SKIN AT BS 610 - 620, STRINGER 31R - STRINGER 32R IAW B653- 0984-MR. PN 143T3520-5, PART NAME SKIN, SN NSN, EXACT FS & BS LOCATION ON ACFT 610 TO 620, EXACT STRINGER & WS LOCATION ON ACFT STRINGER 31R TO STRINGER 32R. ACFT WAS GNDED.
Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,828 hrs · 34,173 cycles
SECTION 43 AT DRAIN CHANNEL BEAM STATION 676 HAS SEVERAL AREAS OF CORROSION. REMOVED CORRODED DRAIN CHANNEL, FIVE EACH AT STATION 676. FABRICATED NEW CHANNEL IAW REA B563-60987 & B563-60967. INSTALLED NEW DRAIN CHANNEL IAW SRM 51-40-02. PN 368-53-33-90988-203, 205, 207, 209, PART NAME DRAIN CHANNEL, CORRODED. FS & BS LOCATION ON ACFT 680 FLOOR, EXACT STRINGER & WS LOCATION RBL 33 TO LBL 76. ACFT WAS GNDED.
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,828 hrs · 34,173 cycles
BULK CARGO, CORROSION AT STRINGER 35L BETWEEN STATION 1480 & 1461. REMOVED DAMAGED SECTION AT STRINGER 35L FROM STATION 1447 - 1526 & ATTACHING STRUCTURE. INSTALLED STRINGER REPAIR IN AREA OF DAMAGE & REINSTALLED ATTACHING STRUCTURE IAW SRM 53-00-03 FIG 201 REPAIR 2. PN 146T3003-20, SN NSN, PART NAME STRINGER, CORRODED, EXACT FS & BS LOCATION ON ACFT 1447 TO 1526, EXACT STRINGER & WS LOCATION ON ACFT STRINGER 35L TO STRINGER 35L. ACFT WAS GNDED.
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,828 hrs · 34,173 cycles
FORWARD LOWER CARGO BETWEEN FUSELAGE STATIONS 478 & 500, STRINGER 36R IS CRACKED & CORRODED. R & R 536R AT STATION 487 TO 509 IAW SRM 51-40-02 & REA B653-60965 MR. CRACKED & CORRODED. PN 143T3001-70, PART NAME STRINGER, FS & BS LOCATION FROM 488 TP 517, STRINGER & WS LOCATION FROM 36R. ACFT WAS GNDED.
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,828 hrs · 34,173 cycles
STRINGER U17C HAS CORROSION TOP & BOTTOM LEGS. INSTALLED NEW SECTION OF STRINGER & SPLICE IAW B767-200 & 57-00-03 REPAIR 2, FIG 201. CORRODED L2, PN 111T3007, SN NSN, PART NAME U17 CTR WING UPPER STRINGER. FS & BS LOCATION ON AC FS 859, STRINGER & WS LOCATION ON ACFT BL 60 TO BL 97. ACFT WAS GNDED.
Part: BULKHEAD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,828 hrs · 34,173 cycles
STATION 852 LT CORROSION ON A PREVIOUS REPAIR ON CANTED PRESS BULKHEAD. REPAIRED ON REA B653-60976-MR. CORRODED L2, PN 111T3012 & 1111T3013, NO SERIAL NR, PART NAME CTR TANK, UPPER SKINS, FS & BS LOCATION ON ACFT FS 859, LBL 60 - 97. ACFT WAS GNDED.
Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,828 hrs · 34,173 cycles
LEFT HAND ABOVE CTR TANK FS 859 LBL 97 STUB BEAM FITTING CORRODED AT ATTACH FASTENERS COMMON TO CTR TANK. REPAIRED STUB BEAM ON REA B653-60969-MR. CORRODED L2, PN 145T1903-5, SN NSN, PART NAME STUB BEAM FITTING, FS & BS LOCATION ON ACFT FS 858 TO 860, STRINGER & WS LOCATION ON ACFT STRINGER 22L TO 23L, LBL 74 - 97. ACFT WAS GNDED.
Part: BULKHEAD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,828 hrs · 34,173 cycles
STATION 889 LT CORROSION ON CANTED PRESS BULKHEAD UNDER BEAM. REPAIRED ON REA B653-60977-MR. CORRODED L2, PN 111T3013-1, SN NSN, PART NAME UPPER CTR WING SKIN, FS & BS LOCATION ON ACFT FS 878 TO 889. ACFT WAS GNDED.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,828 hrs · 34,173 cycles
AFT LOWER CARGO CTR BILGE AREA, THE INTERCOSTAL ABOVE STRINGER 36R BETWEEN 1263 & 1285 IS CORRODED. R & R INTERCOSTAL ABOVE STRINGER 36R BETWEEN STATION 1263 - 1285 IAW SRM 51-40-02. CORRODED L2, PN 146T5000-8, SN NSN, PART NAME SUPPORT, FS & BS LOCATION ON ACFT STATION 1263 TO STATION 1285, STRINGER & WS LOCATION ON ACFT STRINGER 36R. ACFT WAS GNDED.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,828 hrs · 34,173 cycles
CENTER BILGE RT SIDE OTBD INTERCOSTAL CORRODED ABOVE STRINGER 35R AREA. R & R INTERCOSTAL IN CTR BILGE ABOVE STRINGER 35R IAW SRM 51-40-02. CORRODED L2, PN 146T5000-195, SN NSN, PART NAME SUPPORT, CARGO CONTAINER. FS & BS LOCATION ON ACFT STATION 1263 TO STATION 1285. STRINGER & WS LOCATION ON ACFT STRINGER 35R. ACFT WAS GNDED.
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,828 hrs · 34,173 cycles
AFT LOWER CARGO CTR BILGE AREA, STRINGER 36R BETWEEN STATION 1263 & 1285 IS CORRODED. REMOVED DAMAGED STRINGER 36R & INSTALLED NEW REPAIR IAW SRM 53-00-03, REPAIR 2 NR 39 351070. CORRODED L2, PN 146T3003, SN NSN, PART NAME STRINGER, FS & BS LOCATION ON ACFT STATION 1253 TO STATION 1302, STRINGER & WS LOCATION ON ACFT 36R. ACFT WAS GNDED.
Part: STRINGER — CRACKED (FUSELAGE) · airframe 72,828 hrs · 34,173 cycles
STRINGER 26L BETWEEN STATION 1329 & 1353 IS CRACKED AT BOTH STRINGER TIES. NEW STRINGER WILL BE INSTALLED ON NR-0001 WORK ORDER 48362. CRACKED 24 INCHES, PN 146T3002-57, SN NA, PART NAME STRINGER, FS & BS LOCATION ON ACFT FS 1329 TO FS 1353, STRINGERS & WS LOCATION ON ACFT STRINGER 26L. ACFT WAS GNDED.
Part: BEAM — CORRODED (LT WING) · corrosion level 2 · airframe 72,828 hrs · 34,173 cycles
LEFT WING INBD TE PANEL UPPER BEAM CAP IS CRACKED & CORRODED AT WS 280 JUST INBD OF LT MLG. REMOVED UPPER SKIN PANELS, REMOVED LT WING INBD TE UPPER BEAM CAP & REPLACED UPPER BEAM CAP IAW SRM 51-40-02 PARA 4 B & PARA 7D, REINSTALLED UPPER SKIN PANELS IAW SRM 51-40-02. SDR INFO CORRODED L2, PN 113T1623-157, SN NA, PART NAME UPPER CHORD, STRINGERS & WS LOCATION ON ACFT WS 281.0 TO AFT OF REAR SPAR. ACFT WAS GNDED.
Part: SEAT TRACK — CRACKED (COCKPIT) · airframe 72,828 hrs · 34,173 cycles
CAPTAIN'S OTBD FWD SEAT TRACK CRACKED BETWEEN 2 BOLTS FOR FWD STOP. R & R CAPTAIN'S OTBD FWD SEAT TRACK IAW SRM 51-40-02. CRACKED IS 2.0 INCHES, PN 812175-7, PART NAME CAPTAIN & FIRST OFFICER SEAT TRACK, SN NSN, FS & BS LOCATION 196.5. ACFT WAS GNDED.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,828 hrs · 34,173 cycles
AFT LOWER CARGO FWD BILGE THE RT INTERCOSTAL BETWEEN STATION 1153 & 1175 IS CORRODED AT THE BACK CORNER. R & R INTERCOSTAL IN AFT LOWER CARGO BETWEEN STATION 1153 & 1175 IN FWD BILGE ON RT SIDE. CORRODED LEVEL 2, PN 146T5000-58, SN NSN, FS & BS LOCATION FROM STATION 1153 TO STATION 1175, STRINGER & WS LOCATION FROM RBL 18 TO RBL 18. ACFT WAS GNDED.
Part: BEAM — CORRODED (RT MLG) · corrosion level 2 · airframe 72,828 hrs · 34,173 cycles
DURING CURSORY INSPECTION OF RT GEAR AUX BEAM WHERE BUSHING WAS REMOVED, FOUND CORROSION ON CIRCUMFERENCE OF BEAM WHERE BUSING WAS MOUNTED. REAMED HOLE CLEAN & ROUND TO 3.564 DIAMETER, CRO SPOT FACED THE DISCREPANT HOLE, MANUFACTURED & INSTALLED REPAIR BUSHINGS ON REA B657-60982-MR. REPLACED RT MLG AUX BEAM OTBD GREASE ZERK FITTING IAW AMM 20-10-29. CORRODED L2, PN 113T1101-64, PART NAME RT MLG AUX BEAM, SN NSN, STRINGER & WS LOCATION WS 284 TO 284. ACFT WAS GNDED.
Part: COUNTERWEIGHT — CORRODED (RT AILERON) · corrosion level 2 · airframe 72,828 hrs · 34,173 cycles
RIGHT OTBD AILERON, OTBD COUNTERWEIGHT HORN, IS CORRODED & CRACKED AT COUNTER WEIGHT. R & R CORRODED & CRACKED RT OTBD AILERON OTBD COUNTER WEIGHT HORN IAW DWG 113T7106, SRM 51-40-05 & 51-40-08, AMM 51- 21-10-7 & 51-31-01. CORRODED LEVEL 2 PN 1137106, PART NAME COUNTER WEIGHT HORN, SN NSN, STRINGER & WS LOCATION ON ACFT FROM 906 TO 1106. ACFT WAS GNDED.
Part: SKIN PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 72,828 hrs · 34,173 cycles
UPPER WING SURFACE PANEL SEPARATING ON LE JUST FWD OF NR 10 SPOILER, UPPER SURFACE OF THE WING. REMOVED TE WING PANEL TO FOM CORROSION ON WING SKIN IAW SRM 57-20-01 FIG 01 IAW REA B657-60934-MR. CORRODED LEVEL 2, PN 112T3101-6, PART NAME UPPER SKIN, SN N/A, FS & BS LOCATION WS 661 TO WS 665, STRINGER & WS LOCATION TE AFT OF REAR SPAR. ACFT WAS GNDED.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,828 hrs · 34,173 cycles
CORROSION ON SEAT TRACK FS 355 BL10 RT. R & R SEAT TRACK RBC10 IAW SRM 51-40-02. SDR INFO PN 368-53-11-90610, NSN, CORRODED L2, PART SEAT TRACK, FS & BS LOC FS 347 - FS 445. ACFT WAS GNDED.
Part: STRINGER — CRACKED (FUSELAGE) · airframe 72,828 hrs · 34,173 cycles
STRINGER CRACKED AT STATION 1520 LOCATED BY ANTENNA BRACKET APPROX STRINGER 2L OR 3L. INSTALLED NEW SECTION OF STRINGER & SPLICES IAW SRM 53-00-03 REPAIR 1 FIG 201 DETAIL 2. SDR INFO CRACKED 3 INCHES, PN 146T3002, PART NAME STRINGER 3L, SN NSN, FS & BS LOC 1507 TO 1510, STRINGER & WS LOC 3L TO 3L. ACFT WAS GNDED.
Part: STRINGER — CRACKED (FUSELAGE) · airframe 72,828 hrs · 34,173 cycles
DURING INSTALL OF STRINGER SPLICE ON STRINGER 32L AT STATION 434, STRINGER CRACKED WHILE INSTALLING FASTENERS & CORROSION WAS FOUND AT CRACK LOCATION. REPAIRED STRINGER 32L AT FS 434 IAW REA B653-60965-MR. SDR INFO CRACKED 1 INCH, CORRODED, PN 143T3001, PART NAME STRINGER 32L, SN: NSN, FS & BS LOC 434 TO 468, STRINGER & WS LOC STRINGER 32L. ACFT WAS GNDED.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,828 hrs · 34,173 cycles
AFT LOWER CARGO RT SIDE, INTERCOSTAL ABOVE STRINGER 36R BETWEEN STATION 1329 & 1351 CORRODED AT NUTPLATE. R & R INTERCOSTAL IN AFT LOWER CARGO STATION 1329 & 1351, RT SIDE IAW SRM 51-40-02 & DWG 146T5000. SDR INFO PN 146T5000-39, NSN, SUPPORT INTERCOSTAL, CORRODED L2, FS 1329 & 1351, STRINGER 36. ACFT WAS GNDED.
Part: SPLICE PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,828 hrs · 34,173 cycles
SEVERAL CORRODED NUTPLATES FOR FWD BILGE PANEL ON FLOORBEAM UPPER CHORD AT STATION 1175. REMOVED, MANUFACTURED & INSTALLED NEW SPLICE PLATE AT STATION 1175 IAW SRM 51-40-02. SDR INFO CORRODED LEVEL 2, PN 146T5000-92, SN NSN, PART NAME SPLICE PLATE, EXACT FS & BS LOCATION ON ACFT FROM STATION 1173 TO STATION 1175. EXACT STRINGER & WS LOCATION ON ACFT FROM RBL 20.5 TO LBL 20.5. ACFT WAS GNDED.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,828 hrs · 34,173 cycles
AFT LOWER CARGO FWD BILGE AREA BETWEEN STATION 1153 & 1175. THE LT INTERCOSTAL BACK CORNER IS CORRODED. R & R NEW INTERCOSTAL IN FWD BILGE AREA BETWEEN STATION 1153 & 1175 IAW SRM 51-40-02. CORRODED LEVEL 2, PN 146T5000-60, SN NSN, EXACT FS & BS LOCATION ON ACFT FROM STATION 1153 TO 1175. EXACT STR & WS ON ACFT FROM LBL 13. ACFT WAS GNDED.
Part: STRINGER CLIP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,828 hrs · 34,173 cycles
FORWARD LOWER CARGO AFT SIDE OF REAR BULKHEAD FUSELAGE STATION 742 WHERE STRINGER 36R ATTACHES TO BULKHEAD CLIP IS CORRODED. FABRICATED NEW STRINGER CLIP FROM 1518-714-7075-T6511 INSTALLED NEW STRINGER CLIP IAW B65360890. SDR INFO CORRODED, PN 140T2101-413AX, PART NAME STRINGER CLIP, SN NSN, FS & BS LOC 742 TO 742, STRINGER & WS LOC 36R. ACFT WAS GNDED.
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,828 hrs · 34,173 cycles
FORWARD LOWER CARGO FS 456 - 478, STRINGER 33L HAS EVIDENCE OF IMPACT DAMAGE TO SIDE OF STRINGER CAUSING IT NOT TO LAY FLAT AGAINST FUSELAGE SKIN ON LOWER SIDE OF STRINGER. R & R STRINGER AT FS 456 - 478, STRINGER 33L IAW SRM 51-40-02. R & R EQUIP COOLING DUCT, DUCT INSTALLATION IAW AMM 21-58- 09-4. SEE REA 653- 60965, SDR INFO CORRODED, PN 143T3001, PART NAME STRINGER, SN NSN, FS & BS LOCATION FROM 456 TO 478, STRINGER & WS LOCATION FROM STRINGER 33L. ACFT WAS GNDED.
Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,828 hrs · 34,173 cycles
STATION 1417 LBL 8 HAS CORRODED WEB. INSTALLED NEW WEB PN 452T3288-5AX IAW SRM 51-40-2. TWO INTERCOSTALS INSTALLED PN 482T3251-1 & 452T3252-2. SDR INFO CORRODED L2, PN 452T3288-5, 452T3252-2 & 452T3251-1, PART NAME WEB, SN NSN, FS & BS LOC STATION 1417 TO 1400 TO LBL 8 TO LBL 11. ACFT WAS GNDED.
Part: ATTACH FITTING — CORRODED (RT WING) · corrosion level 2 · airframe 72,828 hrs · 34,173 cycles
REAR SPAR TO TE LOWER PANEL ATTACH CHORD ON WING AT INBD END OF INBD AILERON CORRODED. REMOVED PANEL 652JB, REMOVED REAR TE LOWER CHORD AT WS 431.97. INSTALLED NEW TE LOWER CHORD AT WS 431.97 IAW SRM 51-40-02 PARA 7 D & PAR 4 6. REINSTALLED PANEL 652JB IAW SRM 51-40-02. SDR INFO CORRODED, PN 113T1510-68, PART NAME CHORD, SN NSN, FS & BS LOC WS 431. ACFT WAS GNDED.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,828 hrs · 34,173 cycles
BULK CARGO FLOOR SUPPORT ABOVE STRINGER 35R BETWEEN STATION 1417 & 1439 IS CORRODED BETWEEN NUTPLATE & SUPPORT. REPAIR FLOOR SUPPORT & REPLACED TRANSITION SUPPORT AT RBL 25 FS 1439 & 1417 IAW SRM 51-70-11. SDR INFO CORRODED L-2, PN 146T5004-21/146T5006-1, PART NAME SUPPORT & STRINGER, SN NSN, FS LOC 1417 TO 1439, RBL 25. ACFT WAS GNDED.
Part: SKIN — CORRODED (TE FLAP) · corrosion level 2 · airframe 72,828 hrs · 34,173 cycles
LEFT WING INBD MID FLAP AREA UPPER SKIN HAS A CORROSION SPOT THAT HAS BEEN BLENDED BEYOND LIMITS & REQUIRES A COMPOSITE REPAIR IAW NR -1599, 30.5 INCHES FROM OTBD EDGE & 34 INCHES FROM AFT EDGE. REPAIRED CW INBD MID FLAP UPPER SKIN IAW SRM 57-53-01 & 51-70-10. FINISH TO BE RESTORED ON NR 1808 CLEARANCE CHECK TO BE ACCOMPLISHED ON NR 1809. SDR INFO CORRODED, PN 113T2242-3, SN NA, PART NAME INBOARD FLAP SKIN UPPER, EXACT FS & BS LOC ON ACFT TO IFS 265. ACFT WAS GNDED.
Part: STRINGER — CRACKED (FUSELAGE) · corrosion level 2 · airframe 72,828 hrs · 34,173 cycles
STRINGER CRACKED AFT OF STATION 676 LT. REPAIRED STRINGER AT STATION 676 IAW B653-60928-MR. SDR INFO CRACKED 0.50, PN 143T3001-22, PART NAME STRINGER, EXACT FS & BS LOCATION ON ACFT FROM FS 676, STRINGER 12L. ACFT WAS GNDED.
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,828 hrs · 34,173 cycles
FS 452, STRINGER 37R CORRODED AROUND RIVET. FOUND STRINGER TO BE OUT OF LIMITS. R & R NEW STRINGER & REPAIR PARTS SRM 53-00-03. SDR INFO CORRODED, PN 143T3001-72, SN NONE, PART NAME STRINGER, EXACT FS & BS LOCATION ON ACFT FROM FS 434 TO FS 467, EXACT STRINGER & WS LOC ON ACFT STRINGER 37R. ACFT WAS GNDED.
Part: SWIVEL — GOUGED (LT MLG) · corrosion level 2 · airframe 72,828 hrs · 34,173 cycles
SIDE BRACE SPINDLE ON WING HAS CHAFE AREA. BLENDED AREA IS REPAIRED IAW B657-60955-MR. SDR INFO PN 113T1110-7, NSN, 1 INCH GOUGE, PART NAME LT LANDING GEAR SIDE, STRUT SWIVEL, GOUGE, INBD FWD OUTER RADIUS. ACFT WAS GNDED.
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,828 hrs · 34,173 cycles
FORWARD LOWER CARGO FS 452, STRINGER 38R CORRODED AROUND RIVET. FOUND STRINGER TO BE OUT OF LIMITS. R & R NEW STRINGER & REPAIR PARTS IAW SRM 53-00-05. SDR INFO CORRODED, PN 143T3001, SN NONE, PART NAME STRINGER, EXACT FS & BS LOC ON ACFT FROM FS 445 TO FS 467 ST, EXACT STRINGER & WS LOC ON ACFT STRINGER 38R. ACFT WAS GNDED.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,828 hrs · 34,173 cycles
FORWARD LOWER CARGO FUSELAGE STATION 742 AFT BULKHEAD LOWER FLANGE FOR FLOOR PANELS IS CORRODED, UPPER & LOWER SIDES. REPLACED AFT BULKHEAD LOWER FLANGE IAW SRM 51-40-02. SDR INFO PN 453T1637-3, NSN, SUPPORT FOR FLOOR, FS & BS LOC FS 742, CORRODED. ACFT WAS GNDED.
Part: STRINGER — CRACKED (FUSELAGE) · corrosion level 2 · airframe 72,828 hrs · 34,173 cycles
STRINGER CRACKED AT STATION 720, STRINGER 12R. REPAIRED AREA IAW B653-60931-MR. SDR INFO CRACKED 1 INCH & 1/4, PN 143T3001-8, NSN, STRINGER. ACFT WAS GNDED.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,828 hrs · 34,173 cycles
FORWARD LOWER CARGO FUSELAGE STATION 720 - 742 LBL 7 FLOOR ANGLE CORRODED ON BOTTOM SIDE. REPLACED FLOOR SUPPORT IAW SRM 51-40-02. PN 451T1307, SUPPORT, CORRODED, FUSELAGE STATION 720 - 742. ACFT WAS GNDED.
Part: STIFFENER — CRACKED (CARGO DOOR) · airframe 72,828 hrs · 34,173 cycles
BULK CARGO DOOR INTERIOR VERTICAL STIFFENER PN 146T6348-2 IS CRACKED. FOUND WHILE DISASSEMBLING STRUCTURE FOR REPAIRS ON NR 0193. REMOVED DAMAGED CHORD. SABBED NEW CHORD & INSTALLED NEW CHORD IAW SRM 52-30-02 & 51-40-02. SDR INFO CRACKED 1 INCH, PN 146T6348-2, PART NAME CHORD, SN NA, FS & BS LOC FROM LF STA 1439, STRINGER & WS LOC FROM IN LINE WITH TO STRINGER 25L. ACFT WAS GNDED.
Part: SUPPORT ANGLE — CRACKED (VERTICAL STAB) · corrosion level 2 · airframe 72,828 hrs · 34,173 cycles
VERTICAL STAB ACCESS 324CLX & 324AL, SUPPORT STRUCTURE BOX FWD LWR FLANGE CRACKED LT & RT OTBD EDGES. REMOVED CRACKED SUPPORT ANGLE. FABRICATED NEW SUPPORT IAW DWG 173T1215 & SAMPLE. PN 173T1302-1, NSN, SUPPORT ANGLE, CRACKED 2 INCHES & 1.5 INCHES, STATION 1746, STRINGER 2R - 2L. ACFT WAS GNDED.
Part: STIFFENER — CRACKED (NR 2 PYLON) · corrosion level 2 · airframe 72,828 hrs · 34,173 cycles
NUMBER 2 PYLON INBD HYD BAY. AFT HORZ STIFFENER AT NAC 370 HAS DAMAGED HOLES COMMON TO THE LOWER DOOR FRAME CHANNEL. REMOVED DAMAGED STIFFENER IAW SRM 51-40-02. FABRICATED NEW STIFFENER IAW SRM 54-51-71 & 51-30-01, PERFORMED NDT IAW NDTM PART 6 51-00- 19, APPLIED PROTECTIVE COATINGS IAW SRM 51-20-01. INSTALLED NEW STIFFENER IAW SRM 51-40-02. SDR INFO HOLE 1 INCHES, PN 313T3380-488, PART NAME STIFFENER, SN NA, NAC LOC 370 TO 371. ACFT WAS GNDED.
Part: STRINGER SPLICE — CRACKED (FUSELAGE) · corrosion level 2 · airframe 72,828 hrs · 34,173 cycles
FORWARD LOWER CARGO FUSELAGE STATION 437, STRINGER 31R AT STRINGER SPLICE IS CRACKED & CORRODED. REMOVED CORRODED STRINGER SPLICE AT FS 434, STRINGER 31R & INSTALLED NEW STRINGER SPLICE IAW SRM 51-40-02. SDR INFO CRACKED .050 INCHES, PN 140T0115-20, PART NAME STRINGER SPLICE, SN NSN FS & BS LOC FS 434, STRINGER 31R. ACFT WAS GNDED.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 72,828 hrs · 34,173 cycles
FLOORBEAM CORRODED UPPER FWD FLANGE AT STATION 566 RBL 11. REMOVED CORROSION FROM UPPER FWD FLANGE AT FS 566 BLO IAW IAI SUPPLEMENTAL MANUAL TO SRM 53-00-51. SDR INFO CORRODED, PN 368-53-13-90875-103, SN NSN, PART NAME FLOORBEAM, FS & BS LOC FROM FS 566 STRINGER & WS LOC FROM BLO. ACFT WAS GNDED.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 72,828 hrs · 34,173 cycles
FLOORBEAM CORRODED ON UPPER & LOWER FLANGES STATION 588 BL0. BLEND FLOORBEAM UPPER & LOWER FLANGES AT STATION 588 BL0 IAW 53-01-51. REMOVED .003 IA WITHIN ALLOWABLE LIMITS. SDR INFO CORRODED, PN 368-53-13-90873-101, PART NAME BEAM ASSEMBLY, EXACT FS & BS LOC ON ACFT FROM 588 TO 588. ACFT WAS GNDED.
Earlier reports · 2006–2013 · 25 reports
2013
Part: PBE — DAMAGED (COCKPIT) · airframe 715,585 hrs · 33,582 cycles
COCKPIT PBE SEAL DAMAGED. R & R PBE IAW AMM 25-60-00.
Part: ESCAPE REEL — DISLODGED (CABIN) · airframe 71,577 hrs · 33,579 cycles
INERTIAL ESCAPE REEL IN SUPER NUMERARY DROPPED DOWN AFTER TAKEOFF. REPLACE ESCAPE REEL ASSY.
2012
Part: SPAR — CORRODED (CENTER WING) · airframe 70,322 hrs · 33,037 cycles
CENTER TANK UPPER SPAR CHORD CORRODED FROM OUTBOARD END APPROX LBL 28.6 STA 955. CORROSION OUT OF LIMITS. CUT AND REMOVED OUT OF LIMITS SECTION OF CHORD. REPAIRED IAW REA B657-60353-MR. REA B657-60353-MR, REA B657-60353-MR, ACFT WAS GROUNDED.
Part: STRINGER — GOUGED (FUSELAGE) · airframe 70,322 hrs · 33,037 cycles
LEFT WHEEL WELL STRINGER GOUGED AROUND HOLE. BLENDED, FOUND TO BE OUT OF LIMITS. REPLACED FITTING 145T8754-23 IAW BOEING 767 SRM 51-40-2, ACFT WAS GROUNDED.
Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 70,322 hrs · 33,037 cycles
SEAT TRACK STA 933 - 1100 LT LBL 88.5 CRACKED AT 1100 END. REPAIRED DAMAGED TRACK WITH A NEW SECTION IAW REA B653-60322, ACFT WAS GROUNDED.
Part: FITTING — CORRODED (FUSELAGE) · airframe 70,322 hrs · 33,037 cycles
INBOARD & OUTBOARD POCKETS CORRODED ON PICKLE FORK RIGHT STA 955 AFT SIDE. REPLACED RIGHT PICKLE FORK FITTING. REPLACED SIDE FRAME FITTING (PICKLE FORK) IAW EA 53500014-008, AND DOC 47008ORD12, ACFT WAS GROUNDED.
Part: FAILSAFE — CORRODED (FUSELAGE) · airframe 70,322 hrs · 33,037 cycles
SEVEN FASTENER HOLES EXHIBIT EVIDENCE OF FRETTING AND ONE SMALL AREA OF POSSIBLE CORROSION WERE FOUND DURNG THE INSPECTION OF THE LEFT FAILSAFE STRAP. REF STEP 14.5 OF EA 53500013-006. FAILSAFE STRAP REPLACEMENT ACCOMPLISH ON EA53500013-008 AMES DOC 47008ORD11, ACFT WAS GROUNDED.
Part: FAILSAFE — CRACKED (FUSELAGE) · airframe 70,322 hrs · 33,037 cycles
LETFT FAILSAFE STRAP LWR HOLE 3/16 CRACKED. REPLACED LEFT FAILSAFE STRAP STA 955 CORROSION FAILSAFE STRAP REPLACEMENT TO BE ACCOMPLISHED ON EA53500013-008 AMES DOC 47008ORD11, ACFT WAS GROUNDED.
Part: SPAR — CORRODED (LT WING) · airframe 70,322 hrs · 33,037 cycles
AREA OF CORROSION ON THE REAR SPAR WEB 3 INCHES FROM THE TOP. LOCATED AT STA 955 LEFT LBL 79. REMOVED CORROSION IAW B767-200 SRM 57-10-10 FIGURE 101. BLENDOUTS EXCEEDED PUBLISHED LIMITS AREA REPAIRED IAW REA B657-60346MR, ACFT WAS GROUNDED.
Part: FITTING — CORRODED (FUSELAGE) · airframe 70,322 hrs · 33,037 cycles
RIGHT STA 955 SIDE FRAME FITTING HAS SEVERAL AREAS OF CORROSION ON MATING SURFACE COMMON TO REAR SPAR WEB PAD UP AREAS. SIDE FRAME FITTING (PICKLE FORK) REPLACEMENT ACCOMPLISHED ON EA 53500014-008, AMES DOC 47008ORD12 AND NR 0037, ACFT WAS GROUNDED.
Part: FAILSAFE — CORRODED (FUSELAGE) · airframe 70,322 hrs · 33,037 cycles
RIGHT FAILSAFE HAS 5 AREAS OF CORROSION, 1 CHAFED AREA AND SEVERAL TOOLING MARKS. SIDE FRAME FITTING (PICKLE FORK) REPLACEMENT ACCOMPLISHED ON EA 53500014-008, AMES DOC 47008ORD12 AND NR 0037, ACFT WAS GROUNDED.
Part: SPAR — CORRODED (RT WING) · airframe 70,322 hrs · 33,037 cycles
STA 955 REAR SPAR RIGHT O/B PAD UP AREA HAS SEVERAL AREAS OF CORROSION UPPER-LWR. REPAIRED AREA IAW REA B653-60342-MR, ACFT WAS GROUNDED.
Part: SKIN — CORRODED (FUSELAGE) · airframe 70,322 hrs · 33,037 cycles
INTERNAL FUSELAGE SKIN HAS LIGHT CORROSION PITTING THAT WAS HIDDEN BY FAILSAFE STRAP, ADJACENT TO PICKLE FORK FITTING. REMOVED CORROSION IAW B767 SRM 51-10-02. REPAIRED AREA IAW REA B653-60345-MR, ACFT WAS GROUNDED.
Part: TEE FITTING — CORRODED (FUSELAGE) · airframe 70,322 hrs · 33,037 cycles
LEFT T-FITTING CORRODED STA 955. NEW SIDE T-FITTING P/N 100T1440V3 HAS BEEN MATCH DRILLED IAW B767 SRM 51-40-05. NEW FITTING WILL BE INSTALLED ON EA 53500013-008 AMES DOC 47008ORD11 STEP 41, ACFT WAS GROUNDED.
Part: TEE FITTING — CORRODED (FUSELAGE) · airframe 70,322 hrs · 33,037 cycles
RIGHT SIDE T-FITTING STA 955 CORRODED. NEW RIGHT SIDE FITTING P/N 100T1440V4 HAS BEEN MATCH DRILLED IAW B767 SRM 51-40-05. NEW FITTING WILL BE INSTALLED ON EA5350014-008 ANES DOC 47008ORD12 STEP 41, ACFT WAS GROUNDED.
Part: FAILSAFE — CRACKED (FUSELAGE) · airframe 70,322 hrs · 33,037 cycles
RIGHT FAILSAFE STRAP MID HOLE 3/16 CRACK, LWR HOLE 3/16 CRACK. TRIM OUT AND TERMINATION ACTION ACCOMPLISHED ON EA 53500014-003. DOCUMENT 47008ORD04. NO FURTHER ACTION REQUIRED, ACFT WAS GROUNDED.
2010
Part: SUPPORT — CRACKED (TE FLAP) · airframe 68,293 hrs · 31,806 cycles
NR 8 FLAP SUPPORT HAS THREE HOLES THAT HAVE CRACK INDICATION FOUND WITH HFEC 767 NDT. HOLES HAVE BEEN REAMED AND HFEC HAS BEEN ACCOMPLISHED IAW B767 NDTM PART 6-00-16. NO DEFECTS NOTED.
Part: SKIN — DENTED (FUSELAGE) · airframe 68,293 hrs · 31,806 cycles
PERMANENTLY REPAIR THE FUSELAGE SKIN DENT LOCATED AT STA 1361, 328L IAW REA 653-58754-MR REV 'A'. AREA WAS REPAIRED IAW REA B653-58754-MR.
Part: SUPPORT CHANNEL — CRACKED (NR 2 PYLON) · airframe 68,293 hrs · 31,806 cycles
NR 2 PYLON LOWER SUPPORT CHANNEL FOR PANEL 447BL CRACKED AT FWD EDGE. REMOVED AND REPLACED NR 2 PYLON LOWER SUPPORT CHANNEL FOR PANEL IAW 767 SRM 51-40-02.
Part: STRINGER — CRACKED (FUSELAGE) · airframe 68,293 hrs · 31,806 cycles
STRINGER S-11L IS CRACKED JUST AFT OF STA 676. STRINGER REPAIRED IAW REA B653-59115-MR.
Part: STRINGER — CRACKED (FUSELAGE) · airframe 68,293 hrs · 31,806 cycles
STRINGER S10L CRACKED AFT OF STA 676. STRINGER REPAIRED IAW B653-59115-MR.
Part: UNKNOWN — ODOR · airframe 66,670 hrs · 31,146 cycles
AT CRUISE FLIGHT A SMELL SIMILAR TO BURNING RUBBER AND/OR OIL WAS NOTICED. REFERRING TO SMOKE OR FUMES CHECKLIST AND ISOLATED RIGHT PACK AS APPARENT SOURCE. NO FURTHER ODOR REMAINDER OF FLIGHT WITH RIGHT PACK OFF, NO SMOKE EVER VISIBLE. INSP RAM AIR INLET AND EXH DOOR AREA; OPERATED RT PACKS FOR 3 HRS W/APU PWR IN BOTH COLD & HOT FULL POSITIONS, OPERATED RT PACK WITH NR 2 ENGINE NO ODOR NOTED AT THIS TIME. RT PACK & LT PACKS SYST CHECKS GOOD AT THIS TIME.
2007
Part: SWITCH — INOPERATIVE (CABIN) · airframe 62,683 hrs · 29,625 cycles
EMERGENCY / DEPRESS TEST LIGHTS SWITCH INOPERATIVE (WOULD NOT TEST). WIRED SYSTEM TO WDM 33-24-11, SYSTEM TESTS NORMAL.
Part: FIRE LOOP — DEFECTIVE (RT ENGINE) · airframe 62,668 hrs · 29,615 cycles
RIGHT ENGINE FIRE WARNING ALERT IN FLIGHT, EICAS MESSAGE: FIRE RIGHT ENGINE. STATUS PAGE: RIGHT ENGINE FIRE LOOP 1 AND 2. SECURED RIGHT ENGINE, NO FIRE BOTTLES USED. AIR TURNBACK TO MIA. REMOVED AND REPLACED RIGHT ENGINE LOWER AFT FIRE DETECTION LOOP IAW B767 MM 26-11-02. BITE AND RUN UP TEST NORMAL.
2006
Part: SKIN — CRACKED (FUSELAGE) · airframe 62,627 hrs · 29,602 cycles
FOUND FUSELAGE SKIN WAS CRACKED AT R1 DOOR CUTOUT LOWER AFT CORNER. REPAIRED CRACK IAW REA D653-55112.