N742AX
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.
89 reports on file, 2006-04-05 – 2013-09-12.
Part: SHEAR TIE — CORRODED (ZONE 200) · airframe 83,829 hrs · 39,117 cycles
SHEAR TIE FS 544 BETWEEN L33 -34R CORRODED. FABRICATED & HEAT TREATED NEW SHEAR TIE IAW REA B65360693 ACFT WAS GROUNDED.
Part: STRINGER — CORRODED (ZONE 100) · airframe 83,829 hrs · 39,117 cycles
STRINGER 34R BETWEEN BS 522-544 CORRODED ON THE OTBD UPPER LIP. REMOVED STRINGER IAW SRM'S 51-40-02, SRM 53-00-01, REPAIR 1, 53-00-03, REPAIR 2, FIG 210 AND AMM 20-10-12-4 AND REA B653-60675-MR. ACFT WAS GROUNDED.
Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 83,829 hrs · 39,117 cycles
BS 632, RBL 24, CORROSION UNDER NUTPLATES ON FLOORBEAM UPPER TEE. FABRICATED FLOORBEAM UPPER TEE IAW DWG 143T1209, PO: 0037850.ACFT WAS GROUNDED.
Part: STRINGER — CORRODED (ZONE 100) · airframe 83,829 hrs · 39,117 cycles
AFT LOWER CARGO STRINGER 39L BETWEEN BS 1219 & 1241 CORRODED. R & R STRINGER IAW SRM 53-00-03. ACFT WAS GROUNDED.
Part: STRINGER CLIP — CRACKED (BS 1307) · airframe 83,829 hrs · 39,117 cycles
AFT LOWER CARGO LT SIDEWALL TO FLOOR AREA, STRINGER 31L BETWEEN BS 1307 & 1329 CORRODED. STRINGER CLIP BS 1307 S32L CRACKED.
Part: STRINGER — CORRODED (BS 1197-1129) · airframe 83,829 hrs · 39,117 cycles
AFT LOWER CARGO STRINGER 39L BETWEEN BS 1197 & 1129 CORRODED. R & R STRINGER BS 1197 TO 1219 IAW SRM 53-00-03. REPAIR 2. ACFT WAS GROUNDED.
Part: CARGO TRACK — CORRODED (BS 355) · airframe 83,829 hrs · 39,117 cycles
UPPER CARGO, BS 355, RBL 11, CARGO TRACK AND UPPER SURFACE OF SPLICE IS CORRODED. R & R CARGO TRACK AND PLATE AT BS 347-445 IAW REA B653-60668-MR, B653-60687-MR, SRM 51-40-02, PG 4, PAR 7, IAI DWG'S 368-25-16 90621 & 368- 53-11-90590. ACFT WAS GROUNDED.
Part: SHEAR WEB — CORRODED (ZONE 200) · airframe 83,829 hrs · 39,117 cycles
SHEAR WEB BS 488, CORRODED UNDER 232G AND 232E. R & R SHEAR WEB BS 475-525, RBL 11-33- & 55-77 IAW SRM 51-40-02, PG 4, PAR7 & IAI DWG 368-53-13-95590. ACFT WAS GROUNDED.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 83,829 hrs · 39,117 cycles
STAINLESS ANGLE AT BOTTOM OF BACK WALL IN UPPER CARGO HAS CORROSION UNDER IT ON FLOORBEAM, APPROXIMATELY AROUND BS 1556. REMOVED & REINSTALLED STAINLESS ANGLE AT BACK WALL IN UPPER CARGO, REMOVED CORROSION & R & R SEAT TRACKS IAW SRM 51-40-02, PG 4, PAR 7, 53-00-01, REA B653-60666-MR, B653-60664-MR B653-60667-MR & B653-60670-MR. 368-53-16-94451-201X2, 368-53-16-94551-202X2, SEAT TRACKING , NSN, 1405-45 TO 1605.5 STR LBL 33 TO RBL 33. CORRODED. ACFT WAS GROUNDED.
Part: SUPPORT — CORRODED (ZONE 100) · airframe 83,829 hrs · 39,117 cycles
BULK CARGO CEILING LT SIDE AT ZONE 161 JUST AFT OF FLOOR SUPPORT BEAM AT STA 1540 THERE IS A CORRODED MAIN CARGO FLOOR SUPPORT. R & R FLOOR SUPPORT TEE (BEAM) AT STA 1540 IAW DWG 146T0051 & SRM 51-40-02, PG 4, PAR 7. ACFT WAS GROUNDED.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 83,829 hrs · 39,117 cycles
SEAT TRACK AT BS 1461-1502 INBD OF L2 DOOR, FOUND TO BE CORRODED BEYOND LIMITS. R & R SEAT TRACK IAW REA NR B653-60673-MR, DWG 146T0051 & SRM 51-40-02 PAR 7, PG 4. ACFT WAS GROUNDED.
Part: SUPPORT — CORRODED (ZONE 100) · airframe 83,829 hrs · 39,117 cycles
AFT LOWER CARGO CEILING BETWEEN STA 1395, 1417 ON LT SIDE IS A MOUNT/SUPPORT FOR THE BULK CARGO BARRIER DOOR FWD ATTACH POINT THAT IS CORRODED. R & R MOUNT/SUPPORT FOR BULK CARGO BARRIER DOOR FWD ATTACH POINT. IAW SRM 51-40-02, STEPS 4 AND 7D. CORROSION, SUPPORT PLATE, PN: 452T3288-5AX, FS/BS LOC: 1395-1417, STR/WS LOC: LBL 20.5. ACFT WAS GROUNDED.
Part: RIB — CORRODED (RT WING) · airframe 83,829 hrs · 39,117 cycles
RT WING L/E RIB HAS CORROSION JUST OTBD OF NR 9 SLAT INBD AUX TRACK. FOUND TO BE OUT OF LIMITS. FABRICATED NEW RIB IAW REA B657-60644. INSTALLED IAW SRM 51-40-02. ACFT WAS GROUNDED.
Part: STRUT — CORRODED (NR 8 SLAT TRACK) · airframe 83,829 hrs · 39,117 cycles
NR 8 SLAT, INBD AUX TRACK, INBD UPPER STRUT CORRODED AT FWD LOWER END. REMOVED NR 8 SLAT INBD UPPER RIB AT AUX TRACK DUE TO CORROSION. INSTALLED NEW SERVICEABLE UPPER RIB AS REQUESTED IAW SRM 51-40-02. CORRODED 114T2200-18 RIB, FROM L/E 436.00 TO ROW L/GE. ACFT WAS GROUNDED.
Part: RIB — CORRODED (ZONE 600) · airframe 83,829 hrs · 39,117 cycles
NR 11 SLAT OTBD AUX TRACK OTBD LOWER STRUT HAS CORROSION UNDER NUTPLATES. INSTALLED A NEW STRUT RIB, PN: 114T2224-8 IAW SRM 51-40-02 PARA 4 & 7 AND REA-B657-60625-. ACFT WAS GROUNDED.
Part: ANGLE — CRACKED (BS 1809) · airframe 83,829 hrs · 39,117 cycles
LT ANGLE HAS HFEC DEFECT INDICATIONS IN THREE AREAS, NDTM PN 6 53-80-04, FIG 1. REPAIRED DAMAGE BY REPLACING ANGLE, UPPER AND LOWER TENSION FITTINGS, SPLICE FITTING AND SKIN REPAIR IAW SRM 53-80-01. ACFT WAS GROUNDED.
Part: STIFFENER — CRACKED (ZONE 200) · airframe 83,829 hrs · 39,117 cycles
UPPER CARGO FLOORBEAM, SECTION 41, CRACKED AT UNDERSIDE, BENEATH PANEL 221G JUST AFT OF ENTRYWAY FLOOR HATCH. R & R UPPER WEB STIFFENER AT STA 325-355, LBL40 BELOW PANEL 221G IAW DWG 141T5140 & SRM 51-40-02, PAR 7, PG 4, PN 141T5140-109 STIFFENER CRACKED .5" LBL40 FROM 325 TO 355; NSN. ACFT WAS GROUNDED.
Part: STRUT — CORRODED (ZONE 200) · corrosion level 2 · airframe 83,829 hrs · 39,117 cycles
NR 4 SLAT OTBD AUX TRACK INBD LOWER STRUT CORRODED AND FASTENERS MISSING AT FORWARD END. R & R STRUT ON NR 4 SLAT OTBD AUX TRACK INBD. STRUT IAW SRM 51-40-023 & 51-40-05. ACFT WAS GROUNDED.
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 83,829 hrs · 39,117 cycles
FLOOR SUPPORT FROM BS 610 - 632 LBL 8 CORRODED AROUND NUTPLATES. R & R FLOOR SUPPORT IAW SRM 51-40-02.
Part: SKIN — CORRODED (ZONE 200) · corrosion level 2 · airframe 83,829 hrs · 39,117 cycles
UPPER AREA FORWARD OF FRONT SPAR, AFT OF NR 12 SLAT AT WING LES 960 CORRODED. REMOVED CORROSION IAW SRM 57-20-01. SKIN BLEND-OUT AND SPLICE PLATE REPAIR WERE ACCOMPLISHED ON REA B657-60655. ACFT GROUNDED.
Part: FITTING — CORRODED (RUDDER) · airframe 83,829 hrs · 39,117 cycles
RUDDER LT SIDE 8 INCHES BELOW TIP, 4 INCHES FWD OF T/E FASTENER HEAD POPPED, POSSIBLE DELAMINATED. REMOVED RUDDER TIP PANEL, REPLACED RUDDER TIP FITTING, REPLACED RUDDER TIP PANEL IAW SRM 51-40-02 AND SEALED IAW 51-20-5. ACFT WAS GROUNDED.
Part: FLOORBEAM — CORRODED (BS 610) · airframe 83,829 hrs · 39,117 cycles
CORROSION UNDER NUTPLATES ON FLOORBEAM UPPER TEE BS 610, RBL 18 - 30. R & R UPPER TEE IAW SRM 51-40-02. ACFT WAS GROUNDED.
Part: STRINGER — CORRODED (ZONE 100) · airframe 83,829 hrs · 39,117 cycles
AFT LOWER CARGO AREA BETWEEN BS 1502 & 1506 STRINGER 26L IS CORRODED. REMOVED DAMAGED SECTION & REPAIRED IAW SRM 53-00-03, REPAIR 2. ACFT WAS GROUNDED.
Part: CHANNEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,829 hrs · 39,117 cycles
BULK CARGO , AFT DOOR FRAME, TOP CORNER IS A CORRODED STRINGER TIE. R & R STRINGER TIE, END FITTING IAW SRM 51-40-02 AND DWG 146T3007. PN 146T3007, CHANNEL, SKIN PANEL, CORRODED BS1461, STR 24; ACFT WAS GROUNDED.
Part: STRINGER — CORRODED (ZONE 100) · airframe 83,829 hrs · 39,117 cycles
AFT LOWER CARGO BAY STRINGER 35R JUST FWD OF BS 1263 WAS CORRODED. R & R CORRODED STRINGER FROM BS 1254 TO 1259 IAW SRM 53-00-03. ACFT WAS GROUNDED.
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 83,829 hrs · 39,117 cycles
UPPER CARGO, BS 355, LEFT BL33, SEAT TRACK IS CORRODED. R & R SEAT TRACK IAW IA DWG 36853-16-90621, SF SRM 51-40-02 PG 7, SH 4 & REA NR B653-60668-MR. ACFT WAS GROUNDED.
Part: SKIN — DEBONDED (HORIZONTAL STAB) · airframe 83,829 hrs · 39,117 cycles
LT HORIZONTAL STAB UPPER SKIN HONEYCOMB DISBONDED FROM SKIN AUX SPAR STA 127-157, VIEWED FROM INSIDE L/E AUX SPAR. REMOVED LT HORZ STAB UPPER SKIN, SENT OUT FOR REPAIR ON R501623345, REINSTALLED LT HORIZONTAL STABILIZER UPPER SKIN AT STA 127 TO 157 IAW SRM 51-40-02. PN: 185T1001-1, PANEL, ASSY TORQUE BOX SKIN, LT HORZ. L/E STA 100.00 TO 250.25 DISBONDED; ACFT WAS GROUNDED.
Part: DOOR FRAME — CORRODED (BS 1461) · corrosion level 2 · airframe 83,829 hrs · 39,117 cycles
BS 1461 S32L WL 133, AFT LOWER CORNER OF BULK CARGO DOOR CUTOUT IS CORROSION . REPAIRED IAW SRM 50-70-13. ACFT WAS GROUNDED.
Part: STRINGER — CORRODED (ZONE 100) · airframe 83,829 hrs · 39,117 cycles
AFT LOWER CARGO STRINGER 37R BETWEEN BS 1197 & 1219 CORRODED. REMOVED CORRODED SECTION OF STRINGER 37R, SPLICED IN NEW STRINGER SECTION IAW SRM 53-00-03, FIG 201 REPAIR 2. ACFT WAS GROUNDED.
Part: BEAM — DAMAGED (ZONE 800) · airframe 83,829 hrs · 39,117 cycles
R1 DOOR BS 841 INTERIOR BEAM SECOND FROM TOP, AFT AREA. REMOVED & REPLACED BEAM IAW SRM 51-10-02. ACFT WAS GROUNDED.
Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,829 hrs · 39,117 cycles
AFT LOWER CARGO STRINGER 39R BETWEEN BS 1197 & 1219 CORRODED. R & R CORRODED STRINGER IAW SRM 53-00-03. ACFT WAS GROUNDED.
Part: WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 83,829 hrs · 39,117 cycles
SEVERAL AREAS OF WEB CORROSION IN THE BALLMAT AREA. R & R WEB 5, BS 1263-1285 & 1285 -1329 IAW SRM 51-40-02 AND 53-60-53. PANEL, PN: 451T2504, LOC: FS1285-FS1329/RBL 24.92-33.15. ACFT WAS GROUNDED.
Part: STRINGER — CORRODED (ZONE 200) · corrosion level 2 · airframe 83,829 hrs · 39,117 cycles
FS 412 - 434, STRINGER 34R CORRODED INCLUDING SPLICE WITH RIVETS PULLING THROUGH. INSTALLED NEW SECTION OF STRINGER FROM BS 412 TO 434 IAW SRM 51-40-02. ACFT WAS GROUNDED.
Part: SUPPORT ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,829 hrs · 39,117 cycles
FWD LOWER CARGO ANGLE AT FUSELAGE BS 740 S32L TO 32R IS CORRODED ON BOTH UPPER & LOWER SIDES & HAS RUSTY NUTPLATES. R & R ANGLE AND INSTALLED NUT PLATES ON ANGLE IAW SRM 51-40-02. ACFT WAS GROUNDED.
Part: BRACKET — WORN (ZONE 100) · airframe 83,829 hrs · 39,117 cycles
SIDE ROLLER TOP BOLT IS WORN AT THE REAR OF FLC DOOR JAMB AND HAS TWO BUSHINGS MIGRATING OUT OF BRACKET AT ATTCH POINT. REMOVED BRACKET AND REAMED HOLE TO .6275 IAW REAB 625-60635 AND ACCOMPLISHED BUSHING REPAIR IAW REA B625-60646-MR. BRACKET, PN: 452T2202-11, FS/BS LOC: 600 STR/WS: S33R-S34R; ACFT WAS GROUNDED.
Part: STRUCTURE — CORRODED (CARGO DOOR) · airframe 83,829 hrs · 39,117 cycles
SEVERAL SPOTS OF CORROSION ON BULK CARGO DOOR INNER STRUCTURE. REPAIRED, R & R CORRODED AREAS IAW SRM CH'S 51-21-04, 51- 21-10, 51-40-02. PN: 146T6342-1, NSN, INNER CHORD CORRODED. 1263 -1351 STR 28L; ACFT WAS GROUNDED.
Part: STRINGER — CORRODED (BS 1461-1488) · corrosion level 2 · airframe 83,829 hrs · 39,117 cycles
BULK CARGO AFT DOOR FRAME STRINGER 26L IS CORRODED. R & R CORRODED STRINGER 26L AFT OF BULK CARGO DOOR FRAME IAW SRM 53-00-03 USING PN BAC1498-203-7075-T62, PO 0040135 AND PN 7075-T6511-4.00 X 4.00 PO 0040175. PN: 146T3002-40 STRINGER 26L, NSN, CORRODED, 1461 TO 1488; ACFT WAS GROUNDED.
Part: SHEAR TIE — CORRODED (ZONE 200) · corrosion level 2 · airframe 83,829 hrs · 39,117 cycles
BS 720 BETWEEN S36-37L CORRODED BULKHEAD ATTACH FRAME TO SKIN. ALODINED AND PRIMED NEW FABRICATED SHEAR TIE IAW SRM 51-20-01, INSTALLED SHEARTIE AND CLIP IAW SRM 51-40-02. ACFT WAS GROUNDED.
Part: CHANNEL — CRACKED (NR 1 NACELLE) · airframe 83,829 hrs · 39,117 cycles
NR 1 PYLON INBD HYD BAY DOOR LOWER CHANNEL HAS CRACK AT FWD END. R & R NR 1 PYLON INBD H90 BAY DOOR LOWER CHANNEL WITH SERVICEABLE CHANNEL IAW SRM 51-40-02 PARA 7 & 51-40-04 PARA 2B. ACFT WAS GROUNDED.
Part: WEB — CORRODED (ZONE 600) · corrosion level 2 · airframe 83,829 hrs · 39,117 cycles
LEADING EDGE WEB AT LES 441-456 FOUND TO BE EXFOLIATED. REMOVED & REPLACED L/E WEB IAW SRM 51-40-02. NOSE BEAM CORRODED, RT WING LES 454 - 456. AIRCRAFT WAS GROUNDED.
Part: STRINGER — CORRODED (ZONE 100) · airframe 83,829 hrs · 39,117 cycles
AFT LOWER CARGO STRINGER 39R BETWEEN STA 1153 & 1175 CORRODED. AFT LOWER CARGO STRINGER 382, BETWEEN STA 1153 AND 1175, REPAIRED IAW SRM 53-00-03, FIG 201. ACFT WAS GROUNDED.
Part: SILL — CORRODED (BS 1395-1480) · corrosion level 2 · airframe 83,829 hrs · 39,117 cycles
BULK CARGO DOOR, UNDER SILL PLATE, BETWEEN STA 1417 & 1461 THERE IS EVIDENCE OF CORROSION. REMOVED BULK CARGO DOOR SILL PLATE, INNER & CHORD, DRAIN HOLE DOUBLER, L/W INTERCOSTAL, REPLACED INNER & CHORD, AND DRIAN HOLE DOUBLER, REINSTALLED LT INTERCOSTAL, AND BULK CARGO DOOR WILL PALTE IAW SRM 51-40-02 FOR WORK COMPLETED. PN: 146T8008-2, CHORD, INNER CORRODED, STA 1395 TO STA 1480 LBL 44.0; ACFT WAS GROUNDED.
Part: SKIN — CORRODED (ZONE 200) · airframe 83,829 hrs · 39,117 cycles
LIGHT CORROSION FUSE SKIN OUTER SURFACE BS 1582, S9-18R. REMOVED CORROSION TO SKIN IAW 53-80-01 AND 53-00-01. WORK ACCOMPLISHED IAW REA B653- 60659-MR. ACFT GROUNDED.
Part: WEB — CORRODED (ZONE 100) · airframe 83,829 hrs · 39,117 cycles
AFT LOWER CARGO RT FWD BILGE WEB CORRODED. FABRICATED NEW RT FWD BILGE WEB IAW DWG 146T5000. ACFT WAS GROUNDED.
Part: WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,829 hrs · 39,117 cycles
AFT LOWER CARGO LT FWD BILGE WEB CORRODED. FABRICATED NEW LT FWD BILGE WEB IAW BAC DWG 146T5000, PN 146T5000-144, PN WEB CORRODED FS/BS LOC: FS 1263 TO FS 1285, LOC ON ACFT: LBL8 TO LBL33; ACFT WAS GROUNDED.
Part: SHEAR TIE — CORRODED (ZONE 200) · corrosion level 2 · airframe 83,829 hrs · 39,117 cycles
FS 544 LB 0, LBL 6 - RBL 4 SKIN TO UNDER THE FLOOR BULKHEAD ATTACH ANGLES CORRODED. INSTALLED THREE FABRICATED SHEAR TIES IAW SRM 51-40-02. ACFT WAS GROUNDED.
Part: INTERCOSTAL — CORRODED (ZONE 200) · corrosion level 2 · airframe 83,829 hrs · 39,117 cycles
INTERCOSTAL CORRODED BETWEEN BS 1285 & 1307 ABOVE S35R. R & R INTERCOSTAL IAW SRM 51-40-02. ACFT WAS GROUNDED.
Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,829 hrs · 39,117 cycles
STA 522 - S36L TO S39L SHEAR TIES HAVE LIGHT CORROSION CAUSING PAINT TO PEEL. INSTALLED 3 EA FABRICATED SHEARTIES IAW SRM 51-40-02, PN: 140T2102-219-221-223 SHEARTIES CORRODED 25L FROM 536L TO 539L. ACFT WAS GROUNDED.
Part: STRUT — CORRODED (NR 10 SLAT) · airframe 83,829 hrs · 39,117 cycles
NR 10 SLAT, OTBD AUX TRACK, INBD LOWER STRUT CORRODED AROUND NUTPLATES. R & R LOWER STRUT AT NR 10 SLAT OTBD AUX. TRACK IAW SRM 51- 40-02, PARA 7, PN: 114T2217-8, STRUT - CORRODED, LWR OSS 779.437; ACFT WAS GROUNDED.
Part: STRUT — CORRODED (ZONE 500) · airframe 83,829 hrs · 39,117 cycles
NR 2 SLAT, INBD AUX TRACK OTBD LOWER STRUT CORRODED AROUND NUTPLATES. REPLACE STRUT RIB WITH A NEW PART PN: 114T222-7 IAW SRM 51-40-02, PARA 4 & 7. ACFT WAS GROUNDED.
Part: STRUT — CORRODED (NR 3 SLAT) · airframe 83,829 hrs · 39,177 cycles
NR 3 SLAT INBD AUX TRACK OTBD LOWER STRUT CORRODED AROUND NUTPLATES. R & R INBD AUX TRACK OTB LOWER STRUT IAW SRM 51-40-02. ACFT WAS GROUNDED.
Part: STRUT — CORRODED (NR 2 SLAT) · airframe 83,829 hrs · 39,117 cycles
NR 2 SLAT, OTBD AUX TRACK, OTBD LOWER STRUT CORRODED AROUND NUTPLATES. REPLACED STRUT RIB, PN: 114T2224-7 IAW SRM 51-40-02, PARA 4 & 7. PN: 114T2224-7, STRUT, RIB, CORRODED. FROM OSS 937,929 AT L/W L/E; ACFT WAS GROUNDED.
Part: SUPPORT FITTING — CRACKED (RT WING) · airframe 83,829 hrs · 39,117 cycles
RIGHT WING REAR SPAR FITTING AT WS 700, A SUPPORT FITTING FOR THE NR 11 SPOILER AND THE FLAP DRIVE TORQUE TUBE, AFT SUPPORT LEG IS CRACKED IN HALF. R & R NR 11 SPOILER INBD SUPPORT FITTING IAW SRM 51-40-02. PN: 113T1566-26, NSN, FITTING, CRACK 1.5", RIGHT WING REAR SPAR WS 700; ACFT WAS GROUNDED.
Part: ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,829 hrs · 39,117 cycles
CORRODED "J" ANGLE AT BS 1285 ABOVE STRINGER 35 RT. REPAIRED CORRODED "J" ANGLE ON FLOORBEAM AT BS 1285 ABOVE STRINGER 35R IAW DETAIL V. ACFT WAS GROUNDED.
Part: STRUT — CORRODED (NR 5 SLAT TRACK) · corrosion level 2 · airframe 83,829 hrs · 39,117 cycles
NR 5 SLAT OTBD AUX TRACK OTBD LOWER STRUT HAS SMALL AREA OF CORROSION UNDER NUTPLATES. R & R STRUT IAW SRM 51-40- 02 AND REA B657-60628. ACFT WAS GROUNDED.
Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 83,829 hrs · 39,117 cycles
FLOORBEAM CORRODED AT STA 1153 RT SIDE. REMOVED DAMAGE REPAIRED INNER CHORD IAW SRM 53-00-07 AND 51-20-01. FLOORBEAM INNER CHORD, PN: BAC 1506-3123, CORROSION: 2. LOCATION: STA 1153, RBL 30 TO RBL 40; ACFT WAS GROUNDED.
Earlier reports · 2006–2011 · 33 reports
2011
Part: SKIN — CORRODED (FUSELAGE) · airframe 81,096 hrs · 37,811 cycles
FUSELAGE SKIN FOUND CORRODED AT STA 785.9 STR 38R. SKIN WAS REPAIRED IAW REA B653-59567 MR, AWG.
Part: RIB — GOUGED (LE SLAT) · airframe 81,096 hrs · 37,811 cycles
RIGHT WING L/E SLAT 405 CANTED RIB GOUGED SEVERAL AREAS. BLENDED GOUGED ORIG THICKNESS 0.100. REMAINING THICKNESS .083" BLENDOUT ACCEPTABLE IAW REA B657-59566, AWG.
Part: STRINGER — CRACKED (FUSELAGE) · airframe 81,096 hrs · 37,811 cycles
STRINGER CRACKED. REMOVED AND REPLACED STRINGER IAW REA B653-59548 AND BOEING SRM 53-00-03 FIG 201 REPAIR 1, AWG.
Part: SUPPORT — CRACKED (LT WING) · airframe 81,096 hrs · 37,811 cycles
LEFT WING UPPER T/E PANEL SUPPORT CRACKED FWD OF O/B FLAP AT O/B FLAP TRACK WS 825.2. FABBED NEW BRACKET FROM 7075-0 .063 PO 408455711 HEAT TREATED BRACKET TO 7075-76, LOCATED HOLES AND INSTALLED BRACKET IAW B767 SRM 51-40-02. GROUNDED.
Part: SKIN — GOUGED (VERTICAL STAB) · airframe 81,096 hrs · 37,811 cycles
VERTICAL STAB LOWER SKIN GOUGED ON RIGHT SIDE OF VERTICAL STAB FROM HORSE COLLAR. GOUGES ARE LOCATED JUST FWD AND AFT OF STA 1809 SKIN SPLICE. REMOVED DAMAGED SKIN PANELS, FABBED NEW SKIN PANELS FROM 7075T-6 .061 PER MMDS-04; SRM 53-80-01, FIGURE 201, REPAIR 3. REINSTALLED SKIN PANELS IAW BOEING 767-200 SRM 51-40-02, AWG.
Part: STRINGER — CRACKED (FUSELAGE) · airframe 81,096 hrs · 37,811 cycles
STRINGER S11L CRACKED JUST AFT OF STA 676. REPAIRED SECTION OF DAMAGED STRINGER WITH NEW STRINGER AND END CAP IAW REA B653-59549 AND B767 SRM 53-00-003, A/W/G.
Part: FRAME — CRACKED (COWLING) · airframe 81,096 hrs · 37,811 cycles
OUTBD CORE COWL DOUBLER CRACKED ON INSIDE NEAR EXHAUST DUCT. INSTALLED REPAIR DOUBLER IAW SRM 51-40-02 AND DRAWING 314T1210, WELDED REPAIRED DOUBLER IAW ABX PROCESS STANDARDS MANUAL CHAPTER 900-7 REV 49, AWG.
2010
Part: HYDRAULIC LINE — DEFECTIVE (RT MLG WW) · airframe 78,354 hrs · 36,643 cycles
LOST ALL CENTER HYDRAULIC QUANTITY. DEFERRED: 66591. REMOVED & INSTALLED HYD FLEX LINE IN RT W/W AT MAIN LANDING SELECTOR VALVE IAW AMMM 29-20-00 & 20-40-09-8. OPS & LEAK CHECK NORMAL. DEFERRED FOR TRACKING PER GMM CHAPTER 1 SECT 07.04 & MM 20-10-09-8. PLACARD INSTALLED.
Part: PRESSURE PANEL — CORRODED (LT MLG WW) · airframe 77,551 hrs · 36,276 cycles
CORROSION IN LEFT WHEEL WELL BETWEEN DRAIN LINES FOR CANTED PRESS PANEL. REPAIRED DAMAGE IAW REA B653-58758MR.
Part: ATTACH ANGLE — CRACKED (VERTICAL STAB) · airframe 77,551 hrs · 26,276 cycles
VERT STAB LWR ACCESS 324CLX RT LWR FIN/BODY ATTACH ANGLE CRACKED IN RADIUS. HIGH FREQ EDDY CURRENT VERIFIED IAW B NDT PART 6 51-00-19. REMOVED AND REPLACED RT LWR ATTACH ANGLE. INSTALLED WITH HI-LOKS IAW 767 SRM 51-40-02.
Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 77,551 hrs · 36,276 cycles
RT KEEL IS CORRODED ON LOWER O/B FLANGE STA 793. REMOVED N/P CHANNEL TO FOM. REMOVED CORROSION IAW 767 SRM 51-10-02. REPAIRED IAW REA B653-58777. RE-INSTALLED N/R CHANNEL IAW 767 SRM 51-40-02.
Part: SUPPORT — CORRODED (FUSELAGE) · airframe 77,551 hrs · 36,276 cycles
KEEL PANEL SUPPORT AT STA 910 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED SUPPORT IAW B767 SRM 51-40-02.
Part: FRAME — CRACKED (STRUT) · airframe 77,551 hrs · 36,276 cycles
NR 1 STRUT PANEL 437BL CUTOUT LOWER FRAME IS CRACKED AT FWD END. REMOVED AND REPLACED NR 1 STRUT LOWER FRAME OUTBOARD IN HYD ACCESS BAY IAW B767 SRM 51-40-02.
Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 77,551 hrs · 36,276 cycles
RT KEEL BEAM IS CORRODED AT BS 1002 UPPER FLANGE. CORROSION BEYOND LIMITS. REPAIRED IAW B767 SRM 53-50-12 FIG 201.
Part: FRAME — CRACKED (NR 1 STRUT) · airframe 77,551 hrs · 36,276 cycles
NR 1 STRUT PANEL 437BR CUTOUT LOWER FRAME IS CRACKED AT FWD END. REMOVED AND REPLACED FRAME IAW B767 SRM 51-40-02.
Part: SUPPORT BEAM — CRACKED (NACELLE) · airframe 77,551 hrs · 36,276 cycles
HYD BAY LWR SUPPORT BEAM ON INBOARD SIDE CRACKED AT FWD END. REPAIRED AREA IAW B767 REA B654-58745MR.
Part: SUPPORT BEAM — CRACKED (NACELLE) · airframe 77,551 hrs · 36,276 cycles
HYD BAY LOWER SUPPORT BEAM ON OUTBOARD SIDE CRACKED AND WORN AT FWD END. REPAIRED IAW REA B654-58745MR.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 77,551 hrs · 36,276 cycles
STA 742 HAS CORRODED SHEAR TIE ON AFT SIDE BETWEEN STRINGERS 39R AND 39L. REMOVED AND REPLACED SHEAR TIE IAW B767 SRM 51-40-02.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 77,551 hrs · 36,276 cycles
STA 742 HAS CORRODED SHEAR TIE ON AFT SIDE BETWEEN STRINGERS 39R AND 39L. REMOVED AND REPLACED SHEAR TIE IAW B767 SRM 51-40-02.
Part: STRUCTURE — CRACKED (NLG WW) · airframe 77,551 hrs · 36,276 cycles
THE RBL NOSE WHEEL WELL VERTICAL CHORD AT STA 287 IS CRACKED IN THE RADIUS LOCATED 11.75 INCHES BELOW CEILING STRUCTURE. REMOVED DAMAGED SECTION OF CHORD. REPAIRED IAW B767 SRM 51-70-12 FIG 1.
Part: STRUCTURE — CRACKED (NLG WW) · airframe 77,551 hrs · 36,276 cycles
LBL 25 NOSE WHEEL WELL VERTICAL CHORD AT STA 287 IS CRACKED APPROX .875 INCH IN LENGTH IN THE RADIUS. LOCATED 11.75 INCHES BELOW CEILING STRUCTURE. REMOVED DAMAGED SECTION OF CHORD. REPAIRED IAW B767 SRM 51-70-12 FIG 1.
Part: STRUCTURE — CRACKED (NLG WW) · airframe 77,551 hrs · 36,273 cycles
SUPPLEMENTAL INFORMATION - RBL 25 NOSE WHEEL WELL VERTICAL CHORD AT STA 387 IS CRACKED APPROX .5 INCH IN LENGTH IN THE RADIUS. LOCATED 11.75 INCHES BELOW CEILING STRUCTURE. - SUPPLEMENTAL INFO; REMOVED DAMAGED SECTION OF CHORD. REPAIRED IAW B767 SRM 51-70-12 FIG 1. P/N 141T2938-16.
Part: STRUCTURE — CRACKED (NLG WW) · airframe 77,551 hrs · 36,276 cycles
THE LBL 25 NOSE WHEEL WELL VERTICAL CHORD AT STA 287 IS CRACKED IN THE RADIUS. LOCATED 11.75 INCHES BELOW CEILING STRUCTURE. REMOVED DAMAGED SECTION OF CHORD. REPAIRED IAW B767 SRM CH 51-70-12 FIG 1.
2009
Part: SKIN — BULGED (FUSELAGE) · airframe 77,065 hrs · 36,053 cycles
FUSELAGE SKIN BULGE AT S6L AND STA 1307. REPAIRED IAW B767 SRM 53-00-03.
Part: CHARGER — INOPERATIVE (CABIN) · airframe 76,640 hrs · 35,856 cycles
SPARE EMERGENCY LIGHTING POWER SUPPLY (D170) INOP. DEFERRED: 64043, DEFERRED SPARE EMERGENCY LIGHTING POWER SUPPLY PER ABX GMM 01.07.04, INSTALLED PLACARD COD 27. CLEARED: 64043. REMOVED AND REPLACED BATTERY CHARGER ASSY AND BATTERY AT POSITION D170 IAW AMM 33-51-07-2, SYSTEM OPS CHECK GOOD.
Part: STIFFENER — CRACKED (PYLON) · airframe 77,551 hrs · 36,276 cycles
STIFFENER ON OUTBOARD MID INTERNAL PYLON ABOVE PNL 426BR, VIEWED LOOKING THROUGH PNL 442AL LOOKING OUTBOARD BY HYD SUPPORT IS CRACKED AND WORN. REMOVED AND REPLACED STIFFENER IAW B767 SRM 51-40-02 AND 51-10-02.
2008
Part: SKIN — CRACKED (L1 DOOR) · airframe 75,095 hrs · 35,199 cycles
AFT LOWER CORNER OF L1 DOOR CUTOUT HAD A CRACK IN OUTER SKIN LAYER. REPAIRED AFT LOWER CORNER OF L1 DOOR IAW B767 SRM 53-10-01, FIG 201 AND REA B653-57443. (A)
Part: SKIN — CRACKED (FUSELAGE) · airframe 75,095 hrs · 35,199 cycles
LOWER AFT CORNER OF R1 DOOR CUTOUT HAD CRACKS IN BOTH SKIN LAYERS. REPAIRED DOOR CORNER IAW B767 SRM 53-10-01. (A)
Part: SKIN — CRACKED (FUSELAGE) · airframe 75,095 hrs · 35,199 cycles
LOWER FORWARD OF R1 DOOR CUTOUT HAD A CRACK IN OUTER SKIN LAYER. REPAIRED LOWER FORWARD CORNER OF R1 DOOR IAW B767 SRM 53-10-01. (A)
Part: SKIN — CRACKED (FUSELAGE) · airframe 75,095 hrs · 35,199 cycles
LOWER AFT CORNER OF R1 DOOR CUTOUT HAD CRACKS IN BOTH SKIN LAYERS. REPAIRED DOOR CORNER IAW B767 SRM 53-10-01. (A)
2007
Part: CONNECTOR — LOOSE (VIBRATION SENSOR) · airframe 71,976 hrs · 34,272 cycles
DURING CRUISE, RIGHT ENGINE VIBRATION EXCEEDED INDICATION, BECAME INTERMITTENT. MADE PRECAUTIONARY LANDING AT KIX. FOUND N1 VIBRATION SENSOR CONNECTOR LOOSE, TIGHTENED CONNECTOR. PERFORMED FIM PROCEDURE 77-31-00. REMOVED AND REPLACED RIGHT AVM. BITE CHECK GOOD.
2006
Part: SENSOR — MISINSTALLED (LT MLG) · airframe 70,867 hrs · 33,899 cycles
AFTER TAKEOFF LANDING GEAR WOULD NOT RETRACT. FOUND LT GEAR TILT SENSOR'S IMPROPERLY INSTALLED. REMOVED REINSTALLED IAW 767 M/M 32-09-02. ADJUSTED LT & RT MAIN TILT SENSORS IAW 767 M/M 32-09-02, COMPLIED WITH GEAR SWING IAW 767 M/M 32-32-00 GEAR RETRACTION AND INDICATION CHECK NORMAL REF 33011-36/1 FOR PSEU TEST.
Part: FLIGHT DIR — MALFUNCTIONED (COCKPIT) · airframe 70,865 hrs · 33,897 cycles
ALL 3 FLIGHT DIRECTORS FAILED ON DESCENT INTO MIAMI AFTER LANDING FD'S CAME BACK. A/C IN MIA FOR C-CHECK DUE OUT 5/9/06. SCHEDULED FOR MOD AT IAI ON 5/28/06, DUE OUT 10/07/06.