N485MC
Registered owner: UMB BANK TRUSTEE, UT (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
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.
138 reports on file, 2019-01-15 – 2026-07-29.
Part: PANEL — CORRODED (ZONE 600) · corrosion level 2 · airframe 113,499 hrs · 20,012 cycles
RHW L/E UPPER FIXED PANEL O/B EDGE NEAR #3 PYLON O/B FOUND CORROSION(<P>CHORD REPLACED AND INSTALLED AS PER RI-57-41-18383 REV A. NO FURTHER DEFECTS NOTED</P>)
Part: ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 113,499 hrs · 20,012 cycles
NR 2 PACK LOUVER ASSY AFT LOWER ANGLE CORROSION. ANGLE FABRICATED AS PER BOEING DWG 65B41701 AND PL AND NEW ANGLE HOLES TRANSFERRED AS PER SRM 51-40-05 AND NEW ANGLE INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOTED.
Part: ANGLE — CORRODED (ZONE 100) · airframe 113,499 hrs · 20,012 cycles
NR 1 PACK LOWER ASSY AFT LOWER SUPPORT ANGLE CORROSION. ANGLE FABRICATED AS PER BOEING DWG 65B41701 & PL AND NEW ANGLE HOLES TRANSFERRED AS PER SRM 51-40-05 AND NEW ANGLE INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOTED.
Part: BEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 113,499 hrs · 20,012 cycles
AFT CARGO DOOR INNER SURFACE LOWER CLOSEOUT BEAM SURFACE CORR FROM BS 1820 - 1920 SEVERAL PLACES. CORROSION AREA REMOVED IAW SRM 51-10-02 AND REPROTECTED IAW SRM 51-20-01, REWORK AREA MEASURED ORG 0.120", L: 4" X W: 20" X D: 0.011" WITHIN SRM 52-30-02-1A-1A ALLOWABLE DAMAGE 1 FIG 101 LIMITS. NO FURTHER DEFECTS NOTED.
Part: CHANNEL — CRACKED (ZONE 200) · airframe 113,499 hrs · 20,012 cycles
RT STA 840 UPPER DECK TENSION TIE FWD CHANNEL FOUND CRACK. TENSION TIE REPAIRED AS PER SRM 53-20-30-2R-1 REPAIR 1. NO FURTHER DEFECTS NOTED.
Part: RIB — CRACKED (ZONE 500) · airframe 113,499 hrs · 20,012 cycles
LHW L/E ILES 756.95 UPPER FIXED PNL RIB FOUND CRACK(<P>RIB CRACK AREA REPAIRED AS PER RI-57-41-18340 REV A. NO FURTHER DEFECTS NOTED</P>)
Part: STIFFENER — CRACKED (ZONE 500) · airframe 113,499 hrs · 20,012 cycles
STIFFENER CRACK AT LHS WLG W/W STA 1241 LBL 85.65 REAR SPAR WEB HAND O/J PUMP I/B AREA. STIFFENER FABRICATED AS BOEING DWG 65B10671 AND PL REV LTR AND NEW STIFFENER HOLES TRANSFERRED AS PER SRM 51-40-05 AND NEW STIFFENER INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOTED.
Part: PANEL — CRACKED (ZONE 100) · airframe 113,499 hrs · 20,012 cycles
AFT CARGO STA 1920 RH O/B WALKWAY FLOOR PANEL AFT CUTOUT FOUND 1EA CRACKED. PANEL CRACK AREA REPAIRED AS PER ATLAS AIR EA-4425A268 REV 1. NO FURTHER DEFECTS NOTED</P>)
Part: PROFILE — CRACKED (ZONE 200) · airframe 113,499 hrs · 20,012 cycles
M/D BS 1140 TO 1160 RHS O/B RBL 116" L PROFILE FASTENER HOLE FOUND CRACK(<P>ANGLE CRACK AREA REPAIRED AS PER RI-53-44-18392 REV A. NO FURTHER DEFECTS NOTED&NBSP;</P>)
Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 113,499 hrs · 20,012 cycles
AFT CARGO STA 1920 RT O/B WALKAWAY FLOOR PNL CUTOUT SUPPORT FOUND 1EA CRACKED. SUPPORT REPAIRED AS PER ATLAS AIR EA-4425A268 REV 1. NO FURTHER DEFECTS.
Part: STEP — CRACKED (ZONE 200) · airframe 113,499 hrs · 20,012 cycles
M/D BS 500 LHS LADDER #8 STEP ( COUNT FROM BOTTOM ) I/B WEB FWD AND AFT FOUND CRACK(<P>I/B WEB FWD AND AFT CRACK AREA REPAIRED AS PER RI-25-13-18348 REV A. NO FURTHER DEFECTS</P>)
Part: STEP — CRACKED · airframe 113,499 hrs · 20,012 cycles
M/D BS 500 LHS LADDER #7 STEP ( COUNT FROM BOTTOM ) I/B WEB FWD AREA FOUND CRACK(<P>WEB CRACK AREA REPAIRED AS PER RI-25-13-18347 REV A. NO FURTHER DEFECTS NOTED.
Part: PANEL — NICKED (ZONE 200) · airframe 113,499 hrs · 20,012 cycles
M/D LHS BS 1620 TO 1720 DADO PNL AFT EDGE FOUND NICKED. DADO PANEL NICK AREA REPAIRED AS PER RI-25-21-18349 REV A. NO FURTHER DEFECTS NOTED.
Part: ANGLE — CRACKED (ZONE 500) · airframe 113,499 hrs · 20,012 cycles
LHW L/E ILES APPROX 268.81 UPPER SUPPORT RIB AFT CORNER SPLICE FITTING FOUND CRACK. ANGLE REPLACED AND INSTALLED AS PER RI-57-41-18375 REV A. NO FURTHER DEFECTS NOTED.
Part: ANGLE — CRACKED (ZONE 600) · airframe 113,499 hrs · 20,012 cycles
RHW L/E ILES APPROX 268.81 UPPER SUPPORT RIB AFT AREA. ANGLE REPLACED AND INSTALLED IAW RI-57-41-18376 REV A. NO FURTHER DEFECTS NOTED.
Part: LONGERON SPLICE — CRACKED (ZONE 100) · airframe 113,499 hrs · 20,012 cycles
RH BS 1480 LONGERON EXTENSION FITTING INTERIOR SPLICE FITTING 1EA HOLE FOUND CRACK(<P>CRACK FASTENER HOLE REPAIRED AS PER RI-53-60-18406 REV A. NO FURTHER DEFECTS NOTED</P>)
Part: FRAME — CHAFED (ZONE 400) · airframe 113,499 hrs · 20,012 cycles
NR 4L CORE COWL NR 2 FRAME PATCH FOUND CHAFING ( COUNT FROM FWD )(<P>FRAME REPAIRED AS PER SRM 54-41-02-2R-2 REPAIR 2 FIG 201. NO FURTHER DEFECT NOTED</P>)
Part: FITTING — CORRODED (ZONE 600) · corrosion level 2 · airframe 113,499 hrs · 20,012 cycles
RT WING T/E L/G SUPPORT BEAM APPROX 200 UPPR CHORD FWD SUPPORT ROD O/B FITTING FOUND CORROSION WEAR #5 FLAP TRACK. FITTING ASSY FABRICATED AS PER BOEING DWG 69B11720 AND PL REV LTR A AND NEW FITTING ASSY HOLES TRANSFERRED AS PER SRM 51-40-05 AND NEW FITTING ASSY INSTALLED AS PER SRM 51-40-02.</P>)
Part: DOUBLER — CHAFED (ZONE 100) · airframe 113,499 hrs · 20,012 cycles
RH STA 980 UNDERWING LONGERON AREA FOUND REPAIR DOUBLER ADJ SKIN CHAFING(<P>SKIN REPAIRED AS PER RI-53-20-18357 REV B. NO FURTHER DEFECTS NOTED&NBSP;</P>)
Part: DOUBLER — CRACKED (ZONE 200) · airframe 113,499 hrs · 20,012 cycles
RHS STA 2524.4 UPPER LOBE DOUBLER ALONG THE RADIUS FOUND 1EA CRACK APPROX 8" IN LENGTH(<P>CRACK AREA REPAIRED AS PER ATLAS AIR EO 4453A224 REV 10 PART 2 AND RI-53-80-18477 REV A. NO FURTHER DEFECTS NOTED</P>)
Part: DOUBLER — CORRODED · corrosion level 2 · airframe 113,499 hrs · 20,012 cycles
NR 3 FUEL AFT BOOST PUMP FOUND CUTOUT DOUBLER CORROSION. DOUBLER FABRICATED AS PER BOEING DWG 65B19560 AND PL, NEW DOUBLER HOLES TRANSFERRED AS PER SRM 51-40-05 AND NEW DOUBLER INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOTED</P>)
Part: FITTING — CRACKED (ZONE 100) · airframe 113,499 hrs · 20,012 cycles
RH BS 1480 LONGERON EXTENSION FITTING RADIUS AREA FOUND 1EA CRACK(<P>LONGERON EXTENSION FITTING REPLACED AS PER ATLAS AIR EO 4453A818 REV 20 PART 4. NO FURTHER DEFECTS NOTED</P>)
Part: SPAR — CRACKED (ZONE 500) · airframe 113,499 hrs · 20,012 cycles
LHW - UPPER WING T/E MOST I/B FIXED PNL SUPPORT P/N 65B11532-41 CRACK(<P>SUPPORT P/N 65B11532-41 REPLACED AS PER RI-57-20-18384 REV A. NO FURTHER DEFECTS NOTED</P>)
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 113,499 hrs · 20,012 cycles
M/D BS 1020 TO 1070 LBL 11 SEAT TRACK RHS FLANGE BOTTOM SIDE FOUND CORROSION(<P>SEAT TRACK REPLACED AS PER SRM 51-10-02 AND NEW SEAT TRACK HOLES TRANSFERRED AS PER SRM 51-40-05 AND NEW SEAT TRACK INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOTED</P>)
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 113,499 hrs · 20,012 cycles
M/D STA 1200 LBL 105 BELOW FLOOR INTERCOSTAL WEB FOUND CRACKED(<P>WEB REPAIRED AS PER RI-53-40-18377 REV A. NO FURTHER DEFECTS NOTED</P>)
Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 113,499 hrs · 20,012 cycles
M/D STA 1200 RBL 105" BELOW FLOOR INTERCOSTAL WEB FOUND CRACKED(<P>WEB CRACK AREA REPAIRED AS PER RI-53-40-18382 REV A. NO FURTHER DEFECTS NOTED</P>)
Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 113,499 hrs · 20,012 cycles
M/D BS 1220 RHS O/B BELOW FLOOR INTERCOSTAL WEB FOUND CRACK(<P>WEB CRACK AREA REPAIRED AS PER RI-53-40-18381 REV A. NO FURTHER DEFECTS NOTED</P>)
Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 113,499 hrs · 20,012 cycles
M/D BS 1220 LHS O/B BELOW FLOOR INTERCOSTAL WEB FOUND CRACK(<P>WEB CRACK AREA REPAIRED AS PER RI-53-40-18378 REV A. NO FURTHER DEFECTS NOTED</P>)
Part: WEB — CORRODED (ZONE 200) · airframe 113,499 hrs · 20,012 cycles
M/D BS 1180 RHS O/B BELOW FLOOR INTERCOSTAL WEB FOUND CRACK(<P>WEB CRACK AREA REPAIRED AS PER SRM 51-10-02 AND NEW WEB HOLES TRANSFERRED AS PER SRM 51-40-05 AND NEW WEB INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOTED</P>)
Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 113,499 hrs · 20,012 cycles
M/D BS 1180 LHS O/B BELOW FLOOR INTERCOSTAL WEB FOUND CRACK(<P>INTERCOSTAL WEB REPAIRED AS PER RI-53-40-18379 REV A. NO FURTHER DEFECTS NOTED</P>)
Part: WEB — CORRODED (ZONE 200) · airframe 113,499 hrs · 20,012 cycles
LOWER CHORD FASTENER HOLE CRACK AT M/D BS 1180 LH O/B BELOW FLOOR INTERCOSTAL WEB LOWER AREA(<P>LOWER CHORD REPLACED AS PER SRM 51-10-02 AND NEW CHORD HOLES TRANSFERRED AS PER SRM 51-40-05 AND NEW CHORD INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOTED.
Part: SKIN — DAMAGED (ZONE 300) · airframe 113,499 hrs · 20,012 cycles
VERTICAL STABILIZER THE TOP AFT TIP FOUND ELECTRICAL ARCING DAMAGE APPROX 4CM IN DIAMETER(<P>FAIRING DAMAGE AREA REPAIRED AS PER RI-55-31-18434 REV A. NO FURTHER DEFECTS NOTED</P>)
Part: FAIRING — DELAMINATED (ZONE 600 FLAP) · airframe 113,499 hrs · 20,012 cycles
RHW I/B FORE FLAP L/E FAIRING FOUND DELAMINATION(<P>PERFORMED COMPOSITE HOT BOND REPAIR AT DELAMINATION AREA AS PER SRM 51-70-07 PAR 5A (1). NO FURTHER DEFECTS NOTED</P>)
Part: FAIRING — DELAMINATED (ZONE 600) · airframe 113,499 hrs · 20,012 cycles
RHW I/B FORE FLAP L/E FAIRING FOUND DELAMINATION(<P>PERFORMED COMPOSITE HOT BOND REPAIR AT DELAMINATION AREA AS PER SRM 51-70-07 PAR 5A (1). NO FURTHER DEFECTS NOTED</P>)
Part: SKIN — DELAMINATED (ZONE 600) · airframe 113,499 hrs · 20,012 cycles
RHW I/B MID FLAP UPPER T/E FOUND DELAMINATION(<P>PERFORMED COMPOSITE HOT BOND REPAIR AT DELAMINATION AREA AS PER SRM 51-70-07 PAR 5A (1). NO FURTHER DEFECTS NOTED</P>)
Part: SKIN — DELAMINATED (ZONE 600) · airframe 113,499 hrs · 20,012 cycles
RHW I/B MID FLAP UPPER T/E FOUND DELAMINATION(<P>PERFORMED COMPOSITE HOT BOND REPAIR AT DELAMINATION AREA AS PER SRM 51-70-07 PAR 5A (1). NO FURTHER DEFECTS NOTED</P>)
Part: SKIN — DELAMINATED (ZONE 600) · airframe 113,499 hrs · 20,012 cycles
RHW I/B MID FLAP UPPER T/E FOUND DELAMINATION(<P>PERFORMED COMPOSITE HOT BOND REPAIR AT DELAMINATION AREA AS PER SRM 51-70-07 PAR 5A (1). NO FURTHER DEFECTS NOTED</P>)
Part: SKIN — DELAMINATED (ZONE 600) · airframe 113,499 hrs · 20,012 cycles
RHW O/B FORE FLAP L/E FAIRING FOUND DELAMINATION(<P>PERFORMED COMPOSITE HOT BOND REPAIR AT DELAMINATION AREA AS PER SRM 51-70-07 PAR 5A (1). NO FURTHER DEFECTS NOTED</P>)
Part: SKIN — DELAMINATED (ZONE 600) · airframe 113,499 hrs · 20,012 cycles
RHW O/B FORE FLAP UPPER T/E FOUND DELAMINATION(<P>PERFORMED COMPOSITE HOT BOND REPAIR AT DELAMINATION AREA AS PER SRM 51-70-07 PAR 5A (1). NO FURTHER DEFECTS NOTED</P>)
Part: SKIN — DELAMINATED (ZONE 500) · airframe 113,499 hrs · 20,012 cycles
LHW O/B FORE FLAP UPPER T/E FOUND DELAMINATION(<P>PERFORMED COMPOSITE HOT BOND REPAIR AT DELAMINATION AREA AS PER SRM 51-70-07 PAR 5A (1). NO FURTHER DEFECTS NOTED</P>)
Part: FAIRING — DELAMINATED (ZONE 500) · airframe 113,499 hrs · 20,012 cycles
LHW I/B MID FLAP L/E FAIRING FOUND DELAMINATION(<P>PERFORMED COMPOSITE HOT BOND REPAIR AT DELAMINATION AREA AS PER SRM 51-70-07 PAR 5A (1). NO FURTHER DEFECTS NOTED</P>)
Part: FAIRING — DELAMINATED (ZONE 500) · airframe 113,499 hrs · 20,012 cycles
LHW I/B FORE FLAP L/E FAIRING FOUND DELAMINATION(<P>PERFORMED COMPOSITE HOT BOND REPAIR AT DELAMINATION AREA AS PER SRM 51-70-07 PAR 5A (1). NO FURTHER DEFECTS NOTED</P>)
Part: FAIRING — DELAMINATED (ZONE 500) · airframe 113,499 hrs · 20,012 cycles
LHW I/B FORE FLAP L/E FAIRING FOUND DELAMINATION(<P>PERFORMED COMPOSITE HOT BOND REPAIR AT DELAMINATION AREA AS PER SRM 51-70-07 PAR 5A (1). NO FURTHER DEFECTS NOTED</P>)
Part: FAIRING — DELAMINATED (ZONE 500) · airframe 113,499 hrs · 20,012 cycles
LHW I/B FORE FLAP L/E FAIRING FOUND DELAMINATION(<P>PERFORMED COMPOSITE HOT BOND REPAIR AT DELAMINATION AREA AS PER SRM 51-70-07 PAR 5A (1). NO FURTHER DEFECTS NOTED</P>)
Part: FAIRING — DELAMINATED (ZONE 500) · airframe 113,499 hrs · 20,012 cycles
LHW I/B FORE FLAP L/E FAIRING FOUND DELAMINATION(<P>PERFORMED COMPOSITE HOT BOND REPAIR AT DELAMINATION AREA AS PER SRM 51-70-07 PAR 5A (1). NO FURTHER DEFECTS NOTED</P>)
Part: CHANNEL — CRACKED (ZONE 200) · airframe 113,499 hrs · 20,012 cycles
L/H STA 720 UPPER DECK TENSION TIE FWD CHANNEL UPR FLANGE CRACKED. TENSION TIE REPAIRED AS PER SRM 53-20-30-2R-1 REPAIR 1. NO FURTHER DEFECTS NOTED.
Part: FRAME — CRACKED (ZONE 100) · airframe 113,499 hrs · 20,012 cycles
1EA CRACK FOUND ON BS 1000 STR 38R - STR 39R APPROX 0.750". CHORD CRACK AREA REPAIRED AS PER ATLAS AIR EO 4453A506 REV 10 PART 4. NO FURTHER DEFECTS NOTED.
Part: STRUCTURE — CORRODED (ZONE 600) · corrosion level 2 · airframe 113,499 hrs · 20,012 cycles
RHW STA 1241 RH CENTER O/J PUMP CUTOUT FOUND CORROSION(<P>CORROSION AREA REPAIRED AS PER RI-57-10-18355 REV A. NO DEFECTS NOTED</P>)
Part: STRUCTURE — CORRODED (ZONE 500) · corrosion level 2 · airframe 113,499 hrs · 20,012 cycles
LHW STA 1241 CETNER LH O/J PUMP CUTOUT FOUND CORROSION(<P>WEB CORROSION AREA REPAIRED AS PER RI-57-10-18352 REV A. NO FURTHER DEFECTS NOTED</P>)
Part: FRAME — CRACKED (ZONE 200) · airframe 113,499 hrs · 20,012 cycles
LH STA 720 UPPER DECK FRAME 1EA FASTENER HOLE CRACK. CRACK FASTENER HOLE REPAIRED AS PER ATLAS AIR EO 4453A301 REV 12 ITEM 4F. NO FURTHER DEFECTS NOTED.
Part: WEB — CRACKED (RUDDER) · airframe 113,499 hrs · 20,012 cycles
RUDDER STA 207.6 THE WEB FOUND CRACKED, 3CM LENGTH AT LT FWD CORNER. WEB REPAIRED IAW RI-55-40-18393 REV A. NO FURTHER DEFECTS NOTED.
Part: WEB — CRACKED (ZONE 200) · airframe 113,499 hrs · 20,012 cycles
M/D STA 1200 LBL 105 - LBL 109 BELOW FLOOR INTERCOSTAL WEB FWD LWR CHORD ( 2EA ) FASTENER HOLES CRACK(<P>LOWER CHORD REPAIRED AS PER RI-53-40-18377 REV A. NO FURTHER DEFECTS NOTED</P>)
Part: SKIN — DELAMINATED (ZONE 500 K FLAP) · airframe 113,499 hrs · 20,012 cycles
LEFT WING INBD FORE FLAP UPPER T/E FOUND DELAMINATED PERFORMED COMPOSITE HOT BOND REPAIR AT DELAMINATION AREA IAW SRM 51-70-07 PAR 5A (1). NO FURTHER DEFECTS NOTED</P>)
Part: SKIN — DELAMINATED (ZONE 500) · airframe 113,499 hrs · 20,012 cycles
LHW I/B FORE FLAP UPPER T/E FOUND DELAMINATION(<P>PERFORMED COMPOSITE HOT BOND REPAIR AT DELAMINATION AREA AS PER SRM 51-70-07 PAR 5A (1). NO FURTHER DEFECTS NOTED</P>)
Part: SKIN — DEBONDED (ZONE 500) · airframe 113,499 hrs · 20,012 cycles
LHW #1 SPOILER FOUND DISBOND(<P>PERFORMED METAL HOT BOND REPAIR AT DISBOND AREA AS PER&NBSP;HX RI NO.RI-57-73-18361 REV.A. NO FURTHER DEFECTS NOTED</P>)
Part: SKIN — DEBONDED (ZONE 500) · airframe 113,499 hrs · 20,012 cycles
RHW I/B AFT FLAP UPPER O/B PANEL PREVIOUS REPAIR DOUBLER FOUND DISBOND(<P>PERFORMED METAL HOT BOND REPAIR AT DISBOND AREA AS PER HX RI-57-53-18374 REV A. NO FURTHER DEFECTS NOTED</P>)
Part: CHANNEL — CRACKED (ZONE 200) · airframe 113,499 hrs · 20,012 cycles
STA 900 LH UPPER DECK TENSION TIE AFT CHANNEL EA FASTENER HOLE CRACK(<P>TENSION TIE REPAIRED AS PER SRM 53-20-30-2R-1 REPAIR 1 AND RI-53-20-18410 REV A. NO FURTHER DEFECTS NOTED</P>)
Part: FRAME — CRACKED (ZONE 200) · airframe 113,499 hrs · 20,012 cycles
STA 900 LH UPPER DECK FRAME 1EA FASTENER HOLE CRACK(<P>FRAME REPAIRED AS PER RI-53-20-18410 REV A. NO FURTHER DEFECTS NOTED</P>)
Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 113,499 hrs · 20,012 cycles
LOWER CHORD 2EA FASTENER HOLES CRACK AT M/D STA 1220 RH O/B BELOW FLOOR INTERCOSTAL WEB FWD LOWER AREA(<P>LOWER CHORD REPAIRED AS PER RI-53-40-18381 REV A.NO FURTHER DEFECTS NOTED&NBSP;&NBSP;</P>)
Part: FITTING — CRACKED (ZONE 200) · airframe 113,499 hrs · 20,012 cycles
M/D BS 1920 LBL 107" TO LBL 116" SUPPORT WATER DAM FTG CRACK(<P>SUPPORT WATER DAM FTG REPAIRED AS PER RI-53-60-18432 REV A. NO FURTHER DEFECTS NOTED</P>)
Part: SUPPORT — DAMAGED (ZONE 100) · airframe 113,499 hrs · 20,012 cycles
FX AIR COND BAY #2 PACK HEAT EXCHANGER FWD I/B SUPPORT TRIANGLE PLATE MOUNT BOLT HOLE ELONGATED(<P>LOCAL FABRICATED PLATE P/N 69B40167-1 AS PER RI-21-52-18421 REV A AND BOEING DRAWING 69B40167. NO FURTHER DEFECTS NOTED</P>)
Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 113,499 hrs · 20,012 cycles
LOWER CHORD 3EA FASTENER HOLE CRACK AT M/D STA 1200 RH BELOW FLOOR INTERCOSTAL WEB FWD LOWER AREA(<P>LOWER CHORD REPAIRED AS PER RI-53-40-18382 REV A. NO FURTHER DEFECTS NOTED</P>)
Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 113,499 hrs · 20,012 cycles
LOWER CHORD ( 2EA ) FASTENER HOLES CRACK AT M/D STA 1220 LH O/B BELOW FLOOR INTERCOSTAL WEB FWD LOWER.(<P>LOWER CHORD REPAIRED AS PER RI-53-40-18378 REV A. NO FURTHER DEFECTS NOTED</P>)
Part: BEARING RACE — DAMAGED (ZONE 100) · airframe 113,499 hrs · 20,012 cycles
REWORK LH BLG O/B TRUNNION BEARING RACE(<P>PERMANENT REPAIR TO USE BAC5701 TYP 11 CL2 IN LIEU OF SOPM 20-42-05 TYP 11 CL2 AS PER RI-32-13-18385 REV B. NO FURTHER DEFECTS NOTED&NBSP;</P>)
Part: BUSHING — DAMAGED (ZONE 100) · airframe 113,499 hrs · 20,012 cycles
REWORK LH BLG I/B TRUNNION BUSHING(<P>PERMANENT REPAIR TO USE BAC5701 TYP 11 CL2 IN LIEU OF SOPM 20-42-05 TYP 11 CL2 AS PER RI-32-18362 REV B. NO FURTHER DEFECTS NOTED</P>)
Part: BUSHING — DAMAGED (TRUNNION) · airframe 113,499 hrs · 20,012 cycles
REWORK RH BLG I/B TRUNNION BUSHINGS(<P>PERMANENT REPAIR TO USE BAC5701 TYP 11 CL2 IN LIEU OF SOPM 20-42-05 TYP 11 CL2 AS PER RI-32-13-18363 REV B. NO FURTHER DEFECTS NOTED&NBSP;</P>)
Part: SKIN — DAMAGED (ZONE 200) · airframe 113,499 hrs · 20,012 cycles
6EA EXISTING FASTENER HOLES SIZE LARGER THAN BOEING SB 747-53A2651 R1, FASTENERS INSTALL HOLES SIZE AT FX RH TOP SKIN APPROX STA 2537(<P>6EA FASTENERS INSTALLED AS PER RI-53-80-18417 REV A. NO FURTHER DEFECTS NOTED&NBSP;</P>)
Part: FRAME — CRACKED (ZONE 200) · airframe 113,499 hrs · 20,012 cycles
LEFT BS 840 UPPER DECK FRAME ONE EACH FASTENER HOLE CRACKED. FRAME CRACK AREA REPAIRED AS PER RI-53-20-18364 REV A. NO FURTHER DEFECTS NOTED
Part: CHANNEL — CRACKED (ZONE 200) · airframe 113,499 hrs · 20,012 cycles
LH STA 840 UPPER DECK TENSION TIE FWD CHANNEL FOUND CRACK(<P>TENSION TIE REPAIRED AS PER SRM 53-20-30-2R-1 REPAIR 1 AND RI-53-20-18364 REV A. NO FURTHER DEFECTS NOTED</P>)
Part: CHANNEL — CRACKED (ZONE 200) · airframe 113,499 hrs · 20,012 cycles
RH STA 880 UPPER DECK TENSION TIE FWD CHANNEL 2EA FASTENER HOLES CRACK(<P>TENSION TIE REPAIRED AS PER SRM 53-20-30-2R-1 REPAIR 1 AND RI-53-20-18365 REV A. NO FURTHER DEFECTS NOTED</P>)
Part: FRAME — CRACKED (ZONE 200) · airframe 113,499 hrs · 20,012 cycles
RH STA 880 UPPER DECK FRAME FOUND 2EA FASTENER HOLES CRACK(<P>FRAME REPAIRED AS PER RI-53-20-18365 REV A. NO FURTHER DEFECTS NOTED</P>)
Part: CHANNEL — CRACKED (ZONE 200) · airframe 113,499 hrs · 20,012 cycles
LH STA 880 UPPER DECK TENSION TIE FWD CHANNEL 1EA FASTENER HOLE CRACK(<P>TENSION TIE REPAIRED AS PER SRM 53-20-30-2R-1 REPAIR 1 AND RI-53-20-18366 REV A. NO FURTHER DEFECTS NOTED</P>)
Part: FRAME — CRACKED (ZONE 200) · airframe 113,499 hrs · 20,012 cycles
LH STA 880 UPPER DECK FRAME FOUND 1EA FASTENER HOLE CRACK(<P>FRAME CRACK AREA REPAIRED AS PER RI-53-20-18366 REV A. NO FURTHER DEFECTS NOTED</P>)
Part: SPAR — CRACKED (ZONE 500) · airframe 113,499 hrs · 20,012 cycles
LWH UPPER WING T/E MOST I/B FIXED PNL SUPPORT P/N 65B11532-47 CRACK(<P>SUPPORT P/N 65B11532-47 REPLACED AS PER RI-57-20-18405 REV A. NO FURTHER DEFECTS NOTED</P>)
Part: STIFFENER — CRACKED (ZONE 600) · airframe 113,499 hrs · 20,012 cycles
RHW L/E CAVITY APPROX ILES 620 SUPPORT RIB I/B #3 STIFFENER FOUND CRACK ( COUNT FROM FWD ) NEAR #3 PYLON I/B(<P>STIFFENER FABRICATED AS PER BOEING DWG 65B15696 PL REV LTR B AND RI-57-41-18368 REV A AND NEW STIFFENER HOLES TRANSFERRED AS PER SRM 51-40-05 AND NEW STIFFENER INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOTED</P>)
Part: STIFFENER — CRACKED (ZONE 500) · airframe 113,499 hrs · 20,012 cycles
LHW L/E CAVITY APPROX ILES 620 SUPPORT RIB ATT #3 STIFFENER FOUND CRACK ( COUNT FROM FWD )(<P>STIFFENER FABRICATED AS PER BOEING DWG 65B15696 PL REV LTR B AND RI 57-41-18367 REV A AND NEW STIFFENER HOLES TRANSFERRED AS PER SRM 51-40-05 AND NEW STIFFENER INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOTED</P>)
Part: CHANNEL — CRACKED (ZONE 200) · airframe 113,499 hrs · 20,012 cycles
LH STA 920 UPPER DECK TENSION TIE FWD CHANNEL 1EA FASTENER HOLE CRACK(<P>TENSION TIE REPAIRED AS PER SRM 53-20-30-2R-1 REPAIR 1. NO FURTHER DEFECTS NOTED</P>)
Part: DOUBLER — CRACKED (BS 820 FRAME) · airframe 113,499 hrs · 20,012 cycles
RH STA 820 U/D TENSION TIE ATT. FRAME DOUBLER 2EA FASTENER HOLES CRACKED. FRAME DOUBLER REPLACED AS PER SRM 51-10-02 AND NEW FRAME DOUBLER HOLES TRANSFERRED AS PER SRM 51-40-05 AND NEW FRAME DOUBLER INSTALLED AS PER SRM 51-40-02.& NO FURTHER DEFECTS NOTED.
Part: TENSION TIE — CRACKED (ZONE 200) · airframe 113,499 hrs · 20,012 cycles
RH STA 820 UPPER DECK TENSION TIE FWD 2EA FASTENER HOLES CRACK(<P>TENSION TIE REPAIRED AS PER SRM 53-20-30-2R-1 REPAIR 1.&NBSP;NO FURTHER DEFECTS NOTED</P>)
Part: CHANNEL — CRACKED (ZONE 200) · airframe 113,499 hrs · 20,012 cycles
RH STA 740 UPPER DECK TENSION TIE FWD CHANNEL 2EA FASTENER HOLES CRACK(<P>TENSION TIE REPAIRED AS PER SRM 53-20-30-2R-1 REPAIR 1.&NBSP;<SPAN>NO FURTHER DEFECTS NOTED</SPAN></P>)
Part: CHANNEL — CRACKED (ZONE 200) · airframe 113,499 hrs · 20,012 cycles
RH STA 800 UPPER DECK TENSION TIE AFT CHANNEL 1EA FASTENER HOLE CRACK(<P>TENSION TIE REPAIRED AS PER SRM 53-20-30-2R-1 REPAIR 1.&NBSP;<SPAN>NO FURTHER DEFECTS NOTED</SPAN></P>)
Part: CHANNEL — CRACKED (ZONE 200) · airframe 113,499 hrs · 20,012 cycles
RH STA 900 UPPER DECK TENSION TIE AFT CHANNEL 1EA FASTENER HOLE CRACK(<P>TENSION TIE REPAIRED AS PER SRM 53-20-30-2R-1 REPAIR 1.&NBSP;<SPAN>NO FURTHER DEFECTS NOTED</SPAN></P>)
Part: CHANNEL — CRACKED (ZONE 200) · airframe 113,499 hrs · 20,012 cycles
RH STA 760 UPR DECK TENSION TIE FWD CHANNEL 2EA FASTENER HOLES CRACK(<P>TENSION TIE REPAIRED AS PER SRM 53-20-30-2R-1 REPAIR 1.&NBSP;<SPAN>NO FURTHER DEFECTS NOTED</SPAN></P>)
Part: CHANNEL — CRACKED (ZONE 200) · airframe 113,499 hrs · 20,012 cycles
STA 860 LH UPPER DECK TENSION TIE AFT CHANNEL 2EA FASTENER HOLES CRACK. TENSION TIE REPAIRED AS PER SRM 53-20-30-2R-1 REPAIR 1. NO FURTHER DEFECTS NOTED
Part: CHANNEL — CRACKED (ZONE 200) · airframe 113,499 hrs · 20,012 cycles
STA 820 LH UPPER DECK TENSION TIE AFT CHANNEL 1EA FASTENER HOLE CRACK. TENSION TIE REPAIRED AS PER SRM 53-20-30-2R-1 REPAIR 1. NO FURTHER DEFECTS NOTED.
Part: CHANNEL — CRACKED (ZONE 200) · airframe 113,499 hrs · 20,012 cycles
STA 780 LH UPPER DECK TENSION TIE FWD CHANNEL ONE EACH FASTENER HOLE CRACKED. TENSION TIE REPAIRED AS PER SRM 53-20-30-2R-1 REPAIR 1. NO FURTHER DEFECTS NOTED.
Part: CHANNEL — CRACKED (ZONE 200) · airframe 113,499 hrs · 20,012 cycles
RH STA 860 UPPER DECK TENSION TIE FWD CHANNEL 1EA FASTENER HOLE CRACKED TENSION TIE REPAIRED AS PER SRM 53-20-30-2R-1 REPAIR 1. NO FURTHER DEFECTS.
Part: CHANNEL — CRACKED (ZONE 200) · airframe 113,499 hrs · 20,012 cycles
RH BS 720 UPPER DECK TENSION TIE AFT CHANNEL 1EA FASTENER HOLE CRACKED. TENSION TIE REPAIRED AS PER SRM 53-20-30-2R-1 REPAIR 1. NO FURTHER DEFECTS NOTED.
Part: CHANNEL — CRACKED (ZONE 200) · airframe 113,499 hrs · 20,012 cycles
LH STA 760 UPPER DECK TENSION TIE FWD CHANNEL FOUND 2EA FASTENER HOLES CRACKED. TENSION TIE REPAIRED AS PER SRM 53-20-30-2R-1 REPAIR 1. NO FURTHER DEFECTS NOTED.
Part: CHANNEL — CRACKED (ZONE 200) · airframe 113,499 hrs · 20,012 cycles
STA 740 LH UPPER DECK TENSION FWD CHANNEL FOUND FASTENER HOLE CRACKED. TENSION TIE REPAIRED AS PER SRM 53-20-30-2R-1 REPAIR 1. NO FURTHER DEFECTS NOTED.
Part: FITTING — DAMAGED · airframe 113,499 hrs · 20,012 cycles
3EA FASTENER HOLES OVERSIZED TO 0.437" LARGER THAN SB 747-53A2651 R1 FASTENER HOLES SIZE 0.391" - 0.395"(<P>FTG 3EA FASTENER INSTALLED AS PER RI-53-80-18417 REV A. NO FURTHER DEFECTS NOTED</P>)
Part: BEAM — CRACKED (ZONE 400) · airframe 113,499 hrs · 20,012 cycles
RHW L/E NEAR NO.3 PYLON O/B D-BEAM UPPER CHORD FOUND CRACK(<P>UPPER CHORD REPAIRED AS PER SRM 57-41-13-2R-2 REPAIR 2 FIG 201.</P>)
Part: VALVE — FAULTED · airframe 113,190 hrs · 19,962 cycles
DIVERSION FOR BLEED #4 STATUS MESSAGE, #3 BLEED DEFFERED. REPLACED BROKEN TERMINAL (EICAS BLEED 4) ON #4 HIGH PRESS BLEED VALVE #1 STUD IAW SWP 20-30-00. R/R #3 ENG PRV IAW AMM 36-11-19. OPS AND LEAK CHECK PASSED, PERFORMED HP ENG RUN PER 71-00-00. OPS CHECK OK, NO FAULTS. R/R PRV CONTROLLER PER AMM 36-11-20. LEAK CHECK PASSED,
Part: AILERON SYS — DEFLECTION · airframe 113,132 hrs · 19,950 cycles
UPON LANDING, ACFT REQUIRED NEARLY FULL RT AILERON DEFLECTION DURING ROLLOUT TO KEEP WINGS LEVEL. WINDS WERE SUCH THAT LT AILERON DEFLECTION SHOULD HAVE BEEN REQUIRED. SUSPECT A POSSIBLE SPOILER OR LE FLAP ISSUE. PERFORMED C/B RESET & SPEED BRAKE GROUND OPS CHK IAW AMM 27-62-00/501 & 57-57-02, OPS TEST NORMAL.& DUE TO REPEAT & PREVIOUS CREW DESCRIPTION OF EVENT, CURRENT CREW REQUESTS MORE T/S & A MORE DEFINITIVE FIX/FIND. LP 2123136 M2: PERFORMED GVI OF L/E FLAPS WITH FLAPS & SLATS FULLY EXTENDED, L/E, FLAP TRACK FAIRING, SLATS. NO VISUAL DEFECTS NOTED. IAW AMM 22-11-00, 27-88-00 & 27-81-00. FURTHER T/S REQ. LP 2123137 M3-5: PERFORMED OPS CHK OF NR 6 BRAKE IAW AMM 32-44-00. BRAKE IS FREE & OPS NORMAL. FURTHER T/S REQUIRED. PERFORMED DVI OF SPOILER SURFACES TO LINKAGE. SPOILERS HAVE NO SLACK & OPS NORMAL IAW AMM 57-57-00 & 57-57-02 & 27-62-00. NO FAULTS PRESENT & CANNOT PRODUCE AN UNAIRWORTHY CONDITION. PERFORMED SEVERAL FLT CONTROL TESTS IAW AMM 27-00-01 & RON CHECKLIST T2115 (APU POWER). NO DEFECTS NOTED. OPS CHKD GOOD.
Earlier reports · 2019–2025 · 44 reports
2025
Part: THERMAL SWITCH — FAULTED (ZONE 400) · airframe 111,839 hrs · 19,766 cycles
CLIMBING OUT OF 8000FT BLD DUCT LEAK L CAUTION MSG/ BLEED FAMV ENG 4. REF FIM 36-11 TASK 985 & WDM 26-18-13. T/S & WIRE CHK, FOUND THERMAL SW S907 AT FAULT. R & R THERMAL SWITCH IAW AMM 26-18-02 & IPC 26-18-02-01, ITEM 420. FIRE TEST RESULT PASSED, APU RUNNING WITH LT & RT BLEED, OK FOR 30 MINUTES, NO MSG NOTED.
Part: BULKHEAD WEB — CRACKED (ZONE 100) · airframe 111,077 hrs · 19,658 cycles
CRACK - PFM MOD PER SB 747-53A2837 AT STA 2598 FND BULKHEAD RH SIDE WEB AND AFTER CHORD FASTENER HOLE CRACK(<P>1. ACCOMPLISHED EI NO.T2025A53M-2100 REV. 4. 2. JOB COMPLETED AND CONDITION CHK NORMAL</P>)
Part: PANEL — CRACKED (ZONE 100) · airframe 110,067 hrs · 19,518 cycles
RH NWW SIDE PANEL WL150, BETWEEN STA 300 AND STA 320 FOUND 1 EA FASTENER HOLE CRACKED.(<P>NWW STA 320 WL150 SIDE PANEL 1 EA FASTENER HOLE CRACK AREA REPAIRED AND 1 EA STIFFENER REPLACED IAW RI-53-10-17693 REV. A. NO FURTHER DEFECTS NOTED.</P>)
2024
Part: PANEL — DAMAGED (ZONE 200) · airframe 107,343 hrs · 19,106 cycles
FWD CGO STA 662 RBL 42" TORQUE BOX PANEL FOUND PUNCH HOLES.(<P>FWD CGO STA 662 RBL 42" TORQUE BOX PANEL REPAIRED IAW RI-53-12-17162 REV.A. NO FURTHER DEFECTS NOTED</P>)
Part: TRUNNION — CORRODED (LT MLG) · airframe 105,484 hrs · 18,797 cycles
FOUND LH BLG INBD TRUNNION LWR FITTING CORROSION.(<P>1. REMOVE THE CORROSION AREA IAW SRM 53-40-90-2R-1 REV 100 2. ACCOMPLISHED EGAT EI T2024A32M-678 REV 1 REPAIR CORROSION DAMAGE ON THE CAP FITTING OF LH AND RH BODY LANDING GEAR INBOARD TRUNNION VERTICAL SUPPORT FITTING ASSY. 3. CONDITION CHECK NORMAL.</P>)
Part: SCREW — INTERFERENCE (BS 560) · airframe 105,484 hrs · 18,797 cycles
FND EXISTING SCREW INTERFERES WITH WIRE AT STA 560 NEAR RBL 65(<P>1. ACCOMPLISH EI T2024A53M-1060 REV 1 2. JOB COMPLETED AND CONDITION CHECK NORMAL</P>)
Part: DOOR — CRACKED (L1) · airframe 105,484 hrs · 18,797 cycles
CRACK - LOWER SIDE CORNER CRACK AT L1 ENTRY DOOR(<P>1. REMOVED AFFECTED FASTENERS IAW SRM 51-40-02-0G-0 REV 100. 2. ACCOMPLISHED JOB IAW EI T2024A52M-858 REV 1. 3. INSTALLED AFFECTED FASTENERS IAW SRM 51-40-02-0G-0 REV 100, DWG 65B01836 SH2 REV AB AND 65B01836 SH23 REV E. 4. CONDITION CHECK NORMAL AND JOB COMPLETED.&NBSP;</P>)
Part: WEB — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 105,484 hrs · 18,797 cycles
CORROSION - WEB, L/H HST T/E CAVITY STA 381.8 AREA ACCESS PNL 334PBL(<P>1. REMOVED CORROSION WEB IAW SRM 51-40-02-0G-0 REV 100. 2. FABRICATE WEB IAW WORKSHEET 40288. 3. INSTALL FABRICATE WEB IAW SRM 51-40-02-0G-0 REV 100 AND DWG 287U8202 SH2 REV A; 284U7037 SH7 REV- ; 65B03682 SH2 REV C. 3. CONDITIONAL CHECK NORMAL AND JOB COMPLETED.</P>)
Part: FRAME — CRACKED (BS 1480 LBL 110) · airframe 105,484 hrs · 18,797 cycles
CRACK ON FRAME WEB OF STA 1480 NEAR LBL 110 AND WL 150(<P>1. REMOVED AFFECTED FASTERNERS TO GET ACCES IAW 51-40-02-0G-0 REV 100 2. REPAIRED DAMAGE AREA IAW W/S 40241 AND EI T2024A53M-807 REV 1. 3. INSTALLED FASTENERS IAW SRM 57-40-02-0G-0 REV 100, DWG 65B15085 SH34 REV C, 65B15085 SH8 REV R, 65B15085 SH38 REV B AND 65B15085 SH40 REV F 4. CONDITION CHECK NORMAL AND JOB COMPLETED.</P>)
Part: BRACKET — CORRODED (WINGLET RIB) · corrosion level 2 · airframe 105,484 hrs · 18,797 cycles
LEFT WINGLET, RIB BRACKET CORROSION WBL 1243.750(<P>1. REMOVE DAMAGE PART IAW SRM 51-40-02-0G-0 REV 100. 2. INSTALL NEW PART IAW SRM 51-40-02-0G-0 REV 100 AND DWG 11245700 SHEET 1 REV C 3. CONDITION CHECK NORMAL AND JOB COMPLETED.</P>)
Part: SEAT TRACK — CORRODED (BS 1655-1565) · airframe 105,484 hrs · 18,797 cycles
FND FLOOR SEAT TRACK BRK AT M/D STA 1655~1665 RBL 98.58(<P>1. REPAIR DAMAGE AREA IAW WORKSHEET 40276, EI T2024A53M-775 REV 1, DWG 65B38251 SH 62 REV A & SH 66 REV -. 2. JOB COMPLETED AND CONDITIONAL CHECK NORMAL.</P>)
Part: STRUCTURE — CRACKED · airframe 105,484 hrs · 18,797 cycles
CRACK - LWR CHORD, R/H H.S.T TIP 347R PNL LWR CHORD, STAB BL 421.5(<P>1. REPAIRED DAMAGE AREA IAW WORKSHEET 40295 2. JOB COMPLETED & NO FURTHER DEFECTS NOTED</P>)
Part: TRUNNION — CORRODED (RT MLG) · airframe 105,484 hrs · 18,797 cycles
FOUND RH BLG INBD TRUNNION LWR FITTING CORROSION.(<P>1. REMOVE THE CORROSION AREA IAW SRM 53-40-90-R-1 REV 100. 2. ACCOMPLISHED EGAT EI T2024A32M-678 REV 1 REPAIR CORROSION DAMAGE ON THE CAP FITTING OF LH AND RH BODY LANDING GEAR INBOARD TRUNNION VERTICAL SUPPORT FITTING ASSY 3. CONDITION CHECK NORMAL</P>)
Part: BRACKET — CORRODED (RT MLG WW) · corrosion level 2 · airframe 105,484 hrs · 18,797 cycles
CORROSION - BRACKET, RH WING GEAR W/W CENTER WALL HYD TUBE SUPPORT BRACKET, STA 1301(<P>1. REMOVE DAMAGE BRACKET IAW SRM 51-40-02-0G-0 REV 100 2. FABRICATE NEW BRACKET IAW WORK SHEET 40263 3. INSTALLED NEW BRACKET IAW SRM 51-40-02-0G-0 REV 100 AND BOEING DWG 272U4428 SHEET 3 REV 3. JOB COMPLETED AND CONDITIONAL CHECK NORMAL.</P>)
Part: SKIN — CHAFED (LT AILERON) · airframe 105,484 hrs · 18,797 cycles
LH WING INBD AILERON OTBD TE SKIN CHAFING WORN(<P>1) PERFORM REPAIR OF CHAFING WORN SKIN DAMAGE AT LH WING INBD AILERON TE OTBD SIDE UPPER SURFACE. PLEASE REFER TO THE JOB CARD ATTACHING FOR DETAILED REWORK INFO. REF SRM 57-60-01-0I-1 REV 100, SRM 57-60-01-2R-1 REV 100 & SRM 51-70-06-0G-0 REV 100. 2) CONDITION CHECK IS GOOD</P>)
Part: UNKNOWN — CORRODED (UNKNOWN) · corrosion level 2 · airframe 105,484 hrs · 18,797 cycles
CORROSION - FOUND 20 EA CORROSION DAMAGE WHEN PERFORM SB 747-53A878(<P>1. PERFORM EI T2024A53M-753 REV 0, EI T2024A53M-824 REV 0, DWG 140U1480, SH37 REV A, SH38 REV D, DWG 144U0105, SH2 REV C, DWG 140U099, SH20 REV A, SH23 REV C, SH24 REV C, DWG 144U0104, SH5 REV B, DWG 144U0102, SH6 REV D & SH3 REV E 2. ACCOMPLISH EI T2024A53M-824 REV 1 3. JOB COMPLETED.
Part: SPAR — CRACKED (HORIZONTAL STAB) · airframe 105,484 hrs · 18,797 cycles
HOLE CRACK ON RH HST UPR REAR SPAR CHORD NEAR RBL43.(<P>1.REPAIR DAMAGE AREA IAW EI T2024A55M-712 REV 2 2. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)
Part: SEAT TRACK — CORRODED (BS 1820-1840) · corrosion level 2 · airframe 105,484 hrs · 18,797 cycles
FND FLOOR STRUCTURE SEAT TRACK CORROSION AT M/D STA 1820~1840 LBL 75.92.(<P>ACCOMPLISHED WORKSHEET 40277, EI T2024A53M-776 REV 1, WORKSHEET ATTACHED TO W/O 9350399(912) & EI ATTACHED TO W/O 9350399(912). 2. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)
Part: SEAT TRACK — CORRODED (BS 1850 RBL 11) · corrosion level 2 · airframe 105,484 hrs · 18,797 cycles
FND M/D CGO FLOOR STRUCTURE SEAT TRACK CORROSION AT STA 1850 RBL 11.33(<P>1. REPAIR DAMAGE AREA IAW WORK SHEET 40300, EI T2024A53M-877 REV 1, DWG 65B38253 SH 46 REV AL, SH 56 REV A, SH57 REV -, SH49 REV -, SH50 REV A & SH51 REV A. 2. JOB COMPLETED AND CONDITIONAL CHECK NORMAL. PN 65B38273-4</P>)
Part: SEAT TRACK — CORRODED (BS 1842-1858) · corrosion level 2 · airframe 105,484 hrs · 18,797 cycles
FND FLOOR STRUCTURE SEAT TRACK CORROSION AT M/D STA 1842 ~1858, RBL 98.58.(<P>1. REPAIR DAMAGE AREA IAW WORK SHEET 40278, EI T2024A53M-778 REV 1, BOEING DWG 65B38251, SH 62 REV A & SH 66 REV -. 2. JOB COMPLETED AND CONDITIONAL CHECK NORMAL.</P>)
Part: NONE — NONE (NONE) · airframe 105,484 hrs · 18,797 cycles
FOUND AN EXISTING REPAIR ON L1 DOOR UPPER MAIN SILL FROM STA 440 ~ STA 480.(<P>1. ACCOMPLISHED EI T2024A53M-806, REV 0 2. EXISTING REPAIR WAS COVERED BY EO 4457A291, REV 7 REFER RAM FORM N485MC-24-04 ISSUE 3. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)
Part: WEB — CORRODED (LT ELEVATOR) · corrosion level 2 · airframe 105,484 hrs · 18,797 cycles
CORROSION- WEB, L/H HST T/E CAVITY ELEV STA 331.8(<P>1. REMOVED DAMAGED PART IAW SRM 51-40-02-0G-0 REV 100. 2. INSTALL NEW PART IAW SRM 51-40-02-0G-0 REV 100 AND DWG 65B03681 SHEET 2 REV E. 3. CONDITIONAL CHECK NORMAL AND JOB COMPLETED.</P>)
Part: SEAT TRACK — CRACKED (BS 1480) · airframe 105,484 hrs · 18,797 cycles
FND FLOOR STRUCTURE SUBSTITUTE TRACK CRACK AT M/D STA 1480 LBL 75.92(<P>1. REPAIR DAMAGE AREA IAW WORKSHEET 40266, DWG 65B38251 SH32 REV-, SH75 REV-, DWG 144U0802 SH3 REV B 2. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)
Part: SEAT TRACK — CRACKED (BS 990) · airframe 105,484 hrs · 18,797 cycles
FND FLOOR STRUCTURE SUBSTITUTE TRACK CRACK AT M/D STA 990 LBL 75.92(<P>1. REPAIR DAMAGE AREA IAW WORK SHEET 40265 AND DWG 65B38250 SH17 REV A, SH9 REV B, AND DWG 65B16004 SH4 REV A 2. JOB COMPLETED AND CONDITION CHECK NORMAL</P>)
Part: SEAT TRACK — CRACKED (BS 980-1000) · airframe 105,484 hrs · 18,797 cycles
FND FLOOR STRUCTURE SUBSTITUTE TRACK CRACK AT M/D STA 980 ~ 1000 RBL 75.92(<P>1. REPAIR DAMAGE AREA IAW WORKSHEET 40264, DWG 65B38250 SH9 REV B, DWG 65B16004 SH4 REV A & SH3 REV- 2. JOB COMPLETED AND CONDITION CHECK NORMAL</P>)
Part: SEAT TRACK — CORRODED (BS 1870 LBL76) · corrosion level 2 · airframe 105,484 hrs · 18,797 cycles
FND FLOOR STRUCTURE SEAT TRACK CORROSION AT M/D STA 1870 LBL 75.92.(<P>1. REPAIR DAMAGE AREA IAW WORKSHEET 40277, EI T2024A53M-776 REV 1, BOEING DWG 65B38251 SH 62 REV A, SH 32 REV - & DWG 65B38288 SH2 REV A. 2. JOB COMPLETED AND CONDITIONAL CHECK NORMAL.</P>)
Part: SKIN — DEBONDED (RT WING AILERON) · airframe 105,484 hrs · 18,797 cycles
DISBOND - SKIN RH WING INBD AILERON OTBD LWR EDGE(<P>1) PERFORM REPAIR OF DISBOND SKIN DAMAGE AT RH WING INBD AILERON TE OTBD SIDE LWR SURFACE. PLEASE REFER TO THE JOB CARD ATTACHING FOR DETAILED REWORK INFO. REF SRM 57-60-01-0I-1 REV 100, SRM 57-60-01-2R-1 REV 100 & SRM 51-70-06-0G-0 REV 100. 2) CONDITION CHECK IS GOOD</P>)
Part: SKIN — WORN (LT WING TE FLAP) · airframe 105,484 hrs · 18,797 cycles
WORN - SKIN LH OTBD FORE FLAP RH TOP PANEL FASTENER HOLE, FROM LH EDGE 18" AND FROM AFT EDGE 0.5"(<P>1) PERFORM REPAIR OF WORN SKIN DAMAGE AT LH WING OTBD FORE FLAP UPPER SKIN PANEL ASSY (PN 65B01915-427) IAW EGAT EI T2024A57M-838 REV 1. 2) CONDITION CHECK IS GOOD</P>)
Part: SEAT TRACK — CORRODED (BS 2164-2169) · airframe 105,484 hrs · 18,797 cycles
FND FLOOR STRUCTURE SEAT TRACK CORROSION AT M/D STA 2164~2169. RBL 11.33(<P>1. REPAIR DAMAGE AREA IAW WORK SHEET 40281, DWG 65B38253 SH 1 REV AP, SH 51 REV A, SH 52 REV A, SH 53 REV -, SH54 REV - & SH55 REV A. 2. JOB COMPLETED AND CONDITIONAL CHECK NORMAL.</P>)
2023
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 103,857 hrs · 18,523 cycles
RH WING WHEEL WELL FOUND CORROSION NEXT TO DRAG BRACE(<P>1) REMOVED CORRODED "Z" CHORD FROM PANEL ASSY (65B11640-120) IAW B747 SRM 51-40-02 (WAITING FOR NEW PART) ("Z" CHORD IS MATERIAL LOSS). 2) RECEIVED STOCK CHORD, FABRICATED Z CHORD (DRILLED, TRIMMED, ALODINE & PRIMER) AND INSTALLED NEW Z CHORD ON PANEL ASSY (65B11640-120) IAW B747 DWG 65B11514 REV G & SRM 51-40-02. 3) RE-INSTALLED PANEL ASSY (65B11640-120) AT RH WING (WING STA 129 TO 225) JUST AFT OF WING LANDING GEAR IAW SRM 51-40-02. 4) NO FURTHER DEFECTS NOTED</P>)
Part: FILTER — UNKNOWN (UNKNOWN) · airframe 101,998 hrs · 18,193 cycles
ENG 4 FUEL FILTER STATUS MESSAGE, CAUTION MSG-INTERMITTENT.(<P>REMOVED & REPLACED ENG #4 FUEL FILTER PER AMM 73-11-03. OPS CHECK GOOD</P>)
2022
Part: FITTING — LOOSE · airframe 99,666 hrs · 17,812 cycles
DURING RH LANDING GEAR RETRACT ACTUATOR REPLACEMENT, FOUND FITTING ASSY CORRODED(<P>REMOVED AND REPLACED CORRODED FITTING ASSY AT RH WING UPPER PAENL PER SRM 51-40-02-06-0</P>)
2020
Part: FRAME — CRACKED (FUSELAGE) · airframe 89,227 hrs · 16,119 cycles
M/D STA 2231 LH S-20L TO 21L FRAME WEB FOUND CRACK.(<P>M/D STA 2231 LH S-20L TO 21L FRAME WEB REPAIRED AS PER SRM 53-60-15-2R-3 REPAIR 3 FIG 203 DETAIL 3.</P>)
Part: STRUCTURE — CORRODED (TE FLAP) · airframe 89,227 hrs · 16,119 cycles
LHW O/B MID FLAP T/E #587NT UPPER CHORD FOUND CORROSION.(<P>LHW O/B MID FLAP T/E #587NT UPPER CHORD CORROSION AREA REPAIRED AS PER SRM 57-53-02-1A-1.</P>)
Part: STRUCTURE — CORRODED (RT WING) · airframe 89,227 hrs · 16,119 cycles
RHW I/B FIXED PANEL T/E UPPER CHORD FOUND CORROSION.(<P>RHW I/B FIXED PANEL T/E UPPER CHORD REPAIRED AS PER RI-57-51-13990 REV A.</P>)
Part: ACCESS PANEL — CORRODED (TE FLAP) · airframe 89,227 hrs · 16,119 cycles
RHW I/B MID FLAP ACCESS PANEL ( #677JT ) FOUND CORROSION.(<P>RHW I/B MID FLAP ACCESS PANEL ( #677JT ) CORROSION AREA REPAIRED AS PER SRM 57-53-01-1A-0.</P>)
Part: SKIN — CRACKED (FUSELAGE) · airframe 89,227 hrs · 16,119 cycles
FX SKIN STA 1720 - 1740 RH S-39R-S-40R FOUND CORROSION CRACK.(<P>FX SKIN STA 1720 - 1740 RH S-39R-S40R SKIN REPAIRED AS PER RI-53-00-13995 REV A.</P>)
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 89,227 hrs · 16,119 cycles
M/D STA 1220 - 1250 LBL11 AND RBL 11 SEAT TRACK FLANGE FOUND CORROSION.(<P>M/D STA 1220 - 1250 LBL 11 AND RBL 11 SEAT TRACK FLANGE CORROSION AREA REPAIRED AS PER SRM 53-00-52-1A-1.</P>)
Part: LIGHT — INOPERATIVE (CREW DOOR) · airframe 89,227 hrs · 16,119 cycles
U/D EMER DOOR ( SLIDE ) LT RH CREW DOOR FWD FOUND NOT ILLUMINATED.(<P>LT ASSY REPLACED AND LIGHT TEST NORMAL IAW AMM 33-51-05.</P>)
Part: SKIN — CORRODED (FUSELAGE) · airframe 89,227 hrs · 16,119 cycles
FX SKIN STA 1720 - 1740 RH S-43R - S-45R FOUND CORROSION.(<P>FX SKIN STA 1720 - 1740 RH S-43R - S-45R SKIN REPAIRED AS PER RI-53-00-13995 REV A.</P>)
Part: ACCESS PANEL — CORRODED (TE FLAP) · airframe 89,227 hrs · 16,119 cycles
RHW I/B MID FLAP UPPER ACCESS PANEL ( 677KT ) FOUND CORROSION.(<P>RHW I/B MID FLAP UPPER ACCESS PANEL ( 677KT ) CORROSION AREA REPAIRED AS PER SRM 57-53-01-1A-0.</P>)
2019
Part: PDU — MALFUNCTIONED (LE SLATS) · airframe 86,943 hrs · 15,719 cycles
"FLAP CONTROL" AND "LE MULTI DRIVE" EICAS STATUS MESSAGES. PERFORMED FIM TASK 27-88/836, CHECKING WIRING. NO FAULTS FOUND. REMOVED AND REPLACED L1 LE PDU THEN OPS CHECKED OK PER AMM 27-81-03/201.
Part: SEAT TRACK — CRACKED (BS 2020) · airframe 86,581 hrs · 15,655 cycles
MAIN DECK, BS 2020, RBL 98 SEAT TRACK FOUND CRACKED. THE SEAT TRACK WAS REPAIRED IAW RI-53-00-13621 REV A, AND SRM 53-00-52-2R-6 REPAIR 6.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 84,824 hrs · 15,374 cycles
UPPER DECK EMERGENCY CEILING LIGHTS INOP(<P>RELAMPED UPPER DECK EMERGENCY LIGHTS AND TESTED PER MM 33-21-07-962-001</P>)