N360CM
Registered owner: MULLER CLIFFORD L, MN (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.
7 reports on file, 2020-02-28 – 2020-03-17.
Part: INTERCOSTAL — DAMAGED (FUSELAGE) · airframe 99,843 hrs · 16,625 cycles
PERMANENT REPAIR NEEDS INSTALLED AT STA 1043 RBL 54.75-RBL 74.75 MAIN DECK FLOOR PANEL AND INTERCOSTAL DAMAGE. INSTALLED INTERIM REPAIR AT STA 1043 RBL 54-75-74.75 MAIN DECK FLOOR TRACK DAMAGE IAW B767-300 SRM 51-40-05 51-40-02 P.9 AND AMES INTERM REPAIR DOC 47400REA06.
Part: SKIN — CRACKED (FUSELAGE) · airframe 99,843 hrs · 16,625 cycles
AIRCRAFT GROUNDED FOR ATI-767 C CHECK 18. IN COMPLIANCE OF TASK CARD 53-730-00-01. "GVI EXTERIOR SECTION 48 LH", THE FOLLOWING DISCPRENCY WAS IDENTIFIED: LH AFT FUSELAGE EXTERIOR SKIN IS CRACKED STA 1654.5 BETWEEN STRINGER 3L-4L.FABRICATED AND INSTALLED REPAIR DOUBLERS AND FILLERS 2 DOUBLER, 2 DOUBLER 3L FILLER, 4L FILLER AND PER B767 SRM 53-80-01. FABRICATED AND INSTALLED REPAIR DOUBLERS AND FILLERS 2 DOUBLER, 2 DOUBLER 3L FILLER, 4L FILLER AND PER B767 SRM 53-80-01.
Part: SKIN — CRACKED (FUSELAGE) · airframe 99,843 hrs · 16,625 cycles
L/H AFT FUSELAGE EXTERIOR SKIN IS CRACKED STA 1654.5 BETWEEN STRINGER 3L-4L. REMOVED DAMAGE ON L/H AFT FUSELAGE SKIN AT STA 1554E PER B767 SRM 58-80-01 REPAIR 4. CAT A REPAIR NO OTHER ACTIONS REQ IAW B767SRM 51-00-06
Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 99,843 hrs · 16,625 cycles
AIRCRAFT GROUNDED FOR ATI-767 C CHECK 18. IN COMPLIANCE OF TASK CARD 51-041-02-AD-2003-19-09 "CANTED PRESSURE BULKHEAD CAVITY CLEANING" THE FOLLOWING DISCREPANCY WAS IDENTIFIED: RIGHT WHEEL WELL PRESSURE DECK IS CRACKED .350 AT BS 972, RBL 15. DAMAGE IS OUT OF LIMITS. REPAIRED RWW PRESSURE DECK IAW B767 SRM 53-50-51.
Part: PRESSURE DECK — DENTED (RT MLG WW) · airframe 99,843 hrs · 16,625 cycles
THE RIGHT WHEEL WELL PRESSURE DECK IS DENTED AT BS 972, RBL 15. ACCESS IS THROUGH THE CABIN FLOOR PANEL. DAMAGE OUT OF LIMITS REPAIRED IAW B767 SRM 53-50-51 REPAIR 1
Part: SKIN — CRACKED (FUSELAGE) · airframe 99,843 hrs · 16,625 cycles
AIRCRAFT GROUNDED FOR ATI-767 C CHECK 18. IN COMPLIANCE OF TASK CARD 53-730-00-02 "GVI EXTERIOR SECTION 48 RH SIDE" THE FOLLOWING DISCREPANCY WAS IDENTIFIED: AFT EXTERIOR FUSELAGE SKIN IS CRACKED 4.50" AT STA 1620 14R. DAMAGED AREA REMOVED IAW B767 SRM 53-80-01 REPAIR 7 DETAIL VII, DAMAGE AREA CUTOUT HFEC IAW B767 NDTM PART 6 51-00-19. NO DEFECTS NOTED AT THIS TIME. -1 DOUBLER AND -2 FILLER FABRICATED IAW B767 SRM 53-80-01 REPAIR 7 PARA 4. ADDITIONALLY, DOUBLER FILLER INSTALLED IAW B767 SRM 53-80-01
Part: SKIN — CRACKED (FUSELAGE) · airframe 99,843 hrs · 16,625 cycles
AFT EXTERIOR FUSELAGE SKIN IS CRACKED STA 1620 STRINGER 14R