N173CR
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.
19 reports on file, 2016-05-11 – 2016-07-13.
Part: COVER — CORRODED (BS 478) · corrosion level 2 · airframe 84,114 hrs · 21,389 cycles
RIGHT O/B TORQUE BOX COVER BS 478 HAS CORROSION
Part: SKIN — CORRODED (WS 616) · corrosion level 2 · airframe 84,114 hrs · 21,389 cycles
EVIDENCE OF CORROSION AT WS 616 JUST FORWARD OF NR 7 POSITON FORWARD FAIRING
Part: ACCESS PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 84,114 hrs · 21,389 cycles
TORQUE BOX ACCESS PANEL SHOWS EVIDENCE OF CORROSION, FWD TORQUE BOX, STA 544-566, FWD CARGO COMPARTMENT, LBL 20-39, PANEL.
Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 84,114 hrs · 21,389 cycles
CORROSION ON INTERNAL FUSELAGE SKIN AT BS 443, STR 33L.
Part: FRAME — CORRODED (BS 1197) · corrosion level 2 · airframe 84,114 hrs · 21,389 cycles
CORROSION ON FRAME UPPER CHORD BS 1197 + 66 LBL 20.
Part: FAILSAFE — CORRODED (BS 955) · corrosion level 2 · airframe 84,114 hrs · 21,389 cycles
RIGHT WING AFT SPAR WING ROOT FAIL SAFE STRAP CORRODED AT FUSE, BS 955.5.
Part: FRAME — CORRODED (BS 1197) · corrosion level 2 · airframe 84,114 hrs · 21,389 cycles
CORROSION ON FRAME UPPER CHORD BS 1197 LBL 20.
Part: FRAME — CORRODED (BS 1197) · corrosion level 2 · airframe 84,114 hrs · 21,389 cycles
CORROSION ON FRAME UPPER CHORD BS 1197 RBL 20.
Part: STRINGER SPLICE — CORRODED (BS 434) · corrosion level 2 · airframe 84,114 hrs · 21,389 cycles
STRINGER SPLICE CORRODED AT BS 434, STR 37L.
Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 84,114 hrs · 21,389 cycles
CORROSION AT REAR SPAR APPROXIMATELY WS 965 UPPER SURFACE OF RT WING.
Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 84,114 hrs · 21,389 cycles
LEFT WING UPPER SKIN IS CORRODED AT APPROXIMATELY WBL 101, 25" FWD OF REAR SPAR.
Part: FLOOR PANEL — CORRODED (BS 1263-1255) · corrosion level 2 · airframe 84,114 hrs · 21,389 cycles
AFT CARGO BAY RT BS 1263-1255 FLOOR PANEL HAS CORROSION ON BOTH SIDES, K-08, TORQUE BOX.
Part: FLOOR PANEL — CORRODED (CARGO) · corrosion level 2 · airframe 84,114 hrs · 21,389 cycles
CENTER AFT CARGO PIT FLOOR PANEL AT 6 O'CLOCK HAS CORROSION ON BOTH SIDES, K-07, TORQUE BOX.
Part: STRAP — CRACKED (BS 1725) · airframe 84,114 hrs · 21,389 cycles
BS 1725.5 BULKHEAD OUTER CHORD STRAP CRACKED AT STR 7R.
Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 84,114 hrs · 21,389 cycles
CORROSION AT FWD SPAR APPROXIMATELY WS 990 RT UPPER WING SURFACE.
Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 84,114 hrs · 21,389 cycles
CORROSION AT APPROXIMATELY WS 610 L-1, RT WING UPPER SURFACE.
Part: BULKHEAD — CRACKED (BS 1809) · airframe 84,114 hrs · 21,389 cycles
BS 1809.5 BULKHEAD FWD CHORD AT THE END OF STR 7L HAS APPROXIMATELY 2" CRACK IN THE RADIUS.
Part: SKIN — CRACKED (BS 1724) · airframe 84,114 hrs · 21,389 cycles
CRACKED SKIN BS 1724, STR 22L.
Part: STIFFENER — CRACKED (BS 287) · airframe 84,114 hrs · 21,389 cycles
MAIN EQUIPMENT VERTICAL STIFFENER BS 287, ABOVE S39L CRACKED.