N191US
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.
6 reports on file, 2006-06-27 – 2012-04-25.
Part: LIGHT — INOPERATIVE (ROW 6) · airframe 78,216 hrs · 64,508 cycles
ROW NR 6 AISLE EMERGENCY LIGHT INOPERATIVE. MX REPLACED ROW NR 6 EMERGENCY LIGHT IAW MM 33-50-00. OPS CHECKS GOOD, NO DEFECTS NOTED.
Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 77,951 hrs · 64,293 cycles
WHILE PERFORMING A SERVICE CHECK, MX DISCOVERED THAT THE RT OVERWING EMERGENCY EXIT LIGHT WOULD NOT ILLUMINATE. (BULBS WERE GOOD) MX R & R THE RT OVERWING EMERGENCY EXIT LIGHT EMERGENCY BATTERY PACK IAW MM 33-50-0. THE SYS OPERATIONALLY CHECKED GOOD AND THE ACFT WAS RETURNED TO SERVICE.
Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 77,886 hrs · 64,247 cycles
FUSELAGE SKIN BULGING, CORROSION AT EDGE OF LAP, STR. 26RT, BS. 275-294.
Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 77,686 hrs · 64,071 cycles
WHILE THE ACFT WAS IN FOR MX, A BULGE WAS NOTICED ON THE EXTERNAL SKIN AT FRAME STA 218 BETWEEN LONGERONS 22R AND 23R. UPON FURTHER INVESTIGATION IT WAS DETERMINED THAT THE INTERNAL SKIN WAS CORRODED. THE CORRODED SECTION WAS REMOVED AND A REPAIR DOUBLER WAS INSTALLED IAW THE SRM 53-04, FIG 12B, SHEET 81.
Part: SKIN — CORRODED (LT ELEVATOR) · airframe 76,783 hrs · 63,366 cycles
LEFT ELEVATOR BOTTOM SURFACE AT STA XE209 TO OUTBOARD EDGE HAS CORROSION THROUGH THE SKIN WHICH COVERED A CIRCULAR AREA 1.5 INCH ACROSS. REPAIRED CORROSION IAW USA JET EA 96-51-02 USING DC-9 SRM CHAP 55 SECTION 3.
Part: SKIN — GOUGED (BS 121-158) · airframe 76,783 hrs · 63,366 cycles
GOUGE RUNNING FROM FS 121 TO 158 AT L19L TO L20L. GOUGE APPROX .25 INCH WIDTH AND .1 INCH DEPTH. REPAIRED GOUGE BY COLD WORKING AND INSTALLING EXTERNAL REPAIR DOUBLE IAW USA JET EA 06-53-247 AND 8110-3 FROM FLIGHT VEHICLES CONSULTING, INC DATED 6-1-06.