N11
Registered owner: FEDERAL AVIATION ADMINISTRATION, OK (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| Flight Program Operations (RU3A) | Certificate holder | — | Matched by certificate designator |
| Federal Aviation Administration | Operator | on 2008-07-21 | Operator named in NTSB report |
Accident & incident history
Operated by Federal Aviation Administration (per NTSB report)
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.
8 reports on file, 2010-09-27 – 2018-02-08.
Part: WARNING HORN — ACTIVATED (MLG) · airframe 2,348 hrs · 1,774 cycles
GEAR WARNING AND RED LIGHT ILLUMINATED WHEN FULL FLAPS WERE EXTENDED. AFTER FOLLOWING THE CHECKLIST, THE WARNING HORN WAS SILENCED AND THE RED LIGHT WENT OUT. LANDED THE ACFT.
Part: CHANNEL — CRACKED (NR 2 NACELLE) · airframe 1,199 hrs · 671 cycles
DURING INSPECTION, FOUND NR 2 ENGINE OTBD FIRE SEAL CHANNEL CRACKED AT THE FOOT WHERE IT BOLTS TO THE LOWER AFT COWL.
Part: CHANNEL — CRACKED (NR 1 NACELLE) · airframe 1,199 hrs · 671 cycles
DURING INSPECTION, FOUND NR 1 ENGINE INBD FIRE SEAL CHANNEL CRACKED AT THE FOOT WHERE IT BOLTS TO THE LOWER AFT COWL.
Part: CHANNEL — CRACKED (NR 2 NACELLE) · airframe 1,199 hrs · 671 cycles
DURING INSPECTION, FOUND NR 2 ENGINE INBD FIRE SEAL CHANNEL CRACKED AT THE FOOT WHERE IT BOLTS TO THE LOWER AFT COWL.
Part: CHANNEL — CRACKED (NR 1 NACELLE) · airframe 1,199 hrs · 671 cycles
DURING INSPECTION, FOUND NR 1 ENGINE OTBD FIRE SEAL CHANNEL CRACKED AT THE FOOT WHERE IT BOLTS ATTACH TO THE LOWER AFT COWL.
Part: INLET — CRACKED (NR 1 ENGINE) · airframe 1,199 hrs · 671 cycles
DURING INSPECTION FOUND NR 1 ENGINE INLET CRACKED AT THE RIVET ATTACHING THE BRACKET FOR THE INLET HEAT DUCT. CRACKED WHERE THE INLET IS STARTING TO CURVE.
Part: CHANNEL — CHAFED (ELEVATOR) · airframe 319 hrs · 380 cycles
ELEVATOR MOVEMENT TO CERTAIN DISTANCE CAUSES POPPING SOUND IN EMPENNAGE. INVESTIGATION RESULTED IN FINDING THE ELEVATOR TRIM MOTOR TURNBUCKLE UPPER BOLT & NUT RUBBING AGAIN THE ELEVATOR RIGGING CHANNEL, CAUSING CHAFING.
Part: FLEX HOSE — BROKEN (INTAKE ANTI ICE) · airframe 195 hrs · 136 cycles
(UA2R) DURING ROUTINE INSP, FOUND RT ENGINE INBD HOTLIP HOSE BROKEN. INSTALLED NEW HOSE.