Safety record in brief:1 NTSB accident (substantial damage, Feb 2026)1 AD may apply12 service difficulty reports
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The flight crew’s failure to maintain adequate clearance from the blast fence during taxi to the runway for departure, and their inadequate inspection of the airplane after it contacted the blast fence.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for ERA26LA130)
These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2018-07-13 | Landing Gear | May 15, 2018 | Airframe (680A)Serial numbers per UTC Service Bulletins 2-1706-1-32-1 Rev 1 and 2-1675-32-2 Rev 1 (brake assembly serial numbers). Only with: Equipped with brake assembly P/N 2-1706-1 (Model 510) or P/N 2-1675-1 (Models 680/680A) with serial number listed in table 1 of the applicable UTC service bulletin. |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.
RIGHT ELEVATOR HINGE BROKE CAUSING THE ELEVATOR TO SEPARATE FROM THE AIRCRAFT. REPLACED ELEVATOR ASSY. OPS CHECK GOOD. IAW AMM 55-20-05
From FAA Service Difficulty Reports; matched by N-number and serial number.CABIN DOOR OPEN CAS MESSAGE DISPLAYED AFTER SHUTTING MAIN CABIN DOOR. WHILE ON THE PHONE WITH MAINTENANCE, WE WENT THROUGH THEIR PROCEDURE AND OUR PROCEDURE WITH NO SUCCESS. WE THEN SHUT EVERYTHING DOWN PULLED THE BATTERIES WAITED 30 SECONDS TURNED EVERYTHING BACK ON, MESSAGE REMAINED. CHECK DOORS…
From FAA Service Difficulty Reports; matched by N-number and serial number.SECOND FLIGHT OF THE DAY. RIGHT ENGINE STARTED NORMALLY. LEFT ENGINE AT GROUND IDLE HAD A NOTICABLE HARMONIC HUM / VIBRATION (SIMILAR TO A RUMBLE STRIP ON THE SIDE OF THE ROAD AT SLOW SPPED). VIBRATION DID CHANGE WITH CHANGE IN RPM. NO ABNORMAL INDICATIONS NOTED. NO VISIBLE DISCRPANCIES NOTED.…
From FAA Service Difficulty Reports; matched by N-number and serial number.THE EMER LIGHTS DO NOT ILLUMINATE WHEN PLACED IN THE ON POSITION. WE RAN THE QRH AND WE STILL DO NOT HAVE EMER LIGHTS WHEN PLACED IN ON POSITION. WHEN IN ARM, ALL LIGHTS ILLUMINATE EXCEPT THE OVERHEAD LIGHT IN LAV, THE FLOOR LIGHT IN LAV AND THE EXIT LIGHT ON BULKHEAD OUTSIDE LAV. CORRECTIVE…
From FAA Service Difficulty Reports; matched by N-number and serial number.FUEL MOTIVE VLV R AMBER CAS: ENROUTE WHEN CROSSFEED SELECTED LEFT TANK TO RIGHT ENGINE THE AMBER CAS MEASAGE FUEL MOTIVE VLV R ILLUMINATED. CORRECTIVE ACTION REMOVED RH FUEL MOTIVE CHECK VALVE PN 9914716-1 SN N/A AND REPLACED WITH NEW FUEL MOTIVE CHECK VALVE PN 9914716-1 S/N AS PER CESSNA MODEL…
From FAA Service Difficulty Reports; matched by N-number and serial number.RH ENGINE THRUST REVERSER MOUNTING FLANGE CORRODED BETWEEN 3 AND 9 O'CLOCK POSITIONS. NO WORK IS REQUIRED AT THIS TIME NORDOM FIELD ENGINEERING DISPOSITION DOC # NTRSD-22TP-052 DATED 26FEB22 ALLOWS FOR THE UNIT TO RETURN TO REGULAR OPERATIONS FOR 430 +/- 20 FLIGHT HOURS AND UP TO 6 MONTHS.
From FAA Service Difficulty Reports; matched by N-number and serial number.RH ENGINE THRUST REVERSER MOUNTING FLANGE CORRODED BETWEEN 3 AND 9 O'CLOCK POSITIONS. ACCOMPLISHED NORDAM FIELD ENGINEERING DISPOSITION DOCUMENT NUMBER: MTRSD-22TP-052 DATED: 23FEB2022; CORROSION ON ATTACH FLANGE EDGE CITATION LATITUDE SN: 680A-0054 TT: 5202.0 TC: 3471. UNIT CAN RETURN TO REGULAR…
From FAA Service Difficulty Reports; matched by N-number and serial number.CRACK DAMAGE, NOSE LANDING GEAR WHEEL WELL (NWW), FRAME, WEB, AND DOUBLERS, FS 75. ACCOMPLISHED TEXTRON AVIATION FIELD REPAIR SR-680A-ATA53-25890 REV- DATED JUNE 1, 2020 AND 8100-9 DATED 6/1/2020; STANDARD REPAIR - CRACK DAMAGE, NOSE LANDING GEAR WHEEL WELL (NWW), FRAME, WEB, AND DOUBLERS, FS 75.…
From FAA Service Difficulty Reports; matched by N-number and serial number.REPAIR OF HORIZONTAL STABILIZER LEFT AND RIGHT CUFF/FILLET FAIRINGS DAMAGE. ENGINEERING MEMO # DQ24493M1.
From FAA Service Difficulty Reports; matched by N-number and serial number.1) ENGINE CONTROL FAULT L-R AMBER CAS MESSAGE AFTER TAKEOFF 2) IAS INDICATION BOTH ON ADC 2 AMBER CAS. // SIGNOFF// REMOVED AND REPLACED BLOCKED PROBE. PERFORMED PILOT PITOT PRESSURE LEAK CHECK WITH NO FAULTS NOTED. PERFORMED AOC FUNCTIONAL CHECK WITH NO FAULTS NOTED. SEALED PITOT PROBE AND…
From FAA Service Difficulty Reports; matched by N-number and serial number.Showing the 10 most recent of 12 reports.