Safety record in brief:1 NTSB accident (substantial damage, Jan 2022)No ADs since 1998 matched6 service difficulty reports
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The failure of a bolt in the engine valve system which resulted in malfunction of the engine exhaust valve system and a partial loss of engine power. The rough terrain encountered during the forced landing contributed to the outcome.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for CEN22LA106)
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.
No ADs published since 1998 matched this airframe or engine model.
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.
CORROSION FOUND ON RT INBD SEAT TRACK AT FS 373.15. BLENDED CORROSION AT RT INBD SEAT TRACK AT IAW SRM 51-21-00-00-02. BLEND IS WITHIN LIMITS IAW SRM 53-20-49-02-02. PERFORMED FLPI ON BLENDED AREA IAW NDT MANUAL PART 8. NO DEFECTS NOTED. PERFORMED ALODINE TREATMENT IAW SRM 51-21-10-02-01.
From FAA Service Difficulty Reports; matched by N-number and serial number.FRAME FLANGES AT FR 176 STR 32-30P HAVE CORROSION. REMOVED 1 EA RIVET TO FOM AND REMOVED CORROSION IAW SRM 51-42-05-02-01, 53-00-00-02-09 REV 12 AND DISPLACED WIRES IAW AMM 20-30-26-910-801, REV 40. PRIOR TO CORROSION REMOVAL REMOVED AN ADDITIONAL 6 RIVETS IAW SRM 51-42-05-02-01, REV 12. VERIFIED…
From FAA Service Difficulty Reports; matched by N-number and serial number.STRINGER 30S IS CORRODED, FRAME 1.00 TO 19.4. REMOVED CORROSION IAW SRM 51-21-00-00-01 AND RD 8/4-53-3888, MINIMUM REMAINING THICKNESS .057", CONFIRMED CRACK FREE REF NTM 51-00-02-250-801 AND 51-00-01-250-801. MATERIAL LOSS FOUND TO BE WITHIN LIMITS IAW RD 8/4-53-3888. RESTORED SURFACE PROTECTION…
From FAA Service Difficulty Reports; matched by N-number and serial number.CORROSION FOUND AROUND ANTENNA MOUNT BETWEEN FS 295.00 - 310.00. REMOVED 2 RIVETS TO ACCESS CORROSION IAW SRM 51-42-06. BLENDED .002 DEEP BY 1 INCH WIDE AND 1 INCH LONG. ORIGINAL THICKNESS IS .050 INCH. REMAINING MATERIAL AFTER BLEND .048 INCH. BLEND WITHIN LIMITS PER CRJ700 SRM 53-00-00. TREATED…
From FAA Service Difficulty Reports; matched by N-number and serial number.FRAME CRACKED AT BIN RAIL ATTACH POINT. REPAIRED FRAME IAW SRM. (K)
From FAA Service Difficulty Reports; matched by N-number and serial number.AFT CARGO BENT FRAME STA 1070 RIGHT AROUND STR 27R. REMOVED DAMAGED AREA, FABRICATED DOUBLER REPAIR FROM 7075-T6,0. .063 PO NR 9001660 DIMENSIONS 3 1/4' X 8 1/2', FILLER REPAIR FROM 7075-T6 0.063 PO #9001660 DIMENSIONS 1 3/8' BY 1 3/4' AND SHIM FROM 7075-T6 0.090 PO NR 9001777 DIMENSIONS 11/16' BY…
From FAA Service Difficulty Reports; matched by N-number and serial number.