FAA incident reports · 1
FAA accident and incident reports matched to this aircraft by N230AU and the event date: up to this one’s cancellation.
Service difficulty reports · 13
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR USAA990043Skin · crackedTPA - DURING CX-1 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK IN FUSELAGE SKIN STATION 727B AND STRINGER 17L. INSTALLED DOUBLER PER SRM 53-30-3 FIG 25. (M)SDR USAA980644Skin · crackedCLT - DURING RON VISUAL INSPECTION, FOUND A 3 INCH CRACK STATION 737 OF FUSELAGE STRINGER 17 RT SKIN. INSTALLED DOUBLER PER SRM 53-30-3 FIG 25. (M)SDR USAASB98263Engine · fodPHL - FLT 886 - DURING CLIMB-OUT FROM PHL AT APPROXIMATELY 1,100 FT, THE CAPTAIN REPORTED SEEING A LARGE BIRD GO PAST THE AIRCRAFT. THE BIRD STRUCK THE NR 2 ENGINE CAUSING DAMAGE. CAPTAIN SHUT DOWN THE NR 2 ENGINE, DECLARED AN EMERGENCY AND RETURNED TO FIELDSDR USAA980055Skin · crackedROA - DURING 'CX-6' CHECK VISUAL/EDDY CURRENT INSPECTION, FOUND 2.75 INCH CRACK STR 24R STA 885 SKIN (FUSELAGE). STOP DRILLED CRACK AND INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3 FIG 6. (X)SDR USAA980054Skin · crackedROA - DURING CX-6 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK BS 727A PLUS 8 STRINGER 18L FUSELAGE SKIN. STOPPED DRILLED CRACK AND INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3 FIG 6. (M)SDR USAA970118Skin · crackedROA - DURING CX-5 CHECK VISUAL/EDDY CURRENT INSPECTION, FOUND 4.5 INCH CRACK, 3.25 INCH CRACK AT STRINGER 17R BS 727B FUSELAGE SKIN. INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3 PAGE 11. (M)SDR USAASB96201Press Switch · leakingCLT - FL 338 - SHORTLY AFTER TAKEOFF, THE 'A' SYSTEM HYDRAULIC LOW PRESSURE LIGHT ILLUMINATED. HYDRAULIC QUANTITY INDICATED ZERO. CREW RETURNED TO FIELD AT CLT. FLAPS WERE EXTENDED TO 15 DEGREES WITH ALTERNATE SYSTEM AND THE LANDING GEAR WAS LOWERED MANUALLSDR USAASB96128Oil Cooler · failedBOS - FLT 788 - ON CLIMB-OUT AT APPROXIMATELY 10,000 FEET, THE NR 1 ENGINE OIL TEMPERATURE GAUGE WENT INTO THE YELLOW BAND. TEMPERATURE DECREASED WITH POWER INCREASE AND INCREASED WITH POWER DECREASE. CREW DECIDED TO RETURN TO FIELD AT BOS. OIL TEMPERATURE SDR USAA960437Floor Beam · corrosionINT - DURING Q-4 CHECK, FOUND SEVERAL 1 INCH BY 2 INCH CORRODED AREAS AROUND NUT-PLATES SPANNING A TOTAL OF 86 INCHES, STATION 987 LBL 36 INCHES TO RBL 50 INCHES FLOOR BEAM. REMOVED T-CAP SECTION OF FLOOR BEAM AND FABRICATED REPLACEMENT SECTION AND SPLICE BBLSDR USAA960436Angle · corrosionINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 2 NCH AFT ENTRY THRESHOLD 'Z' ANGLE UPPER LEG. REPLACED UPPER LEG OF 'Z' ANGLE, REPAIRED PER SRM 51-40-3. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)SDR USAA960434Frame · crackedINT - DURING Q-4 CHECK EDDY CURRENT, FOUND TWO CRACKS .125 INCH LONG, STATION 727 STRINGER 18A LEFT FRAME. REPLACED FRAME SECTION AND REPAIRED PER EO 5394G068. (M)SDR USAA960435Frame · crackedINT - DURING Q-4 CHECK EDDY CURRENT, FOUND TWO CRACKS .125 INCH LONG, STATION 727 STRINGER 18A RIGHT. REPLACED FRAME SECTION AND REPAIRED PER EO 5394G068. (M)SDR USAA950015Eel · inoperativeDCA - THE LEFT EMERGENCY EXIT OVERWING LIGHT INOPERATIVE. MAINTENANCE REPLACED LIGHT ASSEMBLY AT EMERGENCY EXIT ROW. (W)