FAA incident reports · 2
FAA accident and incident reports matched to this aircraft by N5040Q and the event date: up to this one’s cancellation.
Incident 20170118000429ILanding: Rollout · Dalhart, TXOn January 18, 2017, at 1525 CDT, a Cessna C-402B registration number N5040Q, registered to a private owner, experienced a left main landing gear collapse when it landed at Dalhart Municipal Airport, in Dalhart, TX. The aircraft was being operated on a…Incident 20000505022769IRoll-Out (Fixed Wing) · Cahokia, IL(-23)Inspector statment: the incident ocurred on, may 5, 2000, at the st. Louis Downtown Parks (cps) airport at 0500Z (0000 local) time. The aircraft is an Cessna model 402B, registration number N5040Q, owned and operated by springdale air serivce, inc.…
Service difficulty reports · 14
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 20001120SH005Control Cable · brokenCPS/LIT - WHILE ON FINAL, THE FLAP SYSTEM FAILED. IT WAS DETERMINED THE UPPER FLAP EXTEND CABLE ON THE RIGHT SIDE HAD BROKEN APPROXIMATELY A FOOT OUTBOARD OF THE ACTUATOR CHAIN ATTACH POINT. THE CABLE COULD HAVE BEEN INCORRECTLY ROUTED/RIGGED AND/OR THE CABLSDR 99ZZZX4230Rib · crackedDURING THE COURSE OF COMPLETING A 100-HOUR INSPECTION, MULTIPLE CRACKS WERE FOUND IN THE PRIMARY COMPONENTS THAT MAKE UP CESSNA SERVICE KIT SK404-83. CRACKS WERE FOUND ON BOTH LEFT AND RIGHT RIBS, FILLERS, DOUBLERS, AND ANGLES.SDR 99ZZZX4229Rib · crackedDURING THE COURSE OF COMPLETING A 100-HOUR INSPECTION, MULTIPLE CRACKS WERE FOUND IN THE PRIMARY COMPONENTS THAT MAKE UP CESSNA SERVICE KIT SK414-83. CRACKS WERE FOUND ON BOTH LEFT AND RIGHT RIBS, FILLERS, DOUBLERS, AND ANGLES.SDR 99ZZZX4219Cylinder Head · separatedDURING THE COURSE OF NORMAL FLIGHT, THE PILOT NOTICED RIGHT ENGINE RUNNING ROUGH WITH A DROP IN ITS MANIFOLD PRESSURE. THE AIRCRAFT LANDED WITHOUT EVENT. MAINTENANCE WAS ABLE TO DETERMINE THAT THE NR 2 CYLINDER HEAD HAD SEPARATED FROM THE BARREL OF THE CYLINDSDR 99ZZZX4216Rib · crackedDURING THE COURSE OF COMPLETING A 100-HOUR INSPECTION, A CRACK WAS DISCOVERED IN THE FORWARD PORTION OF RIB, CESSNA P/N 0822175-74. THE RIB HAD BEEN MODIFIED IAW CESSNA SK 414-8E APPROXIMATELY 4,303 HOURS AGO, WHICH, BY LOCATION, IS NOT ASSOCIATED WITH THE CRSDR 99ZZZX4215Rib · crackedDURING THE COURSE OF COMPLETING A 100-HOUR INSPECTION, A CRACK WAS DISCOVERED IN THE FORWARD PORTION OF RIB, CESSNA P/N 0822175-79. THE RIB HAD BEEN MODIFIED IAW CESSNA SK 414-8E APPROXIMATELY 4,303 HOURS AGO, WHICH, BY LOCATION, IS NOT ASSOCIATED WITH THE CRSDR 98ZZZX3037Stud · failedDURING 100-HOUR INSPECTION, MECHANIC NOTICED RIGHT ENGINE, NR 6 CYLINDER, PER MOST AFT AND THE LOWER TWO MOST AFT STUDS HAD BROKEN OFF FLUSH WITH THE CYLINDER BASE/SKIRT. THE CASE WAS INSPECTED FOR CRACKS, AND A CRACK APPROXIMATELY A .50 INCH LONG WAS OBSERVSDR 98ZZZX1996Crankcase Bolt · crackedDURING THE COURSE OF A 100-HOUR INSPECTION, THE MECHANIC NOTICED A SIZEABLE AMOUNT OF OIL ON THE TOP LEFT PORTION OF THE ENGINE CASE. A CLOSER INSPECTION REVEALED A CRACK APPROXIMATELY 1.6250 INCH LONG EMITTING FROM THE 9TH BACKBONE BOLT (COUNTING FROM FRONT SDR 98ZZZX351Bracket · brokenDURING A 100-HOUR INSPECTION, MECHANIC FOUND THE RIGHT TURBO MOUNTING BRACKET BROKEN. CESSNA BRACKET 0851139-3 HAD ITS OUTBOARD LOWER ATTACH LEG BROKEN OFF. UNABLE TO DETERMINE THE CAUSE OF THIS PROBLEM.SDR 97ZZZX4579Cylinder · separationDURING NORMAL FLIGHT, PILOT NOTICED LEFT ENGINE RUNNING ROUGH AND RETURNED TO POINT OF DEPARTURE. DETERMINED THE NR 1 CYLINDER ON THE LEFT ENGINE HAD SEPARATED THE HEAD FROM THE BARREL. SUBMITTER SUGGESTED FROM PAST EXPERIENCE, THIS IS TYPICAL OF A TCM TSIO5SDR 97ZZZX2914Bellcrank · brokenUPON COMPLETING A NORMAL TRIP, THE PILOT ON HIS POST FLIGHT INSPECTION NOTICED THE RT INBOARD LANDING GEAR DOOR WAS OPEN. AFTER A CLOSER INSPECTION, DETERMINED THE BELLCRANK ASSEMBLY THAT ACTUATES THE INBOARD GEAR DOOR WAS BROKEN. IT WAS BROKEN IN SUCH A WAYSDR 97ZZZX2616Rib · crackedDURING A 50-HOUR INSPECTION, MECHANIC NOTICED CRACK IN WING SKIN IN THE MOST AFT OTBD SECTION OF RT WING. ALSO, TWO RIVETS WERE SHEARED THAT ATTACH THE OTBD HINGE BRACKET ASSY (CESSNA PN 5021002-13) WHICH ARE THE SAME RIVETS THAT ATTACH TIP TANK SUPPORT BRACKSDR 97ZZZX2615Support Bracket · rivets shearedDURING A 50-HOUR INSPECTION, MECHANIC NOTICED CRACK IN WING SKIN IN THE MOST AFT OTBD SECTION OF RT WING. ALSO, TWO RIVETS WERE SHEARED THAT ATTACH THE OTBD HINGE BRACKET ASSY (CESSNA PN 5021002-13) WHICH ARE THE SAME RIVETS THAT ATTACH TIP TANK SUPPORT BRACKSDR 97ZZZX2614Skin · crackedDURING A 50-HOUR INSPECTION, MECHANIC NOTICED CRACK IN WING SKIN IN THE MOST AFT OTBD SECTION OF RT WING. ALSO, TWO RIVETS WERE SHEARED THAT ATTACH THE OTBD HINGE BRACKET ASSY (CESSNA PN 5021002-13) WHICH ARE THE SAME RIVETS THAT ATTACH TIP TANK SUPPORT BRACK