Service difficulty reports · 8
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2002FA0000824Switch · failedDURING MAINTENANCE PRE-RUN FOR PHASE INSPECTION, WHEN MASTER AVIONICS SWITCH WAS TURNED OFF, ONLY HALF OR THE AVIONICS COMPONENTS TURNED OFF. ONE SIDE OF THE SWITCH FAILED IN THE ON POSITION. REPLACED SWITCH, OPERATIONAL CHECKED SAT.SDR 2001FA0000129Servo · malfunctionedRPM SET TO 1500 FOR PURGING FUEL VAPORS PRIOR TO TAXI, TAXI AND RUN UP WERE NORMAL. WHEN FULL THROTTLE WAS APPLIED FOR TAKE OFF THE ENGINE WOULD NOT DEVELOP FULL POWER. IT WOULD ONLY DEVELOP 2000 RPM. MAINTENANCE INSTALLED CLEAR FUEL LINE ON OUTLET LINE FROMSDR 20010410AP016Control Housing · brokenDURING PHASE 3 INSPECTION FOUND PILOTS SEAT LOCK CONTROL ASSEMBLY P/N 1611021-05 BROKEN. ONE SEAT LOCK PIN WAS ENGAGED AND WOULD NOT RELEASE DUE TO THE ACTUATOR CABLE BROKEN. THIS IS THE 5TH SEAT CONTROL ASSEMBLY THAT HAS FAILED WITH A BROKEN CABLE FOR THIS SDR 20001101SH011Servo · failedENGINE RSA-5AD1 FUEL SERVO WILL NOT MEET SPECIFICATIONS. FUEL FLOW BELOW 1700 RPM IS TOO HIGH, AT IDLE RPM IS ERRATIC, AND THE IDLE SPEED AND IDLE MIXTURE CANNOT BE SET TO SPECIFICATION WITH SATISFACTORY ENGINE OPERATION. FUEL SERVO REMOVED, SENT FOR REPAIR.SDR 20001018SH006Fuel Line · vapor lockAFTER 3RD SORTIE OF THE DAY, AIRCRAFT SAT FOR 45 MINUTES BEFORE NEXT FLIGHT. ENGINE START WAS DIFFICULT USING HOT STARTING PROCEDURES WITH ENGINE RUNNING RPM WAS INCREASING AND DECREASING 200 RPM AND ENGINE OPERATION WAS ROUGH AND ERRATIC. AN ATTEMPT WAS MADSDR 99ZZZX4156Pump · malfunctionedNEW 172S CONDUCTING FLIGHT TRAINING AT AIRFIELD ABOVE 6,000 FEET WITH AMBIENT TEMP OF 80 DEGREES FAHRENHEIT. ON 3RD SORTIE OF THE DAY, ACFT TAXIED TO RUN-UP AREA AND COMMENCED ENGINE RUN-UP. AT 1,800 RPM, ENGINE WAS RE-LEANED FOR PEAK RPM AND RPM FLUCTUATED SDR 99ZZZX3488Nozzle · looseDURING PHASE INSPECTION, FOUND ALL FOUR FUEL INJECTION NOZZLES, PN LW18265, HAD SCREENS AND SHIELDS LOOSE AROUND NOZZLE BODY. REFERENCE LYCOMING OHM 'SHIELD MUST HAVE A TIGHT FIT ON BODY WHEN INSTALLED'. THIS IS THE SECOND NEW ENGINE WITH SAME PROBLEM.SDR 99ZZZX2734Skin · crackedNEW CESSNA DURING PHASE 1 INSPECTION, FOUND LEFT FLAP TRAILING EDGE, LOWER SKIN, CRACKED AT 4 EACH RIVETS STARTING FROM INBOARD END TO OUTBOARD 2 FEET. REPLACED FLAP WITH NEW ASSY FURNISHED BY CESSNA.
Other aircraft with N948SP · 1
The FAA can assign a mark to another aircraft once a registration is cancelled. N948SP is registered now to the first aircraft listed.