Cessna 402C

Service difficulty reports · 1,782

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duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = '402C'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR JZRR2015011200001Control Cable · frayedTHE FRAYED AILERON CONTROL CABLE WAS FOUND DURING A FINAL INSPECTION AFTER THE ACFT WAS STRIPPED & PAINTED. THE CABLE WAS LOCATED, VISUALLY, IN THE RT FLAP WELL INBD OF THE AILERON BELL-CRANK BETWEEN TWO RIBS, WS 133.29 & 151.04. THE FRAYED CABLE WAS IN PLAINJan 12, 2015 · N88833 · Cessna 402C · Aileron Control SystemSDR HYIA20150107001Spar Cap · mechanic errorUPON DISASSEMBLY OF RT NACELLE LOWER FAIRING FOR INSPECTION OF RT WING SPAR STRAP IAW SID 57-10-16, UNINTENTIONAL DRILL DAMAGE AT WING SPAR STRAP WAS FOUND BY VISUAL INSPECTION. THE DAMAGE EXISTS JUST OTBD OF THE INBD NACELLE FITTING WITH FWD FACE OF RT WINGJan 7, 2015 · N2714M · Cessna 402C · Wing SparSDR HYIA20150108001Warning Switch · out of adjustTHE DOOR WARNING LIGHT ILLUMINATED IN FLIGHT. ALL DOORS REMAINED SECURE IN FLIGHT. ADJUSTED THE EMER EXIT WARNING SWITCH IAW MM 52-70-00 WITH NO FURTHER DEFECT NOTED.Jan 5, 2015 · N375R · Cessna 402C · Door Warning SystemSDR HYIA20150102001Caliper · defectiveTHE BRAKES VERY WEAK, LT BRAKE IS NON-EXISTENT. R & R THE LT MLG CALIPER ASSEMBLY IAW MM CH 32-40-00. RT & LT BRAKES SERVICED IAW MM 12-10-05. OPERATIONS CHECKED GOOD.Jan 1, 2015 · N618CA · Cessna 402C · BrakeSDR HYIA20141231001Fan · malfunctionedTHE LT ANNUNCIATOR INTERMITTENT & AN ELEC SMELL IN CABIN. INSPECTED, R & R LT ALTERNATOR OUT SENSOR IAW MM CH 34-30-0. OPERATIONS CHECKED GOOD. THE SMELL WAS DETERMINED TO BE THE CABIN VENT FAN WHICH WAS PLACED ON MEL. NO FURTHER DEFECTS NOTED.Dec 28, 2014 · N120PC · Cessna 402C · Air Distribution FanSDR HYIA20141231002Caliper · misinstalledRIGHT MAIN TIRE & GEAR BRAKE CALIPER HAS COME LOOSE & MOVED TO JAM UP ON STRUT. R & R THE RT BRAKE CALIPER, PAD SET & TIRE ASSEMBLY IAW MM CH 32-10-00 WITH NO DEFECTS NOTED. FURTHER INVESTIGATION LEAD TO THE DISCOVERY THAT THE RT MAIN TIRE HAD BEEN CHANGED PDec 27, 2014 · N1055 · Cessna 402C · BrakeSDR HYIA20141230001Switch · defectiveSMOKE COMING OUT OF CABIN HEAT SWITCH. REPLACED DEFECTIVE SWITCH WITH SERVICEABLE SPARE W31-X2MIG-15 SWITCH. FUNCTIONAL CHECK NORMAL.Dec 26, 2014 · N525RH · Cessna 402C · Heating SystemSDR HYIA20141224001Governor · defectiveON CLIMB OUT RT PROP INCREASED RPM BEYOND THE RED, BY ITSELF, HAD NO CONTROL OF RT PROP. ALSO RT PROP WOULD NOT FEATHER. PERFORMED AN AIR RETURN & LANDED WITH NO FURTHER INCIDENT. INSPECTED THE RT PROP CONTROL, REPOSITIONED PROP GOVERNOR CABLE. R & R PROP Dec 23, 2014 · N258PB · Cessna 402C · Propeller GovernorSDR HYIA201419003Unknown · odorHEAVY FUEL SMELL IN CABIN. INSPECTED THE CABIN, BOTH WINGS & NOSE BAGGAGE COMPARTMENT FOR ANY EVIDENCE OF FUEL LEAK. NO DEFECTS NOTED.Dec 18, 2014 · N3292M · Cessna 402C · Air Distribution SystemSDR HYIA20141217002Door · unsecureRIGHT SIDE EMER DOOR OPENED AT 1000 FT AFTER DEPARTURE. INSPECTED THE EMER EXIT DOOR SYS, SECURED THE EMER EXIT DOOR, SEALED & SEATED PROPERLY IN THE DOOR FRAME. NO FURTHER DEFECTS FOUND.Dec 16, 2014 · N1361G · Cessna 402C · Emergency ExitsSDR HYIA20141217001Caliper · defectiveRIGHT BRAKE PEDAL INEFFECTIVE. PEDAL GOES TO FLOOR & DOES NOT HOLD ACFT DURING RUN-UP. R & R THE RT BRAKE CALIPER & BRAKE PADS.Dec 16, 2014 · N290CA · Cessna 402C · BrakeSDR HYIA20141212001Sealant · faultyPILOT REPORTED SMELL OF FUEL IS CONSTANT WITHIN CABIN. MX IS IN PROCESS OF RESEALING FAULTY SEALANT IN THE WING TANKS.Dec 10, 2014 · N4652N · Cessna 402C · Fuel StorageSDR HYIA20141208001Engine · failedRT ENG LOST POWER IN FLIGHT & ENDED UP SHUTTING IT DOWN. THE ACFT LANDED WITHOUT INCIDENT. UPON INSPECTION MX FOUND THE RT ENG CRANK CASE HAD BEEN PENETRATED. INITIAL INVESTIGATION LEADS UP TO BELIEVE A CONNECTING ROD SEPARATED FROM THE CRANKSHAFT. THE ENGDec 4, 2014 · N747WS · Cessna 402C · Reciprocating Engine Power SectionSDR HYIA20141202001Pump · faultySMELL OF FUEL IN THE CABIN WHEN HEATER TURNED OFF IN FLIGHT. R & R THE HEATER FUEL PUMP. OPERATIONAL & LEAK CHECK WAS SATISFACTORY.Dec 1, 2014 · N524CA · Cessna 402C · Heating SystemSDR HYIA20141126001Alternator · defectiveBITTER FUME LIKE SMELL IN CABIN. INSPECTED ELEC WIRING & FOUND NO DEFECTS. SMELL WAS DETERMINED TO BE COMING FROM THE LT ALTERNATOR. R & R THE LT ALTERNATOR & RETURNED THE ACFT TO SERVICE WITH NO FURTHER DEFECT NOTED.Nov 25, 2014 · N2649Z · Cessna 402C · DC Generator-AlternatorSDR HYIA20141124001Exhaust Valve · brokenWHILE IN CRUISE POWER, COULD FEEL AN ENG STARTING TO RUN ROUGH. UNTIL THE RT OIL PRESS & RT CYLINDER HEAD TEMPERATURE STARTED TO DROP HE WAS UNSURE WHICH SIDE. IT WAS APPROX 3 - 4MIN FROM WHEN HE FIRST FELT THE ROUGHNESS UNTIL THE RT ENG OIL PRESS & CYLINDERNov 20, 2014 · N5826C · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA201410114001Actuator · failedELEVATOR TRIM JAMMED, CREW COMPLETED FLIGHT & LANDED WITHOUT INCIDENT. R & R THE ELEVATOR TRIM TAB ACTUATOR IAW 402C MM CH 27-30-02. OPERATIONS CHECKED GOOD.Nov 13, 2014 · N762EA · Cessna 402C · Elevator Tab Control SystemSDR HYIA20141014001Fitting · wornEMERGENCY EXIT OPENED IN FLIGHT, DIVERTED. INSPECTED EMER EXIT DOOR. FOUND LATCH CLIP WORN. R & R AS PRECAUTIONARY MEASURE. R & R PLASTIC COVER, OPERATIONS CHECKED GOOD.Oct 12, 2014 · N499CA · Cessna 402C · Emergency ExitsSDR HYIA20141001001Caliper · defectiveON PREFLIGHT PILOT REPORTED RT BRAKES INOPERATIVE, NO BRAKES ON THE RT SIDE. R & R THE RT BRAKE CALIPER & BRAKE PADS IAW MM 32-10-00. OPERATIONS CHECKED GOOD.Sep 30, 2014 · N1376G · Cessna 402C · BrakeSDR HYIA20140930001Nut · looseDURING ROUTINE INSPECTION IT WAS DISCOVERED THAT THE NR 1 MAIN THRU BOLT NUT HAD BACKED OFF THE STUD IN FRONT OF THE OIL COOLER ON N83PB RT ENG. AS PRECAUTIONARY MEASURE THE RT ENG IS BEING CHANGED & SENT OUT FOR OVERHAUL.Sep 27, 2014 · N83PB · Cessna 402C · Reciprocating Engine Power SectionSDR HYIA20140929001Brake Sys · lowVERY POOR BRAKING ALMOST NOTHING. THIS WAS NOTED AFTER DEPARTURE WHICH INDICATES THE PROBLEM WAS FOUND ON LANDING. THE BRAKE SYS WAS THEN SERVICED IAW MM CH 12-10-03 & 32-40-00. OPERATIONS CHECKED TO ADDRESS THE ISSUE.Sep 26, 2014 · N618CA · Cessna 402C · Landing Gear Brake SystemSDR HYIA20140926BUnknown · malfunctionedRIGHT MLG FAILED TO EXTEND. ACFT LANDED WITH THE RT MAIN GEAR UP. FURTHER INVESTIGATION REQUIRED TO DETERMINE CAUSE OF FAILURE.Sep 25, 2014 · N406GA · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA20140926001Connecting Rod · separatedLEFT ENG FAILED AFTER TAKEOFF. UPON INSPECTION, IT WAS NOTED THE NR 5 CYLINDER CONNECTING ROD SEPARATED FROM THE CRANKSHAFT, CAUSING PENETRATION THROUGH THE CASE, EJECTING BOTH MAGNETOS FROM THEIR MOUNTS & CAUSING EXTENSIVE DAMAGE TO THE CYLINDER, CASE & ENG Sep 24, 2014 · N818AN · Cessna 402C · Reciprocating Engine Power SectionSDR HYIA20140905116Transducer · inaccurateON INITIAL CLIMB, THE PILOT REPORTED FUEL FLOW OF 160PPH. AFTER REACHING CRUISING ALTITUDE THE FUEL FLOW WENT TO 0 & THE PILOT REPORTED TEMP POWER LOSS. THE PILOT WENT THROUGH THE ENG FAILURE CHECKLIST & PLACED THE AUXILIARY BOOST PUMP ON IN THE HIGH SETTINGSep 1, 2014 · N2714M · Cessna 402C · Fuel Flow IndicatingSDR HYIA20140712001Hsi · failedHSI HAD FAILED DURING CRUISE FLIGHT ON AN IFR FLIGHT PLAN. SMOKE EMITTED FROM THE INSTRUMENT WITH THE BREAKER TRIPPING. SMOKE WAS BOTH VISIBLE & WAS ABLE TO BE SMELLED. QRH WAS IN HAND IN CASE SMOKE WAS NOT SUBSIDING & AN EMER LANDING AIRPORT WAS FOUND BUT Jul 10, 2014 · N466CA · Cessna 402C · Integrated Flight SystemSDR HYIA20140628002Spar Cap · corrodedDURING SCHEDULED INSPECTION, AREAS OF EXFOLIATING CORROSION WAS FOUND AT RT WING LWR FWD SPAR CAP STRAP OEM PN 5292029-2 PREVIOUSLY INSTALLED TO SATISFY REQUIREMENT OF AD2005-12-13 CONCURRENT WITH MEB05-2 AS TERMINATING ACTION FOR AD2005-05-52. THE DAMAGE HASJun 26, 2014 · N375R · Cessna 402C · Wing SparSDR HYIA20140628001Spar Cap · corrodedDURING SCHEDULED INSPECTION, AREAS OF EXFOLIATING CORROSION WAS FOUND AT LT WING LWR FWD SPAR CAP STRAP OEM PN 5292029-1 PREVIOUSLY INSTALLED TO SATISFY REQUIREMENT OF AD2005-12-13 CONCURRENT WITH MEB05-2 AS TERMINATING ACTION FOR AD2005-05-52. THE DAMAGE HASJun 26, 2014 · N375R · Cessna 402C · Wing SparSDR HYIA20140624004Rib · crackedRUDDER PEDALS STIFF. DURING INSPECTION FOUND PILOT FLOORBOARD CRACKED AT THE LT PEDAL, RUDDER & BRAKE BASE & UNDERNEATH FLOORBOARD ON ANGULAR RIB. PERFORMED STOP DRILL & PATCH ON LT UNDERNEATH FLOORBOARD, ANGULAR RIB WAS RE-ENFORCED.Jun 23, 2014 · N385CA · Cessna 402C · Fuselage Main, Attach FittingsSDR HYIA20140624002Web · crackedDURING SCHEDULED INSPECTION, MULTIPLE WEB FLANGE CRACKS WERE FOUND AT AFT FUSELAGE CARRY THROUGH SPAR ASSEMBLY PN 5211173-2 AT CTR UPPER SECTION FWD & AFT WEBS. THIS DAMAGE AREA DIRECTLY CORRESPONDS TO CTR CABIN FLOORBOARD AREA & IS PRONE TO DAMAGE AS PAXS & Jun 23, 2014 · N4652N · Cessna 402C · Fuselage Miscellaneous StructureSDR HYIA20140624001Beam · crackedDURING VISUAL INSPECTION OF NACELLE STRUCTURE AT TURBOCHARGER REMOVAL FOR OTHER MAINTENANCE, THE RT NACELLE CROSSOVER BEAM WAS FOUND TO BE CRACKED AT TURBOCHARGER MOUNT BRACKET ATTACH HOLE AFT SIDE OF BEAM. CORRECTIVE ACTION WILL BE TO R & R BEAM WITH NEW OEMJun 23, 2014 · N4652N · Cessna 402C · Nacelle/Pylon Miscellaneous StructureSDR HYIA20140624003Dimmer · malfunctionedSMOKE APPEARED FROM INSTRUMENT PANEL LIGHT, DIMMER ASSEMBLY. R & R DIMMER ASSEMBLY PN 5118424-1.Jun 22, 2014 · N36911 · Cessna 402C · Flight Compartment LightingSDR HYIA20140621001Spar Cap · corrodedDURING SCHEDULED INSPECTION, AREAS OF EXFOLIATING CORROSION WERE FOUND AT RT WING LWR SPAR CAP STRAP OEM PN 5292029-2 PREVIOUSLY INSTALLED TO SATISFY REQUIREMENT OF AD2005-12-13 CONCURRENT WITH MEB02-5. THE CORRECTIVE ACTION WILL BE TO PERFORM A DETAILED INSPJun 20, 2014 · N4652N · Cessna 402C · Wing SparSDR HYIA20140623001Axle · crackedWHILE TURNING TO LINE UP WITH RUNWAY CENTERLINE, DIFFICULT TO TURN ACFT RT. ACFT ONLY TURNED TO THE LT. INSPECTION OF LT MLG FOUND WHEEL ASSEMBLY LEANED AGAINST LG. FURTHER INSPECTION FOUND LG AXLE TO BE CRACKED.Jun 17, 2014 · N247GS · Cessna 402C · Main Landing Gear Strut/Axle/TruckSDR HYIA20140614002Spar Cap · corrodedSERVICE KIT SK402-47, CONCURRENT WITH AD2005-12-13 & MEB02-5, WAS INSTALLED ON 07/24/2003 AT AFTT 20,019.7 AS TERMINATING ACTION FOR AD2005-05-52. EDDY CURRENT PRESCRIBED IN SID 57-10-16 REVEALED MULTIPLE AREAS OF SUBSURFACE CORROSION IN LWR FWD SPAR CAP STRAJun 12, 2014 · N121PB · Cessna 402C · Wing SparSDR HYIA20140614001Spar Cap · corrodedSERVICE KIT SK402-47, CONCURRENT WITH AD2005-12-13 & MEB02-5, WAS INSTALLED ON 07/24/2003 AT AFT 20,019.7 AS TERMINATING ACTION FOR AD2005-05-52. EDDY CURRENT PRESCRIBED IN SID 57-10-16 REVEALED MULTIPLE AREAS OF SUBSURFACE CORROSION IN LWR FWD SPAR CAP STRAPJun 12, 2014 · N121PB · Cessna 402C · Wing SparSDR HYIA20140529116Control Cable · frayedDURING A PRE-FLIGHT INSPECTION THE PILOT REPORTED CAPTAINS CONTROL YOKE HAS A SPONGY FEEL WHEN PULLED AFT. MAINTENANCE INSPECTED & FOUND THE RT ELEVATOR CABLE, PN 5200008-31CR, FRAYED AT FS 112.07, ALONG WITH DAMAGE TO THE AILERON CABLE GUARD PIN PN NAS427K22.May 23, 2014 · N401TJ · Cessna 402C · Elevator Control SystemSDR HYIA20140523003Indicator · separatedELEVATOR JAMMED ON TAKEOFF, COULD NOT PULL YOKE BACK TO ROTATE. VOR 2 INDICATOR CASE DROPPED ONTO THE CONTROL YOKE PREVENTING FULL REARWARD TRAVEL. TAKEOFF WAS ABORTED WITH NO FURTHER INCIDENT. FOUND VOR INDICATOR BACK CASE SEPARATED FROM FRONT OF INDICATORMay 21, 2014 · N781EA · Cessna 402C · Visual Omnirange (VOR) SystemSDR HYIA2014052303Beam · crackedDURING ROUTINE SCHEDULED INSPECTION, THE RT NACELLE INBD ENG BEAM WAS FOUND TO BE CRACKED AT INBD AFT FACE. CORRECTIVE ACTION WILL BE TO REMOVE & INSTALL NEW RT NACELLE INBD ENG BEAM IN ITS ENTIRETY. A SUPPLEMENT TO THIS SDR HAS BEEN SUBMITTED TO FURTHER OUTMay 20, 2014 · N290CA · Cessna 402C · Nacelle/Pylon Miscellaneous StructureSDR HYIA20140523001Beam · crackedDURING ROUTINE SCHEDULED INSPECTION, THE RT NACELLE CROSSOVER BEAM WAS FOUND TO BE CRACKED AT LWR U CHANNEL. CORRECTIVE ACTION WILL BE TO REMOVE & INSTALL RT NACELLE CROSSOVER BEAM IN ITS ENTIRETY. A SUPPLEMENT TO THIS SDR HAS BEEN SUBMITTED TO FURTHER OUTLIMay 20, 2014 · N290CA · Cessna 402C · Nacelle/Pylon Miscellaneous StructureSDR HYIA20140606001Sight Tube · splitPILOT REPORTED AFTER DEPARTURE FROM MAZ & DURING TRANSITION FROM CLIMB TO CRUISE SMOKE & FUMES WERE DETECTED COMING FROM DEFROST VENT. PILOT CLOSED DEFROST, RAM AIR & CABIN AIR VENT VLVS. UPON CLOSING CABIN VENTILATION VLVS, PILOT REPORTS SMOKE & FUMES NO LOMay 14, 2014 · N120PC · Cessna 402C · Hydraulic Quantity IndicatorSDR HYIA05032014007Beam · chafedDURING SCHEDULED INSPECTION, CHAFE DAMAGE WAS NOTED AT RT NACELLE OTBD ENG BEAM AFT OF CORRESPONDING ENG MOUNT. THIS DAMAGE WILL BE REPAIRED IAW REPAIR DEFINITION SUPPLIED & SUBSTANTIATED BY DER. A SUPPLEMENT TO THIS SDR WILL BE FORWARDED SEPARATELY FURTHER May 1, 2014 · N258PB · Cessna 402C · Nacelle/Pylon Miscellaneous StructureSDR HYIA05032014006Beam · chafedDURING SCHEDULED INSPECTION, CHAFE DAMAGE WAS NOTED AT LT NACELLE OTBD ENG BEAM AFT OF CORRESPONDING ENG MOUNT. THIS DAMAGE WILL BE REPAIRED IAW REPAIR DEFINITION SUPPLIED & SUBSTANTIATED BY DER. A SUPPLEMENT TO THIS SDR WILL BE FORWARDED SEPARATELY FURTHERMay 1, 2014 · N258PB · Cessna 402C · Nacelle/Pylon Miscellaneous StructureSDR HYIA05032014005Spar · crackedDURING SCHEDULED INSPECTION, MULTIPLE SPAR WEB CRACKS WERE NOTED INITIATING FROM SPAR WEB MOUSE HOLE CUT OUTS AT AFT CARRY THROUGH SPAR ASSEMBLY, PN 5211173-2, AT CTR LOWER SECTION OF FWD & AFT WEBS. THIS DAMAGE WILL BE REPAIRED IAW REPAIR DEFINITION SUPPLIEDMay 1, 2014 · N258PB · Cessna 402C · Wing SparSDR HYIA05032014004Spar · crackedDURING SCHEDULED INSPECTION, MULTIPLE SPAR WEB CRACKS WERE NOTED INITIATING FROM SPAR WEB, MOUSE HOLE CUT OUTS AT FWD CARRY THROUGH SPAR ASSEMBLY, PN 5211171-2, AT CTR LOWER SECTION OF FWD & AFT WEBS. THIS DAMAGE WILL BE REPAIRED IAW REPAIR DEFINITION SUPPLIEMay 1, 2014 · N258PB · Cessna 402C · Wing SparSDR HYIA05032014003Spar · crackedDURING ROUTINE SCHEDULED INSPECTION, MULTIPLE WEB FLANGE CRACKS WERE NOTED AT AFT FUSELAGE CARRY THROUGH SPAR ASSEMBLY, PN 5211173-2 AT CTR UPPER SECTION FWD & AFT WEBS. THIS DAMAGE WILL BE REPAIRED, REPAIR DEFINITION SUPPLIED & SUBSTANTIATED BY DER. A SUPPLMay 1, 2014 · N258PB · Cessna 402C · Wing SparSDR HYIA05032014001Strap · corrodedDURING ROUTINE SCHEDULED INSPECTION, AREAS OF CORROSION WERE FOUND AT LT & RT LOWER WING SPAR CAP STRAPS PREVIOUSLY INSTALLED VIA SK402-47B ON 12/05/2005 TO SATISFY REQUIREMENT OF AD2005-12-13 & MEB02-5. THE CORRECTIVE ACTION TO REMEDIATE CONDITION WILL BE TOMay 1, 2014 · N258PB · Cessna 402C · Wing SparSDR HYIA20140439114Spar · crackedDURING A SCHEDULED MX EVENT, TWO CRACKS WERE FOUND AT THE AFT CARRY THROUGH SPAR WEB FLANGES. THE CRACKS WERE APPROXIMATELY .75 INCHES IN LENGTH & WERE LOCATED AT FS 186.15, RBL 7.75 AT THE FWD & AFT SPAR FLANGE. THE DAMAGE WAS REPAIRED IAW ENGINEERING DRAWIApr 28, 2014 · N2611X · Cessna 402C · Wing SparSDR HYIA20140430115Fluid · lowWHILE TAXIING, THE PILOT ATTEMPTED TO EXECUTE A RT TURN. THE RT BRAKE PEDAL WENT SOFT & THE ACFT STOPPED TURNING & TAXIED STRAIGHT FWD. THE PILOT CLOSED THE THROTTLE & STOPPED, BUT THE ACFTS NOSE & LT TIRE WENT INTO THE GRASS. THE ACFT COULD NOT BE MOVED WApr 27, 2014 · N3249M · Cessna 402C · Master Cylinder/Brake ValveSDR HYIA20140424112Pump · leakingPILOT REPORTED FUEL SMELL IN COCKPIT DURING FLIGHT. AFTER LANDING, A WALK AROUND INSPECTION REVEALED THE ODOR WAS COMING FROM THE NOSE AREA WITH VISIBLE LEAKAGE OUT OF HEATER FUEL PUMP DRAIN. MX VERIFIED BY VISUAL INSPECTION THAT FUEL WAS LEAKING FROM THE HEAApr 23, 2014 · N762EA · Cessna 402C · Heating SystemSDR HYIA20140425113Unknown · malfunctionedPILOT REPORTED LT ENG FUEL FLOW FLUCTUATES AROUND 100 PPH DURING CLIMB WITH FUEL PUMP, AUXILIARY, OFF. REPLACED LT ENG DRIVEN FUEL PUMP IAW CMI MANUAL & RELEASED FOR A FCF. THE FCF WAS UNSATISFACTORY. THE ACFT IS STILL IN MAINTENANCE. THIS REPORT WILL BE AMApr 22, 2014 · N406GA · Cessna 402C · Engine Fuel and Control
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