# Service difficulty reports: N88833, cancelled Apr 8, 2022 A list on [N88833, cancelled Apr 8, 2022](https://openairdocs.org/deregistered/N88833-2022-04-08.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR HYIA20210820001](https://openairdocs.org/sdr/HYIA20210820001.md): Blower · inoperative · Aug 16, 2021 · N88833 · Cessna 402C · Heating System > THE PILOT REPORTED SMOKE IN THE CABIN DURING CRUISE WHILE THE HEATER WAS ON. MAINTENANCE INSPECTED, FOUND THE HEATER BLOWER INOPERABLE, AND REPLACED IT WITH NO FURTHER DEFECTS NOTED. - [SDR HYIA20200304001](https://openairdocs.org/sdr/HYIA20200304001.md): Fan · burned out · Feb 27, 2020 · N88833 · Cessna 402C · Air Distribution Fan > PILOT REPORTED BURNING ODOR IN CABIN. UPON INSPECTION MAINTENANCE, FOUND THE CABIN FAN BURNT OUT. REMOVED AND REPLACED THE CABIN FAN WITH NO FURTHER DEFECTS NOTED. - [SDR HYIA20190115002](https://openairdocs.org/sdr/HYIA20190115002.md): Engine · failed · Jan 12, 2019 · N88833 · Cessna 402C · Engine (Reciprocating) > PILOT REPORTED ENGINE SHUDDERED IN FLIGHT AND THEN STOPPED SHORTLY AFTER. THE AIRCRAFT LANDED WITHOUT INCIDENT. INITIAL INSPECTION REVEALED AN ENGINE CASE PENETRATION AT THE TOP REAR OF THE CASE AT THE NR 1 CYLINDER IN THE AREA UNDER LEFT MAGNETO, AND THE MAGN - [SDR HYIA20180914001](https://openairdocs.org/sdr/HYIA20180914001.md): Beam · cracked · Sep 14, 2018 · N88833 · Cessna 402C · Nacelle/Pylon, Main Frame > DURING NDT TESTING DONE TO SATISFY AD 2015-07-03, A CRACK WAS DISCOVERED ON THE LEFT NACELLE INBOARD ENGINE BEAM P/N: 5654109-6. THIS CRACK IS TRAVELING LEFT TO RIGHT ACROSS THE TOP OF THE BEAM ORIGINATING FROM A FASTENER HOLE ON THE TOP OF THE BEAM TRAVELLING - [SDR HYIA20171121001](https://openairdocs.org/sdr/HYIA20171121001.md): Exhaust Valve · broken · Nov 18, 2017 · N88833 · Cessna 402C · Reciprocating Engine Cylinder Section > PILOT REPORTED RIGHT ENGINE VIBRATING ON FINAL APPROACH AND TAXI. MAINTENANCE INSPECTED AND FOUND NO COMPRESSION ON THE RIGHT ENGINE NR 4 CYLINDER. UPON REMOVAL DISCOVERED THE EXHAUST VALVE HAD CRACKED AND BROKEN. THE CYLINDER WAS REPLACED WITH NO FURTHER DEFE - [SDR HYIA20170828013](https://openairdocs.org/sdr/HYIA20170828013.md): Fitting · cracked · Feb 20, 2017 · N88833 · Cessna 402C · Nacelle/Pylon, Attach Fittings > DURING A SID 57-10-16 NDT INSPECTION, FOUR CRACKS WERE FOUND IN THE LT OUTBOARD FITTING. TWO OF THESE CRACKS WERE FOUND ON THE INBOARD SIDE OF THE FITTING, JUST FORWARD OF THE SPAR STRAP. THEY MEASURED.143 AND.129 IN LENGTH. THE OTHER TWO CRACKS WERE FOUND O - [SDR HYIA20160815072](https://openairdocs.org/sdr/HYIA20160815072.md): Exhaust Valve · cracked · Aug 11, 2016 · N88833 · Cessna 402C · Reciprocating Engine Cylinder Section > CYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION. EXHAUST VALVE CRACKED AND DISPLAYS EVIDENCE OF HEAT DAMAGE. - [SDR HYIA20160810001](https://openairdocs.org/sdr/HYIA20160810001.md): Line · cracked · Aug 9, 2016 · N88833 · Cessna 402C · Hydraulic System, Main > PILOT REPORTED LEFT BRAKE INOPERATIVE AND STEERING NOT AVAILABLE. MAINTENANCE INSPECTED AND FOUND THE BRAKE LINE FROM THE PARKING BRAKE VALVE ELBOW, TO MASTER CYLINDER FLEX HOSE LEAKING. REMOVED AND REPLACED THE LINE. - [SDR HYIA20160122001](https://openairdocs.org/sdr/HYIA20160122001.md): Computer · faulty · Jan 18, 2016 · N88833 · Cessna 402C · Autopilot Computer > PILOT REPORTED ELEC SMELL IN THE COCKPIT 15 MINUTES INTO FLIGHT. INSPECTED & FOUND THE AUTOPILOT COMPUTER TO BE AT FAULT. R & R AUTOPILOT COMPUTER. - [SDR HYIA20151029002](https://openairdocs.org/sdr/HYIA20151029002.md): Fuel Line · loose · Oct 26, 2015 · N88833 · Cessna 402C · Engine Fuel Distribution > PILOT REPORTED A STRONG FUEL SMELL IN CABIN, NOTING THAT THE HEATER WAS OFF DURING FLIGHT. PERFORMED AN OPERATIONAL CHECK OF THE HEATER, INSPECTED THE FUEL LINES & COMPONENTS, NO FUEL LEAKS OR SMELLS NOTED AT THIS TIME. APPLIED TDMI OF RT WING FUEL PANEL SEE - [SDR HYIA20150126001](https://openairdocs.org/sdr/HYIA20150126001.md): Beam · cracked · Jan 24, 2015 · N88833 · Cessna 402C · Nacelle/Pylon Miscellaneous Structure > DURING SCHEDULED INSPECTION EVENT, THE RT NACELLE OTBD ENG BEAM WAS FOUND TO BE CRACKED AT AREA EXTENDING FWD & LWR OF OTBD PORTION OF AFT MOUNT BEAM OVERLAYS. A SUPPLEMENT TO THIS SDR WILL BE SUBMITTED TO ILLUSTRATE DAMAGE POINT. CORRECTIVE ACTION WILL BE C - [SDR JZRR2015011200001](https://openairdocs.org/sdr/JZRR2015011200001.md): Control Cable · frayed · Jan 12, 2015 · N88833 · Cessna 402C · Aileron Control System > THE 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 PLAIN - [SDR HYIA201341220001](https://openairdocs.org/sdr/HYIA201341220001.md): Heater Pump · leaking · Dec 19, 2013 · N88833 · Cessna 402C · Heating System > STRONG SMELL OF FUEL IN COCKPIT DURING FLIGHT. R & R HEATER FUEL PUMP IAW SERVICE MANUAL, LEAK CHECKED GOOD. - [SDR HYIA20140414051](https://openairdocs.org/sdr/HYIA20140414051.md): Drag Brace · cracked · Aug 14, 2013 · N88833 · Cessna 402C · Landing Gear Retraction/Extension System > AT SCHEDULED INSPECTION, NLG DRAG BRACE, OEM PN 5142002-5, WAS FOUND TO BE CRACKED IN THE AREA OF NLG ACTUATOR ATTACH POINT. METHOD OF INSPECTION WAS DYE PENETRANT. THIS CRACK WAS FOUND TO BE BEYOND LIMIT ALLOWABLE. THIS UNIT HAS BEEN SCRAPPED & A REPLACEME - [SDR HYIA20140414048](https://openairdocs.org/sdr/HYIA20140414048.md): Drag Brace · cracked · May 13, 2013 · N88833 · Cessna 402C · Landing Gear Retraction/Extension System > AT SCHEDULED INSPECTION, NLG DRAG BRACE, PN 5142002-5 WAS FOUND TO BE CRACKED IN THE AREA OF NLG ACTUATOR ATTACH POINT. METHOD OF INSPECTION WAS DYE PENETRANT. THIS CRACK WAS FOUND TO BE BEYOND LIMIT ALLOWABLE OF MEB91-11R1. THIS UNIT HAS BEEN SCRAPPED & A - [SDR HYIA20140414039](https://openairdocs.org/sdr/HYIA20140414039.md): Drag Brace · cracked · Dec 12, 2012 · N88833 · Cessna 402C · Landing Gear Retraction/Extension System > AT SCHEDULED INSPECTION, NLG DRAG BRACE, PN 5142002-5 WAS FOUND TO BE CRACKED IN THE AREA OF NLG ACTUATOR ATTACH POINT. METHOD OF INSPECTION WAS DYE PENETRANT. THIS CRACK WAS FOUND TO BE BEYOND LIMIT ALLOWABLE OF MEB91-11R1. THIS UNIT HAS BEEN SCRAPPED & A - [SDR HYIA20111003001](https://openairdocs.org/sdr/HYIA20111003001.md): Trim System · misrigged · Oct 3, 2011 · N88833 · Cessna 402C · Elevator Tab Control System > PILOT WHO WAS ACTING AS INSTRUCTOR FOR THIS TRAINING FLIGHT REPORTED THAT WHILE LEVELING OFF, THE FO NOTED THAT THE ELEVATOR TRIM SEEMED TO BE WORKING BACKWARDS. WHEN THE FO TRIMMED FOR NOSE DOWN, THE NOSE PITCHED UP. THE CAPTAIN TOOK THE CONTROLS AND VERIFIED - [SDR HYIA20140415023](https://openairdocs.org/sdr/HYIA20140415023.md): Drag Brace · cracked · Feb 8, 2011 · N88833 · Cessna 402C · Landing Gear Retraction/Extension System > AT SCHEDULED INSPECTION, NLG DRAG BRACE OEM PN 5142002-5 WAS FOUND TO BE CRACKED IN THE AREA OF NLG ACTUATOR ATTACH POINT. METHOD OF INSPECTION WAS DYE PENETRANT. THIS CRACK WAS FOUND TO BE WITHIN ALLOWABLE LIMIT. THIS UNIT HAS BEEN REPAIRED IAW PROCEDURE O - [SDR 888331](https://openairdocs.org/sdr/888331.md): Pump · seized · Oct 29, 2007 · N88833 · Cessna 402C · Engine Fuel Pump > AIRCRAFT WAS IN CRUISE AND THE RIGHT ENGINE SHUT DOWN WITHOUT WARNING. PILOT PERFORMED EMERGENCY CHECK LIST, DECLARED AND EMERGENCY AND DIVERTED TO MVY AIRPORT. AIRCRAFT LANDED WITH NO FURTHER INCIDENT, TAXIED TO GATE ON 1 ENGINE, AND DEPLANED 7 PASSENGERS. - [SDR N88833](https://openairdocs.org/sdr/N88833.md): Axle · cracked · Aug 22, 2007 · N88833 · Cessna 402C · Main Landing Gear Strut/Axle/Truck > THE RT AXLE OF N88833 CRACKED DURING LANDING. THE LOWER STRUT LEG WAS REPLACED WITH SERVICEABLE ASSY AND A/C RETURNED TO SERVICE. - [SDR HYI2002F00013](https://openairdocs.org/sdr/HYI2002F00013.md): Relay · failed · Jun 24, 2002 · N88833 · Cessna 402C · Starter-Generator > BATTERY SHOWED HIGH RATE OF CHARGE. BOTH ALTERNATORS, AMPERE OUTPUT, TOTAL AVIONICS FAILURE, UTILIZED AVIONICS BYPASS, REGAINED PARTIAL AVIONICS. AIRCRAFT LANDED WITHOUT INCIDENT. MECHANIC REMOVED AND REPLACED RIGHT STARTER RELAY (UNIT HAD FAILED) AND RIGHT ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 n_number = 'N88833' AND deregistration_id = 'N88833-2022-04-08' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N88833-2022-04-08/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.