N216AM, cancelled Feb 7, 2012

Service difficulty reports · 43

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
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 n_number = 'N216AM' AND deregistration_id = 'N216AM-2012-02-07'
  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 2008FA0000490Acoustic Liner · damagedAC RETURNED TO PLATFORM, DURING ENGINE ACCELERATION UP TO 1.4 EPR, STRONG NOISE IN THE RT ENG WAS HEARD. MAINT PERFORMED AN INSPECTION AND DETECTED ACOUSTIC LINER DELAMINATION OF THE DIFFUSER OUTER FAN DUCT, BUT WITHIN LIMITS TO OPERATE TEN HOURS IAW MM 72-00Jun 22, 2008 · N216AM · Doug DC987 · Engine (Turbine/Turboprop)SDR ASMF200805004Strut · failedAIRCRAFT RETURNED OF FLIGHT DUE TO NOSE LANDING GEAR FAILURE. MAINTENANCE PERSONNEL REPLACED THE NOSE GEAR SHOCK STRUT O-RINGS, NOSE GEAR ACTUATOR CYLINDER AND NOSE GEAR BUNGEE CYLINDER IAW MM 32-21-02, 32-32-06 AND 32-32-07, TESTED IAW MM 32-30-00, ALL CORREMay 23, 2008 · N216AM · Doug DC987 · Nose/Tail Landing Gear Strut/AxleSDR ASMF200801001Ils System · malfunctionedCAPTAIN REPORTED THAT DURING FINAL APPROACH, BOTH VHF NAVIGATORS IN THE SAME RADIAL SHOWED A DEVIATION OF 20 DEGREES IN THE TRAJECTORY, THE DIFFERENCE CONTINUED UNTIL LANDING AND RAMP. MAINT REPLACED VOR NR 1, VHF/ILS NAV 1 AND AHRS IAW MM 34-43-01 AND 34-22-0Jan 18, 2008 · N216AM · Doug DC987 · Landing and Taxi AidsSDR ASMF200708002Shutoff Valve · failedAIRCRAFT PERFORMED AN UNSCHEDULED LANDING, DUE TO A CABIN PRESSURE FAILURE AT FL340 USING ANTI ICE AND DE ICE FLOW, THIS CONDITION BECOME WORST WHEN TAIL DE ICE WAS USED AND THE PRESSURIZATION WAS UNCONTROLLABLE IN MANUAL AND AUTO. MAINTENANCE PERSONNEL PERFORAug 8, 2007 · N216AM · Doug DC987 · Pneumatic Distribution SystemSDR ASMF200704005Valve · leakingDURING TRANSIT CHECK, IT WAS DETECTED THE LT OB DUAL SERVO VALVE LEAKING. VALVE WAS REPLACED IAW M/M 32-43-03, TESTED CORRECT.Apr 9, 2007 · N216AM · Doug DC987 · Landing Gear Brake SystemSDR ASMF200703003Skin · dentedDURING TRANSIT CHECK, A DENT WAS DETECTED IN THE RT STATIC PORT AREA. DENT WAS LOCATED AT STATION 389 AND LONGERONS 25 AND 26 RT SIDE AND WAS INSPECTED IAW MM 34-11-01, BEING WITHIN LIMITS.Mar 10, 2007 · N216AM · Doug DC987 · Fuselage Main, Plate/SkinSDR ASMF200702002Skin · damagedDURING OVERNIGHT CHECK AND ACCOMPLISHMENT OF EO 985362, A CRACK OF .1250 LENGTH AT STA Y 198 BETWEEN LONGERONS L20L AND L21L, WAS DETECTED ON THE MAIN STAIRS DOOR. DAMAGED SKIN SECTION WAS REMOVED AND A DOUBLER (PERMANENT REPAIR) WAS INSTALLED IAW SRM 53-05 FIFeb 3, 2007 · N216AM · Doug DC987 · Fuselage Main, Plate/SkinSDR ASMF200701007Blade · nickedDURING TRANSIT CHECK, A BLADE WAS DETECTED DAMAGED DUE TO A FOD IN RT ENGINE. A NICK WAS DETECTED AT 2.5 INCHES BETWEEN PLATFORM AND MIDSPAN SHROUD OF 1 INCH LONG WITH .1250 INCH DEPTH. THE BLADE WAS REWORKED IAW MM 72-33-21 AND BOROSCOPIC INSPECTION WAS PERFOJan 29, 2007 · N216AM · Doug DC987 · Turbine Engine Air Inlet SectionSDR ASMF200612001Pump · leakingAIRCRAFT RETURNED DUE TO RT HYDRAULIC SYSTEM LOST. DURING MAINTENANCE CHECK, THE HYDRAULIC CONTAINER WAS EMPTY AND WITH A DRIP IN THE RT AFT CARGO COMPARTMENT. AIRCRAFT WAS SENT TO THE HANGAR AND A BROKEN LINE IN THE RT HYDRAULIC SYSTEM MODULE AND (3) CLAMPS WDec 2, 2006 · N216AM · Doug DC987 · Hydraulic Pump (Electric/Engine), MainSDR ASMF200610011Transmitter · failedAIRCRAFT REJECTED TAKEOFF AT 60 KNOTS, THE LT ENGINE DID NOT ACCELERATE MORE THAN 1.2 EPR’S, WITH THRUST LEVERS TOTALLY FORWARD, EGT INCREASED TO 570 DEGREE (C) AND N1 AND N2 WERE NORMAL. AIRCRAFT WAS SENT TO THE HANGAR AND ENGINE WAS TESTED IAW MM 71-00-00, EOct 27, 2006 · N216AM · Doug DC987 · Engine Pressure Ratio (EPR)SDR ASMF200607006Blades · damagedDURING TRANSIT CHECK, 2 BLADES OF LT ENGINE WERE DETECTED DAMAGED BY FOD. DAMAGES WERE 1.8750 INCH FROM BLADE ROOT TO MID SPAN, ONE WITH 0.040 INCH DEPTH AND .5625 INCH LONG, AND THE OTHER ONE WITH 0.030 INCH DEPTH AND .5625 INCH LONG. AIRCRAFT WAS SENT TO THEJul 7, 2006 · N216AM · Doug DC987 · Turbine Engine Compressor SectionSDR ASMF200604007Transmitter · failedAIRCRAFT ABORTED TAKEOFF AND RETURNED TO PLATFORM AS A CONSEQUENCE OF THE LEFT ENGINE DID NOT ACCELERATE WITH EPR'S ON 1.4 AND EGT'S LIGHT BLINKING. WATER TRAMP WAS DRAINED AND ACCELERATION CHAMBER WAS LUBRICATED IAW MM 73-20-03 AND 73-20-01. DURING ENGINES Apr 15, 2006 · N216AM · Doug DC987 · Engine Pressure Ratio (EPR)SDR ASMF200603008Vhf Comm · failedAIRCRAFT REJECTED TAKEOFF AT 70 KTS AND RETURNED TO PLATFORM, VHF COMM NR 1 FAILED IN FORWARD 118.1 FREQUENCY. SYSTEM WAS TESTED IAW MM 23-20-00, BEING CORRECT. MAIN LANDING GEAR BRAKES WERE CHECKED IAW MM 32-42-01, ALL CORRECT.Mar 16, 2006 · N216AM · Doug DC987 · VHF Communications SystemSDR ASMF200601017Start Valve · failedAIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF THE LIGHT OF THE RIGHT START VALVE TURNED ON. THE START VALVE REPORT WAS DEFERRED IAW MEL 80-1. DURING OVERNIGHT CHECK, THE RIGHT START VALVE WAS REPLACED IAW MM 80-10-02, TESTED CORRECT.Jan 28, 2006 · N216AM · Doug DC987 · Engine CrankingSDR ASMF200601014Engine · failedAIRCRAFT RETURNED TO PLATFORM, DURING TAXING CAPTAIN INFORMED THAT THE RT ENGINE DID NOT START, THERE WAS NO ROTATION OF N2. THE START VALVE WAS OPENED MANUALLY BUT THE STARTING WAS NOT POSSIBLE. THE STARTER WAS REPLACED BUT THE CONDITION CONTINUED. METALLIC DJan 23, 2006 · N216AM · Doug DC987 · Engine (Turbine/Turboprop)SDR ASMF200512012Shutoff Valve · malfunctionedAIRCRAFT RETURNED TO PLATFORM DURING RT ENGINE STARTING, IT DID NOT HAVE TURN IN N1 AND N2 AND OIL PRESSURE INDICATION. THE RT STARTER AND SHUTOFF VALVE WERE REPLACED IAW MM 80-10-02 AND MM 80-00-00 RESPECTIVELY, TESTED CORRECT.Dec 12, 2005 · N216AM · Doug DC987 · Engine Starting SystemSDR ASMF200508015Starter · failedAIRCRAFT RETURNED TO PLATFORM DURING LT ENGINE STARTING, THE STARTER VALVE LIGHT TURNED ON BUT IT DID NOT HAVE TURN IN N2. DURING MAINTENANCE REVISION, THE LT STARTER WAS DETECTED DAMAGED. THE LT STARTER AND STARTER VALVE WERE REPLACED IAW MM 80-10-01/02 RESPEAug 27, 2005 · N216AM · Doug DC987 · Engine StarterSDR ASMF200508009Symbol Generator · inoperativeAIRCRAFT RETURNED OF FLIGHT, DURING ROTATION HEARD A LOUD NOISE IN THE NOSE LANDING GEAR, LOOSING AHRS 2 WITH HEADING, HORIZON LIGHTS TURNED ON, FMA AND RIGHT ND WITHOUT INFORMATION. AHRS 2 AND 3 WERE SWAPPED IAW MM 34-21-10 AND VISUAL INSPECTION OF NLG WAS PEAug 18, 2005 · N216AM · Doug DC987 · Attitude Gyro and Indicating SystemSDR ASMF200507014Anti-Ice Valve · failedACFT PERFORMED AN UNSCHEDULED LANDING DUE TO PRESSURIZATION FAILURE, AFTER 45 MIN OF USING ANTI-ICE, AT 350 FLT LEVEL, FLOW & CABIN ALT LIGHT TURNED ON. CAPTAIN ACCOMPLISHED THE ABNORMAL PROCEDURE & PERFORMED AN UNSCHEDULED LANDING. DURING REVISION OXYGEN GENSJul 18, 2005 · N216AM · Doug DC987 · Ice/Rain Protection SystemSDR ASMF200411012Pipe · damagedDURING TRANSIT CHECK, A HYDRAULIC LEAK WAS DETECTED IN RIGHT FLIGHT INTERIOR SPOILER. HYDRAULIC PRESSURE LINE WAS DETECTED WITH DAMAGES AND WAS REPLACED IAW MM 27-62-02, TEST CORRECT.Nov 29, 2004 · N216AM · Doug DC987 · Hydraulic System, MainSDR ASMF200410009Fuel Control · malfunctionedAIRCRAFT RETURNED TO PLATFORM, DURING ENGINES STARTING, LT ENGINE WAS UNDER IDLE MINIMUM THRUST REQUIREMENTS, ABNORMAL PROCEDURE WAS APPLIED AND BUT REMAIN THE SAME CONDITION AND FUEL FLOW WAS UNSTABLE. ACCELERATION CAM WAS SERVICED AND WATER TRAMP WAS DRAINEDOct 10, 2004 · N216AM · Doug DC987 · Fuel Control/Turbine EnginesSDR ASMF200410001Tab · lightning strikeDURING TRANSIT CHECK, CAPTAIN REPORTED LIGHTNING STRIKE. THE FOLLOWING NON ROUTINE CARDS WERE GENERATED AND ATTENDED TO CORRECT DAMAGES. RT ELEVATOR GEAR TAB T/E IN 5 SMALL POINTS. RT ELEVATOR ANTI-FLOAT TAB T/E. TWO FASTENERS MELTED FUSELAGE SKIN IN JOINOct 4, 2004 · N216AM · Doug DC987 · Elevator, Tab StructureSDR ASMF200408012Sensor · stuckAIRCRAFT RETURNED TO PLATFORM, DURING TAXING SLAT DISAGREE LIGHT TURNED ON WITH FLAPS UP. DURING CHECK TECHNICAL PERSONNEL DETECTED RT WING D SENSOR GOT STUCK. IT WAS CLEANED AND LUBRICATED AND SLAT/FLAP INDICATIONS RETURNED TO NORMAL, TEST WERE PERFORMED IAW Aug 12, 2004 · N216AM · Doug DC987 · Leading Edge Slat Position Indicating SystemSDR ASMF200407032Proximity Sensor · dirtyAIRCRAFT RETURNED TO PLATFORM, (RUDDER TRAVEL UNRESTRICTED) LIGHT TURNED OFF BEFORE TAKE OFF AND LT GENERATOR INOPERATIVE. PSEU TEST WAS PERFORMED, ALL CORRECT; RUDDER LIMITER PROXIMITY SWITCH WAS CLEANED AND CHECKED, RUDDER WAS ACTUATED WITH HYDRAULIC PRESSURJul 29, 2004 · N216AM · Doug DC987 · Rudder Control SystemSDR ASMF200407027Csd · failedAIRCRAFT RETURNED OF FLIGHT, HIGH TEMPERATURE ON LT CONSTANT SPEED DRIVE (CSD), AND APU OUT OF SERVICE. LT CSD WAS CHECKED AND HIGH LEVEL OF OIL WAS DETECTED, OIL SERVICE WAS PERFORMED IAW MM 12-12-52, CSD AND APU WERE OPERATIVE, ALL CORRECT. DURING OVERNIGHJul 24, 2004 · N216AM · Doug DC987 · Alternator-Generator DriveSDR ASMF200406011Exciter · failedAIRCRAFT RETURNED TO PLATFORM, ENGINE NR 2 WITHOUT IGNITION. CAPTAIN PERFORMED ENGINE START IN OVERRIDE POSITION AND FAIL CONTINUED. EXCITER IGNITION BOX WAS REPLACED IAW MM 74-10-01, TEST CORRECT.Jun 13, 2004 · N216AM · Doug DC987 · ExciterSDR ASMF200406008Water Separator · failedDURING TRANSIT CHECK, WATER WAS FOUND IN THE MIDDLE OF PASSENGERS CABIN CEILING. THE WATER LEAK WAS DETECTED BETWEEN CUSHIONS AND AIR CONDITIONING DUCT IN THE CEILING, THE EMERGENCY LOCATOR ANTENNA WAS SEALED IN THE STATIONS Y937 AND Y980 IN THE UPPER FUSELAGEJun 9, 2004 · N216AM · Doug DC987 · Humidity Control SystemSDR ASMF200406007Solenoid Valve · failedDURING TRANSIT CHECK, WATER WAS FOUND IN THE MIDDLE OF PASSENGERS CABIN CEILING. THE WATER LEAK WAS DETECTED BETWEEN CUSHIONS AND AIR CONDITIONING DUCT IN THE CEILING, THE EMERGENCY LOCATOR ANTENNA WAS SEALED IN THE STATIONS Y937 AND Y980 IN THE UPPER FUSELAGEJun 9, 2004 · N216AM · Doug DC987 · Ice/Rain Protection SystemSDR ASMF200405025Fastener · lightning strikeDURING TRANSIT CHECK, A LIGHTING STRIKE WAS DETECTED ON THE FUSELAGE LT SIDE, FORWARD OF THE WING WITH SOME FASTENERS DAMAGED. LIGHTING STRIKE INSPECTION WAS PERFORMED IAW MM 05-53-00, ALL CORRECT. FASTENERS WERE REPLACED IAW MM 43-04 FIG 38 TABLE B CONDITION May 24, 2004 · N216AM · Doug DC987 · FastenersSDR ASMF200405004Servo · failedDURING TRANSIT CHECK, CAPTAIN REPORTED A DIFFERENCE BETWEEN THROTTLES OF 1.5 INCHES. AUTOTHROTTLE SERVO UNIT WAS REPLACED IAW MM 22-31-01. TRIMMING WAS PERFORMED IAW MPCM 71-00-01 AND AUTOTHROTTLE CLUTCH DRUMS SERVICE WAS PERFORMED IAW MM 76-11-04, TEST CORRECMay 2, 2004 · N216AM · Doug DC987 · Auto Throttle SystemSDR ASMF200405003Strainer · failedAIRCRAFT RETURNED TO PLATFORM. (LT STRAINER CLOGGING) LIGHT TURNED ON AND INTERFERENCE PROBLEMS IN LT SPEAKER. OIL FILTER AND DIFFERENTIAL PRESSURE SWITCH WERE REPLACED IAW MM 79-20-06 AND 79-35-01, RESPECTIVELY, AND TEST WAS PERFORMED IAW MM 79-00-00, ALL COMay 2, 2004 · N216AM · Doug DC987 · Engine Oil Indicating SystemSDR ASMF200403004Control Panel · failedAIRCRAFT RETURNED OF FLIGHT DUE TO ESDP RIGHT PANEL WAS OUT OF SERVICE AND WITHOUT INFORMATION. TEST PANEL WAS PERFORMED BUT FAIL CONTINUED. T34 CIRCUIT BREAKER WAS RESET, CORRECTING THE POWER SUPPLY TO THE RIGHT SIDE. CONNECTORS WERE CLEANED, ALL CORRECT.Mar 9, 2004 · N216AM · Doug DC987 · Instrument PanelSDR MEX2004067Engine · fodFLT 106 - GDL-MEX - DURING TRANSIT CHECK TWO BLADES ON LEFT ENGINE AND NOISE SUPPRESSOR WERE DETECTED WITH DAMAGE BY FOD. THE DAMAGES WERE WITHIN LIMITS IAW MM 72-33-22. THE BLADES WERE REPAIRED IAW MM 72-33-22. THE NON ROUTINE CARD NR A0055136 WAS ISSUED TFeb 18, 2004 · N216AM · Doug DC987 · Engine (Turbine/Turboprop)SDR MEX2003524Adc · failedAIRCRAFT RETURNED TO PLATFORM DUE TO A DIFFERENCE OF 6 KNOTS BETWEEN VELOCIMETERS. AT PLATFORM THE SYSTEM WAS CHECKED, CONFIRMING CADC NR 1 FAILURE. CADC NR 1 WAS REPLACED AND TESTED IAW MM 34-16-01. ADDITIONALLY BRAKE ASSEMBLY WAS CHECKED BY CONDITION, IAWNov 16, 2003 · N216AM · Doug DC987 · Air Data ComputerSDR MEX2003493Engine · out of trimCAPTAIN REPORTED THAT AFTER ENGINES STARTING READINGS IN LT ENGINE WERE OUT OF LIMITS N2 AND EGT`S RISE TO 480. TECHNICAL PERSONNEL PERFORMED TRIM TO LT ENGINE AND IT WAS TESTED IAW MM 73-2-01, BEING PARAMETERS BETWEEN THEIR OPERATIONAL LIMITS.(K)Oct 16, 2003 · N216AM · Doug DC987 · Engine (Turbine/Turboprop)SDR MEX2003403Control Cable · failedAIRCRAFT AIR TURN BACK, WHEN AIRBORE RT ENGINE BECAME ACCELERATING, IT WASN`T ABLE TO CONTROL IT, THROTTLE AT IDLE AND ENGINE AT MAXIMUM TRUST AND ENGINE WAS SHUT DOWN. DURING REVISION WAS DETECTED WITHOUT RT CONTROL ACCELERATOR AND THE 53C CABLE WAS FOUND BRAug 31, 2003 · N216AM · Doug DC987 · Power LeverSDR MEX2003297Thermostat · failedFLT 523 - MEX-VER - AIRCRAFT ARRIVED WITH CAPTAIN REPORT OF 'L ICE PROTECT TEMP HI AND R AIR CON TEMP HI' LIGHTS. THE ELECTRONIC THERMAL LEFT SW WAS REPLACED IAW MM 21-31-4. DURING OVERNIGHT SERVICE THE ANTICIPATOR AND THERMOSTAT RIGHT SIDE AND ELECTRONIC THJul 3, 2003 · N216AM · Doug DC987 · Pneumatic Indicating SystemSDR MEX2003268Microphone · failedAIRCRAFT RETURNED TO PLATFORM, BOTH VHF COM WERE OUT OF SERVICE. MICROPHONES WERE SWAPPED AND THEY WERE OPERATING IN A CORRECT WAY. DURING OVERNIGHT SERVICE THE MICROPHONE OF OBSERVERS SIDE WAS REPLACED IAW MM 23-50-00, ALL TEST CORRECT.May 7, 2003 · N216AM · Doug DC987 · VHF Communications SystemSDR MEX2003147Heat Exchanger · failedAIRCRAFT RETURN TO PLATFORM, ENGINE NR 2, FUEL LEAK. THE FUEL/OIL TEMPERATURE EXCHANGER WAS REPLACED IAW MM, TEST CORRECT.Apr 27, 2003 · N216AM · Doug DC987 · Engine Bleed Air SystemSDR MEX2003145Slat · out of adjustDURING TAKE OFF THE SLAT LIGHT DISAGREE TURN ON WITH 13 DEGREES OF ADJUSTMENT ON SLATS, DISAGREE LIGHT TURN ON BEFORE V1. THE FLAP/SLAT BAR AND POSITION WERE ADJUSTED IAW MM.Apr 27, 2003 · N216AM · Doug DC987 · Leading Edge DevicesSDR MEX2003126Fuel Control · malfunctionedCAPTAIN REPORTED, WHEN ANTI-ICE WAS TURNED ON LT ENGINE, EPR`S WENT DOWN AND RT ENGINE TO SLOW ACCELERATION REQUIRING 40 SECONDS TO ACCELERATE. DURING OVERNIGHT SERVICE LINE PS4 IN RIGHT FCU WAS DRAINED IAW MM, ANTIFLUCTUATION VALVES AND FCU ACCELERATION CAM Apr 8, 2003 · N216AM · Doug DC987 · Fuel Controlling SystemSDR MEX2002341Sensor · out of adjustFLT 950 - MEX-MTY - AIRCRAFT SUSPENDED TAKEOFF AS A RESULT OF SLAT DISAGREE LIGHT TURN O BETWEEN 60 AND 70 KNOW. AIRCRAFT WAS SENT TO THE MAIN BASE. TECHNICAL PERSONNEL PERFORMED A BITE PROXIMITY SWITCH IAW MM 32-60-04, ALL CORRECT. LEFT SLAT ADVISOR SENSORNov 15, 2002 · N216AM · Doug DC987 · Leading Edge Slat Position Indicating SystemSDR MEX2002111Fuel Control · out of rigFLT 278 - MEX-CJS - AIRCRAFT RETURNED TO PLATFORM AS CONSEQUENCE OF THRUST PROBLEM OF ENGINE NR 2. WHEN CAPTAIN TRIED TO MAKE EQUAL THE THRUST OF ENGINE TWO IT WAS UNDER 10 PERCENT. PERSONNEL REVIEW THE EPR'S TRANSMITTER AND THE PT2 AND PT7 LINES, ALL CORRECApr 13, 2002 · N216AM · Doug DC987 · Fuel Control/Turbine Engines
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