# Service difficulty reports: N216AM, cancelled Feb 7, 2012

A list on [N216AM, cancelled Feb 7, 2012](https://openairdocs.org/deregistered/N216AM-2012-02-07.md).

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

- [SDR 2008FA0000490](https://openairdocs.org/sdr/2008FA0000490.md): Acoustic Liner · damaged · Jun 22, 2008 · N216AM · Doug DC987 · Engine (Turbine/Turboprop)
  > AC 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 72-00
- [SDR ASMF200805004](https://openairdocs.org/sdr/ASMF200805004.md): Strut · failed · May 23, 2008 · N216AM · Doug DC987 · Nose/Tail Landing Gear Strut/Axle
  > AIRCRAFT 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 CORRE
- [SDR ASMF200801001](https://openairdocs.org/sdr/ASMF200801001.md): Ils System · malfunctioned · Jan 18, 2008 · N216AM · Doug DC987 · Landing and Taxi Aids
  > CAPTAIN 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 34-22-0
- [SDR ASMF200708002](https://openairdocs.org/sdr/ASMF200708002.md): Shutoff Valve · failed · Aug 8, 2007 · N216AM · Doug DC987 · Pneumatic Distribution System
  > AIRCRAFT 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 PERFOR
- [SDR ASMF200704005](https://openairdocs.org/sdr/ASMF200704005.md): Valve · leaking · Apr 9, 2007 · N216AM · Doug DC987 · Landing Gear Brake System
  > DURING TRANSIT CHECK, IT WAS DETECTED THE LT OB DUAL SERVO VALVE LEAKING. VALVE WAS REPLACED IAW M/M 32-43-03, TESTED CORRECT.
- [SDR ASMF200703003](https://openairdocs.org/sdr/ASMF200703003.md): Skin · dented · Mar 10, 2007 · N216AM · Doug DC987 · Fuselage Main, Plate/Skin
  > DURING 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.
- [SDR ASMF200702002](https://openairdocs.org/sdr/ASMF200702002.md): Skin · damaged · Feb 3, 2007 · N216AM · Doug DC987 · Fuselage Main, Plate/Skin
  > DURING 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 FI
- [SDR ASMF200701007](https://openairdocs.org/sdr/ASMF200701007.md): Blade · nicked · Jan 29, 2007 · N216AM · Doug DC987 · Turbine Engine Air Inlet Section
  > DURING 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 PERFO
- [SDR ASMF200612001](https://openairdocs.org/sdr/ASMF200612001.md): Pump · leaking · Dec 2, 2006 · N216AM · Doug DC987 · Hydraulic Pump (Electric/Engine), Main
  > AIRCRAFT 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 W
- [SDR ASMF200610011](https://openairdocs.org/sdr/ASMF200610011.md): Transmitter · failed · Oct 27, 2006 · N216AM · Doug DC987 · Engine Pressure Ratio (EPR)
  > AIRCRAFT 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, E
- [SDR ASMF200607006](https://openairdocs.org/sdr/ASMF200607006.md): Blades · damaged · Jul 7, 2006 · N216AM · Doug DC987 · Turbine Engine Compressor Section
  > DURING 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 THE
- [SDR ASMF200604007](https://openairdocs.org/sdr/ASMF200604007.md): Transmitter · failed · Apr 15, 2006 · N216AM · Doug DC987 · Engine Pressure Ratio (EPR)
  > AIRCRAFT 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
- [SDR ASMF200603008](https://openairdocs.org/sdr/ASMF200603008.md): Vhf Comm · failed · Mar 16, 2006 · N216AM · Doug DC987 · VHF Communications System
  > AIRCRAFT 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.
- [SDR ASMF200601017](https://openairdocs.org/sdr/ASMF200601017.md): Start Valve · failed · Jan 28, 2006 · N216AM · Doug DC987 · Engine Cranking
  > AIRCRAFT 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.
- [SDR ASMF200601014](https://openairdocs.org/sdr/ASMF200601014.md): Engine · failed · Jan 23, 2006 · N216AM · Doug DC987 · Engine (Turbine/Turboprop)
  > AIRCRAFT 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 D
- [SDR ASMF200512012](https://openairdocs.org/sdr/ASMF200512012.md): Shutoff Valve · malfunctioned · Dec 12, 2005 · N216AM · Doug DC987 · Engine Starting System
  > AIRCRAFT 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.
- [SDR ASMF200508015](https://openairdocs.org/sdr/ASMF200508015.md): Starter · failed · Aug 27, 2005 · N216AM · Doug DC987 · Engine Starter
  > AIRCRAFT 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 RESPE
- [SDR ASMF200508009](https://openairdocs.org/sdr/ASMF200508009.md): Symbol Generator · inoperative · Aug 18, 2005 · N216AM · Doug DC987 · Attitude Gyro and Indicating System
  > AIRCRAFT 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 PE
- [SDR ASMF200507014](https://openairdocs.org/sdr/ASMF200507014.md): Anti-Ice Valve · failed · Jul 18, 2005 · N216AM · Doug DC987 · Ice/Rain Protection System
  > ACFT 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 GENS
- [SDR ASMF200411012](https://openairdocs.org/sdr/ASMF200411012.md): Pipe · damaged · Nov 29, 2004 · N216AM · Doug DC987 · Hydraulic System, Main
  > DURING 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.
- [SDR ASMF200410009](https://openairdocs.org/sdr/ASMF200410009.md): Fuel Control · malfunctioned · Oct 10, 2004 · N216AM · Doug DC987 · Fuel Control/Turbine Engines
  > AIRCRAFT 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 DRAINED
- [SDR ASMF200410001](https://openairdocs.org/sdr/ASMF200410001.md): Tab · lightning strike · Oct 4, 2004 · N216AM · Doug DC987 · Elevator, Tab Structure
  > DURING 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 JOIN
- [SDR ASMF200408012](https://openairdocs.org/sdr/ASMF200408012.md): Sensor · stuck · Aug 12, 2004 · N216AM · Doug DC987 · Leading Edge Slat Position Indicating System
  > AIRCRAFT 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
- [SDR ASMF200407032](https://openairdocs.org/sdr/ASMF200407032.md): Proximity Sensor · dirty · Jul 29, 2004 · N216AM · Doug DC987 · Rudder Control System
  > AIRCRAFT 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 PRESSUR
- [SDR ASMF200407027](https://openairdocs.org/sdr/ASMF200407027.md): Csd · failed · Jul 24, 2004 · N216AM · Doug DC987 · Alternator-Generator Drive
  > AIRCRAFT 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 OVERNIGH
- [SDR ASMF200406011](https://openairdocs.org/sdr/ASMF200406011.md): Exciter · failed · Jun 13, 2004 · N216AM · Doug DC987 · Exciter
  > AIRCRAFT 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.
- [SDR ASMF200406008](https://openairdocs.org/sdr/ASMF200406008.md): Water Separator · failed · Jun 9, 2004 · N216AM · Doug DC987 · Humidity Control System
  > DURING 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 FUSELAGE
- [SDR ASMF200406007](https://openairdocs.org/sdr/ASMF200406007.md): Solenoid Valve · failed · Jun 9, 2004 · N216AM · Doug DC987 · Ice/Rain Protection System
  > DURING 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 FUSELAGE
- [SDR ASMF200405025](https://openairdocs.org/sdr/ASMF200405025.md): Fastener · lightning strike · May 24, 2004 · N216AM · Doug DC987 · Fasteners
  > DURING 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
- [SDR ASMF200405004](https://openairdocs.org/sdr/ASMF200405004.md): Servo · failed · May 2, 2004 · N216AM · Doug DC987 · Auto Throttle System
  > DURING 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 CORREC
- [SDR ASMF200405003](https://openairdocs.org/sdr/ASMF200405003.md): Strainer · failed · May 2, 2004 · N216AM · Doug DC987 · Engine Oil Indicating System
  > AIRCRAFT 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 CO
- [SDR ASMF200403004](https://openairdocs.org/sdr/ASMF200403004.md): Control Panel · failed · Mar 9, 2004 · N216AM · Doug DC987 · Instrument Panel
  > AIRCRAFT 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.
- [SDR MEX2004067](https://openairdocs.org/sdr/MEX2004067.md): Engine · fod · Feb 18, 2004 · N216AM · Doug DC987 · Engine (Turbine/Turboprop)
  > FLT 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 T
- [SDR MEX2003524](https://openairdocs.org/sdr/MEX2003524.md): Adc · failed · Nov 16, 2003 · N216AM · Doug DC987 · Air Data Computer
  > AIRCRAFT 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, IAW
- [SDR MEX2003493](https://openairdocs.org/sdr/MEX2003493.md): Engine · out of trim · Oct 16, 2003 · N216AM · Doug DC987 · Engine (Turbine/Turboprop)
  > CAPTAIN 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)
- [SDR MEX2003403](https://openairdocs.org/sdr/MEX2003403.md): Control Cable · failed · Aug 31, 2003 · N216AM · Doug DC987 · Power Lever
  > AIRCRAFT 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 BR
- [SDR MEX2003297](https://openairdocs.org/sdr/MEX2003297.md): Thermostat · failed · Jul 3, 2003 · N216AM · Doug DC987 · Pneumatic Indicating System
  > FLT 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 TH
- [SDR MEX2003268](https://openairdocs.org/sdr/MEX2003268.md): Microphone · failed · May 7, 2003 · N216AM · Doug DC987 · VHF Communications System
  > AIRCRAFT 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.
- [SDR MEX2003147](https://openairdocs.org/sdr/MEX2003147.md): Heat Exchanger · failed · Apr 27, 2003 · N216AM · Doug DC987 · Engine Bleed Air System
  > AIRCRAFT RETURN TO PLATFORM, ENGINE NR 2, FUEL LEAK. THE FUEL/OIL TEMPERATURE EXCHANGER WAS REPLACED IAW MM, TEST CORRECT.
- [SDR MEX2003145](https://openairdocs.org/sdr/MEX2003145.md): Slat · out of adjust · Apr 27, 2003 · N216AM · Doug DC987 · Leading Edge Devices
  > DURING 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.
- [SDR MEX2003126](https://openairdocs.org/sdr/MEX2003126.md): Fuel Control · malfunctioned · Apr 8, 2003 · N216AM · Doug DC987 · Fuel Controlling System
  > CAPTAIN 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
- [SDR MEX2002341](https://openairdocs.org/sdr/MEX2002341.md): Sensor · out of adjust · Nov 15, 2002 · N216AM · Doug DC987 · Leading Edge Slat Position Indicating System
  > FLT 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 SENSOR
- [SDR MEX2002111](https://openairdocs.org/sdr/MEX2002111.md): Fuel Control · out of rig · Apr 13, 2002 · N216AM · Doug DC987 · Fuel Control/Turbine Engines
  > FLT 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 CORREC

## 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 = 'N216AM' AND deregistration_id = 'N216AM-2012-02-07'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N216AM-2012-02-07/reports

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