# Service difficulty reports: N803ML, cancelled Aug 12, 2010

A list on [N803ML, cancelled Aug 12, 2010](https://openairdocs.org/deregistered/N803ML-2010-08-12.md).

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

Page 1 of 2 · 58 reports

- [SDR ASMF 20090303](https://openairdocs.org/sdr/ASMF%2020090303.md): Wire · damaged · Mar 20, 2009 · N803ML · Doug DC987 · Air Conditioning System Wiring
  > AIRCRAFT RETURNED TO DEPARTURE DUE TO PRESSURIZATION SYSTEM FAIL DURING THE INITIAL CLIMB, CABIN ALTITUDE AND FLOW LIGHTS CAME ON. MX REPLACED BOTH WIRING SECOND SEGMENT SWITCHES IAW AMM 21-31-09, THE PRESSURE CONTROLLER WAS REPLACED IAW AMM 21-32-03, THE WIR
- [SDR MAS2008F00065](https://openairdocs.org/sdr/MAS2008F00065.md): Prbc · malfunctioned · Aug 23, 2008 · N803ML · Doug DC987 · Compressor Bleed Control
  > ACFT REJECTED TAKE OFF AT 70 KNOTS DUE TO RT ENGINE DID NOT ACCELERATE. MX PERSONNEL REPLACED PRBC`S IAW MM 75-31-01 AND FCU IAW 73-20-01. ADDITIONALLY THE PS3 WAS VERIFIED AND CLEANED, THE BLEED VALVES WERE LUBRICATED IAW 75-31-05 AND TRIM BOTH ENGINES WAS
- [SDR MAS2008F00063](https://openairdocs.org/sdr/MAS2008F00063.md): Engine · malfunctioned · Aug 23, 2008 · N803ML · Doug DC987 · Engine (Turbine/Turboprop)
  > ACFT REJECTED TAKE OFF 70 KNOT DUE TO RT ENGINE DID NOT ACCELERATE (EPR 1.14). MX PERSONNEL CHECKED THE RT ENGINE IAW MM 72-00-00 PAGE 501, ALL CORRECT. ADDITIONALLY, A HIGH ENERGY STOP INSPECTION WAS PERFORMED IAW MM 05-57-00, NO DAMAGES WERE FOUND. DURING
- [SDR ASMF200801002](https://openairdocs.org/sdr/ASMF200801002.md): Blades · damaged · Jan 24, 2008 · N803ML · Doug DC987 · Turbine Engine Compressor Section
  > DURING OVERNIGHT CHECK, 10 FAN BLADES OF THE RT ENG WERE DETECTED WITH DENTS AND LOSS OF MATERIAL DUE TO AN FOD. MAINTENANCE PERFORMED A BOROSCOPIC INSP IAW MM 72-00-00 AND NO ADDITIONAL DAMAGES WERE FOUND; THE 10 DAMAGED BLADES WERE REPAIRED IAW MM 72-33-21,
- [SDR ASMF200709003](https://openairdocs.org/sdr/ASMF200709003.md): Powerplant · overspeed · Sep 5, 2007 · N803ML · Doug DC987 · Auto Throttle System
  > CAPTAIN REPORTED WINDSHEAR DURING APPROACH AND ATS DISCONNECTED, SPEED DECREASED, SO AUTOTHOTTLES WERE SET TO THE MAXIMUM POWER. AT PLATFORM, MAINTENANCE PERSONNEL DOWNLOAD THE ENGINES INFORMATION FROM THE MINIQAR DETECTING THAT THE RT ENGINE HAD VALUES OF N1
- [SDR ASMF200706006](https://openairdocs.org/sdr/ASMF200706006.md): Turbine Blades · cracked · Jun 28, 2007 · N803ML · Doug DC987 · Turbine Section
  > DURING LT ENGINE BOROSCOPIC INSPECTION WAS DETECTED A FIRST STAGE TURBINE BLADE WITH A CRACK OF 0.500 INCH IN TIP. ENGINE WAS REPLACED IAW MM 71-00-02 AND OPERATIONALLY TESTED IAW MM 71-00-01, ALL CORRECT.
- [SDR ASMF200703008](https://openairdocs.org/sdr/ASMF200703008.md): Engine · overspeed · Mar 27, 2007 · N803ML · Doug DC987 · Engine (Turbine/Turboprop)
  > AIRCRAFT REJECTED TAKEOFF AT 77 KNOTS DUE TO LT ENGINE REACHED ONLY 1.6 EPR WITH N1 104 PERCENT. AIRCRAFT WAS SENT TO THE HANGAR AND ENGINE WAS REMOVED AND SENT TO THE SHOP. THE NRC A0111096 WAS ISSUED TO CHECK ENGINE PT2 AND PT7 LINES AND MANIFOLD BY LEAKS I
- [SDR ASMF200703007](https://openairdocs.org/sdr/ASMF200703007.md): Unknown · unknown · Mar 27, 2007 · N803ML · Doug DC987 · Engine (Turbine/Turboprop)
  > AIRCRAFT REJECTED TAKEOFF AT 75 KNOTS DUE TO LT ENGINE REACHED ONLY 1.6 EPR WHILE RT ENGINE REACHED 2.04 EPR WITH N1 100 PERCENT, SO AIRCRAFT WAS SENT TO THE HANGAR AND MAINTENANCE PERSONNEL CHECKED ENGINE INLET/OUTLET, CONTROLS, PT2 AND PT7 LINES AND MANIFOL
- [SDR ASMF200703006](https://openairdocs.org/sdr/ASMF200703006.md): Seal · leaking · Mar 17, 2007 · N803ML · Doug DC987 · Wing, Plate/Skin
  > DURING TRANSIT CHECK, A FUEL LEAK WAS DETECTED IN AN UPPER PANEL OF THE LT WING. MAINTENANCE PERSONNEL RELOCATED THE SEAL AND APPLIED SEALANT IAW SRM 51-20-04 AND 51-22-2A, LEAK WAS CORRECTED. AS A PRECAUTIONARY ACTION, DURING OVERNIGHT CHECK THE SEAL WAS REP
- [SDR ASMF200702006](https://openairdocs.org/sdr/ASMF200702006.md): Unknown · unknown · Feb 15, 2007 · N803ML · Doug DC987 · AC Generation System
  > CAPTAIN REPORTED THAT A GEN LOW AND TAIL COMP TEMP HIGH LIGHTS TURNED ON. DURING MAINTENANCE CHECK, THE TAIL CONE COMPARTMENT WAS DETECTED WITH HIGH TEMPERATURE AND THE FIRE EXTINGUISHER CONTAINER ACTIVATED. AIRCRAFT WAS SENT TO THE HANGAR AND RT FIRE EXTINGUI
- [SDR ASMF200611002](https://openairdocs.org/sdr/ASMF200611002.md): Csd · failed · Nov 2, 2006 · N803ML · Doug DC987 · Alternator-Generator Drive
  > AIRCRAFT RETURNED DUE TO HIGH TEMPERATURE IN THE LT CSD AND APU DID NOT START AT 34,000 FEET. DURING OVERNIGHT CHECK, LT CSD AND HEAT EXCHANGER WERE REPLACED IAW MM 24-10-01 AND 24-10-03, AS WELL AS TRIM AND TEST WERE PERFORMED TO THE APU IAW MM 49-00-00, ALL
- [SDR ASMF200608014](https://openairdocs.org/sdr/ASMF200608014.md): Skin · damaged · Aug 23, 2006 · N803ML · Doug DC987 · Cargo/Baggage Doors
  > DURING TRANSIT CHECK, AIRCRAFT HAD A STRIKE ON THE FORWARD SERVICE DOOR BY A CATERING SERVICE TRUCK, PRODUCING A DAMAGE OF 4 X 3 INCHES LENGTH AND 0.085 INCHES DEPTH, BETWEEN LONGERONS 20 AND 21 AND STATIONS 168 THROUGH 180. THE DAMAGED AREA WAS INSPECTED BEIN
- [SDR ASMF200608015](https://openairdocs.org/sdr/ASMF200608015.md): Connector · contaminated · Aug 22, 2006 · N803ML · Doug DC987 · Fire Protection System Wiring
  > AIRCRAFT RETURNED, (FIRE DETECTOR LOOP A), (APU FIRE) AND (LT CSD HIGH TEMPERATURE) LIGHTS TURNED ON, AUDIBLE ALARM WAS ACTIVATED, LT GENERATOR WAS INOPERATIVE AND CAPTAIN ACTIVATED FIRE EXTINGUISHER BOTTLES. AIRCRAFT WAS SENT TO THE HANGAR AND FIRE DETECTION
- [SDR ASMF200608006](https://openairdocs.org/sdr/ASMF200608006.md): Coupling · damaged · Aug 10, 2006 · N803ML · Doug DC987 · Engine Starting System
  > AIRCRAFT RETURNED TO PLATFORM, LT ENGINE DID NOT HAVE TURN IN N1, NEITHER PNEUMATIC SUPPLY AND THE STARTER VALVE LIGHT OPERATING CORRECT. DURING MAINTENANCE REVIEW, THE ENGINE STARTER COUPLE WAS FOUND DAMAGED. THE COUPLE WAS REPLACED IAW MM 80-00-00, TESTED CO
- [SDR ASMF200608005](https://openairdocs.org/sdr/ASMF200608005.md): Coupling · damaged · Aug 9, 2006 · N803ML · Doug DC987 · Engine Starting System
  > AIRCRAFT RETURNED TO PLATFORM DUE TO THE LT ENGINE DID NOT HAVE TURN IN N2. DURING MAINTENANCE REVIEW, THE ENGINE STARTER COUPLE WAS FOUND DAMAGED. THE COUPLE WAS REPLACED IAW MM 80-00-00, TESTED CORRECT.
- [SDR ASMF200605011](https://openairdocs.org/sdr/ASMF200605011.md): Engine · malfunctioned · May 20, 2006 · N803ML · Doug DC987 · Engine (Turbine/Turboprop)
  > AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF DURING LEFT ENGINE START THE TEMPERATURE REACHED 510 DEGREES CELSIUS. DURING MAINTENANCE REVISION, FUEL WAS IN ENGINE CHAMBER NR 1. OVER TEMPERATURE INSPECTION WAS PERFORMED IAW MM 72-00-00, AND ENGINE STARTE
- [SDR ASMF200605002](https://openairdocs.org/sdr/ASMF200605002.md): Warning System · malfunctioned · May 11, 2006 · N803ML · Doug DC987 · Landing Gear Position and Warning
  > AIRCRAFT RETURNED OF FLIGHT AS A CONSEQUENCE OF -L & R LANDING GEAR- LIGHTS REMAINED ON WITH MAIN LANDING GEAR LEVER IN UP POSITION. PROXIMITY SWITCH COMPUTER AND D1-25 AND D1-26 SENSORS WERE TESTED AND CHECKED IAW MM 32-60-04 AND MM 32-31-04, RESPECTIVELY, B
- [SDR ASMF200604002](https://openairdocs.org/sdr/ASMF200604002.md): Circuit Breaker · failed · Apr 4, 2006 · N803ML · Doug DC987 · Central Display
  > AIRCRAFT AIR TURNED BACK AS A CONSEQUENCE OF LOST OF INDICATION OF THE RIGHT OIL PRESS, OIL TEMP, FUEL TEMP, HYD QTY, HYD PRESS AND FLAPS. THE CIRCUIT BREAKERS ASSOCIATED WITH THE FAILURE WERE CHECKED, FOUND THEM IN CLOSE POSITION. THE CIRCUIT BREAKER T-34 O
- [SDR ASMF20060309](https://openairdocs.org/sdr/ASMF20060309.md): Fcu · leaking · Mar 16, 2006 · N803ML · Doug DC987 · APU Engine Fuel and Control
  > A FUEL LEAK WAS DETECTED DURING APU STARTING. APU WAS DEFERRED IAW MM 49-1 AND AFT ACCESSORIES AREA WAS CHECKED, BEING CORRECT. DURING OVERNIGHT CHECK, THE FUEL CONTROL UNIT AND THE AIR CONDITIONING WATER SEPARATORS WERE REPLACED IAW MM 49-30-01 AND 21-20-02,
- [SDR ASMF200512010](https://openairdocs.org/sdr/ASMF200512010.md): Warning Horn · activated · Dec 9, 2005 · N803ML · Doug DC987 · Stabilizer Position Indicating
  > DURING GROUND TESTS, THE CAUTION LONG TRIM STABILIZER WAS OUT OF RANGE ACTIVATING THE TAKEOFF ALARM. AIRCRAFT WAS SENT TO THE HANGAR AND THE TRIM STABILIZER WAS TESTED IAW MM 27-40-12 AND DURING OVERNIGHT CHECK, THE TAKEOFF ALARM SYSTEM WAS VERIFIED IAW MM 27
- [SDR ASMF200511005](https://openairdocs.org/sdr/ASMF200511005.md): Coupler · failed · Nov 6, 2005 · N803ML · Doug DC987 · Engine Starter
  > DURING RIGHT ENGINE STARTING, THE RIGHT ENGINE DID NOT HAVE TURN IN N1 AND N2 AND START VALVE LIGHT TURNED ON. THE ADAPTER SHAFT STARTER WAS REPLACED IAW MM 80-10-01 PAGE 204, TESTED CORRECT. DURING OVERNIGHT CHECK, OPERATIONAL TEST WAS PERFORMED IAW MM 71-0
- [SDR ASMF200508008](https://openairdocs.org/sdr/ASMF200508008.md): Engine · making metal · Aug 17, 2005 · N803ML · Doug DC987 · Powerplant System
  > AIRCRAFT RETURNED TO PLATFORM, DURING RT ENGINE START, THE RT START VALVE OPEN LIGHT FLASHED AT 40 PERCENT RPM, N2 DECREASED TO 35 PERCENT AND RETURNED TO 50-56 PERCENT, 20 SECONDS AFTER THAT ENGINE STOPPED. AIRCRAFT WAS SENT TO THE HANGAR AND DURING MAINTENAN
- [SDR ASMF200508007](https://openairdocs.org/sdr/ASMF200508007.md): Augment Valve · out of adjust · Aug 16, 2005 · N803ML · Doug DC987 · Extinguishing System
  > AIRCRAFT RETURNED TO PLATFORM, DURING THE LT ENGINE START, THE FIRE EXTINGUISHER AGENT 2 LOW LIGHT TURNED ON. THE FIRE EXTINGUISHER POSITION 2 WAS REPLACED IAW MM 26-20-01; LT AUGMENTING VALVE WAS ADJUSTED IAW MM 36-10-01; THE CLAMS OF AUGMENTING VALVE AND REG
- [SDR ASMF200507007](https://openairdocs.org/sdr/ASMF200507007.md): Proximity Switch · out of adjust · Jul 8, 2005 · N803ML · Doug DC987 · Door Warning System
  > AIRCRAFT RETURNED TO PLATFORM, PASSENGER DOOR LIGHT COME ON. PASSENGER DOOR TEST WAS PERFORMED WITH A COMPLETE OPEN/CLOSE CYCLE IAW MM, BEING CORRECT. DURING OVERNIGHT SERVICE, THE GAP BETWEEN PRINTED CIRCUIT AND PROXIMITY SWITCH OF PASSENGER DOOR WAS VERIFIE
- [SDR ASMF200504024](https://openairdocs.org/sdr/ASMF200504024.md): Engine · malfunctioned · Apr 30, 2005 · N803ML · Doug DC987 · Engine (Turbine/Turboprop)
  > AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF CAPTAIN REPORTED DID NOT HAVE ACCELERATION IN RIGHT ENGINE. DURING CHECK BOTH ENGINES WERE DETECTED STABILIZED AT 52 PERCENT OF N2, TESTS WERE CORRECT. AIRCRAFT WAS SENT TO THE HANGAR AND TRIM TO BOTH ENGINES
- [SDR ASMF200504021](https://openairdocs.org/sdr/ASMF200504021.md): Cadc · failed · Apr 25, 2005 · N803ML · Doug DC987 · Altimeter, Barometric/Encoder
  > TECHNICAL PERSONNEL INFORMED THAT DURING TRANSIT CHECK AIR SPEED FLAG WAS SHOWN IN LEFT AIR SPEED INDICATOR AND ALTIMETER. TESTS WERE PERFORMED AND FAIL CONTINUED. CADC NR 1 WAS REPLACED IAW MM 34-16-01, TESTED CORRECT.
- [SDR ASMF200504020](https://openairdocs.org/sdr/ASMF200504020.md): Cadc · failed · Apr 23, 2005 · N803ML · Doug DC987 · Air Data Computer
  > AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF ADC NR 1 FAILURE, AUTO SLATS FAIL LIGHT TURNED ON AND RIGHT EFIS LOST INFORMATION. TESTS WERE PERFORMED CONFIRMING THE FAILURES. ADC NR 1, LEFT STALL COMPUTER AND RIGHT AHRU WERE REPLACED IAW MM 34-16-01, 34-
- [SDR ASMF200501017](https://openairdocs.org/sdr/ASMF200501017.md): Valve · malfunctioned · Jan 31, 2005 · N803ML · Doug DC987 · Pneumatic Indicating System
  > AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF AFTER ENGINES STARTED, EICAS MESSAGES "L ENG BLEED OFF" AND "PACK BITE" WERE SHOWN. CAPTAIN REPORTED THAT PURGE VALVE OF RIGHT ENGINE DID NOT OPEN, RESTARTED RIGHT ENGINE AND THE PURGE VALVE OPENED NORMALLY.
- [SDR ASMF200409008](https://openairdocs.org/sdr/ASMF200409008.md): Pump · failed · Sep 21, 2004 · N803ML · Doug DC987 · Hydraulic Pump (Electric/Engine), Main
  > AIRCRAFT RETURNED TO PLATFORM, LT HYDRAULIC PUMP FAILED. HYDRAULIC PUMP SOLENOID WAS CHECKED AND CIRCUIT BREAKERS WERE RESEATED AND FAIL CONTINUED. LT HYDRAULIC PUMP WAS REPLACED IAW MM 29-01-02, TEST CORRECT.
- [SDR ASMF200408008](https://openairdocs.org/sdr/ASMF200408008.md): Servo Valve · leaking · Aug 8, 2004 · N803ML · Doug DC987 · Hydraulic System, Main
  > DURING TRANSIT CHECK, HYDRAULIC LEAKAGE WAS DETECTED IN INTERIOR DOUBLE SERVO VALVE. IT WAS REPLACED IAW MM32-43-02, TEST WERE CORRECT.
- [SDR ASMF200407029](https://openairdocs.org/sdr/ASMF200407029.md): Warning Light · illuminated · Jul 24, 2004 · N803ML · Doug DC987 · Bleed Air Indicating System
  > AIRCRAFT RETURNED TO PLATFORM, LT ENGINE WITH LOW POWER AND IN IDLE POSITION TEMPERATURE REACHED 485 DEGREE (C) OUT OF LIMITS. AIRCRAFT WAS SENT TO THE HANGAR AND DURING OVERNIGHT SERVICE, THRUST LEVER TRIM WAS CHECKED IAW MM 76-11-00, LT ENGINE BLEED VALVES
- [SDR ASMF200407018](https://openairdocs.org/sdr/ASMF200407018.md): Prbc · failed · Jul 16, 2004 · N803ML · Doug DC987 · Compressor Bleed Control
  > DURING TRANSIT CHECK WAS DETECTED HIGH TEMPERATURE ON LT ENGINE, REACHED 482 DEGREE F. ENGINE RUNNING WAS PERFORMED TO VERIFY EGT INDICATION APPLYING PNEUMATIC AND ELECTRICAL CHARGES GETTING MAXIMUM TEMPERATURE INDICATION OF 445 DEGREE F, BEING WITHIN LIMITS
- [SDR ASMF200407001](https://openairdocs.org/sdr/ASMF200407001.md): Wheel · damaged · Jul 1, 2004 · N803ML · Doug DC987 · Wheel/Ski/Float
  > DURING TRANSIT CHECK, CAPTAIN REPORTED STRONG VIBRATION IN NOSE LANDING GEAR. BOTH NOSE LANDING GEAR WHEEL WERE REPLACED IAW MM 32-40-00, ALL CORRECT.
- [SDR ASMF200406036](https://openairdocs.org/sdr/ASMF200406036.md): Blade · damaged · Jun 30, 2004 · N803ML · Doug DC987 · Turbine Engine Compressor Section
  > DURING TRANSIT CHECK, LT ENGINE BLADE WAS DETECTED WITH DAMAGE FROM FOD. BLADE WAS REPAIRED IAW MM 72-33-21, ALL CORRECT.
- [SDR ASMF200406017](https://openairdocs.org/sdr/ASMF200406017.md): Computer · failed · Jun 18, 2004 · N803ML · Doug DC987 · Integrated Flight System
  > AIRCRAFT RETURNED TO PLATFORM, DURING TAXING AHRU NR 2 FAILED. AHRU WAS REPLACED IAW MM 34-21-10, TEST CORRECT. DURING OVERNIGHT SERVICE SYSTEM WAS CHECKED, ALL CORRECT.
- [SDR ASMF200406014](https://openairdocs.org/sdr/ASMF200406014.md): Ahrs · failed · Jun 15, 2004 · N803ML · Doug DC987 · Attitude Gyro and Indicating System
  > AIRCRAFT RETURNED, AHRU NR 1 FAILED. AIRCRAFT WAS DISPATCHED IAW ABNORMAL PROCEDURES MANUAL 10-4. DURING OVERNIGHT SERVICE, MAGNETIC FLOW VALVE WAS REPLACED IAW MM 34-21-06, TEST CORRECT.
- [SDR ASMF200406013](https://openairdocs.org/sdr/ASMF200406013.md): Gyro · failed · Jun 15, 2004 · N803ML · Doug DC987 · Attitude Gyro and Indicating System
  > CAPTAIN REPORTED THAT DURING FLIGHT UNTIL APPROACH, RDMI AND ND WITH DIFFERENCE BETWEEN 30-40 DEGREES. DURING TRANSIT CHECK AT CUU, AHRU NR 1 WAS REPLACED IAW MM 34-21-10, TEST CORRECT. AIRCRAFT WAS DISPATCHED AND RETURNED OF FLIGHT, DFGC AND AHRU NR 2 FAI
- [SDR ASMF200404013](https://openairdocs.org/sdr/ASMF200404013.md): Fcu · failed · Apr 19, 2004 · N803ML · Doug DC987 · Fuel Controlling System
  > AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF HIGH TEMPERATURE AND EGT OSCILLATIONS ON ENGINE NR 2. AIRCRAFT WAS SENT TO THE HANGAR. THE LEFT FUEL CONTROL UNIT (FCU) WAS REPLACED IAW MM 73-20-01, TEST CORRECT.
- [SDR ASMF200403009](https://openairdocs.org/sdr/ASMF200403009.md): Warning Horn · activated · Mar 15, 2004 · N803ML · Doug DC987 · Trailing Edge Flap Actuator
  > AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF TAKEOFF ALARM ACTIVATED. TECHNICAL PERSONNEL PERFORMED TESTS TO THE PROXIMITY SWITCH STALL COMPUTER AND STATUS TEST PANEL, BEING ALL CORRECT. DURING OVERNIGHT SERVICE AT MEX WIRING WAS REPAIRED ON S30-111 LEA
- [SDR ASMF200403002](https://openairdocs.org/sdr/ASMF200403002.md): Clamp · leaking · Mar 4, 2004 · N803ML · Doug DC987 · Pneumatic Distribution System
  > DURING TRANSIT CHECK WAS DETECTED HIGH TEMPERATURE ON TAIL CONE. AIRCRAFT WAS SENT TO THE HANGAR AND DURING OVERNIGHT SERVICE AUGMENTATION VALVE AND REGULATOR PRESSURE VALVE CLAMPS WERE REPLACED IAW MM 20-10-11, GASKET AND NIPPLE OF 13A STAGE BLEED VALVE WER
- [SDR MEX2003519](https://openairdocs.org/sdr/MEX2003519.md): Switch · malfunctioned · Nov 14, 2003 · N803ML · Doug DC987 · Hydraulic System, Main
  > DURING TRANSIT CHECK, HYDRAULIC LEAKAGE WAS DETECTED IN THE SWITCH S1-168, SUCH SWITCH WAS BEHEADED. THE SWITCH WAS REPLACED AND THE HYDRAULIC SYSTEM WAS TESTED IAW MM 29-30-03. DURING OVERNIGHT SERVICE, THE SYSTEM WAS CHECKED BY LEAKAGES, ALL OK.
- [SDR MEX2003518](https://openairdocs.org/sdr/MEX2003518.md): Pump · failed · Nov 13, 2003 · N803ML · Doug DC987 · Hydraulic Pump (Electric/Engine), Main
  > AIRCRAFT RETURNED TO PLATFORM DUE TO HIGHT TEMPERATURE ON RT HYDRAULIC SYSTEM. THE RT HYDRAULIC PUMP WAS REPLACED. DURING OVERNIGHT SERVICE THE PTU AND RELIEF VALVE WERE REPLACED IAW MM 29-10-12 RESPECTIVELY.
- [SDR MEX2003492](https://openairdocs.org/sdr/MEX2003492.md): Engine · malfunctioned · Oct 15, 2003 · N803ML · Doug DC987 · Engine (Turbine/Turboprop)
  > AIRCRAFT RETURNED TO PLATFORM, AFTER LT ENGINE START, IT HAD HIGH TEMPERATURE INDICATIONS (447 WITHOUT BLEED AND 491 WITH BLEEDS). ENGINE WAS TESTED AND IT HAD 450 WITHOUT BLEED AND 460 WITH BLEEDS BEING WITHIN LIMITS IAW MM 72-00-00. DURING OVERNIGHT SERVIC
- [SDR MEX2003392](https://openairdocs.org/sdr/MEX2003392.md): Proximity Sensor · will not test · Aug 25, 2003 · N803ML · Doug DC987 · Landing Gear Position and Warning
  > AIRCRAFT RETURNED TO PLATFORM DURING TAXING, NOSE LANDING GEAR RED LIGHT CAME ON. THE BITE WAS PERFORMED TO PROXIMITY SWITCH, SENSOR AND CONNECTOR WERE CLEANED AND CHECKED IAW MM, ALL CORRECT.
- [SDR MEX2003258](https://openairdocs.org/sdr/MEX2003258.md): Wire · failed · Jun 30, 2003 · N803ML · Doug DC987 · Fuel System Wiring
  > DURING FUELING SERVICE, WAS DETECTED THE REFUELING CONTROL PANEL OUT OF SERVICE. DURING REVISION WAS DETECTED THE BREAKER E-5 OF PANEL P-11 DAMAGED. THE REFUELING CONTROL PANEL WAS DEFERRED IAW MEL 28-41-6. THE REFUELING CONTROL PANEL WIRING WAS REPAIRED IA
- [SDR MEX2003257](https://openairdocs.org/sdr/MEX2003257.md): Light · intermittent · Jun 29, 2003 · N803ML · Doug DC987 · Exterior Lighting
  > AIRCRAFT RETURNED TO GATE, TAIL CONE LIGHT CAME ON INTERMITTENTLY. LIGHT TEST, SAFETY MECHANISM AND SW OF TAIL CONE WERE CHECK IAW MM 52-70-11, ALL TESTS CORRECT. (M)
- [SDR MEX2003172](https://openairdocs.org/sdr/MEX2003172.md): Lock · broken · May 11, 2003 · N803ML · Doug DC987 · Aerodynamic Fairings
  > THE RADOME RIGHT LOCK WAS BROKEN BY F.O.D. THE RADOME LOCK WAS REPLACED IAW MM 53-51-02, TEST CORRECT.
- [SDR MEX2003163](https://openairdocs.org/sdr/MEX2003163.md): Indicator · failed · May 8, 2003 · N803ML · Doug DC987 · Engine Pressure Ratio (EPR)
  > AIRCRAFT RETURN TO PLATFORM DUE TO LT ENGINE EPR INDICATION FAILURE. DURING REVISION THE INDICATION ON EDP IS LESS THAN 1, THEREFORE, THE LT ENGINE WAS SHUTDOWN. THE EPR TRANS WAS REPLACED IAW MM, TEST CORRECT.
- [SDR MEX2003148](https://openairdocs.org/sdr/MEX2003148.md): Transmitter · failed · Apr 28, 2003 · N803ML · Doug DC987 · Weather Radar System
  > AIRCRAFT AIR TURNBACK DUE TO RADAR FAIL. TX RADAR WAS REPLACED IAW MM, TEST CORRECT.
- [SDR MEX2003131](https://openairdocs.org/sdr/MEX2003131.md): Pitot Tube · failed · Apr 11, 2003 · N803ML · Doug DC987 · Pitot/Static System
  > CAPTAIN REPORTED LEFT PITOT SYSTEM OUT OFF SERVICES. PITOT TUBE WAS REPLACED IAW MM, TEST CORRECT.

Next page: https://openairdocs.org/deregistered/N803ML-2010-08-12/reports.md?page=2

## 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 = 'N803ML' AND deregistration_id = 'N803ML-2010-08-12'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N803ML-2010-08-12/reports

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