# Service difficulty reports: N1003Y, cancelled Jun 30, 2011

A list on [N1003Y, cancelled Jun 30, 2011](https://openairdocs.org/deregistered/N1003Y-2011-06-30.md).

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

- [SDR ASMF200608013](https://openairdocs.org/sdr/ASMF200608013.md): Lock · misinstalled · Aug 17, 2006 · N1003Y · Doug DC982 · Landing Gear Retraction/Extension System
  > AIRCRAFT RETURNED, RT LANDING GEAR RED LIGHT AND (GEAR DOOR OPEN) LIGHT, REMAINED ON. THEREFORE, ABNORMAL PROCEDURE WAS PERFORMED. DURING MAINTENANCE REVIEW, THE LANDING GEAR LOCK WAS DETECTED INSTALLED BUT WITHOUT THE RED TAPE. THE LANDING GEAR LOCK WAS RE
- [SDR ASMF200607015](https://openairdocs.org/sdr/ASMF200607015.md): Rivet · loose · Jul 22, 2006 · N1003Y · Doug DC982 · Aircraft Structures
  > REPORTED A WATER LEAK IN THE OVERHEAD PANEL NEAR TO THE CABIN CREW DOOR. AIRCRAFT WAS SENT TO THE HANGAR AND INTERIORS AND AIR CONDITIONING DUCTS WERE REMOVED, DETECTING 30 RIVETS LOOSEN BETWEEN LONGERONS 1 TO 4, FROM STATION 148 TO 180; IT PROMOTED A PRESSURI
- [SDR ASMF200604013](https://openairdocs.org/sdr/ASMF200604013.md): Fan Blade · damaged · Apr 25, 2006 · N1003Y · Doug DC982 · Turbine Engine Compressor Section
  > DURING TRANSIT CHECK, IT WAS DETECTED ONE LEFT ENGINE C1 FAN BLADE DAMAGED BY AN SCREW SANK INTO THE ACOUSTIC PANEL (FOD). THE DAMAGE WAS EVALUATED IAW M/M 72-00-00 BEING WITHIN LIMITS. DURING OVERNIGHT CHECK, THE FAN BLADE WAS REWORKED IAW M/M 72-00-00 REMA
- [SDR ASMF200501201](https://openairdocs.org/sdr/ASMF200501201.md): Engine · vibration · Dec 22, 2005 · N1003Y · Doug DC982 · Engine (Turbine/Turboprop)
  > CAPTAIN REPORTED THAT DURING FLIGHT WITH EPR BETWEEN 1.0 AND 1.2 IN THE LT ENGINE; VIBRATION AMPLITUDE OCCASIONALLY WITH PEAKS FROM 4 TO 0 AND WHEN THE LT ENGINE WAS SHUTDOWN, VIBRATION WAS FELT IN ALL THE AIRCRAFT. THE LT ENGINE CHIP DETECTORS, ACCESSORIES, P
- [SDR ASMF200512007](https://openairdocs.org/sdr/ASMF200512007.md): Pin · broken · Dec 7, 2005 · N1003Y · Doug DC982 · Nose/Tail Landing Gear
  > DURING PUSH BACK THE NOSE LANDING GEAR TOWING FUSE PIN WAS BROKEN. IT WAS REPLACED IAW MM 32-21-14 AND THE NOSE LANDING GEAR AND GENERAL INSPECTIONS FOR EXCESSIVE LOAD WERE PERFORMED IAW MM 05-51-03 AND MM 32-20-00 RESPECTIVELY, NO DAMAGES WERE FOUND.
- [SDR ASMF200507018](https://openairdocs.org/sdr/ASMF200507018.md): Warning Light · illuminated · Jul 24, 2005 · N1003Y · Doug DC982 · Door Warning System
  > CAPTAIN REPORTED THAT AFTER TAKE OFF AFT STAIRWAY DOOR LIGHT TURN ON. DURING REVISION LEFT HOOK WAS DETECTED NOT SECURED AT AFT STAIRWAY DOOR. REPORT WAS DEFERRED IAW MEL 52-3, CAT D. AFTER, DURING PUSH BACK AT MEX THE AFT STAIRWAY DOOR LIGHT TURN ON. IT WAS N
- [SDR ASMF200506019](https://openairdocs.org/sdr/ASMF200506019.md): Control Cable · broken · Jun 17, 2005 · N1003Y · Doug DC982 · Steering Unit
  > AFTER LANDING WHILE TAXING, THE STEERING WENT LOOSE. DURING CHECK, THE STEERING CABLE WAS DETECTED BROKEN. AIRCRAFT WAS SENT TO THE HANGAR AND STEERING CABLE WAS REPLACED IAW MM 32-51-02, NOSE WHEEL STEERING ADJUSTMENT WAS PERFORMED IAW MM 32-51-00, TESTED CO
- [SDR ASMF200506014](https://openairdocs.org/sdr/ASMF200506014.md): Unknown · unknown · Jun 11, 2005 · N1003Y · Doug DC982 · Cabin Pressure Control System
  > CAPTAIN REPORTED BOTH AIR CONDITION PACKS WITH LOW FLOW AND DURING DESCENT IT WAS NECESSARY TO MAINTAIN THRUST. BOTH A/A PILOT AND PNEUMATIC REGULATORS WERE REPLACED IAW MM 21-20-00, TESTS WERE PERFORMED BUT PRESSURIZATION PROBLEMS CONTINUED. DURING TESTS, L
- [SDR ASMF200503018](https://openairdocs.org/sdr/ASMF200503018.md): Connector · failed · Mar 24, 2005 · N1003Y · Doug DC982 · VHF Communications System
  > AIRCRAFT WAS RECEIPT AT GDL WITH CAPTAIN REPORT "VHF 1 OUT OF SERVICE", AS A CORRECTIVE ACTION BOTH VHF WERE REPLACED AN TESTED, ALL CORRECT. AIRCRAFT RETURNED OF FLIGHT AS A CONSEQUENCE OF VHF FAILURE CONTINUED. COAXIAL CABLE AND VHF NR 1 WERE CHECKED IAW MM
- [SDR ASMF200502003](https://openairdocs.org/sdr/ASMF200502003.md): Valve · leaking · Feb 6, 2005 · N1003Y · Doug DC982 · Hydraulic System, Main
  > DURING TRANSIT CHECK WERE DETECTED HYDRAULIC LEAK AT RIGHT MAIN LANDING GEAR IN VALVE LOCKOUT. THE VALVE LOCKOUT WAS REPLACED IAW MM 32-42-06, TESTED CORRECT. CORRECT, DEFERRED REPORT WAS CLOSED
- [SDR ASMF200412011](https://openairdocs.org/sdr/ASMF200412011.md): Connector · failed · Dec 25, 2004 · N1003Y · Doug DC982 · Fuel Indicating System
  > AIRCRAFT RETURNED TO PLATFORM DUE TO NO FUEL INDICATION IN BOTH CHANNELS. SEM CONNECTORS WERE CHECKED DETECTING ONE CHANNEL LOOSEN, THE FOUR CHANNELS WERE DISCONNECTED AND CHECKED. THE FOUR CONNECTORS WERE INSTALLED AND TESTED IAW MM 28-40-05, ALL CORRECT.
- [SDR ASMF200410005](https://openairdocs.org/sdr/ASMF200410005.md): Modulator · leaking · Oct 7, 2004 · N1003Y · Doug DC982 · Hydraulic System, Main
  > DURING LT ENGINE STARTING CAPTAIN REPORTED LT HYDRAULIC SYSTEM LEAKAGE AND PRESSURE DROP TO ZERO. DURING REVISION THE TECHNICAL PERSONNEL DETECTED THAT THE LEAK WAS FROM A LINE OF THE MAIN FILTERS MODULE. LINE WAS TIGHTENED AND HYDRAULIC FLUID RECHARGED. TESTS
- [SDR ASMF200408022](https://openairdocs.org/sdr/ASMF200408022.md): Thermocouple · damaged · Aug 26, 2004 · N1003Y · Doug DC982 · Engine EGT/TIT Indicating System
  > DURING OVERNIGHT SERVICE WAS DETECTED RT ENGINE WITH HIGH EGT INDICATION. EGT INDICATION WAS CHECKED IAW MM 77-21-00 AND THERMOCOUPLE NR 4 WAS DETECTED WITH DAMAGE, IT WAS REPLACED IAW MM 77-21-03. PT2 AND PT7 WERE CHECKED AND NO LEAKS WERE DETECTED, TRIMMING
- [SDR ASMF200408003](https://openairdocs.org/sdr/ASMF200408003.md): Control Valve · damaged · Aug 3, 2004 · N1003Y · Doug DC982 · Engine Thrust Reverser
  > CAPTAIN REPORTED, DURING CLIMB "LT REVERSE ACCUMULATOR" LIGHT TURNED ON AND LT HYDRAULIC QUANTITY DOWN AT 4 QUARTERS. LT REVERSE VALVE WAS CHECKED AND LEAK ON PRESSURE LINE WAS DETECTED, NIPPLE WAS TIGHTENED AND HYDRAULIC PRESSURE WAS APPLIED AND LEAK CONTINUE
- [SDR ASMF200407013](https://openairdocs.org/sdr/ASMF200407013.md): Actuator · failed · Jul 9, 2004 · N1003Y · Doug DC982 · Landing Gear Door Actuator
  > AIRCRAFT RETURNED AFTER TAKEOFF, IT WAS NOT POSSIBLE TO RETRACT THE NOSE LANDING GEAR WITH STRONG NOISE IN SUCH AREA. THREE FULL EXTENSION AND RETRACTION CYCLES WERE PERFORMED BUT NOSE LANDING GEAR DID NOT RETRACT. DURING CHECK, FORWARD DOOR WAS DETECTED DOW
- [SDR ASMF200406025](https://openairdocs.org/sdr/ASMF200406025.md): Link · failed · Jun 22, 2004 · N1003Y · Doug DC982 · Nose/Tail Landing Gear
  > AIRCRAFT RETURNED OF FLIGHT, STRONG VIBRATION IN NOSE LANDING GEAR. DURING MAINTENANCE CHECK WAS DETECTED LT NOSE LANDING GEAR DOOR OPENED, DOOR AND ACTUATOR WERE CHECKED AND ACTUATOR WAS REPLACED IAW MM 32-22-01, TEST FLIGHT WAS PERFORMED AND THREE CYCLES OF
- [SDR ASMF200406022](https://openairdocs.org/sdr/ASMF200406022.md): Computer · failed · Jun 21, 2004 · N1003Y · Doug DC982 · Attitude and Direction Data System
  > DURING TRANSIT CHECK, CAPTAIN REPORTED SPEED FLAG IN BOTH ADI´S AND FLAG IN EPR LIMIT INDICATOR. CADC´S AND DFGC´S RESEAT WERE PERFORMED AND FAIL CONTINUED. DIFFERENCE OF 150 FEET BETWEEN BOTH ALTIMETERS WAS REPORTED AND CADC´S WERE REPLACED IAW MM 34-16-01,
- [SDR ASMF200406001](https://openairdocs.org/sdr/ASMF200406001.md): Stringer · leaking · Jun 1, 2004 · N1003Y · Doug DC982 · Fuselage Main, Longeron/Stringer
  > DURING TRANSIT CHECK, A WATER LEAK WAS DETECTED ON UPPER CREW CABIN. AIRCRAFT WAS SENT TO THE HANGAR AND DURING OVERNIGHT SERVICE AIRCRAFT WAS PRESSURIZED AND LEAK TEST WAS PERFORMED, DETECTING LEAKS ON STRINGER 1 FS. Y-157 TO Y-157A AND 256, STRINGER 2 AND 3
- [SDR ASMF200405011](https://openairdocs.org/sdr/ASMF200405011.md): Engine · malfunctioned · May 7, 2004 · N1003Y · Doug DC982 · Engine (Turbine/Turboprop)
  > AIRCRAFT SUSPENDED TAKE OFF AND RETURNED TO PLATFORM, LOW POWER ON RT ENGINE. INLET AND OUTLET OF RT ENGINE WERE CHECKED, ALL CORRECT. FUEL CONTROL UNIT WAS REPLACED AND PT2, PT7 AND OIL FILTER WERE CHECKED. TRIM TO BOTH ENGINES WAS PERFORMED AND EGT REACHED 6
- [SDR ASMF20040403](https://openairdocs.org/sdr/ASMF20040403.md): Transceiver · failed · Apr 5, 2004 · N1003Y · Doug DC982 · Weather Radar System
  > AIRCRAFT ARRIVED WITH FOLLOWING REPORTS: RADAR ANTENNA TURNED TO RIGHT. RADAR CONNECTOR WAS RESEATED AND CLEANED IAW MM 34-41-01. L ICE PROTECT TEMP HIGH LIGHT TURNED ON. LEAK WAS CORRECTED AND CLAMPS WERE TIGHTENED IAW MM 30-10-07. LEFT WINDSHIELD WIPER
- [SDR MEX2004052](https://openairdocs.org/sdr/MEX2004052.md): Warning System · failed · Feb 11, 2004 · N1003Y · Doug DC982 · Central Warning
  > FLT 278 - MEX-CJS - AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF DURNIG PUSH-BACK APU SHUTOFF AND APU FIRE, OVERSPEED, AND TAKEOFF ALARMS WERE ACTIVATED. AT PLATFORM, ALARM SYSTEM (CAWS) WAS RESET BUT FAIL CONTINUED. IT WAS REPLACED AND TESTED IAW MM 31
- [SDR MEX2004053](https://openairdocs.org/sdr/MEX2004053.md): Receptacle · damaged · Feb 11, 2004 · N1003Y · Doug DC982 · Landing Gear Position and Warning
  > FLT 278 - MEX-CJS - AIRCRAFT RETURNED DUE TO NOSE LANDING GEAR RED LIGHT TURNED ON. DURING CHECK IT WAS DETECTED A WIRE BROKEN IN THE NOSE LANDING GEAR DOWN SENSOR RECEPTACLE. AIRCRAFT WAS SENT TO THE HANGAR AND DURING OVERNIGHT SERVICE RECEPTACLE R5-1157 AN
- [SDR MEX2003459](https://openairdocs.org/sdr/MEX2003459.md): Wheel · stuck · Oct 3, 2003 · N1003Y · Doug DC982 · Wheel/Ski/Float
  > AIRCRAFT RETURN TO PLATFORM DUE TO TAXING VIBRATION WS FELT ON THE BRAKES AND THE AIRCRAFT STOPS BY ITSELF. DURING REVISION WAS DETECTED THE BRAKE NUMBER THREE TIED. BRAKE ASSEMBLY AND TIRE NUMBER 3 WAS REPLACED IAW MM 32-42-01 AND 32-40-01.
- [SDR MEX2003198](https://openairdocs.org/sdr/MEX2003198.md): Indicator · failed · Jun 1, 2003 · N1003Y · Doug DC982 · Airspeed/Mach Indicator
  > AIRCRAFT SUSPENDS TAKEOFF DUE TO AIRSPEED INDICATIONS SHOWED A 40 KNOTS DIFFERENCE AND SPEED FLAG APPEARED. THE MACH AND AIRSPEED INDICATOR NR 2 WERE REPLACED IAW MM 34-13-01, ALL TESTS CORRECT. (M)
- [SDR MEX2003064](https://openairdocs.org/sdr/MEX2003064.md): Engine · lack of lube · Mar 9, 2003 · N1003Y · Doug DC982 · Turbine Engine Oil System
  > FLT 940 - MEX-MTY, AIRCRAFT RETURNED TO PLATFORM, DURING TAXIING THE LOW QUANTITY OIL LIGHT OF ENGINE NR 2 TURNED ON. THE OIL LEVEL WAS VERIFIED BEING NECESSARY TO ADD 7 QUARTS. THE ENGINE MAIN OIL FILTER WAS INSPECTED IAW MM 79-20-06, ALL CORRECT FOR SERVI
- [SDR MEX2003009](https://openairdocs.org/sdr/MEX2003009.md): Pump · failed · Jan 22, 2003 · N1003Y · Doug DC982 · Hydraulic Pump (Electric/Engine), Main
  > FLT 258 - MEX-CJS - AIRCRAFT RETURNED TO GATE DUE TO LEFT ENGINE HYDRAULIC PUMP OUT OF SERVICE WITH CERO PRESSURE INDICATION. LEFT ENGINE HYDRAULIC PUMP WAS REPLACED IAW MM 29-10-05, ALL CORRECT. (M)
- [SDR MEX2002384](https://openairdocs.org/sdr/MEX2002384.md): Warning Light · illuminated · Dec 28, 2002 · N1003Y · Doug DC982 · Door Warning System
  > AIRCRAFT RETURN TO FLIGHT DUE TO ACCESSORY COMPARTMENT DOOR LIGHT TURNED ON. COMPARTMENT DOOR WAS CHECKED DETECTING TWO SECURES UNSAFE, REINSTALLED. DURING OVERNIGHT SERICE ACCESSORY COMPARTMENT DOOR LIGHT WAS CHECKED IAW MM 52-70-06, TESTS OK. (M)
- [SDR MEX2002298](https://openairdocs.org/sdr/MEX2002298.md): Cover · detached · Sep 13, 2002 · N1003Y · Doug DC982 · Emergency Equipment
  > FLT 509 - MEX-VSA - AIRCRAFT RETURNED TO PLATFORM AS CONSEQUENCE OF THAT THE SLIDE RAFT COVER OF THE REAR SERVICE DOOR WAS DETACHED. THE TECHNICIANS DETECTED THE COVER OUT OF ITS RESPECTIVE RECEPTACLE. THE COVER WAS REINSTALLED IAW MM 25-62-01, AND THE DOOR
- [SDR MEX2002038](https://openairdocs.org/sdr/MEX2002038.md): Relay · failed · Feb 13, 2002 · N1003Y · Doug DC982 · Hydraulic System, Main
  > FLT 119 - TIJ-GDL - PILOT REPORTED THAT L HYD PRESS LOW LIGHT DOES NOT TURN ON. LOW PRESSURE SWITCH WAS CHECKED AN SEVERAL CYCLES WERE PERFORMED WITH THE CONTROL SURFACES. RELAYS R2-497 AND R2-498 WERE SWAPPED, TESTS OK. DURING TRANSIT CHECK IN GDL BOTH REL
- [SDR MEX2002135](https://openairdocs.org/sdr/MEX2002135.md): Hydraulic Line · leaking · Feb 5, 2002 · N1003Y · Doug DC982 · Hydraulic System, Main
  > FLT 136 - MEX-AGS - FIFTEEN MINUTES BEFORE TAKEOFF, WHEN THE CAPTAIN TRIED TO PRESSURE THE HYDRAULIC SYSTEM A HYDRAULIC LEAK WAS DETECTED AT THE TAIL CONE AREA. AIRCRAFT WAS SENT TO THE HANGAR, THE LEAK WAS DETECTED IN THE SUPPLY LINE OF THE HYDRAULIC AUXILIA

## 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 = 'N1003Y' AND deregistration_id = 'N1003Y-2011-06-30'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N1003Y-2011-06-30/reports

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