# Service difficulty reports: N1075T, cancelled Jul 29, 2013

A list on [N1075T, cancelled Jul 29, 2013](https://openairdocs.org/deregistered/N1075T-2013-07-29.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 · 55 reports

- [SDR ASMF200610003](https://openairdocs.org/sdr/ASMF200610003.md): Wire · loose · Oct 3, 2006 · N1075T · Doug DC987 · Ice/Rain Protection System Wiring
  > AIRCRAFT RETURNED TO PLATFORM, THE PITOT STALL HEAT OFF (RUDDER LIMIT) LIGHT TURNED ON, AFTER ENGINES STARTED. THE RELAY R2-100 WAS CHECKED IAW MM 30-31-01, BEING CORRECT, BUT DURING RUDDER LIMITER PITOT TUBE REMOVAL, THE ELECTRICAL LINE OF CONNECTOR P1-361 WA
- [SDR ASMF200608021](https://openairdocs.org/sdr/ASMF200608021.md): Structure · delaminated · Aug 31, 2006 · N1075T · Doug DC987 · Engine Noise Suppressor
  > DURING TRANSIT CHECK, LT ENGINE NOSE COWLING NOISE SUPPRESSOR WAS DETECTED DELAMINATED IN AN AREA OF 17 INCHES WIDTH X 25 INCHES LENGTH BETWEEN 6 AND 7 HOURS POSITION OUT OF LIMITS IAW MM 72-00-00 PAGE 642. AIRCRAFT WAS SENT TO THE HANGAR. PENDING FINAL ACTION
- [SDR ASMF200608012](https://openairdocs.org/sdr/ASMF200608012.md): Control Valve · leaking · Aug 16, 2006 · N1075T · Doug DC987 · Hydraulic System, Main
  > CAPTAIN REPORTED THAT AFTER LANDING, THE LT HYDRAULIC SYSTEM WAS LOST AND LT REVERSE REMAINED EXTENDED. AIRCRAFT WAS TOWED TO PLATFORM AND RECHARGED OF HYDRAULIC LIQUID, DETECTING A LEAK IN THE LT HYDRAULIC REVERSE VALVE CAP. THE LT HYDRAULIC REVERSE VALVE WAS
- [SDR ASMF200608009](https://openairdocs.org/sdr/ASMF200608009.md): Tube · leaking · Aug 15, 2006 · N1075T · Doug DC987 · Turbine Engine Oil System
  > AIRCRAFT PERFORMED AN UNSCHEDULED LANDING, THE LT ENGINE (OIL PRESS LOW) LIGHT TURNED ON. CAPTAIN INFORMED THAT DURING CRUISE THE (OIL PRESS LOW) LIGHT TURNED ON, PERFORMED THE EMERGENCY PROCEDURE AND LT ENGINE WAS SHUTDOWN. DURING MAINTENANCE REVIEW, THE OIL
- [SDR ASMF200605015](https://openairdocs.org/sdr/ASMF200605015.md): Pump · failed · May 27, 2006 · N1075T · Doug DC987 · Fuel Boost Pump
  > AIRCRAFT PERFORMED AN UNSCHEDULED LANDING AT GDL DUE TO THE AFT CENTER FUEL TANK BOOST PUMP WAS OUT OF SERVICE AND BREAKER POPPED OUT, LANDING WITH 5550 POUNDS IN THE LEFT TANK AND 3100 POUNDS IN THE RIGHT TANK. PUMPS WERE DEFERRED IAW MEL 28-2 AND AIRCRAFT W
- [SDR ASMF200605014](https://openairdocs.org/sdr/ASMF200605014.md): Hydraulic Line · leaking · May 26, 2006 · N1075T · Doug DC987 · Hydraulic System, Main
  > DURING TRANSIT CHECK IT WAS DETECTED A HYDRAULIC LEAK IN ONE LINE OF THE LEFT THRUST REVERSE CONTROL VALVE. FLEXIBLE LINE WAS INSTALLED, TESTED CORRECT. DURING OVERNIGHT CHECK THE FLEXIBLE LINE WAS REPLACED IAW MM 78-31-04, TESTED CORRECT.
- [SDR ASMF200603006](https://openairdocs.org/sdr/ASMF200603006.md): Gpu · smoke · Mar 13, 2006 · N1075T · Doug DC987 · Electrical Power System
  > AIRCRAFT ARRIVED TO MEX WITH APU AND HIGH PNEUMATIC PURGE OF LEFT AIR CONDITIONING OUT OF SERVICE AND DEFERRED, SO GPU WAS CONNECTED AND IT INDUCED SMOKE INTO THE CABIN WHEN BOTH AIR-CONDITIONING PACKAGES WERE CONNECTED. AIRCRAFT WAS SENT TO THE HANGAR TO TES
- [SDR ASMF200601010](https://openairdocs.org/sdr/ASMF200601010.md): Starter · failed · Jan 15, 2006 · N1075T · Doug DC987 · Engine Starter
  > DURING TAXING CAPTAIN INFORMED THAT THERE WAS NOT INDICATION OF THE LEFT ENGINE, RETURNING TO PLATFORM. DURING MAINTENANCE REVIEW, THE ENGINE STARTER AND ITS COUPLE WERE FOUND DAMAGED. BOTH ITEMS WERE REPLACED AND SYSTEM TESTED IAW M/M 80-10-01. DURING OVER
- [SDR ASMF200512013](https://openairdocs.org/sdr/ASMF200512013.md): Blade · fod · Dec 14, 2005 · N1075T · Doug DC987 · Engine (Turbine/Turboprop)
  > DURING TRANSIT CHECK, A BLADE OF THE LT ENGINE WAS DETECTED WITH DAMAGE BY FOD. INSPECTION WAS PERFORMED, DETECTING A CRACK OF 0.125 X 0.250 BEING WITHIN LIMITS IAW MM 72-00-00. THE LT ENGINE BLADE WAS REWORKED IAW 72-00-00 PAGE 618, TESTED CORRECT.
- [SDR ASMF200507020](https://openairdocs.org/sdr/ASMF200507020.md): Strut · underserviced · Jul 25, 2005 · N1075T · Doug DC987 · Nose/Tail Landing Gear
  > AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF STRONG NOISE IN THE NOSE LANDING GEAR. THE NOSE LANDING GEAR INSPECTION WAS PERFORMED IAW 32-20-00, ALL CORRECT. THE STRUT WAS SERVICED IAW MM 32-21-02, TESTED CORRECT.
- [SDR ASMF200505028](https://openairdocs.org/sdr/ASMF200505028.md): Actuator · failed · May 25, 2005 · N1075T · Doug DC987 · Entrance Stairs
  > AIRCRAFT RETURNED OF FLIGHT AS A CONSEQUENCE OF PRESSURIZATION WAS UNSTABLE DURING CLIMB. AT PLATFORM, THE VENTRAL STAIRWAY WAS ADJUSTED IAW MM 52-63-00. PRESSURIZATION CONTROLLERS BITE WERE PERFORMED, SYSTEM VALVES WERE REVISED, MANUAL SYSTEM OPERATION WAS
- [SDR ASMF200412005](https://openairdocs.org/sdr/ASMF200412005.md): Warning Light · false activation · Dec 17, 2004 · N1075T · Doug DC987 · Landing Gear Position and Warning
  > AIRCRAFT ARRIVED WITH CAPTAIN REPORT AFTER TAKEOFF THE THREE LANDING GEAR RED LIGHTS AND AUDIBLE ALARM TURNED ON. ABNORMAL PROCEDURE WAS PERFORMED AND LIGHTS AND ALARM TURNED OFF. AIRCRAFT WAS SENT TO THE HANGAR, SWITCHES S-319 AND S1-89 WERE REPLACED IAW M
- [SDR ASMF200407020](https://openairdocs.org/sdr/ASMF200407020.md): Antenna · damaged · Jul 18, 2004 · N1075T · Doug DC987 · Weather Radar System
  > AIRCRAFT RETURNED OF FLIGHT, RADAR WAS OUT OF SERVICE WITH (TR AND FAIL ON DISPLAY) LEGENDS. TRANSCEIVER RADAR WAS CHECKED, RACK AND UNIT CONNECTORS WERE CLEANED AND ANTENNA WAS CHECKED, ALL CORRECT. TRANSCEIVER WAS REINSTALLED AND TESTED IAW MM 34-41-00, ALL
- [SDR ASMF200406015](https://openairdocs.org/sdr/ASMF200406015.md): Radar · failed · Jun 15, 2004 · N1075T · Doug DC987 · Weather Radar System
  > AIRCRAFT PERFORMED AN UNSCHEDULED LANDING, LOW FUEL AND CAPTAIN REPORTED RADAR SYSTEM FAILED. DURING MAINTENANCE REVISION, RADAR, ANTENNA, TRANSCEIVER AND RADAR DISPLAY WERE CHECKED, ALL CORRECT. RADAR TRANSCEIVER WAS REPLACED IAW MM 34-41-04, TEST CORRECT.
- [SDR ASMF200405017](https://openairdocs.org/sdr/ASMF200405017.md): Pressure Valve · failed · May 15, 2004 · N1075T · Doug DC987 · Pressure Regulator/Outflow Valve
  > AIRCRAFT RETURNED FLIGHT BECAUSE IN AUTOMATIC MODE THE PRESSURIZATION SYSTEM HAD OSCILLATIONS AND IN MANUAL MODE THE PRESSURE VALVE COULD NOT BE CLOSED. DURING MAINTENANCE REVISION, THE SWITCH WAS PLACED IN MANUAL POSITION AND VALVE WAS CLOSED, THE SYSTEM OPE
- [SDR MEX2004049](https://openairdocs.org/sdr/MEX2004049.md): Strut · discharged · Feb 6, 2004 · N1075T · Doug DC987 · Main Landing Gear Strut/Axle/Truck
  > FLT 253 - GDL-MEX - DURING TRANSIT CHECK, THE NOSE LANDING GEAR STRUT WAS FOUND COMPRESSED WITHOUT NITROGEN PRESSURE. THE NLG STRUT SEALS WERE REPLACED IAW MM 32-31-02 AND AN AJUSTMENT TO THE GROUND SENSING CONTROL MECHANISM WAS PERFORMED IAW MM 32-23-01, TES
- [SDR MEX2003572](https://openairdocs.org/sdr/MEX2003572.md): Coupler · leaking · Dec 29, 2003 · N1075T · Doug DC987 · Hydraulic System, Main
  > FLT 143 - PVR-MEX - DURING TRANSIT CHECK, OBSERVED HYDRAULIC LEAKAGE COMING FROM THE MLG COMPARTMENT. THE LT HYDRAULIC SYSTEM,WITH LOW LEVEL, WAS PRESSURIZED, OBSERVING AN HYDRUALIC LEAKAGE IN A CONNECTING COUPLE OF THE POWER TRANSFER SHUTOFF VALVE. THE COUP
- [SDR MEX2003563](https://openairdocs.org/sdr/MEX2003563.md): Display · failed · Dec 25, 2003 · N1075T · Doug DC987 · Attitude Gyro and Indicating System
  > FLT 563 - MEX-TAP - CAPTAIN REPORTED THE DURING FLIGHT RIGHT IVSI WAS OCCASIONALLY OUT OF SERVICE. AIRCRAFT WAS SENT TO THE HANGAR AND THE RIGHT IVSI AND BREAKER J-16 WERE REPLACED IAW MM 34-14-00 AND 20-25-00 RESPECTIVELY, ALL CORRECT. (M)
- [SDR MEX2003448](https://openairdocs.org/sdr/MEX2003448.md): Switch · defective · Sep 26, 2003 · N1075T · Doug DC987 · Engine Thrust Reverser
  > FLT 306 - ACA-MEX - AIRCRAFT RETURN TO PLATFORM AS A CONSEQUENCE OF RIGHT ENGINE REVERSE UNLOCKED LIGHT TURNED ON. REVERSE MECHANISM AND ACTUATOR WERE LUBRICATED AND REVERSE WAS OPERATED THREE TIMES NON REPRODUCING THE FAIL. FURTHER, AIRCRAFT RETURN TO PLATF
- [SDR MEX2003277](https://openairdocs.org/sdr/MEX2003277.md): Sensor · malfunctioned · Jul 8, 2003 · N1075T · Doug DC987 · Entrance Stairs
  > AIRCRAFT AIR TURN BACK, DURING FLIGHT THE LIGHT FWD STAIRWAY DOOR COME ON. THE FWD STAIRWAY DOOR SENSOR WAS CHECKED IAW 52-61-00, AND BITE WAS PERFORMED TO PRESSURIZATION CONTROLLERS IAW 21-32-03, ALL TESTS CORRECT.
- [SDR MEX20030321](https://openairdocs.org/sdr/MEX20030321.md): Thrust Reverser · malfunctioned · Jul 3, 2003 · N1075T · Doug DC987 · Engine Thrust Reverser
  > FLT 605 - DFW-MEX - AIRCRAFT RETURN TO PLATFORM, DURING TAXI THE RIGHT ENGINE REVERSE UNLOCKED INDICATOR LIGH TON. DURING REVISION THE LIGHT WAS OFF AND REVERSE WAS OPERATED THREE TIMES, ALL CORRECT. THE REVERSE WAS DEFERRED UNDER MEL 78-1. AT MEX, SWITCH R
- [SDR MEX2003249](https://openairdocs.org/sdr/MEX2003249.md): Turbine · failed · Jun 25, 2003 · N1075T · Doug DC987 · Cabin Cooling System
  > AIRCRAFT ARRIVED WITH CAPTAIN REPORT 'DEFICIENT AIR CONDITIONING'. DURING REVISION THE LEFT TURBINE COOLING WAS DAMAGED. REPORT WAS DEFERRED IAW MEL 21-1, LEFT AIR CONDITION OUT SERVICE. DURING OVERNIGHT SERVICE THE LEFT TURBINE COOLING WAS REPLACED IAW MM
- [SDR MEX2003231](https://openairdocs.org/sdr/MEX2003231.md): Nose Cowl · dented · Jun 17, 2003 · N1075T · Doug DC987 · Engine Air Intake System
  > DURING TRANSIT CHECK WAS DETECTED NOSE COWLING ENGINE RIGHT WITH DENT OUT OF LIMITS OF APPROXIMATELY 2.0 OF DIAMETER. DURING OVERNIGHT SERVICE NOSE COWLING WAS REPLACED IAW MM, ALL CORRECT.
- [SDR MEX2003226](https://openairdocs.org/sdr/MEX2003226.md): Indicator · failed · Jun 14, 2003 · N1075T · Doug DC987 · Integrated Flight System
  > MEX-SLC - FLT 486 - AIRCRAFT PERFORMED UNSCHEDULED LANDING, DURING CRUISE EFIS NR 2 FAILED AFFECTING VOR NR 2 AND ADI NR 1 AND DURING APPROACH BOTH TEMP OIL INDICATION CAME ON. BREAKER AHSRS 2 WAS RESET, EDP WAS TESTED AND ADDITIONALLY TEMP OIL SENSOR WERE CL
- [SDR MEX2003225](https://openairdocs.org/sdr/MEX2003225.md): Thermocouple · damaged · Jun 14, 2003 · N1075T · Doug DC987 · Engine EGT/TIT Indicating System
  > FLT 101 - HMO-CUL - AIRCRAFT RETURNED TO GATE DUE TO ENGINE NR 1 DID NOT HAVE EGT INDICATION. DURING REVISION FOUR, THERMOCOUPLE PROBES WERE DAMAGED. DURING OVERNIGHT SERVICE SUCH THERMOCOUPLE PROBES WERE REPLACED AND TESTED IAW MM 77-21-00, ALL CORRECT. (M
- [SDR MEX2003185](https://openairdocs.org/sdr/MEX2003185.md): Generator · failed · May 19, 2003 · N1075T · Doug DC987 · DC Generating System
  > AIRCRAFT ARRIVED WITH REPORT RIGHT GENERATOR OUT OF SERVICE, GENERATOR WAS REPLACED AND AFTER ENGINES STARTING CAPTAIN INFORMS THAT SAME CONDITION CONTINOUS. AIRCRAFT ARRIVED BY ITS OWN IMPULSE TO THE POSITION S-7, ENGINES WERE SHUTDOWN AND WIRING WERE VERIFI
- [SDR MEX2003170](https://openairdocs.org/sdr/MEX2003170.md): Filter · failed · May 10, 2003 · N1075T · Doug DC987 · Engine Fuel Pump
  > AIRCRAFT RETURN TO PLATFORM DUE TO LOW ACCELERATION ON ENGINE NR 1. SERVICE ON ACCELERATION CAMERA WAS ACCOMPLISHED IAW MM 73-20-01. DURING OVERNIGHT SERVICE THE FUEL PUMP FILTER PS3 WAS REPLACED AND TEST WAS ACCOMPLISHED IAW MM 71-00-00, ALL CORRECT.
- [SDR MEX2003207](https://openairdocs.org/sdr/MEX2003207.md): Relief Valve · failed · Apr 6, 2003 · N1075T · Doug DC987 · Pressure Regulator/Outflow Valve
  > FLT 926 - MEX-CUU - AIRCRAFT AIR TURNBACK AS A CONSEQUENCE OF DURING CRUISE AT 35,000 FEET, STRONG NOISE WAS HEARD, THE FLOW LIGHT CAME ON. PRESSURIZATION VALVE WAS CLOSED AND CABIN ALTITUDE WAS 7,600 FEET. PRESSURIZATION TEST WAS ACCOMPLISHED, NO LEAKS WERE
- [SDR MEX2003073](https://openairdocs.org/sdr/MEX2003073.md): Blade · damaged · Mar 14, 2003 · N1075T · Doug DC987 · Engine (Turbine/Turboprop)
  > DURING TRANSIT CHECK, FOD ON LT ENGINE WAS DETECTED. DURING INSPECTION, DETECTED A BLADE WITH DAMAGE. FAN BLADE FROM ENGINE NR 1 WAS BLENDED IAW MM, ALL CORRECT.
- [SDR MEX2003061](https://openairdocs.org/sdr/MEX2003061.md): Display · failed · Mar 7, 2003 · N1075T · Doug DC987 · Attitude and Direction Data System
  > FLT 169 - CUL-MEX - AIRTURN BACK, DURING CLIMB IN THE FMA, AP TRIM THE NO AUTO LAND MESSAGE WAS SHOWN. THERE WAS A DIFFERENCE BETWEEN RMI'S OF 170 DEGREES. THE FD DISAPPEAR WITHOUT OBEY AUTO THROT AT SELECTED VELOCITIES. TESTS WERE PERFORMED IN STP AND SYST
- [SDR MEX2003041](https://openairdocs.org/sdr/MEX2003041.md): Accelerometer · inoperative · Feb 22, 2003 · N1075T · Doug DC987 · Autopilot System
  > AIRCRAFT RETURNED FROM FLIGHT, AFTER TAKEOFF FLIGHT GUIDANCE COMPUTER WENT OFF. ON BOTH COMPUTERS THERE WERE NO AUTO PILOT AND ATS, PITOT HEAT OFF LIGHT TURN ON AND YAW DAMPER FAILURE LIGHT TURN ON. RESPECT TO PITOT STALL HEATER OFF LIGHT ON, IT WAS DETERMIN
- [SDR MEX2002140](https://openairdocs.org/sdr/MEX2002140.md): Csd · failed · Jun 5, 2002 · N1075T · Doug DC987 · AC Generation System
  > FLT 307 - MEX-ACA - TECHNICAL PERSONNEL AT GATE REPORT THAT THE ENGINE NR 1 CSD HAD DAMAGE OUT OF LIMITS AND THE MASTER CAUTION LIGHT WAS ON AS A CONSEQUENCE OF OIL LOW PRESSURE. AIRCRAFT WAS SENT TO THE HANGAR AND THE CSD AND THE RADIATOR OIL WERE CHANGED IA
- [SDR ASM2002F00003](https://openairdocs.org/sdr/ASM2002F00003.md): Bypass Valve · malfunctioned · May 19, 2002 · N1075T · Doug DC987 · Landing Gear Retraction/Extension System
  > AIRCRAFT RETURNED FROM FLIGHT AS A CONSEQUENCE OF LANDING GEAR DOOR NOT RETRACTING. DURNING CHECK, THE LANDING GEAR BYPASS VALVE WAS OPEN AND NOT SECURED. VALVE WAS REPOSITIONED.
- [SDR MEX2002353](https://openairdocs.org/sdr/MEX2002353.md): Display · failed · Mar 12, 2002 · N1075T · Doug DC987 · Integrated Flight System
  > FLT 353 - MEX-ZIH - AIRCRAFT RETURNED DUE TO PFD AND ND NAVIGATIONAL SYSTEM FAILURE, FIRST OFFICER RDMI FLAGS, AUTOMATIC PILOT, THROTTLES AND DIRECTOR BARS OUT OF SERVICE AND FMA WITHOUT INFORMATION. TECH PERSONNEL RECEIPT THE EQUIPMENT OPERATING IN NORMAL WA
- [SDR MEX2002317](https://openairdocs.org/sdr/MEX2002317.md): Engine · malfunctioned · Jan 10, 2002 · N1075T · Doug DC987 · Engine (Turbine/Turboprop)
  > AIRCRAFT RETURNED TO PLATFORM DUE TO LEFT ENGINE DID NOT ACCELERATE. PARAMETERS WERE ON RIGHT ENGINE 56.5 AND ON LEFT ENGINE 51.0 ENGINE 51.0. ENGINES WERE ADJUSTED ON IDLE, TESTS OK. DURING OVERNIGHT, SERVICE WAS PERFORMED A TRIM TO BOTH ENGINES IAW MM, TE
- [SDR GRAA9663](https://openairdocs.org/sdr/GRAA9663.md): Light · inoperative · Aug 22, 1996 · N1075T · Doug DC987 · Emergency Lighting
  > LINE MAINTENANCE AT IFP, DISCOVERED THAT THE EMERGENCY FLOOR LIGHT WAS INOPERATIVE. MAINTENANCE RELAMPED OPERATIONAL CHECKED NORMAL. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR GRAA9627](https://openairdocs.org/sdr/GRAA9627.md): Batteries · discharged · Apr 12, 1996 · N1075T · Doug DC987 · Emergency Lighting
  > LINE MAINTENANCE AT RNO, DISCOVERED THAT BOTH OVERWING EXITS OVERHEAD EMERGENCY LIGHTS FAILED. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT BATTERIES. MAINTENANCE PERFORMED AN OPEATIONAL CHECK OF THE EMERGENCY LIGHT SYSTEM. THE EMERGENCY LIGHT SYSTEM OP
- [SDR GRAA9625](https://openairdocs.org/sdr/GRAA9625.md): Oil Filter · dirty · Apr 7, 1996 · N1075T · Doug DC987 · Turbine Engine Oil System
  > AT RNO, ON ENGINE START HAD THE RIGHT 'ENGINE OIL CLOGGING' LIGHT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE MAIN ENGINE OIL FILTER. MAINTENANCE PERFORMED AN OPERATIONAL AND LEAK CHECK OF NR 2 ENGINE. NR 2 ENGINE OPERATIONALLY CHECKED NORM
- [SDR GRAA9624](https://openairdocs.org/sdr/GRAA9624.md): Lens · missing · Apr 6, 1996 · N1075T · Doug DC987 · Emergency Lighting
  > LINE MAINTENANCE AT ENV, DISCOVERED THAT THE EMERGENCY FLOOR TRACK LENS WAS MISSING AT ROW 18. MX REPLACED THE LENS ON THE EMERGENCY FLOOR TRACK AT ROW 18. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE EMERGENCY FLOOR LIGHT SYSTEM. THE SYSTEM OPERATIONA
- [SDR GRAA9623](https://openairdocs.org/sdr/GRAA9623.md): Power Supply · inoperative · Apr 5, 1996 · N1075T · Doug DC987 · Emergency Lighting
  > LINE MAINTENANCE AT RNO, DISCOVERED THE FORWARD EMERGENCY FLOOR LIGHT LIGHT STRIP INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLOOR LIGHT POWER SUPPLY. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE SYSTEM. THE EMERGENCY FLOOR LIGHT SYSTE
- [SDR GRAA9621](https://openairdocs.org/sdr/GRAA9621.md): Power Supply · inoperative · Mar 23, 1996 · N1075T · Doug DC987 · Emergency Lighting
  > RNO - LINE MAINTENANCE DISCOVERED THE FLOOR PROXIMITY, EMERGENCY LIGHTS AT ROW 2 AND ROW 3 FAILED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT POWER SUPPLY. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE EMERGENCY LIGHT SYSTEM. SYSTEM OPERATIONA
- [SDR GRAA96](https://openairdocs.org/sdr/GRAA96.md): Press Controller · failed · Mar 21, 1996 · N1075T · Doug DC987 · Cabin Pressure Controller
  > RNO - ON CLIMB-OUT, AIRCRAFT HAD THE AUTOPRESSURIZATION SYSTEM FAIL. AIRCRAFT RETURNED TO RNO WITHOUT FURTHER OCCURRENCE. MAINTENANCE DEFERRED THE AUTOPRESSURIZATION SYSTEM IAW MEL: 21-24. THE AIRCRAFT WAS RETURNED TO SERVICE. (X)
- [SDR GRAA9616](https://openairdocs.org/sdr/GRAA9616.md): Battery Pack · discharged · Mar 13, 1996 · N1075T · Doug DC987 · Emergency Lighting
  > LINE MAINTENANCE AT RNO, DISCOVERED THAT THE LEFT ACCESSORY COMPARTMENT EMERGENCY FLOOR TRACK LIGHTING WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY POWER SUPPLY PACK. MAINTENANCE PERFORMED AND OPERATIONAL CHECK OF THE SYSTEM. THE EMERGENCY
- [SDR GRAA9607](https://openairdocs.org/sdr/GRAA9607.md): Connector · failed · Feb 5, 1996 · N1075T · Doug DC987 · Emergency Lighting
  > LINE MAINTENANCE AT ENV, DISCOVERED THAT THE FORWARD FLIGHT ATTENDANT ENTRY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE CANNON PLUG. OPERATIONALLY CHECKED NORMAL, NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR GRAA9603](https://openairdocs.org/sdr/GRAA9603.md): Strut · req'd serv · Jan 31, 1996 · N1075T · Doug DC987 · Nose/Tail Landing Gear Strut/Axle
  > UPON TAKEOFF AT FAR, NLG WOULD NOT RETRACT. AIRCRAFT RETURNED TO FAR WITHOUT FURTHER INCIDENT. MX WAS NOTIFIED AND A FERRY PERMIT WAS GENERATED. THE AIRCRAFT DEPARTED TO MKE WITH THE GEAR DOWN AND PINNED. MX DISCOVERED THAT THE NLG TORQUE LINK SCISSORS WER
- [SDR GRAA9554](https://openairdocs.org/sdr/GRAA9554.md): Eel Lens · missing · Nov 4, 1995 · N1075T · Doug DC987 · Emergency Lighting
  > MAINTENANCE AT IFP, CLEARED A DMI THAT PERTAINED TO THE FORWARD EMERGENCY TRACK LIGHTING. MAINTENANCE REPLACED THE FLOOR TRACK LAMP PIGTAIL, AND LENS. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE SYSTEM. NO DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERV
- [SDR GRAA9553](https://openairdocs.org/sdr/GRAA9553.md): Battery Pack · discharged · Nov 4, 1995 · N1075T · Doug DC987 · Emergency Lighting
  > AT IFP, FORWARD EMERGENCY CABIN OVERHEAD LIGHTS ILLUMINATE WHEN ELECTRICAL POWER IS TURNED OFF. MAINTENANCE REMOVED AND REPLACED THE FORWARD CABIN OVERHEAD EMERGENCY LIGHTS BATTERY PACK. OPERATIONALLY CHECKED NORMAL. NO DEFECTS NOTED. AIRCRAFT WAS RETURNED
- [SDR 95ZZZM745](https://openairdocs.org/sdr/95ZZZM745.md): Eel Lamp · failed · Nov 4, 1995 · N1075T · Doug DC987 · Emergency Lighting
  > MAINTENANCE AT IFP, CLEARED A DMI THAT PERTAINED TO THE FORWARD EMERGENCY TRACK LIGHTING. MAINTENANCE REPLACED THE FLOOR TRACK LAMP PIGTAIL, AND LENS. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE SYSTEM. NO DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERV
- [SDR GRAA9552](https://openairdocs.org/sdr/GRAA9552.md): Battery Pack · discharged · Oct 25, 1995 · N1075T · Doug DC987 · Emergency Lighting
  > AT IFP, FORWARD EMERGENCY CABIN LIGHTS WERE DISCOVERED TO BE INOPERATIVE. MAINTENANCE DISCOVERED THAT THE FORWARD EMERGENCY BATTERY PACK HAD FAILED. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY BATTERY PACK. THE SYSTEM WAS OPERATIONALLY CHECKED, A
- [SDR GRAA9545](https://openairdocs.org/sdr/GRAA9545.md): Controller · malfunctioned · Sep 28, 1995 · N1075T · Doug DC987 · Cabin Pressure Controller
  > IFP - DURING CLIMB-OUT, THE AIRCRAFT FAILED TO PRESSURIZE. THE AIRCRAFT RETURNED TO IFP, WITHOUT FURTHER INCIDENT. MAINTENANCE RERACKED THE STANDBY PRESSURE CONTROLLER, AND RESEATED THE STATIC LINES. MAINTENANCE PERFORMED A GROUND MAINTENANCE TEST IAW MD-80

Next page: https://openairdocs.org/deregistered/N1075T-2013-07-29/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 = 'N1075T' AND deregistration_id = 'N1075T-2013-07-29'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N1075T-2013-07-29/reports

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