# N1075T: 1988 Mcdonnell Douglas DC-9-87, registration cancelled 2013-07-29 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: July 29, 2013 - Status when cancelled: Sale reported, canceled - Airframe: [Mcdonnell Douglas DC-9-87](https://openairdocs.org/model/mcdonnell-douglas-dc-9-87) (registry code 3022087) - Engine: [Pratt & Whitney JT8D series](https://openairdocs.org/engine/pratt-whitney-jt8d-series) (registry code 52053) - Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) (OpenAirDocs) - Serial number: 49724 - Year built: 1988 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: December 14, 1993 - Last registry action: January 31, 2007 - Mode S code: A021CE - Location: Mexico City, Mexico - Owner type: Individual - The mark today: https://openairdocs.org/aircraft/N1075T - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=1075T - Page: https://openairdocs.org/deregistered/N1075T-2013-07-29 From the FAA registry file of November 5, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe. ADs and bulletins for the Mcdonnell Douglas DC-9-87: https://openairdocs.org/model/mcdonnell-douglas-dc-9-87.md ## Service difficulty reports (55, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR ASMF200610003](https://openairdocs.org/sdr/ASMF200610003), Oct 3, 2006: WIRE. LOOSE. 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, BEI - [SDR ASMF200608021](https://openairdocs.org/sdr/ASMF200608021), Aug 31, 2006: STRUCTURE. DELAMINATED. 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 PO - [SDR ASMF200608012](https://openairdocs.org/sdr/ASMF200608012), Aug 16, 2006: CONTROL VALVE. LEAKING. CAPTAIN REPORTED THAT AFTER LANDING, THE LT HYDRAULIC SYSTEM WAS LOST AND LT REVERSE REMAINED EXTENDED. AIRCRAFT WAS TOWED TO PLATFORM AND RECHARGED OF HYDRAULI - [SDR ASMF200608009](https://openairdocs.org/sdr/ASMF200608009), Aug 15, 2006: TUBE. LEAKING. 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 O - [SDR ASMF200605015](https://openairdocs.org/sdr/ASMF200605015), May 27, 2006: PUMP. FAILED. 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 - [SDR ASMF200605014](https://openairdocs.org/sdr/ASMF200605014), May 26, 2006: HYDRAULIC LINE. LEAKING. 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 - [SDR ASMF200603006](https://openairdocs.org/sdr/ASMF200603006), Mar 13, 2006: GPU. SMOKE. 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 T - [SDR ASMF200601010](https://openairdocs.org/sdr/ASMF200601010), Jan 15, 2006: STARTER. FAILED. DURING TAXING CAPTAIN INFORMED THAT THERE WAS NOT INDICATION OF THE LEFT ENGINE, RETURNING TO PLATFORM. DURING MAINTENANCE REVIEW, THE ENGINE STARTER AND ITS CO - [SDR ASMF200512013](https://openairdocs.org/sdr/ASMF200512013), Dec 14, 2005: BLADE. FOD. 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 - [SDR ASMF200507020](https://openairdocs.org/sdr/ASMF200507020), Jul 25, 2005: STRUT. UNDERSERVICED. 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 CORREC - [SDR ASMF200505028](https://openairdocs.org/sdr/ASMF200505028), May 25, 2005: ACTUATOR. FAILED. 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. PRESSU - [SDR ASMF200412005](https://openairdocs.org/sdr/ASMF200412005), Dec 17, 2004: WARNING LIGHT. FALSE ACTIVATION. AIRCRAFT ARRIVED WITH CAPTAIN REPORT AFTER TAKEOFF THE THREE LANDING GEAR RED LIGHTS AND AUDIBLE ALARM TURNED ON. ABNORMAL PROCEDURE WAS PERFORMED AND LIGHTS AN - [SDR ASMF200407020](https://openairdocs.org/sdr/ASMF200407020), Jul 18, 2004: ANTENNA. DAMAGED. 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 CLEANE - [SDR ASMF200406015](https://openairdocs.org/sdr/ASMF200406015), Jun 15, 2004: RADAR. FAILED. AIRCRAFT PERFORMED AN UNSCHEDULED LANDING, LOW FUEL AND CAPTAIN REPORTED RADAR SYSTEM FAILED. DURING MAINTENANCE REVISION, RADAR, ANTENNA, TRANSCEIVER AND RADAR - [SDR ASMF200405017](https://openairdocs.org/sdr/ASMF200405017), May 15, 2004: PRESSURE VALVE. FAILED. AIRCRAFT RETURNED FLIGHT BECAUSE IN AUTOMATIC MODE THE PRESSURIZATION SYSTEM HAD OSCILLATIONS AND IN MANUAL MODE THE PRESSURE VALVE COULD NOT BE CLOSED. DURING - [SDR MEX2004049](https://openairdocs.org/sdr/MEX2004049), Feb 6, 2004: STRUT. DISCHARGED. 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 3 - [SDR MEX2003572](https://openairdocs.org/sdr/MEX2003572), Dec 29, 2003: COUPLER. LEAKING. FLT 143 - PVR-MEX - DURING TRANSIT CHECK, OBSERVED HYDRAULIC LEAKAGE COMING FROM THE MLG COMPARTMENT. THE LT HYDRAULIC SYSTEM,WITH LOW LEVEL, WAS PRESSURIZED, O - [SDR MEX2003563](https://openairdocs.org/sdr/MEX2003563), Dec 25, 2003: DISPLAY. FAILED. 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 BREAKE - [SDR MEX2003448](https://openairdocs.org/sdr/MEX2003448), Sep 26, 2003: SWITCH. DEFECTIVE. FLT 306 - ACA-MEX - AIRCRAFT RETURN TO PLATFORM AS A CONSEQUENCE OF RIGHT ENGINE REVERSE UNLOCKED LIGHT TURNED ON. REVERSE MECHANISM AND ACTUATOR WERE LUBRICATE - [SDR MEX2003277](https://openairdocs.org/sdr/MEX2003277), Jul 8, 2003: SENSOR. MALFUNCTIONED. 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 PRES - [SDR MEX20030321](https://openairdocs.org/sdr/MEX20030321), Jul 3, 2003: THRUST REVERSER. MALFUNCTIONED. 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 - [SDR MEX2003249](https://openairdocs.org/sdr/MEX2003249), Jun 25, 2003: TURBINE. FAILED. AIRCRAFT ARRIVED WITH CAPTAIN REPORT 'DEFICIENT AIR CONDITIONING'. DURING REVISION THE LEFT TURBINE COOLING WAS DAMAGED. REPORT WAS DEFERRED IAW MEL 21-1, LEFT - [SDR MEX2003231](https://openairdocs.org/sdr/MEX2003231), Jun 17, 2003: NOSE COWL. DENTED. 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 - [SDR MEX2003226](https://openairdocs.org/sdr/MEX2003226), Jun 14, 2003: INDICATOR. FAILED. 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 IND - [SDR MEX2003225](https://openairdocs.org/sdr/MEX2003225), Jun 14, 2003: THERMOCOUPLE. DAMAGED. 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 OVE - [SDR MEX2003185](https://openairdocs.org/sdr/MEX2003185), May 19, 2003: GENERATOR. FAILED. AIRCRAFT ARRIVED WITH REPORT RIGHT GENERATOR OUT OF SERVICE, GENERATOR WAS REPLACED AND AFTER ENGINES STARTING CAPTAIN INFORMS THAT SAME CONDITION CONTINOUS. AI - [SDR MEX2003170](https://openairdocs.org/sdr/MEX2003170), May 10, 2003: FILTER. FAILED. 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 TH - [SDR MEX2003207](https://openairdocs.org/sdr/MEX2003207), Apr 6, 2003: RELIEF VALVE. FAILED. 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 - [SDR MEX2003073](https://openairdocs.org/sdr/MEX2003073), Mar 14, 2003: BLADE. DAMAGED. 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), Mar 7, 2003: DISPLAY. FAILED. 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 - [SDR MEX2003041](https://openairdocs.org/sdr/MEX2003041), Feb 22, 2003: ACCELEROMETER. INOPERATIVE. 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 - [SDR MEX2002140](https://openairdocs.org/sdr/MEX2002140), Jun 5, 2002: CSD. FAILED. 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 - [SDR ASM2002F00003](https://openairdocs.org/sdr/ASM2002F00003), May 19, 2002: BYPASS VALVE. MALFUNCTIONED. 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 - [SDR MEX2002353](https://openairdocs.org/sdr/MEX2002353), Mar 12, 2002: DISPLAY. FAILED. 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 - [SDR MEX2002317](https://openairdocs.org/sdr/MEX2002317), Jan 10, 2002: ENGINE. MALFUNCTIONED. 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 ADJU - [SDR GRAA9663](https://openairdocs.org/sdr/GRAA9663), Aug 22, 1996: LIGHT. INOPERATIVE. LINE MAINTENANCE AT IFP, DISCOVERED THAT THE EMERGENCY FLOOR LIGHT WAS INOPERATIVE. MAINTENANCE RELAMPED OPERATIONAL CHECKED NORMAL. NO DEFECTS NOTED. AIRCRAFT - [SDR GRAA9627](https://openairdocs.org/sdr/GRAA9627), Apr 12, 1996: BATTERIES. DISCHARGED. LINE MAINTENANCE AT RNO, DISCOVERED THAT BOTH OVERWING EXITS OVERHEAD EMERGENCY LIGHTS FAILED. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT BATTERIES. MAINT - [SDR GRAA9625](https://openairdocs.org/sdr/GRAA9625), Apr 7, 1996: OIL FILTER. DIRTY. 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. MAINTENAN - [SDR GRAA9624](https://openairdocs.org/sdr/GRAA9624), Apr 6, 1996: LENS. MISSING. 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. MAIN - [SDR GRAA9623](https://openairdocs.org/sdr/GRAA9623), Apr 5, 1996: POWER SUPPLY. INOPERATIVE. LINE MAINTENANCE AT RNO, DISCOVERED THE FORWARD EMERGENCY FLOOR LIGHT LIGHT STRIP INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLOOR LIGHT POWER - [SDR GRAA9621](https://openairdocs.org/sdr/GRAA9621), Mar 23, 1996: POWER SUPPLY. INOPERATIVE. RNO - LINE MAINTENANCE DISCOVERED THE FLOOR PROXIMITY, EMERGENCY LIGHTS AT ROW 2 AND ROW 3 FAILED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT POWER SU - [SDR GRAA96](https://openairdocs.org/sdr/GRAA96), Mar 21, 1996: PRESS CONTROLLER. FAILED. RNO - ON CLIMB-OUT, AIRCRAFT HAD THE AUTOPRESSURIZATION SYSTEM FAIL. AIRCRAFT RETURNED TO RNO WITHOUT FURTHER OCCURRENCE. MAINTENANCE DEFERRED THE AUTOPRESSURIZ - [SDR GRAA9616](https://openairdocs.org/sdr/GRAA9616), Mar 13, 1996: BATTERY PACK. DISCHARGED. LINE MAINTENANCE AT RNO, DISCOVERED THAT THE LEFT ACCESSORY COMPARTMENT EMERGENCY FLOOR TRACK LIGHTING WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BAT - [SDR GRAA9607](https://openairdocs.org/sdr/GRAA9607), Feb 5, 1996: CONNECTOR. FAILED. LINE MAINTENANCE AT ENV, DISCOVERED THAT THE FORWARD FLIGHT ATTENDANT ENTRY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE CANNON PLUG. OPERATIONALLY C - [SDR GRAA9603](https://openairdocs.org/sdr/GRAA9603), Jan 31, 1996: STRUT. REQ'D SERV. 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 DE - [SDR GRAA9554](https://openairdocs.org/sdr/GRAA9554), Nov 4, 1995: EEL LENS. MISSING. MAINTENANCE AT IFP, CLEARED A DMI THAT PERTAINED TO THE FORWARD EMERGENCY TRACK LIGHTING. MAINTENANCE REPLACED THE FLOOR TRACK LAMP PIGTAIL, AND LENS. MAINTENAN - [SDR GRAA9553](https://openairdocs.org/sdr/GRAA9553), Nov 4, 1995: BATTERY PACK. DISCHARGED. AT IFP, FORWARD EMERGENCY CABIN OVERHEAD LIGHTS ILLUMINATE WHEN ELECTRICAL POWER IS TURNED OFF. MAINTENANCE REMOVED AND REPLACED THE FORWARD CABIN OVERHEAD EMER - [SDR 95ZZZM745](https://openairdocs.org/sdr/95ZZZM745), Nov 4, 1995: EEL LAMP. FAILED. MAINTENANCE AT IFP, CLEARED A DMI THAT PERTAINED TO THE FORWARD EMERGENCY TRACK LIGHTING. MAINTENANCE REPLACED THE FLOOR TRACK LAMP PIGTAIL, AND LENS. MAINTENAN - [SDR GRAA9552](https://openairdocs.org/sdr/GRAA9552), Oct 25, 1995: BATTERY PACK. DISCHARGED. AT IFP, FORWARD EMERGENCY CABIN LIGHTS WERE DISCOVERED TO BE INOPERATIVE. MAINTENANCE DISCOVERED THAT THE FORWARD EMERGENCY BATTERY PACK HAD FAILED. MAINTENANCE - [SDR GRAA9545](https://openairdocs.org/sdr/GRAA9545), Sep 28, 1995: CONTROLLER. MALFUNCTIONED. IFP - DURING CLIMB-OUT, THE AIRCRAFT FAILED TO PRESSURIZE. THE AIRCRAFT RETURNED TO IFP, WITHOUT FURTHER INCIDENT. MAINTENANCE RERACKED THE STANDBY PRESSURE CON All 55: https://openairdocs.org/deregistered/N1075T-2013-07-29/reports.md ## Other aircraft with N1075T - [Cancelled 1991-04-17](https://openairdocs.org/deregistered/N1075T-1991-04-17): Mooney M20J, S/N 243152. Owner: [Caraway Ronald A](https://openairdocs.org/faa-owner/CARAWAY%20RONALD%20A), [Apple Valley, CA](https://openairdocs.org/faa-place/CA/Apple%20Valley) --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.