# Service difficulty reports: N805AM, cancelled Jul 31, 2012 A list on [N805AM, cancelled Jul 31, 2012](https://openairdocs.org/deregistered/N805AM-2012-07-31.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR ASMF200707009](https://openairdocs.org/sdr/ASMF200707009.md): Landing Gear · inoperative · Jul 13, 2007 · N805AM · Boeing 7572Q8 · Nose/Tail Landing Gear > AIRCRAFT RETURNED, NOSE LANDING GEAR DID NOT RETRACT. DURING CHECK, TECH DETECTED THE LOCK PIN OF THE NOSE LANDING GEAR INSTALLED, SO IT WAS REMOVED AND AIRCRAFT WAS DISPATCHED. OVERWEIGHT LANDING INSPECTION WAS NOT NECESSARY, AIRCRAFT LANDED WITH 73900 POUNDS - [SDR ASMF200703004](https://openairdocs.org/sdr/ASMF200703004.md): Idg · leaking · Mar 12, 2007 · N805AM · Boeing 7572Q8 · Alternator-Generator Drive > AIRCRAFT REJECTED TAKEOFF AT 80 KNOTS DUE TO (L GEN) LIGHT TURNED ON IN EICAS. DURING MAINTENANCE CHECK, THE LT IDG WAS DETECTED WITH LOW OIL LEVEL. FAILURE WAS DEFERRED BY MEL 24-00-1, THE LANDING GEAR AND BRAKES WERE CHECKED BY CONDITION, BEING ALL CORRECT. - [SDR ASM200608020](https://openairdocs.org/sdr/ASM200608020.md): Actuator · leaking · Aug 27, 2006 · N805AM · Boeing 7572Q8 · Rudder Actuator > DURING OVERNIGHT CHECK, A HYDRAULIC LEAK WAS DETECTED IN THE RIGHT RUDDER ACTUATOR. RUDDER ACTUATOR WAS REPLACED IAW MM 27-21-20, TESTED CORRECT. - [SDR ASMF200607017](https://openairdocs.org/sdr/ASMF200607017.md): Pdu · malfunctioned · Jul 23, 2006 · N805AM · Boeing 7572Q8 · Trailing Edge Flap Control System > CAPTAIN REPORTED THAT DURING APPROACH THE LT FLAP/SLAT SYSTEM DID NOT OPERATE HYDRAULICALLY IN NORMAL MODE PROCEEDING TO THE ALTERNATE MODE AND FLAPS DISAGREE MESSAGE APPEARED IN EICAS. FIM 27-51-00 PROCEDURE AND BITE 27-7 WERE PERFORMED TO FSEU SHOWING PDU/T - [SDR ASMF200512015](https://openairdocs.org/sdr/ASMF200512015.md): Iru · failed · Dec 16, 2005 · N805AM · Boeing 7572Q8 · Inertial Guidance System > DURING TRANSIT CHECK, THE LT RDMI SHOWED HDG AND VOR FLAGS. THE SENSORS WERE CHECKED IN FMC SHOWING THAT THE THREE INERTIAL UNITS WERE CORRECT; THE LT AND CENTRAL IRS ALIGN PROCEDURE WAS PERFORMED AND THE RMIS WERE INTERCHANGED, BUT FAILURE CONTINUED. THE RT A - [SDR ASMF200511009](https://openairdocs.org/sdr/ASMF200511009.md): Starter · damaged · Nov 23, 2005 · N805AM · Boeing 7572Q8 · Engine Starter > DURING LT ENGINE STARTING, THE PNEUMATIC STARTER FAILED. DURING MAINTENANCE REVISION WAS DETECTED THE PNEUMATIC STARTER WITH DAMAGE, SO IT WAS REPLACED IAW MM 80-11-01 AND OPERATIONAL TEST WAS PERFORMED IAW MM 71-00-01, ALL CORRECT. - [SDR ASMF200506013](https://openairdocs.org/sdr/ASMF200506013.md): Idg · failed · Jun 10, 2005 · N805AM · Boeing 7572Q8 · Alternator-Generator Drive > AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF DURING THE LEFT ENGINE STARTED, THE N2 REACHED 30 PERCENT AND IT DID NOT INCREASE. THE LEFT ENGINE WAS STARTED AGAIN OPENING THE STARTER VALVE MANUALLY AND IT STARTED TO SLOW, APPEARING THE L DRIVE AND L GEN O - [SDR ASMF200506003](https://openairdocs.org/sdr/ASMF200506003.md): Idg · failed · Jun 2, 2005 · N805AM · Boeing 7572Q8 · APU Controls > AIRCRAFT RETURNED, LT GENERATOR FAILURE, APU DID NOT START AT 35 000 FT, 24 22 25 EICAS MESSAGES, 01 GEN OFF DISPLAYED AND 01 AS BUSS OFF REMAINED ILLUMINATED. QRH ABNORMAL PROCEDURE WAS PERFORMED, PAGE 09-03, RETURNING. DURING TEST WAS DETECTED LOW QUANTITY O - [SDR ASMF200505027](https://openairdocs.org/sdr/ASMF200505027.md): Engine · failed · May 24, 2005 · N805AM · Boeing 7572Q8 · Engine (Turbine/Turboprop) > CAPTAIN REPORTED THAT DURING DESCENT AT 18500 FEET, THE LEFT ENGINE OIL FILTER LIGHT CAME ON. THE ABNORMAL PROCEDURE 05-14 WAS PERFORMED AND THE A/T ARMED SWITCH WAS SHUT OFF AND THE ACCELERATOR WAS HELD BUT LIGHT CONTINUED. ENGINE WAS SHUT DOWN. AT PLATFOR - [SDR ASMF200409004](https://openairdocs.org/sdr/ASMF200409004.md): Heat Exchanger · leaking · Sep 11, 2004 · N805AM · Boeing 7572Q8 · Engine Oil Distribution (Airframe Furnished) > DURING TRANSIT CHECK, A LEAK WAS DETECTED ON OIL TANK TUBE SCUPPER AND FUEL/OIL HEAT EXCHANGER. LT ENGINE WAS STARTED AND LEAK INCREASED. FUEL/OIL HEAT EXCHANGER WAS REPLACED IAW MM 79-21-00, TEST CORRECT. DURING OVERNIGHT SERVICE, ENGINE RUNNING WAS PERFORME - [SDR ASMF200405027](https://openairdocs.org/sdr/ASMF200405027.md): Valve · failed · May 28, 2004 · N805AM · Boeing 7572Q8 · Engine (Turbine/Turboprop) > AIRCRAFT RETURNED TO PLATFORM, LT ENGINE WAS SHUTDOWN AND (FUEL CONT) AND (SPAR VALVE) LIGHTS TURNED ON. STATUS DISPLAY MESSAGES, APU PERFORMANCE AND ABNORMAL STATUS WERE CHECKED, ALL CORRECT. LT SPAR FUEL SHUTOFF VALVE WAS OPERATED MANUALLY AND IT WAS WITH FA - [SDR MEX2004019](https://openairdocs.org/sdr/MEX2004019.md): Thrust Reverser · failed · Jan 15, 2004 · N805AM · Boeing 7572Q8 · Engine Thrust Reverser > DURING TRANSIT REVISION, THE LT REVERSER WAS OPEN AND LIGHT AND MESSAGE WAS IN DISPLAY. THE REVERSER WAS REVISED AND ICE AND SNOW WAS DETECTED INTO THE REVERSE. THE REVERSER WAS NOT CLOSED COMPLETELY BECAUSE A GAP OF 2 INCHES IS BETWEEN COVERS. THE CABLE BE - [SDR MEX2003560](https://openairdocs.org/sdr/MEX2003560.md): Indicator · leaking · Dec 23, 2003 · N805AM · Boeing 7572Q8 · Hydraulic Quantity Indicator > FLT 494 - MEX-LAX - AIRCRAFT PERFORMED AN UNSCHEDULED LANDING IN GDL AS CONSEQUENCE OF THE RIGHT QUANTITY INDICATION DECREASE TO.08 QUARTS. AT PLATFORM, THE HYDRAULIC SYSTEM WAS REPLENISHED TO DETECT THE LEAKAGE, THE DIFFERENTIAL PRESSURE INDICATOR WAS REPLA - [SDR MEX2003534](https://openairdocs.org/sdr/MEX2003534.md): Pitot Tube · damaged · Nov 25, 2003 · N805AM · Boeing 7572Q8 · Pitot/Static System > AIRCRAFT RETURNED TO GATE DUE TO (R AUX PITOT) LIGHT WAS TURNED ON AND THE CABIN TEMPERATURE CONTROL HAD A FAILURE, TEMP REACHED 37 DEGREES CELSIUS. AIRCRAFT WAS SENT TO THE HANGAR AND DURING OVERNIGHT SERVICE THE RELATED PITOT WIRES/CONNECTORS AND THE CABIN - [SDR MEX2003273](https://openairdocs.org/sdr/MEX2003273.md): Antenna · failed · Jul 7, 2003 · N805AM · Boeing 7572Q8 · Doppler System > AIRCRAFT ARRIVED WITH CAPTAIN REPORT RADAR OUT OF SERVICE. DURING REVISION WAS DETECTED WAVE GUIDE WITH DAMAGE. AIRCRAFT WAS SENT TO THE HANGAR, AND THE WAVE GUIDE WAS REPLACED IAW 34-40-01. ADDITIONALLY AS A PREVENTIVE ACTION ANTENNA RADAR WAS REPLACED, AL - [SDR MEX2003150](https://openairdocs.org/sdr/MEX2003150.md): Control Unit · failed · May 1, 2003 · N805AM · Boeing 7572Q8 · Brake Anti-Skid Section > DURING TRANSIT CHECK CAPTAIN REPORTED NORM ANTI-SKID AND ALTN ANTI-SKID MESSAGES IN EICAS. MESSAGE APPEARED EVERY TIME THAT THE PARKING BRAKES WERE USED. FIM PROCEDURE WAS ACCOMPLISHED BUT NO FAILURE CODE APPEARS. AIRCRAFT WAS SENT TO THE HANGAR. ANIT-SKID - [SDR MEX2003016](https://openairdocs.org/sdr/MEX2003016.md): Warning System · malfunctioned · Jan 29, 2003 · N805AM · Boeing 7572Q8 · Central Warning > FLT 600 - MEX-ALT - AIRCRAFT RETURNED TO PLATFORM, DURING ENGINES STARTING, MESSAGE EICAS STATUS MAIN BATTERY CHARGE. RESET PROCEDURE WAS PERFORMED AND MESSAGES WAS ERASED, BUT WHEN BATTERY AND BARS WERE DISCONNECTED MESSAGES EICAS STATUS LEFT AND RIGHT CONTR - [SDR MEX2002346](https://openairdocs.org/sdr/MEX2002346.md): Indicator · malfunctioned · Nov 21, 2002 · N805AM · Boeing 7572Q8 · Engine Pressure Ratio (EPR) > FLT 171 - JIJ- DURING TAKEOFF EPR INDICATIONS WAS BLANK RIGHT ENGINE AND N1 WITH FLUCTUATIONS AT REDUCE POWER ON RIGHT ENGINE AFTER 5 MINUTES INDICATIONS WAS NORMAL. AFTER 35 MINUTES IN FLIGHT RETURNED TO AIRPORT. AT PLATFORM, TECHNICAL PERSONNEL CHECKED CHP - [SDR MEX2002297](https://openairdocs.org/sdr/MEX2002297.md): Hydraulic Line · leaking · Sep 13, 2002 · N805AM · Boeing 7572Q8 · Hydraulic System, Main > FLT 405 - JFK - AIRCRAFT RETURNED TO PLATFORM AS CONSEQUENCE OF AN HYDRAULIC LEAKAGE IN THE RIGHT SYSTEM. TECHNICIAN REVIEWED SUCH SYSTEM AND FOUND LEAKAGE IN A PIPELINE FROM THE FILTERS TO THE WHEELS. PIPELINE WAS REPLACED IAW MM 29-11-17, TESTS OK. (M) - [SDR MEX2002145](https://openairdocs.org/sdr/MEX2002145.md): Warning System · activated · Sep 5, 2002 · N805AM · Boeing 7572Q8 · Hydraulic Indicating System > FLT 902 - MEX-MTY - AIRCRAFT RETURN TO GATE DUE TO CENTRAL AND LEFT HYDRAULIC SYSTEM RSVR LIGHT CAME ON. SUPPLY LINES AND DEPRESSURIZATION VALVES WERE CHECKED NO DAMAGE WAS FOUND. NITROGEN SYSTEM WAS SERVICED AND WAS TESTED IAW MM 29-11-00. DURING OVERNIGHT - [SDR MEX2002187](https://openairdocs.org/sdr/MEX2002187.md): Slide · out of adjust · Jun 12, 2002 · N805AM · Boeing 7572Q8 · Escape Slide > FLT 170 - MEX-TIJ - CAPTAIN REPORTED THAT THE DOOR NR 1 SLIDE WAS NOT ARMED. DURING CHECK WAS DETECTED THAT THE ARMED LIGHT WAS INOPERATIVE AND THE ACTIVATION MECHANISM WAS IN AN ABNORMAL POSITION. TECHNICAL PERSONNEL TRIED TO REMOVED THE DOOR COVER AND THE ## 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 = 'N805AM' AND deregistration_id = 'N805AM-2012-07-31' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N805AM-2012-07-31/reports --- 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.