# Service difficulty reports: N803AM, cancelled Nov 14, 2006 A list on [N803AM, cancelled Nov 14, 2006](https://openairdocs.org/deregistered/N803AM-2006-11-14.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR ASMF200607008](https://openairdocs.org/sdr/ASMF200607008.md): Slide · incorrect · Jul 10, 2006 · N803AM · Boeing 7572Q8 · Escape Slide > AIRCRAFT RETURNED TO PLATFORM, RT DOOR NR 1 SLIDE WAS NOT ARMED CORRECTLY. SLIDE WAS ARMED IAW MM 25-66-01 AND DOOR WAS VERIFIED BY CONDITION, BEING ALL CORRECT. - [SDR ASMF200606017](https://openairdocs.org/sdr/ASMF200606017.md): Engine · failed · Jun 28, 2006 · N803AM · Boeing 7572Q8 · Engine Exhaust System > AIRCRAFT RETURNED TO PLATFORM, (L ENG REV CONT) AND (L ENG PRI CONT) MESSAGES WERE SHOWN IN EICAS. FIM 78-34-00, FIGURE 112 PROCEDURE WAS PERFORMED AND LT ENGINE EXCEDENCIES PAGE WAS VERIFIED SHOWING P PDIU/EEC S PDIU/ S354-29, S354-4 CODES. MESSAGES WERE ERAS - [SDR ASMF200606008](https://openairdocs.org/sdr/ASMF200606008.md): Engine · leaking · Jun 12, 2006 · N803AM · Boeing 7572Q8 · Turbine Engine Oil System > ON ARRIVAL, CAPTAIN REPORTED AIRCRAFT FLEW WITH REDUCED THRUST 1.5 HRS DUE TO LOW OIL QUANTITY INDICATION (3QTS) IN LT ENG. MX DETECTED AN OIL LEAK THRU OIL PRESSURE TRANSMITTER AND CORRECTED THE LEAK. SERVICED ENG 12 QTS, RAN ENG. NO DISCREPANCIES REPORTE - [SDR ASMF200604008](https://openairdocs.org/sdr/ASMF200604008.md): Wheel · damaged · Apr 16, 2006 · N803AM · Boeing 7572Q8 · Nose/Tail Landing Gear > AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF DURING TAXIING SPOILERS LIGHT AND EICAS MESSAGE WERE SHOWN. BITE TO SPOILERS MODULE WAS PERFORMED CONTINUING THE FAILURE, REPORT WAS DEFERRED IAW MEL 27-63-1. DURING CHECK WAS DETECTED FOD IN THE LEFT WHEEL O - [SDR ASMF200601004](https://openairdocs.org/sdr/ASMF200601004.md): Idg · failed · Jan 10, 2006 · N803AM · Boeing 7572Q8 · Alternator-Generator Drive > DURING TRANSIT CHECK, CAPTAIN REPORTED THAT APU OIL LIGHT TURNED ON. THE APU REPORT WAS DEFERRED IAW MEL 49-11-1 CAT C AND AIRCRAFT WAS DISPATCHED. LATER, AIRCRAFT RETURNED OF FLIGHT AS A CONSEQUENCE OF DURING CRUISE THE L GEN DRIVE EICAS MESSAGE WAS SHOWN A - [SDR ASMF200502005](https://openairdocs.org/sdr/ASMF200502005.md): Control Module · failed · Feb 5, 2005 · N803AM · Boeing 7572Q8 · Stabilizer Position Indicating > AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF AFTER ENGINES STARTED, EICAS MESSAGES STAB TRIM" WAS SHOWN. REPORT WAS DEFERRED IAW MEL 27-41-2. DURING TRANSIT CHECK AT MEX, LEFT STAB TRIM CONTROL MODULE WAS REPLACED IAW MM 27-41-05, TESTED CORRECT, DEFERRE - [SDR ASMF200502002](https://openairdocs.org/sdr/ASMF200502002.md): Control Module · failed · Feb 5, 2005 · N803AM · Boeing 7572Q8 · Stabilizer Position Indicating > AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF AFTER ENGINES STARTED, EICAS MESSAGES "STAB TRIM" WAS SHOWN. REPORT WAS DEFERRED IAW MEL 27-41-2. DURING TRANSIT CHECK AT MEX, LEFT STAB TRIM CONTROL MODULE WAS REPLACED IAW MM 27-41-05, TESTED CORRECT, DEFER - [SDR ASMF200501014](https://openairdocs.org/sdr/ASMF200501014.md): A/C Pack · inoperative · Jan 23, 2005 · N803AM · Boeing 7572Q8 · Cabin Cooling System > AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF LT AIR CONDITIONING PACK WAS OUT OF SERVICE. AT PLATFORM, BOTH AIR CONDITIONING SYSTEMS WERE CHECKED BEING CORRECT. DURING CHECK, LT ENGINE BLEED AIR OFF LIGHT TURNED ON, LIGHT WAS DEFERRED IAW MM 36-11-1. - [SDR ASMF200411004](https://openairdocs.org/sdr/ASMF200411004.md): Blade · nicked · Nov 5, 2004 · N803AM · Boeing 7572Q8 · Turbine Section > DURING OVERNIGHT SERVICE, BOROSCOPE INSPECTION WAS PERFORMED ON RIGHT ENGINE AND NICKS WERE DETECTED ON ONE BLADE OF 11TH STAGE, OUT OF LIMITS IAW MM 72-00-00. RIGHT ENGINE WAS REPLACED IAW MM 71-00-00, TEST CORRECT. - [SDR ASMF200407015](https://openairdocs.org/sdr/ASMF200407015.md): Bleed Valve · failed · Jul 11, 2004 · N803AM · Boeing 7572Q8 · Compressor Bleed Valve > CAPTAIN REPORTED WHEN STARTING CLIMB FROM FL350 TO FL390 THE RT ENGINE EPR'S INDICATION FLUCTUATE SEVERALLY AND ENGINE PANCAKING AND NOT CLIMBING. AIRCRAFT WAS SENT TO THE HANGAR AND BOROSCOPE INSPECTION AND FIM TESTS WAS PERFORMED TO RT ENGINE IAW MM 72-00-0 - [SDR ASMF200405010](https://openairdocs.org/sdr/ASMF200405010.md): Proximity Sensor · damaged · May 6, 2004 · N803AM · Boeing 7572Q8 · Landing Gear Position and Warning > DURING TRANSIT CHECK, (LANDING GEAR) AND (MAINTENANCE GEAR DOOR) LIGHTS TURNED ON. DURING MAINTENANCE REVISION, PSEU WAS DETECTED WITH DAMAGE ON SENSOR 076. PROXIMITY SWITCH WAS REPLACED IAW MM 32-61-02 AND TEST CORRECT IAW MM 32-61-00. - [SDR MEX2003539](https://openairdocs.org/sdr/MEX2003539.md): Pump · failed · Nov 28, 2003 · N803AM · Boeing 7572Q8 · Turbine Engine Oil System > AIRCRAFT RETURNED TO GATE DUE TO LOW OIL PRESSURE INDICATION ON NR 2 ENGINE DURING STARTING. SYSTEM WAS VERIFIED AND THE OIL PUMP WAS REPLACED IAW MM 79-21-04, TESTS WERE PERFORMED IAW MM 71-00-00, ALL OK. DURING THE OVERNIGHT SERVICE. THE ENGINE WAS VERIFI - [SDR MEX2003387](https://openairdocs.org/sdr/MEX2003387.md): Shutoff Valve · malfunctioned · Aug 23, 2003 · N803AM · Boeing 7572Q8 · Engine (Turbine/Turboprop) > DURING PUSH BACK AND LEFT ENGINE STARTING, ENGINE VALVE LIGHTS TURNED ON, SPAR VALVE DID NOT GO OFF AND N2 WAS BETWEEN 25 PERCENT AND 30 PERCENT WITHOUT EGT INCREMENTATION. THE SPAR VALVE AND FUEL SHUTOFF VALVE WERE RESET IAW MM 73-10-01, ALL TEST CORRECT. D - [SDR MEX2003236](https://openairdocs.org/sdr/MEX2003236.md): Packing · failed · Jun 18, 2003 · N803AM · Boeing 7572Q8 · Hydraulic System, Main > AIRCRAFT ARRIVED WITH CAPTAIN REPORT WITH 1 QUART OF OIL IN ENGINE NR 2. DURING REVISION WAS DETECTED LEAK IN RIGHT HYDRAULIC PUMP. THE RIGHT HYDRAULIC PUMP PACKING WAS REPLACED IAW MM. DURING OVERNIGHT SERVICE RIGHT HYDRAULIC PUMP WAS REPLACED IAW 29-11-40 - [SDR MEX2002299](https://openairdocs.org/sdr/MEX2002299.md): Fuel Control · failed · Sep 16, 2002 · N803AM · Boeing 7572Q8 · Fuel Control/Turbine Engines > FLT 600 - MEX-ATL - AIRCRAFT RETURNED TO PLATFORM AS CONSEQUENCE OF AN STARTING FAILED OF THE RIGHT ENGINE. AT POSITION 24, TECHNICIANS TRIED STARTING AGAIN AND ENGINE REACHED 52 PERCENT OF N2 BUT EGT'S WERE HIGH. AT HANGAR, THE FMC WAS REPLACED IAW MM 73-21 - [SDR ASM2002F00002](https://openairdocs.org/sdr/ASM2002F00002.md): Actuator · failed · May 18, 2002 · N803AM · Boeing 7572Q8 · Fuel Selector/Shut-Off Valve > DURING INSPECTION, DETECTED A LEAK IN THE RIGHT FUEL TANK. THE LEAK WAS AT THE RIGHT SHUTOFF VALVE. RIGHT TANK WAS SEALED. DURING OVERNIGHT SERVICE THE O-RINGS OF SHUTOFF VALVE ACTUATOR WAS REPLACED IAW MM. - [SDR MEX2002105](https://openairdocs.org/sdr/MEX2002105.md): Probe · failed · Apr 10, 2002 · N803AM · Boeing 7572Q8 · Engine EGT/TIT Indicating System > FLT 404 - MEX-JFK - AIRCRAFT WAS SENT TO THE HANGAR FOR HIGH EGT ON NR 2 ENGINE (930 GRADES). PERFORMED A FIM PROCEDURE DETECTED THE PROBES T/C 2 T/C 6 OUT OF LIMITS. THEY WERE CHANGED AND AN EGT TEST WAS PERFORMED DURING ENGINE RUNNING IAW MM 77-21-01. (M) - [SDR MEX2002015](https://openairdocs.org/sdr/MEX2002015.md): Wire Harness · damaged · Jan 18, 2002 · N803AM · Boeing 7572Q8 · Turbine Engine System Wiring > FLT 239 - GDL-MEX - CREW REPORTED THAT DURING THE ENGINE STARTING, THE ENGINE 1 WAS NOT STABILIZED, THE RPM'S REMAINED AT 42 PERCENT AND MAINTENANCE AREA REPORTED THE PRESENCE OF FLAME IN SUCH ENGINE. AT CHECKING IT WAS FOUND A DAMAGE IN THE WIRE BUNDLE NEAR ## 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 = 'N803AM' AND deregistration_id = 'N803AM-2006-11-14' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N803AM-2006-11-14/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.