# Service difficulty reports: N905AJ, cancelled Apr 18, 2018 A list on [N905AJ, cancelled Apr 18, 2018](https://openairdocs.org/deregistered/N905AJ-2018-04-18.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR PCSA2013122601](https://openairdocs.org/sdr/PCSA2013122601.md): Accessory Unit · faulty · Dec 24, 2013 · N905AJ · Boeing 727231 · Landing Gear Retraction/Extension System > AFTER TAKEOFF THE LG LEVER WOULD NOT GO PAST OFF TO UP POSITION. GEAR WOULD NOT COME UP. - [SDR PCSA2013050602](https://openairdocs.org/sdr/PCSA2013050602.md): Bypass Valve · faulty · May 3, 2013 · N905AJ · Boeing 727231 · Trailing Edge Flap Control System > UPON RETRACTION, INBOARD FLAPS REMAINED AT 20°. AFTER LANDING FLAPS RETRACTED NORMALLY. MAINTENANCE REPLACED THE FLAP BYPASS VALVE, THE INBD FLAP ASYMMETRIC RELAY R187 AND THE INBD FLAP INDICATOR PER THE AMM, ACCOMPLISHED THE FLAP OPERATIONAL CHECK PER THE A - [SDR SPUY201304030032](https://openairdocs.org/sdr/SPUY201304030032.md): Floorbeam · corroded · Apr 3, 2013 · N905AJ · Boeing 727231 · Fuselage Main, Floor Beam > DURING ROUTINE C CHECK INSPECTION, MAIN CARGO COMPT- FLOORBEAM CORRODED BS 620 RBL 53 ML 208 REF N/R 0930. - [SDR SPUY201304030031](https://openairdocs.org/sdr/SPUY201304030031.md): Beam · corroded · Apr 3, 2013 · N905AJ · Boeing 727231 · Fuselage Miscellaneous Structure > DURING ROUTINE C CHECK INSPECTION, MAIN CARGO COMPT- SKIN AND BEAM FLANGE LWR SKIN CORRODED, STA 910.000 LBL-27 REF N/R 0922. - [SDR SPUY201304030030](https://openairdocs.org/sdr/SPUY201304030030.md): Beam · corroded · Apr 3, 2013 · N905AJ · Boeing 727231 · Fuselage Miscellaneous Structure > DURING ROUTINE C CHECK INSPECTION, MAIN CARGO COMPT- BEAM FLANGE AND SKIN CORRODED, STA 910 REF N/R 0836. - [SDR SPUY201304030029](https://openairdocs.org/sdr/SPUY201304030029.md): Beam · corroded · Apr 3, 2013 · N905AJ · Boeing 727231 · Fuselage Miscellaneous Structure > DURING ROUTINE C CHECK INSPECTION, MAIN CARGO COMPT- BEAM FLANGE AND SKIN CORRODED STA 910 RBL 25 (LWR PART) REF N/R 0835. - [SDR SPUY201304030028](https://openairdocs.org/sdr/SPUY201304030028.md): Structure · corroded · Apr 3, 2013 · N905AJ · Boeing 727231 · Fuselage Miscellaneous Structure > DURING ROUTINE C CHECK INSPECTION, AFTER CARGO COMPT- CORRODED, S-29R, STA 1110 STA 1130. REF N/R 0703. - [SDR SPUY201304030027](https://openairdocs.org/sdr/SPUY201304030027.md): Skin · corroded · Apr 3, 2013 · N905AJ · Boeing 727231 · Wing, Plate/Skin > DURING ROUTINE C CHECK INSPECTION, RIGHT WING LEADING EDGE UPPER SKIN CORRODED, WBL 92.8. REF N/R 0178. - [SDR PCSA2011090601](https://openairdocs.org/sdr/PCSA2011090601.md): Oil System · overtemp · Sep 6, 2011 · N905AJ · Boeing 727231 · Engine Oil Temperature > NUMBER 3 ENGINE SHUT DOWN DUE TO HIGH OIL TEMPERATURE. - [SDR PCSA2011041501](https://openairdocs.org/sdr/PCSA2011041501.md): Start Valve · malfunctioned · Apr 14, 2011 · N905AJ · Boeing 727231 · Engine Start Valves/Controls > AT FL270 ENGINE NR 3 START VALVE ILLUMINATED. ACCOMPLISHED SUPPLEMENTAL PROCEDURES. SHUT DOWN NR 3 ENGINE. ACCOMPLISHED ABNORMAL ENGINE SHUTDOWN CHECKLIST ON GENERATOR INOP CHECKLIST AND ONE ENGINE INOP LANDING CHECKLIST AND WINDMILLED ENGINE SUPPLEMENTAL P - [SDR PCSA2011011302](https://openairdocs.org/sdr/PCSA2011011302.md): Switch · shorted · Jan 13, 2011 · N905AJ · Boeing 727231 · Fire Detection > DURING APPROACH INTO SAL WHEEL WELL FIRE AND BELL WERE ACTIVATED. AFTER LANDING MAINTENANCE T/S SYSTEM AND FOUND SHORT IN THE TEST SWITCH AND CORRECTED IT. NO PARTS NECESSSARY. - [SDR PCSA2011011301](https://openairdocs.org/sdr/PCSA2011011301.md): Control Unit · defective · Jan 13, 2011 · N905AJ · Boeing 727231 · Fire Detection > DURING TAXI OUT WHEEL WELL FIRE LIGHT AND BELL WENT ON INTERMITTENTLY. - [SDR PCSA2010031801](https://openairdocs.org/sdr/PCSA2010031801.md): Smoke Detector · false activation · Mar 18, 2010 · N905AJ · Boeing 727231 · Smoke Detection > SMOKE DETECTOR NR 3 LIGHT CAME ON INTERMITTENTLY IN FLIGHT. VERIFIED NO SMOKE IN CARGO COMPARTMENT. MAINTENANCE PERFORMED AN OPERATIONAL TEST OF THE SMOKE DETECTION SYSTEM. NO DEFECTS WERE FOUND AND THE AIRCRAFT WAS RETURNED TO SERVICE. - [SDR PCSA2010031502](https://openairdocs.org/sdr/PCSA2010031502.md): Detector · defective · Mar 12, 2010 · N905AJ · Boeing 727231 · Smoke Detection > CREW LOG ITEM " NR 3 SMOKE DETECTOR LIGHT ILLUMIMATED AT TOP OF DESCENT. INSPECTED AREA. FALSE INDICATION". MAINTENANCE REPLACED THE NR 3 SMOKE DETECTOR AND RETURNED THE AIRCRAFT TO SERVICE. - [SDR PCSA2010031501](https://openairdocs.org/sdr/PCSA2010031501.md): Smoke Detector · defective · Mar 11, 2010 · N905AJ · Boeing 727231 · Smoke Detection > CREW LOG ITEM "SMOKE DETECTION SYSTEM NR 3 LIGHT ILLUMINATED IN FLIGHT". MAINTENANCE REPLACED THE NR 3 SMOKE DETECTOR AND RETURNED THE AIRCRAFT TO SERVICE. - [SDR PCSA2010012001](https://openairdocs.org/sdr/PCSA2010012001.md): Duct · cracked · Jan 19, 2010 · N905AJ · Boeing 727231 · Pneumatic Distribution System > CLIMBING THROUGH 9000FT THE NR 2 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED AND A 20 PSI SPLIT IN THE PRESSURE MANIFOLD. PERFORMED THE PROCEDURES, THE LIGHT EXTINGUISHED. OPERATED THE REMAINDER OF THE FLIGHT ON NR 2 BLEED. MAINTENANCE FOUND THE NR 3 ENGINE BLE - [SDR PCSA2009110601](https://openairdocs.org/sdr/PCSA2009110601.md): Clamp · loose · Nov 6, 2009 · N905AJ · Boeing 727231 · Pneumatic Distribution System > DURING INITIAL CLIMB, ENGINE 3 STRUT OVERHEAT LIGHT ILLUMINATED. MAINTENANCE REPLACED THE AFT CLAMP ON 3 ENGINE BLEED AIR SHUTOFF VALVE. THE CLAMP WAS REPLACED AND LEAK CHECKED GOOD IN AN ENGINE OPERATIONAL CHECK. - [SDR PCSA2009102101](https://openairdocs.org/sdr/PCSA2009102101.md): Clamp · loose · Oct 21, 2009 · N905AJ · Boeing 727231 · Pneumatic Distribution System > NUMBER 3 STRUT OVERHEAT LIGHT ILLUMINATED DURING CLIMBOUT. MAINTENANCE DISCOVERED A LOOSE CLAMP ON THE NUMBER 3 PRECOOLER. THE CLAMP WAS RETORQUED AND LEAK CHECKED GOOD IN AN ENGINE OPERATIONAL CHECK. - [SDR PCSA2009072001](https://openairdocs.org/sdr/PCSA2009072001.md): Servo · malfunctioned · Jul 17, 2009 · N905AJ · Boeing 727231 · Autopilot Trim Servo > IN FLIGHT FROM SAP TO MIA "NOSE DOWN RUNAWAY TRIM" AND "JAM STABILIZER AFTER RUNAWAY TRIM". MAINTENANCE FOUND THE STABILIZER TRIM WHEEL MOVING IN THE SAME DIRECTION AT ALL TIMES REGARDLESS OF THE POSITION OF THE STABILIZER CRUISE TRIM SWITCH. THE AUTOPILOT S - [SDR PCSA2009021901](https://openairdocs.org/sdr/PCSA2009021901.md): Smoke Detector · false activation · Feb 19, 2009 · N905AJ · Boeing 727231 · Smoke Detection > LOWER CARGO FIRE DETECTION AMBER LIGHT ON IN FLIGHT (MX LIGHT). MAINTENANCE REPLACED AN AFT CARGO COMPARTMENT SMOKE DETECTOR. - [SDR PCSA12140501](https://openairdocs.org/sdr/PCSA12140501.md): Door · open · Dec 14, 2005 · N905AJ · Boeing 727231 · Electrical/Electronic Compartment Doors > FLIGHT 8313 DEPARTED AND DURING CLIMB OUT CREW REPORTED AIRCRAFT WOULD NOT PRESSURIZE, CREW DUMPED FUEL AND RETURNED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE LOWER 43 ELECTRONICS COMPARTMENT DOOR OPEN, ALSO THE COCKPIT DOOR WARNING INDICATION ## 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 = 'N905AJ' AND deregistration_id = 'N905AJ-2018-04-18' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N905AJ-2018-04-18/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.