# Service difficulty reports: N69523, cancelled May 17, 2006 A list on [N69523, cancelled May 17, 2006](https://openairdocs.org/deregistered/N69523-2006-05-17.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR CALA9701796](https://openairdocs.org/sdr/CALA9701796.md): Transformer · failed · Dec 23, 1997 · N69523 · Doug DC932 · Passenger Compartment Lighting > SPARKS AND SMOKE CAME FROM LT OVERHEAD BIN WHEN BIN WAS OPENED BY A PASSENGER WHILE AIRCRAFT WAS AT GATE IN ELP. THE CIRCUIT BREAKER POPPED AND THE SMOKE AND SPARKS CEASED. MAINTENANCE FOUND TRANSFORMER IN OVERHEAD BIN AT FAULT. THE AIRCRAFT WILL BE FERRIED - [SDR CALA9701751](https://openairdocs.org/sdr/CALA9701751.md): Channel · corroded · Dec 9, 1997 · N69523 · Doug DC932 · Fuselage Miscellaneous Structure > INSPECTION FOUND WING CENTER SECTION Z CHANNEL CORRODED AT FS 680 BETWEEN BL 0 AND LBL 22. THE CHANNEL WAS REMOVED IAW SRM 51-30-2. A REPLACEMENT CHANNEL WAS FABRICATED AND INSTALLED IAW SRM 51-10-1 AND 51-10-3. - [SDR CALA9701750](https://openairdocs.org/sdr/CALA9701750.md): Skin · dented · Dec 9, 1997 · N69523 · Doug DC932 · Fuselage Main, Plate/Skin > INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 237 BETWEEN LONGERON 17 AND 18L. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-04, FIGURE 38, 51-10-3, AND 51-30-2. - [SDR CALA9701748](https://openairdocs.org/sdr/CALA9701748.md): Skin · dented · Dec 9, 1997 · N69523 · Doug DC932 · Fuselage Main, Plate/Skin > INSPECTION FOUND FUSELAGE SKIN DENTED AT FS 427 BETWEEN LONGERON 20 AND 21L. THE DENTED AREA WAS REMOVED. REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 53-04, FIGURE 12B, 51-10-3, 51-30-2, AND 51-20-0. - [SDR CALA9701747](https://openairdocs.org/sdr/CALA9701747.md): Skin · dented · Dec 9, 1997 · N69523 · Doug DC932 · Fuselage Main, Plate/Skin > INSPECTION FOUND FUSELAGE SKIN DENTED AT FS 489, LONGERON 23L. DOUBLER, FILLER, AND FINGER DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 53-04, FIGURE 12B. - [SDR CALA9701746](https://openairdocs.org/sdr/CALA9701746.md): Longeron · cracked · Dec 9, 1997 · N69523 · Doug DC932 · Fuselage Main, Longeron/Stringer > INSPECTION FOUND A 5 CRACK INCH LONGERON 17L AT STA 944. THE LONGERON AND SPLICES WERE REMOVED IAW SRM 51-10-4. A NEW LONGERON AND SPLICES WERE FABRICATED AND INSTALLED IAW SRM 51-10-4, 51-10-3, AND 51-38-2. - [SDR CALA9701745](https://openairdocs.org/sdr/CALA9701745.md): Longeron · cracked · Dec 9, 1997 · N69523 · Doug DC932 · Fuselage Main, Longeron/Stringer > INSPECTION FOUND A 4 CRACK IN LONGERON 12R JUST FORWARD OF R-1 DOOR FRAME AT FS 155. AN ANGLE REPAIR WAS FABRICATED AND INSTALLED IAW ECRA 5310-03633, SRM 51-10-3, AND 51-30-5. - [SDR CALA9701749](https://openairdocs.org/sdr/CALA9701749.md): Skin · dented · Dec 5, 1997 · N69523 · Doug DC932 · Fuselage Main, Plate/Skin > INSPECTION FOUND FUSELAGE SKIN DENTED AT FS 100, LONGERON 24L. THE DENTED AREA WAS REMOVED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-04-0 AND 51-10-3. - [SDR CALA9701703](https://openairdocs.org/sdr/CALA9701703.md): Floorbeam · corroded · Nov 29, 1997 · N69523 · Doug DC932 · Fuselage Main, Floor Beam > INSPECTION FOUND FLOORBEAM CORRODED ON BOTH LT AND RT SIDES OF BS 996. THE CORRODED SECTIONS WERE REMOVED, FILLER AND DOUBLER REPAIRS WERE FABRICATED AND INSTALLED IAW SRM 53-05, FIGURE 108, SRM 51-10-4, 51-10-3, 51-30-2, 51-30-5, AND 51-30-1. - [SDR CALA9701222](https://openairdocs.org/sdr/CALA9701222.md): Oil Pump · seized · Aug 14, 1997 · N69523 · Doug DC932 · Turbine Engine Oil System > THE AIRCRAFT DEVELOPED VIBRATION SHORTLY AFTER TAKEOFF AND THE NR 2 ENGINE OIL QUANTITY BEGAN TO DROP RAPIDLY. THE NR 2 ENGINE WAS SHUT DOWN AND THE AIRCRAFT WAS RETURNED TO DCA WHERE IT LANDED WITHOUT INCIDENT. THE NR 2 ENGINE WAS REMOVED AND REPLACED. *S/ - [SDR CALA9700301](https://openairdocs.org/sdr/CALA9700301.md): Prox Sensor · inoperative · Mar 3, 1997 · N69523 · Doug DC932 · Landing Gear Position and Warning > THE NLG UNSAFE LIGHT FLICKERED AND THEN CAME ON STEADY AFTER GEAR RETRACTION. THE GEAR WAS CYCLED AND THE LIGHT EXTINGUISHED. MAINTENANCE FOUND THE NLG DRAG BRACE PROXIMITY SENSOR AT FAULT. THE SENSOR WAS REMOVED AND REPLACED IAW MM 32-60-1. A GEAR SWING W - [SDR CALA9601784](https://openairdocs.org/sdr/CALA9601784.md): Comp Blade · failed · Dec 11, 1996 · N69523 · Doug DC932 · Turbine Engine Compressor Section > THE NR 1 ENGINE FAILED AT ROTATION WITH NO WINDMILLING RPM OR OIL PRESSURE NOTED IN FLIGHT. THE AIRCRAFT WAS RETURNED TO RSW WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND METAL IN THE NR 1 ENGINE TAILPIPE. THE NR 1 ENGINE WAS REMOVED AND REPLACED. *S - [SDR CALA9600679](https://openairdocs.org/sdr/CALA9600679.md): Fuel Line · leaking · May 29, 1996 · N69523 · Doug DC932 · APU Engine Fuel and Control > A KEROSENE ODOR WAS SMELLED IN THE COCKPIT AND CABIN AFTER TAKEOFF FROM DFW. THE AIRCRAFT WAS RETURNED TO DFW WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND FUEL LINE TO APU FCU LEAKING. THE FUEL LINE WAS REMOVED AND REPLACED. THE APU WAS RUN WITH NO - [SDR CAL960414](https://openairdocs.org/sdr/CAL960414.md): Skin · cracked · Mar 19, 1996 · N69523 · Doug DC932 · Fuselage Main, Plate/Skin > HOU - INSPECTION FOUND CORROSION AND.50 INCH CRACKS IN SKIN AT LONGERON 30, STA 658. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-01, FIGURE 4, SHEET 3. (X) - [SDR CAL960413](https://openairdocs.org/sdr/CAL960413.md): Skin · loose · Mar 13, 1996 · N69523 · Doug DC932 · Horizontal Stabilizer, Plate/Skin > HOU - INSPECTION FOUND SEVERAL LOOSE RIVETS ON LEFT AND RIGHT SIDES OF RUDDER SKIN. THE RIVETS WERE REMOVED AND NEW FASTENERS WERE INSTALLED IAW SRM 51-30-2. (X) - [SDR CAL960412](https://openairdocs.org/sdr/CAL960412.md): Skin · cracked · Mar 13, 1996 · N69523 · Doug DC932 · Horizontal Stabilizer, Plate/Skin > HOU - INSPECTION FOUND TWO 1.25 INCH CRACKS IN TOP RT SIDE OF RUDDER SKIN. A REPAIR DOUBLER WAS INSTALLED IAW SRM 55-01, FIGURE 2. (X) - [SDR CAL960411](https://openairdocs.org/sdr/CAL960411.md): Cables · out of adjust · Mar 13, 1996 · N69523 · Doug DC932 · Aerodynamic Fairings > HOU - THE PULL FROM BOTH THE INTERIOR AND EXTERIOR EMERGENCY TAILCONE RELEASE HANDLES WAS LOW. THE TAILCONE CABLE SYSTEM WAS ADJUSTED IAW MM 53-50-3. (X) - [SDR CAL951016](https://openairdocs.org/sdr/CAL951016.md): Downlock Sensor · inoperative · Nov 3, 1995 · N69523 · Doug DC932 · Landing Gear Position and Warning > FLT NR 1100 - LEAVING IAH, THE RED NOSE GEAR UNSAFE LIGHT REMAINED ILLUMINATED, AFTER GEAR RETRACTION. THE GEAR WAS CYCLED, BUT THE RED LIGHT REMAINED ON WITH GEAR RETRACTED. WHEN THE GEAR WAS EXTENDED FOR RETURN TO IAH, INDICATIONS WERE NORMAL. THE NOSE GE - [SDR CAL950008](https://openairdocs.org/sdr/CAL950008.md): Strut · pressure low · Jan 3, 1995 · N69523 · Doug DC932 · Nose/Tail Landing Gear Strut/Axle > FLT NR 1708 - MDW - THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF AND THE AIRCRAFT WOULD NOT PRESSURIZE. THE AIRCRAFT WAS RETURNED TO MDW. MAINTENANCE CHECKED THE GROUND/AIR SENSE RIG AND FOUND IT TO BE WITHIN LIMITS. THE NOSE GEAR STRUT PRESSURE WAS FOU ## 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 = 'N69523' AND deregistration_id = 'N69523-2006-05-17' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N69523-2006-05-17/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.