N69826

Service difficulty reports not matched to an aircraft · 25

They name N69826, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. Newest first.

Query with SQL
duckdb -csv -c "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 = 'N69826' AND registry_match IS NULL
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR P9RA20050098Battery Pack · dischargedOVERWING EMERGENCY EVACUATION LIGHTS ARE INOP. REMOVED AND REPLACED OVERWING EMERGENCY EVACUATION LIGHTS BATTERY POWER SUPPLY IAW MM 33-53-00. OPS CHECK GOOD.Sep 15, 2005 · N69826 · Doug DC982 · Emergency LightingSDR P9RA20040022Powerpack · malfunctionedDECENT INTO IAH, AT 10,000 FEET, 250 KNOTS, LOUD RUMBLE OCCURED WITH SPEED BRAKE STOWED ACCOMPANIED BY SHARP ROLL RIGHT. EMERGENCY DECLARED. LANDED IN IAH UNEVENTFUL. REMOVED AND REPLACED RUDDER POWER PACK IAW MM 272008. OPS CHECKED GOOD.Jun 20, 2004 · N69826 · Doug DC982 · Rudder Control SystemSDR CALA0300035Seat Track · corrodedINSPECTION FOUND R/H O/B SEAT TRACK CORRODED AT GALLEY MOUNT FOR #2 GALLEY. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED AND A NEW SECTION WAS SPLICED IN IAW SRM 53-05, FIGURE 4F.Feb 11, 2003 · N69826 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0300017Frame · crackedINSPECTION FOUND A 1" CRACK IN CANTED FRAME AT STA 1463, L3L-L3R. THE CRACKED SECTION OF FRAME WAS REMOVED AND REPLACED IAW SRM 51-30-00 AND 51-30-05.Jan 21, 2003 · N69826 · Doug DC982 · Fuselage Main, FrameSDR CALA0300012Clip · out of adjustTHE FORCE REQUIRED TO PULL EXTERIOR TAIL CONE RELEASE HANDLE FROM ITS RETAINING CLIPS EXCEEDED 35 POUNDS. THE HANDLE CLIPS WERE ADJUSTED AND PULL WAS WITHIN LIMITS AT 25 POUNDS.Jan 16, 2003 · N69826 · Doug DC982 · Aerodynamic FairingsSDR CALA2000271LanyardAFT GALLEY SLIDE LANYARD IMPROPERLY INSTALLED AT PREVIOUS STATION BY A CREWMEMBER. REPORTED BY FLIGHT ATTENDANT. REINSTALLED LANYARD PER 25-62-00.May 9, 2002 · N69826 · Doug DC982 · Emergency EquipmentSDR CALA0100616Skin · damagedINSPECTION FOUND FUSELAGE SKIN CREASED JUST BELOW CUSP LINE AT STA 408-446. A REPAIR WAS INSTALLED IAW ECRA 5310-04154 AND SRM 53-04, FIGURE 12B.Jun 28, 2001 · N69826 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA0100541Seat Track · corrodedINSPECTION FOUND LEFT I/B SEAT TRACK CORRODED AT FS 1041-1322. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-05 AND 51-30-01.Jun 12, 2001 · N69826 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0001469Wire · burnedAFTER APPROXIMATELY 15 MINUTES OF LEVEL FLIGHT AT FL310 COCKPIT FILLED WITH SMOKE. POPPING AND SPARKING OCCURRED AT THE JUMP SEAT (OBSERVERS) RT SHOULDER AREA. FOUR AC BUS CIRCUIT BREAKERS POPPED BEHIND CAPTAINS SEAT. AIRCRAFT DIVERTED TO BHM. FOUND 15 WIROct 1, 2000 · N69826 · Doug DC982 · Electrical Power System WiringSDR CALA9901120Balance Wt · corrodedINSPECTION FOUND RT ELEVATOR O/B TIP MASS BALANCE CORRODED. THE RT WEIGHT WAS REMOVED. INSTALLED NEW RIB AND COUNTER WEIGHT IAW SRM 51-30-05.Sep 1, 1999 · N69826 · Doug DC982 · Elevator StructureSDR CALA9901107Skin · dentedINSPECTION FOUND DENTS IN FORWARD FUSELAGE SKIN ABOVE CUSP LINE AT FS 229 - 265, LONGERON 15L - 18L. THE DENTED AREA OF SKIN WAS REMOVED, A NEW SECTION OF SKIN, DOUBLER, AND LONGERON STRAP WERE INSTALLED IAW SRM 51-10-03 AND ECRA 5330-02445.Aug 30, 1999 · N69826 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA9901106Skin · dentedINSPECTION FOUND THE LT ELEVATOR GEAR TRIM TAB DENTED AT I/B TRAILING EDGE. THE TRIM TAB WAS REMOVED, REPAIRED AND REINSTALLED IAW MM 27-30-04.Aug 30, 1999 · N69826 · Doug DC982 · Elevator, Tab StructureSDR CALA9701168Longeron · crackedINSPECTION FOUND A 1 INCH CRACK IN LONGERON 2R AND A 1 INCH CRACK IN LONGERON 2L AT STA 1418. BOTH SECTIONS OF CRACKED LONGERON WERE REMOVED AND REPLACED WITH SPLICE IAW SRM 53-02, FIGURE 18.Aug 6, 1997 · N69826 · Doug DC982 · Fuselage Main, Longeron/StringerSDR CALA9701166Frame · crackedINSPECTION FOUND A .5 INCH CRACK ON BELTFRAME STA 1418 UNDER LONGERON 2L AND A 1 INCH CRACK AT LONGERON 2R. THE CRACKS WERE STOP DRILLED AND REPAIRS WERE INSTALLED IAW DOUGLAS SERVICE REWORK DRAWING SR09530003.Jul 29, 1997 · N69826 · Doug DC982 · Fuselage Main, FrameSDR CALA9701167Intercostal · crackedINSPECTION FOUND A 1 INCH CRACK IN RADIUS OF MAIN CABIN DOOR INTERCOSTAL AFT OF HANDLE TORQUE SHAFT. A NEW INTERCOSTAL WAS INSTALLED IAW SRM 51-30-2.Jul 26, 1997 · N69826 · Doug DC982 · Passenger/Crew DoorsSDR CALA9701169Angle · corrodedINSPECTION FOUND Z-ANGLE CORRODED ALONG ENTIRE LENGTH OF LOWER DOOR JAMB IN AFT BAGGAGE BIN. THE ANGLE WAS REPAIRED IAW SRM 53-05, FIGURE 63.Jul 25, 1997 · N69826 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA9600851Slide · low pressureINSPECTION FOUND AFT TAILCONE SLIDE BOTTLE PRESSURE LOW. THE TAILCONE SLIDE WAS REMOVED AND REPLACED IAW MM 25-62-02.Jun 19, 1996 · N69826 · Doug DC982 · Escape SlideSDR CAL960641Bearing · failedTHE NR 2 ENGINE FAILED WHILE EN ROUTE FROM IAH TO TUS. A MUFFLED BANG WAS HEARD WITH THE EPR AND RPM DROPPING TO ZERO. THE AIRCRAFT WAS DIVERTED TO ELP WHERE IT LANDED WITHOUT INCIDENT. THE NR 2 ENGINE WAS REMOVED AND REPLACED. THE SDR WILL REMAIN OPEN FORMay 21, 1996 · N69826 · Doug DC982 · Engine (Turbine/Turboprop)SDR CAL950817Doubler · crackedHOU - INSPECTION FOUND A 2 INCH CRACK IN SPLICE DOUBLER AT LEADING EDGE STATION 194.843. THE SPLICE DOUBLER WAS REPAIRED IAW ECRA 5710-01645. (M)Aug 21, 1995 · N69826 · Doug DC982 · Wing Miscellaneous StructureSDR CAL950774Rib · crackedHOU - INSPECTION FOUND A 1 INCH CRACK AT LOWER FLANGE OF FOURTH RIB OUTBOARD OF NR 9 FLAP TRACK. A NEW RIB WAS INSTALLED IAW SRM 51-30-2 AND SRM 51-30-5. (X)Aug 21, 1995 · N69826 · Doug DC982 · Wing, Rib/BulkheadSDR CAL950773Skin · dentedHOU - INSPECTION FOUND A 1 INCH LONG DENT IN SKIN AT STA 1193, LONGERON 19L. THE SKIN WAS REPAIRED IAW SRM 53-04, FIGURE 38, SHEET 21. (X)Aug 21, 1995 · N69826 · Doug DC982 · Fuselage Main, Plate/SkinSDR CAL950772Rib · crackedHOU - INSPECTION FOUND A 3 INCH CRACK IN RT WING RIB. A DOUBLER WAS INSTALLED IAW SRM 57-06, FIGURE 5. (X)Aug 21, 1995 · N69826 · Doug DC982 · Wing, Rib/BulkheadSDR CAL950771Belt Frame · corrodedHOU - INSPECTION FOUND BELT FRAME CORRODED AT STA 1309, LONGERON 27L TO LONGERON 27R. THE CORROSION WAS REMOVED AND THE AREA WAS TREATED AND PRIMED IAW SRM 53-01. (X)Aug 21, 1995 · N69826 · Doug DC982 · Fuselage Main, FrameSDR CAL950770Angle · corrodedHOU - INSPECTION FOUND THRESHOLD Z-ANGLE CORRODED IN FORWARD BAGGAGE BIN. THE AREA WAS REPAIRED IAW SRM 53-01 AND SRM 51-10-1. (X)Aug 20, 1995 · N69826 · Doug DC982 · Fuselage Miscellaneous StructureSDR CAL950631Slide · low pressureIAH - FLT 0291 - INSPECTION FOUND THE AFT GALLEY DOOR EMERGENCY EVACUATION SLIDE WITH LOW PRESSURE DURING A PRE-FLIGHT CHECK. THE AFT GALLEY DOOR EMERGENCY EVACUATION SLIDE WAS REMOVED AND REPLACED. (X)Aug 1, 1995 · N69826 · Doug DC982 · Escape Slide
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