N16232, cancelled Jun 15, 1999
Service difficulty reports · 26
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. 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 = 'N16232' AND deregistration_id = 'N16232-1999-06-15' 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.
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 = 'N16232' AND deregistration_id = 'N16232-1999-06-15' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR CALA9701782Cylinder · leakingTHE NR 1 ENGINE HYDRAULIC LOW PRESSURE LIGHT ILLUMINATED AND HYDRAULIC QUANTITY DROPPED TO ZERO ON APPROACH TO EWR. ALL ABNORMAL AND EMERGENCY CHECKLISTS WERE ACCOMPLISHED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LT MLG HYDRAULIC TRANSSDR CALA9700978Light · inoperativeINSPECTION FOUND FIRST CLASS EMERGENCY TRACK LIGHT AT L-1 DOOR INOPERATIVE. MAINTENANCE REPLACED SOCKET AND DAMAGED WIRE, OPERATIONAL CHECK WAS GOOD.SDR CALA9700584Tr Unlock Light · illuminatedONTAKEOFF ROLL, CREW RECEIVED NR 1 THRUST REVERSER UNLOCK LIGHT ILLUMINATE. REJECTED TAKEOFF AT 100 KNOTS. RETURNED TO GATE WHERE MAINTENANCE PERFORMED INSPECTION PER MM 5-5-111 P201-208. ALSO, TESTED TR SYSTEM IAW B7373 MM 78-32-01, ALL CHECKED NORMAL.SDR CALA9601628Solenoid · inoperativeTHE GEAR LATCH WOULD NOT RELEASE AFTER TAKEOFF. THE GEAR HANDLE WOULD NOT MOVE TO THE UP POSITION. CIRCUIT BREAKERS WERE PULLED AND RESET IAW QRH PROCEDURES, BUT WITH NO CHANGE. THE AIRCRAFT WAS RETURNED TO GSO WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCESDR CALA9601188Hyd Pump · leakingTHE A-SYSTEM HYDRAULIC QUANTITY DROPPED TO ZERO FOLLOWED BY LOSS OF PRESSURE ON NR 2 ENGINE WHILE EN ROUTE. AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 ENGINE DRIVEN HYDRAULIC PUMP LEAKING. THE PUMP WAS REMOVED SDR CALA9600906Pcu · inoperativeTHE AIRCRAFT HAD AN UNCOMMANDED ROLL TO THE RIGHT ON TAKEOFF. FIFTEEN TO TWENTY DEGREES OF LEFT AILERON WAS REQUIRED TO MAINTAIN LEVEL FLIGHT. ALL OTHER INDICATIONS WERE NORMAL. THE AIRCRAFT CONTINUED TO CLE WHERE IT LANDED WITHOUT FURTHER PROBLEM. THE YAWSDR CALA9600798Strap · corrodedINSPECTION FOUND STRAP AT C-1 DOOR THRESHOLD CORRODED, STA 420 TO 500. A NEW STRAP WAS FABRICATED AND INSTALLED IAW SRM 51-40-3 AND 51-30-2.SDR CALA9600801Skin · crackedINSPECTION FOUND A 1 INCH CRACK IN UPPER SKIN OF RT WING INBOARD AFT FLAP. THE CRACKED AREA WAS CUT OUT, A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-2 AND MM 51-20-0.SDR CALA9600811Floorbeam · corrodedINSPECTION FOUND FLOORBEAM UPPER CHORD CORRODED AT STA 294, RBL 40 TO 55. THE CORRODED SECTION OF CHORD WAS CUT OUT, A REPLACEMENT CHORD AND L-ANGLE DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 53-10-9, 52-20-1 AND 52-10-2.SDR CALA9600810Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 328. THE FLOORBEAM WAS REMOVED AND A NEW FLOORBEAM WAS FABRICATED AND INSTALLED IAW SRM 53-10-9 AND MM 51-20.SDR CALA9600812Frame · crackedINSPECTION FOUND A 3 INCH CRACK IN FORWARD CARGO FRAME AT STA 480, S21L. THE CRACK WAS STOP DRILLED IAW SRM 51-10-6. REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-30-2 AND 51-10-2.SDR CALA9600803Bracket · crackedINSPECTION FOUND A 1.5 INCH CRACK IN LT ANGLE BRACKET AT REAR SPAR OF VERTICAL STABILIZER. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-00-0, 51-40-3, 51-10-2 AND 51-30-2.SDR CALA9600802Bracket · crackedINSPECTION FOUND A 2 INCH CRACK IN RT ANGLE BRACKET AT REAR SPAR OF VERTICAL STABILIZER. THE CRACK WAS STOP DRILLED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-10-2 AND 51-30-2.SDR CALA9600797Channel · crackedTHE STRINGER TO FLOOR BEAM ATTACHMENT U-CHANNEL HAD TWO 1 INCH CRACKS AT STA 500A, STRINGER 28R. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-20-1, FIGURE 7 AND 51-30-2.SDR CALA9600796Intercostal · crackedINSPECTION FOUND A 1 INCH CRACK IN FORWARD CARGO PIT INTERCOSTAL AT STA 500, STRINGER 27L. THE INTERCOSTAL WAS REMOVED AND A NEW INTERCOSTAL WAS FABRICATED AND INSTALLED IAW SRM 51-20-1, 51-10-2 AND 51-30-2.SDR CALA9600795Frame · crackedINSPECTION FOUND A .5 INCH CRACK IN FRAME AT STA 480, BL 0. THE CRACK WAS REMOVED AND A DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 53-10-4.SDR CALA9600799Blkhd Stiffener · crackedINSPECTION FOUND A .5 INCH CRACK IN RADIUS OF VERTICAL STIFFENER AT STA 727 BULKHEAD. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-4, 51-10-2 AND 51-21.SDR CALA9600809Skin · dentedINSPECTION FOUND SEVERAL DENTS IN FORWARD CARGO DOOR SKIN. THE DENTED AREA WAS CUT OUT, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 52-00-3, 51-30-2 AND 51-10-2.SDR CALA9600808Skin · creasedINSPECTION FOUND A 3 INCH CREASE IN FUSELAGE SKIN AT STA 1120, BL 0. THE CREASED AREA WAS CUT OUT. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-30-3.SDR CALA9600800Aux Track · crackedINSPECTION FOUND A .5 INCH CRACK IN MID AUXILIARY TRACK OF RT WING ABOVE NR 6 SLAT. A REPAIR WAS INSTALLED IAW SRM 51-30-2.SDR CALA9600804Slide · inoperativeTHE L-1 DOOR EVACUATION SLIDE FAILED DEPLOYMENT TEST. THE COVER LANYARD WOULD NOT RELEASE AND THE SLIDE ONLY PARTIALLY INFLATED. THE SLIDE WAS REMOVED AND REPLACED IAW MM 25-61-30.SDR CALA9600807Sign · inoperativeTHE SELF ILLUMINATING EXIT SIGN IN AFT CABIN FAILED ILLUMINOSITY CHECK. THE EXIT SIGN WAS REMOVED AND REPLACED.SDR CALA9600805Wire · damagedA SECTION OF FORWARD CABIN EMERGENCY PATH LIGHTS WERE FOUND INOPERATIVE. THE WIRING AT FORWARD TRACK SECTION WAS REPAIRED IAW MM 33-50-0.SDR CAL950860Chord · crackedGSO - INSPECTION FOUND A 2 INCH CRACK FROM FORWARD HOLE TO AFT HOLE OF RT CHORD AT STA 727, STR 18A. A REPAIR WAS ACCOMPLISHED IAW ECRA 5310-03165 AND EA 5310-02918. (X)SDR CAL950235Hyd Module · inoperativeMSY - FLT 1275 - THE RT MLG RED UNSAFE LIGHT REMAINED ILLUMINATED AFTER TAKEOFF WITH THE GEAR HANDLE IN THE UP POSITION. THE GEAR WAS CYCLED AND RED LIGHT EXTINGUISHED. THE RED LIGHT ILLUMINATED AGAIN WHEN THE GEAR HANDLE WAS PLACED IN THE OFF POSITION, BUT SDR CAL950120Hyd Valve · leakingBWI - FLT 1555 - THE AIRCRAFT LOST THE 'A' SYSTEM HYDRAULIC QUANTITY SHORTLY AFTER TAKEOFF FROM BWI. THE AIRCRAFT WAS RETURNED TO BWI WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE 'A' SYSTEM HYDRAULIC MANUAL SHUT-OFF VALVE IN THE TAIL COMPARTMENT L
Back to N16232, cancelled Jun 15, 1999