N16884, cancelled Sep 13, 2000
Service difficulty reports · 28
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 = 'N16884' AND deregistration_id = 'N16884-2000-09-13' 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 = 'N16884' AND deregistration_id = 'N16884-2000-09-13' 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 CALA0000307Strut · dischargedTHE NOSE GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION DEPARTING IAH. THE GEAR WAS LOWERED AND THE GREEN LIGHT CAME ON. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE X DIMENSION ON NLG STRUT LOW. ASDR CALA9901652Latch · out of rigTAIL CONE PULL FROM INSIDE HANDLE WAS EXCESSIVE. THE TAIL CONE WOULD NOT DEPLOY FROM THE AFT SERVICE DOOR. THE TAIL CONE LATCHES WERE ADJUSTED AND OPERATIONAL CHECKS WERE GOOD IAW MM 53-53-00.SDR CALA9901651Beam · corrodedINSPECTION FOUND Z-BEAM CORRODED BENEATH CENTER THRESHOLD PLATE IN MID CARGO BIN. THE Z-BEAM WAS REPLACED IAW SRM 53-05, FIGURE 63.SDR CALA9901596Frame · crackedINSPECTION FOUND A 2 AND .125 INCH CRACK IN CANTED BELTFRAME WEB AT LEFT SIDE, STA 1463. THE WEB WAS REMOVED AND REPLACED IAW SRM 51-30-1.SDR CALA9901597Angle · corrodedINSPECTION FOUND ANGLE CORRODED AT STA 1338, LONGERON 18L. A NEW SECTION OF ANGLE WAS SPLICED IN IAW SRM 53-03, FIGURE 14.SDR CALA9901579Seat Track · corrodedINSPECTION FOUND RT O/B SEAT TRACK CORRODED AT STA 218-256. THE CORRODED SECTION OF SEAT TRACK WAS REPLACED IAW SRM 53-05, FIGURE 4F.SDR CALA9901566Skin · crackedINSPECTION FOUND A 4 INCH CRACK IN FUSELAGE SKIN NEAR FORWARD LAV ON LT SIDE AT STA 222. REPAIRED IAW ECRA 5330-02445.SDR CALA9901565Longeron · crackedINSPECTION FOUND A .5 INCH CRACK AT LOWER FASTENER HOLE OF LONGERON 17L AT STA 237. A NEW SECTION OF LONGERON WAS INSTALLED IAW SRM 53-02, FIGURE 18.SDR CALA9901564Seat Track · corrodedINSPECTION FOUND LT I/B SEAT TRACK CORRODED AT STA 1079-1309. A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-30-1.SDR CALA9800878Valve · leakingSMOKE APPEARED IN COCKPIT AND CABIN ON DEPARTURE FROM DCA. THE RT PACK WAS SHUT OFF AND THE SMOKE CLEARED. THE FLIGHT WAS CONTINUED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND RT OIL FILLED WATER SEPARATOR VALVE LEAKING OIL. THE VALVE WAS RESDR CALA9800330Wire · burnedTHE AIRCRAFT WAS RETURNED TO IAH WHEN THE PRIMARY TRIM BECAME INOPERATIVE. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE OPENED DOGHOUSE ON VERTICAL STABILIZER AND FOUND WIRE BUNDLES BURNED. NEW WIRES WERE SPLICED IN TO PLUG P10-399 FOR PRIMARY TSDR CALA9701612Skin · crackedINSPECTION FOUND A 2.5 INCH CRACK IN RT WING LEADING EDGE SKIN WHERE NR 2 AND NR 3 SLAT PANELS MEET, WS XOS 286. A REPAIR WAS INSTALLED IAW ECRA 5720-01619.SDR CALA9701600Cable · frayedINSPECTION FOUND TAIL CONE RELEASE CABLE FRAYED. THE CABLE WAS REMOVED AND REPLACED AND PULL CHECKED IAW MM 53-53-00.SDR CALA9701576Doubler · crackedINSPECTION FOUND THREE CRACKS IN COCKPIT LT WINDOW RETAINER DOUBLER. THE CRACKS WERE LOCATED AT FASTENERS AND MEASURED .0625 TO .125 INCH LENGTH. THE COCKPIT LT WINDOW RETAINER DOUBLER WAS REMOVED AND REPLACED IAW EA SA 005-5600-01004.SDR CALA9701575Doubler · crackedINSPECTION FOUND A 1 INCH CRACK IN COCKPIT RT WINDOW RETAINER DOUBLER. THE COCKPIT RT WINDOW RETAINER DOUBLER WAS REMOVED AND REPLACED IAW EA SA 006-5600-01004.SDR CALA9701435Wire · brokenEMERGENCY TRACK LIGHTING INOP FROM ROW 5 THROUGH ROW 12. REPAIRED BROKEN WIRE FOUND AT MID BATTERY PACK.SDR CALA9701380Batteries · dischargedTHE EMERGENCY EXIT LIGHT ARM AND CHARGE CIRCUIT BREAKER POPPED WITH EMERGENCY EXIT LIGHT SWITCH IN ARM POSITION. THE BATTERIES AT ROW 20 AND 21 OVERHEAD BINS WERE REMOVED AND REPLACED. THE CIRCUIT BREAKER WAS RESET AND THE SWITCH WAS ARMED WITH NO FAULTS NOTSDR CALA9701337Strut · leakingTHE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. THE GEAR HANDLE WOULD ONLY GO HALF WAY UP. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. THIS WAS A REPEAT PROBLEM. MAINTENANCE FOUND THE NOSE STRUT FLAT WITH THE STRUT METERING PIN LEASDR CALA9700579Hyd Pump · shaft wornTHE LEFT ENGINE HYDRAULIC PRESSURE DROPPED TO ZERO SHORTLY AFTER TAKEOFF. THE HYDRAULIC QUANTITY WAS NORMAL. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LT ENGINE DRIVEN HYDRAULIC PUMP HAD FAILED DUE TO A WORN SHSDR CALA9700296Brake · locked upTHE WHEEL NOT TURNING LIGHT ILLUMINATED UPON LANDING, NR 2 MAIN TIRE BLEW. MAINTENANCE FOUND THE NR 2 BRAKE LOCKED UP AND THE QUICK DISCONNECT ON NR 2 BRAKE WAS LOOSE AND LEAKING. THE NR 2 BRAKE, NR 2 WHEEL ASSY, AND QUICK DISCONNECT WERE REPLACED. IN ADDITSDR CALA9601493Prox Switch · dirtyTHE RED NOSE GEAR UNSAFE LIGHT ILLUMINATED INTERMITTENTLY AFTER GEAR WAS RETRACTED. THE GEAR WAS CYCLED, BUT THE LIGHT CONTINUED TO ILLUMINATE INTERMITTENTLY. THE LIGHT EXTINGUISHED AT A SPEED OF 240 KNOTS AND REMAINED OUT. THE FLIGHT WAS CONTINUED TO EWR WSDR CALA9600746Batteries · dischargedINSPECTION FOUND BOTH THE LEFT AND RIGHT FORWARD OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE DURING PRE-DEPARTURE CHECK. TROUBLESHOOTING FOUND THE BATTERIES AT FAULT. THE BATTERIES WERE REPLACED AND OPERATION OF THE OVERWING EMERGENCY EXIT LIGHTS WAS RESTOREDSDR CAL951052Beam · crackedHOU - INSPECTION FOUND A 1 INCH CRACK IN HORIZONTAL BEAM AT MAIN CABIN DOOR UPPER AFT CORNER. THE CRACK WAS STOP DRILLED IAW SRM 52-05, PAGE 189, FIGURE 31. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 52-05, PAGE 189, FIGURE 31, SRM 51-30-2, AND SRSDR CAL950650Fuel Control · inoperativeEWR - FLT 0210 - THE APU AUTO SHUT-DOWN WHILE THE APU GENERATOR WAS POWERING THE LEFT BUS DURING CLIMB THROUGH FL 290. THE APU WAS RESTARTED AFTER DESCENDING TO FL 230. WHILE CLIMBING BACK THROUGH FL 270, THE APU RPM APPROACHED 108 PERCENT WITH FREQUENCY IN ESDR CAL950391Eel Wire · brokenFLT NR 0344 - EWR - INSPECTION FOUND THE EMERGENCY EXIT LIGHT ON THE OUTSIDE WALL OF AFT LEFT LAV INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE AT THE EXIT LIGHT. THE WIRE WAS REMOVED AND REPLACED AND OPERATION OF THE EXIT LIGHT WAS RESTORED. (W)SDR CAL950390Eel Batteries · dischargedFLT NR 0344 - EWR - INSPECTION FOUND THE OVERHEAD EMERGENCY LIGHTS IN AFT CABIN AT ROWS 9-14 AND 23-27 INOPERATIVE. THE BATTERIES FOR THREE BATTERY PACKS WERE REPLACED AND OPERATION OF THE OVERHEAD EMERGENCY LIGHTS WAS RESTORED. (W)SDR CAL950287Eel Batteries · dischargedEWR - FLT 301 - THE OVERHEAD EMERGENCY LIGHTS AT ROW 9 TO 14 WERE FOUND INOPERATIVE DURING A PREFLIGHT CHECK. MAINTENANCE REMOVED AND REPLACED THE BATTERIES AND OPERATION OF THE OVERHEAD EMERGENCY LIGHTS WAS RESTORED. (W)SDR CAL950128O-Ring · rupturedFLT NR 0318 - EWR - THE LEFT HYDRAULIC SYSTEM FLUID QUANTITY BEGAN TO DECREASE WHILE IN FLIGHT. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A RUPTURED O-RING ON THE CAPPED END OF VALVE ASSEMBLY LEADING TO LEFT BRAKE PRESSURE TRANSMITTER. THE O-R
Back to N16884, cancelled Sep 13, 2000