N77204, cancelled Mar 17, 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 = 'N77204' AND deregistration_id = 'N77204-1999-03-17' 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 = 'N77204' AND deregistration_id = 'N77204-1999-03-17' 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 CALA9801859Actuator · inoperativeTHE GEAR HANDLE WAS PLACED IN THE OFF POSITION AFTER TAKEOFF AND THE NOSE GEAR CAME DOWN. THE GEAR HANDLE WAS PLACED UP AND THE NOSE GEAR RAISED. THE GEAR HANDLE WAS THEN PLACED TO OFF AND THE GEAR STAYED UP. THE FLIGHT WAS CONTINUED WITHOUT FURTHER PROBLEMSDR CALA9801589Bulb · failedNO NOSE GEAR INDICATION WAS RECEIVED WHEN GEAR WAS EXTENDED ON APPROACH. A GO-AROUND WAS INITIATED AND THE NOSE GEAR LIGHTS DID NOT TEST. THE NOSE GEAR INDICATOR LIGHT BULBS WERE REPLACED AND TESTED GOOD. GOOD INDICATIONS WERE RECEIVED WITH GEAR EXTENDED ANSDR CALA9801498Hyd Pump · leakingTHE NR 2 ENGINE A-HYD PUMP LOW PRESSURE LIGHT ILLUMINATED AFTER TAKEOFF. THE NR 1 ENGINE A-HYD PUMP LOW PRESSURE LIGHT ILLUMINATED AND THE EMERGENCY CHECKLIST FOR LOSS OF HYD WAS COMPLETED. THE AIRCRAFT WAS RETURNED AND LANDED WITHOUT INCIDENT. MAINTENANCE SDR CALA9801052Socket · corrodedINSPECTION FOUND AFT EXTERIOR EXIT SLIDES INOPERATIVE BOTH SIDES. THE RIGHT EXTERIOR SLIDE LIGHT SOCKET WAS CORRODED. THE SOCKET WAS REPLACED. IN ADDITION, BATTERY PACK M572 WAS REPLACED, OPERATION OF BOTH LIGHTS CHECKED GOOD.SDR CALA9701234Dnlock Actuator · inoperativeTHE LANDING GEAR WAS EXTREMELY STIFF DURING RETRACTION FROM UP TO OFF WITH NO NOTICEABLE DETENT AT OFF. THE NOSE GEAR EXTENDED APPROXIMATELY 12 TO 15 SECONDS AFTER MAINS. MAINTENANCE REMOVED AND REPLACED THE NLG LOCK ACTUATOR IAW MM 32-33-21 PAGE 401. THE GSDR CALA9700608Line · chafedLOST A-SYSTEM HYDRAULICS IN FLIGHT. REPLACED NUMBER 2 ENGINE HYDRAULIC SUPPLY LINE AT RIGHT WING ROOT.SDR CALA9700299Thermo Valve · inoperativeTHE RT PACKED TRIPPED AT 6,000 FEET LEAVING EWR AND SMOKE BEGAN TO ENTER THE CABIN. SHORTLY AFTERWARDS THE BLEED TRIPPED. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. THE 450 DEGREE THERMO VALVE WAS REMOVED AND REPLACED, AN ENGINE BLEESDR CALA9700046Stiffener · crackedINSPECTION FOUND A 2 INCH CRACK IN RT WING VERTICAL STIFFENER AT STRINGER 13R. THE STIFFENER WAS REPAIRED IAW ECRA 5710-01773 AND IN REFERENCE TO BOEING DRAWING 65C34533.SDR CALA9700049Spar · tornINSPECTION FOUND A 3 BY .375 INCH TEAR IN LOWER FLANGE OF LT HORIZONTAL STABILIZER FORWARD LEADING EDGE SPAR. THE TEAR WAS LOCATED THREE FEET FROM OUTBOARD EDGE. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 55-10-5, FIGURE 1.SDR CALA9700047Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 328, BL 0 TO RBL 55. A FLOORBEAM WAS FABRICATED AND INSTALLED IAW SRM 51-10-3.SDR CALA9700050Support · corrodedINSPECTION FOUND CENTER FLOORBEAM SUPPORT CORRODED UNDER PANEL NR 8 BETWEEN STA 312 AND 328. A NEW SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 53-10-2.SDR CALA9700048Skin · crackedINSPECTION FOUND A 2.25 INCH CRACK IN RT FUSELAGE SKIN AT STA 745 BETWEEN STRINGERS 15R AND 16R. THE CRACKED AREA WAS REMOVED AND A DOUBLER WAS INSTALLED IAW SRM 51-30-2.SDR CALA9700051Skin · corrodedINSPECTION FOUND LT WING ROOT LOWER SKIN PANEL CORRODED. THE SKIN WAS REPAIRED IAW ECRA 5730-01471.SDR CALA9601601Hyd Line · brokenTHE A-HYDRAULIC SYSTEM PRESSURE AND QUANTITY DROPPED TO ZERO WHEN GEAR WAS LOWERED ON FINAL APPROACH TO CLE. THE FLAPS WERE LOWERED TO 15 DEGREES ELECTRICALLY AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 4 SLAT ACTUATOR HYDRAULIC LINE BSDR CALA9601136Fireloop · malfunctionedTHE NR 1 ENGINE FIRE WARNING LIGHT AND BELL ACTIVATED DURING CLIMB OUT OF EWR. BOTH FIRE BOTTLES WERE DISCHARGED, THE NR 1 ENGINE WAS SHUTDOWN, AND AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 1 ENGINE BOTTOM FIRE DSDR CALA9600827Hyd Line · chafedTHE A-SYSTEM HYDRAULIC QUANTITY DROPPED TO ZERO WHILE EN ROUTE. THE HYDRAULIC LOSS CHECKLIST WAS COMPLIED WITH AND THE AIRCRAFT WAS DIVERTED TO GSO WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE A-SYSTEM HYDRAULIC SUPPLY LINE IN THE RT REAR SPAR ARESDR CAL950980Actuator · inoperativeFLT NR 1598 - GSO - THE NR 4 SLAT WOULD NOT RETRACT DURING CLIMB-OUT OF GSO, THE AIRCRAFT WAS RETURNED TO GSO. MAINTENANCE FOUND THE NR 4 LEADING EDGE SLAT ACTUATOR AT FAULT. THE ACTUATOR WAS REMOVED AND REPLACED. LEAK AND OPERATIONAL CHECKS WERE GOOD. (MSDR CAL950873Track · crackedEWR - INSPECTION FOUND A .25 INCH CRACK IN LT OUTBOARD TRAILING EDGE FLAP TRACK. THE CRACKED AREA WAS REPAIRED IAW ECRA 5750-02364. (X)SDR CAL950261Intercostal · crackedGSO - INSPECTION FOUND A .50 INCH CRACK IN INTERCOSTAL UPPER FLANGE AT BS 984, LBL 37. THE INTERCOSTAL WAS REMOVED AND REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 53-10-2 AND SRM 51-30-0. (X)SDR CAL950260Angle · crackedGSO - INSPECTION FOUND A .50 INCH CRACK IN FRAME TO STRINGER ATTACH ANGLE AT STR 26R, STA 333. THE CRACKED ANGLE WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, SRM 51-30-2, AND SRM 53-10-3. (X)SDR CAL950259Stringer · crackedGSO - INSPECTION FOUND A 1 INCH CRACK IN STR 28R, LOCATED IN THE FORWARD PIT AT STA 420 - STA 440. THE DAMAGED AREA WAS CUT OUT AND CHANNEL FILLER AND SHIMS WERE INSTALLED IAW SRM 53-10-3, SRM 51-10-2, AND SRM 51-30-2. (X)SDR CAL950258Stringer · corrodedGSO - INSPECTION FOUND CORROSION ON STR 27R AT STA 446. REPAIR ANGLES WERE FABRICATED AND INSTALLED IAW SRM 53-10-3 AND SRM 51-30-2. (X)SDR CAL950257Angle · corrodedGSO - INSPECTION FOUND CORROSION INSIDE WEB OF DOOR SILL ANGLE AND NUT PLATES AT STA 440, STR 25R. A NEW ANGLE WAS INSTALLED IAW SRM 51-10-2 AND SRM 51-1-21A. (X)SDR CAL950256Web · corrodedGSO - NOSE WHEELWELL, LEFT UPPER PANEL WEB, WAS FOUND BULGED AT FORWARD EDGE AND THERE WAS CORROSION ON UPPER SURFACE AND INSIDE FASTENER HOLES. AN INTECOSTAL WAS FABRICATED AND INSTALLED IAW SRM 54-10-3 AND SRM 51-30-2. (X)SDR CAL950255Web · corrodedGSO - THE NOSE WHEELWELL, RT UPPER PANEL WEB, WAS FOUND BULGED AT FORWARD EDGE AND THERE WAS CORROSION INSIDE FASTENER HOLE. AN INTERCOSTAL WAS FABRICATED AND INSTALLED IAW SRM 54-10-3 AND SRM 51-30-2. (X)SDR CAL950254Skin · crackedGSO - INSPECTION FOUND CRACK INDICATIONS IN SKIN AT LEFT FS BS 188-253, WL 208.1 TO WL 234.35. THE CRACKS WERE APPROXIMATELY .50 INCH LONG. THE CRACKED AREAS OF SKIN WERE CUT OUT AND DOUBLERS AND FILLERS WERE INSTALLED IAW EA 5310-01188. (X)
Back to N77204, cancelled Mar 17, 1999