N809NY, cancelled Nov 26, 2002
Service difficulty reports · 56
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 = 'N809NY' AND deregistration_id = 'N809NY-2002-11-26' 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 = 'N809NY' AND deregistration_id = 'N809NY-2002-11-26' 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 CALA0001979Cargo Track · gougedINSPECTION FOUND GOUGES IN MID PIT RT AFT CARGO TRACK AT FS 693-788. THE TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-30-1.SDR CALA0001977Structure · crackedINSPECTION FOUND TORQUE BOX WEB CRACKED AT FS 200-208, LBL 54 (AFT OF L-1 DOOR). THE TORQUE BOX WEB WAS REMOVED AND REPLACED IAW SRM 51-30-1.SDR CALA0001976Angle · corrodedINSPECTION FOUND RT Z-ANGLE THAT MOUNTS TO CARGO TRACK CORRODED AT FS 693-733. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-1 AND 51-10-4.SDR CALA0001969Web · crackedINSPECTION FOUND A 2 INCH CRACK AT LIGHTENING HOLE OF AFT CARGO TORQUE BOX WEB, FS 1211, L27R. THE WEB, ATTACHING STRAPS, AND L-ANGLE SUPPORT WERE REMOVED AND A NEW WEB WAS INSTALLED USING ATTACHMENT PARTS IAW SRM 51-30-2 AND 51-30-5.SDR CALA0001964Support · crackedINSPECTION FOUND AFT CARGO FLOORBOARD SUPPORT IN CARGO DOOR AREA CRACKED AT FS 1136-1220. THE SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-1, 51-30-2, AND 51-30-5.SDR CALA0001956Angle · corrodedINSPECTION FOUND L-1 DOOR JAMB CUSP ANGLE CORRODED AT FS 200, LBL 54. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2, 51-30-5, ECRA 5310-04082, AND EA 9-5310-2-A809.SDR CALA0001955Angle · crackedINSPECTION FOUND A 2 INCH CRACK IN L-1 DOOR FORWARD LOWER CORNER ANGLE. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-10-4, 51-10-3, AND 51-30-8.SDR CALA0001954Skin · dentedINSPECTION FOUND EXTERIOR SKIN OF MID CARGO DOOR DENTED IN TWO PLACES. THE DENTED AREAS WERE CUT OUT AND DOUBLER AND FILLER REPAIRS WERE INSTALLED IAW SRM 52-05, FIGURE 3, 51-10-3, AND ECRA 5230-01207.SDR CALA0001953Cargo Track · corrodedINSPECTION FOUND RT FORWARD CARGO TIE DOWN TRACK CORRODED AT STA 218-370. THE TIE DOWN TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-30-1 AND 51-10-4.SDR CALA0001952Floor Support · corrodedINSPECTION FOUND FLOOR SUPPORT I/B OF DOOR SCUFF PLATE AT AFT SERVICE DOOR CORRODED. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 53-14-3, FIGURE 12 AND 51-30-02.SDR CALA0001951Rib · corrodedINSPECTION FOUND FASTENER HOLES CORRODED IN MID PIT FORWARD BULKHEAD SUPPORT RIBS. THE SUPPORT RIBS(2) WERE REMOVED AND TWO NEW SUPPORT RIBS WERE INSTALLED IAW SRM 51-10-4, 51-10-3, AND 51-30-2.SDR CALA0001950Stop · wornINSPECTION FOUND MID CARGO DOOR STOP PADS NR 2, 5, & 6 CHAFED/WORN. THE WORN AREAS WERE REMOVED AND A REPAIR DOUBLER WAS INSTALLED AT EACH LOCATION IAW SRM 51-10-3 AND ECRA 5330-02819.SDR CALA0001941Floor Support · corrodedINSPECTION FOUND FORWARD ENTRY SUBFLOOR CORRODED AT FS 148, RBL 6 AND AT FS 160-170, RBL 9. A REPAIR DOUBLER WAS INSTALLED AT EACH LOCATION IAW SRM 53-01, FIGURE 4 AND 51-10-3.SDR CALA0001940Seat Track · corrodedINSPECTION FOUND CABIN LT I/B SEAT TRACK CORRODED AT FS 896. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-1 AND 51-30-5.SDR CALA0001939Intercostal · corrodedINSPECTION FOUND INTERCOSTAL CORRODED AT FS 1022-1041. THE INTERCOSTAL WAS REMOVED AND A NEW INTERCOSTAL WAS INSTALLED IAW SRM 51-10-4, 51-10-3, AND 51-10-5.SDR CALA0001937Seat Track · corrodedINSPECTION FOUND CABIN RT SEAT TRACK CORRODED AT FS 265-790. THE SEAT TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-30-2, 53-04, FIGURE 4F, AND 53-05, FIGURE 4B.SDR CALA0001936Web · crackedINSPECTION FOUND 1 INCH CRACKS IN LT CUSP WEBS AT STA 1032, 1231, AND 1260. DOUBLERS WERE INSTALLED AT EACH CRACK LOCATION IAW SRM 53-01, FIGURE 2 AND 51-30-2.SDR CALA0001935Cargo Track · corrodedINSPECTION FOUND LT CARGO TRACK IN MID PIT CORRODED ON UPPER AND LOWER SURFACES BETWEEN STA 541 AND 788. THE TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-30-2, 51-30-5, AND 51-30-1.SDR CALA0001934Floor Support · corrodedINSPECTION FOUND FORWARD ENTRY SUBFLOOR AND FLOOR SUPPORT CORRODED AT FS 160-200, LBL 54. THE SUBFLOOR AND FLOOR SUPPORT WERE REMOVED AND A REPAIR WAS INSTALLED IAW SRM 51-30-1, 51-10-4, AND 53-14-1, FIGURE 11.SDR CALA0001933Seat Track · corrodedINSPECTION FOUND LT O/B SEAT TRACK CORRODED AT STA 256. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-05, FIGURE 4F.SDR CALA0001929Web · corrodedINSPECTION FOUND CUSP WEB CORRODED AT FS 200-237, LBL 56. THE CUSP WEB WAS REMOVED AND A NEW CUSP WEB WAS INSTALLED IAW SRM 51-30-2, 51-30-5, AND 53-14-1, FIGURE 11.SDR CALA0001925Fitting · corrodedINSPECTION FOUND NR 1 GALLEY SUPPORT FITTINGS (TWO EACH) CORRODED IN FASTENER HOLES AT STA 160, RBL 44 AND RBL 50. THE FITTINGS WERE REMOVED AND NEW FITTINGS WERE INSTALLED IAW SRM 51-30-5, 51-10-4, AND 51-10-3.SDR CALA0001924Door Frame · brokenINSPECTION FOUND A 2 INCH PIECE BROKEN OUT OF AFT CARGO DOOR FRAME CUTOUT AT AFT UPPER EDGE, BS 1211, LONGERON 21R. THE FRAME CUTOUT WAS REMOVED AND REPLACED IAW SRM 51-30-5.SDR CALA0001920Floor Support · corrodedINSPECTION FOUND FORWARD ENTRY FLOOR SUPPORT CORRODED AT FS 140-150, RBL 54. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-5, 51-30-2, AND 51-30-4.SDR CALA0001919Doubler · chafedINSPECTION FOUND DOUBLER AT FORWARD LOWER CORNER OF FORWARD CARGO DOOR CHAFED. THE DOUBLER WAS REMOVED AND A NEW DOUBLER WAS INSTALLED IAW SRM 51-10-4, 51-30-2, AND 51-10-3.SDR CALA0001915Web · corrodedINSPECTION FOUND FORWARD ENTRY CUSP WEB CORRODED AT FS 200-205, RBL 49-54 ON AFT SIDE OF FLOORBEAM. THE CORRODED SECTION OF CUSP WEB WAS CUT OUT AND A REPAIR DOUBLER AND FILLER WERE INSTALLED IAW SRM 51-10-3, 51-30-2, AND 51-30-8.SDR CALA0001914Seat Track · corrodedINSPECTION FOUND LT O/B SEAT TRACKS CORRODED AT FS 807-1136 AND AT STA 1136-1309. THE SEAT TRACKS WERE REMOVED AND NEW TRACKS WERE INSTALLED IAW SRM 51-10-4, 51-10-3, 51-30-1, 51-30-2, AND 51-10-2.SDR CALA0001913Seat Track · corrodedINSPECTION FOUND LT CENTER SEAT TRACK CORRODED AT FS 1032-1309. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED USING A SPLICE REPAIR IAW SRM 51-30-1, 51-10-4, 53-05, FIGURE 4, 51-30-5, AND 51-30-2.SDR CALA0001912Cargo Track · corrodedINSPECTION FOUND FORWARD CARGO LT TIE DOWN TRACK CORRODED BETWEEN FS 218 AND 522. THE TIE DOWN TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-30-1 AND 51-30-2.SDR CALA0001909Skin · dentedINSPECTION FOUND AFT FUSELAGE LT LOWER SKIN DENTED AT STA 1322, LONGERON 27L-28L. A DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38, 51-10-4, AND 51-10-3.SDR CALA0001908Fitting · corrodedINSPECTION FOUND NR 1 GALLEY SUPPORT MOUNT FITTING CORRODED AT STA 160, RBL 12. THE GALLEY SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-5.SDR CALA0001907Doubler · chafedINSPECTION FOUND FORWARD LOWER CORNER OF MID CARGO DOOR CHAFED. THE REPAIR DOUBLER WAS REMOVED AND A NEW DOUBLER WAS INSTALLED IAW SRM 51-10-4 AND 51-30-2.SDR CALA0001901Floorbeam · corrodedINSPECTION FOUND TOP OF FLOORBEAM CORRODED AROUND NUTPLATE HOLES IN R/H AFT LAV AT FS 1322, RBL 17 TO RBL 53. A REPAIR ANGLE WAS INSTALLED IAW SRM 53-05, FIGURE 20A AND 51-30-05.SDR CALA0001900Web · corrodedINSPECTION FOUND LT CUSP WEB CORRODED AT FS 1140 (L-2 DOOR). THE CUSP WEB WAS REMOVED AND A DOUBLER AND FILLER WERE INSTALLED IAW SRM 51-10-4, 53-14-3, AND 51-30-2.SDR CALA0001893Seat Track · corrodedINSPECTION FOUND CABIN RT CENTER SEAT TRACK CORRODED AT STA 225. THE SEAT TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-30-1, 53-05, FIGURE 4F, AND 51-30-5.SDR CALA0001892Skin · dentedINSPECTION FOUND FUSELAGE SKIN DENTED AT STA 294 BETWEEN LONGERON 24 AND 25L AND AT STA 225, L16L. A DOUBLER WAS INSTALLED AT EACH LOCATION IAW SRM 53-04, FIGURE 38, 51-10-3, AND 51-30-02.SDR CALA0001881Floor Support · corrodedINSPECTION FOUND FORWARD ENTRY SUB FLOOR AND ATTACHING STRUCTURE CORRODED AT FS 160-200, RBL 54. TORQUE BOX STRAP, SUB FLOOR ATTACH ANGLES, AND DOUBLER WERE REMOVED IAW SRM 51-30-5 AND 51-30-2. DOUBLERS WERE INSTALLED IAW SRM 51-30-2 AND 51-30-5.SDR CALA0001873Skin · dentedINSPECTION FOUND FUSELAGE SKIN DENTED AT STA 270, LONGERON 17L. A DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38, SHEET 21 AND 51-30-0.SDR CALA0001869Skin · dentedINSPECTION FOUND RT FUSELAGE SKIN DENTED AT STA 237-256. A DOUBLER AND FILLER WERE INSTALLED IAW SRM 53-04, FIGURE 38 AND 53-04.SDR CALA9900215Sensor · inopTHE NOSE GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION LEAVING IAH. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NOSE GEAR DOWNLOCK PROXIMITY SENSOR AT FAULT. THE NOSE GEAR DOWNLOCK PROXIMITY SENSORSDR CALA9801968Cable · out of adjTHE AFT ENTRY DOOR TAILCONE RELEASE PULLED HIGH AT 25 POUNDS. THE CABLE AND CONDUIT WERE REPLACED AND AN ADJUSTMENT/TEST WAS PERFORMED IAW MM 53-53-00.SDR CALA9801967Longeron · corrodedINSPECTION FOUND LONGERON 24L CORRODED IN AFT CARGO COMPARTMENT AT STA 1231. REPAIRED IAW SRM 53-02, FIGURE 18.SDR CALA9801966Beam · crackedINSPECTION FOUND A CRACK IN FORWARD SERVICE DOOR LOWER BEAM. THE LOWER BEAM WAS REPLACED IAW SRM 51-30-2.SDR CALA9801958Doubler · corrodedCORROSION IN AFT BAG BIN AT STA 1309 JUST ABOVE LONGERON 23 LEFT SIDE. REMOVED AND REPLACED DOUBLER PER 51-30-02.SDR CALA9801950Jamb · corrodedMBB DOOR JAMB BEAM CORRODED. REMOVED AND REPLACED BEAM PER SRM 51-30-02 AND 51-30-05.SDR CALA9800686Strut · flatTHE NLG WOULD NOT RETRACT AFTER TAKEOFF. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NLG STRUT FLAT. A NEW GLAND NUT WAS INSTALLED AND THE STRUT WAS REPACKED.SDR CALA9800578Support · crackedINSPECTION FOUND A .375 INCH CRACK AT LOWER RIVET HOLE IN FORWARD LEFT VERTICAL STABILIZER SPAR SUPPORT AT 37.3 INCHES AFT OF STA 1089.3 IN TAIL COMPARTMENT ABOVE CATWALK. THE AREA WAS REPAIRED IAW SRM 55-02, FIGURE 26.SDR CALA9701236Oil Screen Cover · leakingTHE NR 1 ENGINE OIL QUANTITY DROPPED TO ZERO FOLLOWED BY OIL PRESSURE DECREASING TO 10 PSI AFTER TAKEOFF. THE AIRCRAFT WAS RETURNED TO LAX WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND PLUG ON MAIN OIL SCREEN COVER LEAKING. A NEW OIL SCREEN COVER ASSESDR CALA9700663Fan · inoperativeLIGHT SMOKE WAS REPORTED IN CABIN WHILE EN ROUTE TO SEA. THE RECIRCULATION FAN CIRCUIT BREAKER WAS PULLED AND THE SMOKE CLEARED. THE AIRCRAFT LANDED AT SEA WITHOUT FURTHER PROBLEM. MAINTENANCE FOUND THE AIR DISTRIBUTION FAN AT FAULT. THE FAN WAS REMOVED ANSDR CALA9601473Support Leg · crackedFOUND OUTBOARD SUPPORT BRACKET OF LEFT HAND GROUND SPOILER UPPER AFT LEG WITH ONE INCH CRACK IN SUPPORT LEG. REPLACED CROSS BRACE PER EC/RA 5710-01756.
Back to N809NY, cancelled Nov 26, 2002