N398CA
Service difficulty reports · 172
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 = 'N398CA' AND registry_match = 'registration' 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 = 'N398CA' AND registry_match = 'registration' 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 REXA2019050400622Doubler · corrodedINITIAL INSPECTION: CORROSION ON INTERNAL DOUBLER IN STA. FS= 295 TO FS= 310 BETWEEN STR 26L TO 26R AT MAIN AVIONICS COMPARTMENT. (E/E)(TCI:53-20-304). INTERNAL DOUBLER IN STA. FS= 295 TO FS= 310 BETWEEN STR 26L TO 26R WAS REPLACED PER SRM 51-42-06-001-001-A01SDR REXA2019050300626Stringer Splice · corrodedINITIAL INSPECTION. CORROSION ON STRINGER SPLICE 25R IN STA. FS= 329 TO FS= 339 AT MAIN AVIONICS COMPARTMENT.(TCI:53-20-305) (E/E).
STRINGER SPLICE 25R IN STA. FS= 329 TO FS= 339 AT MAIN AVIONICS COMPARTMENT WAS REPLACED PER SRM 51-42-06-001-001-A01.SDR REXA2019050100653Floorbeam · corrodedINITIAL INSPECTION : CORROSION ON FLOORBEAM 27LBL BTW FS=1006 TO FS=1041 AT REAR FUSELAGE INTERNAL STRUCTURE (FUS) ( TCI:53-30-310). FLOORBEAM WAS REPAIRED PER SRM 53-00-42-201-001-A01.SDR REXA2019050100641Support Angle · corrodedAWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON PROTECTION PLATE SUPPORT ANGLE IN STA. FS= 322 BETWEEN 41RBL TO 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) CORROSION LEVEL 2. DUE TO NOT ALLOWED ON PROTECTION PLATE SUPPORT ASDR REXA2019050100631Fitting · corrodedINITIAL INSPECTION. CORROSION ON CLIPS FS 310 AND 349 STRG 20R AT MAIN AVIONICS COMPARTMENT. (E/E)(SM)(TCI :53-20-304).
CORROSION ON CLIPS FS 310 AND 349 STR 20R AT MAIN AVIONICS COMPARTMENT. CLIP ON FS 310 WAS CLEANED PER. SRM. 51-26-00-001-001-A01. AND CLISDR REXA2019043000649Angle · corrodedAWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON SUPPORT MOUNTING ANGLE IN STA. FS= 319 TO FS= 349 AND 41RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) SUPPORT MOUNTING ANGLE BTW FS319/349 AND 41RBL AT GALLEY SERVICE DOOR LOWER SSDR REXA2019043000646Support · corrodedAWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON PROTECTION PLATE SUPPORT IN STA. FS= 329 BETWEEN 41RBL TO 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) SUMMARY OF NRC S/N 00296: CORROSION LEVEL 2. DUE TO NOT DAMAGE ALLOWED ONSDR REXA2019043000644Support Angle · corrodedAWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON PROTECTION PLATE SUPPORTS ANGLE IN STA. FS= 346 BETWEEN 41RBL TO 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) CORROSION LEVEL 2. DUE TO NOT ALLOWED ON PROTECTION PLATE SUPPORT SDR REXA2019042800648Support · corrodedSUPPLEMENTAL INFORMATION (CORRECTING BUTT LINE LOCATION) - (AWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON PROTECTION PLATE SUPPORT IN STA. FS= 346 BETWEEN 41RBL TO 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX)
SUMMARY OF NSDR REXA2019042800645Support · corrodedAWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON PROTECTION PLATE SUPPORT IN STA. FS= 322 BETWEEN 41RBL TO 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) SUMMARY OF NRC 00295: CORROSION LEVEL 2. DUE TO NOT DAMAGE ALLOWED ON PROSDR REXA2019042800647Support · corrodedAWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON PROTECTION PLATE SUPPORT IN STA. FS= 339 BETWEEN 41RBL TO 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX)SUMMARY OF NRC 00297: CORROSION LEVEL 2. DUE TO NOT DAMAGE ALLOWED ON PROTSDR REXA2019042800643Support Angle · corrodedAWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON PROTECTION PLATE SUPPORT ANGLE IN STA. FS= 339 BETWEEN 41RBL TO 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) SUMMARY OF NRC 00293: CORROSION LEVEL 2. DUE TO NOT ALLOWED ON PROTSDR REXA2019042800642Support Angle · corrodedAWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON PROTECTION PLATE SUPPORT ANGLE IN STA. FS= 329 BETWEEN 41RBL TO 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) SUMMARY OF NRC 00292: CORROSION LEVEL 2. DUE TO NOT ALLOWED ON PROTSDR REXA2019042600639Seat Track · corrodedCORROSION ON SIDE SEAT RAIL STRUCTURE (LT/R) FROM FS953+8 TO FS985+2 AT PAX CABIN (TCI: 53-20-356) NEW SIDE SEAT RAIL STRUCTURE (LT/RT) FROM FS953+8 TO FS985+2 WERE REPLACED PER AMM 53-00-49-400-801 (CONFIG. A17). LEVEL CORROSION 2.SDR REXA2019042600638Seat Track · corrodedINITIAL INSPECTION: CORROSION ON SIDE SEAT RAIL STRUCTURE (LH/RH) FROM FS708+4 TO FS761.85, FS785.15 TO FS 847+6, FS847+6 TO FS863+5 AND FS863+5 TO FS 953+8 AT PAX CABIN (TCI: 53-20-318) SIDE SEAT RAIL STRUCTURE (LH/RH) FROM FS708+4 TO FS761.85, FS785.15 TO SDR REXA2019042600637Seat Track · corrodedINITIAL INSPECTION: CORROSION ON SIDE SEAT RAIL STRUCTURE (LH/RH) FROM FS379 TO FS485, FS485 TO FS 565+8, FS565 TO FS677 AND FS677 TO FS 708+3 AT PAX CABIN (TCI: 53-20-245) SIDE SEAT RAIL STRUCTURE (LH/RH) FROM FS379 TO FS485, FS485 TO FS 565+8, FS565 TO FS6SDR REXA2019042600635Seat Track · corrodedINITIAL INSPECTION: CORROSION ON SEAT TRACK RAILS BTW FS677+3 / FS830.40+3 AND LBL9.00 SIDE ABOVE FLOOR (TCI: 53-20-245)
SEAT TRACK RAILS BTW FS677+3 / FS830.40+3 AND LBL9.00 WAS REPLACED PER AMM 53-00-49-400-801 (CONFIG A03)SDR REXA2019042600633Seat Track · corrodedINITIAL INSPECTION: CORROSION ON SEAT TRACK RAILS BTW FS485 / FS581 AND RBL9.00 / LBL9.00 SIDE ABOVE FLOOR (TCI: 53-20-245)
SEAT TRACK RAILS BTW FS485 / FS581 AND RBL9.00 / LBL9.00 WERE REPLACED PER AMM 53-00-49-400-801 (CONFIG A03)SDR REXA2019042500640Doubler · chafedINITIAL INSPECTION: CHAFING ON PREVIOUS REPAIR DOUBLER, TRIPLER AND TAPER SHIMS IN FS=968 TO FS=985 AT FUSELAGE SKIN.(FUS)(SM)(TCI 53-20-252). REPAIR DOUBLER, TRIPLER AND TAPER SHIMS IN FS=968 TO FS=985 AT FUSELAGE SKIN WERE REPLACED PER REO 670-53-00-290 SDR REXA2019042500636Seat Track · corrodedINITIAL INSPECTION: CORROSION ON SEAT TRACK RAILS BTW FS349 / FS485 AND RBL9.00 SIDE ABOVE FLOOR (TCI: 53-20-243) SEAT TRACK RAILS BTW FS349 / FS485 AND RBL9.00 WAS REPLACED PER AMM 53-00-49-400-801 (CONFIG A03)SDR REXA2019042400630Stringer · corrodedINITIAL INSPECTION: CORROSION ON STRINGER 21RH IN STA. FS= 280 TO FS= 364 AT MAIN AVIONICS COMPARTMENT. (E/E)(TCI:53-20-304)
STRINGER 21R IN SECTION STA. FS= 280 TO FS=333 WAS CLEANED PER SRM. 51-26-00-001-001-A01 AND DAMAGE NO FOUND, STRINGER 21R AND SPLICESDR REXA2018091000816Oxygen Bottle · leakingCREW O2 SYSTEM LOSING 10PSI PRESURE EVERY 5-10 MINUTES. REMOVE AND REPLACED CREW O2 BOTTLE IAW AMM 35-11-03.SDR REXA2018082410712Oxygen Mask · leakingFIRST OFFICER`S OXYGEN MASK FOUND TO BE LEAKING AFTER SERVICING. REMOVED AND REPLACED THE OXYGEN MASK IAW AMM 35-11-12. OPS TESTED GOOD, NO LEAKS DETECTED, NO DEFECTS DETECTED.SDR REXA2018081000681Cylinder · low pressurePORTABLE OXYGEN CYLINDER PRESSURE 1500, REMOVED & REPLACED THE CYLINDER IAW AMM 35-31-01-00-801.SDR ASOA201706071661Stiffener · crackedFS 202.75 FWD SIDE OF BULKHEAD AT RBL 30 HAS INDICATION NOTED AT TOP OF I BEAM INTERSECTION .150" LONG. FAILED NDT INSPECTION. REPAIRED RBL 30 I BEAM IAW SRM 53-11-10-201-005-A01.SDR ASOA201706061650Frame · crackedRT FS 235 FRAME HAS ONE INDICATION NOTED NEAR I/B RADIUS AT STR 13A .300" LONG FAILED NDT. REMOVED UNSERVICEABLE RT FS 235 FRAME P/N CC670-34133-4 AND INSTALLED A SERVICEABLE RT FS 235 FRAME P/N CC670-34133-10 IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01SDR ASOA201705241660Seat Track · corrodedRT SEAT TRACK AT RBL 9 FS687 TO FS840 IS CORRODED. COMPLIED WITH EC/TC REO 670-53-00-343 REV K AND REO 670-53-00-343 REV K.SDR ASOA201705241659Seat Track · corrodedLT SEAT TRACK AT LBL 9 FS687 TO FS840 IS CORRODED. COMPLIED WITH EC/TC REO 670-53-00-343 REV K AND REO 670-53-00-343 REV K.SDR ASOA201612015091Connector · unsecureDURING SCHEDULED MAINTENANCE, THE OVERHEAD ISLE EMERGENCY LIGHT AT ROW 9 WAS FOUND INOPERATIVE. MX SECURED THE CONNECTOR J358 AND PERFORMED OPS CHECK WITH SATISFACTORY RESULTS. ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA2016081115239Engine · failedAFTER TAKE OFF, ACFT BEGAN TO SHAKE, RT ENGINE VIBRATION CAUTION UP TO 6.8. AND ITT WENT RED. SHUT RT ENGINE DOWN AND RETURNED TO DEPARTURE. REMOVED AND REPLACED THE RT ENGINE IAW AMM 71-00-00. INSTALLED RT ENGINE IDG IAW AMM 24-11-01.SDR ASOA2015112414126Bulb · burned outGALLEY FORWARD LOWER EXIT SIGNS HAD ONE BULB BURNED. R & R BURNED BULBS AS REQUIRED. OPS CHECK GOOD IAW AMM 33-51-00.SDR ASOA2015112414128Bulb · burned outMAIN ENTRANCE LOWER EXIT SIGN HAD TWO LIGHT BULBS BURNED OUT. R & R BURNED OUT BULBS AS REQURIED. OPS CHECK GOOD IAW AMM 33-51-00.SDR ASOA2015112414127Bulb · burned outGALLEY AFT LOWER EXIT SIGN HAVE 1 BULB BURNED OUT. R & R BURNED OUT BULBS AS REQURIED. OPS CHECK GOOD IAW AMM 33-51-00.SDR ASOA2015112414125Bulb · burned out12 CD LOWER EXIT SIGN ONE BULB BURNED OUT. R & R BURNED OUT BULBS AS REQURIED. OPS CHECK GOOD IAW AMM 33-51-00.SDR ASOA2015101213887Warning Light · illuminatedELECTRICAL ODOR NOTED AFTER REV D, A STBY PITOT HEAT CAUTION MESSAGE AND A TAT PROBE CAUTION. ENROUTE, ACFT DIVERTED DUE TO MAINTENANCE. EMERGENCY DECLARED AS A PRECAUTION. R & R ABO ADSHC IAW AMM 30-31-15, IPC 30-31-15, PG 0, FIG 1, ITEM 5. OPS TEST GOOD,SDR ASOA2015072413382Lens · damagedPAX DOOR EXIT SIGN LENS DARKENED WHEN RECEIVED. REMOVED AND INSTALLED NEW PAX DOOR EXIT SIGN LENS IAW AMM 33-51-05-000-801-A01 AND 33-51-05-400-801-A01.SDR ASOA2015072413381Lens · damagedSERVICE DOOR EMERGENCY LIGHT LENS DAMAGED. REMOVED SERVICE DOOR EMERGENCY LIGHT LENS IAW AMM 33-51-05-000-801A-01. INSTALLED SERVICEBALE EMERGENCY LIGHT LENS IAW AMM 33-51-05-400-801-A01.SDR ASOA2015072413380Intercostal · corrodedDISCOVERED INTERCOSTAL AT STR 27L BETWEN FS 265 TO FS 280 IS CORRODED. EVALUATED DAMAGE AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00-101-A01. REMOVED INTERCOSTAL AT LT SIDE OF STR 27 BETWEEN FS 265-280 IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.SDR ASOA2015072413379Skin · corrodedFUSELAGE SKIN CORRODED UNDERNEATH THE BOTTOM ADF ANTENNA. NO DAMAGE ALLOWED ON SKIN UNDERNEATH ADR ANTENNA IAW SRM 53-31-01-101-003-A01. COMPLIED WITH EA 32-2015-281, REV A. COMPLIED WITH EA 32-2015-281.SDR ASOA2015071713369Doubler · corrodedTCAS DOUBLER CORRODED AT FS 295-310 BETWEEN STRINGERS 26L AND 26R. REMOVED TCAS DOUBLER IAW SRM 51-42-06-001-001-A01. LOCATED AND DRILLED NEW TCAS DOUBLER IAW SRM 51-40-11-001-001-A01. INSTALLED NEW TCAS DOUBLER IAW SRM 51-42-06-001-001-A01 AND FINISHED RIVSDR ASOA2015072413378Frame · corrodedFS 565, FRAME HAS CORROSION BETWEEN STRINGERS 18 - 19L. EVALUATED FRAME AND FOUND IT TO BE EXTREMELY EXFOILATED, NO ALLOWABLE DAMAGE IS PERMITTED IN THIS AREA. RECEIVED AND COMPLIED WITH REO 670-53-31-345, REV-- (P1), DATED 2015-07-03. RECEIVED AND COMPLIEDSDR ASOA2015072413377Shear Tie · corrodedFS 565 FRAME ATTACH ANGLE BETWEEN STRINGERSS 18 - 19L HAS CORROSION. COMPLIED WITH REO 670-53-31-345 AND ECTC REO 670-53-31-345.SDR ASOA2015071713368Frame · corrodedBS 549, FRAME HAS CORROSION BETWEEN STRINGERS 18 AND 19L. REMOVED THE CORROSION IAW SRM 51-21-06-001-001-A01.SDR ASOA2015071513362Angle · corrodedFS 549 FRAME ANGLE CORRODED BETWEEN STR 18-19L . REMOVED CORROSION FROM ANGLE IAW SRM 51-21-06-001-001-A01. BLENDED AREA WAS FOUND TO BE WITHIN LIMITS ON SRM 53-31-23-101-001-A01. UPON FURTHER EVALUATION FOUND ADDITIONAL CORROSION ON ANGLE. REMOVED FASTENESDR ASOA2015071513361Seat Track · corrodedRBL 9 SEAT TRACK CORROSION BS 485-581. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801, CONFIG A03. AND INSTALLED A NEW SEAL TRACK IAW AMM 53-00-49-400-801, CONFIG A03.SDR ASOA2015071513360Seat Track · corrodedLBL 9 SEAT TRACK HAS CORROSION ON BS 581- 677, LBL 9, FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-13. R & R SEAT TRACK IAW AMM 53-00-49-000-801-A03 AND 53-00-49-400-801-A03.SDR ASOA2015071513359Seat Track · corrodedLBL 9 SEAT TRACK HAS CORROSION ON BS 485-581 SEGMENT. CORRODED BEYOND LIMITS. R & R SEAT TRACK IAW AMM 53-00-49-000-801-A03 AND AMM 53-00-49-400-801-A03.SDR ASOA2015071713367Plate · corrodedRT OVERWING EMERGENCY EXIT STEP PLATE CORRODED. REMOVED RT O/W EXIT STEP PLATE BY REMOVING 8 SCREWS AND LIFTING PLATE. INSTALLED RT EMERGENCY EXIT STEP RATE BY INSTALLING 8 SCREWS IAW SRM 51-41-02-001-001-A01. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01SDR ASOA2015071513358Door Frame · corrodedLEFT DOOR POST CORRODED AT BS 280 CROSSBEAM. REMOVED CORROSION ON LT DOOR POST AT 280 CROSSBEAM AREA IAW SRM 51-21-06-001-001-A01. COMPLIED WITH STS EA 25-2015-195. COMPLIED WITH EA 25-2015-197.SDR ASOA2015071513357Door Frame · corrodedRIGHT DOOR POST CORRODED AT BS 280 CROSSBEAM. REMOVED CORROSION ON RT DOOR POST AT 280 CROSSBEAM AREA IAW SRM 51-21-06-001-001-A01. COMPLIED WITH STS EA 25-2015-195. COMPLIED WITH EA 25-2015-195.
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