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 REXA2026083101752Bulb · inoperative1 SERVICE DOOR FLOOD LAMP BULB INOP. R & R EMERGENCY FLOOD LIGHT BULB P/N OL3071BPE/GPL REF AMM 33-51-05. OPS CHECK GOOD.SDR REXA2026042700362Door · bindingSERVICE DOOR HARD TO OPEN FROM INSIDE EVEN HARDER FROM OUTSIDE. FOUND CHAFE DAMAGE ON BACKSIDE OF ALIGNMENT MARK HOUSING. COMPLYED WITH EA CRJ752-22072.OPS TEST GOOD SEE NRWC #938126 FOR DETAILSSDR REXA2026042700361Fitting · faultedPASSENGER DOOR HARD TO OPEN FROM OUTSIDE. ADJUSTED HANDRAILS PER AMM 52-11-05. ADJUSTED AFT SPIGOT PER AMM 53-21-23, REPLACED ROD BEARING PER FIM 52-11-00, ADJUSTED PAX DOOR OUTER HANDLE PER AMM 52-11-03. R/R AFT CAM FITTING PER SRM 51-42-21. ADJUSTED COUNTESDR REXA2026080301386Fitting · damagedBUSHINGS IN AILERON LH, OVERSIZED WAS FOUND ON INBD LUG BORE TO WING TRAILING EDGE AILERON HINGE FITTING #1 AT WS294.50, LHS FOR OVERSIZED LUG BORE TO WING TRAILING EDGE AILERON HINGE FITTING #1 ASSEMBLY AT WS294.50, LHS WAS REPAIRED PER REO 670-57-51-697 REV SDR REXA2026080301388Beam · corrodedSEVERAL CORROSION ON BEAM RBL 9.00 BTW FS477.40 TO FS830.00 WERE FOUND. BEAM RBL 9.00 BTW FS 477.40 TO FS 830.00 WAS REPAIRED PER REP 670-53-41-827 REV --SDR REXA2026080301415Strap · corrodedSECONDARY NRC FROM NRC:00305: AFTER REMOVAL OF CHANNELS, CORROSION ON STRAP AT PANNEL NRB 195DL. STRAP OF PANEL NR 195DL WAS FABRICATED PER EA NO: CRJ753-21742 REV. IRSDR REXA2026080301394Fitting · corrodedCORROSION ON MACHINED FITTING LOCATED ON FS847 BETWEEN STRG 25L TO STRG 25R (INTERNAL FUSELAGE). MACHINED FITTING LOCATED ON FS847 BETWEEN STRG 25L TO STRG 25R (INTERNAL FUSELAGE) WERE REPAIRED PER REO 670-53-41-834 REV --SDR REXA2026080301393Fitting · corrodedCORROSION ON MACHINED FITTING LOCATED ON FS847 BETWEEN STRG 25L TO STRG 25R (INTERNAL FUSELAGE). MACHINED FITTING LOCATED ON FS847 BETWEEN STRG 25L TO STRG 25R (INTERNAL FUSELAGE) WERE REPAIRED PER REO 670-53-41-834 REV --SDR REXA2026080301407Beam · corrodedSEVERAL CORROSION ON BEAM LBL 9.00 BTW FS477.40 TO FS830.00 WERE FOUND BEAM LBL 9.00 BTW FS477.40 TO FS 830.00 WAS REPAIRED PER REO 670-53-41-833 REV --, REO 670-55-41-835 REV --,REO 670-53-31-1169 REV -- AND EA CRJ753-21644 REV IRSDR REXA2026080301392Fitting · corrodedCORROSION ON STGR 22L, FROM FS 389 TO FS 409, AT MAIN AVIONICS COMPARTMENT. STGR 22L, FROM FS 389 TO FS 409, AT MAIN AVIONICS COMPARTMENT WAS REPAIRED PER CRJ-700 SRM 53-00-03-201-001-A01.SDR REXA2026080301391Fitting · corrodedCORROSION ON STGR 22L, FROM FS 389 TO FS 409, AT MAIN AVIONICS COMPARTMENT. STGR 22L, FROM FS 389 TO FS 409, AT MAIN AVIONICS COMPARTMENT WAS REPAIRED PER CRJ-700 SRM 53-00-03-201-001-A01.SDR REXA2026080301406Strap · corrodedINITIAL INSPECTION: CORROSION ON JOINT STRAP, SETTLEMENT Ï¿½REA OF FAIRING ACCESS PANEL 194AB & 193AB JOINT STRAP (FRAME ASSY) SETTLEMENT AREA OF FAIRING ACCESS PANEL 194AB & 193AB WAS REPAIRED PER REO 670-53-82-733. REV. --SDR REXA2026080301390Floorbeam · crackedCRACKED CENTER COCKPIT FLOOR BEAM RBL 12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT CENTER COCKPIT FLOOR BEAM RBL 12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT WAS REPAIRED PER REO 670-53-11-2278REV. --SDR REXA2026080301385Rib · crackedCRACK ON MACHINED RIB OF LEADING EDGE SS57.16 AT RH WING CRACK ON MACHINED RIB OF LEADING EDGE SS57.16 AT RH WING WAS REPAIRED PER REO 670-57-41-681 REV - -.SDR REXA2026080301414Track · corrodedCORROSION ON RAILS ON FWD CARGO COMPARTMENT 10E/AÏ¿½S RAILS (2EAS P/N: DSY7058-5) WERE REPLACED AND VERIFIED PER CRJ-700 IPC: 52-51-02-01 ITEM: 250, RAILS (2EAS P/N: DSY7058-3) WERE FABRICATED PER CRJ-700 EA NO.CRJ725-21615 REV. IR., RAILS (2EAS P/N: DSY7058-SDR REXA2026080301413Track · corrodedCORROSION ON RAILS ON FWD CARGO COMPARTMENT 10E/AÏ¿½S RAILS (2EAS P/N: DSY7058-5) WERE REPLACED AND VERIFIED PER CRJ-700 IPC: 52-51-02-01 ITEM: 250, RAILS (2EAS P/N: DSY7058-3) WERE FABRICATED PER CRJ-700 EA NO.CRJ725-21615 REV. IR., RAILS (2EAS P/N: DSY7058-SDR REXA2026080301412Track · corrodedCORROSION ON RAILS ON FWD CARGO COMPARTMENT 10E/AÏ¿½S RAILS (2EAS P/N: DSY7058-5) WERE REPLACED AND VERIFIED PER CRJ-700 IPC: 52-51-02-01 ITEM: 250, RAILS (2EAS P/N: DSY7058-3) WERE FABRICATED PER CRJ-700 EA NO.CRJ725-21615 REV. IR., RAILS (2EAS P/N: DSY7058-SDR REXA2026080301411Hinge · corrodedCORROSION ON HINGE FWD/MID/AFT (3EAS), ALSO DEGRADED PAINT OF STEP PLATE AT AFT CARGO COMPARTMENT HINGE MID (P/N: MM670-35623-003) OF STEP PLATE AT AFT CARGO COMPARTMENT WAS REPLACED PER CRJ-700 SRM 51-42-06-001-001-A01, HINGE FWD (P/N: MM670-35622-003) WAS FSDR REXA2026080301410Hinge · corrodedCORROSION ON HINGE FWD/MID/AFT (3EAS), ALSO DEGRADED PAINT OF STEP PLATE AT AFT CARGO COMPARTMENT HINGE MID (P/N: MM670-35623-003) OF STEP PLATE AT AFT CARGO COMPARTMENT WAS REPLACED PER CRJ-700 SRM 51-42-06-001-001-A01, HINGE FWD (P/N: MM670-35622-003) WAS FSDR REXA2026080301409Hinge · corrodedCORROSION ON HINGE FWD/MID/AFT (3EAS), ALSO DEGRADED PAINT OF STEP PLATE AT AFT CARGO COMPARTMENT HINGE MID (P/N: MM670-35623-003) OF STEP PLATE AT AFT CARGO COMPARTMENT WAS REPLACED PER CRJ-700 SRM 51-42-06-001-001-A01, HINGE FWD (P/N: MM670-35622-003) WAS FSDR REXA2026080301404Seal Rest · corrodedINITIAL INSPECTION: CORROSION ON AFT BAGGAGE BAY DOOR SEAL REST BTW FS1000.00 TO FS1047.00 AND LBL 43 APROX. CORROSION ON AFT BAGGAGE BAY DOOR SEAL REST BTW FS1000.00 TO FS1047.00 AND LBL 43 APROX WAS EVALUATED OUT LIMITS PER CRJ700 SRM 53-61-23-101-001-A01 THSDR REXA2026080301387Plate · crackedCRACK ON SUPPORT PANEL OF RH SIDE CONSOLE AT FLIGHT COMPARTMENT. SUPPORT PANEL OF RH SIDE CONSOLE AT FLIGHT COMPARTMENT WAS REPAIRED PER EA CRJ725-21690 REV. IRSDR REXA2026080301403Drain Pan · crackedCRACK AND BEND LEFT AND RIGHT DRAIN PAN AT AFT EQUIPMENT COMPARTMENT. LEFT AND RIGHT DRAIN PAN AT AFT EQUIPMENT COMPARTMENT WERE REPAIRED PER CRJ/700 SRM 51-71-59-001-001-A01 AND CRJ/700 SRM 51-25-16-001-001-A01SDR REXA2026080301402Drain Pan · crackedCRACK AND BEND LEFT AND RIGHT DRAIN PAN AT AFT EQUIPMENT COMPARTMENT. LEFT AND RIGHT DRAIN PAN AT AFT EQUIPMENT COMPARTMENT WERE REPAIRED PER CRJ/700 SRM 51-71-59-001-001-A01 AND CRJ/700 SRM 51-25-16-001-001-A01SDR REXA2026080301401Stiffener · wornINITIAL INSPECTION: WEAR ON INTERNAL SKIN AND ANGLE ON TAIL BUMPER CUTOUT AREA BTW STGR 26L TO STGR 27R AND VS67.5% APPROX AT AFT EQUIPMENT COMPARTMENT PAINT ON INTERNAL SKIN WAS REMOVED AND NOT DAMAGE WAS FOUND PER CRJ-700 SRM 51-26-01-001-001-A01 AND ANGLE OSDR REXA2026080301400Angle · corrodedINITIAL INSPECTION: CORROSION ON MID CAP AT PASSENGER DOOR CUTOUT. CORROSION ON MID CAP AT PASSENGER DOOR CUTOUT WAS EVALUATED OUT LIMITS PER CRJ-700 SRM 51-10-06-001-001-A01 THEREFORE WAS REPLACED PER CRJ700 SRM 51-41-02-001-001-A01SDR REXA2026080301389Angle · crackedCRACK ON LH FWD AND AFT DRAG ANGLES ON 67.5% REAR SPAR DATUM AT VERTICAL STABILIZER LH FWD AND AFT DRAG ANGLES ON 67.5% REAR SPAR DATUM AT VERTICAL STABILIZER WERE REPAIRED PER CRJ700 SRM 55-31-00-201-001-A01SDR REXA2025111000981Lamp · inoperativeCENTER AISLE SECOND TO LAST EMERGENCY LIGHT INOPERATIVE. R & R LIGHT BULB IAW CRJ 700 AMM 33-51-09 OPS TEST GOOD PN ON/OFF:1317SDR REXA2022111502544Support Angle · crackedAFT CARGO DOOR FORWARD TRACK LOWER SUPPORT ANGLE CLIP MISSING FABRICATED AND INSTALLED NEW AFT CARGO DOOR FORWARD TRACK LOWER SUPPORT ANGLE CLIPSDR REXA2022111102532Torque Link · corrodedRIGHT MAIN LANDING GEAR TORQUE LINKS ( UPPER AND LOWER ) HAVE AREAS OF CORROSION AS WELL AS MISSING PROTECTIVE FINISH " REPLACED R/H UPPER MLG TORQUE LINK ASSEMBLY REF CRJ 700 AMM 32-11-37-400-801 CONFIG
A01,"SDR REXA2022102602315Skin · wornRH WING FLAP SKIN PANEL 684GB CHAFED. REPLACED PANEL 684GB WITH NEW PANEL.SDR REXA2022102602314Baffle · wornR/H UPPER TRANSCOWL HAS CHAFED BAFFLE ON FWD COWL EDGE. NO MANUFACTURER DAMAGE LIMITATIONS FOR PART; REPLACE BAFFLE REMOVED DAMAGE BAFFLE AND INSTALLED 1 EA NEW BAFFLE REF CRJ700 SRM 51-42-06-001-001-A01SDR REXA2022102602313Baffle · crackedRH UPPER TRANSCOWL HAS CRACKED BAFFLE ON FWD COWL EDGE. REMOVED DAMAGED BAFFLE AND INSTALLED 1 EA NEW BAFFLE REF CRJ700 SRM 51-42-06-001-001-A01SDR REXA2022102502288Baffle · crackedRH UPPER TRANSCOWL BAFFLE CRACKED AT FWD END OF COWL. REPLACED CRACKED BAFFLE WITH SERVICEABLE PART PER CRJ700 SRM 51-42-06-001-001-A01SDR REXA2019050700656Frame · corrodedDUE EXCESSIVE DAMAGE CORROSION, OUT LIMITS DAMAGES ON FRAME FS=364 BTW STR 26L TO 25R AT MAIN AVIONIC COMPARTMENT. (E/E)(TCI : 53-20-304) IN REFERENCE NRC 00132. CORROSION LEVEL 2: FRAME FS=364 BTW STR 26L TO 25R AT MAIN AVIONICS COMPARTMENT WAS REPAIRED PER SSDR REXA2019050700651Striker · corrodedAWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON LOWER STRIKER IN STA. FS= 319 TO FS= 349 AND 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) SUMMARY: CORROSION LEVEL 2. DUE TO NOT DAMAGE ALLOWED ON LOWER STRIKER THIS WAS REPLASDR REXA2019050700628Stringer · corrodedINITIAL INSPECTION: CORROSION ON STRINGER 23R / 24R IN STA. FS= 280 TO FS= 333 AT MAIN AVIONICS COMPARTMENT. (E/E)(TCI:53-20-304).
CORROSION LEVEL 1: CORROSION ON STRINGER 23R IN STA. FS= 298 TO FS=315 AT MAIN AVIONICS COMPARTMENT WAS REMOVED PER SRM 51-21-06SDR REXA2019050700625Frame · corrodedINITIAL INSPECTION: CORROSION ON FRAME IN STA. FS= 319 BETWEEN STR 26L TO 25R AT MAIN AVIONIC COMPARTMENT. (E/E)(TCI : 53-20-304).
SUMMARY NRC S/N 00131: CORROSION LEVEL 2 ON FRAME FS319 BTW STR 25L TO 25R AT MAIN AVIONIC COMPARTMENT WAS REPAIRED PER EA N° CRSDR REXA2019050700624Frame · corrodedINITIAL INSPECTION: CORROSION ON FRAME IN STA. FS= 310 BETWEEN STR 24L TO 26R AT MAIN AVIONIC COMPARTMENT. (E/E)(TCI : 53-20-304)
SUMMARY NRC S/N 00129: CORROSION LEVEL 2 ON FRAME FS310 BTW STR 24L TO 24R AT MAIN AVIONIC COMPARTMENT WAS REPAIRED PER EA N° CRJSDR REXA2019050600652Canister · crackedSUPPLEMENTAL INFORMATION (UPDATNG WING STATION) - INITIAL INSPECTION. CRACK ON SLAT TRACK CANISTER 1-3 AT RT WING MAIN FUEL TANK WS 148. (SM)(AD). SLAT TRACK CANISTER 1-3 AT RT WING MAIN FUEL TANK WS 148 WAS REPAIRED PER REO 670-57-42-577 REV. --. LEAK TEST WASDR REXA2019050600654Channel · corrodedINITIAL INSPECTION : CORROSION ON INTERCOSTAL AND CHANNEL FS=1031 / FS=1051 STRG 27 AT REAR FUSELAGE INTERNAL STRUCTURE (FUS) ( TCI:53-30-310).(C2) INTERCOSTAL WAS CLEANED PER SRM 51-26-00-001-001-A01, AFTER CLEANING ON INTERCOSTAL RE-INSPECTION WAS PERFORMEDSDR REXA2019050600650Floor Support · corrodedAWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON FLOOR SUPPORT [ JUMPER/PROX-SENSOR/CONNECTOR-WIRING ANGLE ] IN STA. FS= 310 TO FS= 349 AND 41LBL AT MAIN ENTRANCE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) CORROSION LEVEL 2: FLOOR SUPPORT IN STA. SDR REXA2019050500658Stringer · corrodedCORROSION ON STRINGER 25R FROM FS 333 TO 364 AT MAIN AVIONICS COMPARTMENT.(SM)(E/E). CORROSION LEVEL 2: STRINGER 25R FROM FS 333 TO 364 AT MAIN AVIONICS COMPARTMENT WAS REPLACED PER SRM 51-42-06-001-001-A01.SDR REXA2019050500657Stringer · corrodedCORROSION ON STRINGER 24L FROM FS 280 TO 333 AT MAIN AVIONICS COMPARTMENT.(SM)(E/E). CORROSION LEVEL 2: STRINGER 24L FROM FS. 280 TO FS. 333 WAS REPLACED PER SRM 51-42-06-001-001-A01SDR REXA2019050500634Seat Track · corrodedINITIAL INSPECTION: CORROSION ON SEAT TRACK RAILS BTW FS581 / FS677+3 AND LBL9.00/ RBL9.00 SIDE ABOVE FLOOR (TCI: 53-20-245)
CORROSION LEVEL 2: SEAT TRACK RAILS BTW FS581 / FS677+3 AND LBL9.00/ RBL9.00 WERE REPLACED PER AMM 53-00-49-400-801 (CONFIG A03)SDR REXA2019050500632Intercostal · corrodedINITIAL INSPECTION: CORROSION ON INTERCOSTAL 6 LBL / 6RBL 2LBL AND 2RBL BTW FS 364 TO 349. AT E/E COMPARTMENT.(TCI:53-20-313).
CORROSION LEVEL 2: DUE TO SEVERE DAMAGE INTERCOSTAL 6 LBL / 6RBL 2LBL AND 2RBL BTW FS 364 TO 349. AT E/E COMPARTMENT WERE REPLACED PSDR REXA2019050500627Stringer · corrodedINITIAL INSPECTION: CORROSION ON STRINGER 27 IN STA. FS= 280 TO FS= 295 ALSO 25L BTW FS=295 TO FS=310 AT MAIN AVIONICS COMPARTMENT. (E/E)(TCI:53-20-305). CORROSION LEVEL 2. STRINGER 27 IN STA. FS= 280 TO FS= 295 AND 25L FS=280 TO FS=333 WERE REPLACED PER SRM SDR REXA2019050500623Frame · corrodedINITIAL INSPECTION: CORROSION ON FRAME IN STA. FS= 295 BETWEEN STR 26L TO 23R AT MAIN AVIONIC COMPARTMENT. (E/E)(TCI : 53-20-304)
SUMMARY: FRAME WAS REPAIR PER EA NO CRJ953-08849 REV.IR.SDR REXA2019050400655Frame · corrodedINITIAL INSPECTION:CORROSION ON FRAME AT FS.517, FS.533, FS.549 BTW STR 25L TO 25R. AT THE FORWARD BAGGAGE COMPARMENT. (CAR) (SM)
CORROSION ON SECTION FRAME FS 533 AND FS 549 WAS REMOVED PER FRAME FS=533 WAS MEASURED WITH THE FOLLOWING CONDITIONS: ORIGINAL THSDR REXA2019050400629Stringer · corrodedINITIAL INSPECTION: CORROSION ON STRINGER 26R IN STA. FS= 280 TO FS= 295 ALSO 25RH BTW FS=280 TO FS=310 AT MAIN AVIONICS COMPARTMENT. (E/E) (TCI:53-20-304). STRINGER 26R IN STA. FS= 280 TO FS= 333 AND 25R BTW FS=280 TO FS=333 WAS REPLACED PER SRM 51-42-06-001-
Back to N398CA