# Service difficulty reports: N398CA

A list on [N398CA](https://openairdocs.org/aircraft/N398CA.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 4 · 172 reports

- [SDR REXA2026083101752](https://openairdocs.org/sdr/REXA2026083101752.md): Bulb · inoperative · Aug 27, 2026 · N398CA · Cndair CL6002C10 · Emergency Lighting
  > 1 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 REXA2026042700362](https://openairdocs.org/sdr/REXA2026042700362.md): Door · binding · Apr 21, 2026 · N398CA · Cndair CL6002C10 · Service Doors
  > SERVICE 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 DETAILS
- [SDR REXA2026042700361](https://openairdocs.org/sdr/REXA2026042700361.md): Fitting · faulted · Apr 21, 2026 · N398CA · Cndair CL6002C10 · Passenger/Crew Doors
  > PASSENGER 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 COUNTE
- [SDR REXA2026080301386](https://openairdocs.org/sdr/REXA2026080301386.md): Fitting · damaged · Mar 26, 2026 · N398CA · Cndair CL6002C10 · Ailerons
  > BUSHINGS 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 REXA2026080301388](https://openairdocs.org/sdr/REXA2026080301388.md): Beam · corroded · Mar 13, 2026 · N398CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > SEVERAL 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 REXA2026080301415](https://openairdocs.org/sdr/REXA2026080301415.md): Strap · corroded · Feb 23, 2026 · N398CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > SECONDARY 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. IR
- [SDR REXA2026080301394](https://openairdocs.org/sdr/REXA2026080301394.md): Fitting · corroded · Feb 16, 2026 · N398CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION 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 REXA2026080301393](https://openairdocs.org/sdr/REXA2026080301393.md): Fitting · corroded · Feb 16, 2026 · N398CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION 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 REXA2026080301407](https://openairdocs.org/sdr/REXA2026080301407.md): Beam · corroded · Feb 13, 2026 · N398CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > SEVERAL 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 IR
- [SDR REXA2026080301392](https://openairdocs.org/sdr/REXA2026080301392.md): Fitting · corroded · Feb 12, 2026 · N398CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION 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 REXA2026080301391](https://openairdocs.org/sdr/REXA2026080301391.md): Fitting · corroded · Feb 12, 2026 · N398CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION 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 REXA2026080301406](https://openairdocs.org/sdr/REXA2026080301406.md): Strap · corroded · Feb 11, 2026 · N398CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > INITIAL 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 REXA2026080301390](https://openairdocs.org/sdr/REXA2026080301390.md): Floorbeam · cracked · Feb 11, 2026 · N398CA · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > CRACKED 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 REXA2026080301385](https://openairdocs.org/sdr/REXA2026080301385.md): Rib · cracked · Feb 11, 2026 · N398CA · Cndair CL6002C10 · Wing, Rib/Bulkhead
  > CRACK 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 REXA2026080301414](https://openairdocs.org/sdr/REXA2026080301414.md): Track · corroded · Feb 10, 2026 · N398CA · Cndair CL6002C10 · Cargo/Baggage Doors
  > CORROSION 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 REXA2026080301413](https://openairdocs.org/sdr/REXA2026080301413.md): Track · corroded · Feb 10, 2026 · N398CA · Cndair CL6002C10 · Cargo/Baggage Doors
  > CORROSION 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 REXA2026080301412](https://openairdocs.org/sdr/REXA2026080301412.md): Track · corroded · Feb 10, 2026 · N398CA · Cndair CL6002C10 · Cargo/Baggage Doors
  > CORROSION 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 REXA2026080301411](https://openairdocs.org/sdr/REXA2026080301411.md): Hinge · corroded · Feb 10, 2026 · N398CA · Cndair CL6002C10 · Fuselage, Door Hinge
  > CORROSION 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 F
- [SDR REXA2026080301410](https://openairdocs.org/sdr/REXA2026080301410.md): Hinge · corroded · Feb 10, 2026 · N398CA · Cndair CL6002C10 · Fuselage, Door Hinge
  > CORROSION 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 F
- [SDR REXA2026080301409](https://openairdocs.org/sdr/REXA2026080301409.md): Hinge · corroded · Feb 10, 2026 · N398CA · Cndair CL6002C10 · Fuselage, Door Hinge
  > CORROSION 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 F
- [SDR REXA2026080301404](https://openairdocs.org/sdr/REXA2026080301404.md): Seal Rest · corroded · Feb 10, 2026 · N398CA · Cndair CL6002C10 · Fuselage Main, Structure
  > INITIAL 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 TH
- [SDR REXA2026080301387](https://openairdocs.org/sdr/REXA2026080301387.md): Plate · cracked · Feb 10, 2026 · N398CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CRACK 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. IR
- [SDR REXA2026080301403](https://openairdocs.org/sdr/REXA2026080301403.md): Drain Pan · cracked · Feb 8, 2026 · N398CA · Cndair CL6002C10 · Fuselage Main, Structure
  > CRACK 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-A01
- [SDR REXA2026080301402](https://openairdocs.org/sdr/REXA2026080301402.md): Drain Pan · cracked · Feb 8, 2026 · N398CA · Cndair CL6002C10 · Fuselage Main, Structure
  > CRACK 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-A01
- [SDR REXA2026080301401](https://openairdocs.org/sdr/REXA2026080301401.md): Stiffener · worn · Feb 8, 2026 · N398CA · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > INITIAL 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 O
- [SDR REXA2026080301400](https://openairdocs.org/sdr/REXA2026080301400.md): Angle · corroded · Feb 6, 2026 · N398CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > INITIAL 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-A01
- [SDR REXA2026080301389](https://openairdocs.org/sdr/REXA2026080301389.md): Angle · cracked · Feb 5, 2026 · N398CA · Cndair CL6002C10 · Vertical Stabilizer Miscellaneous Structure
  > CRACK 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-A01
- [SDR REXA2025111000981](https://openairdocs.org/sdr/REXA2025111000981.md): Lamp · inoperative · Nov 7, 2025 · N398CA · Cndair CL6002C10 · Emergency Lighting
  > CENTER AISLE SECOND TO LAST EMERGENCY LIGHT INOPERATIVE. R & R LIGHT BULB IAW CRJ 700 AMM 33-51-09 OPS TEST GOOD PN ON/OFF:1317
- [SDR REXA2022111502544](https://openairdocs.org/sdr/REXA2022111502544.md): Support Angle · cracked · Nov 12, 2022 · N398CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR FORWARD TRACK LOWER SUPPORT ANGLE CLIP MISSING FABRICATED AND INSTALLED NEW AFT CARGO DOOR FORWARD TRACK LOWER SUPPORT ANGLE CLIP
- [SDR REXA2022111102532](https://openairdocs.org/sdr/REXA2022111102532.md): Torque Link · corroded · Nov 9, 2022 · N398CA · Cndair CL6002C10 · Main Landing Gear
  > RIGHT 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 REXA2022102602315](https://openairdocs.org/sdr/REXA2022102602315.md): Skin · worn · Oct 18, 2022 · N398CA · Cndair CL6002C10 · Trailing Edge Flaps
  > RH WING FLAP SKIN PANEL 684GB CHAFED. REPLACED PANEL 684GB WITH NEW PANEL.
- [SDR REXA2022102602314](https://openairdocs.org/sdr/REXA2022102602314.md): Baffle · worn · Oct 15, 2022 · N398CA · Cndair CL6002C10 · Engine Thrust Reverser
  > R/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-A01
- [SDR REXA2022102602313](https://openairdocs.org/sdr/REXA2022102602313.md): Baffle · cracked · Oct 15, 2022 · N398CA · Cndair CL6002C10 · Engine Thrust Reverser
  > RH 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-A01
- [SDR REXA2022102502288](https://openairdocs.org/sdr/REXA2022102502288.md): Baffle · cracked · Oct 15, 2022 · N398CA · Cndair CL6002C10 · Engine Thrust Reverser
  > RH UPPER TRANSCOWL BAFFLE CRACKED AT FWD END OF COWL. REPLACED CRACKED BAFFLE WITH SERVICEABLE PART PER CRJ700 SRM 51-42-06-001-001-A01
- [SDR REXA2019050700656](https://openairdocs.org/sdr/REXA2019050700656.md): Frame · corroded · May 7, 2019 · N398CA · Cndair CL6002C10 · Fuselage Main, Frame
  > DUE 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 S
- [SDR REXA2019050700651](https://openairdocs.org/sdr/REXA2019050700651.md): Striker · corroded · May 7, 2019 · N398CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > AWR; [ 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 REPLA
- [SDR REXA2019050700628](https://openairdocs.org/sdr/REXA2019050700628.md): Stringer · corroded · May 7, 2019 · N398CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > INITIAL 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 51-21-06
- [SDR REXA2019050700625](https://openairdocs.org/sdr/REXA2019050700625.md): Frame · corroded · May 7, 2019 · N398CA · Cndair CL6002C10 · Fuselage Main, Frame
  > INITIAL 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° CR
- [SDR REXA2019050700624](https://openairdocs.org/sdr/REXA2019050700624.md): Frame · corroded · May 7, 2019 · N398CA · Cndair CL6002C10 · Fuselage Main, Frame
  > INITIAL 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° CRJ
- [SDR REXA2019050600652](https://openairdocs.org/sdr/REXA2019050600652.md): Canister · cracked · May 6, 2019 · N398CA · Cndair CL6002C10 · Leading Edge Devices
  > SUPPLEMENTAL 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 WA
- [SDR REXA2019050600654](https://openairdocs.org/sdr/REXA2019050600654.md): Channel · corroded · May 6, 2019 · N398CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > INITIAL 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 PERFORMED
- [SDR REXA2019050600650](https://openairdocs.org/sdr/REXA2019050600650.md): Floor Support · corroded · May 6, 2019 · N398CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > AWR; [ 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 REXA2019050500658](https://openairdocs.org/sdr/REXA2019050500658.md): Stringer · corroded · May 5, 2019 · N398CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION 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 REXA2019050500657](https://openairdocs.org/sdr/REXA2019050500657.md): Stringer · corroded · May 5, 2019 · N398CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION 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-A01
- [SDR REXA2019050500634](https://openairdocs.org/sdr/REXA2019050500634.md): Seat Track · corroded · May 5, 2019 · N398CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > INITIAL 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 REXA2019050500632](https://openairdocs.org/sdr/REXA2019050500632.md): Intercostal · corroded · May 5, 2019 · N398CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > INITIAL 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 P
- [SDR REXA2019050500627](https://openairdocs.org/sdr/REXA2019050500627.md): Stringer · corroded · May 5, 2019 · N398CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > INITIAL 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 REXA2019050500623](https://openairdocs.org/sdr/REXA2019050500623.md): Frame · corroded · May 5, 2019 · N398CA · Cndair CL6002C10 · Fuselage Main, Frame
  > INITIAL 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 REXA2019050400655](https://openairdocs.org/sdr/REXA2019050400655.md): Frame · corroded · May 4, 2019 · N398CA · Cndair CL6002C10 · Fuselage Main, Frame
  > INITIAL 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 TH
- [SDR REXA2019050400629](https://openairdocs.org/sdr/REXA2019050400629.md): Stringer · corroded · May 4, 2019 · N398CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > INITIAL 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-

Next page: https://openairdocs.org/aircraft/N398CA/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/aircraft/N398CA/reports

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