# Service difficulty reports: N379CA

A list on [N379CA](https://openairdocs.org/aircraft/N379CA.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 5 · 227 reports

- [SDR REXA2026101201887](https://openairdocs.org/sdr/REXA2026101201887.md): Door · fod · Oct 9, 2026 · N379CA · Cndair CL6002C10 · Passenger/Crew Doors
  > AFTER LANDING, FA'S COULD NOT OPEN MAIN CABIN DOOR FROM INSIDE. RAMP WAS ABLE TO OPEN FROM OUTSIDE. CLEANED DIRT AND DEBRIS FROM PAX DOOR. CHECKS GOOD IAW AMM 52-11-00. OK FOR SVC.
- [SDR REXA2026012600024](https://openairdocs.org/sdr/REXA2026012600024.md): Lamp · inoperative · Jan 25, 2026 · N379CA · Cndair CL6002C10 · Emergency Lighting
  > LH OVERWING EMERGENCY LIGHT FOUND INOPERATIVE. R & R LIGHT BULB IAW AMM 33-51-15 OPS CHECK GOOD.
- [SDR REXA2025112000986](https://openairdocs.org/sdr/REXA2025112000986.md): Light · odor · Nov 14, 2025 · N379CA · Cndair CL6002C10 · Passenger Compartment Lighting
  > FA REPORTS FLOOR LIGHT BY MAIN CABIN DOOR BURNT OUT. ASSOCIATED W/ EMER LIGHTS. REMOVED AND REPLACED FLOOR LEVEL EMERGENCY FLOOD LIGHT IAW CRJ700 AMM 33-51-11. ALL CHECKS GOOD.
- [SDR REXA2025052900625](https://openairdocs.org/sdr/REXA2025052900625.md): Intercostal · corroded · May 27, 2025 · N379CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORRODED INTERCOSTAL P/N:SH670-32077-3 BETWEEN FS 349.00 AND FS 364.00 AT STGR 26L. INSTALLED INTERCOSTAL P/N:SH670-32077-3 BETWEEN FS 349.00 AND FS 364.00 STGR 26L IAW CRJ700 SRM 51-42-06-001-001-A01. AND CRJ700 SRM 51-42-21-001-001-A01
- [SDR REXA2025051400587](https://openairdocs.org/sdr/REXA2025051400587.md): Seat Track · corroded · May 12, 2025 · N379CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > FABRICATION REQUIRED OF PN SH670-37411-3 FOR PARTS REQUIRED ON JOB HN00228139 SN 721 FABRICATED NEW RBL 9 SEAT TRACK FROM FS 830.40 - FS 985 (SH670-37411-3 MADE FROM 20276-288-0-0A PO# 5-19497) FOR REPAIR ON HN00228139 IAW MHIRJ REO 670-53-00-589 REV C DATED 2
- [SDR REXA2025072500759](https://openairdocs.org/sdr/REXA2025072500759.md): Frame · corroded · May 9, 2025 · N379CA · Cndair CL6002C10 · Fuselage Main, Frame
  > FS310 FRAME IS CORRODED BETWEEN STGR25L AND STGR26R. WHILE WORKING FS310 FRAME IS CORRODED BETWEEN STGR25L AND STGR26R.FOUNDFRAME SEGMENT BETWEEN 26L-27 TO BE OUT OF LIMITS. REPAIRED (INSTALLED FALSE FLANGE AT FRAME 310 BETWEEN STRG 27 AND 26L IAW CRJ 700 SR
- [SDR REXA2025050600558](https://openairdocs.org/sdr/REXA2025050600558.md): Floor Support · corroded · May 5, 2025 · N379CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FABRICATION OF LBL 9 FLOOR BEAM P/N MM670-35301-005 IS REQUIRED FOR FLOOR BEAM REPLACEMENT ON MWC HN00233441,S/N 898. FABRICATED FLOOR BEAM P/N MM670-35301-005 FOR LBL 9 FROM FS 977 - FS 1098 (MADE FROM 7075-T73511 PO# 5-37778) IAW CRJ 700 SRM 51-24-36-001-0
- [SDR REXA2025050600557](https://openairdocs.org/sdr/REXA2025050600557.md): Stringer Splice · corroded · May 5, 2025 · N379CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER SPLICE AT STGR 21 F.S. 333 IS CORRODED INSTALLED NEW SERVICEABLE STRING SPLICE PN: SH670-31197-1 FOR STR 21R AT FS 333 IAW CRJ700 SRM 51-42-06-001-001-A01.
- [SDR REXA2025050500551](https://openairdocs.org/sdr/REXA2025050500551.md): Stringer · corroded · May 5, 2025 · N379CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER 23R FROM FS 333 TO 379 CORRODED ALONG LENGTH OF STRINGER REMOVED STGR 23R FROM FS333 TO FS379 IAW CRJ-700 SRM 51-42-06-001-001-A01. INSTALLED NEW STGR 23R P/N: SH670-31380-1S SEGMENT FROM FS 333.00 TO FS 379.00 IAW CRJ700 SRM 51-42-06-001-001-A01.
- [SDR REXA2025050500550](https://openairdocs.org/sdr/REXA2025050500550.md): Stringer · corroded · May 4, 2025 · N379CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STGR25R IS CORRODED BETWEEN FS280 AND FS310. INSTALLED NEW SERVICEABLE STGR 25R (P/N SH670-31212-2U) FROM FS280 TO FS333 IAW CRJ-700 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01.
- [SDR REXA2025050500549](https://openairdocs.org/sdr/REXA2025050500549.md): Stringer · corroded · May 4, 2025 · N379CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STGR26R IS CORRODED BETWEEN FS280 AND FS310. INSTALLED NEW SERVICEABLE STGR 26R (P/N SH670-31634-2 FROM FS280 TO FS333 IAW CRJ-700 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01.
- [SDR REXA2025050100536](https://openairdocs.org/sdr/REXA2025050100536.md): Stringer Splice · damaged · Apr 28, 2025 · N379CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > FABRICATE REPAIR STRINGER SPLICE AT F.S 533 TO F.S 571, SHIMS AS REQUIRE AND REPAIR SPLICE FOR STRINGER 27 IAW CRJ700 SRM 53-00-03-201-001-A01 FABRICATED, DRILLED, DEBURRED 1EA. STRINGER SPLICE, 1EA.SHIMS, AND 2EA. ANGLES REPAIR SPLICE FOR STRINGER 27 IAW
- [SDR REXA2025050100535](https://openairdocs.org/sdr/REXA2025050100535.md): Floorbeam · corroded · Apr 27, 2025 · N379CA · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > FS280 RH FLOOR CROSSBEAM IS CORRODED. REPAIRED IAW BOMBARDIER GREO 670-53-11-579, REV. B DATE: 2013/05/01.
- [SDR REXA2025042800517](https://openairdocs.org/sdr/REXA2025042800517.md): Stringer Splice · corroded · Apr 27, 2025 · N379CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION FOUND ON SPLICE LOCATED ON FS333 AND STR24R. REMOVED STGR 24R SPLICE PN: SH670-32429-2 AT FS333 FOR REPLACEMENT IAW CRJ700 SRM 51-42-06-001-001-A01. INSTALLED NEW STGR SPLICE P/N:SH670-32429-4S AT STGR 24R FS 333.00 IAW CRJ700 SRM 51-42-06-001-001
- [SDR REXA2025042800516](https://openairdocs.org/sdr/REXA2025042800516.md): Stringer · corroded · Apr 27, 2025 · N379CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STGR23R IS CORRODED BETWEEN FS280 AND FS319. REMOVED STGR23R (P/N SH670-31211-4) FROM FS280-FS333 IAW CRJ-700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. INSTALLED NEW STGR 23R P/N: SH670-31211-4U SEGMENT FROM FS 280.00 TO FS 333.00 IAW CRJ700 SRM 51-
- [SDR REXA2025042800515](https://openairdocs.org/sdr/REXA2025042800515.md): Stringer Splice · corroded · Apr 27, 2025 · N379CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER SPLICE AT STGR23R AND FS 333 IS HEAVILY IN MULTIPLE AREAS. REMOVED SPLICE AT STGR 23R AND FS333 IAW CRJ-700 SRM 51-42-06-001-001-A01. INSTALLED NEW STGR SPLICE P/N:SH670-32429-4S AT STGR 23R FS 333.00 IAW CRJ700 SRM 51-42-06-001-001-A01.
- [SDR REXA2025042800514](https://openairdocs.org/sdr/REXA2025042800514.md): Floorbeam · corroded · Apr 27, 2025 · N379CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FS280 LH FLOOR CROSSBEAM IS CORRODED. REMOVED FS280 L/H FLOOR CROSSBEAM, IAW CRJ-700 SRM 51-42-41-001-001-A01, 51-42-06-001-001-A01, 51-42-13-001-001-A01. INSTALLED FS 280.00 L/H FLOOR CROSSBEAM, P/N: CC670-34094JP-1S, IAW GREO 670-53-11-579, REV. B, DATE 20
- [SDR REXA2025042800513](https://openairdocs.org/sdr/REXA2025042800513.md): Skin · chafed · Apr 18, 2025 · N379CA · Cndair CL6002C10 · Trailing Edge Flaps
  > "WHILE SANDING RH I/B FLAP FOR PAINT FOUND SKIN TO BE CHAFED AT I/B HINGE ARM FROM CONTACT WITH CANOE FAIRING WHILE SANDING RH I/B FLAP FOR PAINT FOUND SKIN TO BE CHAFED AT I/B HINGE ARM FROM CONTACT WITH CANOE FAIRING CHAFING WAS REMOVED IAW CRJ700 SRM TASK
- [SDR REXA2025042100464](https://openairdocs.org/sdr/REXA2025042100464.md): Angle · damaged · Apr 18, 2025 · N379CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > UPON REMOVAL OF FS379 REINFORCEMENT ANGLE P.N. SH670-32119-1, FOUND ANGLE TO HAVE MULTIPLE OVERSIZED HOLES AND REQUIRES REPLACEMENT. FS379 REINFORCEMENT ANGLE P.N. SH670-32119-1 REQUIRES DRILL AND LOCATE DRILLED AND LOCATED FS379 REINFORCEMENT ANGLE P.N. SH67
- [SDR REXA2025052200593](https://openairdocs.org/sdr/REXA2025052200593.md): Skin · damaged · Apr 17, 2025 · N379CA · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > "MR 25425 LOCATE THE REPAIR ON THE AFT LH FUSELAGE LOCATED BELOW THE HP DOOR, BETWEEN FS1108.00 - FS1126.00 AT S21L. REMOVED PREVIOUS REPAIR IAW CRJ700 SRM 51-42-21-001-001-A01. PERFORMED EDDY CURRENT ON FUSELAGE SKIN AND DOUBLER BETWEEN FS1116-FS1126 STRINGE
- [SDR REXA2025050800568](https://openairdocs.org/sdr/REXA2025050800568.md): Floorbeam · corroded · Apr 16, 2025 · N379CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > "FOUND CORROSION UNDER SEAT TRACK ON LBL9 FLOOR BEAM BETWEEN FS 1000 AND 1060. FOUND CORROSION UNDER SEAT TRACK ON LBL9 FLOOR BEAM BETWEEN FS 1000 AND 1060. BLENDED CORROSION ON LBL9 FLOOR BEAM BETWEEN FS 1000 AND 1060 IAW CRJ700 SRM 51-21-06-001-001-A01. C/W
- [SDR REXA2025043000531](https://openairdocs.org/sdr/REXA2025043000531.md): Angle · corroded · Mar 23, 2025 · N379CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > "CORRODED FS 280.00 ""J"" ANGLE BETWEEN LBL9 AND RBL9. NO DAMAGE ALLOWED ON SRM TO THIS PART. LOCATED AND DRILLED NEW FS280.00 J-ANGLE P/N: CC67034095-3S, ITEM 10, IAW BOMBARDIER GREO 670-53-11-579, REV. B. DATE: 2013/05/01 AND SRM 51-40-11-001-001-A01 INSTA
- [SDR REXA2025072400754](https://openairdocs.org/sdr/REXA2025072400754.md): Frame · corroded · Mar 22, 2025 · N379CA · Cndair CL6002C10 · Fuselage Main, Frame
  > FOUND CORROSION ON FRAME SECTION P/N SH670-32033-1 AT F.S. 333 BETWEEN STR 19 AND STR 20. INSTALLED NEW SERVICEABLE FRAME SECTION P/N SH670-32033-1 TO TIE FITTING AT FS 333 BETWEEN STGR 19R AND STGR 20R IAW CRJ-700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-00
- [SDR REXA2025072400753](https://openairdocs.org/sdr/REXA2025072400753.md): Stringer · corroded · Mar 22, 2025 · N379CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > HEAVY CORRODED STGR SPLICE AT STGR 22L FS 333.00. LOCATED AND DRILLED NEW STGR SPLICE P/N:SH670-32429-3. AT STGR 22L FS 333.00. IAW CRJ700 SRM 51-40-11-001-001-A01. INSTALLED NEW STGR SPLICE P/N:SH670-32429-3 AT STGR 22L FS 333.00 IAW CRJ700 SRM 51-42-06-001-0
- [SDR REXA2025051400586](https://openairdocs.org/sdr/REXA2025051400586.md): Frame · corroded · Mar 22, 2025 · N379CA · Cndair CL6002C10 · Fuselage Main, Frame
  > FS319 FRAME IS CORRODED BETWEEN STGR20L AND STGR21L. REMOVED AND REPLACED FRAME P/N SH670-31891-3 AT FS319 BETWEEN STR18L AND STR21L IAW CRJ700 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01.
- [SDR REXA2025051400585](https://openairdocs.org/sdr/REXA2025051400585.md): Frame · corroded · Mar 22, 2025 · N379CA · Cndair CL6002C10 · Fuselage Main, Frame
  > FS319 FRAME IS CORRODED BETWEEN STGR26L AND STGR26R. INSTALLED NEW FRAME AT FS319 (P/N:SH670-31355-1S) BETWEEN STR23R AND STR21L IAW CRJ700 SRM 51-42-06-001-001-A01
- [SDR REXA2025051300583](https://openairdocs.org/sdr/REXA2025051300583.md): Frame · corroded · Mar 22, 2025 · N379CA · Cndair CL6002C10 · Fuselage Main, Frame
  > FS319 FRAME IS CORRODED BETWEEN STGR20L AND STGR21L. REMOVED AND REPLACED FRAME P/N SH670-31891-3 AT FS319 BETWEEN STR18L AND STR21L IAW CRJ700 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01.
- [SDR REXA2025051300582](https://openairdocs.org/sdr/REXA2025051300582.md): Stringer · corroded · Mar 22, 2025 · N379CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STGR24R IS CORRODED BETWEEN FS280 AND FS319. REMOVED AND REPLACED STRINGER 24R P/N SH670-31212-2 BETWEEN FS280 AND FS333 IAW CRJ700 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01.
- [SDR REXA2025051300581](https://openairdocs.org/sdr/REXA2025051300581.md): Frame · corroded · Mar 22, 2025 · N379CA · Cndair CL6002C10 · Fluid Service Doors
  > INTERNAL STRUCTURE BEHIND FWD TOILET SERVICE DOOR IS CORRODED, F.S.379 BETWEEN STGR 23R TO 22R. REMOVED AND REPLACED 379 (P/N SH670-32118-1) IAW CRJ-700 SRM 51-42-06-001-001-A01.
- [SDR REXA2025051200575](https://openairdocs.org/sdr/REXA2025051200575.md): Stringer · corroded · Mar 22, 2025 · N379CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > "STGR20R IS CORRODED BETWEEN FS280 AND FS310. UPON FURTHER INVESTIGATION FOUND THE DISCREPANT AT STGR 20R BETWEEN FS280 AND FS310 TO BE DAMAGE WITHIN PAINT ONLY NO CORROSION NOTED AT THIS TIME IAW CRJ700 SRM 51-26-01-001-001-A01 APPLIED SURFACE FINISH TO STGR
- [SDR REXA2025050800567](https://openairdocs.org/sdr/REXA2025050800567.md): Stringer · corroded · Mar 22, 2025 · N379CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > FOUND MULTIPLE CORRODED FASTNERS IN STR 20R BETWEEN FS 319 AND FS 333. EVALUATED AND FOUND TO BE OUT OF LIMIT DUE TO NO DAMAGE ALLOWED ON THIS AREA, IAW CRJ-700 SRM 53-21-03-101-002-A01. LOCATED AND DRILLED NEW SERVICEABLE STRINGER AT STR 20R P/N: SH670-32428
- [SDR REXA2025050700562](https://openairdocs.org/sdr/REXA2025050700562.md): Stringer · corroded · Mar 22, 2025 · N379CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STGR22L IS CORRODED BETWEEN FS310 AND FS319. LOCATED AND DRILLED NEW STGR 22L P/N:SH670-31210-1U SEGMENT FROM FS 280.00 AND FS 333.00 IAW CRJ700 SRM 51-40-11-001-001-A01. REFER TO TASK 4A FOR INSTALLATION OF NEW PART. INSTALLED SAME SERVICEABLE STGR CLEATS 3 E
- [SDR REXA2025043000530](https://openairdocs.org/sdr/REXA2025043000530.md): Stringer · corroded · Mar 22, 2025 · N379CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER 22R FROM FS 333 TO 379 CORRODED ALONG LENGTH OF STRINGER. INSTALLED NEW STGR 22R P/N:SH670-31379-1S SEGMENT FROM FS 333.00 TO FS 349.00 IAW CRJ700 SRM 51-42-06-001-001-A01.
- [SDR REXA2025042800512](https://openairdocs.org/sdr/REXA2025042800512.md): Stringer Clip · corroded · Mar 22, 2025 · N379CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER 21R FROM FS 295 TO 333 CORRODED ALONG LENGTH OF STRINGER (MARKED ORANGE/RED) REMOVED AND REPLACED STR 21R P/N: SH670-31636-1 FROM F.S. 280- F.S. 333 IAW CRJ700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
- [SDR REXA2025042800511](https://openairdocs.org/sdr/REXA2025042800511.md): Stringer Splice · corroded · Mar 22, 2025 · N379CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER 21R FROM FS 333 TO 379 CORRODED ALONG LENGTH OF STRINGER UPON FURTHER INVESTIGATION FOUND STRINGER 21R FROM FS333-FS379 TO BE OUT OF LIMITS DUE TO CORROSION BEING ON MORE THEN ONE ELEMENT IAW CRJ700 SRM 53-21-03-101-006-A01. REMOVED STRINGER 21R FR
- [SDR REXA2025041700428](https://openairdocs.org/sdr/REXA2025041700428.md): Stringer · corroded · Mar 22, 2025 · N379CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER 23R FROM FS 295 TO 333 CORRODED ALONG LENGTH OF STRINGER (MARKED ORANGE/RED) REMOVED AND REPLACED STGR23R (P/N SH670-31211-4) FROM FS280-FS333 IAW CRJ-700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
- [SDR REXA2025041000416](https://openairdocs.org/sdr/REXA2025041000416.md): Stringer · corroded · Mar 22, 2025 · N379CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > "STGR19R IS CORRODED BETWEEN FS280 AND FS295. BLENDED CORROSION AT STGR19R BETWEEN FS280 AND FS295 IAW CRJ700 SRM 51-21-06-001-001-A01. HFEC PERFORMED ON REWORKED AREAS OF STGR 19R IAW CRJ 700 NDTM PT 1 51-20-006-250-A01 NO INDICATIONS NOTED AT THIS TIME. PERF
- [SDR REXA2025072400751](https://openairdocs.org/sdr/REXA2025072400751.md): Intercostal · corroded · Mar 20, 2025 · N379CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > LH JACKING FITTING INTERCOSTAL IS CORRODED. LH JACKING FITTING INTERCOSTAL IS CORRODED. UPON FURTHER INVESTIGATION FOUND LH JACK FITTING INTERCOSTAL P/N:CC670-32179-1 HEAVY CORRODED ON MULTIPLE AREAS AROUND FASTENERS. NO ALLOWABLE DAMAGE PROVIDED PER CRJ700 SR
- [SDR REXA2025061900671](https://openairdocs.org/sdr/REXA2025061900671.md): Stringer · corroded · Mar 20, 2025 · N379CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER 24L IS CORRODED AROUND 2EA. RIVETS AT APPROX. F.S.490. STRINGER 24L IS CORRODED AROUND 2EA. RIVETS AT APPROX. F.S.490. CHAFING AROUND 3 RIVETS NEEDS REMOVED ON STRINGER 24L F.S 490 REMOVED CORROSION ON STRINGER 24L F.S 490 IAW SRM 51-21-06-001-001-A
- [SDR REXA2025052900595](https://openairdocs.org/sdr/REXA2025052900595.md): Angle · corroded · Mar 20, 2025 · N379CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > RH JACKING FITTING INTERCOSTAL IS CORRODED. RH JACKING FITTING INTERCOSTAL IS CORRODED. UPON FURTHER INVESTIGATION FOUND RH JACK FITTING INTERCOSTAL P/N:CC670-32179-2 HEAVY CORRODED ON MULTIPLE AREAS AROUND FASTENERS. NO ALLOWABLE DAMAGE PROVIDED PER CRJ700
- [SDR REXA2025050200545](https://openairdocs.org/sdr/REXA2025050200545.md): Stringer · corroded · Mar 20, 2025 · N379CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER 22R FROM FS 295 TO 333 CORRODED ALONG LENGTH OF STRINGER (MARKED ORANGE/RED) STRINGER 22R FROM F.S. 295 - F.S. 333 IS HEAVILY CORRODED ON MULTIPLE ELEMENTS WITH DEEP PITTING IN RADIUS. STRINGER REQUIRES REPLACEMENT. LOCATED AND DRILLED NEW STGR 22R P/
- [SDR REXA2025050200544](https://openairdocs.org/sdr/REXA2025050200544.md): Stringer · corroded · Mar 20, 2025 · N379CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > "STRINGER 27 HAS SEVERAL AREAS OF CORROSION BETWEEN FS533 TO FS581 STRINGER 27 HAS SEVERAL AREAS OF CORROSION BETWEEN FS533 TO FS581 AFTER FURTHER INVESTIGATION CORROSION IS ONLY BETWEEN F.S. 533 - F.S. 565, NO CORROSION NOTED ON STRINGER 27 BETWEEN F.S. 565 -
- [SDR REXA2025041000415](https://openairdocs.org/sdr/REXA2025041000415.md): Web · corroded · Mar 20, 2025 · N379CA · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR FWD WEB CORRODED, REQUIRES REPLACEMENT. REMOVED PAX DOOR FWD WEB AND INSTALLED A SERVICEABLE FWD WEB IAW CRJ 700 SRM 51-42-06-001-001-A01 AND 51-40-11-001-001-A01.
- [SDR REXA2025041000414](https://openairdocs.org/sdr/REXA2025041000414.md): Drag Angle · corroded · Mar 20, 2025 · N379CA · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR AFT WEB DRAG ANGLE HAS PREVIOUS REPAIR THAT INTERFERES WITH MODSUM, REQUIRES REPLACEMENT.. REMOVED PAX DOOR AFT WEB DRAG ANGLE IAW CRJ700 SRM 51-42-06-001-001-A01. INSTALLED A SERVICEABLE PAX DOOR AFT WEB DRAG ANGLE IAW CRJ700 SRM 51-42-06-001-001-A01
- [SDR REXA2025041000413](https://openairdocs.org/sdr/REXA2025041000413.md): Web · corroded · Mar 20, 2025 · N379CA · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR AFT WEB CORRODED, REQUIRES REPLACEMENT. REMOVED PAX DOOR AFT WEB IAW CRJ700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. INSTALLED A SERVICEABLE PAX DOOR AFT WEB IAW CRJ700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
- [SDR REXA2025050600556](https://openairdocs.org/sdr/REXA2025050600556.md): Floor Support · corroded · Mar 19, 2025 · N379CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > "MULTIPLE AREAS OF CORROSION ON FLOOR BEAM RBL9 BETWEEN FS1088.20 - 1015. BLENDED CORROSION ON FLOORBEAM BETWEEN FS1015-FS1088 RBL9 100% MATERIAL LOSS NO DAMAGE ALLOWED IAW CRJ700 SRM 51-21-06-001-001-A01, SRM 53-61-43-101-001-A01. INSTALLED NEW SERVICEABLE N
- [SDR REXA2025050100533](https://openairdocs.org/sdr/REXA2025050100533.md): Stringer Splice · corroded · Mar 19, 2025 · N379CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER SPLICE JOINT @ 22R FS 333 CORRODED ALONG LENGTH OF STRINGER SPLICE STRINGER SPLICE P/N SH670-32429-2 AT STGR 22R F.S. 333 IS HEAVILY CORRODED WITH DEEP PITTING IN RADIUS, AND HAS NO ALLOWABLE DAMAGE LIMITS LISTED IN CRJ-700 SRM. STRINGER SPLICE REQUIR
- [SDR REXA2025042200468](https://openairdocs.org/sdr/REXA2025042200468.md): Intercostal · cracked · Mar 19, 2025 · N379CA · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL DD4 P/N 601R318081-1 CORRODED IN MULTIPLE LOCATIONS INSTALLED NEW SERVICEABLE PAX DOOR INTERCOSTAL MID DD4 IAW CRJ700 SRM 51-42-06-001-001-A01 AND51-42-21-001-001-A01
- [SDR REXA2025041400421](https://openairdocs.org/sdr/REXA2025041400421.md): Bushing · damaged · Mar 19, 2025 · N379CA · Cndair CL6002C10 · Ailerons
  > "FOUND L/H AILERON SIDE LUGS LABELED ""C"" AND ""F"" TO BE PREVIOUSLY OVERSIZED. FOUND L/H AILERON SIDE LUGS LABELED ""C"" AND ""F"" TO BE PREVIOUSLY OVERSIZED. FABRICATION OF (QTY. 2) O/S AILERON BUSHINGS ARE REQUIRED. COMPLIED WITH STEPS 6(4), 6(5) & 6(6) OF
- [SDR REXA2025041000412](https://openairdocs.org/sdr/REXA2025041000412.md): Panel · corroded · Mar 19, 2025 · N379CA · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR TOP FIXED PANEL CORRODED AROUND FASTENER HOLES. REMOVED ATTACHING ANGLES AND CANON PLUG CUP FROM DAMAGED TOP PANEL. LOCATED AND DRILLED NEW SERVICEABLE PANEL P/N 601R317075-3. INSTALLED ATTACHING ANGLES AND CANON PLUG CUP IAW CRJ 700 SRM 51-40-11-00

Next page: https://openairdocs.org/aircraft/N379CA/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 = 'N379CA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N379CA/reports

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