# Service difficulty reports: N331CA

A list on [N331CA](https://openairdocs.org/aircraft/N331CA.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 6 · 284 reports

- [SDR REXA2026072301086](https://openairdocs.org/sdr/REXA2026072301086.md): Lamp · inoperative · Jul 21, 2026 · N331CA · Cndair CL6002C10 · Emergency Lighting
  > 2 EMERGENCY FLOOD LIGHT BULBS INOP. R & R 2 EMERGENCY FLOOD LIGHT LAMPS P/N OL3071BPE/GPL REF AMM 33-51-05 OPS CHECK GOOD.
- [SDR REXA2025051900590](https://openairdocs.org/sdr/REXA2025051900590.md): Fitting · corroded · Mar 12, 2025 · N331CA · Cndair CL6002C10 · Fuselage, Landing Gear Attach Fittings
  > O/B BUSHING FOR THE L/H MLG SIDESTAY IN WHEEL WELL IS WORN. VISUAL INSPECTION REVEALED CORROSION AND LIGHT PITTING INSIDE BORE AND ON OUTBOARD FACE (SURFACES IN CONTACT WITH O/B BUSHING) OF LH MLG SIDE STAY FITTING P/N CC670-10608-5. ENGINEERING DISPOSITION RE
- [SDR REXA2025022500214](https://openairdocs.org/sdr/REXA2025022500214.md): Stringer · corroded · Feb 24, 2025 · N331CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STGR26L HAS CORROSION AROUND FASTENER TAILS FROM FS409- FS453. REMOVED CORRODED STRINGER 26L FROM F.S.409 TO F.S.453 AND INSTALLED NEW SERVICABLE STRINGER IAW CRJ 700 SRM 51-42-06-001-001-A01.
- [SDR REXA2025022500213](https://openairdocs.org/sdr/REXA2025022500213.md): Shear Tie · corroded · Feb 23, 2025 · N331CA · Cndair CL6002C10 · Fuselage Internal Mounting Structure
  > FRAME AT FS421 HAS CORROSION ON SHEAR TIE ON AFT SIDE OF FRAME AROUND FASTENER. REPAIRED LOWER FUSELAGE FRAME SECTOR AT F.S.421 BETWEEN STGR 26L AND 26R IAW MHIRJ REO 670-53-21-2527 REV -- DATED 2024-12-28.
- [SDR REXA2025021900202](https://openairdocs.org/sdr/REXA2025021900202.md): Stringer · corroded · Feb 18, 2025 · N331CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STGR 26L HAS CORROSION AROUND FASTENER HEADS FS879-FS885. REPAIRED STRINGER 26L BETWEEN F.S.879 AND F.S.885 IAW MHIRJ REO 670-53-51-328 REV-- DATED 2025-01-13.
- [SDR REXA2024123101624](https://openairdocs.org/sdr/REXA2024123101624.md): Stringer Splice · corroded · Dec 30, 2024 · N331CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > UPON REMOVAL JOINT PIECE STGR P/N:SH670-33241-1 FROM FS.477 STGR 26L FOUND PART TO BE HEAVILY CORRODED, REQUIRES REPLACEMENT. EVALUATED JOINT SPLICE AT STGR 26L, FS477 HAS PITTING CORROSION THROUGH PART. 100% MATERIAL LOSS. FOUND OUT OF LIMITS. CRJ700 S
- [SDR REXA2024123101623](https://openairdocs.org/sdr/REXA2024123101623.md): Stringer Splice · corroded · Dec 30, 2024 · N331CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > UPON REMOVAL OF STGR 21R FS280-FS333, FOUND JOINT PIECE SPLICE (P/N:SH670-31197-1) AT FS333.00 TO HAVE CORROSION REQUIRES EVAL REPLACED AND INSTALLED NEW SERVICEABLE JOINT SPLICE (P/N:SH670-31197-1S) @ FS333 STGR 21R IAW CRJ 700 51-42-06-001-001-A01 LOCAT
- [SDR REXA2025010800017](https://openairdocs.org/sdr/REXA2025010800017.md): Stringer · corroded · Dec 29, 2024 · N331CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > UPON REMOVAL OF STGR 24R FROM FS280-FS333 FOUND STGR 24R SPLICE AT FS 333 TO BE CORRODED REMOVED CORROSION ON STGR 24R SPLICE IAW CRJ 700 SRM 51-21-06-001-001-A01. ORIGINAL MATERIAL THICKNESS WAS.063, MATERIAL REMOVED WAS.011, REMAINING MATERIAL THICKNESS IS
- [SDR REXA2025032800361](https://openairdocs.org/sdr/REXA2025032800361.md): Stringer · corroded · Dec 28, 2024 · N331CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER 24R HEAVILY CORRODED BETWEEN FS333.00 AND FS394.00. REPAIRED STRINGER 24R FS333-FS394 PN: SH670-31368-6 IAW CRJ700 SRM 53-00-03-201-001-A01
- [SDR REXA2025010800015](https://openairdocs.org/sdr/REXA2025010800015.md): Stringer · corroded · Dec 27, 2024 · N331CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER 24R BETWEEN FS 295 TO FS 310 IS CORRODED. REMOVED 10 EA RIVETS FROM STR 24R BETWEEN FS 295 TO FS 310 FOR ACCESS TO REMOVE CORROSION IAW CRJ700 SRM 51-42-06-001-001-A01 DISPLACED CLEATS ON STGR 24R AT FS 310 AND FS 319 IAW CRJ700 SRM 51-42-06-001-001-
- [SDR REXA2024123001615](https://openairdocs.org/sdr/REXA2024123001615.md): Stringer Splice · corroded · Dec 22, 2024 · N331CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > UPON REMOVAL OF STGR 21R FS280-FS333, FOUND JOINT PIECE SPLICE (P/N:SH670-31197-1) AT FS333.00 TO HAVE CORROSION REQUIRES EVAL. EPLACED AND INSTALLED NEW SERVICEABLE JOINT SPLICE (P/N:SH670-31197-1S) @ FS333 STGR 21R IAW CRJ 700 51-42-06-001-001-A01 LOCATE
- [SDR REXA2025010800014](https://openairdocs.org/sdr/REXA2025010800014.md): Door Sill · corroded · Dec 21, 2024 · N331CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > "WHILE INSTALLING NEW AFT CARGO DOOR SURROUND, LOWER SILL P/N MM670-35655-003 FOUND 1 EACH FASTENER HOLE DRILLED NEXT TO A PILOT HOLE AT APPROX. FS1044, LBL 43. REMOVED AFT CARGO DOOR SURROUND, LOWER SILL P/N MM670-35655-003 IAW CRJ700 SRM 51-42-13-001-001-A01
- [SDR REXA2025011000031](https://openairdocs.org/sdr/REXA2025011000031.md): Frame · corroded · Dec 19, 2024 · N331CA · Cndair CL6002C10 · Fuselage Main, Frame
  > F.S. 295 FRAME IS CORRODED ON FWD SIDE OF AT STGR 26R - STGR 27. REPAIRED PER CRJ-700 SRM 53-00-06-201-006-A01.
- [SDR REXA2024121701595](https://openairdocs.org/sdr/REXA2024121701595.md): Stringer Splice · corroded · Dec 16, 2024 · N331CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STGR SPLICE P/N: SH670-32429-1 AT FS 333.00 STGR 23L FOUND HEAVY CORRODED. LOCATED AND DRILLED NEW STGR SPLICE P/N:SH670-32429-3 IAW CRJ700 SRM 51-40-11-001-001-A01.INSTALLED NEW STGR SPLICE P/N: SH670-32429-3 AT FS 333.00 STGR 23L IAW CRJ700 SRM 51-42-0
- [SDR REXA2024121701594](https://openairdocs.org/sdr/REXA2024121701594.md): Stringer Splice · corroded · Dec 16, 2024 · N331CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > JOINT PIECE FS 333.00 STGR 22L FOUND HEAVY CORRODED. LOCATED AND DRILLED NEW STGR SPLICE P/ N: SH670-32429-3 IAW CRJ700 SRM 51-40-11-001-001-A01.INSTALLED NEW STGR SPLICE P/N: SH670-32429-3 AT FS 333.00 S22L IAW CRJ700 SRM 51-42-06-001-001-A01
- [SDR REXA2024121601586](https://openairdocs.org/sdr/REXA2024121601586.md): Stringer · corroded · Dec 15, 2024 · N331CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > BETWEEN FS 349.00 AND FS 364.00 L/H STRINGER 23L IS CORRODED. REPAIRED STRINGER 23L BETWEEN F.S.349 TO F.S.364 IAW CRJ 700 SRM 53-00-03-201-001-A01.
- [SDR REXA2025021000155](https://openairdocs.org/sdr/REXA2025021000155.md): Fitting · damaged · Dec 12, 2024 · N331CA · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR FWD FITTING FOUND TO HAVE 5 EACH ELONGATED HOLES UPON REMOVAL FOR ACCESS. REMOVED DAMAGED FITTING. FABRICATED, DRILLED AND INSTALLED NEW FABRICATED FITTING PN 600-38044-S0101 IAW MHIRJ EO 600-380440S01 AND 601R31702-S12
- [SDR REXA2025021400196](https://openairdocs.org/sdr/REXA2025021400196.md): Door Frame · corroded · Dec 10, 2024 · N331CA · Cndair CL6002C10 · Fuselage Main, Structure
  > PAX DOOR FRAME FS313.56 BETWEEN DD4 AND DD5 CORRODED AND REQUIRES REPLACEMENT. REMOVED DAMAGED FRAME. LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE FRAME (P/N 601R318086-1) IAW CRJ 700 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.
- [SDR REXA2025012100053](https://openairdocs.org/sdr/REXA2025012100053.md): Former · corroded · Dec 10, 2024 · N331CA · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR FORMER @FS 335.163 IS CORRODED AND REQUIRES REPLACEMENT. REMOVED CORRODED FORMER. LOCATED AND DRILLED NEW SERVICEABLE FORMER IAW CRJ 700 SRM 51-40-11-001-001-A01. INSTALLED NEW SERVICEABLE FORMER P#601R31902-15 IAW CRJ 700 SRM 51-42-06-001-001-A01
- [SDR REXA2025011500048](https://openairdocs.org/sdr/REXA2025011500048.md): Former · corroded · Dec 10, 2024 · N331CA · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR FORMER FS311.75 HAS PREVIOUS REPAIR THAT INTERFERES WITH NEW MODSUM. REQUIRES REPLACEMENT. LOCATED AND DRILLED PAX DOOR FORMER @ FS311.75 IAW CRJ 700 SRM 51-40-11-001-001-A01. INSTALLED NEW SERVICEABLE FORMER P#601R318031-5S IAW CRJ 700 SRM 51-42-06-0
- [SDR REXA2025011300037](https://openairdocs.org/sdr/REXA2025011300037.md): Stringer · corroded · Dec 10, 2024 · N331CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER 22R BETWEEN FS 319.00 AND FS 333.00 IS CORRODED. LOCATED AND DRILLED NEW SERVICEABLE STR 22R FROM FS 280 TO FS 333 (PN# SH670-31210-2U) IAW CRJ700 SRM 51-40-11-001-001-A01. INSTALLED NEW SERVICEABLE STR 22R FROM FS 280 TO FS 333 (PN# SH670-31210-2U)
- [SDR REXA2025010700008](https://openairdocs.org/sdr/REXA2025010700008.md): Structure · corroded · Dec 10, 2024 · N331CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > "UPON INVESTIGATION, AFT INNER CHORD P/N: MM670-35657-003 OF AFT BAGGAGE DOOR SURROUND STRUCTURE WITH CORROSION. REMOVED CORROSION IAW CRJ 700 SRM 51-21-06-001-001-A01, FINAL THICKNESS 0.013"" OF NOMINAL THICKNESS 0.063"" NOT ALLOWED DAMAGE. REQUIRES REPLACEME
- [SDR REXA2025010300003](https://openairdocs.org/sdr/REXA2025010300003.md): Intercostal · corroded · Dec 10, 2024 · N331CA · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL DD7A FWD CORRODED AND REQUIRES REPLACEMENT. LOCATED AND DRILLED INTERCOSTAL IAW CRJ 700 SRM 51-40-11-001-001-A01. INSTALLED NEW SERVICEABLE INTERCOSTAL PN:601R318083-1 IAW CRJ 700 SRM 51-42-06-001-001-A01.
- [SDR REXA2024121601585](https://openairdocs.org/sdr/REXA2024121601585.md): Stringer · corroded · Dec 10, 2024 · N331CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER SPLICE AT FS 333.00 STGR 22R CORRODED. REPLACED STRINGER SPLICE
- [SDR REXA2025010800013](https://openairdocs.org/sdr/REXA2025010800013.md): Stringer · corroded · Dec 3, 2024 · N331CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > UPON REMOVAL OF AVIONICS SUPPORT BRACKET ANGLE AT F.S.295, STGR 21R FOUND CORROSION ON STGR 21R UNDER BRACKET REMOVED ALL RIVETS ON STRINGER 21R BETWEEN FS 280.00 AND FS 333.00 IAW CRJ 700 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01. REMOVED STRINGER 21R JO
- [SDR REXA2025011000030](https://openairdocs.org/sdr/REXA2025011000030.md): Stringer · corroded · Nov 27, 2024 · N331CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER 22L BETWEEN F.S.333 TO F.S.349 IS CORRODED. REPAIRED PER CRJ700 SRM 53-00-03-201-001-A01.
- [SDR REXA2024123001614](https://openairdocs.org/sdr/REXA2024123001614.md): Stringer · corroded · Nov 27, 2024 · N331CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER 22R BETWEEN F.S.333 TO F.S.349 IS CORRODED. EVALUATED DAMAGE FOUND TO BE 100% MATERIAL LOSS, FOUND P/N SH670-31379-1 TO BE OUT OF ALLOWABLE LIMITS IAW CRJ700 SRM 53-21-03-101-006-A01 REQUIRES REPLACEMENT INSTALLED NEW SERVICEABLE STRG SPLICE FROM
- [SDR REXA2024122401606](https://openairdocs.org/sdr/REXA2024122401606.md): Stringer · corroded · Nov 27, 2024 · N331CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER 21R AT F.S.364 IS CORRODED. REMOVED DAMAGED STGR 21R SEGMENT BETWEEN FS 333.00 AND FS 379.00 IAW CRJ700 SRM 51-42-06-001-001-A01. INSTALLED NEW STGR 21R P/N:SH670-31383-1S BETWEEN FS 333.00 AND FS 379.00. IAW CRJ700 SRM 51-42-06-001-001-A01.
- [SDR REXA2024120901558](https://openairdocs.org/sdr/REXA2024120901558.md): Intercostal · corroded · Nov 27, 2024 · N331CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > F.S.394 TO F.S.409 CENTER LEFT INTERCOSTAL AT STGR 27 IS CORRODED ON BOTTOM FLANGE. REMOVED INTERCOSTAL (PN# SH670-32075-4) FROM STR 27 BETWEEN FS 394 - FS 409 IAW CRJ700 SRM 51-42-06-001-A01 AND 51-42-21-001-001-A01. LOCATED AND DRILLED NEW SERVICEABLE IN
- [SDR REXA2024120901557](https://openairdocs.org/sdr/REXA2024120901557.md): Seat Track · corroded · Nov 27, 2024 · N331CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > R/H FS712-FS756 SIDE SEAT RAIL IS CORRODED. REMOVED UNSERVICEABLE SIDE SEAT RAIL P/N:SH670-37509-1 ON R/H BETWEEN FS712-FS763. IAW CRJ700 53-00-49-000-801-A03.PAINTED NEW SERVICEABLE SEAT RAIL P/N:SH670-37509-1 IAW BOMBARDIER MODSUM IS67053000195 REV A. DAT
- [SDR REXA2025010800016](https://openairdocs.org/sdr/REXA2025010800016.md): Lug · damaged · Nov 26, 2024 · N331CA · Cndair CL6002C10 · Wing, Control Surface Attach Fittings
  > "RH AILERON # 2 AND #3 HINGE LUGS WERE FOUND OVERSIZED UPON REMOVAL OF BEARINGS. #2 LUG BORE IS.9895"" THE #3 LUG BORE IS.9935"" C/W MHIRJ REO 690-57-61-351 REV A DATED 2024-12-21."
- [SDR REXA2025010800012](https://openairdocs.org/sdr/REXA2025010800012.md): Frame · corroded · Nov 26, 2024 · N331CA · Cndair CL6002C10 · Fuselage Main, Frame
  > FS863 FRAME IS CORRODED FROM STGR 26L-26R ON FWD AND AFT SIDE IF FRAME AND ON SHEAR TIES. REPAIRED IAW ENDEAVOR AIR EA# CRJ753-17935, REV IR, DATED 12/15/2024.
- [SDR REXA2024123001613](https://openairdocs.org/sdr/REXA2024123001613.md): Frame · corroded · Nov 26, 2024 · N331CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > F.S. 517 STR 25L-25R CORRODED AFT SIDE LEG AND GOING UP FACE OF FRAME LOCATED AND DRILLED NEW SERVICEABLE BOTTOMS STUB FRAME AT FS518 BETWEEN STGRS25L AND 26L IAW CRJ-700 SRM 51-40-11-001-001-A01. INSTALLED NEW SERVICEABLE BOTTOM STUB FRAME P/N SH670-332
- [SDR REXA2025010800011](https://openairdocs.org/sdr/REXA2025010800011.md): Bushing · damaged · Nov 25, 2024 · N331CA · Cndair CL6002C10 · Wing Main, Frame Structure
  > "LH AILERON PCU LUGS MARKED C AND F WERE FOUND OVERSIZED UPON REMOVAL OF BUSHINGS. COMPLIED WITH STEPS #6.2, #6.5, & #6.6 OF BOMBARDIER REO 670-57-61-107 REV. -B DATED 2019-01-14. STEP #6.2 - FINAL LUG BORE INTERNAL DIAMETERS ARE (C = 0.8445"") & (F = 0.8450""
- [SDR REXA2025021000154](https://openairdocs.org/sdr/REXA2025021000154.md): Intercostal · corroded · Nov 24, 2024 · N331CA · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL DD4 IS CORRODED REMOVED DAMAGED INTERCOSTAL. LOCATED, DRILLED AND INSTALLED NEW DD4 INTERCOSTAL PN 601R318081-1S IAW CRJ700 51-40-11-001-001-A01, 51-42-21-001-001-A01 AND 51-42-06-001-001-A01
- [SDR REXA2025010300002](https://openairdocs.org/sdr/REXA2025010300002.md): Intercostal · corroded · Nov 24, 2024 · N331CA · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL DD3 IS CORRODED. INSTALLED NEW SERVICEABLE INTERCOSTAL PN:601R318056-1S IAW CRJ 700 SRM 51-42-06-001-001-A01.
- [SDR REXA2025010600007](https://openairdocs.org/sdr/REXA2025010600007.md): Door Sill · corroded · Nov 15, 2024 · N331CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR SILL CORRODED MULTIPLE PLACES BETWEEN F.S. 1000 - F.S. 1047 REMOVED AND INSTALLED NEW AFT CARGO DOOR SILL PN P/N MM670-35655-003 IAW CRJ700 SRM 53-61-23-201-001-A01 AND CRJ700 SRM 51-42-13-001-001-A01 AND CRJ700 SRM 51-45-00-001-001-A01 AND
- [SDR REXA2024102400942](https://openairdocs.org/sdr/REXA2024102400942.md): Lamp · inoperative · Oct 22, 2024 · N331CA · Cndair CL6002C10 · Emergency Lighting
  > RIGHT FWD AND LEFT AFT EXTERIOR EMERGENCY LIGHTS INOP AND LENS COVERS DETERIORATED. R&R EMERGENCY LIGHTS BULBS AND LENS COVERS PER AMM 33-51-15. CHECK GOOD. PN ON/OFF 8GH002473-08, 9EL400042-11
- [SDR REXA2021122701188](https://openairdocs.org/sdr/REXA2021122701188.md): Fitting · gouged · Nov 19, 2021 · N331CA · Cndair CL6002C10 · Wing Structure
  > INSPECTED THE L/H WING AILERON BUSHING BORE AT WS 343.50 AND FOUND DAMAGE TO THE TOP CENTER OF THE O/B BUSHING BORE. - FOUND L/H WING AILERON BUSHING BORE TOP CENTER OF THE I/B BUSHING BORE REPAIRED BORE IAW MHIRJ 670-57-51-455, REV.A DATED 2021-11-10.
- [SDR REXA2021122701187](https://openairdocs.org/sdr/REXA2021122701187.md): Fitting · gouged · Nov 18, 2021 · N331CA · Cndair CL6002D24 · Wing Structure
  > SUPPLEMENTAL INFORMATION / CORRECTED INFORMATION. THIS CONTAINS THE CORRECT ATA AND AIRCRAFT MODEL NUMBER.
- [SDR REXA2020100500677](https://openairdocs.org/sdr/REXA2020100500677.md): Battery · failed · Sep 30, 2020 · N331CA · Cndair CL6002C10 · Emergency Lighting
  > OVERHEAD AISLE EMERGENCY FLOOD LIGHTS AND EMERGENCY EXIT SIGN DO NOT ILLUMUNATE W/EMERGENCY LIGHTING ACTIVE. REMOVED AND REPLACED EMERGENCY BATTERY PACK NR 2, IAW CRJ 700 JOBCARD 33-900-701. OPS CHECK GOOD.
- [SDR N6WA20181115401](https://openairdocs.org/sdr/N6WA20181115401.md): Light · broken · Nov 14, 2018 · N331CA · Cndair CL6002C10 · Emergency Lighting
  > EMERGENCY ESCAPE PATH LIGHTING BROKEN AND MISSING AT EXIT ROW.REPLACED SAFETY GLOW EXIT ROW AT LH SIDE REPLACING WITH SAFETY GLOW FROM ROW 1A IAW CRJ 900AMM 33-51-01.
- [SDR V0XD20180713001](https://openairdocs.org/sdr/V0XD20180713001.md): Skin · cracked · Jul 13, 2018 · N331CA · Cndair CL6002C10 · Passenger/Crew Doors
  > PASSENGER DOOR INTERNAL SKIN AT PANEL 832AL IS CRACKED. REPAIRED INTERNAL SKIN IAW REO 670-52-11-1025 DATED 2018-06-19.
- [SDR V0XD2018061904](https://openairdocs.org/sdr/V0XD2018061904.md): Bracket · cracked · Jun 15, 2018 · N331CA · Cndair CL6002C10 · Passenger/Crew Doors
  > TWO BRACKETS FOUND CRACKED AT THE PASSENGER DOOR UPPER EDGE. REMOVED AND REPLACED IAW SRM 51-40-00.
- [SDR V0XD2018052202](https://openairdocs.org/sdr/V0XD2018052202.md): Angle · corroded · May 22, 2018 · N331CA · Cndair CL6002C10 · Passenger/Crew Doors
  > PASSENGER DOOR MID-CAP IS CORRODED. REMOVED AND REPLACED THE MID-CAP IAW SRM 51-42-02, 51-40-11, AMM 52-70-04, AND 20-21-00.
- [SDR V0XD201805220001](https://openairdocs.org/sdr/V0XD201805220001.md): Frame · cracked · May 22, 2018 · N331CA · Cndair CL6002C10 · Fuselage Main, Frame
  > FRAME BS 333, STRINGER 0 FOUND CRACKED. REMOVED AND REPLACED THE FRAME IAW SRM 51-42-06, 51-42-21, 51-40-11, 53-21-23, 51-32-59, 51-24-36, AMM 20-70-00, 20-30-00, DRAWING SH670-41536, AND SH670-698-41558.
- [SDR V0XD2018053121001](https://openairdocs.org/sdr/V0XD2018053121001.md): Hinge · excess play · May 21, 2018 · N331CA · Cndair CL6002C10 · Fuselage, Door Hinge
  > PASSENGER DOOR HINGE HAD PLAY.: REPAIRED THE DOOR HINGE IAW EO 670-53-21-582, REV F, AND REO 670-53-21-1527.
- [SDR V0XD201805210001](https://openairdocs.org/sdr/V0XD201805210001.md): Bracket · cracked · May 21, 2018 · N331CA · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > AFT EQUIPMENT BAY WATER LINE BRACKET AT STRINGER 9L WAS FOUND CRACKED. REPLACED THE BRACKET IAW SRM 51-42-21, AND AMM 20-21-00.
- [SDR V0XD20180520001](https://openairdocs.org/sdr/V0XD20180520001.md): Link Assy · cracked · May 20, 2018 · N331CA · Cndair CL6002C10 · Passenger/Crew Doors
  > PASSENGER DOOR LATCH MECHANISM LINK SUB-ASSEMBLY CRACKED. REPLACED PASSENGER DOOR LATCH MECHANISM LINK SUB-ASSEMBLY IAW AMM 52-11-02.
- [SDR V0XD20180521002](https://openairdocs.org/sdr/V0XD20180521002.md): Seat Track · corroded · May 17, 2018 · N331CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK NR 1 FROM BS 374 - 485 WAS CORRODED. FABRICATED AND INSTALLED A NEW SEAT TRACK IAW REO 670-53-00-013, REV J, AND REO 670-53-00-343, REV M.

Next page: https://openairdocs.org/aircraft/N331CA/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 = 'N331CA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N331CA/reports

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OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.