# Service difficulty reports: N835AY

A list on [N835AY](https://openairdocs.org/aircraft/N835AY.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 2 · 97 reports

- [SDR 2021F00391](https://openairdocs.org/sdr/2021F00391.md): Fitting · none · Dec 13, 2021 · N835AY · Bombdr BD1001A10 · Horizontal Stabilizer Miscellaneous Structure
  > LH HORIZONTAL STABILIZER TO ELEVATOR OUTBOARD FLUTTER DAMPER FITTING AT BL56.92 RIB NUMBER 5 HAD MULTIPLE DAMAGES ON FORWARD END OF FITTING CAUSED BY TOOLING DAMAGE/PERSONAL ERROR WHICH WAS CLASSIFIED AS A MAJOR REPAIR. FLUTTER DAMPER FITTING WAS REMOVED AN
- [SDR REXA2021030900082](https://openairdocs.org/sdr/REXA2021030900082.md): Bulkhead · damaged · Feb 20, 2021 · N835AY · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FWD FACE OF 621 BULKHEAD HAS MULTIPLE SCREW SHANK MARKS ON SKIN AND RIVET HEADS. REPAIRED 300 B/H IAW MHI REO 601R53-61-7567
- [SDR REXA2020070600584](https://openairdocs.org/sdr/REXA2020070600584.md): Battery Pack · discharged · Jun 16, 2020 · N835AY · Cndair CL6002B19 · Emergency Lighting
  > FWD MOST EXTERIOR EMERGENCY LIGHTS INOP. REMOVED AND INSTALLED THE EPSU BATTERY PACK PS1LF IAW JOB CARD 33-900-701. PERFORMED OPS CHECK. OPS CHECK GOOD. PN OFF: 2013-1A SN OFF: 103895 PN ON: 2013-1ASMI SN ON: 8724.
- [SDR REXA2019061270863](https://openairdocs.org/sdr/REXA2019061270863.md): Floor Support · corroded · Jun 7, 2019 · N835AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RH FLOOR SILL CORRODED FS 559+96. REMOVED AND REPLACED FLOOR SILL
- [SDR REXA2019061230862](https://openairdocs.org/sdr/REXA2019061230862.md): Angle · cracked · Jun 3, 2019 · N835AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 559 LNL 19 AND RBL 18 CRACKED AT LOWER CAP ANGLE. REPAIRED AND MODIFIED IAW EO P53025
- [SDR REXA2019061230860](https://openairdocs.org/sdr/REXA2019061230860.md): Plate · cracked · Jun 3, 2019 · N835AY · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR KICKPLATE CRACKED. NEW KICK PLATE LOCATED AND DRILLED I.A.W. CRJ-200 SRM 51-40-11 TR 51-42. REFER TO AAR WORK ORDER 1017193-2000-0085 S/N 7119114 FOR INSTALLATION.
- [SDR REXA201906120861](https://openairdocs.org/sdr/REXA201906120861.md): Skin · gouged · Jun 2, 2019 · N835AY · Cndair CL6002B19 · Engine Cowling System
  > 445AB OUTER SKIN GOUGED AT LATTCHES. REMOVED GOUGED DOUBLER AND REPLACED WITH NEW FABRICATED DOUBLER I.A.W. CRJ-200 CMM 71-12-01.
- [SDR REXA2019061260859](https://openairdocs.org/sdr/REXA2019061260859.md): Angle · corroded · May 26, 2019 · N835AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FUSELAGE, FORWARD WING TO BODY FAIRING MOUNT ANGLE CORRODED RHS. REMOVED AND REPLACED FAIRING MOUNT ANGLE ON FUSELAGE AT FWD WING TO BODY IAW CRJ 200 SRM 51-42-06.
- [SDR REXA2019061240858](https://openairdocs.org/sdr/REXA2019061240858.md): Floor Support · corroded · May 24, 2019 · N835AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LBL 27 I/B AND O/B FLOOR PANEL LANDINGS HAVE CORROSION SPOTS BETWEEN FS 610 THRU FS 621, IN THE CARGO BAY. REPAIRED LBL 27 INBOARD AND OUTBOARD FLOOR PANEL LANDINGS IAW ENDEAVOR E.A NO# CRJ 253-09044 AAR SM 107
- [SDR REXA2019061220856](https://openairdocs.org/sdr/REXA2019061220856.md): Stringer · corroded · May 22, 2019 · N835AY · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > STGR 23R HAS CORROSION BETWEEN FRAMES 319.70 AND 310, IN THE FWD E & E BAY. REPAIRED IAW EA CRJ 253-08988 REV IR AAR SM 107
- [SDR REXA2019061690857](https://openairdocs.org/sdr/REXA2019061690857.md): Strap · corroded · May 19, 2019 · N835AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR PANEL LANDING ANGLE STRIP HAS CORROSION SPOTS AT FS 621 BETWEEN LBL 27 AND THE LH FLOOR SILL, IN THE CARGO BAY. REMOVED DAMAGE IAW CRJ 200 REO 601R-53-61-117 AAR SM 58
- [SDR REXA2019061219850](https://openairdocs.org/sdr/REXA2019061219850.md): Intercostal · corroded · May 19, 2019 · N835AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INTERCOSTAL ON TOP OF STGR 20R HAS CORROSION BETWEEN FRAMES 310 AND 319.70, IN THE FWD E & E BAY. REMOVED AND REPLACED INTEROCASTAL ATTACHED TO STRINGER 20R IAW CRJ 200 SRM 51-42-06 AAR SM 84
- [SDR REXA2019061219849](https://openairdocs.org/sdr/REXA2019061219849.md): Frame · cracked · May 19, 2019 · N835AY · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME FS333.0 CRACKED AT TOOLING HOLE AT LBL 5.0 ABOVE PAX DOOR. REPAIRED FRAME 333 IAW EA CRJ 253-08930 AAR R SM 4
- [SDR REXA2019061260855](https://openairdocs.org/sdr/REXA2019061260855.md): Angle · cracked · May 16, 2019 · N835AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > ANGLE AT STA. 473.15 LH FUSELAGE SUPPORT BEAM ABOVE CTR WING IS CRACKED. REPLACED ANGLE @ STA 473.15 L/H FUSELAGE ABOVE CTR WING IAW CRJ 200 SRM 51-42-06 AND 51-42-21 AAR SM 33
- [SDR REXA2019061260854](https://openairdocs.org/sdr/REXA2019061260854.md): Angle · cracked · May 16, 2019 · N835AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > ANGLE AT STA. 461.00 RH FUSELAGE SUPPORT BEAM ABOVE CTR WING IS CRACKED. ANGLE @ STA 461.00 R/H FUSELAGE ABOVE CTR WING WAS REPLACED IAW CRJ 200 SRM 51-42-06 AAR SM 33
- [SDR REXA2019061260853](https://openairdocs.org/sdr/REXA2019061260853.md): Angle · cracked · May 16, 2019 · N835AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > ANGLE AT STA. 449.85 RH FUSELAGE SUPPORT BEAM ABOVE CTR WING IS CRACKED REPLACED ANGLE @ STA 449.85 R/H FUSELAGE ABOVE CTR WING IAW CRJ 200 SRM 51-42-06 AAR SM 33
- [SDR REXA2019061260852](https://openairdocs.org/sdr/REXA2019061260852.md): Angle · cracked · May 16, 2019 · N835AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > ANGLE AT STA. 449.85 LH FUSELAGE SUPPORT BEAM ABOVE CTR WING IS CRACKED REPLACED ANGLE @ STA 449.85 L/H FUSELAGE ABOVE CTR WING IAW CRJ 200 SRM 51-42-06 AAR SM 33
- [SDR REXA2019061260851](https://openairdocs.org/sdr/REXA2019061260851.md): Angle · cracked · May 16, 2019 · N835AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > ANGLE AT STA.473.15 RH FUSELAGE SUPPORT BEAM ABOVE CTR WING IS CRACKED REPLACED ANGLE @ STA 473.15 R/H FUSELAGE ABOVE CTR WING IAW CRJ 200 SRM 51-42-06 51-42-21 AAR SM 107
- [SDR REXA201901214848](https://openairdocs.org/sdr/REXA201901214848.md): Floor Support · corroded · May 14, 2019 · N835AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LBL 27 I/B AND O/B FLOOR PANEL LANDINGS HAS CORROSION SPOTS BETWEEN FS 574 THRU FS 610, IN THE CARGO BAY. REMOVED AND REPLACED LBL 27 I/B AND OUTBOARD FLOOR PANEL LANDINGS AND BEAM CAP BETWEEN F.S. 574 AND 610 IN THE CARGO BAY I.A.W. CRJ-200 SRM 51-42-21 AAR
- [SDR REXA201901230845](https://openairdocs.org/sdr/REXA201901230845.md): Support · cracked · May 13, 2019 · N835AY · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR FWD TRACK, LOWER SUPPORT IS CRACKED AND BENT. REMOVED AND REPLACED LOWER SUPPORT IAW SRM 51-42-06 ON FWD CARGO DOOR TRACK.
- [SDR REXA201906120864](https://openairdocs.org/sdr/REXA201906120864.md): Light · inoperative · May 10, 2019 · N835AY · Cndair CL6002B19 · Emergency Lighting
  > LAST AFT EMERGENCY CEILING FLOOD LIGHT INOP. REMOVED/REPLACED AFT EMERGENCY CEILING FLOOD LIGHT IAW CRJ 200 AMM 33-51-16 OPS TEST ACCOMPLISHED ON W/O 1017193 2000 0017 SN7119046 AAR R RE 13
- [SDR REXA2019061200846](https://openairdocs.org/sdr/REXA2019061200846.md): Attach Angle · cracked · May 10, 2019 · N835AY · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > STRINGER 3L ATTACH ANGLE CRACKED AT FS 280. REMOVED AND REPLACED THE ATTACH ANGLE IAW SRM 51-42-21 AND 51-42-06.
- [SDR REXA2019061280844](https://openairdocs.org/sdr/REXA2019061280844.md): Seat Track · corroded · May 8, 2019 · N835AY · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK ON TOP OF LBL 9 HAS CORROSION BETWEEN FS 559+112 AND FS 574, IN THE CARGO BAY. REMOVED AND REPLACED I.A.W. CRJ-200 AMM 53-00-49 AAR SM 58
- [SDR REXA2019061280843](https://openairdocs.org/sdr/REXA2019061280843.md): Seat Track · corroded · May 8, 2019 · N835AY · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK ON TOP OF RBL 9 HAS CORROSION BETWEEN FS 559+112 AND FS 574, IN THE CARGO BAY. REMOVED AND REPLACED IAW CRJ 200 AMM 53-00-49 AAR SM 58
- [SDR REXA2019061207847](https://openairdocs.org/sdr/REXA2019061207847.md): Attach Bracket · cracked · May 7, 2019 · N835AY · Cndair CL6002B19 · Wing, Attach Fittings
  > ATTACH BRACKET FOR L/E PANEL 630AL IS CRACKED REMOVED AND REPLACED BRACKETS IAW CRJ 200 SRM 51-41-02. AAR SM 58
- [SDR REXA2019061230842](https://openairdocs.org/sdr/REXA2019061230842.md): Rub Strip · worn · May 3, 2019 · N835AY · Cndair CL6002B19 · Nacelle/Pylon Miscellaneous Structure
  > RUB STRIP WORN IN SEVERAL AREAS. REMOVED AND REPLACED THE RUB STRIP ON ACCESS COWL 432AB IAW CMM 71-14-01 AAR SM 58
- [SDR REXA2018121181225](https://openairdocs.org/sdr/REXA2018121181225.md): Battery Pack · inoperative · Dec 8, 2018 · N835AY · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHTS WON'T ILLUMINATE. R/R EMERGENCY BATTERY PACKS IAW AMM 33-51-04.OPS CHK'D EMERGENCY LIGHTS GOOD.NO DEFECTS NOTED.
- [SDR REXA201808220711](https://openairdocs.org/sdr/REXA201808220711.md): Oxygen Mask · leaking · Aug 19, 2018 · N835AY · Cndair CL6002B19 · Crew Oxygen System
  > FIRST OFFICER`S MASK LEAKED AND DOES NOT SEAL ON THE FACE. REMOVED AND REPLACED THE OXYGEN MASK IAW AMM 35-11-12. PERFORMED AN OPS TEST IAW 35-10-00-710-801. OPS CHECKED GOOD. ACFT OK FOR SERVICE.
- [SDR REXA2018062760538](https://openairdocs.org/sdr/REXA2018062760538.md): Apu · unknown · Jun 26, 2018 · N835AY · Cndair CL6002B19 · APU Core Engine
  > APU HAD AN UNCOMMANDED SHUTDOWN ON THE GROUND & DURING FLIGHT. NO ASSOCIATED CAUTIONS OR WARNING MESSAGES. VIBRATION FELT AT AROUND 90% RPM DURING START OF APU, JET FUEL ODOR IN THE COCKPIT AFTER SHUTDOWN DURING FLIGHT. OPS CHECKED THE APU WAS SATISFACTORY
- [SDR REXA2018041700293](https://openairdocs.org/sdr/REXA2018041700293.md): Battery Pack · inoperative · Apr 17, 2018 · N835AY · Cndair CL6002B19 · Emergency Equipment
  > PILOT`S FLASHLIGHT, RED FLASHING LED INOPERATIVE. REMOVED AND REPLACED THE BATTERY IAW CMM 25-60-02.
- [SDR REXA2017012100109](https://openairdocs.org/sdr/REXA2017012100109.md): Floor Support · corroded · Jan 21, 2017 · N835AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT AT PAX DOOR THRESHOLD CORRODED. REMOVED IAW SRM 51-42-06, 51-42-21, 51-42-13. FABRICATED A REPLACEMENT IAW SRM 51-24-21, 51-24-36, 51-40-11. INSTALLED IAW SRM 51-42-06, 51-42-21, 51-42-13 OPS CHECKED.
- [SDR REXA2017011800117](https://openairdocs.org/sdr/REXA2017011800117.md): Mount · gouged · Jan 18, 2017 · N835AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AFT ACCY COMPARTMENT, LEFT SIDE AFT APU ENCLOSURE MOUNT AROUND FASTENER HOLE AREA IS GOUGED. REMOVED AND REPLACED IAW SRM 51-42-06.
- [SDR REXA2017011800116](https://openairdocs.org/sdr/REXA2017011800116.md): Intercostal · cracked · Jan 18, 2017 · N835AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INTERCOSTAL AT BS 621 AND STRINGER 16L IS CRACKED. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-42-22 & 51-42-21.
- [SDR REXA2017011800115](https://openairdocs.org/sdr/REXA2017011800115.md): Intercostal · cracked · Jan 18, 2017 · N835AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INTERCOSTAL AT BS 621 AND STRINGER 15L IS CRACKED. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-42-21 & 51-42-22.
- [SDR REXA2017011800114](https://openairdocs.org/sdr/REXA2017011800114.md): Angle · cracked · Jan 18, 2017 · N835AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > ANGLE AT BS 621 AND STRINGER 14L IS CRACKED. REMOVED AND REPLACED THE ANGLE IAW SRM 51-42-06 & 51-42-21.
- [SDR REXA2017011800113](https://openairdocs.org/sdr/REXA2017011800113.md): Intercostal · cracked · Jan 18, 2017 · N835AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INTERCOSTAL AT BS 621 AND STRINGER 14L IS CRACKED. REMOVED & REPLACED THE INTERCOSTAL IAW SRM 51-42-21 & 51-42-22.
- [SDR REXA2017011800112](https://openairdocs.org/sdr/REXA2017011800112.md): Intercostal · cracked · Jan 18, 2017 · N835AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INTERCOSTAL AT BS 621 AND STRINGER 13L IS CRACKED. REMOVED & REPLACED THE INTERCOSTAL IAW SRM 51-42-21 & 51-42-22.
- [SDR REXA2017011700111](https://openairdocs.org/sdr/REXA2017011700111.md): Support Bracket · cracked · Jan 17, 2017 · N835AY · Cndair CL6002B19 · Wing Miscellaneous Structure
  > RT INBD LEADING EDGE OF WING, SUPPORT BRACKET AFT OF SPAR CAP IS CRACKED AT LOWER AFT CORNER. REMOVED AND REPLACED IAW CRJ 200 SRM 51-41-02, 51-42-06, AND 51-40-11.
- [SDR REXA2017011700110](https://openairdocs.org/sdr/REXA2017011700110.md): Attach Angle · cracked · Jan 17, 2017 · N835AY · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > ATTACH ANGLE CRACKED AT BS 473 LBL 36. REMOVED AND REPLACED THE ATTACH ANGLE IAW SRM 51-42-21.
- [SDR REXA2017011700106](https://openairdocs.org/sdr/REXA2017011700106.md): Cargo Track · corroded · Jan 17, 2017 · N835AY · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > AFT CARGO TRACK IS CORRODED AND GOUGED BS 559+80 - 559+96, RBL 9. REMOVED AND REPLACED THE CARGO TRACK IAW AMM 53-00-49 RBL-9.
- [SDR REXA2017011700105](https://openairdocs.org/sdr/REXA2017011700105.md): Cargo Track · corroded · Jan 17, 2017 · N835AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AFT CARGO TRACK IS CORRODED AND GOUGED BS 559+80 - 559+96, RBL 27. REMOVED AND REPLACED THE CARGO TRACK IAW AMM 53-00-49.
- [SDR REXA2017011600118](https://openairdocs.org/sdr/REXA2017011600118.md): Structure · cracked · Jan 16, 2017 · N835AY · Cndair CL6002B19 · APU Cowling/Containment
  > APU ENCLOSURE AFT SIDE AREAS ARE CRACKED. REPAIRED IAW REO 601R-49-11-070 REV B. REPAIREDTHE REMAINING AREAS IAW REO 601R-49-11-071.
- [SDR REXA2017011500102](https://openairdocs.org/sdr/REXA2017011500102.md): Seat Track · corroded · Jan 15, 2017 · N835AY · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT SIDEWALL SEAT TRACK IS CORRODED AND GOUGED, BS 409+111 - 444. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11.
- [SDR REXA2017011500093](https://openairdocs.org/sdr/REXA2017011500093.md): Seat Track · corroded · Jan 15, 2017 · N835AY · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT SIDEWALL SEAT TRACK IS CORRODED AND GOUGED, BS 409+112 - 449+85. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11.
- [SDR REXA2017011500089](https://openairdocs.org/sdr/REXA2017011500089.md): Seat Track · corroded · Jan 15, 2017 · N835AY · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK IS CORRODED AND GOUGED LBL 93, BS 409+126 - 559. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-11.
- [SDR REXA2017011400108](https://openairdocs.org/sdr/REXA2017011400108.md): Floorbeam · cracked · Jan 14, 2017 · N835AY · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOORBEAM BS 280 ANGLE CRACKED LBL 9. REMOVED THE ANGLE. FABRICATED, AND INSTALLED A NEW ANGLE IAW SRM 51-24-21 AND 51-42-21.
- [SDR REXA2017011400101](https://openairdocs.org/sdr/REXA2017011400101.md): Seat Track · corroded · Jan 14, 2017 · N835AY · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT SIDEWALL SEAT TRACK IS CORRODED AND GOUGED. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11.
- [SDR REXA2017011400095](https://openairdocs.org/sdr/REXA2017011400095.md): Seat Track · corroded · Jan 14, 2017 · N835AY · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT SIDEWALL SEAT TRACK IS CORRODED AND GOUGED. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11.
- [SDR REXA2017011400094](https://openairdocs.org/sdr/REXA2017011400094.md): Seat Track · corroded · Jan 14, 2017 · N835AY · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT SIDEWALL SEAT TRACK IS CORRODED AND GOUGED. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11.
- [SDR REXA2017011200104](https://openairdocs.org/sdr/REXA2017011200104.md): Cargo Track · corroded · Jan 12, 2017 · N835AY · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT SIDEWALL CARGO TRACK IS CORRODED AND GOUGED, BS 554 - 559+79 RBL 27. REMOVED AND REPLACED THE CARGO TRACK IAW AMM 53-00-49.

Next page: https://openairdocs.org/aircraft/N835AY/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 = 'N835AY' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N835AY/reports

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