# Service difficulty reports: N834AY

A list on [N834AY](https://openairdocs.org/aircraft/N834AY.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 3 · 104 reports

- [SDR REXA2022060601073](https://openairdocs.org/sdr/REXA2022060601073.md): Lamp · inoperative · May 30, 2022 · N834AY · Cndair CL6002B19 · Emergency Lighting
  > LEFT OVER WING EMERRGENCY LIGHT HAS BURNED OUT BULBS INSIDE R/R'D LEFT OVERWING EMERGENCY LIGHT BULBS IAW AMM 33-51-10, OPS CHECK GOOD.
- [SDR REXA2022060601072](https://openairdocs.org/sdr/REXA2022060601072.md): Lamp · inoperative · May 30, 2022 · N834AY · Cndair CL6002B19 · Emergency Lighting
  > RIGHT OVERWING EMERGENCY LIGHT HAS BURNED OUT BULBS INSIDE R/R'D RIGHT OVERWING EMERGENCY LIGHT BULBS IAW AMM 33-51-10, OPS CHECK GOOD.
- [SDR REXA2022060601071](https://openairdocs.org/sdr/REXA2022060601071.md): Lamp · inoperative · May 30, 2022 · N834AY · Cndair CL6002B19 · Emergency Lighting
  > SERVICE DOOR EMERGENCY FLOOD LIGHT HAS BURNED OUT BULBS R/R'D SERVICE DOOR EMERGENCY LIGHT BULBS IAW AMM 33-51-10, OPS CHECK GOOD.
- [SDR REXA2021020800063](https://openairdocs.org/sdr/REXA2021020800063.md): Bulkhead Web · cracked · Jan 29, 2021 · N834AY · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > INDICATION NOTED AT THE FS 202.75 PRESSURE BULKHEAD AT BL 23.71 BRAKE CABLE PASS THROUGH HOLE AT THE 12 O'CLOCK APPROX..100"" IN LENGTH VERTICALLY AND 100% FULL SCREEN HEIGHT FAILING NDT. REPAIRED FS 202.75 PRESSURE BULKHEAD AT PARKING BRAKE CABLE PASS THROU
- [SDR REXA2021020800061](https://openairdocs.org/sdr/REXA2021020800061.md): Bulkhead Web · cracked · Jan 29, 2021 · N834AY · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUND FS 559 RH SIDE BULKHEAD WEB OB OF RBL 9.0 WL 58.70.300 LONG 75% FSH. FAILED NDT INSPECTION. COMPLIED WITH REPAIR TO THE 559 BULKHEAD IAW EO P53025 REO 601R-53-41- 260 REV G, 601R-53-41-609 REV D AND 601R-53-41-2856 REV--.NO DEFECTS NOTED.
- [SDR REXA2021020800060](https://openairdocs.org/sdr/REXA2021020800060.md): Bulkhead Web · cracked · Jan 29, 2021 · N834AY · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUND REAR PRESSURE BULKHEAD WEB AT LBL 27.50 WL 130 HAS INDICATION NOTED TOP OF CARGO DOOR TRACK.400 LONG 80% FSH FAILED NDT INSPECTION. REPAIRED REAR PRESSURE BULKHEAD AT LBL 27.50, WL 130 IAW BOMBARDIER REO 601R-53-61-1541 REV. F, DATED 2014/11/12. THIS
- [SDR REXA2021020800062](https://openairdocs.org/sdr/REXA2021020800062.md): Attach Angle · cracked · Jan 20, 2021 · N834AY · Cndair CL6002B19 · Wing, Attach Fittings
  > ATTACH ANGLE ON LEADING EDGE 530JL IS CRACKED. DRILLED & INSTALLED ANGLE 600-12045-11 IAW SRM 51-40-11 & 51-41-02.
- [SDR REXA2021020800058](https://openairdocs.org/sdr/REXA2021020800058.md): Fitting · cracked · Jan 20, 2021 · N834AY · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CABIN FLOOR BEAM FITTING CRACKED AT FS 460 OUTBD SIDE OF RBL 9.0 BEAM. REMOVED AND REPLACED FLOORBEAM FITTING IAW CRJ 200 SRM 51-42-21 AND 51-40-11.
- [SDR REXA2021020800054](https://openairdocs.org/sdr/REXA2021020800054.md): Bracket · cracked · Jan 17, 2021 · N834AY · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > "RH MLG VOLUMETRIC FUSE MOUNT BRACKET CRACKED. "INSTALLED RH MLG VOLUMETRIC FUSE MOUNT BRACKET P/N: 601R75278-11 IAWCRJ 200 SRM 51-42-06. "
- [SDR REXA2021020800055](https://openairdocs.org/sdr/REXA2021020800055.md): Stop Fitting · cracked · Jan 16, 2021 · N834AY · Cndair CL6002B19 · Fuselage Main, Structure
  > "PAX DOOR UPPER STOP FITTING CRACKED AT FS 310 FRAME. REMOVED AND REPLACED UPPER STOP FITTING @ FS 310 PAX DOOR OPENING WITH PART #600-38087-31 IAW CRJ 200 SRM 57-42-21 REMOVED TAPE. "
- [SDR REXA2021020800059](https://openairdocs.org/sdr/REXA2021020800059.md): Angle · cracked · Jan 12, 2021 · N834AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > "CARGO DOOR SUPPORT BEAM BOTTOM ANGLE CRACKED AT FWD FACE OF FS 621 BULKHEAD WEB, WL 114. "REMOVED TAPE. REMOVED AND REPLACED ANGLE LOCATED ON CARGO DOOR SUPPORT BEAM BOTTOM AREA AT FWD FACE OF FS 621 BULKHEAD WEB, WL 114 IAW CRJ 200 SRM 51-42-20. "
- [SDR REXA2021020800057](https://openairdocs.org/sdr/REXA2021020800057.md): Fitting · cracked · Jan 12, 2021 · N834AY · Cndair CL6002B19 · Fuselage Main, Structure
  > CO-PILOTS WINDSHIELD SIDE POST BOTTOM AFT FITTING CRACKED P/N:601R33235-4. REMOVED AND REPLACED COPILOTS WINDSHIELD SIDE POST BOTTOM AFT FITTING IAW CRJ 200 SRM 51-40-11 AND 51-42-21.
- [SDR REXA2021020800056](https://openairdocs.org/sdr/REXA2021020800056.md): Fitting · cracked · Jan 12, 2021 · N834AY · Cndair CL6002B19 · Fuselage Main, Structure
  > PILOTS WINDSHIELD SIDE POST BOTTOM AFT FITTING CRACKED P/N: 601R33235-3. REMOVED AND REPLACED PILOTS WINDSHIELD SIDE POST BOTTOM AFT FITTING IAW CRJ 200 SRM 51-40-11 AND 51-42-21.
- [SDR REXA2019120211715](https://openairdocs.org/sdr/REXA2019120211715.md): Battery · discharged · Dec 1, 2019 · N834AY · Cndair CL6002B19 · Emergency Lighting
  > EMER LGTS BATTERY DEPLETED RECHARGED BATTERY WITH AIRCRAFT POWER IAW CMM 25-60-03 FOR 6 HOURS PERFORMED OPS TEST OF THE EMREGENCY LIGHTS IAW AMM 33-51-04 PERFORMED OPS TEST OF THE BATTERY PACK/CHARGER ASSY IAW AMM 33-51-00 OPS TEST PASSED A/C GOOD FOR SVC
- [SDR REXA2019040200341](https://openairdocs.org/sdr/REXA2019040200341.md): Charger · inoperative · Apr 2, 2019 · N834AY · Cndair CL6002B19 · Emergency Lighting
  > LH FWD OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED #2, PS2LF EMERGENCY BETTERY CHARGER ASSEMBLY. IAW CRJ AMM 33-51-05 OPS CHECKS GOOD AT THIS TIME.
- [SDR REXA2019030300270](https://openairdocs.org/sdr/REXA2019030300270.md): Bulkhead · dented · Mar 3, 2019 · N834AY · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > LOWER AREA OF REAR PRESSURE BULKHEAD BY LBL 9.5 HAS A LARGE DENT. REPAIRED FS621 AFT PRESSURE BULKHEAD DENT @ LBL9 LWR AREA IAW REO 601R-53-61-68-78 OPERATIONAL CK OF CARGO BAY DOOR BALANCE SPRING C/W IAW AMM 52-31-08 NO DEFECTS NOTED.
- [SDR REXA2019022600268](https://openairdocs.org/sdr/REXA2019022600268.md): Seal · worn · Feb 26, 2019 · N834AY · Cndair CL6002B19 · Engine Cowling System
  > RT ENG LWR NOSE COWL TE IS KNIFE EDGED. REMOVED/REPLACED NOSE COWL T/E IAW CMM 71-14-01.
- [SDR REXA2019022500269](https://openairdocs.org/sdr/REXA2019022500269.md): Step · cracked · Feb 25, 2019 · N834AY · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR STAIR EDGE MEMBER CRACKED ON AFT SIDE. CUTOUT DAMAGE/REPAIRED IAW REO 601R-52-11-279.
- [SDR REXA2019022200267](https://openairdocs.org/sdr/REXA2019022200267.md): Seal · chafed · Feb 22, 2019 · N834AY · Cndair CL6002B19 · Engine Collector/Tailpipe/Nozzle
  > LT TAIL PIPE FAIRING LE METAL SEAL HAS CHAFING DAMAGE. REMOVED AND REPLACED WITH NEW METAL SEAL ON LT TAIL PIPE FAIRING L/E IAW CMM 20-42-06 AND CMM 78-11-00.
- [SDR REXA2019022200261](https://openairdocs.org/sdr/REXA2019022200261.md): Retainer · cracked · Feb 22, 2019 · N834AY · Cndair CL6002B19 · Nacelle/Pylon Miscellaneous Structure
  > RT PYLON PANEL 422BT SEAL RETAINER CRACKED. REMOVED AND REPLACED PANEL 422BT SEAL RETAINER IAW SRM 51-42-06.
- [SDR REXA2019021900266](https://openairdocs.org/sdr/REXA2019021900266.md): Hinge · cracked · Feb 19, 2019 · N834AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AFT CARGO THRESHOLD HINGE BROKEN/CRACKED IN 2 AREAS. REMOVED/REPLACED HINGE IAW SRM 51-40-11-00 TR 51-42.
- [SDR REXA2019021700260](https://openairdocs.org/sdr/REXA2019021700260.md): Retainer · cracked · Feb 17, 2019 · N834AY · Cndair CL6002B19 · Nacelle/Pylon Miscellaneous Structure
  > LT PYLON PANEL 412DB SEAL RETAINER CRACKED. REMOVED/REPLACED SEAL RETAINER IAW SRM 51-42-06.
- [SDR REXA2019021400258](https://openairdocs.org/sdr/REXA2019021400258.md): Seat Track · corroded · Feb 14, 2019 · N834AY · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT HAND SEAT TRACK NR 2 HAS CORROSION. REMOVED/REPLACED SEAT TRACK IAW AMM 53-01-11 SEAT TRACK FABRICATED ON CARD#6915030 1016735 2000 0162.
- [SDR REXA2019021400256](https://openairdocs.org/sdr/REXA2019021400256.md): Panel · chafed · Feb 14, 2019 · N834AY · Cndair CL6002B19 · Wing Miscellaneous Structure
  > SUPPLEMENTAL INFORMATION. PANEL 599CB ON THE ZONE 5 PANEL RACK HAS CHAFING. REMOVED CHAFE FOUND TO BE OUT OF LIOMITS IAW SRM 57-60-00. DRILLED AND LOCATED NEW 599CB PANEL IAW SRM 51-40-11.
- [SDR REXA2019021200259](https://openairdocs.org/sdr/REXA2019021200259.md): Seat Track · corroded · Feb 12, 2019 · N834AY · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT HAND SEAT TRACK NR 3 HAS CORROSION. REMOVED/REPLACED SEAT TRACK IAW AMM 53-01-11.
- [SDR REXA2019021200257](https://openairdocs.org/sdr/REXA2019021200257.md): Seat Track · corroded · Feb 12, 2019 · N834AY · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT HAND SEAT TRACK NR 3 HAS CORROSION. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-11.
- [SDR REXA2019021000265](https://openairdocs.org/sdr/REXA2019021000265.md): Seat Track · corroded · Feb 10, 2019 · N834AY · 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 SEAT TRACK IAW AMM 53-00-49.
- [SDR REXA2019021000264](https://openairdocs.org/sdr/REXA2019021000264.md): Seat Track · corroded · Feb 10, 2019 · N834AY · 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 SEAT TRACK IAW AMM 53-00-49.
- [SDR REXA2019021000263](https://openairdocs.org/sdr/REXA2019021000263.md): Seat Track · corroded · Feb 10, 2019 · N834AY · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK ON TOP OF RBL 27 HAS CORROSION BETWEEN FS 559+80 AND FS 559+96, IN THE CARGO BAY. REMOVED AND REPLACED SEAT TRACK IAW AMM 33-00-49.
- [SDR REXA2019021000262](https://openairdocs.org/sdr/REXA2019021000262.md): Seat Track · corroded · Feb 10, 2019 · N834AY · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK ON TOP OF RBL 9 HAS CORROSION BETWEEN FS 559+80 AND FS 559+96, IN THE CARGO BAY. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-00-49.
- [SDR REXA2019021000254](https://openairdocs.org/sdr/REXA2019021000254.md): Seat Track · corroded · Feb 10, 2019 · N834AY · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT HAND SEAT TRACK NR 1 HAS CORROSION. REMOVED AND REPLACED SEAT TRACK IAW SRM 53-01-11.
- [SDR REXA2019020900255](https://openairdocs.org/sdr/REXA2019020900255.md): Seat Track · corroded · Feb 9, 2019 · N834AY · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT HAND SEAT TRACK NR 1 HAS CORROSION. REMOVED AND REPLACED SEAT TRACK STICK NR 4 IAW AMM 53-01-11-420-01.
- [SDR REXA2018070600596](https://openairdocs.org/sdr/REXA2018070600596.md): Seal · broken · Jul 5, 2018 · N834AY · Cndair CL6002B19 · Emergency Equipment
  > AFT PBE SEAL BROKEN. INSTALLED AFT PBE SEAL AS REQUIRED. A/C OK FOR SVC.
- [SDR REXA2018070600595](https://openairdocs.org/sdr/REXA2018070600595.md): Seal · missing · Jul 2, 2018 · N834AY · Cndair CL6002B19 · Emergency Equipment
  > CABIN PBE MISSING SEAL. REPLACED BROKEN SEAL ON CABIN PBE AS REQUIRED.
- [SDR REXA2017080300855](https://openairdocs.org/sdr/REXA2017080300855.md): Elt · no test · Aug 3, 2017 · N834AY · Cndair CL6002B19 · Emergency Locator Beacon
  > ELT FAILED INERTIA TEST. REMOVED AND REPLACED ELT ASSY IAW AMM 25-62-01 OPS CHECKED GOOD.
- [SDR REXA2017012900140](https://openairdocs.org/sdr/REXA2017012900140.md): Fuel · leaking · Jan 29, 2017 · N834AY · Cndair CL6002B19 · Engine Fuel Distribution
  > NR 2 ENGINE N2 LAG BEHIND DURING START DRY MOTOR ENGINE. FLAMES REPORTED AND FUEL LEAKING. RAN THE ENGINE FIRE ON THE GROUND SEVERE OR ENG FIRE CHECKLIST. ANOTHER REPORT CAME IN THAT WE WERE STILL ON FIRE. CALLED THE FIRE TRUCKS TO TAKE A LOOK. MAINTENANCE INS
- [SDR REXA2016121302467](https://openairdocs.org/sdr/REXA2016121302467.md): Seal · broken · Dec 13, 2016 · N834AY · Cndair CL6002B19 · Emergency Equipment
  > FA REPORTED THE FLASHLIGHT SEAL BROKEN. REPLACED FA FLASHLIGHT SEAL, IAW AMM 25-61-02.
- [SDR REXA2016112202289](https://openairdocs.org/sdr/REXA2016112202289.md): Vane · chafed · Nov 22, 2016 · N834AY · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT INBD FLAP VANE CHAFED. REMOVED & REPLACED THE FLAP VANE IAW SRM 51-42-13.
- [SDR REXA2016112102299](https://openairdocs.org/sdr/REXA2016112102299.md): Sign · inoperative · Nov 21, 2016 · N834AY · Cndair CL6002B19 · Emergency Lighting
  > FLOOR LEVEL EXIT SIGN AT PAX DOOR DOES NOT OPERATE WHEN TESTING EMER BATTERY PACKS 1 AND 3. PERFORMED OPS TEST OF EMERGENCY LIGHT BATTERY PACKS 1 AND 3. NO DEFECTS NOTED IAW AMM 33-51-04-740-801.
- [SDR REXA2016112102295](https://openairdocs.org/sdr/REXA2016112102295.md): Fitting · cracked · Nov 21, 2016 · N834AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > WHILE REMOVING CORROSION ON LBL27 FS 605 - FS 621 FOUND CRACK ON O/B FLANGE. REPAIRED O/B FLANGE OF FITTING AT LBL27 FS 605-621 IAW EA CRJ253-05050.
- [SDR REXA2016112002296](https://openairdocs.org/sdr/REXA2016112002296.md): Floor Support · corroded · Nov 20, 2016 · N834AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOORBOARD SUPPORT AT FS621 BETWEEN LBL27 AND LH SILL HAS CORROSION AROUND SCREW HOLES. REMOVED DAMAGE AND REPAIRED IAW REO 601R-53-61-117.
- [SDR REXA2016111902283](https://openairdocs.org/sdr/REXA2016111902283.md): Panel · cracked · Nov 19, 2016 · N834AY · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR FWD RISER PANEL IS CRACKED BY THIRD STEP. COMPLIED WITH REPAIR TO THE PAX DOOR FWD SIDE PANEL IAW REO.NO:601R-52-11-702 REV. E.
- [SDR REXA2016111902279](https://openairdocs.org/sdr/REXA2016111902279.md): Floorbeam · cracked · Nov 19, 2016 · N834AY · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOORBEAM FOUND CRACKED AT LBL 9 BS 280. REMOVED DAMAGE, FABRICATED, LOCATED, DRILLED AND INSTALLED A REPAIR IAW REO 601R-53-11-136.
- [SDR REXA2016111802280](https://openairdocs.org/sdr/REXA2016111802280.md): Bulkhead · cracked · Nov 18, 2016 · N834AY · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUND A CRACK ON THE LOWER BULKHEAD WEB RBL 9 BS 280. REMOVED DAMAGE, FABRICATED, LOCATED, DRILLED AND INSTALLED A REPAIR IAW REO 601R-53-11-171.
- [SDR REXA2016111802278](https://openairdocs.org/sdr/REXA2016111802278.md): Floorbeam · corroded · Nov 18, 2016 · N834AY · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > MAIN CABIN FLOORBEAM IS CORRODED BS 280 LBL 9 - RBL9. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-42-06.
- [SDR REXA2016111602290](https://openairdocs.org/sdr/REXA2016111602290.md): Guide Plate · cracked · Nov 16, 2016 · N834AY · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT OUTBOARD FLAP, MID HINGE, OUTBOARD FAIRING GUIDE PLATE IS CRACKED. REMOVED AND REPLACED RIGHT OUTBOARD FLAP MID HINGE OUTBOARD FAIRING GUIDE PLATE IAW SRM 51-42-06 APPLIED TOP COAT IAW SRM 51-25-16.
- [SDR REXA2016111302286](https://openairdocs.org/sdr/REXA2016111302286.md): Angle · cracked · Nov 13, 2016 · N834AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > ANGLE IS CRACKED ON THE O/B SIDE OF LBL 27 AT BS 473.15, IN CABIN BELOW FLOOR. REMOVED AND INSTALLED A NEW ANGLE IAW SRM 51-42-20.
- [SDR REXA2016111302277](https://openairdocs.org/sdr/REXA2016111302277.md): Cargo Track · corroded · Nov 13, 2016 · N834AY · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LBL 9 CARGO TRACK BETWEEN BS 613 TO 618 IS CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-61-49. INSTALLED A REPLACEMENT CARGO TRACK IAW REO 601R-53-00-485.
- [SDR REXA2016111302275](https://openairdocs.org/sdr/REXA2016111302275.md): Cargo Track · corroded · Nov 13, 2016 · N834AY · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LBL 27 CARGO TRACK BETWEEN BS 559+79 AND 559+96 HAS CORROSION. FOUND TO BE OUT OF LIMITS IAW SRM 53-61-49. REMOVED AND REPLACED THE CARGO TRACK IAW AMM 53-01-11 AND REO 601R-53-00-485.
- [SDR REXA2016111302267](https://openairdocs.org/sdr/REXA2016111302267.md): Seat Track · corroded · Nov 13, 2016 · N834AY · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LBL 9 SEAT TRACK BETWEEN BS 559+110 TO 568 IS CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-61-49. REMOVED AND REPLACED THE SEAT TRACK IAW REO-601R-53-00-485.

Next page: https://openairdocs.org/aircraft/N834AY/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 = 'N834AY' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N834AY/reports

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