# Service difficulty reports: N840AY

A list on [N840AY](https://openairdocs.org/aircraft/N840AY.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 · 80 reports

- [SDR REXA2022050300758](https://openairdocs.org/sdr/REXA2022050300758.md): Pump · inoperative · Apr 27, 2022 · N840AY · Cndair CL6002B19 · Turbine Engine Air Inlet Section
  > ON TAKE OFF WE WENT TO SET TAKE OFF THRUST TO 85.2% N1 THE FO SET IT TO 85.2% N1 THEN IT DROPPED APPROX 10% N1 ON RT ENG THEN HE PUSHED THE THRUST BACK UP TO 85% THEN IT DROPPED BACK DOWN AGAIN APPROX 10% WE BOTH CALLED ABORT @ ABOUT 70-75 KTS ON TAXI BACK TO
- [SDR REXA2021031100120](https://openairdocs.org/sdr/REXA2021031100120.md): Skin · dented · Feb 16, 2021 · N840AY · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FOUND DENT ON RIGHT AFT FUSELAGE JUST AFT OF FS 700.0 BETWEEN STRINGERS 18R AND 17R. REPAIRED DENT ON RH SIDE OF FUSELAGE JUST AFT OF F.S 700.0 BETWEEN R 18R AND 17R IAW CRJ 200 SRM 53-00-31.
- [SDR REXA2021031100118](https://openairdocs.org/sdr/REXA2021031100118.md): Bulkhead Web · damaged · Feb 16, 2021 · N840AY · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FWD FACE BS 621 BULK HEAD HAS 18 SCREW SHANK MARKS ON SKIN & RIVET HEADS. REPAIRED FWD FACE OF F.S 621 BULKHEAD (18EA) ARCAB IAW MHI REO 601R-53-61-7570.
- [SDR REXA2021031100115](https://openairdocs.org/sdr/REXA2021031100115.md): Bracket · cracked · Feb 5, 2021 · N840AY · Cndair CL6002B19 · Nacelle/Pylon, Main Frame
  > LH PYLON HAS A CRACKED BRACKET "REPAIRED LH PYLON INTERVAL (BRACKET) IAW ENDEAVOR AIR E.A. NO. CRT 258-11191 "
- [SDR REXA2021032400119](https://openairdocs.org/sdr/REXA2021032400119.md): Frame · corroded · Feb 4, 2021 · N840AY · Cndair CL6002B19 · Fuselage Main, Frame
  > F.S 333 FRAME HAS CORROSION ON FWD SIDE AT STGR 26L. FLOOR BOARD SUPPORT FOUND TO BE OUT OF LIMITS. " REMOVED CORROSION IAW CRJ 200 SRM 51-21-06 FOUND TO BE WITHIN LIMITS IAW CRJ 200 SRM 53-00-00 REAPPLIED TOPCOAT PER SRM 51-21-11 51-25-06 AND 51-25-16. REMOVE
- [SDR REXA2021031100117](https://openairdocs.org/sdr/REXA2021031100117.md): Retaining Clip · cracked · Jan 29, 2021 · N840AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > F.S 280 RBL 9 OB CLIP IS CRACKED "REMOVED AND REPLACED F.S 280 RBL 9 OB CLIP IAW CRJ 200 SRM 51-24-16 AND 51-42-21 "
- [SDR REXA2021031100116](https://openairdocs.org/sdr/REXA2021031100116.md): Retainer · cracked · Jan 28, 2021 · N840AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 484 RBL 22 OB CLIP IS CRACKED REMOVED AND REPLACED CLIP IAW CRJ 200 SRM 51-42-21
- [SDR REXA2020030500322](https://openairdocs.org/sdr/REXA2020030500322.md): Light · inoperative · Mar 4, 2020 · N840AY · Cndair CL6002B19 · Emergency Lighting
  > DURING WALK-AROUND FOUND EXTERIOR EMERGENCY LIGHT 3 INOP (FS 406+120.50L) RELAMPED EXTERIOR EMERGENCY LIGHT 3 IAW AMM 33-51-21, OPERATIONAL TEST GOOD, NO DEFECTS NOTED AT THIS TIME. P/N 1317
- [SDR REXA2019101061412](https://openairdocs.org/sdr/REXA2019101061412.md): Striker · bent · Oct 6, 2019 · N840AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PASSENGER DOOR SEAL STRIKER AT FS 310.00 STGR 8L PREVIOUS REPAIR IS DAMAGED. INCLUDES 8804031/235. REMOVED PREVIOUS REPAIR, FOUND ELONGATED HOLES. REPLACED FWD SEAL STRIKER AT FS 310.00 STGR 8L IAW CRJ 200 SRM 51-42-06 & 51-42-21. OPS/LEAK CHECK GOOD.
- [SDR REXA2019101041405](https://openairdocs.org/sdr/REXA2019101041405.md): Floor Support · corroded · Oct 4, 2019 · N840AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RH FLOOR SILL CORRODED AROUND FLOORBOARD FASTENER HOLES BTWN FS 559+80 AND FS 621. INCLUDES 8804031/221. BLENDED FLOOR SILL RH AT FS 574-621 AND FOUND TO BE WITHIN LIMITS AND REPLACED RH FLOOR SILL AT 559+80 - 559+112 IAW BSC REO 601R-53-00-526 AND SRM 51-42-
- [SDR REXA2019101031404](https://openairdocs.org/sdr/REXA2019101031404.md): Stiffener · cracked · Oct 3, 2019 · N840AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > VERTICAL BEAM ON FRAME 409.00+128 AT RBL 18.0 SHOWS EVIDENCE OF A CRACK IN BOTTOM RADIUS OB SIDE OF BEAM. R/R 409+128 POST AT RBL 18.0 IAW BSC REO 601R-53-41-889 REV B.
- [SDR REXA2019101091413](https://openairdocs.org/sdr/REXA2019101091413.md): Seat Track · corroded · Sep 29, 2019 · N840AY · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LH SIDE SEAT RAIL CORRODED BETWEEN FS 364 AND FS 409.00+18.02. REMOVED & REPLACED LH SIDE SEAT RAIL BETWEEN FS 364 AND FS 409.00+18.02 WITH A NEW SERVICEABLE SEAT RAIL PN 601R38312-31 IAW CRJ 200 AMM 53-01-11-000-802 AND 53-01-11-400-802.
- [SDR REXA2019101091398](https://openairdocs.org/sdr/REXA2019101091398.md): Seat Track · corroded · Sep 27, 2019 · N840AY · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RH SIDE SEAT RAIL CORRODED BETWEEN FS 364 AND FS 409.00+18.02. R/R SIDE SEAT RAIL RH BETWEEN FS 364 AND FS 409+1.02 IAW CRJ 200 AMM 53-01-11-400-802. NO DEFECTS NOTED. PN 601R38312-31. WVAC EMP 722 STAMP
- [SDR REXA2019101091414](https://openairdocs.org/sdr/REXA2019101091414.md): Seat Track · corroded · Sep 26, 2019 · N840AY · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RH SIDE SEAT RAIL CORRODED BETWEEN FS 535.02 & FS 559.00+79. REMOVED AND REPLACED SEAT TRACK IAW CRJ 200 AMM 53-01-11-400-802.
- [SDR REXA2019101091401](https://openairdocs.org/sdr/REXA2019101091401.md): Seat Track · corroded · Sep 25, 2019 · N840AY · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LH SIDE SEAT RAIL CORRODED BETWEEN FS 495.98 AND FS 535.02. REPALCED SEAT TRACK IAW GREO 601R-53-00-055.
- [SDR REXA2019101091400](https://openairdocs.org/sdr/REXA2019101091400.md): Seat Track · corroded · Sep 25, 2019 · N840AY · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LH SIDE SEAT RAIL CORRODED BETWEEN FS 444.02 AND FS 495.98. REMOVED AND REPLACED L/H SIDE SEAT RAIL BETWEEN FS 444.02 AND FS 495.98 WITH A NEW SERVICEABLE RAIL P/N 601R38312-115S IAW CRJ200 AMM 53-01-11-000-802 AND 53-01-11-400-802.
- [SDR REXA2019101091409](https://openairdocs.org/sdr/REXA2019101091409.md): Seat Track · corroded · Sep 24, 2019 · N840AY · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LH SIDE SEAT RAIL CORRODED BETWEEN FS 409.00+18.02 AND FS 409.00+111.02. REMOVED AND REPLACED L/H SIDE SEAT RAIL BETWEEN FS 409.00+18.02 AND FS 409.00+111.02 IAW BOMBARDIER REO #601R-53-00-055, STEPS 1 THRU 3 REPAIR ""B"" COMPLETE SEGMENT REPLACEMENT REV C DA
- [SDR REXA2019101091408](https://openairdocs.org/sdr/REXA2019101091408.md): Seat Track · corroded · Sep 24, 2019 · N840AY · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RH SIDE SEAT RAIL CORRODED BETWEEN FS 409.00+18.02 AND FS 409.00+111.02. REMOVED AND REPLACED R/H SEAT RAIL BETWEEN FS 409.00+18.02 AND FS 409.00+111.02 IAW BOMBARDIER REO NO. 601R-53-00-055 REV C DATED 2017-03-21 STEPS 1 TO 3 (REPAIR ""B"" COMPLETE SEGMENT R
- [SDR REXA201910101407](https://openairdocs.org/sdr/REXA201910101407.md): Seat Track · corroded · Sep 24, 2019 · N840AY · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LH SIDE SEAT RAIL CORRODED BETWEEN FS 409.00+111.02 AND FS 444.02. REMOVED AND REPLACED L/H SIDE SEAT RAIL BETWEEN FS 409.00+111.02 AND FS 444.02 WITH A NEW SERVICEABLE SEAT RAIL IAW CRJ200 AMM 53-01-11-000-802 AND 53-01-11-400-802 P/N 601R38312-119S.
- [SDR REXA2019101091406](https://openairdocs.org/sdr/REXA2019101091406.md): Seat Track · corroded · Sep 24, 2019 · N840AY · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LH SIDE SEAT RAIL CORRODED BETWEEN FS 535.02 AND FS 559.00+79. REMOVED AND REPLACED LH SIDE SEAT RAIL BETWEEN FS 535.02 AND FS 559.00+79 IAW BOMBARDIER REO 601R-53-00-55.
- [SDR REXA2019101091403](https://openairdocs.org/sdr/REXA2019101091403.md): Bracket · cracked · Sep 24, 2019 · N840AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > HYD SYS #3 PRESSURE TRANSDUCER BRACKET CRACKED IN RH MLG WHEEL WELL CEILING FS 528, RBL 18-27. REMOVED DAMAGED HYD STS #3 PRESSURE TRANSDUCER BRACKET AND REPLACED WITH NEW ITEM PN601R752662-157 IAW CRJ 200 SRM 51-42-06.
- [SDR REXA2019101091402](https://openairdocs.org/sdr/REXA2019101091402.md): Seat Track · corroded · Sep 24, 2019 · N840AY · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LH SIDE SEAT RAIL CORRODED BETWEEN FS 409.00+111.02 AND FS 444.02 REMOVED AND REPLACED L/H SIDE SEAT RAIL BETWEEN FS 409.00+111.02 AND FS 444.02 WITH A NEW SERVICEABLE SEAT RAIL IAW CRJ200 AMM 53-01-11-000-802 AND 53-01-11-400-802 P/N 601R38312-119S.
- [SDR REXA2019101091399](https://openairdocs.org/sdr/REXA2019101091399.md): Seat Track · corroded · Sep 24, 2019 · N840AY · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LH SIDE SEAT RAIL CORRODED BETWEEN FS 535.02 AND FS 559.00+79. REMOVED AND REPLACED LH SIDE SEAT RAIL BETWEEN FS 535.02 AND FS 559.00+79 IAW BOMBARDIER REO 601R-53-00-55. WVAC EMP STAMP 769
- [SDR REXA2019101091397](https://openairdocs.org/sdr/REXA2019101091397.md): Channel · cracked · Sep 24, 2019 · N840AY · Cndair CL6002B19 · Vertical Stabilizer
  > VERTICAL STAB LEADING EDGE PANEL 324AT INNER WEB DAMAGE AT BOTTOM OF LEADING EDGE AND SEVERAL RIVETS PULLED THROUGH. REMOVED AND REPLACED CHANNEL ON L/E OF VERTICAL STAB IAW CRJ200 SRM 51-42-06. WVAC EMP STAMP 771
- [SDR REXA2019101091411](https://openairdocs.org/sdr/REXA2019101091411.md): Fitting · cracked · Sep 19, 2019 · N840AY · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > RH WINDSHIELD SIDE POST OB FITTING IS CRACKED. REMOVED & REPLACED CRACKED RH WINDSHIELD SIDE POST LOWER FITTING WITH A NEW SERVICEABLE SID EPOST LOWER FITTING PN 601R33235-3S IAW SRM 51-42-21.
- [SDR REXA201910101410](https://openairdocs.org/sdr/REXA201910101410.md): Fitting · cracked · Sep 19, 2019 · N840AY · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > LH WINDSHIELD SIDE POST LOWER OB FITTING IS CRACKED. REMOVED & REPLACED CRACKED LH WINDSHIELD SIDE POST LOWER FITTING WITH A NEW SERVICEABLE SIDE POST LOWER FITTING IAW CRJ 200 SRM 51-42-21. PN 601R33235-4S.
- [SDR REXA2018081390682](https://openairdocs.org/sdr/REXA2018081390682.md): Oxygen Mask · failed · Aug 9, 2018 · N840AY · Cndair CL6002B19 · Crew Oxygen System
  > FIRST OFFICER`S OXYGEN MASK HEAD BAND WONT INFLATE AND FAILED A FFOD TEST. REMOVED AND REPLACED THE OXYGEN STOWAGE BOX AND MASK IAW AMM 35-11-15, OPS CHECKED GOOD, NO DEFECTS NOTED.
- [SDR REXA2018070600597](https://openairdocs.org/sdr/REXA2018070600597.md): Light · inoperative · Jul 5, 2018 · N840AY · Cndair CL6002B19 · Emergency Lighting
  > SECOND EMERGENCY LIGHT ON THE CEILING BY ROW 5 IS OUT. RELAMPED SECOND EMERGENCY LIGHT LAW AMM 33-51-16. OPS CHECK GOOD NO DEFECTS NOTED AT THIS TIME.
- [SDR REXA2018032800230](https://openairdocs.org/sdr/REXA2018032800230.md): Unknown · smoke · Mar 28, 2018 · N840AY · Cndair CL6002B19 · Air Distribution System
  > AFTER LANDING, ON TURNING ONTO TAXIWAY, COCKPIT FILLED WITH SMOKE. SMOKE AND BURNING ODOR REPORTED IN CABIN. THERE WAS NO HEAVY BRAKING ON LANDING. FIRE DEPARTMENT INSPECTED THE AIRCRAFT. NO EVIDENCE OF SMOKE OR FIRE. TAXIED TO THE GATE. INSPECTED THE A
- [SDR REXA2018032100216](https://openairdocs.org/sdr/REXA2018032100216.md): Oxygen Mask · no test · Mar 21, 2018 · N840AY · Cndair CL6002B19 · Crew Oxygen System
  > FIRST OFFICER`S OXYGEN MASK TEST BUTTON FAILED. R & R THE OXYGEN BOX IAW AMM 35-11-15. OPS CHECKED GOOD. SERVICED CREW OXYGEN TO 1780 PSI IAW AMM 12-16-35.
- [SDR REXA2017110501151](https://openairdocs.org/sdr/REXA2017110501151.md): Lamp · burned out · Nov 5, 2017 · N840AY · Cndair CL6002B19 · Emergency Lighting
  > LEFT FORWARD EMERGENCY LIGHT BURNED OUT. REPLACED THE LAMPS IAW AMM 33-51-21.OPS CHECKED GOOD.
- [SDR REXA2017110301140](https://openairdocs.org/sdr/REXA2017110301140.md): Gear · defective · Nov 3, 2017 · N840AY · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > GEAR DISAGREE ON DEPARTURE. NOSE GEAR STAYED DOWN. PERFORMED QRH. LANDED WITHOUT INCIDENT. PERFORMED QRH. MESSAGE CLEARED, LANDED WITHOUT DISCREPANCY.
- [SDR REXA2017092701036](https://openairdocs.org/sdr/REXA2017092701036.md): Duct · loose · Sep 27, 2017 · N840AY · Cndair CL6002B19 · APU Bleed Air System
  > JUST AFTER ROTATION, APU FIRE WARNING ACTIVATED. RAN QRH, INDICATION PERSISTED FOR A FEW MINUTES AFTER BOTTLE DISCHARGE. APU FIRE FAIL & APU FIRE INDICATIONS PERSISTED INTERMITTENTLY THROUGHOUT FLIGHT. FOUND LOOSE DUCT TO UPPER ATTACHMENT OF APU LCV. REA
- [SDR REXA2017061900718](https://openairdocs.org/sdr/REXA2017061900718.md): Oxygen Mask · leaking · Jun 19, 2017 · N840AY · Cndair CL6002B19 · Crew Oxygen System
  > FIRST OFFICER`S OXYGEN MASK IS LEAKING. REMOVED AND REPLACED THE OXYGEN MASK IAW AMM 35-11-12-500-801. OPS AND LEAK CHECKED GOOD.
- [SDR REXA2017032800404](https://openairdocs.org/sdr/REXA2017032800404.md): Unknown · odor · Mar 28, 2017 · N840AY · Cndair CL6002B19 · Air Distribution System
  > STARTED APU ON APPROACH CHECK AT 10,000' GOT VERY FOUL SMELL IN CABIN + COCKPIT, BUT ALL INDICATIONS WERE NORMAL. SHUTDOWN APU AND SMELL WENT AWAY LANDED W/ NO ISSUES. INSPECTED APU ENCLOSURE FOR LEAKS AND NO LEAKS NOTED AND PERFORMED ADJ/ TEST OF APU IAW AMM
- [SDR REXA2017020600184](https://openairdocs.org/sdr/REXA2017020600184.md): Bulkhead Web · chafed · Feb 6, 2017 · N840AY · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > CARGO AFT BULKHEAD CHAFED IN SEVERAL PLACES BS 621. REMOVED DAMAGE IAW SRM 51-12-00.
- [SDR REXA2017020600183](https://openairdocs.org/sdr/REXA2017020600183.md): Bulkhead Web · scratched · Feb 6, 2017 · N840AY · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > CARGO AFT BULKHEAD FWD FACE SCRATCHED, RT 12 INCHES ABOVE FLOOR, 8 INCHES INBD OF FUSELAGE. REMOVED DAMAGE IAW SRM 51-12-00. FOUND TO BE WITHIN LIMITS IAW REO #601R-53-61-5924.
- [SDR REXA2017020600174](https://openairdocs.org/sdr/REXA2017020600174.md): Door Sill · corroded · Feb 6, 2017 · N840AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PAX DOOR OPENING LOWER FRAME, LOWER ANGLE HAS CORROSION SPOTS ON THE INBD AND OTBD SIDE BETWEEN BS 310 AND 349. REMOVED AND REPLACED THE LOWER SILL ANGLE IAW SRM 51-42-21 AND 51-42-06.
- [SDR REXA2017020600173](https://openairdocs.org/sdr/REXA2017020600173.md): Bulkhead · cracked · Feb 6, 2017 · N840AY · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > BS 202 BULKHEAD HAS CRACKS AT BRAKE CABLE PASS THRU HOLE. REPAIR THE BULKHEAD IAW REO 601R-53-11-563.
- [SDR REXA2017020300182](https://openairdocs.org/sdr/REXA2017020300182.md): Stiffener · cracked · Feb 3, 2017 · N840AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AFT ACCESSORY BAY, LT SIDE VERTICAL STIFFENERS, OTBD ANGLE IS CRACKED ADJACENT TO STRINGER 15L. REMOVED AND REPLACED THE STIFFENER IAW SRM 51-42-21.
- [SDR REXA2017020300181](https://openairdocs.org/sdr/REXA2017020300181.md): Intercostal · cracked · Feb 3, 2017 · N840AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > BS 621 - 625 INTERCOSTAL ANGLE AT STRINGER 14L FOUND CRACKED. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-42-06, 51-42-21, AND 51-42-22.
- [SDR REXA2017020300179](https://openairdocs.org/sdr/REXA2017020300179.md): Skin · dented · Feb 3, 2017 · N840AY · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBD FLAP LOWER SKIN HAS FOUR DENTS ON INBD SIDE. REMOVED AND REPLACED THE FLAP SKIN IAW SRM 57-52-00, 51-40-11, & 51-42-13,
- [SDR REXA2017020200177](https://openairdocs.org/sdr/REXA2017020200177.md): Structure · bent · Feb 2, 2017 · N840AY · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBD FLAP, TRAILING EDGE IS BENT IN TWO PLACES ON INBD AREA. REMOVED & REPLACED THE FLAP TRAILING EDGE IAW SRM 51-42-12.
- [SDR REXA2017012900178](https://openairdocs.org/sdr/REXA2017012900178.md): Rib · damaged · Jan 29, 2017 · N840AY · Cndair CL6002B19 · Trailing Edge Flaps
  > UPON REMOVAL OF LT LOWER INBD SKIN FOUND TWO DAMAGED RIBS. REMOVED & REPLACED THE RIBS IAW SRM 51-42-06.
- [SDR REXA2017012500176](https://openairdocs.org/sdr/REXA2017012500176.md): Seat Track · corroded · Jan 25, 2017 · N840AY · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > IN PASSENGER CABIN RIGHT SIDEWALL SEAT TRACK NR 5 IS CORRODED AND GOUGED. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11.
- [SDR REXA2017012500175](https://openairdocs.org/sdr/REXA2017012500175.md): Seat Track · corroded · Jan 25, 2017 · N840AY · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > IN PASSENGER CABIN RIGHT SIDEWALL SEAT TRACK NR 4 IS CORRODED AND GOUGED. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11.
- [SDR REXA2017010800013](https://openairdocs.org/sdr/REXA2017010800013.md): Defibrillator · discharged · Jan 8, 2017 · N840AY · Cndair CL6002B19 · Emergency Equipment
  > AED NOT CHARGED IAW FA. INSTALLED SERVICEABLE AED. OK FOR SERVICE.
- [SDR REXA2016101001920](https://openairdocs.org/sdr/REXA2016101001920.md): Lamp · inoperative · Oct 10, 2016 · N840AY · Cndair CL6002B19 · Emergency Lighting
  > DURING WAKE UP CHECK, FOUND EMERGENCY LIGHT NR 6 OUT. REPLACED THE LAMPS IAW AMM 33-51-21, OPS TESTED GOOD.
- [SDR REXA2016080901529](https://openairdocs.org/sdr/REXA2016080901529.md): Clamp · loose · Aug 9, 2016 · N840AY · Cndair CL6002B19 · Pneumatic Distribution System
  > AFTER TAKE OFF, WITH BLEEDS ON THE ENGINE. 10TH DUCT WARNING MESSAGE. QRH COMPLETED. NORMAL LANDING AFTER DIVERSION. LEAKS FOUND COMING FROM ACM CLAMPS FOUND BOLTS ON ACM FRONT HOUSING LOOSE & THE CLAMPS FOR ACM NR 1 DUCTING LOOSE AS WELL. ALL BOLTS & CLA
- [SDR REXA2016050200697](https://openairdocs.org/sdr/REXA2016050200697.md): Life Vest · torn · May 2, 2016 · N840AY · Cndair CL6002B19 · Life Jacket
  > ONE EACH INFANT LIFE VEST & FLIGHT ATTENDANT LIFE VEST TORN. R & R ONE EACH INFANT & FLIGHT ATTENDANT LIFE VEST IAW AMM 25-61-03 & IAW PA 25-096A.

Next page: https://openairdocs.org/aircraft/N840AY/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 = 'N840AY' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N840AY/reports

---
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.