# Service difficulty reports: N801AY

A list on [N801AY](https://openairdocs.org/aircraft/N801AY.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 · 106 reports

- [SDR REXA2019012500095](https://openairdocs.org/sdr/REXA2019012500095.md): Skin Panel · cracked · Jan 25, 2019 · N801AY · Cndair CL6002B19 · Wing, Plate/Skin
  > REFUEL STRUCTURE BOX AT THE RT WING FWD SPAR, O/B SKIN PANEL IS CRACKED AT THE AFT LOWER BEND RADIUS AT RBL 45. REMOVED AND REPLACED REFUEL STRUCTURE BOX AT RT FWD SPAR O/B SKIN PANEL IAW SRM 51-42-06&51-41-02.
- [SDR REXA2019012400094](https://openairdocs.org/sdr/REXA2019012400094.md): Angle · corroded · Jan 24, 2019 · N801AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PAX DOOR OPENING LOWER LONGERON ANGLE STRIP HAS CORROSION ON THE I/B AND O/B SIDE. REMOVED AND REPLACED PAX DOOR LOWER SILL ANGLE IAW SRM 51-42-06. OPERATIONAL CHECK COMPLIED WITH ON WO#1016610 8000/0011 SN 6825460.
- [SDR REXA2019011900091](https://openairdocs.org/sdr/REXA2019011900091.md): Cowling · chafed · Jan 19, 2019 · N801AY · Cndair CL6002B19 · Engine Cowling System
  > LT UPPER NOSE COWL TRAILING EDGE IS CHAFED. REPLACED AFT EDGE STRIP IAW CMM 71-14-01.
- [SDR REXA2019011700100](https://openairdocs.org/sdr/REXA2019011700100.md): Seat Track · corroded · Jan 17, 2019 · N801AY · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RT AISLE SEAT TRACKE STICK 2 HAS CORROSION SPOTS BETWEEN FS 394 THRU FS 409+128, IN THE CABIN BELOW THE FLOOR. REMOVED AND REPLACED SEAT TRACK RT FS394 - FS409 + 128 IAW AMM 53-01-11.
- [SDR REXA2019011700093](https://openairdocs.org/sdr/REXA2019011700093.md): Bracket · cracked · Jan 17, 2019 · N801AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > ANGLE CLIP IS CRACKED ON TOP OF FRAME 625.30 AND AT THE SAME LEVEL AS STR 14R, IN THE AFT EQUIPMENT BAY. REMOVED AND REPLACED CRACKED CLIP IAW SRM 51-42-21.
- [SDR REXA2019011700092](https://openairdocs.org/sdr/REXA2019011700092.md): Attach Angle · cracked · Jan 17, 2019 · N801AY · Cndair CL6002B19 · Wing, Attach Fittings
  > LT WING L/E SPAR, PNL 520JL OUTBD ATTACH ANGLE AT TRANSITION DUCT CRACKED. REMOVED AND REPLACED CRACKED ANGLE IAW SRM 51-41-02.
- [SDR REXA2019011700090](https://openairdocs.org/sdr/REXA2019011700090.md): Seat Track · corroded · Jan 17, 2019 · N801AY · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RT AISLE SEAT TRACK STICK 2 HAS CORROSION SPOTS BETWEEN FS 394 THRU FS 409+128, IN THE CABIN BELOW THE FLOOR. REMOVED AND REPLACED SEAT TRACK RT FS394 - FS409 + 128 IAW AMM 53-01-11.
- [SDR REXA2019011700089](https://openairdocs.org/sdr/REXA2019011700089.md): Angle · cracked · Jan 17, 2019 · N801AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > ANGLE CLIP IS CRACKED AT THE RT VERTICAL BEAM AT FS 202.75 TOP SIDE, IN THE NOSE GEAR BAY. REMOVED AND REPLACED ANGLE CLIP IN NLG BAY IAW SRM 51-42-21.
- [SDR REXA2019011700088](https://openairdocs.org/sdr/REXA2019011700088.md): Support Bracket · cracked · Jan 17, 2019 · N801AY · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR AFT HANDRAIL SUPPORT BRACKET IS CRACKED. REMOVED AND REPLACED HANDRAIL SUPPORT IAW SRM 51-42-21.
- [SDR REXA2019011700087](https://openairdocs.org/sdr/REXA2019011700087.md): Attach Angle · cracked · Jan 17, 2019 · N801AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > NLG BAY, ATTACH ANGLE CLIP CRACKED AT FS 200.00 RBL7. REPLACED ATTACH ANGLE CLIP IN NLG BAY AT FS 200 AND RBL 7 IAW SRM 51-42-21.
- [SDR REXA2019011700086](https://openairdocs.org/sdr/REXA2019011700086.md): Bracket · cracked · Jan 17, 2019 · N801AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > OBLIQUE ANGLE BRACKET BETWEEN AFT PRESSURE BULKHEAD AND FRAME 625.30 IN THE AFT EQUIPMENT BAY. REMOVED AND REPLACED BRACKET AT FRAME STATION 625 AND STRINGER 14L IAW SRM 51-42-21.
- [SDR REXA2019011600085](https://openairdocs.org/sdr/REXA2019011600085.md): Bracket · cracked · Jan 16, 2019 · N801AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > OBLIQUE ANGLE BRACKET BETWEEN AFT PRESSURE BULKHEAD AND FRAME 625.30IN THE AFT EQUIPMENT BAY. REMOVED AND REPLACED CRACKED BRACKET IAW SRM 51-42-21 AND 51-42-22.
- [SDR REXA2019011600084](https://openairdocs.org/sdr/REXA2019011600084.md): Skin Panel · cracked · Jan 16, 2019 · N801AY · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FUSELAGE NEAR LEFT TRU DOOR, AFT LATCH, HAS A CRACK. REPAIRED FUSELAGE SKIN AT LT TRU DOOR AFT LATCH IAW EA 253-8202REV IR.
- [SDR REXA2019011400083](https://openairdocs.org/sdr/REXA2019011400083.md): Bracket · cracked · Jan 14, 2019 · N801AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > ANGLE CLIP IS CRACKED ON TOP OF FRAME 625.30 AT THE SAME LEVEL AS STR 14L, IN THE AFT EQUIPMENT BAY. REMOVED AND REPLACED CLIP ON TOP OF FRAME 625.30 IAW SRM 51-42-06.
- [SDR REXA2019011400082](https://openairdocs.org/sdr/REXA2019011400082.md): Bracket · cracked · Jan 14, 2019 · N801AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LT MLG WW, SYS 3A HYD PRESSURE SWITCH MOUNT BRACKET CRACKED. REMOVED AND REPLACED CRACKED BRACKET IAW SRM 51-42-06.
- [SDR REXA2019011300077](https://openairdocs.org/sdr/REXA2019011300077.md): Mount Bracket · cracked · Jan 13, 2019 · N801AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT MLG W/W, SYS 3B HYD PRESSURE SWITCH MOUNT BRACKET CRACKED. REMOVED AND REPLACED CRACKED BRACKET IAW SRM 51-42-06.
- [SDR REXA2019011200075](https://openairdocs.org/sdr/REXA2019011200075.md): Splice Plate · corroded · Jan 12, 2019 · N801AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SPLICE PLATE ON FRAME 319.70 AND INTERCOSTAL ON STR 18R HAS CORROSION SPOTS, IN THE CABIN JUST ABOVE AND BELOW THE FLOOR. REMOVED CORRODED SPLICE PLATE AND REPLACED WITH NEW SPLICE PLATE IAW SRM 51-42-21.
- [SDR REXA2019011000096](https://openairdocs.org/sdr/REXA2019011000096.md): Light · missing · Jan 10, 2019 · N801AY · Cndair CL6002B19 · Emergency Lighting
  > CENTER CEILING EMER EXIT LIGHT IS MISSING SMALL WHITE LIGHT LENS AND BULB. REPLACED CNT CEILING PANEL EMER EXIT WHITE LENS AND BULB IAW AMM 33-51-14. OPS CHECK ACCOMPLISHED ON W/O 1016610-2000-0009 S/N: 6285015.
- [SDR REXA2019011000074](https://openairdocs.org/sdr/REXA2019011000074.md): Attach Angle · cracked · Jan 10, 2019 · N801AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LT FLT CONTROL CABLE FAIRLEAD BRACKET ATTACH ANGLE CLIPS, INBD AND OUTBD, AT FS 484.0 CRACKED. REMOVED DAMAGED CLIP AND FABRICATED NEW CLIP AND INSTALLED IAW SRM 51-42-21.
- [SDR REXA2019010900076](https://openairdocs.org/sdr/REXA2019010900076.md): Fitting · cracked · Jan 9, 2019 · N801AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > I/B AND O/B ANGLE CLIPS ON STR 3L IS CRACKED JUST AFT OF FRAME 280, IN THE CABIN. REMOVED AND REPLACED CRACKED CLIPS IAW SRM 51-42-06 AND 51-42-21.
- [SDR REXA2019010600080](https://openairdocs.org/sdr/REXA2019010600080.md): Seat Track · corroded · Jan 6, 2019 · N801AY · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LT SIDEWALL SEAT TRACK STICK 3 HAS CORROSION SPOTS FROM FS 409+16 THRU FS 409+112, IN THE CABIN. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-11.
- [SDR REXA2019010500079](https://openairdocs.org/sdr/REXA2019010500079.md): Seat Track · corroded · Jan 5, 2019 · N801AY · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT SIDE FLOOR SEAT TRACK CORRODED, AT APPROX STA-559.96. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-11.
- [SDR REXA2019010500078](https://openairdocs.org/sdr/REXA2019010500078.md): Seat Track · corroded · Jan 5, 2019 · N801AY · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT SIDE FLOOR SEAT TRACK, "STICK - 3 " GOUGED AND CORRODED. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-11.
- [SDR REXA2019010500071](https://openairdocs.org/sdr/REXA2019010500071.md): Seat Track · corroded · Jan 5, 2019 · N801AY · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT SIDE FLOOR SEAT TRACK, "STICK - 3 " GOUGED AND CORRODED. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-11.
- [SDR REXA2019010500070](https://openairdocs.org/sdr/REXA2019010500070.md): Seat Track · corroded · Jan 5, 2019 · N801AY · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT SIDE FLOOR SEAT TRACK, "STICK - 4 " GOUGED AND CORRODED. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-11.
- [SDR REXA2019010500068](https://openairdocs.org/sdr/REXA2019010500068.md): Seat Track · corroded · Jan 5, 2019 · N801AY · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT SIDE FLOOR SEAT TRACK, "STICK - 1 " GOUGED AND CORRODED. REMOVED ADN REPLACED WITH NEW SEAT TRACK IAW AMM 53-01-11.
- [SDR REXA2019010400072](https://openairdocs.org/sdr/REXA2019010400072.md): Panel · damaged · Jan 4, 2019 · N801AY · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > PANEL 422BB IS KNIFE EDGED AT TOP OF DIVIDER. R&R FWD AND AFT DIVIDERS IAW SRM 51-42-06.
- [SDR REXA2019010200073](https://openairdocs.org/sdr/REXA2019010200073.md): Seat Track · gouged · Jan 2, 2019 · N801AY · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT SIDE FLOOR SEAT TRACK, "STICK - 2 " GOUGED. R&R WITH NEW SEAT TRACK IAW AMM 53-01-11.
- [SDR REXA2018123001392](https://openairdocs.org/sdr/REXA2018123001392.md): Seat Track · corroded · Dec 30, 2018 · N801AY · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT SIDE FLOOR SEAT TRACK, "STICK - 2 " GOUGED AND CORRODED. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-11.
- [SDR REXA2018122901391](https://openairdocs.org/sdr/REXA2018122901391.md): Support Bracket · cracked · Dec 29, 2018 · N801AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT OVERWING SUPPORT BRACKET IS CRACKED ON BOTH SIDES OF BRACKET NEAR FS409+128. SEE STREAMER. REMOVED CRACKED BRACKET IAW SRM 51-72-86. FABRICATED NEW BRACKET IAW SRM 51-24-36. APPLIED FINISH IAW SRM 51-25.
- [SDR REXA2018120101248](https://openairdocs.org/sdr/REXA2018120101248.md): Seat Track · corroded · Dec 1, 2018 · N801AY · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RT SIDEWALL SEAT TRACK STICK 6 HAS CORROSION SPOTS, IN THE CABIN. REMOVED AND REPLACED RT SIDEWALL SEAT TRACK STICK 6 IAW AMM 53-01-11.
- [SDR REXA2018100500931](https://openairdocs.org/sdr/REXA2018100500931.md): Battery · discharged · Oct 4, 2018 · N801AY · Cndair CL6002B19 · Emergency Equipment
  > F/A EMER FLASHLIGHT OUT OF SERVICE. REPLACED FWD F.A. FLASH LIGHT BATTERY AS REQUIRED. OPS TEST GOOD. REF: AMM 25-61-00.
- [SDR REXA2018081650702](https://openairdocs.org/sdr/REXA2018081650702.md): Apu · seized · Aug 15, 2018 · N801AY · Cndair CL6002B19 · APU Core Engine
  > APU AUTO SHUTDOWN WITH NO INDICATIONS OTHER THAN A BAD ODOR. R & R THE APU IAW 200-49-10-00. PERFORMED A LEAK CHECK AND OPS CHECK, BOTH CHECKS WERE GOOD. ACFT OK FOR SERVICE.
- [SDR REXA2018072400643](https://openairdocs.org/sdr/REXA2018072400643.md): Bulkhead · cracked · Jul 22, 2018 · N801AY · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUND A CRACK IN THE REAR PRESSURE BULKHEAD WEB FACE AT THE MACHINED FITTING IB 0.25" L. COMPLETED REPAIR TO REAR PRESSURE BULKHEAD NEAR LINTLE AREA FITTING AT FS 621 IAW REO 601R-53-61-1230 REV F. NDT COMPLIED WITH.
- [SDR REXA2018061300488](https://openairdocs.org/sdr/REXA2018061300488.md): Pbe · unserviceable · Jun 13, 2018 · N801AY · Cndair CL6002B19 · Emergency Equipment
  > DURING INSPECTION NOTED WARDROBE PBE PACKAGE HAS LOST VACUUM SEAL. REMOVED & REPLACED WARDROBE PBE IAW AMM CH 35-30-00. P/N OFF/ON: MR-10042N. NO S/N OFF/ON.
- [SDR REXA2017102201115](https://openairdocs.org/sdr/REXA2017102201115.md): Pbe · damaged · Oct 22, 2017 · N801AY · Cndair CL6002B19 · Emergency Equipment
  > COCKPIT PBE HAS LOST VACUUM ON PACKAGE. REMOVED AND REPLACED COCKPIT PBE IAW AMM 35-30-00.
- [SDR REXA2017080400856](https://openairdocs.org/sdr/REXA2017080400856.md): Element · inoperative · Aug 4, 2017 · N801AY · Cndair CL6002B19 · Overheat Detection
  > RT 14TH STAGE BLEED WARNING AT FL 280 PERFORMED QRHM MESSAGE DID NOT GO OUT, CLOSED 4 14TH STAGE BLEED, OPENED ISOLATION VALVE REDUCED RT THRUST TO IDLE. LANDED FLAPS 20. R & R PYLON SENSING ELEMENT ON RT SIDE LOOP A58WK IAW AMM 36-21-04. OPS CHECKED GOOD.
- [SDR REXA2017042800556](https://openairdocs.org/sdr/REXA2017042800556.md): Actuator · inoperative · Apr 28, 2017 · N801AY · Cndair CL6002B19 · Trailing Edge Flap Actuator
  > FLAP FAIL OCCURRED IN FLIGHT APPROX 40 MIN INTO FLIGHT WHILE SELECTING FLAPS FROM 30 TO 45 FLAPS STOPPED AT 36 AIRSPEED 160KTS OAT 12C FOLLOWED QRH SELECTED FLAPS TO 30 LEFT AND RT FLAPS REMAINED AT 36. UNDER DIRECTION OF MOC PERFORMED FLAP FAIL RESET IAW FIM
- [SDR REXA2017031200347](https://openairdocs.org/sdr/REXA2017031200347.md): Bulb · inoperative · Mar 12, 2017 · N801AY · Cndair CL6002B19 · Emergency Lighting
  > PAX CALL SIGN LIGHT FRONT SIDE MID CABIN EXIT SIGN OUT. R & R THE BULB IAW AMM 33-51-14. OPS CHECKED GOOD. OK FOR SERVICE
- [SDR REXA2017021500241](https://openairdocs.org/sdr/REXA2017021500241.md): Flap System · inoperative · Feb 15, 2017 · N801AY · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAIL CAUTION MESSAGE AT 3500FT MSL, 200KT, GEAR DOWN PERFORMED TROUBLESHOOTING IAW FIM REV. 52. REPLACED THE RT OTBD FLAP ACTUATOR, RT BPSU, AND RT NR 5 FLEX DRIVE SHAFT DUE TO UNUSUAL NOISE IAW AMM 27-53-10, 27-51-10,,AND 2753-05.
- [SDR REXA2016101401928](https://openairdocs.org/sdr/REXA2016101401928.md): Strut · defective · Oct 14, 2016 · N801AY · Cndair CL6002B19 · Nose/Tail Landing Gear Strut/Axle
  > ON T/O AT "GEAR UP" NOSE DOOR OPEN WARNING, RAN QRH. PUT GEAR DOWN, ALL GREEN. DEFERRED LANDING GEAR RETRACTION SYS. NOTIFIED PINS SAFTIED AND INSTALLED MMO2 UPDATED FLAGS REMOVED. R&R NLG DRESSED ASSY IAW JOB CARD 200-32-21-02. OPS + FUNCTIONAL CHEC K G
- [SDR REXA2016092101805](https://openairdocs.org/sdr/REXA2016092101805.md): Oxygen Bottle · damaged · Sep 21, 2016 · N801AY · Cndair CL6002B19 · Portable Oxygen System
  > PORTABLE OXYGEN BOTTLE KNOB BROKEN OFF. REPLACED THE OXYGEN BOTTLE IAW AMM 35-30-00
- [SDR REXA2016080101452](https://openairdocs.org/sdr/REXA2016080101452.md): Bulkhead · gouged · Aug 1, 2016 · N801AY · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > GOUGE ON AFT PRESSURE BULKHEAD FS 621, LBL 17.5 30" ABOVE FLOOR WENT OUT OF LIMITS AND REQUIRES REPAIR. REPAIRED APB LBL 17.5 30" ABOVE FLOOR IAW REO 601R-53-61-1285, REV D. PERFORMED OPS TEST, OPS TEST GOOD IAW AMM 74-30-400-801, STEP 4D.
- [SDR REXA2016080101451](https://openairdocs.org/sdr/REXA2016080101451.md): Door Sill · corroded · Aug 1, 2016 · N801AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LT FLOOR SILL FROM FS 621-559+112 IS CORRODED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS FROM STA 596-598. ALL OTHER AREAS IN LIMITS IAW REO 601R-53-00-526, REPAIRED FLOORSILL STA 596-598 IAW EA CRJ253-04611, REV IR.
- [SDR REXA2016073101450](https://openairdocs.org/sdr/REXA2016073101450.md): Bulkhead · gouged · Jul 31, 2016 · N801AY · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > GOUGE ON AFT PRESSURE BULKHEAD FS 621, LBL 27, 30" ABOVE FLOOR, OUT OF LIMITS AND REQUIRES REPAIR. REPAIRED FS 621 AFT PRESSURE BULKHEAD AT LBL27, 30" ABOVE FLOOR IAW REO 601R-53-61-1285, REV D.
- [SDR REXA2016073101449](https://openairdocs.org/sdr/REXA2016073101449.md): Floorbeam · corroded · Jul 31, 2016 · N801AY · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOORBEAM AT LBL 27 AND FS 610 AND 559+112 HAS CORROSION ON BOTH INBD AND OTBD LANDINGS. R & R FLOORBEAM, CAP, LBL27, FROM FS 559+112-FS 610 IAW SRM 51-42-21, & SRM 51-42-24.
- [SDR REXA2016073001453](https://openairdocs.org/sdr/REXA2016073001453.md): Door · obstructed · Jul 30, 2016 · N801AY · Cndair CL6002B19 · Emergency Exits
  > RIGHT OVERWING EMERGENCY DOOR WILL NOT OPEN AT ALL. NEEDS EVALUATION. UPON FURTHER EVALUATION FOUND PROBLEM TO BE EXCESSIVE PAINT BUILD UP, OPENED DOOR AND PERFORMED OPS TEST, OPS TEST GOOD IAW AMM 52-21-00-710-801.
- [SDR REXA2016072901444](https://openairdocs.org/sdr/REXA2016072901444.md): Bulkhead · cracked · Jul 29, 2016 · N801AY · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > 621 REAR PRESSURE BULKHEAD FORWARD SIDE IS CRACKED AT TOP OF CARGO DOOR TRACK. REPAIRED 621 REAR PRESSURE BULKHEAD FORWARD SIDE AT TOP OF CARGO DOOR TRACK IAW REO 601R-53-61-1541, REV F.
- [SDR REXA2016072901443](https://openairdocs.org/sdr/REXA2016072901443.md): Seat Track · corroded · Jul 29, 2016 · N801AY · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > IN MAIN CABIN SIDEWALL SEAT RAILS ON LEFT SIDE NR 5-7 ARE CORRODED AND GOUGED IN MULTIPLE AREAS. R & R LT SIDE SEAT RAILS NR 5 TO NR 7 IAW AMM 53-01-11, PAR 2A AND PAR 3A.
- [SDR REXA2016072801447](https://openairdocs.org/sdr/REXA2016072801447.md): Frame · cracked · Jul 28, 2016 · N801AY · Cndair CL6002B19 · Fuselage Main, Frame
  > FS 333, FRAME IS CRACKED ADJACENT TO STR 1L. REPAIRED CRACK IN FS 333 AT STR 1L IAW REO 601R-53-21-2740.

Next page: https://openairdocs.org/aircraft/N801AY/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 = 'N801AY' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N801AY/reports

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