# Service difficulty reports: N837AS, cancelled Jun 8, 2017

A list on [N837AS, cancelled Jun 8, 2017](https://openairdocs.org/deregistered/N837AS-2017-06-08.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 · 125 reports

- [SDR ASOA2015021312223](https://openairdocs.org/sdr/ASOA2015021312223.md): Isolator · broken · Feb 9, 2015 · N837AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD ISOLATOR ABOVE WL 73.50 ON RBL 9.50 IS BROKEN. REMOVED DEFECTIVE ISOLATOR AND INSTALLED NEW ISOLATOR IAW SRM 51-42-13. REPAIR CLASSIFIED AS MINOR IAW GMM 5-3.
- [SDR ASOA2015021312222](https://openairdocs.org/sdr/ASOA2015021312222.md): Isolator · broken · Feb 9, 2015 · N837AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD ISOLATOR ABOVE WL 73.50 ON LBL 9.50 IS BROKEN. REMOVED DEFECTIVE ISOLATOR AND INSTALLED NEW ISOLATOR IAW SRM 51-42-13. REPAIR CLASSIFIED AS MINOR IAW GMM 5-3.
- [SDR ASOA2015020412142](https://openairdocs.org/sdr/ASOA2015020412142.md): Light · intermittent · Jan 31, 2015 · N837AS · Cndair CL6002B19 · Emergency Lighting
  > PASSENGER CABIN CEILING EMERGENCY LIGHT INTERMITTENT. R & R THE CEILING EMERGENCY LIGHT IAW AMM 33-51-16. OPS CHECKED GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME.
- [SDR ASOA2014111311637](https://openairdocs.org/sdr/ASOA2014111311637.md): Structure · damaged · Nov 10, 2014 · N837AS · Cndair CL6002B19 · Fuselage Main, Structure
  > DAMAGE NOTED ON REPAIR MADE TO UPPER LT WING ROOT. COMPLIED WITH GREO 601R-53-41-341
- [SDR ASOA2014091911269](https://openairdocs.org/sdr/ASOA2014091911269.md): Connector · unsecure · Sep 16, 2014 · N837AS · Cndair CL6002B19 · Light System Wiring
  > ENTRY LEVEL EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND RESEATED CONNECTOR ON EMERGENCY EXIT LIGHT ASSY AT ENTRY LEVEL AND REINSTALLED LIGHT ASSY IAW AMM 33-51-10, OPS CHECKED GOOD. ACFT OK FOR SERVICE.
- [SDR ASOA2014021909973](https://openairdocs.org/sdr/ASOA2014021909973.md): Battery · inoperative · Feb 15, 2014 · N837AS · Cndair CL6002B19 · Emergency Lighting
  > NR 3 EMERGENCY BATTERY INOPERATIVE. R & R NR 3 EMERGENCY BATTERY IAW AMM 33-51-04. OPS CHECKED GOOD.
- [SDR ASOA2013090608966](https://openairdocs.org/sdr/ASOA2013090608966.md): Battery Pack · discharged · Sep 4, 2013 · N837AS · Cndair CL6002B19 · Emergency Equipment
  > F/A FLASHLIGHT INOPERATIVE. REPLACED FA FLASHLIGHT BATTERIES. OPS CHECKED GOOD IAW AMM 25-61-00.
- [SDR ASOA2013051303508](https://openairdocs.org/sdr/ASOA2013051303508.md): Drag Angle · cracked · May 8, 2013 · N837AS · Cndair CL6002B19 · Passenger/Crew Doors
  > CRACK AT PAX DOOR AFT DRAG ANGLE BY FITTING.
- [SDR ASOA2013031103150](https://openairdocs.org/sdr/ASOA2013031103150.md): Bulb · burned out · Mar 7, 2013 · N837AS · Cndair CL6002B19 · Emergency Lighting
  > RT NR 3 EMERGENCY LIGHT INOPERATIVE. R & R BULB IAW AMM 33-51-21. OPS CHECKED GOOD.
- [SDR ASOA2013030503106](https://openairdocs.org/sdr/ASOA2013030503106.md): Light · cracked · Feb 27, 2013 · N837AS · Cndair CL6002B19 · Passenger/Crew Doors
  > EXIT/PULL BETA LIGHT ON PAX DOOR LATCH/LOCK LEVER FOUND TO BE CRACKED. R & R CRACKED BETA EXIT/PULL LIGHT ON PAX DOOR LATCH/LOCK LEVER WITH NEW IAW AMM 20-21-00-901-801.
- [SDR ASOA2013030103093](https://openairdocs.org/sdr/ASOA2013030103093.md): Seat Track · corroded · Feb 13, 2013 · N837AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK ON LBL 9 BETWEEN FS 409+126 TO FS 559+4 HAVE NUMEROUS SPOTS OF CORROSION. REMOVED SEAT TRACK IAW AMM 53-01-11-000-802, SUBTASK 53-01-11-020-002, PART B. LOCATED AND DRILLED NEW SEAT TRACK IAW SRM 51-40-11. INSTALLED NEW SEAT TRACK IAW MM TASK 53
- [SDR ASOA2013030503105](https://openairdocs.org/sdr/ASOA2013030503105.md): Seat Track · corroded · Feb 12, 2013 · N837AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK RBL 9.0 FS 559.00 - 559.00+80 HAS NUMEROUS SPOTS OF MINOR CORROSION. R & R DAMAGED SEAT TRACK IAW MM TASK 53-01-11-000-802 AND GREO 601R-53-00-485.
- [SDR ASOA2013030503104](https://openairdocs.org/sdr/ASOA2013030503104.md): Bulkhead · cracked · Feb 12, 2013 · N837AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUND REAR PRESSURE BULKHEAD WEB HAS INDICATION NOTED APPROX 3.0" IN LENGTH 70 PERCENT FSH AT BL 0.0 WL 108 TO WL 111. FAILED NDT INSPECTION. REPAIRED IAW REO 601R-53-61-4813.
- [SDR ASOA2013030503103](https://openairdocs.org/sdr/ASOA2013030503103.md): Bulkhead · cracked · Feb 12, 2013 · N837AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUND REAR PRESSURE BULKHEAD WEB HAS INDICATION NOTED AT BL 0.0, WL 136.0 APPROX 1.0" IN LENGTH 50 PERCENT FSH. FAILED NDT INSPECTION. COMPLIED WITH REO 601R-53-61-4813.
- [SDR ASOA2013030103092](https://openairdocs.org/sdr/ASOA2013030103092.md): Bulkhead · cracked · Feb 12, 2013 · N837AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUND REAR PRESSURE BULKHEAD WEB HAS INDICATION NOTED APPROX 3.0" IN LENGTH 70 PERCENT FSH AT BL 0.0, WL 108 TO WL 111. FAILED NDT INSPECTION. REPAIRED IAW REO 601R-53-61-1285 REV D, DATED 10/31/2011.
- [SDR ASOA2013030103091](https://openairdocs.org/sdr/ASOA2013030103091.md): Bulkhead · cracked · Feb 12, 2013 · N837AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUND REAR PRESSURE BULKHEAD WEB HAS INDICATION NOTED AT BL 0.0, WL 136.0, APPROX 1.0" IN LENGTH 50 PERCENT FSH. FAILED NDT INSPECTION. REPAIRED IAW REO 601R-53-61-4813.
- [SDR ASOA2013030103090](https://openairdocs.org/sdr/ASOA2013030103090.md): Angle · corroded · Feb 12, 2013 · N837AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AFTER REMOVAL OF THE DRAINAGE RAMP IN LWR PAX DOOR FOUND BOTH ANGLES AT FS 320.10 AND THE CLIPS AT FS 338.00 ARE CORRODED BEYOND LIMITS. R & R THE ANGLES IAW SRM 51-42-06.
- [SDR ASOA2013030103089](https://openairdocs.org/sdr/ASOA2013030103089.md): Angle · corroded · Feb 12, 2013 · N837AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AFTER REMOVAL OF THE DRAINAGE RAMP IN LWR PAX DOOR, FOUND THE AFT CORNER HAS CORROSION BEYOND LIMITS AND THE FWD CORNER. REMOVED THE PAX DOOR FWD LWR CORNER IAW SRM 51-42-06, SRM 51-42-13 AND SRM 51-42-21. INSTALLED THE NEW PAX DOOR FWD LWR CORNER IAW SRM 51
- [SDR ASOA2013030103088](https://openairdocs.org/sdr/ASOA2013030103088.md): Seat Track · corroded · Feb 12, 2013 · N837AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK LBL 9.00 FS 364-409+128 IS SEVERELY CORRODED. REMOVED SEAT TRACK IAW AMM 53-01-11-000-802. INSTALLED NEW SEAT TRACK IAW AMM 53-01-11-400-802.
- [SDR ASOA2013030103087](https://openairdocs.org/sdr/ASOA2013030103087.md): Floorbeam · cracked · Feb 12, 2013 · N837AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOORBEAM CRACKED AT RBL 9.00 AND LBL 9.00 BETWEEN FS 559.00. REPAIRED IAW SRM 51-42-06.
- [SDR ASOA2013022803085](https://openairdocs.org/sdr/ASOA2013022803085.md): Seat Track · corroded · Feb 12, 2013 · N837AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK ON RBL 9.00 FROM FS 364.00 TO FRAME STATION 409+128 HAS NUMEROUS SPOTS OF MINOR CORROSION. REMOVED RBL 9.00 FS 364.00-399.50 CORRODED SEAT TRACK IAW AMM 53-01-11-000-802. INSTALLED NEW SEAT TRACK PN 601R31032-15 IAW AMM 53-01-11-400-802. REMOVED
- [SDR ASOA2013030503102](https://openairdocs.org/sdr/ASOA2013030503102.md): Spar · cracked · Feb 8, 2013 · N837AS · Cndair CL6002B19 · Wing Spar
  > CRACK AT LT WS 148.019 AND THE REAR WING SPAR. AN INDICATION WAS NOTED APPROX.250L.60 PERCENT FULL SCREEN HEIGHT. REPAIRED LT WS 148.019 IAW REO 601R-57-21-130 AND 601R-57-21-131.
- [SDR ASOA2013022803084](https://openairdocs.org/sdr/ASOA2013022803084.md): Seat Track · corroded · Feb 8, 2013 · N837AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LT FLOOR SEAT TRACK, LBL 9 CORRODED THROUGH SIDE OF SEAT TRACK, FS 364.00 - FS 399.50. REMOVED CORRODED FLOOR SEAT TRACK FROM FS 364.00 - FS 399.00, LBL 9 IAW AMM SUBTASK 53-01-11-020-002, FIG 401.B. INSTALLED NEW SEAT TRACK IAW AMM SUBTASK 53-01-11-420-001
- [SDR ASOA2013022803083](https://openairdocs.org/sdr/ASOA2013022803083.md): Post · cracked · Feb 8, 2013 · N837AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FOUND FS 409+128 VERTICAL POST BL0.0 LT SIDE HAS INDICATION NOTED APPROX 3" IN LENGTH, 50 PERCENT FSH AT AFT FLANGE RADIUS WL 69.0. FAILED NDT INSPECTION. REMOVED POST AT STA 409+128 BL 0 IAW SRM 51-42-06. DRILLED UP NEW POST PN 601R32208-159, ASSY AND INST
- [SDR ASOA2012092702305](https://openairdocs.org/sdr/ASOA2012092702305.md): Light · cracked · Sep 23, 2012 · N837AS · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHT NEXT TO PASSENGER DOOR HAS A CRACKED FRAME. R & R FLOOD LIGHT, FLOOR LEVEL EMERGENCY LIGHT ASSY IAW AMM 33-51-11. OPS CHECKS GOOD ACFT GOOD FOR SERVICE. SDR CLOSED.
- [SDR ASOA201201712](https://openairdocs.org/sdr/ASOA201201712.md): Wire · disconnected · May 31, 2012 · N837AS · Cndair CL6002B19 · Light System Wiring
  > WIRES FOUND DISCONNECTED FROM EXIT SIGN, BELOW F/A JUMPSEAT. RECONNECTED AND RESECURED BROKEN WIRE TO FWD ENTRY WAY LIGHTED FLOOR LEVEL EXIT SIGN IAW AMM 33-51-10. OPS CHECKED GOOD.
- [SDR ASOA201100264](https://openairdocs.org/sdr/ASOA201100264.md): Light · inoperative · Feb 11, 2011 · N837AS · Cndair CL6002B19 · Emergency Lighting
  > PAX DOOR AND SERVICE DOOR EMERGENCY LIGHTS INOP. R & R BOTH PAX DOOR AND SERVICE DOOR EMERGENCY LIGHTS IAW AMM 33-51-00. OPS CHECKED GOOD.
- [SDR ASOA201100210](https://openairdocs.org/sdr/ASOA201100210.md): Wire · broken · Feb 3, 2011 · N837AS · Cndair CL6002B19 · Light System Wiring
  > WIRE FOR EMERGENCY LIGHT ON WARDROBE BROKEN. REPLACED SPLICE WITH QUARTER TURN QUICK DISCONNECT. OPS TEST OF EMERGENCY LIGHTS REQUIRED IAW 33-51-00-710-801. PERFORMED OPS TEST OF EMERGENCY LIGHT IAW 33-51-00-710-801. ALL CHECKS GOOD AT THIS TIME.
- [SDR ASOA201100209](https://openairdocs.org/sdr/ASOA201100209.md): Floorbeam · corroded · Feb 3, 2011 · N837AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOORBEAM CAP AT RBL 27 FS 621 IS CORRODED. REO 601R-53-61-3968 REV HAS BEEN ACCOMPLISHED AND ALL STEPS HAVE BEEN DOCUMENTED AND SIGNED FOR ON A NON-ROUTINE WORKCARD. ALL RII'S HAVE BEEN ACCOMPLISHED BY A TRAINED, QUALIFIED AND AUTHORIZED RII INSPECTOR IAW G
- [SDR ASOA201100191](https://openairdocs.org/sdr/ASOA201100191.md): Floorbeam · corroded · Jan 31, 2011 · N837AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOORBEAM CAP AT LBL 27, FS 621 TO FS 574 IS CORRODED. REPAIRED.
- [SDR ASOA201100190](https://openairdocs.org/sdr/ASOA201100190.md): Floorbeam · corroded · Jan 31, 2011 · N837AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CORROSION FOUND ON RT END OF FLOORBEAM, NEAR SERVICE DOOR. REO 601R-53-21-1230 HAS BEEN ACCOMPLISHED AND ALL STEPS HAVE BEEN DOCUMENTED AND SIGNED FOR ON A NON-ROUTINE WORK CARD. RETURNED TO SERVICE.
- [SDR ASOA201100165](https://openairdocs.org/sdr/ASOA201100165.md): Isolation Mount · cracked · Jan 25, 2011 · N837AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FWD BULKHEAD ISOLATION MOUNT CRACKED. R & R ISOLATOR MOUNTS ON FWD BULKHEAD FS 621 IAW SRM 51-42-06.
- [SDR ASOA201100135](https://openairdocs.org/sdr/ASOA201100135.md): Frame · cracked · Jan 19, 2011 · N837AS · Cndair CL6002B19 · Fuselage Main, Frame
  > FS 605, LEFT FRAME IS CRACKED AT FASTENERS JUST BELOW WL 73. REMOVED DAMAGED FRAME IAW SRM 51-42-06, PARA 11, PG 18. LOCATED, DRILLED AND INSTALLED NEW FRAME SECTION PN 601R36026-29 IAW SRM 51-42-06, 51-42-21, 51-40-11.
- [SDR ASOA201100134](https://openairdocs.org/sdr/ASOA201100134.md): Doubler · corroded · Jan 19, 2011 · N837AS · Cndair CL6002B19 · Fuselage Floor Panel
  > LT PRESSURE FLOOR SKIN DOUBLER OTBD OF LBL 36 JUST FWD OF FS 544 IS CORRODED. REMOVED CORROSION ON LT PRESSURE FLOOR SKIN DOUBLER IAW REO 601R-53-41-666. REF MATERIAL LOSS FOR PREVIOUS BLENDOUT WAS.010. REMOVED.003 MORE MATERIAL MAKING.013 TOTAL MATERIAL
- [SDR ASOA201100133](https://openairdocs.org/sdr/ASOA201100133.md): Doubler · corroded · Jan 19, 2011 · N837AS · Cndair CL6002B19 · Fuselage Floor Panel
  > RT PRESSURE FLOOR SKIN DOUBLER OTBD OF RBL 36 AT FS 529 IS CORRODED. REMOVED CORROSION ON RT PRESSURE FLOOR SKIN ASSY IAW REO 601R-53-41-666. REF MATERIAL LOSS FOR PRESSURE FLOOR SILL ASSY ANGLE WAS.010 FROM PREVIOUS BLENDOUT. REMOVED.004 MORE MATERIAL MA
- [SDR ASOA201100132](https://openairdocs.org/sdr/ASOA201100132.md): Floor Skin · corroded · Jan 19, 2011 · N837AS · Cndair CL6002B19 · Fuselage Floor Panel
  > LT PRESSURE FLOOR SKIN OTBD OF LBL 36 IS CORRODED AT FS 461. REMOVED CORROSION ON RT PRESSURE FLOOR SKIN ASSY IAW REO 601R-53-41-666. REF MATERIAL LOSS FOR PRESSURE FLOOR SILL ASSY ANGLE WAS.010 FROM PREVIOUS BLENDOUT. REMOVED.002 MORE MATERIAL MAKING.012
- [SDR ASOA201100131](https://openairdocs.org/sdr/ASOA201100131.md): Doubler · corroded · Jan 19, 2011 · N837AS · Cndair CL6002B19 · Fuselage Floor Panel
  > LT PRESSURE FLOOR SKIN DOUBLER AT FS 461 OTBD OF LBL 36 IS CORRODED. REMOVED CORROSION ON LT PRESSURE FLOOR DOUBLER IAW REO 601R-53-41-666. REF MATERIAL LOSS FOR PRESSURE FLOOR SILL ASSY ANGLE WAS.010 FROM PREVIOUS BLENDOUT DATED 1/21/09. REMOVED.002 MORE M
- [SDR ASOA201100130](https://openairdocs.org/sdr/ASOA201100130.md): Doubler · corroded · Jan 19, 2011 · N837AS · Cndair CL6002B19 · Fuselage Floor Panel
  > LT PRESSURE FLOOR SKIN DOUBLER OTBD OF LBL 36 AT FS 424 IS CORRODED. REMOVED CORROSION ON LT PRESSURE FLOOR SILL ASSY (SKIN DOUBLER) IAW REO 601R-53-41-666. MATERIAL LOSS IS.003, REMAINING MATERIAL IS.077. MINIMUM ALLOWABLE MATERIAL THICKNESS IS.055. ARE
- [SDR ASOA201100129](https://openairdocs.org/sdr/ASOA201100129.md): Doubler · corroded · Jan 19, 2011 · N837AS · Cndair CL6002B19 · Fuselage Floor Panel
  > LT PRESSURE FLOOR SKIN DOUBLER OTBD OF LBL 36 AT FS 449+85 IS CORRODED. REMOVED CORROSION ON LT PRESSURE FLOOR SILL ASSY (SKIN DOUBLER) IAW REO 601R-53-41-666. REF MATERIAL LOSS FOR PRESSURE FLOOR SILL ASSY ANGLE WAS.010 FROM PREVIOUS BLENDOUT DATED 1/21/09.
- [SDR ASOA201100128](https://openairdocs.org/sdr/ASOA201100128.md): Doubler · corroded · Jan 19, 2011 · N837AS · Cndair CL6002B19 · Fuselage Floor Panel
  > LT PRESSURE FLOOR SKIN DOUBLER OTBD OF LBL 36 AT FS 544 IS CORRODED. REMOVED CORROSION ON LT PRESSURE FLOOR SILL ASSY (SKIN DOUBLER) IAW REO 601R-53-41-666. REF MATERIAL LOSS FOR PRESSURE FLOOR SILL ASSY ANGLE WAS.010 FROM PREVIOUS BLENDOUT. REMOVED.002 MO
- [SDR ASOA201100120](https://openairdocs.org/sdr/ASOA201100120.md): Floor Support · cracked · Jan 17, 2011 · N837AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT ANGLE AT FS 621 ON OTBD RT SIDE IS CRACKED IN THE RADIUS. REPLACED EXISTING REPAIR WITH NEW SERVICEABLE PARTS IAW REO 601R-53-61-117, REV C, STEPS 1 THRU 7. REPAIR OF THE DAMAGED PORTIONS OF ANGLE 601R35031-239 IS COMPLETED IAW REO 601R-53-61-1
- [SDR ASOA201100109](https://openairdocs.org/sdr/ASOA201100109.md): Attach Fitting · cracked · Jan 13, 2011 · N837AS · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > FS 280 AND RBL 9, LBL 9 CLIPS ARE CRACKED. R & R CLIPS AT FS 280 LBL 9 INBD AND OTBD AND RBL 9 INBD IAW SRM 51-42-21.
- [SDR ASOA201100092](https://openairdocs.org/sdr/ASOA201100092.md): Angle · corroded · Jan 13, 2011 · N837AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FWD "J" ANGLE AT FS 280 IS CORRODED. FOUND FWD "J" ANGLE CORRODED BEYOND LIMITS. REMOVED FS 280 FWD ANGLE IAW SRM 51-42-06. CLASSIFIED AS A MINOR REPAIR.
- [SDR ASOA201100091](https://openairdocs.org/sdr/ASOA201100091.md): Web · cracked · Jan 13, 2011 · N837AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 280, LOWER WEB AT RBL 11.0 IS CRACKED. REPAIRED IAW REO 601R-53-11-926, REV B.
- [SDR ASOA201100090](https://openairdocs.org/sdr/ASOA201100090.md): Floorbeam · corroded · Jan 13, 2011 · N837AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CORROSION FOUND ON RT END OF FLOORBEAM, PN 601R32005-1, NEAR SERVICE DOOR. REPAIRED IAW REO 601R-53-21-1230.
- [SDR ASOA201100089](https://openairdocs.org/sdr/ASOA201100089.md): Floor Support · corroded · Jan 13, 2011 · N837AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT CARGO FLOOR SUPPORT FROM FS 621 TO FS 559+80 IS CORRODED. REMOVED CORROSION IAW SRM 51-21-06. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00. REMOVED FLOOR SUPPORT AND LOCATED AND DRILLED NEW SUPPORT IAW SRM 51-42-06 AND 51-42-21. INSTALLED NEW SILL IAW RE
- [SDR ASOA201100088](https://openairdocs.org/sdr/ASOA201100088.md): Floor Support · corroded · Jan 13, 2011 · N837AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOORBEAM CAP AT RBL 27, FS 621 TO 574 IS CORRODED. REMOVED FLOORBEAM CAP RBL 27 FS 574 TO FS 621.00 IAW SRM 51-42-06. LOCATED AND DRILLED UP NEW CAP IAW SRM 51-40-11, SRM 51-42-06 AND SRM 51-42-21. RBL 27, INSTALLED RBL 27, FLOORBEAM CAP IAW REO'S 601R-
- [SDR ASOA201100087](https://openairdocs.org/sdr/ASOA201100087.md): Floor Support · corroded · Jan 13, 2011 · N837AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LT CARGO FLOOR SUPPORT SILL FROM FS 621 TO FS 559+80 IS CORRODED. REMOVED AND LOCATED NEW FLOOR SILL IAW SRM 51-42-06 AND 51-42-21.
- [SDR ASOA201100085](https://openairdocs.org/sdr/ASOA201100085.md): Floor Support · corroded · Jan 13, 2011 · N837AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOORBEAM CAP AT LBL 27, FS 621 TO FS 574 IS CORRODED. REMOVED AND LOCATED AND DRILLED NEW CAP IAW SRM 51-42-06 AND 51-42-21.
- [SDR ASOA201100084](https://openairdocs.org/sdr/ASOA201100084.md): Cargo Track · corroded · Jan 13, 2011 · N837AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CARGO TRACKS LBL 27, LBL 9, & RBL 27 ARE CORRODED. REPLACED CARGO TRACKS IAW SRM 51-41-02.

Next page: https://openairdocs.org/deregistered/N837AS-2017-06-08/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 = 'N837AS' AND deregistration_id = 'N837AS-2017-06-08'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N837AS-2017-06-08/reports

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