# Service difficulty reports: N841AS, cancelled Aug 11, 2021

A list on [N841AS, cancelled Aug 11, 2021](https://openairdocs.org/deregistered/N841AS-2021-08-11.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 · 133 reports

- [SDR ASOA2015111714089](https://openairdocs.org/sdr/ASOA2015111714089.md): Smoke Detector · false indication · Nov 17, 2015 · N841AS · Cndair CL6002B19 · Smoke Detection
  > "SMOKE TOILET" CAUTION ON TAKEOFF, MESSAGE WENT AWAY ON FINAL APPROCH. R & R LAV SMOKE DETECTOR REF AMM 26-16-01. OPS CHECK GOOD, NO OTHER DEFECTS NOTED.
- [SDR ASOA2015012812105](https://openairdocs.org/sdr/ASOA2015012812105.md): Isolator · broken · Jan 20, 2015 · N841AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > BROKEN ISOLATOR ON FS 621 BULKHEAD. R & R ISOLATOR IAW SRM 51-42-13.
- [SDR ASOA2015012612092](https://openairdocs.org/sdr/ASOA2015012612092.md): Angle · cracked · Jan 20, 2015 · N841AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > BS 621 ANGLE CRACKED. R & R THE ANGLE IAW SRM 51-42-21 & TR 51-32.
- [SDR ASOA2015012812104](https://openairdocs.org/sdr/ASOA2015012812104.md): Floor Support · corroded · Jan 13, 2015 · N841AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LT CABIN FLOOR SUPPORT CORRODED BEYOND LIMITS OF REO 601R-53-41-666 BS 426 - 519. CUT OUT DAMAGE IAW REO 601R-53-41-1871, REV P1. FABRICATED REPAIR IAW REO 601R-53-41-1871, REV P1. INSTALLED THE REPAIR IAW REO 601R-53-41-1871, REV P1
- [SDR ASOA2015012812103](https://openairdocs.org/sdr/ASOA2015012812103.md): Skin · cracked · Jan 13, 2015 · N841AS · Cndair CL6002B19 · Wing, Plate/Skin
  > RT LOWER WING PLANK/TRUNNION HAS AN INDICATION NOTED IN BORE OF THE 4TH FASTENER GOING AFT FROM FWD END NOTED IN SB 601R-57-046, REV C. INDICATION IS ON INBD SIDE.450" FROM LOWER SURFACE,.150" LONG AND 60 PERCENT FSH. FAILED NDT. COMPLIED WITH STEP 13 OF R
- [SDR ASOA2015012812102](https://openairdocs.org/sdr/ASOA2015012812102.md): Skin · corroded · Jan 12, 2015 · N841AS · Cndair CL6002B19 · Wing, Plate/Skin
  > CORROSION FOUND ON LOWER WING PLANK LANDING AFT/INBD EDGE UNDER PANEL 650BB. COMPLIED WITH EC/TC EO 600-57-81. C/W IAW REO 601R-57-21-030, REV L.
- [SDR ASOA2015012612091](https://openairdocs.org/sdr/ASOA2015012612091.md): Angle · cracked · Jan 12, 2015 · N841AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > BS 621, UPPER LT AND RT OBLIQUE ANGLES ARE CRACKED. R & R THE ANGLES IAW SRM 51-42-21.
- [SDR ASOA2015012612090](https://openairdocs.org/sdr/ASOA2015012612090.md): Stringer · cracked · Jan 9, 2015 · N841AS · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > STRINGER 3L AT BS 280 BULKHEAD CRACKED. REPAIRED IAW SRM 51-42-06 AND SRM 51-40-11-00.
- [SDR ASOA2015012812101](https://openairdocs.org/sdr/ASOA2015012812101.md): Bulkhead Web · cracked · Jan 8, 2015 · N841AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUND REAR PRESSURE BULKHEAD WEB HAS A CRACK INDICATION. LBL 18.00, WL 140 REMOVED FS 621.00 BULKHEAD STIFFENING ANGLE IAW SRM 51-42-06. INSTALLED SERVICEABLE FS 621, BULKHEAD STIFFENING ANGLE IAW REO 601R-53-61-1285, REV D AND REO 601R-53-61-5420, REV. CO
- [SDR ASOA2015012812100](https://openairdocs.org/sdr/ASOA2015012812100.md): Bulkhead Web · cracked · Jan 8, 2015 · N841AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUND REAR PRESSURE BULKHEAD WEB HAS A CRACK INDICATION AT BL 0.0, WL 102. REPAIRED IAW EC/TC REO 601R-53-61-1285 AND GREO 601R-53-61-1285, REV D.
- [SDR ASOA2015012812099](https://openairdocs.org/sdr/ASOA2015012812099.md): Floor Support · corroded · Jan 8, 2015 · N841AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PRESSURE FLOOR SUPPORT HAS MINOR CORROSION BETWEEN BS 409+128 - 559. FOUND TO BE WITHIN LIMITS OF REO 601R-53-41-666.
- [SDR ASOA2015012812098](https://openairdocs.org/sdr/ASOA2015012812098.md): Skin · cracked · Jan 8, 2015 · N841AS · Cndair CL6002B19 · Wing, Plate/Skin
  > LOWER WING PLANK ACCESS HOLE HAS AN INDICATION NOTED ON LANDING, FOR PANEL 650DB AT AFT INBD EDGE APPROXIMATELY.250" X.250" X 50 PERCENT FSH. FAILED NDT. COMPLIED WITH EC/TC EO 600-57-81. C/W IAW REO 601R-57-21-030, REV L.
- [SDR ASOA2015012812097](https://openairdocs.org/sdr/ASOA2015012812097.md): Skin · cracked · Jan 8, 2015 · N841AS · Cndair CL6002B19 · Wing, Plate/Skin
  > LOWER WING PLANK ACCESS HOLE HAS MULTIPLE INDICATIONS NOTED, ON LANDING FOR PANEL 610AB AT FWD OUTBD EDGE, APPROXIMATELY 1.0" X.250" X 50 PERCENT FSH, FAILED NDT. COMPLIED WITH EC/TC EO 600-57-81. C/W IAW REO 601R-57-21-030, REV L.
- [SDR ASOA2015012812096](https://openairdocs.org/sdr/ASOA2015012812096.md): Skin · cracked · Jan 8, 2015 · N841AS · Cndair CL6002B19 · Wing, Plate/Skin
  > LOWER WING PLANK ACCESS HOLE HAS MULTIPLE INDICATIONS NOTED ON LANDING FOR PANEL 650FB AT FWD AND OTBD EDGE, APPROXIMATELY.250" X.250" X 50 PERCENT FSH. COMPLIED WITH EC/TC EO 600-57-81. C/W IAW REO 601R-57-21-030, REV L.
- [SDR ASOA2015012612089](https://openairdocs.org/sdr/ASOA2015012612089.md): Bulkhead Web · cracked · Jan 8, 2015 · N841AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUND REAR PRESSURE BULKHEAD WEB HAS A CRACK INDICATION NOTED AT LBL 36.20, WL 76.0. REPAIRED IAW REO 601R-53-61-5417, REV.
- [SDR ASOA2015012612088](https://openairdocs.org/sdr/ASOA2015012612088.md): Bulkhead Web · cracked · Jan 8, 2015 · N841AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUND REAR PRESSURE BULKHEAD WEB HAS A CRACK INDICATION NOTED AT RBL 18.00, WL 108. REPAIRED IAW EC/TC REO 601R-53-61-1285 & GREO 601R-53-61-1285.
- [SDR ASOA2015012612087](https://openairdocs.org/sdr/ASOA2015012612087.md): Floor Support · corroded · Jan 8, 2015 · N841AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PRESSURE FLOOR SUPPORT HAS MINOR CORROSION BETWEEN BS 409+128 - 559. REPAIRED IAW EC/TC REO 601R-53-41-666-01 AND REO 601R-53-41-666, REV C.
- [SDR ASOA2015012612086](https://openairdocs.org/sdr/ASOA2015012612086.md): Intercostal · cracked · Jan 8, 2015 · N841AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INTERCOSTAL AT STRINGER 13L BS 621 IS CRACKED. REMOVED AND REPLACED TEH INTERCOSTAL IAW SRM 51-42-06 AND 51-42-21.
- [SDR ASOA2015012612085](https://openairdocs.org/sdr/ASOA2015012612085.md): Angle · cracked · Jan 8, 2015 · N841AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INTERCOSTAL AT BS 484, LBL 27 HAS A CRACKED ANGLE. R & R THE ANGLE IAW SRM 51-40-11 AND 51-42-21.
- [SDR ASOA2015012612084](https://openairdocs.org/sdr/ASOA2015012612084.md): Angle · cracked · Jan 7, 2015 · N841AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INTERCOSTAL AT FS 484, LBL 36 HAS A CRACKED ANGLE. REPAIRED IAW REO 601R-53-41-1870 AND REO 601R-53-41-059.
- [SDR ASOA2015012612083](https://openairdocs.org/sdr/ASOA2015012612083.md): Angle · cracked · Jan 7, 2015 · N841AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INTERCOSTAL AT BS 484, RBL 27 HAS A CRACKED ANGLE. R & R THE ANGLE IAW SRM 51-40-11 AND 51-42-21.
- [SDR ASOA2015012612082](https://openairdocs.org/sdr/ASOA2015012612082.md): Angle · cracked · Jan 7, 2015 · N841AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INTERCOSTAL AT FS 484, RBL 36.00 HAS A CRACKED ANGLE. REPAIRED IAW REO 601R-53-41-1870 AND REO 601R-53-41-059.
- [SDR ASOA2015012612081](https://openairdocs.org/sdr/ASOA2015012612081.md): Skin · cracked · Jan 6, 2015 · N841AS · Cndair CL6002B19 · Wing, Plate/Skin
  > RT BOOST PUMP CUTOUT HAS MULTIPLE INDICATIONS ALL AROUND THE VERTICAL AND HORIZONTAL LANDING 60 PERCENT FSH FAIL NDT. COMPLIED WITH EA 32-2015-004.
- [SDR ASOA2015012812095](https://openairdocs.org/sdr/ASOA2015012812095.md): Door · delaminated · Jan 3, 2015 · N841AS · Cndair CL6002B19 · Landing Gear Doors
  > LEFT NLG DOOR L/E DELAMINATED. REPAIRED LT NLG DOOR IAW REO 601R-52-81-020, REV NC DATED 99-09-17. PAINTED REPAIRED AREA ON LT NLG DOOR L/E IAW SRM 51-25-01. APPLIED ABRASION RESISTANT FILM ON LT NLG DOOR L/E IAW SRM 51-27-19. COMPLIED WITH EC/TC REO 601R-
- [SDR ASOA2015010512002](https://openairdocs.org/sdr/ASOA2015010512002.md): Landing Gear · malfunctioned · Dec 28, 2014 · N841AS · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > NOSE GEAR DID NOT RETRACT AFTER TAKEOFF. ACFT RETURNED TO DEPARTURE. GEAR EXTENDED MANUALLY.
- [SDR ASOA2014122211893](https://openairdocs.org/sdr/ASOA2014122211893.md): Rod · broken · Dec 18, 2014 · N841AS · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR WILL NOT OPEN. FOUND PRESSURE RELIEF VENT FLAP ROD BROKEN. REPLACED PAX DOOR VENT FLAP ROD IAW AMM 52-11-15. OPS CHECK GOOD. ACFT OK FOR SERVICE.
- [SDR ASOA2014013109816](https://openairdocs.org/sdr/ASOA2014013109816.md): Support Bracket · cracked · Jan 26, 2014 · N841AS · Cndair CL6002B19 · Cargo/Baggage Doors
  > FWD SUPPORT BRACKET IN AFT CARGO DOOR IS CRACKED. R & R FWD SUPPORT BRACKET IAW SRM 51-42-06.
- [SDR ASOA2013062708511](https://openairdocs.org/sdr/ASOA2013062708511.md): Skin · damaged · Jun 23, 2013 · N841AS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN DAMAGED AT FS 310 NEAR STR 16L AT SKIN EDGE. REPAIRED IAW GREO 601R-53-21-160, REO 601R-53-21-2447.
- [SDR ASOA2013020702969](https://openairdocs.org/sdr/ASOA2013020702969.md): Floor Support · corroded · Jan 23, 2013 · N841AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT FLOOR SUPPORT FWD OF SERVICE DOOR CUTOUT IS CORRODED FROM FS 310 TO FS 319. R & R FLOOR SUPPORT ANGLE IAW SRM 51-42-06. LOCATED, DRILLED NEW FLOOR SUPPORT IAW SRM 51-40-11.
- [SDR ASOA2013020502958](https://openairdocs.org/sdr/ASOA2013020502958.md): Rib · cracked · Jan 21, 2013 · N841AS · Cndair CL6002B19 · Wing, Rib/Bulkhead
  > RT WING L/E RIB AT WS 167.46 IS CRACKED AT EDGE OF PICCOLO TUBE CUTOUT. REMOVED CRACKED RIB AT WS 167.46 IAW SRM 51-42-06. INSTALLED NEW RIB, PN 601R12047-4 IAW SRM 51-42-06.
- [SDR ASOA2013020502957](https://openairdocs.org/sdr/ASOA2013020502957.md): Angle · cracked · Jan 21, 2013 · N841AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > WHILE REPLACING FWD J ANGLE ON FS 280, FOUND INBD CLIPS AT LBL 9 & RBL 9 TO BE CRACKED. REMOVED CLIPS IAW SRM 51-42-21. FABRICATED & INSTALLED INBD CLIPS AT LBL 9 & RBL 9 IAW REO 601R-53-11-926.
- [SDR ASOA2013020702968](https://openairdocs.org/sdr/ASOA2013020702968.md): Post · cracked · Jan 17, 2013 · N841AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FOUND FS 409.00+128 VERTICAL POST BL 0.0 LT & RT SIDE HAVE INDICATIONS NOTED APPROX.2" IN LENGTH 50 PERCENT FSH AT AFT FLANGE RADIUS FAILED NDT INSPECTION. REMOVED FS 409+128 BL 0 VERT POST ASSY IAW SRM 51-42-06 & 51-42-21. DRILL/LOCATED NEW SERVICEABLE FS
- [SDR ASOA2013020702967](https://openairdocs.org/sdr/ASOA2013020702967.md): Angle · corroded · Jan 16, 2013 · N841AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PAX DOOR LOWER SILL ANGLE IS CORRODED. REMOVED PAX DOOR LOWER SILL ANGLE IAW SRM 51-42-21, 51-42-13 & 51-42-06. LOCATED & DRILLED NEW SERVICEABLE PAX DOOR LOWER SILL ANGLE IAW SRM 51-40-11. INSTALLED NEW SERVICEABLE PAX DOOR LOWER SILL ANGLE IAW SRM 51-42-2
- [SDR ASOA2013020602964](https://openairdocs.org/sdr/ASOA2013020602964.md): Beam · corroded · Jan 16, 2013 · N841AS · Cndair CL6002B19 · Fuselage Main, Structure
  > CORROSION FOUND ON END OF TRANSVERSE BEAM AT FS 349 RT SIDE. REPAIRED IAW REO 601R-53-21-2401.
- [SDR ASOA2013020602963](https://openairdocs.org/sdr/ASOA2013020602963.md): Sill · corroded · Jan 16, 2013 · N841AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON LOWER SERVICE DOOR SILL ANGLE BETWEEN FS 319 AND FS 349. REMOVED CORRODED SILL FOR REPLACEMENT IAW SRM 51-42-06, 51-42-13 AND 51-42-21. INSTALLED NEW SILL ANGLE IAW SRM 51-42-06, SRM 51-42-13 & SRM 51-42-21. LOCATED AND DRILLED NEW SERVIC
- [SDR ASOA2013020602962](https://openairdocs.org/sdr/ASOA2013020602962.md): Fitting · cracked · Jan 16, 2013 · N841AS · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > CO-PILOT SIDE POST LOWER AFT FITTING IS CRACKED (FITTING IS FOR WINDOWS). R & R LOWER AFT FITTING ON THE CO-PILOT'S SIDE POST WITH A NEW SERVICEABLE FITTING IAW SRM 51-42-21.
- [SDR ASOA2013020502956](https://openairdocs.org/sdr/ASOA2013020502956.md): Frame · corroded · Jan 16, 2013 · N841AS · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME 605 IS CORRODED AT STRINGER 27. PERFORMED FRAME REPAIR NR 2 FRAME OUTER FLANGE REPAIR TO FS 605 BETWEEN STR 26-27 IAW SRM 53-00-15, REPAIR NR 2. COMPLIED WITH SRM 53-00-15.
- [SDR ASOA2013020502955](https://openairdocs.org/sdr/ASOA2013020502955.md): Angle · corroded · Jan 16, 2013 · N841AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON FS 280.00 J-ANGLE. R & R WITH NEW SERVICEABLE J-ANGLE IAW SRM 51-42-06 AND SRM 51-42-21.
- [SDR ASOA2013020602961](https://openairdocs.org/sdr/ASOA2013020602961.md): Seat Track · corroded · Jan 15, 2013 · N841AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON LT AND RT AISLE SEAT TRACKS FROM FS 364.00 TO FS 559.00+32. REMOVED LT NR 1 SEAT TRACK IAW AMM 53-01-11-000-802. LOCATED & DRILLED NR 1 LT SEAT TRACK FABBED FROM N126-2075 EXTRUSION IAW REO 601R-53-00-485. INSTALLED LT NR 1 FABBED SEAT TRACK PN
- [SDR ASOA2013020602960](https://openairdocs.org/sdr/ASOA2013020602960.md): Skin · corroded · Jan 15, 2013 · N841AS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > EXTERIOR SKIN PANELS BETWEEN FS 559.00+96 AND 559.00+112 CENTERLINE OF BELLY HAS CORROSION AROUND BUTTON HEAD RIVETS. BETWEEN FS 559+96 AND FS 559+112 BETWEEN STR 26L & STR 26R BLENDED AREAS TO SMOOTH CONTOUR. REPAIRED IAW REO 601R-53-51-215 AND SRM 51-42-06
- [SDR ASOA2013020502954](https://openairdocs.org/sdr/ASOA2013020502954.md): Rib · cracked · Jan 15, 2013 · N841AS · Cndair CL6002B19 · Wing, Rib/Bulkhead
  > RT BATT RIB ASSY CRACKED AT WS 53.60 APPROX 1" LONG. REPAIRED IAW REO 601R-57-51-046.
- [SDR ASOA2013020102951](https://openairdocs.org/sdr/ASOA2013020102951.md): Bracket · cracked · Jan 15, 2013 · N841AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > REAR PRESSURE BULKHEAD AT FS 621.00 HAS 4 ISOLATOR BRACKET ASSY CRACKED AT RBL 45, 1 BRACKET AT RBL 9, 1 BRACKET AT LBL 9, 1 BRACKET AT LBL 27 AND 1 BRACKET AT LBL 36. REMOVED 8 EA DAMAGED ISOLATORS FROM FS 621 PRESSURE BULKHEAD AND INSTALLED NEW ISOLATORS,
- [SDR ASOA2013020102950](https://openairdocs.org/sdr/ASOA2013020102950.md): Angle · cracked · Jan 14, 2013 · N841AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT FS 621-625 INTERCOSTAL ANGLE CRACKED AT S14R. LOCATED FASTENER HOLES IN NEW ANGLE IAW SRM 51-40-11 AND INSTALLED NEW ANGLE IAW SRM 51-42-21.
- [SDR ASOA2012071301899](https://openairdocs.org/sdr/ASOA2012071301899.md): Lamp · burned out · Jul 9, 2012 · N841AS · Cndair CL6002B19 · Emergency Lighting
  > FWD WARDROBE FLOOR FLOOD EMERGENCY LIGHT HAS SEVERAL BULBS INOPERATIVE. RELAMPED FLOOR LEVEL EMERGENCY FLOOD LIGHT ON WARDROBE. OPS CHECKED GOOD.
- [SDR ASOA201100845](https://openairdocs.org/sdr/ASOA201100845.md): Latch · binding · Apr 25, 2011 · N841AS · Cndair CL6002B19 · Passenger/Crew Doors
  > UNABLE TO UNLATCH PAX DOOR FROM OUTSIDE. PERFORMED OPS CHECK OF PAX DOOR HANDLE IAW AMM 52-11-02.
- [SDR ASOA201100218](https://openairdocs.org/sdr/ASOA201100218.md): Light · broken · Feb 4, 2011 · N841AS · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHT FLOOR LEVEL FLOODLIGHT AT PASSENGER DOOR BROKEN. R & R FLOOR LEVEL EMERGENCY FLOOD LIGHT IAW CRJ 200 33-51-19-000-801 & -400-801. EMERGENCY LIGHTS OPS CHECKED OK IAW MM 33-51-00-710-801.
- [SDR ASOA201100208](https://openairdocs.org/sdr/ASOA201100208.md): Wire · broken · Jan 25, 2011 · N841AS · Cndair CL6002B19 · Light System Wiring
  > PANEL 232BZ HAS A BROKEN WIRE ON THE EXIT LIGHT PANEL. R & R EXIT LIGHT ON PANEL 232BZ IAW AMM 33-51-10-000-801 AND 33-51-10-400-801. OPS CHECK DUE. PERFORMED OPS CHECK FOR EXIT LIGHT ON PANEL 232BZ IAW AMM 33-51-00-710-805. OPS CHECK GOOD. (CLOSED)
- [SDR ASOA201100184](https://openairdocs.org/sdr/ASOA201100184.md): Isolator · broken · Jan 24, 2011 · N841AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT BULKHEAD 621 ISOLATOR IS BROKEN. INSTALLED A NEW SERVICEABLE ISOLATOR ON THE 621 BULKHEAD IAW SRM 51-42-13. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW SOP 5702.
- [SDR ASOA201100161](https://openairdocs.org/sdr/ASOA201100161.md): Web · cracked · Jan 24, 2011 · N841AS · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR AFT WEB IS CRACKED AT FWD EDGE OF STEP 832AT. REPAIRED DAMAGE IAW REO NR: 601R-52-11-1901.
- [SDR ASOA201100160](https://openairdocs.org/sdr/ASOA201100160.md): Floor Support · corroded · Jan 24, 2011 · N841AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON NUTPLATES OF FLOOR SUPPORT FS 585 - 600 LBL 27.

Next page: https://openairdocs.org/deregistered/N841AS-2021-08-11/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 = 'N841AS' AND deregistration_id = 'N841AS-2021-08-11'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N841AS-2021-08-11/reports

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