# Service difficulty reports: N854AS

A list on [N854AS](https://openairdocs.org/aircraft/N854AS.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 6 · 270 reports

- [SDR SWIA2024021900011](https://openairdocs.org/sdr/SWIA2024021900011.md): Engine · damaged · Feb 11, 2024 · N854AS · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > AFTER TAKEOFF DURING CLIMBOUT RECEIVED R FIRE FAIL CAUTION MESSAGE. SHORTLY AFTER THAT, RECEIVED R ENG FIRE WARNING MESSAGE WITH THE FIRE PUSH ILLUMINATED. NO LOSS OF ENGINE POWER, ITT WAS NORMAL. CHECKED SYNOPTIC PAGES, HYDRAULIC PUMP 2A WAS RED. BY THE TIME
- [SDR SWIA2024021200001](https://openairdocs.org/sdr/SWIA2024021200001.md): Fire Warning · illuminated · Feb 11, 2024 · N854AS · Cndair CL6002B19 · Fire Detection
  > AFTER TAKEOFF DURING CLIMBOUT RECEIVED R FIRE FAIL CAUTION MESSAGE. SHORTLY AFTER THAT, RECEIVED R ENG FIRE WARNING MESSAGE WITH THE FIRE PUSH ILLUMINATED. NO LOSS OF ENGINE POWER, ITT WAS NORMAL. CHECKED SYNOPTIC PAGES, HYDRAULIC PUMP 2A WAS RED. BY THE TIME
- [SDR SWIA20230907831](https://openairdocs.org/sdr/SWIA20230907831.md): Unknown · dented · Aug 31, 2023 · N854AS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > TRANSFER FROM EAML 1202516: -1 AREA OF DENT DAMAGE TO EXISTING DOUBLERS REPAIR (GREO601R-53-21-180, REF) ON SKIN PANEL (DWG: 601R31062, REF) LOCATED BETWEEN STR 15 €“ STR 16 AND AT FS310.00. DENT AFFECTS ENTIRE STACKUP OF REPAIR AND MEASURES 0.5€? (L) X 0.2
- [SDR SWIA202266457](https://openairdocs.org/sdr/SWIA202266457.md): None · smoke · Sep 12, 2022 · N854AS · Cndair CL6002B19 · Air Conditioning System
  > PAX IN 11D SAW WHITE/GREY SMOKE COMING FROM SIDE WALL/FLOOR ON T/O WAS NOT REPORTED UNTIL JUST PRIOR TO LANDING. A FEW PAX AROUND THE AREA ALSO SMELLED ODOR BUT DID NOT SEE SMOKE (FLIGHT #5122 FILED CLOSED) PERFORMED AN OPERATIONAL CHECK OF THE AIR CONDITIO
- [SDR SWIA202265047](https://openairdocs.org/sdr/SWIA202265047.md): None · bent · Feb 4, 2022 · N854AS · Cndair CL6002B19 · Ailerons
  > AFT RIB ON THE LH INBOARD FLAP IS BENT AT PREVIOUS SKIN REPAIR (MARKED) (C-CHECK RO 3/14/2022) REMOVED PREVIOUS SKIN REPAIR AND REPLACED WITH NEW DOUBLER, FILLER AND ANGLE REF CRJ200 SRM 57-52-00 REPAIR NO. 3 / COMPLIED WITH TASK CARD 51-900-1003-SKY
- [SDR SWIA202265046](https://openairdocs.org/sdr/SWIA202265046.md): None · cracked · Feb 4, 2022 · N854AS · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > : DURING FLOOR SUPPORT ANGLE REMOVAL FROM FLOOR BEAM AT FS280, LBL9-RBL9, IT WAS FOUND FLOOR BEAM VERTICAL ATTACH ANGLE CRACKED AT FS280.00, LBL9 (C-CHECK RO 3/14/2022) REMOVED DAMAGED FLOOR BEAM VERTICAL ATTACH ANGLE AT FS280.00, LBL9 AND REPLACED BY A
- [SDR SWIA202265045](https://openairdocs.org/sdr/SWIA202265045.md): None · elongated · Jan 29, 2022 · N854AS · Cndair CL6002B19 · Horizontal Stabilizer Miscellaneous Structure
  > ENLOGATED HOLE ON FLANGE ANGLE ON RIGHTHAND HORIZONTAL TIP (C-CHECK RO 3/14/2022) REMOVED AND REPLACED RIGHTHAND HORIZONTAL TIP UPPER FLANGE ANGLE IAW CRJ 200 SRM 51-42-06 / CRJ SRM 51-42-15 AND DRAWING # 601R23037 REV -B. (SEE CONTINUATION SHEET FOR FUR
- [SDR SWIA202265044](https://openairdocs.org/sdr/SWIA202265044.md): None · gouged · Jan 27, 2022 · N854AS · Cndair CL6002B19 · Fuselage Main, Keel
  > IN MAIN CABIN AT CABIN AT FS319.00 AT STRINGER8R BRACKET HAS GOUGES (C-CHECK RO 3/14/2022) REMOVED GOUGES ON BRACKET IN MAIN CABIN AT FS319.00 AT STRINGER8R IAW CRJ 200 SRM 51-12-00 / EVALUATED BRACKET IN MAIN CABIN AT FS319.00 AT STGR8R FOUND TO BE OUT
- [SDR SWIA202265043](https://openairdocs.org/sdr/SWIA202265043.md): None · cracked · Jan 26, 2022 · N854AS · Cndair CL6002B19 · Fuselage Structure (General)
  > COPILOTS WIDOW SIDE POST THE LOWER FITTING IS CRACKED (MARKED) (C-CHECK RO 3/14/2022) REMOVED AND REPLACED CO PILOTS WINDOW SIDE POST LOWER ATTACH FITTING P/N 601R33235-4. INSTALLED REF BOMBARDIER DWG 601R33007 REV -U AND CRJ 200 SRM 51-42-21. COMPLIED
- [SDR SWIA202265042](https://openairdocs.org/sdr/SWIA202265042.md): None · cracked · Jan 25, 2022 · N854AS · Cndair CL6002B19 · Fuselage Main, Frame
  > COMPLY WITH AD 2008-06-10/04 REPAIR OF CRACKS IN FRAME REINFORCEMENT DOUBLER ONLY DUE BEFORE FURTHER FLIGHT. (C-CHECK RO 3/14/2022) COMPLIED WITH PARAGRAPH (H)(2) OF THIS AD FOR ANY CRACK FOUND IN THE FRAME REINFORCEMENT DOUBLER ONLY, BY DOING THE FRAME
- [SDR SWIA202265041](https://openairdocs.org/sdr/SWIA202265041.md): None · corroded · Jan 18, 2022 · N854AS · Cndair CL6002B19 · Wing, Rib/Bulkhead
  > *RIGHT WING LOWER WING PLANK ACCESS HOLE 650BB HAS COROSION. (C-CHECK RO 3/14/2022) REMOVED CORROSION FROM RIGHT WING LOWER WING PLANK AROUND THE MATING SURFACE OF WING PANEL 650BB REF BOMBARDIER REO 601R-57-21-030 REV -L DATED 2014-02-05. EVALUATED AND
- [SDR SWIA202265093](https://openairdocs.org/sdr/SWIA202265093.md): None · gouged · Jan 17, 2022 · N854AS · Cndair CL6002B19 · Wing Structure
  > CENTER HINGE FITTINGS FOR THE RH AILERON HAS GOUGES (MARKED) (C-CHECK RO 3/14/2022) BLENDED RH AILERON CENTER HINGE FITTINGS TO A SMOOTH CONTOUR. REF: CRJ200 SRM 51-12-00. FOUND TO BE OUT OF LIMITS REF REF CRJ 200 SRM 57-51-14 FIGURE 101.RECIEVED REO 601
- [SDR SWIA202265088](https://openairdocs.org/sdr/SWIA202265088.md): None · corroded · Jan 13, 2022 · N854AS · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > *IN MAIN CABIN, ON INTERCOSTAL BETWEEN FRAME FS349 AND FS364, AND BETWEEN STR17L AND STR16L, SIDEWALL SUPPORT BRACKET IS CORRODED. (MARKED) (C-CHECK RO 3/14/2022) FOUND SIDEWALL SUPPORT BRACKET BETWEEN FS 349 AND FS 364 AND BETWEEN STR 17L AND 16L OUT O
- [SDR SWIA202265087](https://openairdocs.org/sdr/SWIA202265087.md): None · corroded · Jan 13, 2022 · N854AS · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > *IN MAIN CABIN, AT FS349 NEAR STR15L, SIDE SEAT BRACKET CORRODED. (MARKED) (C-CHECK RO 3/14/2022) FOUND CORROSION ON BRACKET AT FS 349 NEAR STR 15L OUT OF LIMITS REF CRJ 200 SRM 53-00-00 AND INSTALLED NEW BRACKET REF CRJ 200 SRM 51-42-06.
- [SDR SWIA202265074](https://openairdocs.org/sdr/SWIA202265074.md): None · corroded · Jan 13, 2022 · N854AS · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > *RIGHT SIDE SEAT RAIL STRUCTURE APPROX FS449.85 THRU FS499.00 HAS PITTING AND CORRODED AROUND SCREWS. (C-CHECK RO 3/14/2022) REMOVED CORROSION ON R/H SIDE SEAT RAIL BETWEEN FS449.85 TO FS499.00. REF: CRJ-200 SRM 51-21-06. FOUND TO BE OUT OF LIMITS. REF:
- [SDR SWIA202265073](https://openairdocs.org/sdr/SWIA202265073.md): None · corroded · Jan 13, 2022 · N854AS · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > *IN MAIN CABIN, AT FS349 NEAR STR15L INTERCOSTAL, TIE AT INTERCOSTAL TO FRAME IS CORRODED. (MARKED) (C-CHECK RO 3/14/2022) FOUND CORROSION AT FS 349 NEAR STR 15L GUSSET TIE OUT OF LIMITS REF CRJ 200 SRM 53-00-00 USING DIGITAL CALIPARS TUC 9393 CAL DUE 31
- [SDR SWIA202265072](https://openairdocs.org/sdr/SWIA202265072.md): None · cracked · Jan 12, 2022 · N854AS · Cndair CL6002B19 · Fuselage, Door Hinge
  > STIFFENER ON LWR LH AFT FS621.0 BULKHEAD CRACKED (MARKED) (C-CHECK RO 3/14/2022) REMOVED AND REPLACED STIFFENER ON LWR LH AFT FS621.0 BULKHEAD WITH NEW P/N 601R36008-51 REF CRJ200 SRM 51-42-06
- [SDR SWIA202265091](https://openairdocs.org/sdr/SWIA202265091.md): None · chafed · Jan 11, 2022 · N854AS · Cndair CL6002B19 · Doors
  > *PASSENGER DOOR, AT UPPER END OF DOOR, AT AFT EDGE OF FWD DOOR CAP, CHAFING ON STRUCTURE AND FASTENER HEAD. (MARKED) (C-CHECK RO 3/14/2022) BLENDED OUT CHAFING ON STRUCTURE ON PASSENGER DOOR, AT UPPER END OF DOOR, AT AFT EDGE OF FWD DOOR CAP. REF: CRJ-2
- [SDR SWIA202265040](https://openairdocs.org/sdr/SWIA202265040.md): None · dented · Jan 11, 2022 · N854AS · Cndair CL6002B19 · Doors
  > *PASSENGER DOOR, ON INNER SKIN/STEP SUPPORT STRUCTURE, DENT ON INSIDE SKIN AT ACCESS HOLE FOR COUNTER BALANCE PULLEY MOUNT BOLT. (MARKED) (C-CHECK RO 3/14/2022) REPAIED PASSENGER DOOR, ON INNER SKIN/STEP SUPPORT STRUCTURE REF REO 601R-52-11-2915 REV-- D
- [SDR SWIA202265090](https://openairdocs.org/sdr/SWIA202265090.md): None · corroded · Jan 10, 2022 · N854AS · Cndair CL6002B19 · Fuselage Structure (General)
  > *AFT CARGO FLOOR SUPPORT ANGLE BETWEEN LBL 27 €“ 36, ATTACHED TO BULKHEAD 621.00 (C-CHECK RO 3/14/2022) REMOVED CORROSION AFT CARGO FLOOR SUPPORT ANGLE BETWEEN LBL27-36 ATTACHED TO BULKHEAD FS 621.00 REF CRJ200 SRM 51-21-06 / ORIGINAL MATERIAL.094 IAW
- [SDR SWIA202265086](https://openairdocs.org/sdr/SWIA202265086.md): None · corroded · Jan 10, 2022 · N854AS · Cndair CL6002B19 · Doors
  > *ON PASSENGER DOOR, LOWER LATCH MECHANISMTORQUE TUBE STOP BOLT HAS CORRODED HARDWARE AND NUTPLATE. (MARKED) (C-CHECK RO 3/14/2022) REMOVED CORRODED HARDWARE @ PAX DOOR LOWER TORQUE TUBE AND REPLACED WITH NEW STOP HARDWARE FOR STOP FITTING. REF CRJ200
- [SDR SWIA202265085](https://openairdocs.org/sdr/SWIA202265085.md): None · corroded · Jan 10, 2022 · N854AS · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > *CORROSION ON STANDOFF ATTACHED TO RH FLOOR SILL BETWEEN FS 574.00 €“ 589.00, RBL 36 €“ 45 (C-CHECK RO 3/14/2022) REMOVED AND INSTALLED NEW STANDOFF AT RH FLOOR SILL BETWEEN FS574.00- 589.00 RBL45. REF. CRJ 200 SRM 51-45-00
- [SDR SWIA202265084](https://openairdocs.org/sdr/SWIA202265084.md): None · corroded · Jan 10, 2022 · N854AS · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > *CORROSION ON 2EA STANDOFFS ATTACHED TO RH FLOOR SILL BETWEEN FS 409.00+112 €“ 409.00+128 (C-CHECK RO 3/14/2022) REMOVED AND REPLACED NEW STANDOFFS 2 EA ATTACHED TO RH FLOOR SILL BETWEEN FS 409.00+112 €“ 409.00+128 REF. CRJ 200 SRM 51-45-00
- [SDR SWIA202265083](https://openairdocs.org/sdr/SWIA202265083.md): None · corroded · Jan 10, 2022 · N854AS · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > *CORROSION ON FLOOR SUPPORT BEAM AT FS 333.00 BETWEEN RBL 27 €“ 36 (C-CHECK RO 3/14/2022) REMOVED CORROSION ON FLOOR SUPPORT BEAM AT FS 333.00 BETWEEN RBL 27 TO 36 REF: CRJ-200 SRM 51-21-06 / FOUND TO BE OUT OF LIMITS REF CRJ 200 SRM 53-00-00. MEASURED
- [SDR SWIA202265071](https://openairdocs.org/sdr/SWIA202265071.md): None · corroded · Jan 10, 2022 · N854AS · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > *CORROSION ON FLOOR SEAT TRACK RBL9 BETWEEN FS 349.00 €“ 409.00+128. AREAS MARKED (C-CHECK RO 3/14/2022) REMOVED AND REPLACED 2 EA. FLOOR SEAT RAILS FROM APPROX. FS 349.00 TO FS409+128 AT RBL 9.0 REF: CRJ-200 AMM 53-01-11-000-802 AND CRJ-200 AMM 53-01-
- [SDR SWIA202265039](https://openairdocs.org/sdr/SWIA202265039.md): None · corroded · Jan 10, 2022 · N854AS · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > RH PRESSURE FLOOR SILL FS409.0+128 TO FS559.0 HAS MULTIPLE AREAS OF CORROSION (MARKED) (C-CHECK RO 3/14/2022) REMOVED CORROSION R/H PRESSURE FLOOR SILL PANEL FS 409.0+128 TO FS 559.0 REF MHIRJ REO 601R-53-41-666 REV-C DATE-2012-11-06 / COMPLIED WITH RE
- [SDR SWIA202265038](https://openairdocs.org/sdr/SWIA202265038.md): None · corroded · Jan 10, 2022 · N854AS · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > LH PRESSURE FLOOR SILL FS409.0+128 TO FS559.0 HAS MULTIPLE AREAS OF CORROSION (MARKED) (C-CHECK RO 3/14/2022) REMOVED CORROSION L/H PRESSURE FLOOR SILL PANEL FS 409.0+128 TO FS 559.0 REF REO 601R-53-41-666 REV-C DATE-2012-11-06.COMPLIED WITH REO 601R-
- [SDR SWIA202265037](https://openairdocs.org/sdr/SWIA202265037.md): None · corroded · Jan 10, 2022 · N854AS · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > *CORROSION ON RH FLOOR SILL BETWEEN FS 559.00+80 €“ APPROX. 559.00+96 (C-CHECK RO 3/14/2022) BLENDED RH FLOOR SILL BETWEEN FS559.00+80 TO APPROX. FS559.00+96 IN LIMITS AND RESTORED REF CRJ200 SRM 51-42-15, CRJ200 SRM 51-21-06, CRJ200 SRM 53-51-43, CRJ20
- [SDR SWIA202265036](https://openairdocs.org/sdr/SWIA202265036.md): None · corroded · Jan 10, 2022 · N854AS · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > *CORROSION ON RH FLOOR SILL BETWEEN FS 559.00 €“ APPROX 559.00+80 (C-CHECK RO 3/14/2022) REMOVED CORROSION FROM RH FLOOR SILL BETWEEN FS559.00-559.00+80 IAW CRJ200 SRM 51-21-06-00.INTERCOSTAL AT 559-559+16 FOUND TO BE OUT OF LIMITS REF CRJ 200 SRM 53-
- [SDR SWIA202265035](https://openairdocs.org/sdr/SWIA202265035.md): None · corroded · Jan 10, 2022 · N854AS · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > *CORROSION ON LH FLOOR SILL BETWEEN FS 559.00 €“ 559.00+80 (C-CHECK RO 3/14/2022) REPAIRED AFT CABIN LEFTHAND FLOOR SILL BETWEEN FS559.00 TO FS559.00+80 ON LEFTHAND SIDE IAW REO 601R-53-00-526 REV -- DATE 22-MAY-2013 STEPS. 1-7 (SEE CONTINUATION SHEET F
- [SDR SWIA202265034](https://openairdocs.org/sdr/SWIA202265034.md): None · corroded · Jan 10, 2022 · N854AS · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > *CORROSION ON LH FLOOR SILL BETWEEN FS 349.00 €“ AFT OF 409.00 (C-CHECK RO 3/14/2022) REPAIRED FORWARD CABIN FLOOR SILL ON LEFTHAND SIDE BETWEEN FS349.00 TO FS409.00 IAW REO 601R-53-00-530 REV -A DATE 2014-10-07 STEPS.1-9 (SEE CONTINUATION SHEET FOR FUR
- [SDR SWIA202265033](https://openairdocs.org/sdr/SWIA202265033.md): None · corroded · Jan 10, 2022 · N854AS · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > *CORROSION ON LH FLOOR SILL SUPPORT AT FS 349.00 (C-CHECK RO 3/14/2022) REPAIRED FORWARD CABIN FLOOR SILL SUPPORT ON LEFTHAND SIDE AT FS349.00 IAW REO 601R-53-00-530 REV -A DATE 2014-10-07 STEPS.1-9 (SEE CONTINUATION SHEET FOR FURTHER DETAILS)
- [SDR SWIA202265032](https://openairdocs.org/sdr/SWIA202265032.md): None · corroded · Jan 10, 2022 · N854AS · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > *CORROSION ON FLOOR SUPPORT BEAM AT FS 349.00, APPROX. LBL36 (C-CHECK RO 3/14/2022) REMOVED CORROSION AT FLOOR SUPPORT BEAM AT FS 349.00 APPROX. LBL 36 REF: CRJ-200 SRM 51-21-06 / NOMINAL THICKNESS OF 0.063" REF CRJ 200 SRM 53-21-15 FIGURE 5. REMAINING T
- [SDR SWIA202265031](https://openairdocs.org/sdr/SWIA202265031.md): None · corroded · Jan 10, 2022 · N854AS · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > *CORROSION ON LH FLOOR SILL DOUBLER BETWEEN FS 310.00 €“ 295.00 (C-CHECK RO 3/14/2022) REPAIRED FORWARD CABIN FLOOR SILL DOUBLER BETWEEN FS295.00 TO FS310.00 ON LEFTHAND SIDE IAW REO 601R-53-00-530 REV -A DATE 2014-10-07 STEPS. 1-9 (SEE CONTINUATION SHE
- [SDR SWIA202265030](https://openairdocs.org/sdr/SWIA202265030.md): None · corroded · Jan 10, 2022 · N854AS · Cndair CL6002B19 · Fuselage Structure (General)
  > *CORROSION ON STOWAGE AFT OTBD FLOOR MOUNT DOUBLER LBL 36 (C-CHECK RO 3/14/2022) REMOVED CORROSION FROM AFT OTBD FLOOR MOUNT DOUBLER LBL 36 REF: CRJ-200 SRM 51-21-06. FOUND TO BE IN LIMITS REF CRJ200 SRM 53-00-00, SEE CONTINUATION CARD FOR DETAILS OF WOR
- [SDR SWIA202265029](https://openairdocs.org/sdr/SWIA202265029.md): None · damaged · Jan 10, 2022 · N854AS · Cndair CL6002B19 · Wing, Rib/Bulkhead
  > COMPLY WITH AD 2002-03-14/10 REPAIR OF RIGHT SIDE LOWER WING PLANK DUE BEFORE FURTHER FLIGHT. (C-CHECK RO 3/14/2022) COMPLIED WITH PARAGRAPH (B) OF AD 2002-03-14 BY REPAIRING CRACK ON THE RIGHT SIDE LOWER WING PLANK BEFORE FURTHER FLIGHT PER A METHOD APP
- [SDR SWIA202265028](https://openairdocs.org/sdr/SWIA202265028.md): None · corroded · Jan 10, 2022 · N854AS · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > *CORROSION ON FS 280.00 FWD FLOOR BEAM ANGLE BETWEEN RBL 9 €“ LBL 9 (C-CHECK RO 3/14/2022) REPLACED FLOOR SUPPORT ANGLE P/N600-34017-351 ON FLOOR BEAM AT FS280.00 BETWEEN LBL9 AND RBL9 PER REF CRJ200 SRM 51-42-06 AND DRAWING 600-34017 REV AD / COMPLIED
- [SDR SWIA202265027](https://openairdocs.org/sdr/SWIA202265027.md): None · corroded · Jan 10, 2022 · N854AS · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > *CORROSION ON RH FLOOR SILL BETWEEN FS 295.00 €“ 310.00 (C-CHECK RO 3/14/2022) BLENDED RH FLOOR SILL BETWEEN FS295 TO FS310 IN LIMITS AND RESTORED REF CRJ200 SRM 51-42-06, CRJ200 SRM 51-21-06, CRJ200 SRM 53-21-43, CRJ200 SRM 51-25-16, CRJ200 SRM 51-42-1
- [SDR SWIA202265026](https://openairdocs.org/sdr/SWIA202265026.md): None · corroded · Jan 10, 2022 · N854AS · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > *CORROSION ON RH FLOOR SILL DOUBLER BETWEEN FS 310.00 €“ 319.00 (C-CHECK RO 3/14/2022) BLENDED CORROSION ON RH FLOOR SILL DOUBLER BETWEEN FS 310.00-319.00 PER REF CRJ 200 SRM 51-12-00 / FOUND TO BE OUT OF LIMITS / REMOVED AND INSTALLED NEW RH FLOOR SIL
- [SDR SWIA202265025](https://openairdocs.org/sdr/SWIA202265025.md): None · corroded · Jan 10, 2022 · N854AS · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > *CORROSION ON RH FLOOR SILL SUPPORT AFT OF FS 349.00 (C-CHECK RO 3/14/2022) BLENDED CORROSION ON RH FLOOR SILL AFT OF FS 349.00 PER REO 601R-53-00-530 REV -A DATE 2014-10-07. FOUND TO BE IN LIMITS REF REO 601R-53-00-530 REV -A DATE 2014-10-07. COMPLIED
- [SDR SWIA202265070](https://openairdocs.org/sdr/SWIA202265070.md): None · damaged · Jan 9, 2022 · N854AS · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > *RIGHT SIDE SEAT RAIL STRUCTURE APPROX FS544.00 THRU FS559.00+80 HAS PITTING AND SCRATCH'S. (C-CHECK RO 3/14/2022) REMOVED CORROSION ON R/H SIDE SEAT RAIL BETWEEN FS544.00 TO FS559.00+80 REF: CRJ-200 SRM 51-21-06. FOUND TO BE OUT OF LIMITS. REF: CRJ-200
- [SDR SWIA202265069](https://openairdocs.org/sdr/SWIA202265069.md): None · damaged · Jan 9, 2022 · N854AS · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > *RIGHT SIDE SEAT RAIL STRUCTURE APPROX FS499.00 THRU FS544.00 HAS PITTING AND SCRATCH'S. (C-CHECK RO 3/14/2022) REMOVED CORROSION ON R/H SIDE SEAT RAIL BETWEEN FS499.00 TO FS544.00. REF: CRJ-200 SRM 51-21-06. FOUND TO BE OUT OF LIMITS. REF: CRJ-200 SRM
- [SDR SWIA202265068](https://openairdocs.org/sdr/SWIA202265068.md): None · corroded · Jan 9, 2022 · N854AS · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > *RIGHT SIDE SEAT RAIL STRUCTURE APPROX FS409.00+112 THRU FS449.85 HAS PITTING AND CORRODED AROUND SCREWS. (C-CHECK RO 3/14/2022) REMOVED CORROSION ON SIDE SEAT RAIL BETWEEN FS409.00+112 TO FS449.85 ON RIGHTHAND SIDE IAW CRJ 200 SRM 51-21-06. FOUND TO BE
- [SDR SWIA202265067](https://openairdocs.org/sdr/SWIA202265067.md): None · corroded · Jan 9, 2022 · N854AS · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > *RIGHT SIDE SEAT RAIL STRUCTURE APPROX FS409.00+16 THRU FS409.112 HAS PITTING AND CORRODED AROUND SCREWS. (C-CHECK RO 3/14/2022) REMOVED CORROSION ON SIDE SEAT RAIL BETWEEN FS409.00+16 TO FS409+112 ON RIGHT HAND SIDE IAW CRJ 200 SRM 51-21-06. FOUND TO BE
- [SDR SWIA202265066](https://openairdocs.org/sdr/SWIA202265066.md): None · corroded · Jan 9, 2022 · N854AS · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > * RIGHT SIDE SEAT RAIL STRUCTURE APPROX FS364.00 THRU FS409.00 HAS PITTING AND CORRODED AROUND SCREWS. (C-CHECK RO 3/14/2022) REPLACED RIGHT SIDE SEAT RAIL STRUCTURE APPROX. FS364.00 TO FS409.00 REF REO 601R-53-00-055 REV.-C DATED 2017-03-21 ALL STEPS CO
- [SDR SWIA202265065](https://openairdocs.org/sdr/SWIA202265065.md): None · corroded · Jan 9, 2022 · N854AS · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > *LEFT SIDE SEAT RAIL STRUCTURE AFT OF FS499.00 HAS MULTIBLE AREA'S CHAFING AND GOUGES. (C-CHECK RO 3/14/2022) FOUND LH SIDE SEAT RAIL FROM FS 499 TO FS 599 OUT OF LIMITS REF CRJ 200 SRM 53-21-49 AND INSTALLED NEW SIDE SEAT RAIL REF CRJ 200 AMM 53-01-11-4
- [SDR SWIA202265064](https://openairdocs.org/sdr/SWIA202265064.md): None · corroded · Jan 9, 2022 · N854AS · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > *LEFT HAND SIDE SEAT RAIL CORRODED IN MULTIPLE AREA'S APPROX FS449.85 THRU FS499.00. (C-CHECK RO 3/14/2022).REMOVED CORROSION FROM L/H SIDE SEAT RAIL FROM APPROX. FS449.85 THRU FS499.00 REF: CRJ-200 SRM 51-21-06. FOUND TO BE OUT OF LIMITS. REF: CRJ-200
- [SDR SWIA202265063](https://openairdocs.org/sdr/SWIA202265063.md): None · corroded · Jan 9, 2022 · N854AS · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > *LEFT HAND SIDE SEAT RAIL CORRODED IN MULTIPLE AREA'S APPROX FS409.00+112 THRU FS449.85. (C-CHECK RO 3/14/2022) REMOVED CORROSION FROM LH SIDEWALL SEAT RAIL FS409.00+112 TO FS449.85 BY BLENDING IAW CRJ200 SRM 51-21-06 FOUND TO BE OUT OF LIMITS PER SRM 5
- [SDR SWIA202265062](https://openairdocs.org/sdr/SWIA202265062.md): None · corroded · Jan 9, 2022 · N854AS · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > *LEFT HAND SIDE SEAT RAIL CORRODED IN MULTIPLE AREA'S APPROX FS409.00+16 THRU FS409.00+112. (C-CHECK RO 3/14/2022) REMOVED CORROSION FROM LH SIDEWALL SEAT RAIL FS409.00+16 TO FS409.00+112 BY BLENDING IAW CRJ200 SRM 51-21-06 FOUND TO BE OUT OF LIMITS PER
- [SDR SWIA202265061](https://openairdocs.org/sdr/SWIA202265061.md): None · corroded · Jan 9, 2022 · N854AS · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > *LEFT HAND SIDE SEAT RAIL CORRODED IN MULTIPLE AREA'S FS364.00 THRU FS409.00+16. (C-CHECK RO 3/14/2022) REMOVED CORROSION FROM LH SIDEWALL SEAT RAIL FS364.00 TO FS409.00+16 BY BLENDING IAW CRJ200 SRM 51-21-06 FOUND TO BE OUT OF LIMITS PER SRM 53-21-49 RE

Next page: https://openairdocs.org/aircraft/N854AS/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 = 'N854AS' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N854AS/reports

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