# Service difficulty reports: N881AS

A list on [N881AS](https://openairdocs.org/aircraft/N881AS.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 5 · 206 reports

- [SDR SWI20240729000606](https://openairdocs.org/sdr/SWI20240729000606.md): Switch · damaged · Jul 28, 2024 · N881AS · Cndair CL6002B19 · Cabin Cooling System
  > R PACK HIGH TEMP CAUTION IN CLIMB CAUSING DEPRESSURIZATION (FLIGHT 4688 - FILED CLOSED)TROUBLESHOT RH PACK REF FIM 21-50-00. FOUND THE RH PACK COMPRESSOR OVERTEMPERATURE SWITCH DAMAGED CAUSING INTERMITTENT R PAK HIGH TEMP CAUTION MESSAGE. REMOVED AND REPLACED
- [SDR SWIA202403040002](https://openairdocs.org/sdr/SWIA202403040002.md): Landing Gear · warning message · Mar 2, 2024 · N881AS · Cndair CL6002B19 · Landing Gear Position and Warning
  > *CAT II DOWNGRADED*D:GEAR DISAGREE MOMENTARILY ON APPROACH WHEN EXTENDING GEAR AROUND 200KTS. GEAR INDICATED 3 DOWN. RAN QRH. DID NOT RETRACT GEARC:MEL 32-30-1CAT "A" DUE IN 1 FLT DAYMX ACTION COMPLIED WITHGEAR DISAGREE MOMENTARILY ON APPROACH WHEN EXTENDING G
- [SDR SWIA202266912](https://openairdocs.org/sdr/SWIA202266912.md): Blades · damaged · Nov 27, 2022 · N881AS · Cndair CL6002B19 · Cylinder Head Temperature (CHT) Indicating System
  > NR 2 ENGINE SEIZED ON CLIMB OUT. LOUD AGGRESSIVE BANG FROM ENGINE. ITT IN THE RED. N1 ROLLED BACK. RAN QRC QRH FOR SEVERE ENGINE FAILURE IN FLIGHT. SHUT DOWN ENGINE. NO OVERWEIGHT LANDING. NORMAL LANDING. (FLIGHT 5405) DUE TO RT ENGINE EXPERIENCING AN UNRECOV
- [SDR SWIA202266426](https://openairdocs.org/sdr/SWIA202266426.md): None · failed · Sep 5, 2022 · N881AS · Cndair CL6002B19 · Pneumatic System
  > L 14TH DUCT WARNING MESSAGE. QRH PROCEDURE DID NOT CLEAR MESSAGE. RETURNED TO KPSC AS DIRECTED BY QRH (FLIGHT #5788 FILED CLOSED) INSPECTED L/H 14TH STAGE DUCTS IN AFT EQUIPMENT BAY REFERENCING CRJ 200 AMM TASK 36-12-04, FOUND CONNECTION BETWEEN DUCT AND S
- [SDR SWIA202265647](https://openairdocs.org/sdr/SWIA202265647.md): None · failed · May 23, 2022 · N881AS · Cndair CL6002B19 · Landing Gear Door Actuator
  > NOSE GEAR DISAGREE AND NOSE DOOR OPEN WARNING MESSAGE ON APPROACH. RAN QRH. REQUIRED MANUAL GEAR EXTENSION. WARNING MESSAGES EXTINGUISHED FOLLOWED BY A PRECAUTIONARY LANDING (FLIGHT 5247 - FILED CLOSED) REMOVED AND REPLACED NLG SELECTOR VOVLE PER CRJ200
- [SDR SWIA2021073059789](https://openairdocs.org/sdr/SWIA2021073059789.md): Spoiler Sys · faulted · Jul 28, 2021 · N881AS · Cndair CL6002B19 · Drag Control System
  > D:GND SPLR DEPLOY SHORT FINAL. QRH COMPLIED WITH. / C: MEL 27-65-1B / CAT C DUE ON 08/07/2021 / GND SPLR DEPLOY SHORT FINAL. QRH COMPLIED WITH. (FLIGHT 5856 - FILED CLOSED) JUL 28, 2021 STATION: SFO--CREW REPORTED NO OVERWEIGHT LANDING, DID NOT DEPLOY MAS
- [SDR SWIA2021073059841](https://openairdocs.org/sdr/SWIA2021073059841.md): Intercostal · cracked · Jun 24, 2021 · N881AS · Cndair CL6002B19 · Fuselage Main, Structure
  > PRESSURE FLOOR INTERCOSTAL K601R38908-2001 AT FS460 HAS CRACK AT LBL9 ATTACH FASTENER HOLE. (C-CHECK RO 7/27/2021) REPAIRED PRESSURE FLOOR INTERCOSTAL K601R38908-2001 AT FS460.00 BETWEEN LBL9 & LBL18. REF REO 601R-53-41-2940 REV -- DATED 2021-06-29, CR
- [SDR SWIA2021073059840](https://openairdocs.org/sdr/SWIA2021073059840.md): Drag Angle · elongated · Jun 22, 2021 · N881AS · Cndair CL6002B19 · Passenger/Crew Doors
  > MULTIPLE ELONGATED HOLES ON AFT PAX DOOR DRAG ANGLE. (C-CHECK RO 7/27/2021) REMOVED, REPLACED, AND INSTALLED PAX DOOR AFT, DRAG ANGLE REF. CRJ200 SRM 51-42-06, CRJ200 SRM 51-42-13, AND DWG 601R31707 REV -E. COMPLIED WITH 51-900-1003-SKY
- [SDR SWIA2021073059839](https://openairdocs.org/sdr/SWIA2021073059839.md): Web · cracked · Jun 19, 2021 · N881AS · Cndair CL6002B19 · Passenger/Crew Doors
  > CRACK ON AFT PAX DOOR WEB WHERE STEP PANEL 832DT AND TOP PANEL MEET. (C-CHECK RO 7/27/2021) REMOVED AND REPLACED NEW AFT PAX DOOR WEB P/N 601R31707-11S INSTALLED REF BOMBARDIER REO 601R-52-11-702 REV -E DATED 2016-08-14 AND BOMBARDIER DWG 601R31707 R
- [SDR SWIA2021073059838](https://openairdocs.org/sdr/SWIA2021073059838.md): Landing · damaged · Jun 17, 2021 · N881AS · Cndair CL6002B19 · Wing, Plate/Skin
  > THE CUT-OUT/LAND FOR PANEL 572AL HAS 2EA. ELONGATED HOLES. (C-CHECK RO 7/27/2021) REPAIRED THE CUT OUT LAND FOR PANEL 572AL REF REO 601R-57-31-1368 REV -- 2021-07-12, SKYCARD 51-900-1003 STRUCTURAL MAJOR REPAIR COMPLIED WITH.
- [SDR SWIA2021073059837](https://openairdocs.org/sdr/SWIA2021073059837.md): Bracket · corroded · Jun 16, 2021 · N881AS · Cndair CL6002B19 · Passenger/Crew Doors
  > CORROSION ON PAX DOOR BRACKET, COMMON TO DD4 AFT INTERCOSTAL (C-CHECK RO 7/27/2021) REMOVED AND INSTALLED NEW PAX DOOR BRACKET COMMON TO DD4 AFT INTERCOSTAL. REF DWG# 601R31702 REV -N & CRJ200 SRM 51-42-06. COMPLIED WITH TASK CARD 51-900-1003-SKY. PRES
- [SDR SWIA2021073059836](https://openairdocs.org/sdr/SWIA2021073059836.md): Bracket · corroded · Jun 16, 2021 · N881AS · Cndair CL6002B19 · Passenger/Crew Doors
  > CORROSION ON PAX DOOR BRACKET, COMMON TO DD6 AFT INTERCOSTAL (C-CHECK RO 7/27/2021) REMOVED AND INSTALLED NEW PAX DOOR BRACKET COMMON TO DD6 AFT INTERCOSTAL. REF DWG# 601R31702 REV -N & CRJ200 SRM 51-42-06. COMPLIED WITH TASK CARD 51-900-1003-SKY. PRES
- [SDR SWIA2021073059835](https://openairdocs.org/sdr/SWIA2021073059835.md): Intercostal · corroded · Jun 16, 2021 · N881AS · Cndair CL6002B19 · Passenger/Crew Doors
  > CORROSION ON PAX DOOR, DD7 AFT INTERCOSTAL (C-CHECK RO 7/27/2021) REMOVED AND INSTALLED NEW DD7 AFT INTERCOSTAL. REF DWG# 601R31702 REV -N & CRJ200 SRM 51-42-06. COMPLIED WITH TASK CARD 51-900-1003-SKY. PRESSURE LEAK CHECK WAS SATISFACTORY. SEE CONTIN
- [SDR SWIA2021073059834](https://openairdocs.org/sdr/SWIA2021073059834.md): Intercostal · corroded · Jun 11, 2021 · N881AS · Cndair CL6002B19 · Passenger/Crew Doors
  > CORROSION ON PAX DOOR CENTER INTERCOSTAL DD6, FS327.763 (C-CHECK RO 7/27/2021) REMOVED AND REPLACED PAX DOOR CENTER INTERCOSTAL DD6 REF CRJ200 SRM 51-42-06, 51-42-21 AND DWG 601R31702 REV N. ALL CHECKS GOOD. SEE CONTINUAION CARD FOR FULL DETAILS. COMPL
- [SDR SWIA2021073059833](https://openairdocs.org/sdr/SWIA2021073059833.md): Former · corroded · Jun 11, 2021 · N881AS · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR CORROSION ON EXSISTING FORMER REPAIR FS347.27 UNDER AFT GUIDE PULLEY MOUNT BETWEEN INTERCOSTALS DD4 AND DD5 (C-CHECK RO 7/27/2021) REMOVED AND REPLACED PAX DOOR FORMER AT FS 347.37 REF CRJ200 SRM 51-42-06, CRJ200 SRM 51-42-21, AND DWG 601R3170
- [SDR SWIA2021073059832](https://openairdocs.org/sdr/SWIA2021073059832.md): Intercostal · damaged · Jun 11, 2021 · N881AS · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL FWD DD4 HAS A DRILL START LOCATED ON UPPERFLANGE (C-CHECK RO 7/27/2021) REMOVED AND REPLACED FWD DD4 INTERCOSTAL REF CRJ200 SRM 51-42-06 AND DWG 601R31702 REV -N. ALL CHECKS GOOD. SEE CONTINUATION CARD FOR FULL DTAILS. COMPLIED WI
- [SDR SWIA2021073059831](https://openairdocs.org/sdr/SWIA2021073059831.md): Gusset · corroded · Jun 8, 2021 · N881AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PASSENGER DOOR SURROUND STRUCTURE GUSSET CORRODED FS310.00 APPROX. WL144.18. (MARKED) (C-CHECK RO 7/27/2021) REMOVED AND INSTALLED REPLACEMENT GUSSET WITH REPLACEMENT FASTENERS REF DRW. 601R31096 REV D. AND REF CRJ200 SRM 51-42-06. FOUND TO OUT OF LIMIT
- [SDR SWIA2021073059830](https://openairdocs.org/sdr/SWIA2021073059830.md): Gusset · corroded · Jun 8, 2021 · N881AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PASSENGER DOOR SURROUND STRUCTURE GUSSET CORRODED FS310.00 APPROX. WL135.681. (MARKED) (C-CHECK RO 7/27/2021) CORROSION ON GUSSET PASSENGER DOOR SURROUND STRUCTURE GUSSET FS310.00 APPROX. WL135.681 IS AROUND FASTENER HOLES AND IS OUT OF LIMITS REF CRJ20
- [SDR SWIA2021073059829](https://openairdocs.org/sdr/SWIA2021073059829.md): Gusset · corroded · Jun 8, 2021 · N881AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PASSENGER DOOR SURROUND STRUCTURE GUSSET CORRODED FS310.00 APPROX. STRG. 9. (MARKED) (C-CHECK RO 7/27/2021) CORROSION ON GUSSET PASSENGER DOOR SURROUND STRUCTURE GUSSET FS310.00 APPROX. STRG. 9 IS AROUND FASTENER HOLES AND IS OUT OF LIMITS REF CRJ200 SR
- [SDR SWIA2021073059828](https://openairdocs.org/sdr/SWIA2021073059828.md): Gusset · corroded · Jun 8, 2021 · N881AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PASSENGER DOOR SURROUND STRUCTURE GUSSET CORRODED FS310.00 APPROX. WL115.07. (MARKED) (C-CHECK RO 7/27/2021) CORROSION ON GUSSET PASSENGER DOOR SURROUND STRUCTURE GUSSET FS310.00 APPROX. WL115.07 IS AROUND FASTENER HOLES AND IS OUT OF LIMITS REF CRJ200
- [SDR SWIA2021073059827](https://openairdocs.org/sdr/SWIA2021073059827.md): Gusset · corroded · Jun 7, 2021 · N881AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > *PASSENGER DOOR SURROUND STRUCTURE GUSSET CORRODED FS310.00 BETWEEN STGR14L & STGR15L. (MARKED) (C-CHECK RO 7/27/2021) CORROSION ON GUSSET PASSENGER DOOR SURROUND STRUCTURE GUSSET FS310.00 STGR14L & STGR15L IS AROUND FASTENER HOLES AND IS OUT OF LIMITS
- [SDR SWIA2021073059826](https://openairdocs.org/sdr/SWIA2021073059826.md): Gusset · corroded · Jun 7, 2021 · N881AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > *PASSENGER DOOR SURROUND STRUCTURE GUSSET CORRODED FS310.00 BETWEEN STGR12L & STGR13L. (MARKED) (C-CHECK RO 7/27/2021) REMOVED AND INSTALLED NEW PASSENGER DOOR SURROUND STRUCTURE GUSSET. FS310.00 BETWEEN STGR12L & STGR13L RESTORED FINISH AND APPLIED CIC
- [SDR SWIA2021073059825](https://openairdocs.org/sdr/SWIA2021073059825.md): Gusset · corroded · Jun 7, 2021 · N881AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > *PASSENGER DOOR SURROUND STRUCTURE GUSSET CORRODED FS310.00 BETWEEN STGR11L & STGR12L. (MARKED) (C-CHECK RO 7/27/2021) REMOVED AND INSTALLED NEW PAX DR SURROUND GUSSET AT FS310 BETWEEN STGR 11L-12L REF CRJ 200 SRM 51-42-06 SEE CONTINUATION CARD FOR DETA
- [SDR SWIA2021073059869](https://openairdocs.org/sdr/SWIA2021073059869.md): Hinge · corroded · Jun 5, 2021 · N881AS · Cndair CL6002B19 · Elevator Structure
  > * R/H ELEVATOR #4 HINGE ON H STAB HAS CORRODED HARDWARE (C-CHECK RO 7/27/2021) REMOVED AND REPLACED HARDWARE ON R/H ELEVATOR #4 HINGE ON H STAB REF CRJ 200 SRM 51-41-02
- [SDR SWIA2021073059868](https://openairdocs.org/sdr/SWIA2021073059868.md): Hinge · corroded · Jun 5, 2021 · N881AS · Cndair CL6002B19 · Elevator Structure
  > * R/H ELEVATOR #3 HINGE ON H STAB HAS CORRODED HARDWARE (C-CHECK RO 7/27/2021) INSTALLED NEW BONDING JUMPER AND HARDWARE ON RH ELEVATOR #3 HINGE BONDING TEST GOOD REF CRJ 200 AMM 51-80-00-400-802, SEE CONTINUATION CARD FOR DETAILS.
- [SDR SWIA2021073059867](https://openairdocs.org/sdr/SWIA2021073059867.md): Hinge · corroded · Jun 5, 2021 · N881AS · Cndair CL6002B19 · Elevator Structure
  > * R/H ELEVATOR #2 HINGE ON H STAB HAS CORRODED HARDWARE (C-CHECK RO 7/27/2021) REMOVED AND REPLACED HARDWARE ON R/H ELEVATOR #2 HINGE ON H STAB REF CRJ 200 SRM 51-41-02
- [SDR SWIA2021073059866](https://openairdocs.org/sdr/SWIA2021073059866.md): Hinge · corroded · Jun 5, 2021 · N881AS · Cndair CL6002B19 · Elevator Structure
  > * L/H ELEVATOR #4 HINGE ON H STAB HAS CORRODED HARDWARE (C-CHECK RO 7/27/2021) REMOVED AND REPLACED HARDWARE ON L/H ELEVATOR #4 HINGE ON H STAB REF CRJ 200 SRM 51-41-02
- [SDR SWIA2021073059865](https://openairdocs.org/sdr/SWIA2021073059865.md): Hinge · corroded · Jun 5, 2021 · N881AS · Cndair CL6002B19 · Elevator Structure
  > * L/H ELEVATOR #3 HINGE ON H STAB HAS CORRODED HARDWARE (C-CHECK RO 7/27/2021) INSTALLED NEW BONDING JUMPER AND HARDWARE. BONDING TEST GOOD REF CRJ 200 AMM 51-80-00-400-802
- [SDR SWIA2021073059864](https://openairdocs.org/sdr/SWIA2021073059864.md): Hinge · corroded · Jun 5, 2021 · N881AS · Cndair CL6002B19 · Elevator Structure
  > * L/H ELEVATOR #2 HINGE ON H STAB HAS CORRODED HARDWARE (C-CHECK RO 7/27/2021) REMOVED AND REPLACED HARDWARE ON L/H ELEVATOR #2 HINGE ON H STAB REF CRJ 200 SRM 51-41-02
- [SDR SWIA2021073059863](https://openairdocs.org/sdr/SWIA2021073059863.md): Hinge · corroded · Jun 5, 2021 · N881AS · Cndair CL6002B19 · Elevator Structure
  > * L/H ELEVATOR #1 HINGE ON H STAB HAS CORRODED HARDWARE (C-CHECK RO 7/27/2021) REMOVED AND REPLACED HARDWARE ON L/H ELEVATOR #1 HINGE ON H STAB REF CRJ 200 SRM 51-41-02
- [SDR SWIA2021073059824](https://openairdocs.org/sdr/SWIA2021073059824.md): Access Panel · corroded · Jun 5, 2021 · N881AS · Cndair CL6002B19 · Wing, Plate/Skin
  > *LH LOWER WING PLANK ACCESS HOLE 510AB FLANGE HAS CORROSION LOWER SIDE. (C-CHECK RO 7/27/2021) BLENDED CORROSION FROM LWR SIDE OF LH LOWER WING PLANK ACCESS HOLE 510AB FLANGE TO A SMOOTH CONTOUR AND RESTORED FINISH. REMAINING MATERIAL IN REWORKED AREAS
- [SDR SWIA2021073059823](https://openairdocs.org/sdr/SWIA2021073059823.md): Access Panel · corroded · Jun 5, 2021 · N881AS · Cndair CL6002B19 · Wing, Plate/Skin
  > *LH LOWER WING PLANK ACCESS HOLE 540BB FLANGE HAS CORROSION LOWER SIDE. (C-CHECK RO 7/27/2021) BLENDED CORROSION FROM LWR SIDE OF LH LOWER WING PLANK ACCESS HOLE 540BB FLANGE TO A SMOOTH CONTOUR AND RESTORED FINISH. REMAINING MATERIAL IN REWORKED AREAS
- [SDR SWIA2021073059822](https://openairdocs.org/sdr/SWIA2021073059822.md): Floorbeam · cracked · Jun 5, 2021 · N881AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > UPON REMOVAL STEP FOR FS 280.0 FLOOR BEAM REPAIR, FOUND CRACK ON COCKPIT FLOOR SUPPORT ANGLE. (C-CHECK RO 7/27/2021) REPLACED COCKPIT FLOOR SUPPORT ANGLE WITH NEW 600-34017-351 PO T-59936 REF BOMBARDIER DWG 600-34017 REV AD AND CRJ 200 SRM 51-42-06.
- [SDR SWIA2021073059821](https://openairdocs.org/sdr/SWIA2021073059821.md): Skin · dented · Jun 5, 2021 · N881AS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > * DENTS IN FUSELAGE SKIN FS625.30-FS640.00 BETWEEN STGR22L & STGR21L (C-CHECK RO 7/27/2021) REPAIRED DENTED FUSELAGE SKIN FROM FS621.00 TO FS640.00 BETWEEN STGR21L & STGR22L. REF REO 601R-53-61-7677 REV -- DATED 2021-07-05, CRJ200 SRM 51-42-21, & CRJ200
- [SDR SWIA2021073059820](https://openairdocs.org/sdr/SWIA2021073059820.md): Skin · chafed · Jun 4, 2021 · N881AS · Cndair CL6002B19 · Wing, Plate/Skin
  > LH LOWER WING SKIN HAS CHAFING DAMAGE BY FLAP ACTUATOR FARING 583AB AND 586AB AS MARKED. (C-CHECK RO 7/27/2021) BLENDED AND REMOVED CHAFING DAMAGE ON LOWER WING SKIN COMMON TO FAIRINGS 583AB AND 586AB. REF. CRJ200 SRM 51-12-00 / NO DAMAGE ALLOWED IAW CR
- [SDR SWIA2021073059819](https://openairdocs.org/sdr/SWIA2021073059819.md): Hinge Arm · damaged · Jun 4, 2021 · N881AS · Cndair CL6002B19 · Trailing Edge Flaps
  > *L/H INBD FLAP, INBD HINGE ARM, HAS FOD DAMAGE AT HINGE LOCATION ON ARM. (AREA MARKED) (C-CHECK RO 7/27/2021) REPAIRED AREA L/H INBD FLAP, INBD HINGE ARM, FOD DAMAGE AT HINGE LOCATION ON ARM BY COMPLYING WITH REO 601R-57-54-330 REV-- DATED 2021-06-16 (S
- [SDR SWIA2021073059818](https://openairdocs.org/sdr/SWIA2021073059818.md): Door Sill · cracked · Jun 4, 2021 · N881AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > *AFT SIDE LOWER SILL PAX DOOR FS 364.00 BETWEEN STRG 17L AND 18L UNDER SIDE HAS A POSSIBLE CRACK AT INBOARD FASTENER FOR AFT CLEAT AS MARKED. (C-CHECK RO 7/27/2021) REPAIRED PAX DOOR LWR LONGERON BETWEEN FS349.00 AND FS364.00. REF REO 601R-53-21-3461 R
- [SDR SWIA2021073059817](https://openairdocs.org/sdr/SWIA2021073059817.md): Access Panel · elongated · Jun 3, 2021 · N881AS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FASTENER HOLES AROUND LH FWD ACCESS PANEL 131AL ARE ELONGATED AS MARKED (C-CHECK RO 7/27/2021) REPAIRED FASTENER HOLES AROUND LH FWD ACCESS PANEL 131AL REF REO 601R-53-11-3703 REV €“ DATED 2021-06-18 STEPS 1-11. ALL STEPS COMPLIED WITH. COMPLIED WITH
- [SDR SWIA2021073059816](https://openairdocs.org/sdr/SWIA2021073059816.md): Bulkhead Web · cracked · Jun 3, 2021 · N881AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > PERFORM A FULL REPAIR TO BULKHEAD WEB FS 280.0 LBL 20.75 TO RBL 20.75 PER REO 601R-53-11-926 REV B DATED 2006/05/10,DUE TO CRACK TO LONG OUT OF LIMIT FOR LOCAL REPAIR. (C-CHECK RO 7/27/2021) PERFORMED A FULL REPAIR TO BULKHEAD WEB FS 280.0 LBL 20.75
- [SDR SWIA2021073059862](https://openairdocs.org/sdr/SWIA2021073059862.md): Anchor Fitting · corroded · Jun 2, 2021 · N881AS · Cndair CL6002B19 · Passenger/Crew Doors
  > * PAX DOOR AFT ANCHOR FITTING HAS CORRODED HARDWARE. FLAGGED (C-CHECK RO 7/27/2021) REMOVED AND INSTALLED NEW HARDWARE TO PAX DOOR AFT ANCHOR TORQUE LEVEL 35LB TUC4978 CAL DUE 30-JUN-21 REF CRJ 200 AMM 52-11-17-000-802 AND 52-11-17-400-802
- [SDR SWIA2021073059861](https://openairdocs.org/sdr/SWIA2021073059861.md): Anchor Fitting · corroded · Jun 2, 2021 · N881AS · Cndair CL6002B19 · Passenger/Crew Doors
  > * PAX DOOR FWD ANCHOR FITTING HAS CORRODED HARDWARE. FLAGGED (C-CHECK RO 7/27/2021) REMOVED AND REPLACED PAX DOOR FWD ANCHOR FITTING AND CORRODED HARDWARE WITH A SERVICEABLE FWD ANCHOR FITTING AND NEW ATTACHMENT HARDWARE IAW CRJ-200 AMM 52-11-17-000-80
- [SDR SWIA2021073059815](https://openairdocs.org/sdr/SWIA2021073059815.md): Floor Support · corroded · Jun 2, 2021 · N881AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > * MULTIPLE CORROSION SPOTS FOUND ON FLOOR BEAM APPROX F.S559.80 AT STGR25R (AREA MARKED). (C-CHECK RO 7/27/2021) REMOVED AND REPLACED RBL9 (STGR 25R) FLOORBEAM CAP BETWEEN FS559.00+5 AND FS570.00. REF REO 601R-53-51-593 REV -- DATED 2021-06-16, DWG 601R
- [SDR SWIA2021073059814](https://openairdocs.org/sdr/SWIA2021073059814.md): Floor Support · corroded · Jun 2, 2021 · N881AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > * MULTIPLE SURFACE CORROSION FOUND ON FLOOR BEAM APPROX F.S409.00+32--409.00+128 AT STGR25L (AREA MARKED) (C-CHECK RO 7/27/2021) REMOVED AND INSTALLED NEW FLOOR BEAM CAP AT LBL 9.0 BETWEEN F/S 409+32 AND F/S 409-128 IAW REO 601R-53-31-1198 REV. -- DATE
- [SDR SWIA2021073059813](https://openairdocs.org/sdr/SWIA2021073059813.md): Floor Support · corroded · Jun 2, 2021 · N881AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > * MULTIPLE CORROSION SPOTS FOUND AT FLOOR BEAM APPROX F.S409.00+32-409.00+128 AT STGR25R (AREA MARKED) (C-CHECK RO 7/27/2021) REMOVED AND REPLACED RBL9 (STGR25R) FLOOR BEAM CAP BETWEEN FS409.00+32 AND FS409.00+128. REF REO 601R-53-31-1198 REV--, DATED
- [SDR SWIA2021073059812](https://openairdocs.org/sdr/SWIA2021073059812.md): Mount · corroded · Jun 2, 2021 · N881AS · Cndair CL6002B19 · Fuselage, Equipment Attach Fittings
  > *FLOOR STRUCTURE: G1 GALLEY MOUNT TOP PLATE AT APPROX FS 286 / RBL 38 HAS EVIDENCE OF CORROSION. (C-CHECK RO 7/27/2021) REMOVED AND REPLACED GALLEY PLATE P/N: 601R38669-65. FLOOR STRUCTURE G1 GALLEY AT APPROX FS 286 / RBL 38. REF: DWG# 601R38669, REV -N
- [SDR SWIA2021073059811](https://openairdocs.org/sdr/SWIA2021073059811.md): Floorbeam · corroded · Jun 2, 2021 · N881AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > *FS 349 FLOOR CROSSBEAM CAP BETWEEN RBL 27 AND RH FLOOR SILL HAS EXFOLIATION CORROSION. (C-CHECK RO 7/27/2021) REMOVED AND REPLACED ANGLE P/N 601R38783-13. FS 349 FLOOR CROSSBEAM CAP BETWEEN RBL 27 AND RH FLOOR SILL. REF DWG# 601R386651, REV --, CRJ-20
- [SDR SWIA2021073059810](https://openairdocs.org/sdr/SWIA2021073059810.md): Mount · corroded · Jun 2, 2021 · N881AS · Cndair CL6002B19 · Fuselage, Equipment Attach Fittings
  > *FLOOR STRUCTURE: ENTRANCE CABINET MOUNT TOP PLATE AT APPROX FS 308 / LBL 20 HAS EVIDENCE OF CORROSION. (C-CHECK RO 7/27/2021) REPLACED ENTRANCE CABINET MOUNT TOP PLATE AT FS308.00 & LBL 20. REF CRJ200 DWG# 601R38670 REV -T & CRJ200 SRM 51-42-13. COMPLI
- [SDR SWIA2021073059809](https://openairdocs.org/sdr/SWIA2021073059809.md): Mount · corroded · Jun 2, 2021 · N881AS · Cndair CL6002B19 · Fuselage, Equipment Attach Fittings
  > *FLOOR STRUCTURE: G1 GALLEY MOUNT TOP PLATE AT APPROX FS 317 / RBL 5 HAS EVIDENCE OF CORROSION. (C-CHECK RO 7/27/2021) REPLACED GALLEY 1 MOUNT TOP PLATE AT APPROX FS 317 / RBL 5. REF CRJ200 SRM 51-42-13 AND DWG# 601R38669 REV -N. COMPLIED WITH SKYWEST T
- [SDR SWIA2021073059846](https://openairdocs.org/sdr/SWIA2021073059846.md): Seat Track · corroded · Jun 1, 2021 · N881AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > * RIGHT SIDE SEAT RAIL STRUCTURE AFT OF FS409.0+128 HAS MULTABLE AREA'S OF CORROSION. (C-CHECK RO 7/27/2021) REMOVED AND INSTALLED NEW R/H SIDE SEAT RAIL FS409.00+112 TO FS449.00 WITH NEW HARDWARE. REF CRJ200 AMM 53-01-11-000-802 & CRJ200 AMM 53-01-11-4
- [SDR SWIA2021073059845](https://openairdocs.org/sdr/SWIA2021073059845.md): Seat Track · corroded · Jun 1, 2021 · N881AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > * LEFT SIDE SEAT RAIL STRUCTURE AFT OF FS409.0+128 IS CORRODED. MARKED WITH GREASE PENCIL (C-CHECK RO 7/27/2021) REMOVED AND INSTALLED TWO NEW SIDE SEAT TRACKS WITH NEW HARDWARE AFT OF FS409.00+128. REF CRJ200 AMM 53-01-11-000-802 & CRJ200 AMM 53-01-11

Next page: https://openairdocs.org/aircraft/N881AS/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 = 'N881AS' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N881AS/reports

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