# Service difficulty reports: N889AS

A list on [N889AS](https://openairdocs.org/aircraft/N889AS.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 4 · 162 reports

- [SDR SWIA202266135](https://openairdocs.org/sdr/SWIA202266135.md): None · dented · Jun 9, 2022 · N889AS · Cndair CL6002B19 · Wing Structure
  > LH WINGLET FRONT SPAR FITTING DENTED REFER TO SRM 57-31-14 ITEM 35. (FILED CLOSED) REMOVED AND REPLACED LH WINGLET FRONT SPAR FITTING IN REF TO SRM51-42-21 AND DWG 601R10376. COMPLIED WITH TASK CARD 51-900-1003-SKY.
- [SDR SWIA202266134](https://openairdocs.org/sdr/SWIA202266134.md): Beam · damaged · Jun 4, 2022 · N889AS · Cndair CL6002B19 · Wing Structure
  > TRANSFER FROM EAML 920632: TRANSFERRED FROM CAMP 24914026. FOUND LH WING WINGLET BEAM DAMAGED (REF. SRM 57-31-14 ITEM #25) (FILED CLOSED) REMOVED AND REPLACED LH WINGLET BEAM ASSY (REF. SRM 57-31-14 ITEM #25) IN REF TO SRM 51-42-06. COMPLETED 51-900-1003
- [SDR SWIA202266133](https://openairdocs.org/sdr/SWIA202266133.md): None · damaged · Jun 4, 2022 · N889AS · Cndair CL6002B19 · Wing Structure
  > TRANSFER FROM EAML 920630: TRANSFERRED FROM CAMP 24914020. FOUND LH WING WINGLET DIAPHRAGM DAMAGED (REF. SRM 57-31-14 ITEM #20) (FILED CLOSED) REMOVED AND REPLACED LH WINGLET DIAPHRAGM (REF. SRM 57-31-14 ITEM #20) IN REF TO SRM 51-42-06. COMPLETED 51-900
- [SDR SWIA202266132](https://openairdocs.org/sdr/SWIA202266132.md): Beam · damaged · Jun 4, 2022 · N889AS · Cndair CL6002B19 · Wing Structure
  > TRANSFER FROM EAML 920629: TRANSFERRED FROM CAMP 24914018. FOUND LH WING WINGLET BEAM DAMAGED (REF. SRM 57-31-14 ITEM #18) (FILED CLOSED) REMOVED AND REPLACED LH WINGLET BEAM (REF. SRM 57-31-14 ITEM #18) IN REF TO SRM 51-42-06. COMPLETED 51-900-1003-SKY
- [SDR SWIA202161794](https://openairdocs.org/sdr/SWIA202161794.md): None · inoperative · Oct 19, 2021 · N889AS · Cndair CL6002B19 · Aircraft Fuel System
  > ON TAKEOFF RECEIVED R XFER SOV CAUTION MESSAGE AND LOST LEFT, CENTER FUEL QUANTITY INDICATIONS AT SAME TIME. THE RIGHT AND TOTAL FUEL QUANTITY INDICATIONS WERE ALREADY ON MEL. NO FUEL QUANTITY INDICATIONS AT ALL. RETURNED BACK TO FIELD. (FLIGHT 5783 - FIL
- [SDR SWIA2020050150424](https://openairdocs.org/sdr/SWIA2020050150424.md): Floor Support · corroded · Mar 6, 2020 · N889AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS409.00+5 LBL9 THRU FS409.00+119 LBL9 FLOOR SUPPORT UPPER CAP SURFACE FOUND TO BE OUT OF LIMITS FOLLOWING CORROSION REMOVAL. (C-CHECK) RO 4/30/2020 REMOVED AND REPLACED FLOOR SUPPORT FS409+5 - FS409+115 LBL9 DUE TO CORROSION OUT OF LIMITS IAW CRJ200 AMM
- [SDR SWIA2020050150423](https://openairdocs.org/sdr/SWIA2020050150423.md): Floor Support · corroded · Mar 6, 2020 · N889AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS409.00+5 RBL9 THRU FS409.00+119 RBL9 FLOOR SUPPORT UPPER CAP SURFACE FOUND TO BE OUT OF LIMITS FOLLOWING CORROSION REMOVAL. (C-CHECK) RO 4/30/2020 REMOVED AND REPLACED FLOOR SUPPORT FS409+5 - FS409+119 RBL9 DUE TO CORROSION OUT OF LIMITS IAW CRJ200 AM
- [SDR SWIA2020050150480](https://openairdocs.org/sdr/SWIA2020050150480.md): Stand Off · corroded · Mar 4, 2020 · N889AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INTERIOR AFT RIGHT FUSELAGE STANDOFF AT FRAME 574+3,STRINGER 17 ( FLOOR LEVEL) IS CORRODED (C-CHECK) RO 4/30/2020 REMOVED AND REPLACED STANDOFF AT FRAME 574+3, STRINGER 17 RIGHT HAND IAW CRJ 200 SRM
- [SDR SWIA2020050150479](https://openairdocs.org/sdr/SWIA2020050150479.md): Fastener · corroded · Feb 28, 2020 · N889AS · Cndair CL6002B19 · Spoilers
  > RIGHT WING #2 GROUND SPOILER INBOARD HINGE ATTACHING HARDWARE CORRODED CAMP # 20561405 (C-CHECK) RO 4/30/2020 REMOVED AND REPLACED HARDWARE ON RH WING OB GROUND SPOILER IAW CRJ200 AMM.
- [SDR SWIA2020050150478](https://openairdocs.org/sdr/SWIA2020050150478.md): Fastener · corroded · Feb 28, 2020 · N889AS · Cndair CL6002B19 · Spoilers
  > RIGHT WING #2 GROUND SPOILER CENTER HINGE ATTACHING HARDWARE CORRODED CAMP # 20561222 (C-CHECK) RO 4/30/2020 REMOVED AND REPLACED RIGHT WING GROUND SPOILER CENTER HINGE ATTACHING HARDWARE I A.W CRJ200 AMM AND CRJ200 AMM TORQUE WRENCH STS 0381 CALIBRATION
- [SDR SWIA2020050150477](https://openairdocs.org/sdr/SWIA2020050150477.md): Bolt · corroded · Feb 28, 2020 · N889AS · Cndair CL6002B19 · Spoilers
  > RIGHT WING SPOILERON INBOARD AND OUTBOARD HINGE ATTACH POINT MIGRATION PLATE (SAFETY KEEPER) HARDWARE IS CORRODED CAMP # 20560510 (C-CHECK) RO 4/30/2020 REMOVED AND REPLACED CORRODED HARDWARE ON RIGHT WING SPOILERON INBOARD AND OUTBOARD HINGE ATTACH POINT
- [SDR SWIA2020050150476](https://openairdocs.org/sdr/SWIA2020050150476.md): Nut · corroded · Feb 28, 2020 · N889AS · Cndair CL6002B19 · Spoilers
  > RIGHT WING FLIGHT SPOILER CENTER OUTBOARD HINGE FITTING ATTACH HARDWARE HAS CORROSION ON NUT CAMP # 20560419 (C-CHECK) RO 4/30/2020 REMOVED AND REPLACED RIGHT WING FLIGHT SPOILER CENTER OUTBOARD HINGE FITTING ATTACH HARDWARE IAW CRJ 200 AMM TQ WRENCH: STS
- [SDR SWIA2020050150475](https://openairdocs.org/sdr/SWIA2020050150475.md): Nut · corroded · Feb 28, 2020 · N889AS · Cndair CL6002B19 · Spoilers
  > RIGHT WING SPOILERON BOTH CENTER INBOARD AND OUTBOARD HINGE ATTACH HARDWARES HAVE CORRODED NUTS CAMP # 20560943 (C-CHECK) RO 4/30/2020 REMOVED AND REPLACED NUT ON RIGHT WING SPOILERONBOTH CENTER INBOARD AND OUTBOARD TORQUE STS 0609 CAL 06 AUG 19 DUE 06AUG
- [SDR SWIA2020050150474](https://openairdocs.org/sdr/SWIA2020050150474.md): Seat Track · corroded · Feb 28, 2020 · N889AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT LBL9 FROM FS 364.00 TO 394,00 NEEDS CORROSION REMOVED AND EVALUATED. (C-CHECK) RO 4/30/2020 REMOVED AND REPLACED SEAT TRACK FROM LBL9 FS364.00 TO 394.00 IAW CRJ-200 AMM. SCREW GUN 1703044 DUE 10OCT2020.
- [SDR SWIA2020050150473](https://openairdocs.org/sdr/SWIA2020050150473.md): Fastener · corroded · Feb 28, 2020 · N889AS · Cndair CL6002B19 · Spoilers
  > LEFT WING FLIGHT SPOILER ATTACH HARDWARE AT INBOARD AND OUTBOARD HINGE ATTACH POINTS CORRODED CAMP # 20559282 (C-CHECK) RO 4/30/2020 REMOVED AND REPLACED L/H WING #3 SPOILER ATTACH HARDWARE AT I/B AND O/B HINGE POINTS IAW CRJ-200 AMM. STS TOOLING# 3819 DUE
- [SDR SWIA2020050150472](https://openairdocs.org/sdr/SWIA2020050150472.md): Nut · corroded · Feb 28, 2020 · N889AS · Cndair CL6002B19 · Spoilers
  > LEFT WING SPOILERON OUTBOARD CENTER HINGE ATTACH HARDWARE NUT IS CORRODED CAMP # 20559207 (C-CHECK) RO 4/30/2020 REMOVE AND REPLACE LEFT WING OUTBOARD SPOILERON CENTER HINGE ATTACH HARDWARE NUT I.A.W CRJ200 AMM
- [SDR SWIA2020050150471](https://openairdocs.org/sdr/SWIA2020050150471.md): Nut · corroded · Feb 28, 2020 · N889AS · Cndair CL6002B19 · Spoilers
  > LEFT WING SPOILERON INBOARD HINGE ATTCH HARDWARE NUT CORRODED CAMP # 20559194 (C-CHECK) RO 4/30/2020 REMOVED AND REPLACED LEFT WING SPOILERON INBOARD HINGE ATTACH HARDWARE NUT I.A.W CRJ200 AMM. TORQUE WRENCH STS 3818 DUE DATE 05 APR 20
- [SDR SWIA2020050150470](https://openairdocs.org/sdr/SWIA2020050150470.md): Fastener · corroded · Feb 28, 2020 · N889AS · Cndair CL6002B19 · Spoilers
  > LEFT WING SPOILERON OUTBOARD HINGE ATTACH HARDWARE NUT CORRODED CAMP 20559149 (C-CHECK) RO 4/30/2020 REMOVED AND REPLACED LEFT WING SPOILERON OUTBOARD HINGE ATTACH HARDWARE NUT IAW CRJ 200 AMM. TORQUE WRENCH: STS3819 DUE DATE: 05/ APRIL 2020
- [SDR SWIA2020050150430](https://openairdocs.org/sdr/SWIA2020050150430.md): Angle · cracked · Feb 28, 2020 · N889AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS280 UNDERFLOOR INTERCOASTAL CLIP ANGLE AT COCKPIT ENTRY APPEARS CRACKED AT TOP AND BOTTOM CORNERS. (C-CHECK) RO 4/30/2020 REPLACED AND SEALED UNDERFLOOR INTERCOASTAL CLIP ANGLE AT FS 280 LBL 9 AND RBL 9 COCKPIT ENTRANCE IAW CRJ 200 SRM.
- [SDR SWIA2020050150469](https://openairdocs.org/sdr/SWIA2020050150469.md): Fastener · corroded · Feb 27, 2020 · N889AS · Cndair CL6002B19 · Spoilers
  > LEFT WING OUTBOARD GROUND SPOILER, ACTUATOR HINGE HAS HARDWARE CORRODED (C-CHECK) RO 4/30/2020 REMOVED AND REPLACED L/H WING OUTBOARD GROUND SPOILER, ACTUATOR HINGE HARDWARE IAW CRJ-200 AMM STS TOOLING # 0609 CAL DUE 06-AUG-2020
- [SDR SWIA2020050150468](https://openairdocs.org/sdr/SWIA2020050150468.md): Bolt · corroded · Feb 27, 2020 · N889AS · Cndair CL6002B19 · Spoilers
  > LEFT WING INBOARD GROUND SPOILER, AFT ACTUATOR FITTING TOP BOLT CORRODED (C-CHECK) RO 4/30/2020 REMOVE AND REPLACED LEFT WING GROUND SPOILER, AFT ACTUATOR FITTING HARDWARE. I A.W CRJ200 AMM AND CRJ200 AMM TORQUE WRENCH STS 0381 CALIBRATION DUE DATE IS 10
- [SDR SWIA2020050150467](https://openairdocs.org/sdr/SWIA2020050150467.md): Fastener · corroded · Feb 26, 2020 · N889AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AT PASSENGER DOOR CUT OUT FS 310 ANCHOR FITTING HAS SERVERAL CORRODED HARDWARE. REF # CAMP 20547767 (C-CHECK) RO 4/30/2020 REMOVED AND REPLACED HARDWARE AT PASSENGER DOOR CUT OUT AT FUS STA 310 ANCHOR FITTING TORQUE: STS 3816 S/N 0518902020 CAL DUE 05
- [SDR SWIA2020050150466](https://openairdocs.org/sdr/SWIA2020050150466.md): Fastener · corroded · Feb 26, 2020 · N889AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AT PASSENGER DOOR CUT OUT, FS 349 ANCHOR FITTING HAS SERVERAL CORRODED HARDWARE. REF # CAMP 20547754 (C-CHECK) RO 4/30/2020 REMOVED AND REPLACED PASSENGER DOOR FITTING HARDWARE AT FUS STA 349 FOR ANCHOR FITTING TORQ STS 3817 S/N 0518902024 CALL 05-APR-1
- [SDR SWIA2020050150465](https://openairdocs.org/sdr/SWIA2020050150465.md): Fastener · corroded · Feb 26, 2020 · N889AS · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSANGER DOOR AFT ROD ATTACHING HARDWARE IS CORRODED WHERE IT ATTACH TO FRAME (C-CHECK) RO 4/30/2020 REMOVED AND RELACED PASSENGER DOOR AFT ROD ATTACHING HARDWARE THAT IS ATTACHED TO THE FRAME IAW CRJ 200 AMM
- [SDR SWIA2020050150464](https://openairdocs.org/sdr/SWIA2020050150464.md): Floor Support · corroded · Feb 26, 2020 · N889AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON CABIN FLOOR SUPPORT AT FS 559 STR 17 R CAMP# 20547335 (C-CHECK) RO 4/30/2020 REMOVED AND REPLACED NEW STRAP AT CORROSION FOUND ON CABIN FLOOR SUPPORT AT FS 559 STR 17 R CRJ200 IAW
- [SDR SWIA2020050150463](https://openairdocs.org/sdr/SWIA2020050150463.md): Mount Bolt · corroded · Feb 25, 2020 · N889AS · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR ACTUATOR FOUR MOUNT BOLTS CORRODED. REF # CAMP 20542837 (C-CHECK) RO 4/30/2020 REMOVED AND REPLACED CORRODED BOLTS ON ACTUATOR FOUR MOUNT IAW CRJ200 AMM. TORQUE WRENCH C-ID STS-0381 CDD 10-DEC-2020.
- [SDR SWIA2020050150462](https://openairdocs.org/sdr/SWIA2020050150462.md): Fastener · corroded · Feb 25, 2020 · N889AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK BLL 9.0 FS 556 TO FS 621 CORRODED HARDWARE (C-CHECK) RO 4/30/2020 REMOVED AND REPLACED CORRODED HARDWARE FROM FS 559 TO 621 BLL 9.0 IAW CRJ-200 AMM. TORQUE SCREWDRIVER SN 0919113214, PN 401SM, ALT STS-4351 CAL DUE 1-30-21
- [SDR SWIA2020050150461](https://openairdocs.org/sdr/SWIA2020050150461.md): Fastener · corroded · Feb 25, 2020 · N889AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK BLR 9.0, FS 559 + 80 TO FS 559 + 119 CORRODED HARDWARE (C-CHECK) RO 4/30/2020 REMOVED AND REPLACED CORRODED SEAT TRACK HARDWARE FROM FS559+80 TO FS559+119. PER CRJ200-AMM AND SRM. TORQUE WRENCH # STS3817. CAL DUE DATE 05APR2020.
- [SDR SWIA2020050150460](https://openairdocs.org/sdr/SWIA2020050150460.md): Fastener · corroded · Feb 25, 2020 · N889AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK BL 27.0, FS 559 + 96 CORRODED HARDWARE (C-CHECK) RO 4/30/2020 REMOVED CORRODED HARDWARES AND REPLACED WITH NEW HARDWARES ON SEAT TRACK BL 27.0, FS 559 + 80 TO FS 559 + 96 IAW CRJ 200 AMM 53-01-11 / TQ WRENCH: STS3819 / DUE DATE:05 APR 20
- [SDR SWIA2020050150459](https://openairdocs.org/sdr/SWIA2020050150459.md): Nut Plate · corroded · Feb 25, 2020 · N889AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT FLOOR EDGE MEMBER FS 559 + 32, 4 NUTPLATE CORRODED (C-CHECK) RO 4/30/2020 REMOVED AND REPLACED 4EA CORRODED NUTPLATES ON RIGHT FLOOR EDGE MEMBER FS 559 +32 IAW CRJ200 SRM.
- [SDR SWIA2020050150458](https://openairdocs.org/sdr/SWIA2020050150458.md): Fastener · corroded · Feb 25, 2020 · N889AS · Cndair CL6002B19 · Passenger/Crew Doors
  > PASANGER DOOR AFT ANCHOR FITTING HARDWARE CORRODED (C-CHECK) RO 4/30/2020 REMOVED AND REPLACED PASSENGER DOOR AFT ANCHOR FITTING HARDWARE IAW CRJ 200 TORQUE WRENCH STS 3744 CAL DUE 14 JAN 21
- [SDR SWIA2020050150456](https://openairdocs.org/sdr/SWIA2020050150456.md): Fastener · corroded · Feb 25, 2020 · N889AS · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSANGER DOOR AFT ROD END ATTACH TO AIRCRAFT FRAME HARDWARE CORRODED (C-CHECK) RO 4/30/2020 REMOVED AND REPLACED HARDWARE ON PASSENGER DOOR AFT ROD END ATTACH TO AIRCRAFT FRAME IAW CRJ 200 AMM.
- [SDR SWIA2020050150455](https://openairdocs.org/sdr/SWIA2020050150455.md): Fastener · corroded · Feb 25, 2020 · N889AS · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSANGER DOOR FORWARD ROD END ATTACH TO AIRCRAFT FRAME HARDWARE CORRODED (C-CHECK) RO 4/30/2020 REMOVED AND REPLACED HARDWARE ON PASSENGER DOOR FORWARD ROD END ATTACHED TO THE AIRCRAFT FRAME IAW CRJ200 AMM.
- [SDR SWIA2020050150454](https://openairdocs.org/sdr/SWIA2020050150454.md): Strap · corroded · Feb 25, 2020 · N889AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR STRUCTURE AT AFT. END OF PRESSURE FLOOR SILL AT FS 559 HAS A LOT OF SURFACE CORROSION TOP AND BOTTOM. REF: 20541521 (C-CHECK) RO 4/30/2020 REMOVED AND REPLACED STRAP AT AFT END OF PRESSURE FLOOR SILL AT FS 559 HAS A LOT OF SURFACE CORROSION TOP BOTTO
- [SDR SWIA2020050150453](https://openairdocs.org/sdr/SWIA2020050150453.md): Nut Plate · corroded · Feb 25, 2020 · N889AS · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBOARD FLAP HINGE BOX # 2 MIDDLE BOTTOM NUTPLATE ON OUTBOARD SIDE CORRODED FASTENERS (C-CHECK) RO 4/30/2020 REMOVED AND REPLACED L/H I/B #2 HINGE BOX MIDDLE BOTTOM NUTPLATE O/B IAW CRJ 200 SRM
- [SDR SWIA2020050150451](https://openairdocs.org/sdr/SWIA2020050150451.md): Fastener · corroded · Feb 25, 2020 · N889AS · Cndair CL6002B19 · Spoilers
  > RH INBD GROUND SPOILER AND INBD GROUND SPOILER PCU LINKS AND MOUNTING HARDWARE NEED REPLACEMENT DUE TO CORROSION. (C-CHECK) RO 4/30/2020 R/H INB AND OUTBD GROUND SPOILER PCU LINK AND MOUTING HARDWARE HAVE BEEN REPLACED AND CLEANED PER CRJ 200 SRM, AMM. TO
- [SDR SWIA2020050150420](https://openairdocs.org/sdr/SWIA2020050150420.md): Door Sill · corroded · Feb 25, 2020 · N889AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LIGHT SURFACE CORROSION ON PRESSURE FLOOR SILL AT FS 449.85. REF: 20541560 (C-CHECK) RO 4/30/2020 REMOVED CORROSION ON FLOOR SILL PANEL AT F.S 449.85 RIGHT SIDE, ORIGIONAL MATERIAL THICKNESS IS 0.055" MATERIAL REMOVED 0.001" AND REMAINING THICKNESS 0.054"
- [SDR SWIA2020050150481](https://openairdocs.org/sdr/SWIA2020050150481.md): Structure · corroded · Feb 24, 2020 · N889AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION AT NUTPLATES FROM FRAME 559+112 TO FRAME 621 AT FLOOR (7 EA). R/H SIDE (C-CHECK) RO 4/30/2020 REMOVED 7 EACH NUTPLATES BETWEEN FRAME 559+112 AND 621 AT FLOOR STRUCTURE R/H SIDE IAW CRJ200 SRM, REMOVED LIGHT SURFACE CORROSION BY HAND AROUND NUTPL
- [SDR SWIA2020050150450](https://openairdocs.org/sdr/SWIA2020050150450.md): Nut · corroded · Feb 24, 2020 · N889AS · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT # 4 HINGE BOX, AFT FITTING ATTACHING NUT CORRODED (C-CHECK) RO 4/30/2020 REMOVED AND REPLACED L/H #4 HINGE BOX AFT ATTACH FITTING NUT IAW CRJ 200 AMM. NO FURTHER DEFECTS NOTED AT THIS TIME. TORQUE WRENCH INFO STS-4227 DUE 11 FEB 21
- [SDR SWIA2020050150449](https://openairdocs.org/sdr/SWIA2020050150449.md): Nut · corroded · Feb 24, 2020 · N889AS · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT # 4 HINGE BOX MIDDLE FITTING ATTACHING NUTS CORRODED (C-CHECK) RO 4/30/2020 REMOVED AND REPLACED AT LEFT # 4 HINGE BOX MIDDLE FITTING NUTS IAW CRJ 200 AMM STS TOOL 0252 S/N 0411010479 CAL 10 DEC 2019 DUE 10 DEC 2020
- [SDR SWIA2020050150448](https://openairdocs.org/sdr/SWIA2020050150448.md): Nut · corroded · Feb 24, 2020 · N889AS · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT # 4 HINGE BOX FORWARD FITTING ATTACHING NUT CORRODED (C-CHECK) RO 4/30/2020 REMOVED AND REPLACED #4 LEFT HINGE BOX FORWARD ATTACHING NUT IAW CRJ 200 AMM. TORQUE WRENCH STS- 0252 DUE 10-DEC-20 AND STS-3817 DUE 05APR20
- [SDR SWIA2020050150447](https://openairdocs.org/sdr/SWIA2020050150447.md): Support · corroded · Feb 24, 2020 · N889AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON PASSENGER DOOR SILL SUPPORT FRAME. (C-CHECK) RO 4/30/2020 INSTALLED NEW DOOR SILL SUPPORT AND SUPPORT ANGLES IAW CRJ 200 SRM. REFERENCE CONTINUATION CARD FOR CORRECTIVE ACTION TAKEN.
- [SDR SWIA2020050150446](https://openairdocs.org/sdr/SWIA2020050150446.md): Nut · corroded · Feb 24, 2020 · N889AS · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT # 5 HINGE BOX, MIDDLE FITTING NUTS CORRODED (C-CHECK) RO 4/30/2020 REMOVED, REPLACED AND TORQUED #5 HINGE BOX MIDDLE FITTING NUTS/HARDWARE. IAW CRJ-200 AMM. TORQUE WRENCH CALIBRATED ID: STS-2250 S/N: AB77460 IDENT: KEL-298775 CAL: 25-NOV-19 DUE: 25- N
- [SDR SWIA2020050150445](https://openairdocs.org/sdr/SWIA2020050150445.md): Fastener · corroded · Feb 24, 2020 · N889AS · Cndair CL6002B19 · Rudder Structure
  > RIGHT # 3 OUTBOARD ACTUATOR FITTING ASSY MOUNT HARDWARE CORRODED (C-CHECK) RO 4/30/2020 REMOVED AND REPLACED R/H #3 FITTING ACTUATOR HARDWARE IAW CRJ 200 AMM TORQUE WRENCH STS-2250 DUE 10NOV2020
- [SDR SWIA2020050150444](https://openairdocs.org/sdr/SWIA2020050150444.md): Bolt · corroded · Feb 24, 2020 · N889AS · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT FLAP HINGE BOX # 4 FITTING ASSY MOUNT HARDWARE CORRODED (C-CHECK) RO 4/30/2020 REMOVED AND REPLACED R.H. FLAP HINGE #4 FITTING ASSEMBLY MOUNT HARDWARE. IAW CRJ-200 AMM. SRM. TORQUE WRENCH: 3817. CAL DUE DATE 17 MAR 21
- [SDR SWIA2020050150443](https://openairdocs.org/sdr/SWIA2020050150443.md): Nut · corroded · Feb 24, 2020 · N889AS · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT FLAP HINGE BOX # 4 SELF LKG, CSTL FORWARD CORRODED (C-CHECK) RO 4/30/2020 REMOVED AND REPLACED R/H FLAP HINGE BOX #4 NUT IAW CRJ 200 AMM TORQUE WRENCH STS-2250 DUE 25 NOV 20
- [SDR SWIA2020050150442](https://openairdocs.org/sdr/SWIA2020050150442.md): Nut · corroded · Feb 24, 2020 · N889AS · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT FLAP HINGE BOX # 5 ACTUATOR ATTACHING NUT CORRODED (C-CHECK) RO 4/30/2020 REMOVED AND REPLACED R/H #5 ACTUATOR ATTACHING NUT IAW CRJ 200 AMM SEE CAMP#20179174 FOR FINAL INSTALL OF ACTUATOR.
- [SDR SWIA2020050150441](https://openairdocs.org/sdr/SWIA2020050150441.md): Fastener · corroded · Feb 24, 2020 · N889AS · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT FLAP HINGE BOX # 5 FITTING ASSY MOUNT HARDWARE CORRODED (C-CHECK) RO 4/30/2020 REMOVED AND REPLACED L/H #5 O/B FLAP HINGE BOX 4 ASSEMBLY MOUNTING HARDWARE IAW CRJ 200 AMM.
- [SDR SWIA2020050150429](https://openairdocs.org/sdr/SWIA2020050150429.md): Stringer · cracked · Feb 23, 2020 · N889AS · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > STGR 3 CRACKED ON INBOARD SIDE AT FS 280.0. (C-CHECK) RO 4/30/2020 REMOVED AND REPLACED SPLICE ANGLE AT STGR 3L FS 280.0 INBOARD SIDE IAW: CRJ200 SRM.
- [SDR SWIA2020050150428](https://openairdocs.org/sdr/SWIA2020050150428.md): Stringer · cracked · Feb 22, 2020 · N889AS · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > STGR 3 CRACKED ON FWD SIDE OF FRAME AT FS 379.0. (C-CHECK) RO 4/30/2020 REPAIRED STGR 3L FS 379-FS 394 IAW STS EA 70-2020-046. AND COMPLIED WITH MAJOR REPAIR AND SKYCARD WEIGHT REMOVED FROM AIRCRAFT WAS 0.0 LBS AND WEIGHT ADDED WAS.057 LBS WEIGHT AND BALA

Next page: https://openairdocs.org/aircraft/N889AS/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 = 'N889AS' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N889AS/reports

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OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.