# Service difficulty reports: N907SW, cancelled Mar 8, 2023

A list on [N907SW, cancelled Mar 8, 2023](https://openairdocs.org/deregistered/N907SW-2023-03-08.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 4 · 159 reports

- [SDR SWIA202159606](https://openairdocs.org/sdr/SWIA202159606.md): Engine · uncontrollable · Jul 19, 2021 · N907SW · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > LEFT ENGINE DID NOT RESPOND TO THRUST LEVER MOVEMENT. LEFT ENGINE APR FIRED. EVEN IN SHUTOFF POSITION ENGINE STILL WAS RUNNING. RAN SEVERE ENGINE DAMAGE IN FLIGHT EMERGENCY CHECKLIST. PROBLEM RESOLVED AFTER PUSHING LH ENG FIRE PUSH SWITCH LIGHT, AND ASSOCIATED
- [SDR SWIA202054338](https://openairdocs.org/sdr/SWIA202054338.md): Bracket · cracked · Nov 12, 2020 · N907SW · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO COMPARTMENT FWD CARGO DOOR TRACK LOWER U CHANNEL ATTACH BRACKET CRACKED, MARKED. C-CHECK RO 11/23/2020. REMOVED AND INSTALLED NEW FWD CARGO DOOR TRACK LOWER U CHANNEL ATTACH BRACKET P/N 601R35050-25 CRJ200 SRM.
- [SDR SWIA202054339](https://openairdocs.org/sdr/SWIA202054339.md): Frame · corroded · Nov 11, 2020 · N907SW · Cndair CL6002B19 · Fuselage Main, Frame
  > FS 589.0 FRAME AT STR 26L TO AT 26R HAS CORROSION ON FWD SIDE. C-CHECK RO 11/23/2020. REMOVED CORROSION ON FS 589 FRAME AT STGR 26L TO STGR 26R, REF CRJ200 SRM, FOUND TO BE OUT OF LIMITS. RECEIVED AND COMPLIED WITH ALL STEPS OF REO, NO LEAKS NOTED.
- [SDR SWIA202054337](https://openairdocs.org/sdr/SWIA202054337.md): Angle · cracked · Nov 11, 2020 · N907SW · Cndair CL6002B19 · Fuselage Main, Structure
  > RT 280 CROSSBEAM CLIPS ARE CRACKED AROUND RBL 9 FLOORBEAM. C-CHECK RO 11/23/2020. REMOVED AND INSTALLED NEW RT 280 CROSSBEAM CLIPS AT RBL 9 FLOORBEAM, REF CRJ200 SRM AND DWG. COMPLIED WITH TASK CARD.
- [SDR SWIA202054336](https://openairdocs.org/sdr/SWIA202054336.md): Angle · cracked · Nov 11, 2020 · N907SW · Cndair CL6002B19 · Fuselage Main, Structure
  > LT 280 CROSSBEAM CLIPS ARE CRACKED AROUND LBL 9 FLOORBEAM. C-CHECK RO 11/23/2020. REMOVED AND INSTALLED NEW LT 280 CROSSBEAM CLIPS AT LBL 9 FLOORBEAM, REF CRJ200 SRM AND DWG. COMPLIED WITH TASK CARD.
- [SDR SWIA202054335](https://openairdocs.org/sdr/SWIA202054335.md): Strap · corroded · Nov 11, 2020 · N907SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LT TOP STRAP AT FS 559.0 FROM LBL 27 TO SILL HAS CORROSION. C-CHECK RO 11/23/2020. REMOVED CORROSION AT LT TOP STRAP AT FS 559.00 LBL 27 TO SILL, REF CRJ200 SRM, FOUND TO BE OUT OF LIMITS. REMOVED AND INSTALLED NEW LT TOP STRAP AT FS 559.00 LBL 27, REF CRJ2
- [SDR SWIA202054342](https://openairdocs.org/sdr/SWIA202054342.md): Rivet · gouged · Nov 9, 2020 · N907SW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 621 BULKHEAD FWD SIDE HAS 4 GOUGES RIVET HEADS AT APPROXIMATELY WL 87 & RBL 9, RBL 18, RBL 27, RBL 36, MARKED. C-CHECK RO 11/23/2020. REMOVED AND INSTALLED NEW FASTENERS ON FWD SIDE OF FS 621 BULKHEAD AT APPROXIMATELY WL 87 & RBL 9, RBL 18, RBL 27, RBL 36
- [SDR SWIA202054341](https://openairdocs.org/sdr/SWIA202054341.md): Isolator · loose · Nov 9, 2020 · N907SW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 621 BULKHEAD FWD SIDE HAS 3 ISOLATORS LOOSE, MARKED. C-CHECK RO 11/23/2020. REPLACED 6 EA SOLID RIVETS ON FS 621 BULKHEAD FWD SIDE HAS 3 ISOLATORS, REF CRJ200 SRM.
- [SDR SWIA202054340](https://openairdocs.org/sdr/SWIA202054340.md): Isolator · bent · Nov 9, 2020 · N907SW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 621 BULKHEAD FWD SIDE HAS 14 ISOLATOR BRACKETS BENT/DEFORMED, MARKED. C-CHECK RO 11/23/2020. REMOVED AND REPLACED 14 EA ISOLATOR BRACKET ASSEMBLY FROM FWD SIDE OF FS 621 BULKHEAD, REF CRJ200 SRM, NO LEAKS NOTED.
- [SDR SWIA202054334](https://openairdocs.org/sdr/SWIA202054334.md): Skin · corroded · Nov 9, 2020 · N907SW · Cndair CL6002B19 · Wing, Plate/Skin
  > WING PLANK LAND AT 610AB HAS FRETTING CORROSION, MARKED. C-CHECK RO 11/23/2020. REMOVED CORROSION ON RT WING PLANK LAND AT 610AB, REF REO, FOUND TO BE WITHIN LIMITS. COMPLIED WITH ALL STEPS OF REO, NO LEAKS NOTED. COMPLIED WITH TASK CARD. BONDING TEST GOO
- [SDR SWIA202054333](https://openairdocs.org/sdr/SWIA202054333.md): Skin · corroded · Nov 9, 2020 · N907SW · Cndair CL6002B19 · Wing, Plate/Skin
  > WING PLANK LAND AT 640BB HAS FRETTING CORROSION, MARKED. C-CHECK RO 11/23/2020. REMOVED CORROSION ON RT WING PLANK LAND AT 640BB, REF REO, FOUND TO BE WITHIN LIMITS. COMPLIED WITH ALL STEPS OF REO, NO LEAKS NOTED. COMPLIED WITH TASK CARD. BONDING TEST GOO
- [SDR SWIA202054332](https://openairdocs.org/sdr/SWIA202054332.md): Skin · corroded · Nov 9, 2020 · N907SW · Cndair CL6002B19 · Wing, Plate/Skin
  > WING PLANK LAND AT 640CB HAS FRETTING CORROSION, MARKED. C-CHECK RO 11/23/2020. REMOVED CORROSION ON RT WING PLANK LAND AT 640CB, REF REO, FOUND TO BE WITHIN LIMITS. COMPLIED WITH ALL STEPS OF REO, NO LEAKS NOTED. COMPLIED WITH TASK CARD. BONDING TEST GOO
- [SDR SWIA202054331](https://openairdocs.org/sdr/SWIA202054331.md): Skin · corroded · Nov 9, 2020 · N907SW · Cndair CL6002B19 · Wing, Plate/Skin
  > WING PLANK LAND AT 640EB HAS FRETTING CORROSION, MARKED. C-CHECK RO 11/23/2020. REMOVED CORROSION ON RT WING PLANK LAND AT 640EB, REF REO, FOUND TO BE WITHIN LIMITS. COMPLIED WITH ALL STEPS OF REO, NO LEAKS NOTED. COMPLIED WITH TASK CARD. BONDING TEST GOO
- [SDR SWIA202054330](https://openairdocs.org/sdr/SWIA202054330.md): Skin · corroded · Nov 9, 2020 · N907SW · Cndair CL6002B19 · Wing, Plate/Skin
  > WING PLANK LAND AT 650AB HAS FRETTING CORROSION, MARKED. C-CHECK RO 11/23/2020. REMOVED CORROSION ON RT WING PLANK LAND AT 650AB, REF REO, FOUND TO BE WITHIN LIMITS. COMPLIED WITH ALL STEPS OF REO, NO LEAKS NOTED. COMPLIED WITH TASK CARD. BONDING TEST GOO
- [SDR SWIA202054329](https://openairdocs.org/sdr/SWIA202054329.md): Skin · corroded · Nov 9, 2020 · N907SW · Cndair CL6002B19 · Wing, Plate/Skin
  > WING PLANK LAND AT 650BB HAS FRETTING CORROSION, MARKED. C-CHECK RO 11/23/2020. REMOVED CORROSION ON RT WING PLANK LAND AT 650BB, REF REO, FOUND TO BE WITHIN LIMITS. COMPLIED WITH ALL STEPS OF REO, NO LEAKS NOTED. COMPLIED WITH TASK CARD 51-900-1003-SKY.
- [SDR SWIA202054328](https://openairdocs.org/sdr/SWIA202054328.md): Skin · corroded · Nov 9, 2020 · N907SW · Cndair CL6002B19 · Wing, Plate/Skin
  > WING PLANK LAND AT 510AB HAS FRETTING CORROSION, MARKED. C-CHECK RO 11/23/2020. REMOVED CORROSION ON LT WING PLANK LAND AT 510AB, REF REO, FOUND TO BE WITH IN LIMITS. COMPLIED WITH ALL STEPS OF REO, NO LEAKS NOTED. BONDING TEST GOOD, REF CRJ 200 AMM TUC780
- [SDR SWIA202054327](https://openairdocs.org/sdr/SWIA202054327.md): Skin · corroded · Nov 9, 2020 · N907SW · Cndair CL6002B19 · Wing, Plate/Skin
  > WING PLANK LAND AT 510BB HAS FRETTING CORROSION, MARKED. C-CHECK RO 11/23/2020. REMOVED CORROSION ON LT WING PLANK LAND AT 510BB, REF REO. FOUND TO BE WITH IN LIMITS. COMPLIED WITH ALL STEPS OF REO, NO LEAKS NOTED. BONDING TEST GOOD, REF CRJ 200 AMM TUC78
- [SDR SWIA202054326](https://openairdocs.org/sdr/SWIA202054326.md): Skin · corroded · Nov 9, 2020 · N907SW · Cndair CL6002B19 · Wing, Plate/Skin
  > WING PLANK LAND AT 540AB HAS FRETTING CORROSION, MARKED. C-CHECK RO 11/23/2020. REMOVED CORROSION ON LT WING PLANK LAND AT 540AB, REF REO, FOUND TO BE WITHIN LIMITS. COMPLIED WITH ALL STEPS OF REO, NO LEAKS NOTED. BONDING TEST GOOD, REF CRJ 200 AMM TUC7801
- [SDR SWIA202054325](https://openairdocs.org/sdr/SWIA202054325.md): Skin · corroded · Nov 9, 2020 · N907SW · Cndair CL6002B19 · Wing, Plate/Skin
  > WING PLANK LAND AT 540BB HAS FRETTING CORROSION, MARKED. C-CHECK RO 11/23/2020. REMOVED CORROSION ON LT WING PLANK LAND AT 540BB, REF REO, FOUND TO BE WITH IN LIMITS. COMPLIED WITH ALL STEPS OF REO, DATED 2014-02-05, NO LEAKS NOTED. BONDING TEST GOOD, REF
- [SDR SWIA202054324](https://openairdocs.org/sdr/SWIA202054324.md): Skin · corroded · Nov 9, 2020 · N907SW · Cndair CL6002B19 · Wing, Plate/Skin
  > WING PLANK LAND AT 540CB HAS FRETTING CORROSION, MARKED. C-CHECK RO 11/23/2020. REMOVED CORROSION ON LT WING PLANK LAND AT 540CB, REF REO, FOUND TO BE WITHIN LIMITS. COMPLIED WITH ALL STEPS OF REO, NO LEAKS NOTED. BONDING TEST GOOD, REF CRJ 200 AMM TUC7801
- [SDR SWIA202054323](https://openairdocs.org/sdr/SWIA202054323.md): Skin · corroded · Nov 9, 2020 · N907SW · Cndair CL6002B19 · Wing, Plate/Skin
  > WING PLANK LAND AT 540DB HAS FRETTING CORROSION, MARKED. C-CHECK RO 11/23/2020. REMOVED CORROSION ON LT WING PLANK LAND AT 540DB, REF REO, FOUND TO BE WITHIN LIMITS. COMPLIED WITH ALL STEPS OF REO, NO LEAKS NOTED. BONDING TEST GOOD, REF CRJ 200 AMM TUC7801
- [SDR SWIA202054322](https://openairdocs.org/sdr/SWIA202054322.md): Skin · corroded · Nov 9, 2020 · N907SW · Cndair CL6002B19 · Wing, Plate/Skin
  > WING PLANK LAND AT 540EB HAS FRETTING CORROSION, MARKED. C-CHECK RO 11/23/2020. REMOVED CORROSION ON LT WING PLANK LAND AT 540EB, REF REO, FOUND TO BE WITHIN LIMITS. COMPLIED WITH ALL STEPS OF REO, NO LEAKS NOTED. BONDING TEST GOOD, REF CRJ 200 AMM TUC7801
- [SDR SWIA202054321](https://openairdocs.org/sdr/SWIA202054321.md): Skin · corroded · Nov 9, 2020 · N907SW · Cndair CL6002B19 · Wing, Plate/Skin
  > WING PLANK LAND AT 540FB HAS FRETTING CORROSION, MARKED. C-CHECK RO 11/23/2020. REMOVED CORROSION ON LT WING PLANK LAND AT 540FB, REF REO, FOUND TO BE WITHIN LIMITS. COMPLIED WITH ALL STEPS OF REO, NO LEAKS NOTED. BONDING TEST GOOD, REF CRJ 200 AMM TUC7801
- [SDR SWIA202054320](https://openairdocs.org/sdr/SWIA202054320.md): Skin · corroded · Nov 9, 2020 · N907SW · Cndair CL6002B19 · Wing, Plate/Skin
  > WING PLANK LAND AT 550AB HAS FRETTING CORROSION, MARKED. C-CHECK RO 11/23/2020. REMOVED CORROSION ON LT WING PLANK LAND AT 550AB, REF REO, FOUND TO BE WITHIN LIMITS. COMPLIED WITH ALL STEPS OF REO, NO LEAKS NOTED. TASK CARD COMPLIED WITH. BONDING TEST GOO
- [SDR SWIA202054319](https://openairdocs.org/sdr/SWIA202054319.md): Skin · corroded · Nov 9, 2020 · N907SW · Cndair CL6002B19 · Wing, Plate/Skin
  > WING PLANK LAND AT 550CB HAS FRETTING CORROSION, MARKED. C-CHECK RO 11/23/2020. REMOVED CORROSION ON LT WING PLANK LAND AT 550CB, REF REO, FOUND TO BE WITHIN LIMITS. COMPLIED WITH ALL STEPS OF REO, NO LEAKS NOTED. TASK CARD COMPLIED WITH. BONDING TEST GOO
- [SDR SWIA202054318](https://openairdocs.org/sdr/SWIA202054318.md): Skin · corroded · Nov 9, 2020 · N907SW · Cndair CL6002B19 · Wing, Plate/Skin
  > WING PLANK LAND AT 550DB HAS FRETTING CORROSION, MARKED. C-CHECK RO 11/23/2020. REMOVED CORROSION ON LT WING PLANK LAND AT 550DB, REF REO, FOUND TO BE WITHIN LIMITS. COMPLIED WITH ALL STEPS OF REO, NO LEAKS NOTED. BONDING TEST GOOD, REF CRJ 200 AMM TUC7801
- [SDR SWIA202054317](https://openairdocs.org/sdr/SWIA202054317.md): Skin · corroded · Nov 9, 2020 · N907SW · Cndair CL6002B19 · Wing, Plate/Skin
  > WING PLANK LAND AT 550EB HAS FRETTING CORROSION, MARKED. C-CHECK RO 11/23/2020. REMOVED CORROSION ON LT WING PLANK LAND AT 550EB, REF REO, FOUND TO BE WITH IN LIMITS. COMPLIED WITH ALL STEPS OF REO, NO LEAKS NOTED. TASK CARD COMPLIED WITH. BONDING TEST GO
- [SDR SWIA202054316](https://openairdocs.org/sdr/SWIA202054316.md): Skin · corroded · Nov 9, 2020 · N907SW · Cndair CL6002B19 · Wing, Plate/Skin
  > WING PLANK LAND AT 550FB HAS FRETTING CORROSION, MARKED. C-CHECK RO 11/23/2020. REMOVED CORROSION ON LT WING PLANK LAND AT 550FB, REF REO. FOUND TO BE WITHIN LIMITS. COMPLIED WITH ALL STEPS OF REO, NO LEAKS NOTED. BONDING TEST GOOD, REF CRJ 200 AMM TUC780
- [SDR SWIA202054315](https://openairdocs.org/sdr/SWIA202054315.md): Skin · corroded · Nov 9, 2020 · N907SW · Cndair CL6002B19 · Wing, Plate/Skin
  > WING PLANK LAND AT 550HB HAS FRETTING CORROSION, MARKED. C-CHECK RO 11/23/2020. REMOVED CORROSION ON LT WING PLANK LAND AT 550HB, REF REO. FOUND TO BE WITH IN LIMITS. COMPLIED WITH ALL STEPS OF REO, NO LEAKS NOTED. BONDING TEST GOOD, REF CRJ 200 AMM TUC78
- [SDR SWIA202054314](https://openairdocs.org/sdr/SWIA202054314.md): Bulkhead · gouged · Nov 9, 2020 · N907SW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 621 BULKHEAD FWD SIDE HAS 3 GOUGES AT APPROXIMATELY WL 103 & RBL 18, RBL 27, RBL 36, MARKED. C-CHECK RO 11/23/2020. BLENDED OUT DAMAGE TO A SMOOTH SURFACE AT FS 621 WL 103 & RBL 18, RBL 27, RBL 36, REF CRJ200 SRM. FOUND TO BE OUT OF LIMITS. RECEIVED AND
- [SDR SWIA202054343](https://openairdocs.org/sdr/SWIA202054343.md): Vane · chafed · Nov 7, 2020 · N907SW · Cndair CL6002B19 · Trailing Edge Flaps
  > LT INBOARD FLAP VANE TRAILING EDGE MID UPPER SIDE HAS CHAFING DAMAGE. C-CHECK RO 11/23/2020. REMOVED THE CHAFE DAMAGE FROM THE LT INBOARD FLAP VANE UPPER TRAILING EDGE SKIN, REF CRJ200 SRM, FOUND TO BE OUT OF LIMITS. RECEIVED AND COMPLIED WITH ALL STEPS OF
- [SDR SWIA202054313](https://openairdocs.org/sdr/SWIA202054313.md): Vane · chafed · Nov 7, 2020 · N907SW · Cndair CL6002B19 · Trailing Edge Flaps
  > RT INBOARD FLAP VANE LEADING EDGE INBOARD SIDE HAS CHAFING DAMAGE. C-CHECK RO 11/23/2020. REMOVED CHAFE DAMAGE FROM RT INBOARD FLAP VANE LEADING EDGE, INBOARD SIDE, REF CRJ200 SRM. FOUND TO BE OUT OF LIMITS. REMOVED AND INSTALLED NEW RT INBOARD FLAP VANE C
- [SDR SWIA202054312](https://openairdocs.org/sdr/SWIA202054312.md): Vane · chafed · Nov 7, 2020 · N907SW · Cndair CL6002B19 · Trailing Edge Flaps
  > LT INBOARD FLAP VANE LEADING EDGE OUTBOARD SIDE HAS CHAFING DAMAGE. C-CHECK RO 11/23/2020. REMOVED CHAFE DAMAGE ON LT INBOARD FLAP VANE LEADING EDGE OUTBOARD SIDE, REF CRJ200 SRM. FOUND TO BE OUT OF LIMITS. REMOVED AND INSTALLED NEW VANE CAP AT LT INBOARD
- [SDR SWIA2019012945470](https://openairdocs.org/sdr/SWIA2019012945470.md): Stiffener · chafed · Dec 23, 2018 · N907SW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > THE REAR PRESSURE BULKHEAD, VERTICAL STIFFENER AT THE CENTER, IS CHAFED IN THE UPPER PORTION OF ITS HEIGHT, ON THE AFT LEG SURFACE AND AFT CORNER. (C-CHECK) RO:01/25/2019 REPAIRED PRESSURE BULKHEAD VERTICAL STIFFENER AT THE CENTER IAW REO.
- [SDR SWIA201845472](https://openairdocs.org/sdr/SWIA201845472.md): Floor Skin · dented · Dec 18, 2018 · N907SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PRESSURE FLOOR SKIN DENT FS516 RBL13. (C-CHECK) RO:01/25/2019 PRESSURE FLOOR SKIN DENT AT FS516 RBL13 IAW REO.
- [SDR SWIA2019012945463](https://openairdocs.org/sdr/SWIA2019012945463.md): Floor Skin · dented · Dec 18, 2018 · N907SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PRESSURE FLOOR SKIN DENT FS501 RBL15 (C-CHECK) RO:01/25/2019 REPAIRED DENT IAW SRM.
- [SDR SWIA2019012945468](https://openairdocs.org/sdr/SWIA2019012945468.md): Buttstrap · corroded · Dec 17, 2018 · N907SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR BUTTSTRAP AT FS559.00 FROM LBL27-LBL43 HAS EXFOILIATED CORROSION. (C-CHECK) RO:01/25/2019 REPAIRED FLOOR BUTTSTRAP AT FS559.00 FROM LBL27-LBL43 IAW REO.
- [SDR SWIA2019012945467](https://openairdocs.org/sdr/SWIA2019012945467.md): Strap · corroded · Dec 16, 2018 · N907SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT SIDE STRAP AT FS559.00 BETWEEN RBL 27.0 TO RBL 41.75 IS CORRODED. (C-CHECK) RO:01/25/2019 REPAIRED RT SIDE STRAP AT FS 559.00 BETWEEN RBL 27.0 TO RBL 41.75 IAW REO.
- [SDR SWIA2019012945469](https://openairdocs.org/sdr/SWIA2019012945469.md): Floorbeam · corroded · Dec 15, 2018 · N907SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOORBEAM CAP - INBOARD AND OUTBOARD FLANGES ARE CORRODED AROUND THE FASTENER HOLES. LBL27, FS569.5 €“ FS621.00. (C-CHECK) RO:01/25/2019 REMOVED AND REPLACED FLOORBEAM CAP AT LBL27 BETWEEN FS 569.5 TO FS621 IAW SRM AND REO.
- [SDR SWIA2019012945466](https://openairdocs.org/sdr/SWIA2019012945466.md): Frame · corroded · Dec 15, 2018 · N907SW · Cndair CL6002B19 · Fuselage Main, Frame
  > SEVERAL AREAS OF CORROSION ON FRAME AT FS589 BETWEEN STRG 21L AND 23L. (C-CHECK) RO:01/25/2019 REPAIRED DAMAGED AREA OF FRAME AT FS589 BETWEEN STR 21L AND STR 23L IAW REO.
- [SDR SWIA2019012945474](https://openairdocs.org/sdr/SWIA2019012945474.md): Door Sill · corroded · Dec 14, 2018 · N907SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LT PRESSURE FLOOR SILL HAS CORROSION IN MULTIPLE PLACES BETWEEN FS 409+128 €“ FS 559 (C-CHECK) RO:01/25/2019 REMOVED CORROSION FROM LT PRESSURE FLOOR SILL IN MULTIPLE PLACES BETWEEN FS 409+128 €“ FS 559.00 IAW REO.
- [SDR SWIA2019012945471](https://openairdocs.org/sdr/SWIA2019012945471.md): Floorbeam · corroded · Dec 14, 2018 · N907SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > RBL 9 FLOORBEAM FS 409.00+48 TO 409.00 +112 APPROX. HAS CORROSION. (C-CHECK) RO:01/25/2019 REPAIRED RBL 9 FLOORBEAM AT FS409.00+48 TO FS409+112 IAW REO.
- [SDR SWIA2019012945462](https://openairdocs.org/sdr/SWIA2019012945462.md): Vane · damaged · Dec 8, 2018 · N907SW · Cndair CL6002B19 · Trailing Edge Flaps
  > REPLACE LT INBOARD FLAP CENTER VANE CAP. (C-CHECK) RO:01/25/2019 REPLACED LT IB FLAP CENTER VANE CAP WITH NEW P/N 601R14303-51 IAW REO.
- [SDR SWIA2019012945473](https://openairdocs.org/sdr/SWIA2019012945473.md): Hinge · scratched · Dec 5, 2018 · N907SW · Cndair CL6002B19 · Fuselage, Door Hinge
  > PAX DOOR HINGE FUSELAGE SIDE HAS MULTIBLE SCRATCH'S AND NICKS. (C-CHECK) RO:01/25/2019 / REMOVED AND REPLACED WITH NEW FUSELAGE SIDE PAX DOOR HINGE IAW REO.
- [SDR SWIA2019012945465](https://openairdocs.org/sdr/SWIA2019012945465.md): Panel · chafed · Dec 5, 2018 · N907SW · Cndair CL6002B19 · Ailerons
  > LEFT HAND AILERON LOWER FIXED LEADING EDGE PANELS HAVE CHAFES. (C-CHECK) RO:01/25/2019 LT AILERON INBD LEADING EDGE PANEL REMOVED AND REPLACED WITH NEW PANEL (P/N CC670-13053-1) IAW SRM.
- [SDR SWIA2019012945464](https://openairdocs.org/sdr/SWIA2019012945464.md): Strap · corroded · Dec 3, 2018 · N907SW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > STRAP AT FS349.00 STR 3L HAS CORROSION AT MULTIPLE PLACES. (C-CHECK) RO:01/25/2019REMOVED AND INSTALLED NEW STRAP AT FS349.00 STGR 3L IAW SRM.
- [SDR SWIA201743181](https://openairdocs.org/sdr/SWIA201743181.md): Skin · dented · Apr 4, 2017 · N907SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > LEFT SIDE OF FUSELAGE SKIN HAS A DENT BETWEEN BS 605 AND 621, STRINGERS 21 - 22L. PERFORMED PERMANENT REPAIR IAW REO AND SRM.
- [SDR SWIA201440415](https://openairdocs.org/sdr/SWIA201440415.md): Vane · unsecure · Dec 12, 2014 · N907SW · Cndair CL6002B19 · Cabin Cooling System
  > RIGHT RAM AIR EXHAUST DUCT VANE IS MISSING ADHESIVE, C-CHECK, RO 12/13/14, CLEANED AND REAPPLIED ADHESIVE TO RT RAM AIR EXHAUST DUCT VANE IAW REO.
- [SDR SWIA201440411](https://openairdocs.org/sdr/SWIA201440411.md): Vane · unsecure · Dec 12, 2014 · N907SW · Cndair CL6002B19 · Cabin Cooling System
  > LEFT RAM AIR EXHAUST DUCT VANE IS MISSING ADHESIVE. CLEANED AND REAPPLIED ADHESIVE TO LT RAM AIR EXHAUST DUCT VANE IAW REO.
- [SDR SWIA201440403](https://openairdocs.org/sdr/SWIA201440403.md): Nut · unsecure · Dec 9, 2014 · N907SW · Cndair CL6002B19 · Aerial Tow Equipment
  > CO-PILOTS AILERON CONTROL COLUMN HAS CLICKING. RETORQUED COPILOTS CONTROL COLUMN NUT ON FWD SIDE OF THE CONTROL WHEEL SHAFT REF REO AND AMM.

Next page: https://openairdocs.org/deregistered/N907SW-2023-03-08/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 = 'N907SW' AND deregistration_id = 'N907SW-2023-03-08'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N907SW-2023-03-08/reports

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