# Service difficulty reports: N200SY

A list on [N200SY](https://openairdocs.org/aircraft/N200SY.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR SWIA202505280018](https://openairdocs.org/sdr/SWIA202505280018.md): Stringer · corroded · May 18, 2025 · N200SY · Emb ERJ170200LR · Fuselage Main, Longeron/Stringer
  > CENTER FUSELAGE III LOWER PORTION: STGR 22L AT FR86 CORRODED. CUTOUT DAMAGED PORTION OF STRINGER 22L FR83-87. SPLICED IN NEW STRINGER 22L FR 83-87, REF ETD2025-170-921353. REPAIR PARTS WEIGHTED LESS THAN 2.5LBS, NO WEIGHT AND BALANCE ADJUSTMENT REQUIRED.
- [SDR SWI2025F00677](https://openairdocs.org/sdr/SWI2025F00677.md): Shear Tie · corroded · May 15, 2025 · N200SY · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > CORROSION IN SHEAR CLIP FR.86 BETWEEN STR. 21L-22L. (C-CHECK RO 05/27/2025)REMOVED AND REPLACED SHEAR CLIP FR86 BETWEEN STGR 21L-22L. REF EMB SRM 51-40-08. (SEE CONTINUATION CARD FOR WORK ACCOMPLISHED). REPLACED WITH OEM PART AND REPAIR DOES NOT EFFECT WEIGHT
- [SDR SWIA202505280015](https://openairdocs.org/sdr/SWIA202505280015.md): Shear Tie · corroded · May 15, 2025 · N200SY · Emb ERJ170200LR · Fuselage Main, Frame
  > CORROSION IN SHEAR CLIP FR.86 BETWEEN STR. 22L-23L. (C-CHECK RO 05/27/2025)REMOVED AND REPLACED SHEAR CLIP FR86 BETWEEN STGR 22L-23L. REF EMB SRM 51-40-08. (SEE CONTINUATION CARD FOR WORK ACCOMPLISHED). REPLACED WITH OEM PART AND REPAIR DOES NOT EFFECT WEIGHT
- [SDR SWI2025F00682](https://openairdocs.org/sdr/SWI2025F00682.md): Shear Tie · corroded · May 14, 2025 · N200SY · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > CORROSION DAMAGE ON SHEAR CLIP AT FRAME 89 BETWEEN STRINGERS 25L AND 23L. REMOVED AND REPLACED SHEAR CLIP AT FRAME 89 BETWEEN STRINGERS 25L AND 23L. REF EMB SRM 51-40-08. (SEE CONTINUATION CARD FOR WORK ACCOMPLISHED). REPLACED WITH OEM PART AND REPAIR DOES NO
- [SDR SWI2025F00681](https://openairdocs.org/sdr/SWI2025F00681.md): Shear Tie · corroded · May 14, 2025 · N200SY · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > CORROSION DAMAGE ON SHEAR CLIP AT FRAME 87 BETWEEN STRINGERS 23L AND 21L. REMOVED AND REPLACED SHEAR CLIP AT FRAME 87 BETWEEN STRINGERS 23L AND 21L. REF EMB SRM 51-40-08. REPLACED WITH NEW OEM PART, NO WEIGHT AND BALANCE ADJUSTMENT REQUIRED.
- [SDR SWI2025F00680](https://openairdocs.org/sdr/SWI2025F00680.md): Shear Tie · corroded · May 14, 2025 · N200SY · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > CORROSION DAMAGE ON SHEAR CLIP AT FRAME 88 BETWEEN STRINGERS 21L AND 20L. (C-CHECK RO 05/27/2025)REMOVED AND REPLACED SHEAR CLIP AT FRAME 88 BETWEEN STRINGERS 21L AND 20L, REF SRM 51-40-08. REPLACED WITH NEW OEM PART, NO WEIGHT AND BALANCE ADJUSTMENT REQUIR
- [SDR SWI2025F00679](https://openairdocs.org/sdr/SWI2025F00679.md): Shear Tie · corroded · May 14, 2025 · N200SY · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > CORROSION DAMAGE ON SHEAR CLIP AT FRAME 87 BETWEEN STRINGERS 21L AND 20L. REMOVED AND REPLACED SHEAR CLIP AT FRAME 87 BETWEEN STRINGERS 21L AND 20L.REF EMB SRM 51-40-08. (SEE CONTINUATION CARD FOR WORK ACCOMPLISHED). REPLACED WITH OEM PART AND REPAIR DOES NO
- [SDR SWI2025F00678](https://openairdocs.org/sdr/SWI2025F00678.md): Shear Tie · corroded · May 14, 2025 · N200SY · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > POST REMOVAL: CORROSION IN SHEAR CLIP FR.90A BETWEEN STR. 23L-25L. (C-CHECK RO 05/27/2025)REMOVED AND REPLACED FR 90A BETWEEN STGR 17R-17L REF. EMB SRM 51-40-08. SEE CONTINUATION CARD FOR WORK PERFORMED. REPLACED WITH OEM PART AND REPAIR DOES NOT EFFECT WEIGH
- [SDR SWIA202505280014](https://openairdocs.org/sdr/SWIA202505280014.md): Shear Tie · corroded · May 14, 2025 · N200SY · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > POST REMOVAL: CORROSION IN SHEAR CLIP FR.86 BETWEEN STR. 26L-27L. (C-CHECK RO 05/27/2025)REMOVED AND REPLACED SHEAR CLIP FR86 BETWEEN STR. 26L-27L. REF EMB SRM 51-40-08. (SEE CONTINUATION CARD FOR WORK ACCOMPLISHED). REPLACED WITH OEM PART AND REPAIR DOES NOT
- [SDR SWIA2025052800013](https://openairdocs.org/sdr/SWIA2025052800013.md): Shear Tie · corroded · May 13, 2025 · N200SY · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > AFT CARGO SHEAR CLIP CORRODED AT FR 86 STGR 22L-23L. (C-CHECK RO 05/27/2025)REMOVED AND REPLACED AFT CARGO SHEAR CLIP FR86 BETWEEN STGR 22L - 23L. REF EMB SRM 51-40-08. (SEE CONTINUATION CARD FOR WORK ACCOMPLISHED) REPLACED WITH OEM PART AND REPAIR DOES NOT EF
- [SDR SWIA202505280010](https://openairdocs.org/sdr/SWIA202505280010.md): Shear Tie · corroded · May 10, 2025 · N200SY · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > CORROSION IN SHEAR CLIP FR.89 BETWEEN STR.21L-23L. (C-CHECK RO 05/27/2025)REMOVED AND REPLACED SHEAR CLIP FR.89 BETWEEN STR.21L-23L. REF EMB SRM 51-40-08. (SEE CONTINUATION CARD FOR WORK ACCOMPLISHED). REPLACED WITH OEM PART AND REPAIR DOES NOT EFFECT WEIGHT
- [SDR SWIA202505280009](https://openairdocs.org/sdr/SWIA202505280009.md): Stringer · corroded · May 9, 2025 · N200SY · Emb ERJ170200LR · Fuselage Main, Longeron/Stringer
  > CORROSION DAMAGE ON STRINGER AT FRAME 89 - 90 STRINGER 23L. PERFORMED STRINGER 23L PERMANENT REPAIR BETWEEN FR90 - FR81. REF ETD2025-170-920831 REV B. REPAIR WEIGHS 130 GRAMS AND DOES NOT EFFECT WEIGHT AND BALANCE.
- [SDR SWI2025F00690](https://openairdocs.org/sdr/SWI2025F00690.md): Shear Tie · corroded · May 8, 2025 · N200SY · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > AFT CARGO: SHEAR CLIP CORRODED FR79 STGR21L - 22L. (C-CHECK RO 05/27/2025)REMOVED AND REPLACED SHEAR CLIP FR79 STGR 21L - 22L. REF EMB SRM 51-40-08. REPLACED WITH OEM PART AND REPAIR DOES NOT EFFECT WEIGHT AND BALANCE.
- [SDR SWI2025F00689](https://openairdocs.org/sdr/SWI2025F00689.md): Shear Tie · corroded · May 8, 2025 · N200SY · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > AFT CARGO: SHEAR CLIP CORRODED FR77 STGR21L - 20L. (C-CHECK RO 05/27/2025)REMOVED AND REPLACED AFT CARGO: SHEAR CLIP FR77 STGR21L - 20L REF EMB SRM 51-40-08. REPLACED WITH OEM PART AND REPAIR DOES NOT EFFECT WEIGHT AND BALANCE.
- [SDR SWI2025F00688](https://openairdocs.org/sdr/SWI2025F00688.md): Stringer · corroded · May 8, 2025 · N200SY · Emb ERJ170200LR · Fuselage Main, Longeron/Stringer
  > CORROSION DAMAGE ON STRINGER 21L AT FRAME 90. PERFORMED STRINGER 21L SPLICE REPAIR BETWEEN FAME 86-87 AND REPLACED STRINGER FROM FRAME 86-90 REF ETD2025-170-920827 REV. A. REPAIR PARTS WEIGHED LESS THAN 2.5 LBS. NO CHANGE TO WEIGHT AND BALANCE REQUIRED. SEE
- [SDR SWI2025F00687](https://openairdocs.org/sdr/SWI2025F00687.md): Support · corroded · May 8, 2025 · N200SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > CORROSION DAMAGE ON STABILIZER SUPPORT AT FRAME 90 AND STRINGER 21L. REMOVED AND REPLACED STABILIZER SUPPORT AT FRAME 90 AND STRINGER 21L. REF EMB SRM 51-40-08. REPLACED WITH OEM PART AND REPAIR DOES NOT EFFECT WEIGHT AND BALANCE.
- [SDR SWI2025F00686](https://openairdocs.org/sdr/SWI2025F00686.md): Support · corroded · May 8, 2025 · N200SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > CORROSION DAMAGE ON STABILIZER SUPPORT AT FRAME 90 AND STRINGER 23L. REMOVED AND REPLACED STABILIZER SUPPORT AT FRAME 90 AND STRINGER 23L. REF EMB SRM 51-40-08. REPLACED WITH OEM PART AND REPAIR DOES NOT EFFECT WEIGHT AND BALANCE.
- [SDR SWI2025F00685](https://openairdocs.org/sdr/SWI2025F00685.md): Shear Tie · corroded · May 8, 2025 · N200SY · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > CORROSION DAMAGE ON SHEAR CLIP AT FRAME 90 BETWEEN STRINGERS 21L AND 19L. (C-CHECK RO 05/27/2025)REMOVED AND REPLACED SHEAR CLIP AT FRAME 90 BETWEEN STRINGERS 21L AND 19L REF EMB SRM 51-40-08. REPLACED WITH OEM PART AND REPAIR DOES NOT EFFECT WEIGHT AND BALAN
- [SDR SWI2025F00684](https://openairdocs.org/sdr/SWI2025F00684.md): Shear Tie · corroded · May 8, 2025 · N200SY · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > CORROSION DAMAGE ON SHEAR CLIP AT FRAME 90 BETWEEN STRINGERS 23L AND 21L. REMOVED AND REPLACED SHEAR CLIP AT FRAME 90 BETWEEN STRINGERS 23L AND 21L REF EMB SRM 51-40-08. REPLACED WITH OEM PART AND REPAIR DOES NOT EFFECT WEIGHT AND BALANCE.
- [SDR SWI2025F00683](https://openairdocs.org/sdr/SWI2025F00683.md): Shear Tie · corroded · May 8, 2025 · N200SY · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > CORROSION DAMAGE ON SHEAR CLIP AT FRAME 90 BETWEEN STRINGERS 25L AND 23L. REMOVED AND REPLACED SHEAR CLIP AT FRAME 90 BETWEEN STRINGERS 25L AND 23L REF EMB SRM 51-40-08. REPLACED WITH OEM PART AND REPAIR DOES NOT EFFECT WEIGHT AND BALANCE.
- [SDR SWIA2025052800008](https://openairdocs.org/sdr/SWIA2025052800008.md): Shear Tie · corroded · May 8, 2025 · N200SY · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > CORROSION DAMAGE ON SHEAR CLIP AT FRAME 90 BETWEEN STRINGERS 28L AND 27L. REMOVED AND REPLACED SHEAR CLIP AT FRAME 90 BETWEEN STRINGERS 28L AND 27L.REF EMB SRM 51-40-08. REPLACED WITH OEM PART AND REPAIR DOES NOT EFFECT WEIGHT AND BALANCE.
- [SDR SWI2025F00692](https://openairdocs.org/sdr/SWI2025F00692.md): Beam · damaged · May 7, 2025 · N200SY · Emb ERJ170200LR · Fuselage Main, Structure
  > DAMAGE FOUND ON RH BEAM BETWEEN FR 85-86. REMOVED AND REPLACED RH BEAM FR85-86, REF SRM 51-40-08. REPLACED WITH NEW OEM PART, NO WEIGHT AND BALANCE ADJUSTMENT REQUIRED.
- [SDR SWI2025F00691](https://openairdocs.org/sdr/SWI2025F00691.md): Shear Tie · corroded · May 7, 2025 · N200SY · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > AFT CARGO: SHEAR CLIP CORRODED FR79 STGR23L. REMOVED AND REPLACED AFT CARGO SHEAR CLIP FR79 STGR 23L. REF EMB SRM 51-40-08. ( FACTORY PART WITH NO EFFECT ON WEIGHT AND BALANCE.
- [SDR SWIA202505280007](https://openairdocs.org/sdr/SWIA202505280007.md): Shear Tie · corroded · May 7, 2025 · N200SY · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > AFT CARGO: SHEAR CLIP CORRODED FR78 STGR22L. (C-CHECK RO 05/27/2025)REMOVED AND REPLACED AFT CARGO SHEAR CLIP FR78 STGR 22L. REF EMB SRM 51-40-08. (SEE CONTINUATION CARD FOR WORK ACCOMPLISHED). FACTORY PART WITH NO EFFECT ON WEIGHT AND BALANCE.
- [SDR SWI2025F00674](https://openairdocs.org/sdr/SWI2025F00674.md): Shear Tie · corroded · May 5, 2025 · N200SY · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > AFT CARGO: SHEAR CLIP CORRODED FR78 STGR23L. (C-CHECK RO 05/27/2025)REMOVED AND REPLACED AFT CARGO SHEAR CLIP FR78 STGR 23L. REF EMB SRM 51-40-08. (SEE CONTINUATION CARD FOR WORK ACCOMPLISHED). FACTORY PART WITH NO EFFECT ON WEIGHT AND BALANCE.
- [SDR SWI2025F00673](https://openairdocs.org/sdr/SWI2025F00673.md): Shear Tie · corroded · May 5, 2025 · N200SY · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > AFT CARGO: SHEAR CLIP CORRODED FR77 STGR23L. (C-CHECK RO 05/27/2025)REMOVED AND REPLACED SHEAR CLIP AT AFT CARGO, FRAME 77 AND STRINGER 23L AS MARKED.SEE CONTINUATION CARD FOR WORK PERFORMED. REF SRM 51-40-08. FACTORY REPLACEMENT PART THIS REPAIR DOES NOT AF
- [SDR SWI2025F00672](https://openairdocs.org/sdr/SWI2025F00672.md): Shear Tie · corroded · May 5, 2025 · N200SY · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > AFT CARGO: SHEAR CLIPT CORRODED FR75 STGR22L. REMOVED AND REPLACED AFT CARGO SHEAR CLIP FR75 STGR 22L. REF EMB SRM 51-40-08. FACTORY PART WITH NO EFFECT ON WEIGHT AND BALANCE.
- [SDR SWI2025F00671](https://openairdocs.org/sdr/SWI2025F00671.md): Seat Track · gouged · May 5, 2025 · N200SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > PASSENGER CABIN CENTER FUSELAGE I L/H LATERAL SEAT TRACK IS GOUGE ON FR 24/25, FR 25/26, FR 26/27, FR 27/28, FR 28/29, FR 30/31, FR 31/32, FR 32/33, FR 33/34, AND FR 34/43 (C-CHECK RO 05/27/2025)REMOVED AND REPLACED LH LATERAL SEAT TRACK FR24-34 REF SRM 51-4
- [SDR SWI2025F00670](https://openairdocs.org/sdr/SWI2025F00670.md): Seat Track · gouged · May 5, 2025 · N200SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > PASSENGER CABIN CENTER FUSELAGE I R/H SEAT TRACK IS GOUGE ON FR 22/23, FR 23/24, FR 25/26, FR 27/28, FR 28/29, FR 30/31, FR 31/32, FR 32/33, FR 33/34, AND FR 34/43. REMOVED AND REPLACED PASSENGER CABIN CENTER FUSELAGE I RH SEAT TRACK FR23-34, REF SRM 51-40-0
- [SDR SWI2025F00669](https://openairdocs.org/sdr/SWI2025F00669.md): Seat Track · gouged · May 5, 2025 · N200SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > PASSENGER CABIN CENTER FUSELAGE I R/H SEAT TRACK IS GOUGE ON FR 20/21. REMOVED AND REPLACED RH I/B SEAT TRACK FR12-20, REF SRM 51-40-08. REPLACED WITH NEW OEM PART, NO WEIGHT AND BALANCE ADJUSTMENT REQUIRED.
- [SDR SWI2025F00668](https://openairdocs.org/sdr/SWI2025F00668.md): Seat Track · gouged · May 5, 2025 · N200SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > PASSENGER CABIN CENTER FUSELAGE I R/H LATERAL SEAT TRACK IS GOUGE ON FR 20/21. REMOVED AND REPLACED PASSENGER CABIN CENTER FUSELAGE I R/H LATERAL SEAT TRACK FR 16 - FR 20 REF SRM 51-40-08. FACTORY REPLACEMENT PART NO CHANGE TO AIRCRAFT WEIGHT AND BALANCE.
- [SDR SWIA202505280005](https://openairdocs.org/sdr/SWIA202505280005.md): Shear Tie · corroded · May 5, 2025 · N200SY · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > AFT CARGO: SHEAR CLIPT CORRODED FR77 STGR22L. (C-CHECK RO 05/27/2025)REMOVED AND REPLACED SHEAR CLIP AT AFT CARGO, FRAME 77 AND STRINGER 22L. SEE CONTINUATION CARD FOR WORK PERFORMED. REF SRM 51-40-08FACTORY REPLACEMENT PART USED FOR THIS REPAIR. NO CHANGE T
- [SDR SWIA202505280004](https://openairdocs.org/sdr/SWIA202505280004.md): Shear Tie · corroded · May 4, 2025 · N200SY · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > AFT CARGO: SHEAR CLIP CORRODED AT FR 84 STGR 23L. REMOVED AND REPLACED AFT CARGO: SHEAR CLIP AT FR 84 STGR 23L REF EMB SRM 51-40-08. REPLACED WITH OEM PART AND REPAIR DOES NOT EFFECT WEIGHT AND BALANCE.
- [SDR SWIA202505280003](https://openairdocs.org/sdr/SWIA202505280003.md): Seat Track · corroded · May 3, 2025 · N200SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > R/H I/B SEAT TRACK HAS CORROSION AT SEAT MOUNT POINTS FROM FR.74 TO FR.84. EVALUATED CORROSION ON R/H I/B SEAT TRACK AT SEAT MOUNT POINTS FROM FR.74 TO FR.84. AND REMOVED DAMAGE BY BLENDING. MAX. MEASURED MATERIAL LOSS ON CROWN TOOTH: FR73-74=0.02"; FR74-75=
- [SDR SWI2025F00676](https://openairdocs.org/sdr/SWI2025F00676.md): Beam · corroded · May 2, 2025 · N200SY · Emb ERJ170200LR · Fuselage Main, Structure
  > LH BEAM HAS CORROSION FRAME 87. REMOVED AND REPLACED LH BEAM BETWEEN FR86 - FR89. REF EMB SRM 51-40-08.. REPLACED BEAM WITH O.E.M PART AND DOES NOT EFFECT WEIGHT AND BALANCE.
- [SDR SWI2025F00675](https://openairdocs.org/sdr/SWI2025F00675.md): Beam · corroded · May 2, 2025 · N200SY · Emb ERJ170200LR · Fuselage Main, Structure
  > RH IB BEAM HAS CORROSION FRAME 85-87. REMOVED AND REPLACED RH IB BEAM BETWEEN FR86 - FR89. REF EMB SRM 51-40-08. FACTORY REPLACEMENT PART NO CHANGE TO AIRCRAT WEIGHT AND BALANCE.
- [SDR SWIA202505280002](https://openairdocs.org/sdr/SWIA202505280002.md): Rib · cracked · May 2, 2025 · N200SY · Emb ERJ170200LR · Horizontal Stabilizer, Spar/Rib
  > R/H HORIZONTAL STABILIZER RIB 12A BETWEEN FRONT SPAR AND MIDDLE SPAR SUSPECTED CRACK. (C-CHECK RO 05/27/2025)REMOVED AND REPLACED RIB12A ON RH HORIZONTAL STABILIZER BETWEEN FRONT AND MIDDLE SPAR.REF SRM 51-40-08.(SEE CONTINUATION CARD FOR ALLWORKED ACCOMPLISH
- [SDR SWIA202265556](https://openairdocs.org/sdr/SWIA202265556.md): None · damaged · Apr 25, 2022 · N200SY · Emb ERJ170200LR · Fuselage, Powerplant Attach Fittings
  > RIGHT HAND INBOARD SEAT TRACK AT SEAT 2C DOES NOT ALLOW PROPER ENGAGEMENT OF SEAT TRACK SPLICE DEVICE. (C-CHECK RO 5/4/2022) REMOVED RH INBOARD SEAT TRACK BEAM BETWEEN FRAMES 23-26. PERFORMED SPLICE REPAIR AS PER SRM. / RESTORED SURFACE PROTECTION.
- [SDR SWIA202265566](https://openairdocs.org/sdr/SWIA202265566.md): None · gouged · Apr 7, 2022 · N200SY · Emb ERJ170200LR · Fuselage, Powerplant Attach Fittings
  > LH INBOARD SEAT TRACK SECTION 23-34 HAS GOUGES AFT OF FRAMES 23, 24, 25, 30, 32 AND 33. (C-CHECK RO 5/4/2022) REMOVED GOUGES ONLH INBOARD SEAT TRACK SECTION 23-34. AFT OF FRAMES 23, 24, 25, 30, 32 AND 33. FOUND MAXIUM MATERIAL LOSS AT FRAMES 24, 25, AND
- [SDR SWIA202265565](https://openairdocs.org/sdr/SWIA202265565.md): None · corroded · Apr 7, 2022 · N200SY · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > CORROSION ON L/H BEAM SUPPORT BETWEEN FR 19 AND FR 20. (C-CHECK RO 5/4/2022) REMOVED AND REPLACED L/H BEAM SUPPORT BETWEEN FR 19 AND FR 20 REF SRM 51-40-08
- [SDR SWIA202265564](https://openairdocs.org/sdr/SWIA202265564.md): None · corroded · Apr 6, 2022 · N200SY · Emb ERJ170200LR · Fuselage Main, Frame
  > CORROSION, AFT WET AREA, ON CENTER SPLICE PLATE AT FRAME 90 (X = -4€?). (C-CHECK RO 5/4/2022) REMOVED AND REPLACED CENTER SPLICE PLATE AT FR 90. REF EMB SRM 51-40-08. SEE CONTINUATION FOR WORK PERFORMED.
- [SDR SWIA202265563](https://openairdocs.org/sdr/SWIA202265563.md): None · corroded · Apr 6, 2022 · N200SY · Emb ERJ170200LR · Fuselage Main, Frame
  > CORROSION, AFT WET AREA, ON RH GUSSET PLATE AT FRAME 90 (X = +25€?). (C-CHECK RO 5/4/2022) REMOVED AND REPLACED AND RESTORED SURFACE PROTECTION AFT WET AREA RH GUSSET PLATE AT FR 90 REF SRM 51-40-08, 51-23-06
- [SDR SWIA202265562](https://openairdocs.org/sdr/SWIA202265562.md): None · corroded · Apr 6, 2022 · N200SY · Emb ERJ170200LR · Fuselage Main, Frame
  > CORROSION, AFT WET AREA, ON RH GUSSET PLATE AT FRAME 90 (X = +11€?). (C-CHECK RO 5/4/2022) REMOVED AND REPLACED AND RESTORED SURFACE PROTECTION AFT WET AREA RH GUSSET PLATE AT FRAME 90 REF SRM 51-40-08, 51-23-06
- [SDR SWIA202265561](https://openairdocs.org/sdr/SWIA202265561.md): None · corroded · Apr 6, 2022 · N200SY · Emb ERJ170200LR · Fuselage Main, Frame
  > CORROSION, AFT WET AREA, ON RH SPLICE PLATE AT FRAME 89 (X = +11€?). (C-CHECK RO 5/4/2022) REMOVED AND REPLACED R/H SPLICE PLAT AT FR 89. REF EMB SRM 51-40-08. SEE CONTINUATION FOR WORK PERFORMED.
- [SDR SWIA202265560](https://openairdocs.org/sdr/SWIA202265560.md): None · corroded · Apr 6, 2022 · N200SY · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > CORROSION, AFT WET AREA, ON RH LONGITUDINAL FLOOR BEAM AT FRAME 87 WHERE THE BEAM PASSES BETWEEN THE CENTER AND RH SHEAR PANELS. (C-CHECK RO 5/4/2022) REMOVED AND REPLACED R/H LONGITUDINAL FLOOR BEAM AT FR 87. REF EMB SRM 51-40-08. SEE CONTINUATION FOR
- [SDR SWIA202265559](https://openairdocs.org/sdr/SWIA202265559.md): None · corroded · Apr 6, 2022 · N200SY · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > CORROSION, AFT WET AREA, ON LH LONGITUDINAL FLOOR BEAM AT FRAME 87 WHERE THE BEAM PASSES BETWEEN THE LH AND CENTER SHEAR PANELS. (C-CHECK RO 5/4/2022) REMOVED AND REPLACED L/H LONGITUDINAL FLOOR BEAM AT FR 87. REF EMB SRM 51-40-08. SEE CONTINUATION FOR
- [SDR SWIA202265558](https://openairdocs.org/sdr/SWIA202265558.md): None · corroded · Apr 6, 2022 · N200SY · Emb ERJ170200LR · Fuselage, Powerplant Attach Fittings
  > CORROSION, AFT WET AREA ON END OF RH INBOARD SEAT TRACK BETWEEN FRAME 84 AND 85. (C-CHECK RO 5/4/2022) BLENDED AND EVALUATED CORROSION, AFT WET AREA ON END OF LH INBOARD SEAT TRACK BETWEEN FR 84 AND 85. MEASUREMENTS 0.39"L X 0.33"W X 0.75"H. NOMINAL THI
- [SDR SWIA202265557](https://openairdocs.org/sdr/SWIA202265557.md): None · corroded · Apr 6, 2022 · N200SY · Emb ERJ170200LR · Fuselage, Powerplant Attach Fittings
  > CORROSION, AFT WET AREA ON END OF LH INBOARD SEAT TRACK BETWEEN FRAME 84 AND 85. (C-CHECK RO 5/4/2022) BLENDED AND EVALUATED CORROSION, AFT WET AREA ON END OF LH INBOARD SEAT TRACK BETWEEN FR 84 AND 85. MEASUREMENTS 0.39"L X 0.33"W X 0.19"H. NOMINAL THI
- [SDR SWIA202265555](https://openairdocs.org/sdr/SWIA202265555.md): None · corroded · Apr 6, 2022 · N200SY · Emb ERJ170200LR · Fuselage Main, Frame
  > CORROSION, AFT WET AREA, ON FRAME 90 CROSS BEAM LEFT END BELOW THE AFT END OF THE LH PANEL SUPPORT (X = -28€?). (C-CHECK RO 5/4/2022) REMOVED AND REPLACED FRAME 90 CROSS BEAM REF SRM 51-40-08
- [SDR SWIA2019081346179](https://openairdocs.org/sdr/SWIA2019081346179.md): Unknown · odor · Aug 13, 2019 · N200SY · Emb ERJ170200LR · Air Distribution System
  > AFT FLIGHT ATTENDANT REPORTED SMOKE LIKE SMELL IN AFT CABIN. FLIGHT CREW REPORTS NO SMOKE DETECTOR MESSAGES OR WARNINGS. NO REPORTS OF SMOKE SEEN. NO ODD ENGINES PARAMETERS NOTED. LANDING NORMAL. (FLT5934) CONFIRMED WITH CREW THAT APU BLEED WAS OFF. PERFORMED

## 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 = 'N200SY' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N200SY/reports

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