# Service difficulty reports: N213NN

A list on [N213NN](https://openairdocs.org/aircraft/N213NN.md).

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

- [SDR SIMA20260816002](https://openairdocs.org/sdr/SIMA20260816002.md): Seat Track · corroded · Aug 16, 2026 · N213NN · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > POSSIBLE CORROSION AT MAIN CABIN RH LONGITUDINAL SEAT TRACK AT FRAME 82, (MAJOR REPAIR) (LEVEL 2 CORROSION) BLENDED CORROSION AT RH SEAT TRACK FR 82 BELOW TEETH IAW SRM 51-10-03. L=1" W=.75" D=.035" AND IS FOUND TO BE OUT OF LIMITS IAW SRM 53-23- 10/AD01. LOCA
- [SDR SIMA20260816003](https://openairdocs.org/sdr/SIMA20260816003.md): Seat Track · corroded · Aug 16, 2026 · N213NN · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > POSSIBLE CORROSION AT MAIN CABIN LH LONGITUDINAL SEAT TRACK AT FRAME 82, (MAJOR REPAIR) (LEVEL 2 CORROSION) BLENDED CORROSION AT LH SEAT TRACK AT FR 84 UNDER TEETH IAW SRM 51-10-03. L=1" W=.5" D=.030" AND IS FOUND TO BE OUT OF LIMITS PER EMB 175 SRM 53-23- 10/
- [SDR SIMA20260810002](https://openairdocs.org/sdr/SIMA20260810002.md): Floorbeam · corroded · Aug 10, 2026 · N213NN · Emb ERJ170200LR · Fuselage Main, Floor Beam
  > AFT WET AREA FLOOR STRUCTURE CORROSION ON RH BEAM AT FR 87 Y +12". (MAJOR REPAIR) (LEVEL 2 CORROSION) BLEND MEASUREMENTS OF AFT WET AREA FLOOR STRUCTURE CORROSION ON RH BEAM AT FR 87 Y +12" MEASURE L=.3" W=.2" D=.022". PART IS OUT OF LIMITS PER EMB 175 SRM 53-
- [SDR SIMA20260810001](https://openairdocs.org/sdr/SIMA20260810001.md): Floorbeam · corroded · Aug 10, 2026 · N213NN · Emb ERJ170200LR · Fuselage Main, Floor Beam
  > AFT WET AREA FLOOR STRUCTURE CORROSION ON LT BEAM AT FR 87 Y -12". (MAJOR REPAIR) (LEVEL 2 CORROSION) MEASUREMENTS OF AFT WET AREA FL OOR STRUCTURE CORROSION ON LH BEAM AT FR 87 Y -12" MEASURES L=.2" W=.1" D=.025" FOUND TO BE OUT OF LIMITS PER EMB 175 SRM 53-2
- [SDR SIMA20260718002](https://openairdocs.org/sdr/SIMA20260718002.md): Pin · corroded · Jul 18, 2026 · N213NN · Emb ERJ170200LR · Main Landing Gear
  > RIGHT MLG SHOCK STRUT AFT PINTLE PIN HAS CORROSION. (LEVEL 2 CORROSION) REMOVED AND REPLACED RH MLG AFT PINTLE PIN IAW AMM 32-11-01. PN OFF:1810- 0024 SN OFF:L1180 PN ON:1840-0024 SN ON:L 2194
- [SDR SIMA20260718001](https://openairdocs.org/sdr/SIMA20260718001.md): Pin · corroded · Jul 18, 2026 · N213NN · Emb ERJ170200LR · Main Landing Gear
  > RIGHT MLG SHOCK STRUT FWD PINTLE PIN HAS CORROSION. (MAJOR REPAIR) (LEVEL 2 CORROSION) REMOVED AND REPLACED RH MLG FWD PINTLE PIN REF:EMB 175 AMM 32-11-01. PN OFF:1840- 0002 SN OFF:L2252 PN ON:1840-0002 SN ON:L 3201
- [SDR SIMA20260717004](https://openairdocs.org/sdr/SIMA20260717004.md): Rod · gouged · Jul 17, 2026 · N213NN · Emb ERJ170200LR · Flight Compartment Windows
  > GOUGED AT PILOT DV WINDOW LOWER ROD MECHANISM. (MAJOR REPAIR) BLENDED ON PILOT DV WINDOW LOWER ROD MECHANISM IAW EMB-175 SRM 51-10-03. DAMAGE DIAMETER MEASUREMENT IS 0.688" AND CANNOT EXCEED MINIMUM DIAMETER OF 0.696" PER EMB-175 AMM 56-12-00/ 800, SUBTASK 300
- [SDR SIMA20260716014](https://openairdocs.org/sdr/SIMA20260716014.md): Shear Tie · corroded · Jul 16, 2026 · N213NN · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > AFT CARGO FRAME HAS CORROSION AT FR 87 BTWN STR 28R - STR 27R. (MAJOR REPAIR) (LEVEL 2 CORROSION) BLENDED CORROSION ON AFT CARGO FRAME 87 BTWN STR 28R - 27R IAW E-175 SRM 51-10-03. ORIGINAL THICKNESS.063" IAW SRM 53-23-04. MATERIAL REMOVED.040" MATERIAL REMA
- [SDR SIMA20260716007](https://openairdocs.org/sdr/SIMA20260716007.md): Shear Tie · corroded · Jul 16, 2026 · N213NN · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > AFT CARGO FRAME SHEAR CLIP HAS CORROSION AT FR 81 BETWEEN STR 28R - STR 29R (MAJOR REPAIR) (LEVEL 2 CORROSION) EVALUATED SHEAR CLIP AT FR 81 BETWEEN STR 28R - STR 29R IS FOUND TO BE CORRODED PER EMB-175 SRM 51-10-02. NO ALLOWABLE LIMITS. REMOVED SHEAR CLIP AT
- [SDR SIMA20260716008](https://openairdocs.org/sdr/SIMA20260716008.md): Shear Tie · corroded · Jul 16, 2026 · N213NN · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > AFT CARGO SHEAR CLIP HAS CORROSION AT FR 88 BETWEEN STR 28R - STR 27R. (MAJOR REPAIR) (LEVEL 2 CORROSION) EVALUATED SHEAR CLIP AT FR 88 BETWEEN STR 28R - STR 27R IS FOUND TO BE CORRODED PER EMB-175 SRM 51-10-02. NO ALLOWABLE LIMITS. REMOVED SHEAR CLIP AT FR 88
- [SDR SIMA20260803006](https://openairdocs.org/sdr/SIMA20260803006.md): Frame · corroded · Jul 16, 2026 · N213NN · Emb ERJ170200LR · Fuselage Main, Frame
  > AFT CARGO FRAME HAS CORROSION AT FR 88 BETWEEN STR 28R - STR 27R. (MAJOR REPAIR) (LEVEL 2 CORROSION) BLENDED CORROSION ON AFT CARGO FRAME 88 BETWEEN STR 28R - 27R IAW E-175 SRM 51-10-03. BLENDED AREA MEASURES L= 6" W=4" H=.027". ORIGINAL THICKNESS.063" IAW E-
- [SDR SIMA20260803011](https://openairdocs.org/sdr/SIMA20260803011.md): Shear Tie · corroded · Jul 16, 2026 · N213NN · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > AFT CARGO FRAME SHEAR CLIP HAS CORROSION AT FR 85 BETWEEN STR 28R - STR 27R. (MAJOR REPAIR) (LEVEL 2 CORROSION) EVALUATED SHEAR CLIP AT FR 85 BETWEEN STR 28R - STR 27R IS FOUND TO BE CORRODED PER EMB-175 SRM 51-10-02. NO ALLOWABLE LIMITS. REMOVED SHEAR CLIP AT
- [SDR SIMA20260716012](https://openairdocs.org/sdr/SIMA20260716012.md): Shear Tie · corroded · Jul 16, 2026 · N213NN · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > AFT CARGO FRAME SHEAR CLIP HAS CORROSION AT FR 84 BETWEEN STR 28R - STR 27R. (MAJOR REPAIR) (LEVEL 2 CORROSION) EVALUATED SHEAR CLIP AT FR 84 BETWEEN STR 28R - STR 27R IS FOUND TO BE CORRODED PER EMB-175 SRM 51-10-02. NO ALLOWABLE LIMITS. REMOVED SHEAR CLIP AT
- [SDR SIMA20260716013](https://openairdocs.org/sdr/SIMA20260716013.md): Shear Tie · corroded · Jul 16, 2026 · N213NN · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > AFT CARGO SHEAR CLIP HAS CORROSION AT FR 86 BETWEEN STR 28R - STR 27R. (MAJOR REPAIR) (LEVEL 2 CORROSION) EVALUATED SHEAR CLIP AT FR 86 BETWEEN STR 28R - STR 27R IS FOUND TO BE CORRODED PER EMB-175 SRM 51-10-02. NO ALLOWABLE LIMITS. REMOVED SHEAR CLIP AT FR 86
- [SDR SIMA20260716009](https://openairdocs.org/sdr/SIMA20260716009.md): Shear Tie · corroded · Jul 16, 2026 · N213NN · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > AFT CARGO, FRAME SHEAR CLIP, HAS CORROSION AT FR 82 BETWEEN STR 28R - STR 27R. (MAJOR REPAIR) (LEVEL 2 CORROSION) EVALUATED SHEAR CLIP AT FR 82 BETWEEN STR 28R - STR 27R IS FOUND TO BE CORRODED PER EMB-175 SRM 51-10-02. NO ALLOWABLE LIMITS. REMOVED SHEAR CLIP
- [SDR SIMA20260716005](https://openairdocs.org/sdr/SIMA20260716005.md): Shear Tie · corroded · Jul 16, 2026 · N213NN · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > AFT CARGO FRAME SHEAR CLIP HAS CORROSION AT FR 83 BETWEEN STR 28R - STR 27R. (MAJOR REPAIR) (LEVEL 2 CORROSION) EVALUATED SHEAR CLIP AT FR 83 BETWEEN STR 28R - STR 27R IS FOUND TO BE CORRODED PER EMB-175 SRM 51-10-02. NO ALLOWABLE LIMITS. REMOVED SHEAR CLIP AT
- [SDR SIMA20260716010](https://openairdocs.org/sdr/SIMA20260716010.md): Shear Tie · corroded · Jul 16, 2026 · N213NN · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > SSI 53-23-003-009 AFT CARGO FRAME SHEAR CLIP HAS CORROSION AT FR 81 BETWEEN STR 28R - STR 27R. (MAJOR REPAIR) (LEVEL 2 CORROSION) EVALUATED SHEAR CLIP AT FR 81 BETWEEN STR 28R - STR 27R AND FOUND TO BE CORRODED PER EMB-175 SRM 51-10-02. NO ALLOWABLE LIMITS. RE
- [SDR SIMA20260713005](https://openairdocs.org/sdr/SIMA20260713005.md): Profile · gouged · Jul 13, 2026 · N213NN · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > SSI 52-43-002-0001 FWD AVONICS BAY ACCESS DOOR HAS GOUGING ON SURROUND FRAME WITH PREVIOUS BLENDING COMMON TO BOTH AFT DOORSTOP FITTINGS. (MAJOR REPAIR) EVALUATED GOUGES ON DOOR NO ALLOWABLE LIMITS FOUND. LOCATED, DRILLED, DEBURRED, AND TREATED FASTENER HOLES
- [SDR SIMA20260803004](https://openairdocs.org/sdr/SIMA20260803004.md): Seat Track · corroded · Jul 13, 2026 · N213NN · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RH TRACK AT FR 17, Y= +10" (MAJOR REPAIR) (LEVEL 2 CORROSION) BLENDED CORROSION ON RT TRACK AT FR 17, Y=+10" IAW E-175 SRM 51-10-03. BLENDED AREA MEASURES L=1.5" W=1" H=.051" MAX MATERIAL LOSS ON RH SEAT TRACK FLANGE AT FR 17, Y+10" IS.051" OUT O
- [SDR SIMA20260713003](https://openairdocs.org/sdr/SIMA20260713003.md): Seat Track · corroded · Jul 13, 2026 · N213NN · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON LH TRACK IN MULTIPLE LOCATIONS BETWEEN FRS 18-20, Y=-10". (MAJOR REPAIR) (LEVEL 2 CORROSION) BLENDED ON FWD LH SEAT TRACK PER EMB 175 SRM 51-10-03. BLENDED 3EA AREAS. BLEND 1 MEASURES L=2.0" W=.8" D=.042", BLEND 2 MEASURES L=2.1" W=.9" D=.040", BL
- [SDR SIMA20260710002](https://openairdocs.org/sdr/SIMA20260710002.md): Beam · corroded · Jul 10, 2026 · N213NN · Emb ERJ170200LR · Fuselage Main, Structure
  > FWD CARGO DOOR CUTOUT LOWER BEAM HAS CORROSION ON TOP SURFACE TOWARDS MIDDLE OF BEAM. (MAJOR REPAIR) (LEVEL 2 CORROSION) BLENDED CORROSION ON FWD CARGO DOOR AFT FINGER PLATE PER EMB-175 SRM 51-10-03. BLENDED AREA MEASURES L=4.100" W=2.200" H=.025" AND WAS FOU
- [SDR SIMA20260803003](https://openairdocs.org/sdr/SIMA20260803003.md): Shear Tie · corroded · Jun 16, 2026 · N213NN · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > AFT CARGO, FRAME SHEAR CLIP, HAS CORROSION AT FR 87 BETWEEN STR 28R - STR 27R. (MAJOR REPAIR) (LEVEL 2 CORROSION) EVALUATED SHEAR CLIP AT FR 87 BETWEEN STR 28R - STR 27R IS FOUND TO BE CORRODED PER SRM 51-10-02. NO ALLOWABLE LIMITS. REMOVED SHEAR CLIP AT FR 87
- [SDR SIMA20260607001](https://openairdocs.org/sdr/SIMA20260607001.md): Torque Tube · failed · Jun 7, 2026 · N213NN · Emb ERJ170200LR · Leading Edge Slat Control System
  > SLAT FAIL ON APPROACH. TRANSFERRED TO NRWC 013-ORD-04163 EMERGENCY DECLARED. R & R SLAT TORQUE TUBE LT WING MOST OUTBOARD IAW AMM 27-81-03. OPS CHKD GOOD,
- [SDR SIMA20260308002](https://openairdocs.org/sdr/SIMA20260308002.md): Light · inoperative · Mar 8, 2026 · N213NN · Emb ERJ170200LR · Emergency Lighting
  > PHOTOLUMINESCENT INDICATOR STRIP LIGHTS INOP IN FWD GALLEY. RAR PHOTOLUMINESCENT INDICATOR STRIP LIGHTS AT FWD GALLEY IAW AMM 33-50-21. NO FUTHER DEFECTS NOTED.
- [SDR SIMA20260308001](https://openairdocs.org/sdr/SIMA20260308001.md): Light · inoperative · Mar 8, 2026 · N213NN · Emb ERJ170200LR · Emergency Lighting
  > EMERGENCY PHOTOLUMINESCENT INDICATOR STRIP LIGHT INOP AT SEAT 3FD 4FD 22FD AND 23 FD. R & R EMERGENCY PHOTOLUMINESCENT INDICATOR STRIP LIGHT INOP AT SEAT 3FD 4FD 22FD AND 23 FD IAW AMM 33-50-21. NO FUTHER DEFECTS NOTED.
- [SDR SIMA2023111326003](https://openairdocs.org/sdr/SIMA2023111326003.md): Seat Track · corroded · Oct 26, 2023 · N213NN · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > RH TRACK CORRODED BETWEEN FR 13 AND 14 (LEVEL 2 CORROSION).-C/A-BLENDED CORROSION FROM RH SEAT TRACK AT FR13 AND FR 14. FOUND TO BE CORRODED OUT OF ALLOWABLE LIMITS IAW EMB SRM 53-00-01. REMOVED CORRODED SEAT TRACK IAW EMB SRM 51-40-08. DRILLED NEW RH SEAT TRA
- [SDR SIMA2023111326001](https://openairdocs.org/sdr/SIMA2023111326001.md): Unknown · unknown · Oct 26, 2023 · N213NN · Emb ERJ170200LR · Fuselage Main, Structure
  > BEAM AT FR 87 Y-11 CORRODED (LEVEL 2 CORROSION)-C/A-BLENDED CORROSION ON BEAM AT FR 87Y -11 PER EMB SRM 51-10-03. FOUND TO BE OUT OF LIIMITS. REMOVED CORRODED BEAM AT FR 87 Y-11 IAW EMB SRM 51-40-08. LOCATED AND DRILLED NEW BEAM PN 170-65669-003 IAW EMB SRM 51
- [SDR SIMA2023111326002](https://openairdocs.org/sdr/SIMA2023111326002.md): Beam · corroded · Oct 26, 2023 · N213NN · Emb ERJ170200LR · Fuselage Main, Structure
  > BEAM AT FR 87 Y+11 CORRODED (LEVEL 2 CORROSION)-C/A-BLENDED CORROSION ON BEAM AT FR 87 Y+11. ORIGINAL THICKNESS.080" REOMOVED.040" REMAINING.040" OUT OF LIMITS PER E175 SRM 53-23-10. REMOVED BEAM AT FR87 Y+11 IAW EMB SRM 51-40-08 RECEIVED NEW BEAM PN 170-65
- [SDR SIMA20220315002](https://openairdocs.org/sdr/SIMA20220315002.md): Light · damaged · Mar 15, 2022 · N213NN · Emb ERJ170200LR · Emergency Lighting
  > FIRST CLASS EMERGENCY PHOTOLUMINESCENT STRIP DAMAGE-C/A-RAR FIRST CLASS EMERGENCY PHOTOLUMINESCENT STRIP IAW AMM 33-50-21
- [SDR SIMA20211023001](https://openairdocs.org/sdr/SIMA20211023001.md): None · none · Oct 23, 2021 · N213NN · Emb ERJ170200LR · Emergency Lighting
  > FWD SERVICE DOOR EMERGENCY EXIT SIGN INOP-C/A-RAR FWD SERVICE EXIT IDENTIFIER SIGN IAW AMM 33-50-15. OPC BAD. TROUBLESHOT IAW FIM 33-50-00-810-816-A RAR RH FWD EMERGENCY-LIGHT POWER UNIT IAW AMM 33-50-01. OPC GOOD. NO FURTHER DEFECTS NOTED
- [SDR SIMA20210522003](https://openairdocs.org/sdr/SIMA20210522003.md): Autothrottle Sys · failed · May 22, 2021 · N213NN · Emb ERJ170200LR · Autopilot System
  > ABORTED TAKEOFF 90KTS- ON TAKE OFF ROLL WITH AUTO THROTTLE ENGAGED AND THRUST ALREADY SET GOT AT FAIL AND AT FAULT REJECTED T/O PRIOR TO 80 KTS BUT A/C DID GET TO 90KTS BEFORE DECELLERATING ACFT RTG AND SWAP.-C/A-PERFOMED AUTO THROTTLE FUNCTION TEST IAW AMM TA
- [SDR SIMA20210201001](https://openairdocs.org/sdr/SIMA20210201001.md): Power Supply · inoperative · Feb 1, 2021 · N213NN · Emb ERJ170200LR · Emergency Lighting
  > PAX CABIN CEILING PNL 227BLC EMERGENCY EXIT LIGHT DOES NOT ILLUMINATE-C/A-PERFORMED TROUBLESHOOTING OF EMERGENCY LIGHT PANELS NOT LIGHTING UP AND DETERMINED THAT THE POWER UNIT WAS NOT SUPPLYING REQUIRED POWER. REMOVED AND REPLACEDEMOERGENCY POWER SUPPLY REF E
- [SDR SIMA20210109007](https://openairdocs.org/sdr/SIMA20210109007.md): Seat Track · corroded · Jan 9, 2021 · N213NN · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION RT INBOARD SEAT TRACK CORRODED, AS MARKED FR 84. LEVEL 2 CORROSION. C/A: INSTALLED NEW RT INBOARD SEAT TRACK SPLICEREPAIR PARTS AT FR 84 NCR-EJ-53-025 ETD2021-170--0008883.
- [SDR SIMA20210109006](https://openairdocs.org/sdr/SIMA20210109006.md): Beam · corroded · Jan 9, 2021 · N213NN · Emb ERJ170200LR · Fuselage Main, Structure
  > CORROSION RT AFT SERVICE DOOR BEAM CORRODED, AS MARKED AT FWD AND AFT GIRT BAR FITTINGS. EVALUATION LEVEL 2 CORROSION. C/A: REMOVED AND REPLACED RT AFT SERVICE DOOR THRESHOLD BEAM, REF SRM 51-40--08.
- [SDR C77A202001070010](https://openairdocs.org/sdr/C77A202001070010.md): Shutoff Valve · inoperative · Jan 5, 2020 · N213NN · Emb ERJ170200LR · Landing Gear Brake System
  > L/H BRAKE FAULT MSG UPON GEAR EXTENSION. PERFORMED QRH 13.12.
- [SDR C77A2019111500007](https://openairdocs.org/sdr/C77A2019111500007.md): Rib · dented · Nov 15, 2019 · N213NN · Emb ERJ170200LR · Horizontal Stabilizer, Spar/Rib
  > WHILE TAXIING IN PDX, AIRCRAFT 213NN WAS STRUCK BY ANOTHER AIRCRAFT BEING TOWED. EXTENSIVE DAMAGE WAS SUSTAINED TO THE RH HORIZONTAL STABILIZER. THE RH ELEVATOR WAS FRACTURED COMPLETELY AND WILL BE REPLACED SEPARATELY FROM THIS EO. THE RH HORIZONTAL STABILIZER
- [SDR C77A2019111500006](https://openairdocs.org/sdr/C77A2019111500006.md): Rib · dented · Nov 15, 2019 · N213NN · Emb ERJ170200LR · Horizontal Stabilizer, Spar/Rib
  > WHILE TAXIING IN PDX, AIRCRAFT 213NN WAS STRUCK BY ANOTHER AIRCRAFT BEING TOWED. EXTENSIVE DAMAGE WAS SUSTAINED TO THE RH HORIZONTAL STABILIZER. THE RH ELEVATOR WAS FRACTURED COMPLETELY AND WILL BE REPLACED SEPARATELY FROM THIS EO. THE RH HORIZONTAL STABILIZER
- [SDR C77A2019111500005](https://openairdocs.org/sdr/C77A2019111500005.md): Rib · dented · Nov 15, 2019 · N213NN · Emb ERJ170200LR · Horizontal Stabilizer, Spar/Rib
  > WHILE TAXIING IN PDX, AIRCRAFT 213NN WAS STRUCK BY ANOTHER AIRCRAFT BEING TOWED. EXTENSIVE DAMAGE WAS SUSTAINED TO THE RH HORIZONTAL STABILIZER. THE RH ELEVATOR WAS FRACTURED COMPLETELY AND WILL BE REPLACED SEPARATELY FROM THIS EO. THE RH HORIZONTAL STABILIZER
- [SDR C77A2019111500004](https://openairdocs.org/sdr/C77A2019111500004.md): Rib · dented · Nov 15, 2019 · N213NN · Emb ERJ170200LR · Horizontal Stabilizer, Spar/Rib
  > WHILE TAXIING IN PDX, AIRCRAFT 213NN WAS STRUCK BY ANOTHER AIRCRAFT BEING TOWED. EXTENSIVE DAMAGE WAS SUSTAINED TO THE RH HORIZONTAL STABILIZER. THE RH ELEVATOR WAS FRACTURED COMPLETELY AND WILL BE REPLACED SEPARATELY FROM THIS EO. THE RH HORIZONTAL STABILIZER
- [SDR C77A2019111500003](https://openairdocs.org/sdr/C77A2019111500003.md): Rib · dented · Nov 15, 2019 · N213NN · Emb ERJ170200LR · Horizontal Stabilizer, Spar/Rib
  > WHILE TAXIING IN PDX, AIRCRAFT 213NN WAS STRUCK BY ANOTHER AIRCRAFT BEING TOWED. EXTENSIVE DAMAGE WAS SUSTAINED TO THE RH HORIZONTAL STABILIZER. THE RH ELEVATOR WAS FRACTURED COMPLETELY AND WILL BE REPLACED SEPARATELY FROM THIS EO. THE RH HORIZONTAL STABILIZER
- [SDR C77A2019111500002](https://openairdocs.org/sdr/C77A2019111500002.md): Skin · dented · Nov 15, 2019 · N213NN · Emb ERJ170200LR · Horizontal Stabilizer, Plate/Skin
  > WHILE TAXIING IN PDX, AIRCRAFT 213NN WAS STRUCK BY ANOTHER AIRCRAFT BEING TOWED. EXTENSIVE DAMAGE WAS SUSTAINED TO THE RH HORIZONTAL STABILIZER. THE RH ELEVATOR WAS FRACTURED COMPLETELY AND WILL BE REPLACED SEPARATELY FROM THIS EO. THE RH HORIZONTAL STABILIZER
- [SDR C77A2019111500001](https://openairdocs.org/sdr/C77A2019111500001.md): Skin · dented · Nov 15, 2019 · N213NN · Emb ERJ170200LR · Horizontal Stabilizer, Plate/Skin
  > WHILE TAXIING IN PDX, AIRCRAFT 213NN WAS STRUCK BY ANOTHER AIRCRAFT BEING TOWED. EXTENSIVE DAMAGE WAS SUSTAINED TO THE RH HORIZONTAL STABILIZER. THE RH ELEVATOR WAS FRACTURED COMPLETELY AND WILL BE REPLACED SEPARATELY FROM THIS EO. THE RH HORIZONTAL STABILIZER
- [SDR C77A20171127003](https://openairdocs.org/sdr/C77A20171127003.md): Power Supply · inoperative · Nov 26, 2017 · N213NN · Emb ERJ170200LR · Emergency Lighting
  > FWD CABIN EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED THE FWD L/H ELPU IAW AMM 33-50-01, OPS CHECKED GOOD. MSG CLEARED NO FURTHER DEFECTS NOTED.
- [SDR C77A20161115005](https://openairdocs.org/sdr/C77A20161115005.md): Diaphragm · damaged · Nov 13, 2016 · N213NN · Emb ERJ170200LR · Passenger/Crew Doors
  > DURING L2 DOOR ASSIST BOTTLE 48 HR CHECK, FOUND BOTTLE BELOW EXCEPTABLE LIMITS. REMOVED AND REPLACED AFT PASSENGER DOOR PNEUMATIC ASSY. DIAPHRAGMIAW AMM 52-12-53. SERVICED L2 DOOR ASSY. BTL IAW AMM 52-12-51 TO 2100 PSI. NO FURTHER DEFECTS NOTED AT THIS TIME.
- [SDR C77A20161011003](https://openairdocs.org/sdr/C77A20161011003.md): Flashlight · missing · Oct 9, 2016 · N213NN · Emb ERJ170200LR · Emergency Equipment
  > L1 FLASHLIGHT MISSING. INSTALLED THE L1 FLASHLIGHT IAW AMM 33-51-01. OPS CHECKED GOOD

## 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 = 'N213NN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N213NN/reports

---
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.