# Service difficulty reports: N261NN

A list on [N261NN](https://openairdocs.org/aircraft/N261NN.md).

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

- [SDR SIMA20260829001](https://openairdocs.org/sdr/SIMA20260829001.md): Sign · cracked · Aug 29, 2026 · N261NN · Emb ERJ170200LR · Emergency Lighting
  > EXIT SIGN ABOVE 1R DOOR MISSING. INSTALLED EXIT-MARKING-SIGN LENS ON R1 DOOR IAW AMM33-50-17 OPS CHECK GOOD
- [SDR SIMA20260501001](https://openairdocs.org/sdr/SIMA20260501001.md): Battery · inoperative · May 1, 2026 · N261NN · Emb ERJ170200LR · Emergency Lighting
  > INTERIOR EMERGENCY LIGHTS CEILING LIGHTS OUT 1ST AND 3RD ROW. REF AML: 101701098, MEL 3308 - AUTH# 05-44D-C REPAIR C - POSITION EMERGEN - FMR 06133033A - MEL DEFERRAL - CATEGORY C.. RAR EMERGENCY POWER UNIT 2 IAW AMM 33-50-01. OPS CHECK GOOD. MEL ITEM RESTORE
- [SDR SIMA20260406002](https://openairdocs.org/sdr/SIMA20260406002.md): Shear Tie · corroded · Mar 16, 2026 · N261NN · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > SHEAR TIE ON FRAME 86 BTWN STR 28R AND 27R IS CORRODED (MAJOR REPAIR) BLENDED CORROSION ON SHEAR TIE FR86 BETWEEN STR 28R & 27R IAW SRM 51-10-03. ORIGINAL THICKNESS.050" IAW SRM 53-23-04. MATERIAL REMOVED.030" MATERIAL REMAINING.020" FOUND OUT OF ALLOWABLE
- [SDR SIMA20260406003](https://openairdocs.org/sdr/SIMA20260406003.md): Rib · cracked · Mar 16, 2026 · N261NN · Emb ERJ170200LR · Horizontal Stabilizer, Spar/Rib
  > RH HORIZONTAL STABILIZER RIB 14 IS CRACKED ON UPPER AFT SIDE. (MAJOR REPAIR). REMOVED RH HORIZONTAL STABILIZER RIB 14 PER EMB 175 SRM 51-40-08. LOCATED AND DRILLED NEW RH HORIZONTAL STAB RIB 14 PN: 170-62620-002 PER EMB 175 SRM 51-40-02, INSTALLED 30EA NUT PLA
- [SDR SIMA202604064001](https://openairdocs.org/sdr/SIMA202604064001.md): Seat Track · corroded · Mar 14, 2026 · N261NN · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK IS CORRODED BETWEEN FR 84 & 85, Y+276 (MAJOR REPAIR). BLENDED CORROSION IN MULTIPLE AREAS, AREAS OUT OF ALLOWABLE LIMITS IAW SRM 53-23-10 AD01. REMOVED DAMAGED SECTION OF RT AFT SEAT TRACK IAW ETD2022-170-022163 REV.:C. LOCATED, TRIMMED, DRILLE
- [SDR SIMA20260314003](https://openairdocs.org/sdr/SIMA20260314003.md): Floorbeam · corroded · Mar 14, 2026 · N261NN · Emb ERJ170200LR · Fuselage Main, Floor Beam
  > RIGHT FLOORBEAM CORRODED, Y+276 AFT OF FRAME FR 90 (MAJOR REPAIR). BLENDED CORROSION ON RT FLOORBEAM IAW SRM 51-10-03. BLENDED AREA MEASURES (INTERCOSTAL - W =1.3", L = 2.0", H = 010".) ORIGINAL MATERIAL THICKNESS OF.040, (ANGLE - W =.8", L = 2.- 0", H =.0
- [SDR SIMA20260310011](https://openairdocs.org/sdr/SIMA20260310011.md): Shear Tie · corroded · Mar 10, 2026 · N261NN · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > SHEAR CLIP ON FRAME 86 BETWEEN STRINGERS 28R AND 27R IS CORRODED (LEVEL 2 CORROSION) REMOVED AND REPLACED SHEAR CLIP (SHEAR CLIP PN 170-66033-001, P.O.# 349163) AT FR 86 BETWEEN STR 27R - 28R REF EMB 175 SRM 51-40-08. (MS14218AD5-5 PO# 321413, MS2047AD5-5 PO3
- [SDR SIMA20260310010](https://openairdocs.org/sdr/SIMA20260310010.md): Seat Track · corroded · Mar 10, 2026 · N261NN · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > RH FLOOR BEAM CORRODED @ Y+276 AFT OF FRAME FR90 (LEVEL 2 CORROSION) REMOVED AND REPLACED INTERCOSTAL (RH FLOOR BEAM) PART# 170-61041-402 PO# 349163 AND ANGLE SUPPORT PART# 170-60287- 002 PO# 349163) IAW E-175 SRM 51-40-08. SEE WIPS AND TASK FOR ALL WORK ACC
- [SDR SIMA20260228002](https://openairdocs.org/sdr/SIMA20260228002.md): Unknown · vibration · Feb 28, 2026 · N261NN · Emb ERJ170200LR · Engine (Turbine/Turboprop)
  > HIGH N2 VIBES. RAN QRH. VIBES STAYED BELOW LEVEL 4. EMERGENCY DECLARED. PENDING CORRECTIVE ACTION.
- [SDR SIMA20250904001](https://openairdocs.org/sdr/SIMA20250904001.md): Steering Sys · faulted · Sep 4, 2025 · N261NN · Emb ERJ170200LR · Landing Gear Steering System
  > STEER FAIL CAUTION MESSAGE. RAN QRH AND DID NOT SOLVE THE PROBLEM. STEERING WHEEL WAS ENGAGED AT ABOUT 22 KNOTS GROUND SPEED ON ROLLOUT FROM LANDING. FAIL MESSAGE OCCURRED AS WE STARTED TURNING, WE WE'RE ABLE TO SMOOTHLY STOP. PERFORMED STEERING FEEDBACK SENSO
- [SDR SIMA20250807003](https://openairdocs.org/sdr/SIMA20250807003.md): Sensor · failed · Aug 7, 2025 · N261NN · Emb ERJ170200LR · Leading Edge Slat Position Indicating System
  > SLAT FAIL FLAP FAIL ON EICAS. SOFT LANDING LESS THEN 300 FPM WEIGHT 72,000 LBS. TRANSFERRED TO NRWC 061-DFW-04708 ITEM-1. EMERGENCY DECLARED. R & R OUTBOARD LEFT SLAT SKEW SENSOR IAW AMM 27-83-01. OPS CHECKED GOOD.
- [SDR SIMA20240812002](https://openairdocs.org/sdr/SIMA20240812002.md): Light · inoperative · Aug 12, 2024 · N261NN · Emb ERJ170200LR · Emergency Lighting
  > EMERGENCY PHOTOLUMINESCENT INDICATOR STRIP LIGHT NEXT TO SEAT 3FD AND SEAT 4FD IS INOP REMOVE AND REPLACED EMERGENCY PHOTOLUMINESCENT INDICATOR STRIP LIGHT NEXT TO SEAT 3FD AND SEAT 4FD IAW AMM 33-50-21. OPS CHECK GOOD.
- [SDR SIMA20230716001](https://openairdocs.org/sdr/SIMA20230716001.md): Unknown · unknown · Jul 16, 2023 · N261NN · Emb ERJ170200LR · AC Generation System
  > REJECTED TAKEOFF 110KTS DUE TO IDG2 FAIL. -C/A-PERFORMED HIGH ENERGY STOP CONDITION INSPECTION W/C IAW 05-50-12-200-801-A. NO DEFECTS NOTED AT THIS TIME.
- [SDR SIMA20230604002](https://openairdocs.org/sdr/SIMA20230604002.md): Unknown · corroded · Jun 4, 2023 · N261NN · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > CORRODED PANEL SUPPORT BETWEEN FRAME 89-90 STR 17R (LEVEL 2 CORROSION)
- [SDR SIMA20220720003](https://openairdocs.org/sdr/SIMA20220720003.md): Bleed Air Sys · dirty · Jul 20, 2022 · N261NN · Emb ERJ170200LR · Pneumatic Distribution System
  > E1 BLEED FAIL/DIVR TO LIT FOR MORE FUEL -C/A-T/S DLEED 1 FAIL MSG IAW FIM 36-11-00-810-809. CLEAN THE NAPRSOV FILTER IAW AMM 36-11-03. PERFORMED ENGINE PNEUMATIC BLEED SYSTEM OPERATIONAL CHECK IAW AMM 36-11-00. OPC GOOD. NO DEFECTS NOTED. MEL RESTORED.
- [SDR SIMA20201013004](https://openairdocs.org/sdr/SIMA20201013004.md): None · cracked · Oct 13, 2020 · N261NN · Emb EMB110* · Wing, Plate/Skin
  > RIGHT WING TIP SPAR 1 CRACKED INSIDE ACCESS PANEL 651AB-C/A-COMPLETE:THE RIGHT WING TIP SPAR 1 THAT IS CRACKED INSIDE ACCESS PANEL 651AB WILL BE REPLACED DURING THE ACCOMPLISHMENT OF EO EJ-5700-004R1 PART B. SEE NRTC E819785
- [SDR SIMA201912176001](https://openairdocs.org/sdr/SIMA201912176001.md): Static Wick · broken · Dec 16, 2019 · N261NN · Emb ERJ170200LR · Ailerons
  > L/H AILERON HAS TWO STATIC WICKS ALONG WITH MOUNT BASE BROKEN OFF WITH UPPER SKIN GOUGED AT SAME LOCATIONS. ONE DAMAGE 16,500 INCHES FROM OUTBOARD EDGE AND THE OTHER 3.500 INCHES FROM OUTBOARD EDGE.-C/A-ACCOMPLISHED PERMANENT REPAIR IAW ERS-EJ-57MR-1158
- [SDR SIMA20190810003](https://openairdocs.org/sdr/SIMA20190810003.md): None · none · Aug 10, 2019 · N261NN · Emb EMB110* · Wing Main, Frame Structure
  > INSPECT LH WINGLET TO WING SPAR 1 ATTACH FITTING FOR CRACKING.-C/A-COMPLIED WITH GVI OF LH WINGLET TO WING SPAR 1 ATTACH FITTING AND EDDY CURRENT INSPECTION IAW ENVOY NDT MANUAL TASK ET 0400-1 AND FOUND TO BE CRACKED. SEE ITEM 2 OF THIS NRWC.

## 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 = 'N261NN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N261NN/reports

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