N261NN

Service difficulty reports · 18

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

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR SIMA20260829001Sign · crackedEXIT SIGN ABOVE 1R DOOR MISSING. INSTALLED EXIT-MARKING-SIGN LENS ON R1 DOOR IAW AMM33-50-17 OPS CHECK GOODAug 29, 2026 · N261NN · Emb ERJ170200LR · Emergency LightingSDR SIMA20260501001Battery · inoperativeINTERIOR 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 RESTOREMay 1, 2026 · N261NN · Emb ERJ170200LR · Emergency LightingSDR SIMA20260406002Shear Tie · corrodedSHEAR 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 Mar 16, 2026 · N261NN · Emb ERJ170200LR · Fuselage Internal Mounting StructureSDR SIMA20260406003Rib · crackedRH 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 PLAMar 16, 2026 · N261NN · Emb ERJ170200LR · Horizontal Stabilizer, Spar/RibSDR SIMA202604064001Seat Track · corrodedSEAT 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, DRILLEMar 14, 2026 · N261NN · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach FittingsSDR SIMA20260314003Floorbeam · corrodedRIGHT 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 = .0Mar 14, 2026 · N261NN · Emb ERJ170200LR · Fuselage Main, Floor BeamSDR SIMA20260310011Shear Tie · corrodedSHEAR 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 PO3Mar 10, 2026 · N261NN · Emb ERJ170200LR · Fuselage Internal Mounting StructureSDR SIMA20260310010Seat Track · corrodedRH 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 ACCMar 10, 2026 · N261NN · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach FittingsSDR SIMA20260228002Unknown · vibrationHIGH N2 VIBES. RAN QRH. VIBES STAYED BELOW LEVEL 4. EMERGENCY DECLARED. PENDING CORRECTIVE ACTION.Feb 28, 2026 · N261NN · Emb ERJ170200LR · Engine (Turbine/Turboprop)SDR SIMA20250904001Steering Sys · faultedSTEER 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 SENSOSep 4, 2025 · N261NN · Emb ERJ170200LR · Landing Gear Steering SystemSDR SIMA20250807003Sensor · failedSLAT 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.Aug 7, 2025 · N261NN · Emb ERJ170200LR · Leading Edge Slat Position Indicating SystemSDR SIMA20240812002Light · inoperativeEMERGENCY 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.Aug 12, 2024 · N261NN · Emb ERJ170200LR · Emergency LightingSDR SIMA20230716001Unknown · unknownREJECTED 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.Jul 16, 2023 · N261NN · Emb ERJ170200LR · AC Generation SystemSDR SIMA20230604002Unknown · corrodedCORRODED PANEL SUPPORT BETWEEN FRAME 89-90 STR 17R (LEVEL 2 CORROSION)Jun 4, 2023 · N261NN · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR SIMA20220720003Bleed Air Sys · dirtyE1 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.Jul 20, 2022 · N261NN · Emb ERJ170200LR · Pneumatic Distribution SystemSDR SIMA20201013004None · crackedRIGHT 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 E819785Oct 13, 2020 · N261NN · Emb EMB110* · Wing, Plate/SkinSDR SIMA201912176001Static Wick · brokenL/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-1158Dec 16, 2019 · N261NN · Emb ERJ170200LR · AileronsSDR SIMA20190810003None · noneINSPECT 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.Aug 10, 2019 · N261NN · Emb EMB110* · Wing Main, Frame Structure
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