# Service difficulty reports: N241NN

A list on [N241NN](https://openairdocs.org/aircraft/N241NN.md).

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

- [SDR SIMA20260909001](https://openairdocs.org/sdr/SIMA20260909001.md): Track · lack of lube · Sep 9, 2026 · N241NN · Emb ERJ170200LR · Passenger/Crew Doors
  > GATE AGENT STATED L1 DOOR HARD TO OPEN CLEANED AND LUBRICATED L1 DOOR TRACKS AND ROLLERS. REF AMM 53-10-21. OPS CHK GOOD. NO FURTHER DEFECTS NOTED.
- [SDR SIMA202602132001](https://openairdocs.org/sdr/SIMA202602132001.md): Door · lack of lube · Feb 12, 2026 · N241NN · Emb ERJ170200LR · Passenger/Crew Doors
  > L1 DOOR VERY TIGHT AND HARD TO MOVE PER FLIGHT ATTENDANT & GATE AGENT. LUBRICATED THE L1 DOOR IAW AMM 12-26-00. OPS CHKD GOOD.
- [SDR SIMA20250626001](https://openairdocs.org/sdr/SIMA20250626001.md): Floorbeam · corroded · Jun 26, 2025 · N241NN · Emb ERJ170200LR · Fuselage Main, Floor Beam
  > AFT WET AREA CORROSION AT LH FLOOR BEAM FR86-87 @Y=-10. (MAJOR REPAIR) (LEVEL 2 CORROSION). BLENDED CORROSION ON LH FLOOR BEAM PER EMB 175 SRM 51-10-03. BLENDED AREA MEASURES (L:.50? W:.50? D:.030?) AND IS FOUND TO BE OUT OF LIMITS PER EMB 175 SRM 51-75-16.
- [SDR SIMA20250618002](https://openairdocs.org/sdr/SIMA20250618002.md): Floorbeam · corroded · Jun 18, 2025 · N241NN · Emb ERJ170200LR · Fuselage Main, Floor Beam
  > AFT WET AREA FLOOR STRUCTURE, RH BEAM AT FR 87 AND Y=+10.75? HAS CORROSION. (MAJOR REPAIR) (LEVEL 2 CORROSION). BLENDED CORROSION ON R/H BEAM AT FRAME 87 AND Y =+10.75" IAW E-175 SRM 51-10-03, MEASURED BEAM TO BE.088", MATERIAL LOSS.086" FOUND TO BE OUT OF A
- [SDR SIMA20250618003](https://openairdocs.org/sdr/SIMA20250618003.md): Floorbeam · gouged · Jun 18, 2025 · N241NN · Emb ERJ170200LR · Fuselage Main, Floor Beam
  > FLOOR BEAM GOUGED AT FWD WET AREA FR12- FR13, Y=+37". (MAJOR REPAIR). BLENDED GOUGED AREA PER EMB 175 SRM 51-10-03. AREA FOUND TO BE IN NO DAMAGE ALLOWABLE AREA PER EMB SRM 53-00-10/AD01. REMOVED BEAM AT FR12-13 Y= +37 PER EMB 175 SRM 51-40-08. LOCATED AND DRI
- [SDR SIMA20250617001](https://openairdocs.org/sdr/SIMA20250617001.md): Seat Track · corroded · Jun 17, 2025 · N241NN · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > RH LONGITUDINAL SEAT TRACK AT FR84 -7" AND Y= +10.75 HAS CORROSION (MAJOR REPAIR) (LEVEL 2 CORROSION). BLENDED RH LONGITUDINAL SEAT TRACK AT FR84 -7" AND Y= +10.75 PER EMB 175 SRM 51-10-03, UPON EVALUATION FOUND AREA TO BE IN A NO DAMAGE ALLOWED AREA AND OUT O
- [SDR SIMA20250617002](https://openairdocs.org/sdr/SIMA20250617002.md): Seat Track · corroded · Jun 17, 2025 · N241NN · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > LH LATERAL SEAT TRACK FROM FR74-FR84 HAS (5) GOUGES, SOME WITH CORROSION. (MAJOR REPAIR) (LEVEL 2 CORROSION). BLENDED SEAT TRACK FROM FRS-74-84 PER SRM 51-10-03. MEASUREMENTS FOR THE DEEPEST BLEND IS L=1 W=0.4 D=0.020 DEPTH OF 0.020 IS FOUND TO BE OUT OF LIMI
- [SDR SIMA2025041106003](https://openairdocs.org/sdr/SIMA2025041106003.md): Tire · flat · Apr 6, 2025 · N241NN · Emb ERJ170200LR · Tire
  > NUMBER 4 MAIN TIRE FLAT DURING THE LANDING ROLL OUT. BRK RH FAULT ADVISORY MSG OBSERVED. FOUND #4 MLG TIRE BLOWN OUT AND COMPLETELY FLAT. RAR #4 MLG TIRE AND PERFORMED BRAKE INSPECTION IAW W/C EA32-49-05-801. TREAD DID NOT SEPERATE FROM WHEEL. THERE IS NO EVID
- [SDR SIMA20250406002](https://openairdocs.org/sdr/SIMA20250406002.md): Tire · failed · Apr 6, 2025 · N241NN · Emb ERJ170200LR · Tire
  > BRK RH FAULT ADVISORY ON APPROACH TO LANDING. UPON EXITING THE RUNWAY IT BECAME CLEAR THE NUMBER 3 OR 4 TIRE HAD BECOME DEFLATED. AFTER TOW TO THE GATE AND VISUAL INSPECTION, IT IS CONFIRMED THE NUMBER 4 TIRE IS COMPLETELY FLAT. FOUND #4 MLG TIRE BLOWN OUT AND
- [SDR SIMA20241227001](https://openairdocs.org/sdr/SIMA20241227001.md): Bleed Valve · failed · Dec 27, 2024 · N241NN · Emb ERJ170200LR · Compressor Bleed Valve
  > BLEED FAIL IN FLIGHT. EMERGENCY DECLARED. DIVERT TO LIT DUE TO WEATHER. REMOVED AND REPLACED LH ENGINE NACELLE PRESSURE REGULATING SHUTOFF VALVE IAW AMM 36-11-03. LEAK CHECK GOOD IAW AMM 36-11-03-790-802A. NO FURTHER DEFECTS NOTED. MEL RESTORED.
- [SDR SIMA20231022001](https://openairdocs.org/sdr/SIMA20231022001.md): Bleed Valve · failed · Oct 22, 2023 · N241NN · Emb ERJ170200LR · Compressor Bleed Valve
  > BLD #1 FAIL IN FLT.AT FL220 WE DID QRH REST PROCEDURES. BLEED 1 FAIL MESSAGE WENT OFF FOR APROX. 5 MIN THEN CAME BACK ON. EMERGENCY DECLARED. CONT TO ORD-C/A-RAR ENGINE #1 NACELLE PRESSURE REGULATING SHUTOFF VALVES IAW EMBRAER 175 AMM 36-11-03 OPS CHECK GOOD
- [SDR SIMA20220805007](https://openairdocs.org/sdr/SIMA20220805007.md): Frame · none · Aug 5, 2022 · N241NN · Emb EMB110* · Fuselage Main, Structure
  > FRAME 13 HAS ELECTRICAL SHORT DAMAGE BETWEEN STRINGER 22L AND 23L IN THE INTERIOR SIDE OF THE AIRCRAFT. -C/A-PERFORMED PERMANENT REPAIR TO FRAME 13 ELECTRICAL SHORT DAMAGE BETWEEN STRINGER 22L AND 23L IAW ERS-EJ-53MR-4615.
- [SDR SIMA20220804011](https://openairdocs.org/sdr/SIMA20220804011.md): Beam · corroded · Aug 4, 2022 · N241NN · Emb ERJ170200LR · Fuselage Main, Structure
  > SSI 53-23-005 RH FLOOR BEAM IS CORRODED AROUND 2 FASTENER HOLES BTW FR88-89. (LEVEL 2 CORROSION)-C/A-INSTALLED SERVICABLE RH FLOOR BEAM FROM 86-89 IAW EMB 175 SRM51-40-08, 51-41-01, 51-- 43-03, 51-21-01
- [SDR SIMA20220803011](https://openairdocs.org/sdr/SIMA20220803011.md): None · corroded · Aug 3, 2022 · N241NN · Emb EMB110* · Fuselage Main, Structure
  > SSI 53-23-005 RH LWR SEAT TRACK IS CORRODED BTW FR83-84 (LEVEL 2 CORROSION) -C/A-REPAIRED LOWER SEAT TRACK CORROSION BTW FR 83-84 BY INSTALLING SPLICE DEVICE ON RH LOWER SEAT TRACK BTW FR 83-84 IAW EMB 175 SRM 53-00-10
- [SDR SIMA20220803009](https://openairdocs.org/sdr/SIMA20220803009.md): None · corroded · Aug 3, 2022 · N241NN · Emb EMB110* · Fuselage Main, Structure
  > SSI 53-23-005 CENTER SHEAR PANEL AT FR.87 CORRODED (LEVEL 2 CORROSION) -C/A-INSTALLED SERVICEABLE CENTER SHEAR PANEL AT FR 87 IAW EMB-175 SRM 51-40-08, SRM 51-21-01, SRM 51-42-01, SRM 51-43-03
- [SDR SIMA20220803008](https://openairdocs.org/sdr/SIMA20220803008.md): None · corroded · Aug 3, 2022 · N241NN · Emb EMB110* · Fuselage Main, Structure
  > SSI 53-23-005 RH FLOOR SEAT TRACK BETWEEN FR84-85 CORRODED (MAJOR REPAIR) (LEVEL 2 CORROSION) -C/A-INSTALLED REPAIR DOUBLER AND FILLER FOR RH FLOOR SEAT TRACK REPAIR BTW FR 84-85 IAW ERS EJ-53MR-4599
- [SDR SIMA20220803007](https://openairdocs.org/sdr/SIMA20220803007.md): Seat Track · corroded · Aug 3, 2022 · N241NN · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > SSI 53-22-012 LH MIDDLE SEAT TRACK IS CORRODED BTW FR33-34. (LEVEL 2 CORROSION) (MAJOR REPAIR) -C/A-INSTALLED REPAIR ON LH MIDDLE SEAT TRACK BTW FR30-34 IAW EMB 175 SRM 53-00-10 REPAIR 01P ETN-EJ-53-010.
- [SDR SIMA20220803006](https://openairdocs.org/sdr/SIMA20220803006.md): Floor Support · corroded · Aug 3, 2022 · N241NN · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > SSI 53-10-027 RH FLOOR SILL AT FR4 CORRODED. (LEVEL 2 CORROSION) -C/A-REMOVED AND REPLACED WITH SERVICEABLE RH FLOOR SILL AT FR14 IAW EMB-175 SRM 51-40-08
- [SDR SIMA2022081503002](https://openairdocs.org/sdr/SIMA2022081503002.md): Seat Track · corroded · Aug 3, 2022 · N241NN · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > SSI 53-10-027 LH CTR SEAT TRACK BETWEEN FR19-20 CORRODED (LEVEL 2 CORROSION)-C/A-BLENDED OUT DAMAGED SECTION OF LH CENTER SEAT TRACK BTW FR 19-20 IAW ERS# ERS-EJ-5300-4600R1.
- [SDR SIMA20220803003](https://openairdocs.org/sdr/SIMA20220803003.md): Track · corroded · Aug 3, 2022 · N241NN · Emb ERJ170200LR · Fuselage Main, Structure
  > SSI 53-10-027 RH CTR SEAT TRACK BETWEEN FR17-18 CORRODED. (LEVEL 2 CORROSION)-C/A-BLENDED OUT DAMAGED AREA OF RH CENTER SEAT TRACK BTW FR 17-18 IAW ERS# ERS-EJ-5300-4603R1.
- [SDR SIMA20220803004](https://openairdocs.org/sdr/SIMA20220803004.md): Panel · corroded · Aug 3, 2022 · N241NN · Emb ERJ170200LR · Fuselage Main, Structure
  > SSI 53-23-005 RH SHEAR PANEL AT FR.87 CORRODED. (LEVEL 2 CORROSION)-C/A-COMPLETED REMOVAL AND INSTALLATION OF SERVICEABLE RH SHEAR PANEL AT FR 87 IAW EMB 175 SRM 51-40-00
- [SDR SIMA20220803001](https://openairdocs.org/sdr/SIMA20220803001.md): Floorbeam · corroded · Aug 3, 2022 · N241NN · Emb ERJ170200LR · Fuselage Main, Structure
  > SSI 53-23-005 FLOOR SPLICE AT FR 90 ON RH BEAM CORRODED-C/A-REMOVED AND REPLACE FLOOR SPLICE AT FR 90 ON RH BEAM IAW EMB-175 SRM 51-40-08 (LEVEL 2 CORROSION)
- [SDR SIMA20220611003](https://openairdocs.org/sdr/SIMA20220611003.md): Spar · cracked · Jun 11, 2022 · N241NN · Emb ERJ170200LR · Wing, Plate/Skin
  > LH WING TIP REQUIRES REPLACEMENT DUE TO SPAR CRACK-C/A-REMOVED LH WING TIP AND INSTALLED SERVICEABLE WING TIP IAW AMM 57-30-00-400-801
- [SDR SIMA20220611002](https://openairdocs.org/sdr/SIMA20220611002.md): Spar · cracked · Jun 11, 2022 · N241NN · Emb ERJ170200LR · Wing, Plate/Skin
  > RH WING TIP REQUIRES REPLACEMENT DUE TO SPAR CRACK.-C/A-INSTALLED RH WING TIP IAW AMM 57-30-00.
- [SDR SIMA20220611004](https://openairdocs.org/sdr/SIMA20220611004.md): Spar · cracked · Jun 11, 2022 · N241NN · Emb ERJ170200LR · Wing Main, Frame Structure
  > RH WING SPAR 1 IS CRACKED AT WING TIP CONNECTION AREA.-C/A-RAR RH WING SPAR 1 ASSEMBLY AT WING TIP CONNECTION AREA IAW SRM 51-40-08. SEE NRWC 241-MQT-02843 FOR PAINT TOUCH UP OF REPAIR AREA.
- [SDR SIMA20220304002](https://openairdocs.org/sdr/SIMA20220304002.md): None · none · Mar 4, 2022 · N241NN · Emb ERJ170200LR · Emergency Lighting
  > PHOTOLUMINESCENT EMERGENCYY LIGHT STRIPS IN FRONT OF WARDROBE WORN-C/A-FOUND 3 RH FWD PHOTOLUMINESCENT EMERGENCY LIGHT STRIPS DULL AND WORN. RAR PHOTOLUMINESCENT STRIPS IAW AMM 33-50-21.
- [SDR SIMA202005265001](https://openairdocs.org/sdr/SIMA202005265001.md): Warning System · false activation · May 25, 2020 · N241NN · Emb ERJ170200LR · Brake
  > RT BRK FAULT EICAS MESSAGE ANNUNCITED WHILE AT CRUSE ALT OF FL 360. C/A-CMC FAULT CODE 32412003BCM RT INBD WHEEL SPEEED FAULT PERFORMED FIM TASK 32-41-00 FOUND TO BE TRANSIT CONDITION SAME BCM2 AIRCRAFT OK FOR SERVICE NO FAULTS PRESENT.
- [SDR SIMA2020022019001](https://openairdocs.org/sdr/SIMA2020022019001.md): Windshield · cracked · Feb 19, 2020 · N241NN · Emb ERJ170200LR · Flight Compartment Windows
  > CRACKED WINDSHIELD IN FLIGHT "TRANSFERRED TO NRWC 041-DFW-01448"-C/A-TRANSFERRED FROM NRWC 041-DFW-01448. REMOVED AND REPLACED RH COCKPIT WINDSHIELD IAW EMB 175 AMM 56-11-00. OPERATIONAL CHECK AND PRESSURIZATION CHECK GOOD.
- [SDR SIMA20190711006](https://openairdocs.org/sdr/SIMA20190711006.md): Coupling · loose · Jul 11, 2019 · N241NN · Emb ERJ170200LR · Pneumatic Distribution System
  > SOON AFTER TAKE-OFF EICAS BLEED (1) LEAK, RAN CHECK LIST / ANNUNCIATION WENT OUT. "TRANSFERRED TO NRWC 041-DFW-01059". C/A- TIGHTENED LT ENGINE HIGH STAGE BLEED VALVE UPPER COUPLING TO PROPER TORQUE VALUE IAW AMM 36-11-01. PERFORMED HIGH POWER RUN IAW AMM 71-0
- [SDR SIMA20190626005](https://openairdocs.org/sdr/SIMA20190626005.md): Light · inoperative · Jun 26, 2019 · N241NN · Emb ERJ170200LR · Emergency Lighting
  > PCR: RT FWD 2 EMERGENCY LIGHT STRIPS PARTIALLY INOP. C/A-COMPLETE:REMOVED AND REPLACED RH FWD 2 EMERGENCY PHOTOLUMINESCENT LIGHT STRIPS IAW AMM 33-50-21. OPC GOOD.
- [SDR SIMA201809287001](https://openairdocs.org/sdr/SIMA201809287001.md): Lens · cracked · Sep 27, 2018 · N241NN · Emb ERJ170200LR · Emergency Lighting
  > EMERGENCY EXIT LIGHT COVER ABOVE FWD SERVICE DOOR IS CRACKED.-C/A-FOUND FWD SERVICE DOOR EMERGENCY EXIT LIGHT COVER CRACKED. RAR NEW EMERGENCY EXIT LIGHT COVER. IAW AMM 33-50-19.
- [SDR SIMA20170625004](https://openairdocs.org/sdr/SIMA20170625004.md): Mechanism · lack of lube · Jun 25, 2017 · N241NN · Emb ERJ170200LR · Passenger/Crew Doors
  > L2 SERVICE DIFFICULT TO OPEN & CLOSE. LUBRICATED THE L2 DOOR OPENING & CLOSING MECHANISM. OPS CHECKED GOOD IAW AMM 52-11-00.
- [SDR SIMA20170625003](https://openairdocs.org/sdr/SIMA20170625003.md): Mechanism · lack of lube · Jun 25, 2017 · N241NN · Emb ERJ170200LR · Passenger/Crew Doors
  > MAIN CABIN PAX DOOR DIFFICULTY IN OPENING & CLOSING. LUBED MAIN DOOR OPENING & CLOSING MECHANISM. OPS CHECKED GOOD IAW AMM 52-11-00.
- [SDR SIMA20161202001](https://openairdocs.org/sdr/SIMA20161202001.md): Gasket · leaking · Dec 2, 2016 · N241NN · Emb ERJ170200LR · Pneumatic Indicating System
  > CLIMBING THRU FL 190 A BLEED LEAK 2 ILLUMINATED ON EICAS. RAN CHECKLIST, RETURNED TO DEPARTURE. REMOVED AND REPLACED THE RIGHT ENGINE PRECOOLER FWD AND AFT INTERFACE GASKETS IAW AMM 36-11-08. OPS CHECKED GOOD IAW AMM 36-21-00-810-802-A.
- [SDR SIMA20161026006](https://openairdocs.org/sdr/SIMA20161026006.md): Shutoff Valve · locked · Oct 26, 2016 · N241NN · Emb ERJ170200LR · Pneumatic Indicating System
  > AFTER TAKEOFF, BLEED 1 FAIL AND BLEED 1 OVERPRESSURE MESSAGE DISPLAYED ON EICAS. QR4 PROCEDURES COMPLIED WITH. FOUND NACELLE PRSOV TO BE LOCKED IN THE OPEN POSITION, RECONFIGURED VALVE TO ITS RIGHT POSITION AND PERFORMED OPS CHECK OF THE AIR BLEED SYSTEM IAW

## 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 = 'N241NN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N241NN/reports

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