# Service difficulty reports: N209LF A list on [N209LF](https://openairdocs.org/aircraft/N209LF.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR 2A6D20220504004](https://openairdocs.org/sdr/2A6D20220504004.md): Bulkhead · damaged · May 4, 2022 · N209LF · Urocop EC130B4 · Fuselage Structure (General) > SHORT ED AND SHORT PD HOLES WERE DISCOVERED ON THE 7 DEGREE BULKHEAD ADJACENT TO THE RECESSED MEDICAL WALL INSTALLATION. - [SDR 2A6D20220503003](https://openairdocs.org/sdr/2A6D20220503003.md): Xmsn Deck · chafed · May 3, 2022 · N209LF · Urocop EC130B4 · Fuselage Main, Frame > R/H SIDE FWD. TRANSMISSION DECK WEB (P/N: 350A21-4418) IS DAMAGED IN THE FORM OF A CHAFING. THE DAMAGE IN THE FWD IS APPROXIMATELY 0.3” IN LENGTH, 0.3” IN WIDTH AND 0.019” IN DEPTH AND DAMAGE AT AFT IS APPROXIMATELY 0.3” IN LENGTH, 0.25” IN WIDTH AND 0.010” IN - [SDR 2A6D20220429002](https://openairdocs.org/sdr/2A6D20220429002.md): Xmsn Deck · chafed · Apr 29, 2022 · N209LF · Urocop EC130B4 · Fuselage Structure (General) > CHAFING DAMAGE WAS DISCOVERED ON THE RH SIDE OF THE TRANSMISSION DECK. THE DEEPEST DEPTH IS 0.015" WITH A LENGTH OF 2.1" AND WIDTH OF 0.1. - [SDR 2A6D20220418001](https://openairdocs.org/sdr/2A6D20220418001.md): Frame · chafed · Apr 13, 2022 · N209LF · Urocop EC130B4 · Fuselage Main, Frame > DAMAGE TO BOTH X1790 FRAME (P/N: 350A214099) AND SUPPORT (P/N: 350A214107) IN THE FORM OF A DENT AND CHAFE NEAR A LOWER FAIRING MOUNTING POINT. THE DAMAGE AREA WAS MEASURED TO BE 0.2” IN LENGTH, 0.2” IN WIDTH AND 0.03” IN DEPTH. - [SDR 2A6R2019012251001](https://openairdocs.org/sdr/2A6R2019012251001.md): Reinforcement · cracked · Jan 22, 2019 · N209LF · Urocop EC130B4 · Fuselage Miscellaneous Structure > CRACK DAMAGE WAS NOTED ON THE RIGHT SIDE OF THE CABIN FLOOR NEAR THE DOOR POST WITHIN THE AREA OF THE DOOR STRUT FITTING. - [SDR 2A6R2018120551003](https://openairdocs.org/sdr/2A6R2018120551003.md): Structure · corroded · Dec 5, 2018 · N209LF · Urocop EC130B4 · Fuselage Main, Structure > CORROSION AND DELAMINATION OF THE ALUMINUM GROUND PLANE OF THE CABIN ROOF (CANOPY)IN SEVERAL SPOTS - [SDR 2A6R201812025102](https://openairdocs.org/sdr/2A6R201812025102.md): Door · cracked · Dec 5, 2018 · N209LF · Urocop EC130B4 · Passenger/Crew Doors > HINGED RIGHT HAND CABIN DOOR HAS A 9 INCH VERTICAL CRACK IN THE DOOR. - [SDR 2A6R201812055101](https://openairdocs.org/sdr/2A6R201812055101.md): Frame · cracked · Dec 5, 2018 · N209LF · Urocop EC130B4 · Rotorcraft Tail Boom > TAIL BOOM 3035 RING FRAME CRACKED AT 11:00 POSITION AT SKIN LAP. - [SDR QMLA2018100818109](https://openairdocs.org/sdr/QMLA2018100818109.md): Blower · odor · Oct 4, 2018 · N209LF · Urocop EC130B4 · Cabin Cooling System > WHILE ON APPROACH TO HOSPITAL LANDING PAD, THE GENERATOR DISENGAGED. IT WAS RESET, AND THE SUBSEQUENT APPROACH AND LANDING WERE COMPLETED NORMALLY. THE CREW REPORTED AN ELECTRICAL ODOR AFTER LANDING. UPON INSPECTION, NO PROBLEMS WERE FOUND WITH ELECTRICAL SYS - [SDR QMLA2016022316008](https://openairdocs.org/sdr/QMLA2016022316008.md): Unknown · odor · Feb 23, 2016 · N209LF · Urocop EC130B4 · Air Distribution System > SMELL OF AN UNIDENTIFIED BURNING ODOR IN COCKPIT. - [SDR QMLA2014102914128](https://openairdocs.org/sdr/QMLA2014102914128.md): Unknown · smoke · Oct 29, 2014 · N209LF · Urocop EC130B4 · Air Distribution System > DURING CRUISE FLIGHT A CREW MEMBER REPORTED SEEING SMOKE IN THE CABIN FWD OF THE STRETCHER WITH A STRANGE SMELL IN THE CABIN. THE PILOT DID NOT WITNESS THIS SMOKE, BUT RETURNED TO BASE FOLLOWING A DISCUSSION WITH THE MEDICAL CREW. ONCE ON THE GND, THE PILOT - [SDR QMLA2014072914093](https://openairdocs.org/sdr/QMLA2014072914093.md): Connector · contaminated · Jul 29, 2014 · N209LF · Urocop EC130B4 · Engine Oil System Wiring > FLIGHT ABORTED DUE TO NOISE COMING FROM OIL COOLER FAN. DETERMINED WATER WAS PRESENT IN THE CONNECTOR. - [SDR QMLA2014051814057](https://openairdocs.org/sdr/QMLA2014051814057.md): Attach Fitting · cracked · May 18, 2014 · N209LF · Urocop EC130B4 · Rotorcraft Tail Boom > ON A POST FLIGHT INSPECTION, FOUND THE UPPER LT HORIZONTAL STABILIZER ATTACH FITTING CRACKED. REMOVED THE HORIZONTAL STABILIZER & FOUND THAT THE FITTING HAD COMPLETELY CRACKED INTO TWO SEPARATE PIECES. THE CRACK APPEARED TO PROPAGATE FROM THE TWO BOLTS THAT - [SDR QMLA2014041114035](https://openairdocs.org/sdr/QMLA2014041114035.md): Attach Fitting · cracked · Apr 11, 2014 · N209LF · Urocop EC130B4 · Fuselage Miscellaneous Structure > CRACK FOUND ON RT SIDE CANOPY FRAME ATTACHMENT WEB PANEL FWD ON BELLY OF ACFT DURING AN EC130 AAIP A0560 100HOUR, 12MONTH AIRFRAME INSPECTION - [SDR QMLA2013050213062](https://openairdocs.org/sdr/QMLA2013050213062.md): Audio Panel · failed · May 2, 2013 · N209LF · Urocop EC130B4 · Communications System > PILOT WAS GOING INTO A HOVER DETECTED SOMETHING BURNING, AT THE SAME TIME LOST ALL RADIO AND ICS COMMUNICATIONS. PILOT PUT THE ACFT BACK DOWN AND NOTICED HIS PILOT ICS CIRCUIT BREAKER POPPED. AFTER EXTENSIVE TROUBLESHOOTING, MX AOG ORDERED A 2 AMP CIRCUIT BRE - [SDR UNFR20120100003](https://openairdocs.org/sdr/UNFR20120100003.md): Attach Fitting · broken · Feb 17, 2012 · N209LF · Urocop EC130B4 · Rotorcraft Tail Boom > DURING AN INSPECTION, HORIZONTAL STAB WAS REQUIRED TO BE REMOVED. UPON REMOVAL, THE UPPER LT MOUNT FITTING WAS FOUND BROKEN COMPLETELY IN HALF. AN EDDY CURRENT INSPECTION OF THE AREA RESULTED IN THE DISCOVERY OF THE UPPER RT FITTING BEING CRACKED ALSO. ## 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 = 'N209LF' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N209LF/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.