# Service difficulty reports: N572RP, cancelled Oct 18, 2019 A list on [N572RP, cancelled Oct 18, 2019](https://openairdocs.org/deregistered/N572RP-2019-10-18.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR CHQA20140501136](https://openairdocs.org/sdr/CHQA20140501136.md): Fitting · corroded · May 1, 2014 · N572RP · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION, THE SHEAR CLIP AT FRAME 65 WAS FOUND TO BE CRACKED AT STRINGERS 18L & 19L. THE SHEAR CLIP WAS REPLACED IAW SRM 51-40-02. - [SDR CHQA20140427142](https://openairdocs.org/sdr/CHQA20140427142.md): Structure · corroded · Apr 27, 2014 · N572RP · Emb EMB145LR · Passenger/Crew Doors > DURING INSPECTION, CORROSION WAS FOUND ON THE LOWER FWD PAX DOOR STRUCTURE. THE LOWER FWD PAX DOOR STRUCTURE WAS REPLACED IAW SRM 51-40-02. - [SDR CHQA20140425132](https://openairdocs.org/sdr/CHQA20140425132.md): Fitting · cracked · Apr 25, 2014 · N572RP · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION, THE SHEAR CLIP AT FRAME 81 & STRINGER 10L WAS FOUND TO BE CRACKED. THE SHEAR CLIP WAS REPLACED IAW SRM 51-40-02. - [SDR CHQA20140425131](https://openairdocs.org/sdr/CHQA20140425131.md): Fitting · cracked · Apr 25, 2014 · N572RP · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION, THE SHEAR CLIP AT FRAME 81 & STRINGER 10R WAS FOUND TO BE CRACKED. THE SHEAR CLIP WAS REPLACED IAW SRM 51-40-02. - [SDR CHQA20140423144](https://openairdocs.org/sdr/CHQA20140423144.md): Structure · corroded · Apr 23, 2014 · N572RP · Emb EMB145LR · Passenger/Crew Doors > DURING INSPECTION, CORROSION WAS FOUND ON THE INNER STRUCTURE OF THE LOWER AFT CORNER OF THE MAIN ENTRY DOOR. THE LOWER AFT CORNER STRUCTURE OF THE LOWER MAIN ENTRY DOOR WAS REPLACED IAW SRM 51-40-02. - [SDR CHQA20140423143](https://openairdocs.org/sdr/CHQA20140423143.md): Reinforcement · corroded · Apr 23, 2014 · N572RP · Emb EMB145LR · Passenger/Crew Doors > DURING INSPECTION, CORROSION WAS FOUND ON THE DOOR STOP REINFORCEMENT INSIDE OF THE FWD FRAME OF THE MAIN ENTRY DOOR. THE DOOR STOP REINFORCEMENT WAS REPLACED IAW SRM 51-40-02. - [SDR CHQA20140423141](https://openairdocs.org/sdr/CHQA20140423141.md): Structure · corroded · Apr 23, 2014 · N572RP · Emb EMB145LR · Passenger/Crew Doors > DURING INSPECTION, CORROSION WAS FOUND & A CRACK WAS FOUND ON THE STRUCTURE UNDER THE MIDDLE FWD STAIR SUPPORT ON THE MAIN ENTRY DOOR. THE STRUCTURE UNDER THE MIDDLE FWD STAIR SUPPORT WAS REPLACED IAW SRM 51-40-02. - [SDR CHQA20140423140](https://openairdocs.org/sdr/CHQA20140423140.md): Structure · corroded · Apr 23, 2014 · N572RP · Emb EMB145LR · Passenger/Crew Doors > DURING INSPECTION, CORROSION WAS FOUND ON THE INNER STRUCTURE OF THE LOWER FWD AREA OF THE MAIN ENTRY DOOR. THE INNER STRUCTURE OF THE LOWER FWD AREA OF THE MAIN ENTRY DOOR WAS REPLACED IAW SRM 51-40-02. - [SDR CHQA20140423139](https://openairdocs.org/sdr/CHQA20140423139.md): Reinforcement · corroded · Apr 23, 2014 · N572RP · Emb EMB145LR · Passenger/Crew Doors > DURING INSPECTION, CORROSION WAS FOUND AROUND THE THE REINFORCEMENT FOR THE BOTTOM DOOR STOP INSIDE THE AFT STRUCTURE OF THE MAIN ENTRY DOOR. THE DOOR STOP WAS REPLACED IAW SRM 51-40-02. - [SDR CHQA20140423138](https://openairdocs.org/sdr/CHQA20140423138.md): Door Frame · corroded · Apr 23, 2014 · N572RP · Emb EMB145LR · Fuselage Main, Structure > DURING INSPECTION, CORROSION WAS FOUND ON FRAME 65 AT THE CARGO DOOR FRAME JUST BELOW THE DOOR BUMPER PLATE. THE FRAME WAS REPAIRED IAW ETD 2014-145-034902. - [SDR CHQA20140423137](https://openairdocs.org/sdr/CHQA20140423137.md): Fitting · damaged · Apr 23, 2014 · N572RP · Emb EMB145LR · Aileron Control System > DURING INSPECTION, THE LT AILERON ACTUATOR ATTACH LUG OTBD HAT BUSHING WAS FOUND TO BE MIGRATING AWAY FROM THE LUG. THE LT AILERON PCA FITTING WAS REPLACED IAW SRM 51-20-01 & SRM 51-40-02. - [SDR CHQA20140423133](https://openairdocs.org/sdr/CHQA20140423133.md): Door · chafed · Apr 23, 2014 · N572RP · Emb EMB145LR · Passenger/Crew Doors > DURING INSPECTION, A CHAFE WAS FOUND ON THE INNER AFT FACE OF THE MAIN ENTRY DOOR FOLDING FLAP. THE CHAFE WAS REPAIRED IAW ETD 2014-145-034319. - [SDR CHQA20140422135](https://openairdocs.org/sdr/CHQA20140422135.md): Support · corroded · Apr 22, 2014 · N572RP · Emb EMB145LR · Fuselage, Seat/Cargo Attach Fittings > DURING INSPECTION, THE LT SIDEWALL SEAT TRACK SUPPORT WAS FOUND TO BE CORRODED AT FRAME 45. THE SEAT TRACK SUPPORT WAS REPLACED IAW SRM 51-40-02. - [SDR CHQA20140422134](https://openairdocs.org/sdr/CHQA20140422134.md): Doubler · corroded · Apr 22, 2014 · N572RP · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION, A PREVIOUS REPAIR DOUBLER ON THE LT FWD OMEGA BEAM FWD CAP AT FRAME 20 WAS FOUND TO BE CORRODED. THE REPAIR DOUBLER WAS REPLACED IAW SRM 51-40-02. - [SDR CHQA20131206442](https://openairdocs.org/sdr/CHQA20131206442.md): Smoke Detector · false activation · Dec 6, 2013 · N572RP · Emb EMB145LR · Smoke Detection > CREW REPORTED THAT THEY RECEIVED A LAVATORY SMOKE MESSAGE ON CLIMB OUT. THE CREW FURTHER REPORTED NO VISIBLE SMOKE. THE SMELL OF DE-ICING FLUID WAS REPORTED AS PRESENT IN THE AIRCRAFT. THE CREW RETURNED TO FIELD & LANDED WITHOUT INCIDENT. MX RAN THE ENGS W - [SDR CHQA20130831331](https://openairdocs.org/sdr/CHQA20130831331.md): Light · inoperative · Aug 31, 2013 · N572RP · Emb EMB145LR · Emergency Lighting > DURING INSPECTION, THE RT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MX REPLACED THE RT OVERWING LIGHT ASSY. OPS CHECKED GOOD WITH NO FURTHER DEFECTS NOTED. - [SDR CHQA20130708261](https://openairdocs.org/sdr/CHQA20130708261.md): Control Valve · faulty · Jul 8, 2013 · N572RP · Emb EMB145LR · Landing Gear Brake System > CREW REPORTED THAT ON GEAR EXTENSION, RECEIVED A BRAKE DEGRADED MESSAGE ON THE EICAS DISPLAY. DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MX REPLACED THE RT BRAKE CONTROL VALVE. OPS CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED. - [SDR CHQA20130405105](https://openairdocs.org/sdr/CHQA20130405105.md): Switch · dirty · Apr 5, 2013 · N572RP · Emb EMB145LR · Door Warning System > CREW REPORTED THAT THEY RECEIVED A BAGGAGE DOOR INDICATION IN FLIGHT. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE DEFERRED THE BAGGAGE DOOR INDICATION. THE DEFERRAL WAS CLEARED ON 4/12/2013 WHEN THE DOOR INDICATION MICROSWITCHES WERE - [SDR CHQA20130117020](https://openairdocs.org/sdr/CHQA20130117020.md): Tire · separated · Jan 17, 2013 · N572RP · Emb EMB145LR · Tire > CREW REPORTED DURING TAKEOFF THE RIGHT INBOARD MAIN LANDING GEAR TIRE SEPARATED. THE CREW DECLARED AN EMERGENCY. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE RIGHT INBOARD MAIN LANDING GEAR TIRE. A TIRE TREAD SEPARATION INSPECTION WAS ALS - [SDR CHQA20120727247](https://openairdocs.org/sdr/CHQA20120727247.md): Support Fitting · corroded · Jul 27, 2012 · N572RP · Emb EMB145LR · Passenger/Crew Doors > DURING INSPECTION, CORROSION WAS FOUND ON THE PASSENGER DOOR FORWARD AND AFT STEP SUPPORT FITTING AT THE STEP BUSHING AREAS. MAINTENANCE REPLACED THE FORWARD AND AFT SUPPORT FITTINGS. - [SDR CHQA20120727246](https://openairdocs.org/sdr/CHQA20120727246.md): Support Fitting · corroded · Jul 27, 2012 · N572RP · Emb EMB145LR · Passenger/Crew Doors > DURING INSPECTION, CORROSION WAS FOUND ON THE PASSENGER DOOR FORWARD AND AFT STEP SUPPORT FITTING AT THE STEP BUSHING AREAS. MAINTENANCE REPLACED THE FORWARD AND AFT SUPPORT FITTINGS. - [SDR CHQA20120726242](https://openairdocs.org/sdr/CHQA20120726242.md): Shear Plate · cracked · Jul 26, 2012 · N572RP · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION, A CRACK WAS FOUND IN THE SHEAR FOOT FRAME 68 BETWEEN STRINGER 6L-7L. MAINTENANCE REPLACED THE SHEAR CLIP AT FRAME 68 BETWEEN STRINGERS 6L AND 7L. - [SDR CHQA20120726241](https://openairdocs.org/sdr/CHQA20120726241.md): Shear Plate · cracked · Jul 26, 2012 · N572RP · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION A CRACK WAS FOUND IN SHEAR FOOT FRAME 61 BETWEEN STRINGER 6R-7R. MAINTENANCE REPLACED THE SHEAR FOOT AT FRAME 61. - [SDR CHQA20120725240](https://openairdocs.org/sdr/CHQA20120725240.md): Door Frame · cracked · Jul 25, 2012 · N572RP · Emb EMB145LR · Passenger/Crew Doors > DURING INSPECTION, A CRACK WAS FOUND IN THE MAIN PASSENGER LOWER DOOR FRAME AT THE AFT STOP, SECOND FROM THE BOTTOM, WITH THE DOOR IN THE OPEN POSITION. MAINTENANCE REPAIRED THE DAMAGED AREA IN ACCORDANCE WITH ETD 2012-145-010458. - [SDR CHQA201100389](https://openairdocs.org/sdr/CHQA201100389.md): Wire Harness · defective · Sep 27, 2011 · N572RP · Emb EMB145LR · Landing Gear System Wiring > CREW REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. THE CREW FOLLOWED ALL CHECKLISTS AND RETURNED TO KDCA. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS FOUND TO SAFE FOR A FERRY FLIGHT TO KSDF WITH THE LANDING GEAR DOWN AND THE GE - [SDR CHQA201100367](https://openairdocs.org/sdr/CHQA201100367.md): Proximity Switch · dirty · Sep 10, 2011 · N572RP · Emb EMB145LR · Landing Gear Position and Warning > CREW REPORTED, COULD NOT LIFT THE LANDING GEAR LEVER AND THE LANDING GEAR WOULD NOT RETRACT. RETURNED TO KIAD AND LANDED WITHOUT INCIDENT. MAINTENANCE CLEANED AND LUBRICATED ALL PROXIMITY SWITCHES IN THE LANDING GEAR SYSTEM. OPERATIONAL CHECKS WERE GOOD WIT - [SDR CHQA201100344](https://openairdocs.org/sdr/CHQA201100344.md): Skin · scratched · Aug 15, 2011 · N572RP · Emb EMB145LR · Fuselage Main, Plate/Skin > DURING INSPECTION, SEVERAL SCRATCHES WERE FOUND ON THE FUSELAGE UPPER SKIN UNDERNEATH ADF ANTENNA NUMBER 1 AND NUMBER 2. MAINTENANCE REPAIRED THE SCRATCHES ON THE FUSELAGE UPPER SKIN UNDER THE NUMBER 1 AND NUMBER 2 ADF ANTENNA IN ACCORDANCE WITH ETD 2011-145- - [SDR CHQA201100347](https://openairdocs.org/sdr/CHQA201100347.md): Stop Fitting · damaged · Aug 11, 2011 · N572RP · Emb EMB145LR · Fuselage Main, Structure > DURING INSPECTION, THE PASSENGER DOOR STOP WAS FOUND TO BE DAMAGED. MAINTENANCE BLENDED THE PASSENGER DOOR STOPS IN ACCORDANCE WITH SRM 53-21-15. A HIGH FREQUENCY EDDY CURRENT INSPECTION WAS PERFORMED IN ACCORDANCE WITH NDI MANUAL, INTRODUCTION PAGE 17E, WIT - [SDR CHQA201100346](https://openairdocs.org/sdr/CHQA201100346.md): Bonding Strap · corroded · Aug 10, 2011 · N572RP · Emb EMB145LR · Ailerons > DURING INSPECTION, CORROSION WAS FOUND ON THE LEFT AND RIGHT AILERON UPPER SHROUD BONDING STRAP. MAINTENANCE REWORKED THE LEFT AND RIGHT AILERON UPPER SHROUD BONDING STRAP IN ACCORDANCE WITH CPM 51-14-02. - [SDR CHQA201100345](https://openairdocs.org/sdr/CHQA201100345.md): Skin · damaged · Aug 10, 2011 · N572RP · Emb EMB145LR · Rudder, Plate/Skin > DURING INSPECTION, THE SKIN WAS FOUND TO BE DAMAGED AND AN ANCHOR NUT MISSING ON RUDDER II, BETWEEN X27083 AND X27621 AS WELL AS BETWEEN ZV1932 AND ZV2277. MAINTENANCE REPAIRED THE SKIN (PN: 120-21755-001) AND ANCHOR NUT ON RUDDER II (PN: 120-20808-509) BETWE - [SDR CHQA201100343](https://openairdocs.org/sdr/CHQA201100343.md): Beam · corroded · Aug 10, 2011 · N572RP · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION, CORROSION WAS FOUND ON THE MIDDLE BEAM AT Y0.0. MAINTENANCE REPLACED THE MIDDLE BEAM AT Y0.0 IN ACCORDANCE WITH SRM 51-40-02. - [SDR CHQA201100342](https://openairdocs.org/sdr/CHQA201100342.md): Structure · corroded · Aug 10, 2011 · N572RP · Emb EMB145LR · Passenger/Crew Doors > DURING INSPECTION, CORROSION WAS FOUND ON THE PASSENGER DOOR LOWER STRUCTURE FORWARD AND AFT U-SHAPE. MAINTENANCE REPLACED THE FORWARD (PN:145-24131-009) AND AFT (PN:145-24131-011) U-SHAPE ON THE PASSENGER DOOR LOWER STRUCTURE IN ACCORDANCE WITH SRM 51-40-02. - [SDR CHQA201100340](https://openairdocs.org/sdr/CHQA201100340.md): Beam · corroded · Aug 10, 2011 · N572RP · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION, AN EXISTING REPAIR ON THE LEFT BEAM Y479.0 AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REPAIRED THE LEFT BEAM, Y479.0 AT FRAME 20 IN ACCORDANCE WITH SRM 53-00-10. - [SDR CHQA201100314](https://openairdocs.org/sdr/CHQA201100314.md): Frame · corroded · Aug 10, 2011 · N572RP · Emb EMB145LR · Fuselage Main, Frame > DURING INSPECTION, CORROSION WAS FOUND ON THE LEFT CHANNEL FRAME AT FRAME 65 BETWEEN STRINGERS 15L AND 16L. MAINTENANCE REPAIRED THE FORWARD FRAME OF THE CARGO DOOR CUT-OUT LOWER PORTION IN ACCORDANCE WITH ETD 2011-145-103278. THE FINAL CORRECTIVE ACTION IS - [SDR CHQA201100313](https://openairdocs.org/sdr/CHQA201100313.md): Shear Plate · corroded · Aug 10, 2011 · N572RP · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION, CORROSION WAS FOUND ON THE AFT AND FORWARD L-SHAPE SHEAR CLIP. MAINTENANCE REPAIRED THE FORWARD AND AFT L-SHAPE SHEAR CLIPS IN ACCORDANCE WITH ETD2011-145-103275 REVISION A. A HIGH FREQUENCY EDDY CURRENT INSPECTION WAS CARRIED OUT ON THE C - [SDR CHQA201100348](https://openairdocs.org/sdr/CHQA201100348.md): Skin · dented · Aug 9, 2011 · N572RP · Emb EMB145LR · Fuselage Main, Plate/Skin > DURING C-CHECK, A DENT, FORWARD OF THE SERVICE DOOR, ON THE CENTER FUSELAGE I, BETWEEN STRINGERS 12R AND 13R, WAS REPAIRED. THE DENT WAS PREVIOUSLY DEFERRED (DMI 67032/1). THE FINAL REPAIR OF THE DENT, FORWARD OF THE SERVICE DOOR, ON THE CENTER FUSELAGE I, B - [SDR CHQA201100026](https://openairdocs.org/sdr/CHQA201100026.md): Unknown · contaminated · Jan 26, 2011 · N572RP · Emb EMB145LR · Air Distribution System > PRIOR TO TAKEOFF THE AIRCRAFT WAS DE-ICED, AND AT APPROXIMATELY 500FT ON TAKEOFF, THE FLIGHT ATTENDANT REPORTED HAZE IN THE CABIN THAT SMELLED LIKE GLYCOL. THERE WERE NO WARNING MESSAGES ON EICAS, AND THE HAZE DISSIPATED QUICKLY. IT WAS DECIDED TO CONTINUE T - [SDR CHQA200900202](https://openairdocs.org/sdr/CHQA200900202.md): Battery Pack · discharged · Sep 8, 2009 · N572RP · Emb EMB145LR · Emergency Lighting > DURING INSPECTION WHILE TESTING EMERGENCY LIGHT SYSTEM THE OVERWING EMERGENCY LIGHTS WERE INOP WHEN TESTED. MAINTENANCE REPLACED THE NR 4 EMERGENCY LIGHT BATTERY AND THE EMERGENCY LIGHTS OPERATED NORMALLY. - [SDR CHQA200900061](https://openairdocs.org/sdr/CHQA200900061.md): Strut · underserviced · Feb 20, 2009 · N572RP · Emb EMB145LR · Nose/Tail Landing Gear Strut/Axle > UPON GEAR RETRACTION THE CREW RECEIVED A L/G AIR/GND FAIL MESSAGE ON THE EICAS. FOLLOWED SHORTLY BY E1-2 REVERSE DISAGREE MESSAGE. THE CREW RETURNED TO THE FIELD AND BOTH MESSAGES CLEARED ON GEAR EXTENSION. A NORMAL LANDING WAS MADE. UPON INSPECTION BY MAI - [SDR CHQA200700090](https://openairdocs.org/sdr/CHQA200700090.md): Warning Message · false activation · Dec 5, 2007 · N572RP · Emb EMB145LR · Central Warning > IND TO CVG - DURING CLIMB-OUT OF IND IN ICING CONDITIONS THE CREW RECEIVED A BLEED 1 LEAK EICAS MESSAGE WITH LEAK ILLUMINATED ON THE ENGINE BLEED VALVE SELECTOR SWITCH. THE AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED ENGINE - [SDR CHQA200700010](https://openairdocs.org/sdr/CHQA200700010.md): O-Ring · broken · Apr 7, 2007 · N572RP · Emb EMB145LR · Engine Bleed Air System > FLIGHT 6218 - CVG-CMH - ON DESCENT INTO CMH, RECEIVED NR 2 ENGINE BLEED LEAK. SHUT OFF ENGINE PER QRH. INTERMITTENTLY IN AND OUT OF ICING CONDITIONS, SHUTTING OFF THE BLEED CAUSED THE WING ANTI-ICE TO FAIL. DECLARED AN EMERGENCY. MAINTENANCE FOUND LEAK AT - [SDR CHQA200600005](https://openairdocs.org/sdr/CHQA200600005.md): Bulb · missing · Jan 6, 2006 · N572RP · Emb EMB145LR · Emergency Lighting > FLOOR PROXIMITY LIGHT STRIP MISSING. INSTALLED FLOOR PROXIMITY LIGHT STRIP IAW EMB 145 MM 33-50-12. - [SDR CHQA200500049](https://openairdocs.org/sdr/CHQA200500049.md): Light · inoperative · Mar 9, 2005 · N572RP · Emb EMB145LR · Emergency Lighting > AFT EMERGENCY FLOOR PROXIMITY LIGHT STRIP IS INOP. REMOVED AND REPLACED FLOOR PROXIMITY LIGHT STRIP IAW EMB 145 AMM 33-50-12-4. OPS CHECK 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 = 'N572RP' AND deregistration_id = 'N572RP-2019-10-18' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N572RP-2019-10-18/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, except the copies of manufacturers’ service documents, which belong to their rights holders.