# Service difficulty reports: N563RP, cancelled Jul 11, 2018

A list on [N563RP, cancelled Jul 11, 2018](https://openairdocs.org/deregistered/N563RP-2018-07-11.md).

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

- [SDR UHLA201512210838](https://openairdocs.org/sdr/UHLA201512210838.md): Arm · failed · Dec 21, 2015 · N563RP · Emb EMB145LR · Service Doors
  > THE MAIN ENTRY DOOR WAS UNABLE TO BE OPENED FROM THE EXTERIOR AND MAINTENANCE FOUND THE LT HINGE AT THE BASE OF THE DOOR INOPERATIVE. MAINTENANCE R & R THE RT MAIN DOOR ROTATING ARM IAW AMM 52-11-03 AFTER WHICH ALL OPERATIONAL CHECKS WERE GOOD. NO FURTHER DE
- [SDR UHLA201510230774](https://openairdocs.org/sdr/UHLA201510230774.md): Step · broken · Oct 23, 2015 · N563RP · Emb EMB145LR · Passenger/Crew Doors
  > THE MAIN ENTRY DOOR STEPS WERE FOUND TO BE BROKEN. MAINTENANCE ADJUSTED THE SPRINGS ON THE MAIN ENTRY DOOR STEPS IAW AMM 52-10-01 AND ALL OPS CHECKS WERE GOOD. NO FURTHER DEFECTS HAVE BEEN NOTED.
- [SDR UHLA201506120495](https://openairdocs.org/sdr/UHLA201506120495.md): Skin · dented · Jun 12, 2015 · N563RP · Emb EMB145LR · Cargo/Baggage Doors
  > DURING INSPECTION, THE BAGGAGE COMPARTMENT DOOR WAS FOUND TO BE DENTED. THE DENT WAS REPAIRED IAW SRM 52-30-01.
- [SDR UHLA201506050490](https://openairdocs.org/sdr/UHLA201506050490.md): Floor Support · corroded · Jun 5, 2015 · N563RP · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING INSPECTION, CORROSION WAS FOUND ON THE UPRIGHT AT FRAME 20 ON THE LT OMEGA BEAM. THE STANTION WAS R & R IAW SRM 51-40-02.
- [SDR UHLA201506040489](https://openairdocs.org/sdr/UHLA201506040489.md): Floor Support · corroded · Jun 4, 2015 · N563RP · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING INSPECTION, CORROSION WAS FOUND ON THE CENTER OMEGA BEAM AT FRAMES 20-23. THE OMEGA BEAM WAS R & R IAW SRM 51-40-02.
- [SDR UHLA201506010494](https://openairdocs.org/sdr/UHLA201506010494.md): Floor Support · corroded · Jun 1, 2015 · N563RP · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING INSPECTION, CORROSION WAS FOUND AT THE CAPTAIN'S OTBD FLOOR SILL AT FRAMES 09-12. THE CORROSION WAS REPAIRED IAW ETD 2015-145-053918A.
- [SDR UHLA201506010491](https://openairdocs.org/sdr/UHLA201506010491.md): Seat Track · corroded · Jun 1, 2015 · N563RP · Emb EMB145LR · Fuselage, Seat/Cargo Attach Fittings
  > DURING INSPECTION, CORROSION WAS FOUND ON THE CAPTAIN'S INBD SEAT TRACK FLOOR GUSSET AT FRAME 08-09. THE CORROSION WAS REPAIRED IAW ETD 2015-145-053918.
- [SDR UHLA201506010488](https://openairdocs.org/sdr/UHLA201506010488.md): Bushing · migrated · Jun 1, 2015 · N563RP · Emb EMB145LR · Wing, Attach Fittings
  > DURING INSPECTION, THE RT AILERON DAMPER ATTACH FITTING, OTBD HAT BUSHING WAS FOUND TO BE MIGRATED AND GOUGED. THE FITTING WAS R & R IAW SRM 51-40-02.
- [SDR UHLA201506010487](https://openairdocs.org/sdr/UHLA201506010487.md): Bushing · migrated · Jun 1, 2015 · N563RP · Emb EMB145LR · Wing, Attach Fittings
  > DURING INSPECTION, THE RT AILERON PCA ATTACH FITTING HAT BUSHINGS WERE FOUND TO BE MIGRATED AND GOUGED. THE FITTING WAS R & R IAW SRM 51-40-02.
- [SDR UHLA201506010486](https://openairdocs.org/sdr/UHLA201506010486.md): Bushing · migrated · Jun 1, 2015 · N563RP · Emb EMB145LR · Wing, Attach Fittings
  > DURING INSPECTION, THE LT AILERON DAMPER ATTACH FITTING, OTBD HAT BUSHING WAS FOUND TO HAVE MIGRATED. THE FITTING WAS R & R IAW SRM 51-21-06.
- [SDR UHLA201506010485](https://openairdocs.org/sdr/UHLA201506010485.md): Bushing · migrated · Jun 1, 2015 · N563RP · Emb EMB145LR · Wing, Attach Fittings
  > DURING INSPECTION, THE LT AILERON PCA ATTACH FITTING HAT BUSHINGS WERE FOUND TO HAVE MIGRATED OUT. THE FITTING WAS R & R IAW SRM 51-40-02.
- [SDR UHLA201505310492](https://openairdocs.org/sdr/UHLA201505310492.md): Stringer · cracked · May 31, 2015 · N563RP · Emb EMB145LR · Fuselage Main, Longeron/Stringer
  > DURING INSPECTION, THE STRINGER STIFFENER 3L WAS FOUND TO BE CRACKED BETWEEN FRAMES 18 AND 19. THE STRINGER STIFFENER WAS R & R IAW SRM 51-40-02.
- [SDR CHQA20141121331](https://openairdocs.org/sdr/CHQA20141121331.md): Switch · faulty · Nov 21, 2014 · N563RP · Emb EMB145LR · Gust Lock Damper System
  > THE CREW REPORTED THAT THE GUST LOCK LIGHT CAME ON IN CRUISE FLIGHT. THE CREW DECLARED AN EMER & LANDED WITHOUT INCIDENT AT ITS INTENDED DESTINATION. THE GUST LOCK SYS WAS DEFERRED. THE DEFERRAL WAS CLEARED ON 11/22/2014 WHEN MX REPLACED MICRO SWITCH S0658.
- [SDR CHQA20140508146](https://openairdocs.org/sdr/CHQA20140508146.md): Light · broken · May 8, 2014 · N563RP · Emb EMB145LR · Emergency Lighting
  > DURING INSPECTION, THE EMERGENCY FLOOR LIGHT STRIP AT ROW 10A WAS FOUND TO BE BROKEN. THE FLOOR STRIP WAS REPLACED & ALL OPERATIONAL CHECKS WERE GOOD.
- [SDR CHQA20131229470](https://openairdocs.org/sdr/CHQA20131229470.md): Battery · discharged · Dec 29, 2013 · N563RP · Emb EMB145LR · Emergency Lighting
  > DURING INSPECTION, THE FWD EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED THE NR 1 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.
- [SDR CHQA20130608211](https://openairdocs.org/sdr/CHQA20130608211.md): Frame · damaged · Jun 11, 2013 · N563RP · Emb EMB145LR · Fuselage Main, Frame
  > FRAME WAS CREASED. THE FRAME WAS REPLACED IAW SRM 51-40-02.
- [SDR CHQA20130608219](https://openairdocs.org/sdr/CHQA20130608219.md): Stringer · bent · Jun 8, 2013 · N563RP · Emb EMB145LR · Fuselage Main, Longeron/Stringer
  > DURING INSPECTION, A STRINGER 12L WAS FOUND TO BE BENT BETWEEN FRAMES 71 AND 72. THE STRINGER WAS REPLACED IAW ETD 2012-145-017997-A.
- [SDR CHQA20130608218](https://openairdocs.org/sdr/CHQA20130608218.md): Frame · damaged · Jun 8, 2013 · N563RP · Emb EMB145LR · Fuselage Main, Frame
  > DURING INSPECTION, A FINAL REPAIR WAS COMPLETED FOR A DEFERRED MX ITEM ON FRAME 62 AT STRINGER 13L WHICH WAS CREASED. THE FRAME WAS REPAIRED IAW ETD2012-145-017869-D AND SRM 53-00-04.
- [SDR CHQA20130608216](https://openairdocs.org/sdr/CHQA20130608216.md): Stringer · damaged · Jun 8, 2013 · N563RP · Emb EMB145LR · Fuselage Main, Longeron/Stringer
  > DURING INSPECTION, A FINAL REPAIR FOR STRINGER 13L DAMAGE BETWEEN FRAME 62 AND FRAME 62A WAS COMPLETED. THE STRINGER WAS REPLACED IAW ETD 2012-145-017997.
- [SDR CHQA20130607217](https://openairdocs.org/sdr/CHQA20130607217.md): Floor Support · cracked · Jun 7, 2013 · N563RP · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING INSPECTION, THE RT SIDE OMEGA BEAM AT FRAME 59 HAS A CRACK IN THE NUT PLATE HOLE. THE BEAM WAS REPAIRED IAW ETD 2013-145-011759.
- [SDR CHQA20130603210](https://openairdocs.org/sdr/CHQA20130603210.md): Door Frame · corroded · Jun 3, 2013 · N563RP · Emb EMB145LR · Fuselage Main, Structure
  > DURING INSPECTION, CORROSION WAS FOUND ON THE SERVICE DOOR LOWER FRAME AROUND THE NUT PLATE HOLES. THE FRAME WAS REPAIRED IAW ETD 2013-145-011762.
- [SDR CHQA20130602213](https://openairdocs.org/sdr/CHQA20130602213.md): Frame · corroded · Jun 2, 2013 · N563RP · Emb EMB145LR · Fuselage Main, Frame
  > DURING INSPECTION, CORROSION WAS FOUND ON THE REPAIR ANGLE AT FRAME 23. THE REPAIR DOUBLER WAS REPLACED IAW SRM 51-40-02.
- [SDR CHQA20130601214](https://openairdocs.org/sdr/CHQA20130601214.md): Frame · corroded · Jun 1, 2013 · N563RP · Emb EMB145LR · Fuselage Main, Frame
  > DURING INSPECTION, CORROSION WAS FOUND ON FRAME 65 AT THE LOWER DOOR PLATE. THE FRAME WAS REPAIRED IAW SRM 53-31-04 AND SRM 51-40-02.
- [SDR CHQA20130601212](https://openairdocs.org/sdr/CHQA20130601212.md): Frame · corroded · Jun 1, 2013 · N563RP · Emb EMB145LR · Fuselage Main, Frame
  > DURING INSPECTION, A GOUGE WAS FOUND ON FRAME 60 BETWEEN STRINGERS 4L AND 5L. THE FRAME WAS REPAIRED IAW SRM 53-00-04.
- [SDR CHQA20130531215](https://openairdocs.org/sdr/CHQA20130531215.md): Skin · damaged · May 31, 2013 · N563RP · Emb EMB145LR · Nacelle/Pylon, Plate/Skin
  > DURING INSPECTION, THE LEFT HAND ENGINE PYLON WAS FOUND TO HAVE DAMAGE AROUND THE DRILLED SCREW SHANK ON THE UPPER FORWARD SURFACE. THE DAMAGE WAS REPAIRED IAW SRM 54-50-01 AND ETD 2013-145-011772.
- [SDR CHQA20121205451](https://openairdocs.org/sdr/CHQA20121205451.md): Engine · leaking · Dec 5, 2012 · N563RP · Emb EMB145LR · Engine (Turbine/Turboprop)
  > CREW REPORTED THAT THEY RECEIVED A LAVATORY SMOKE INDICATION ON CLIMBOUT. THEY REPORTED NO VISIBLE SMOKE WAS PRESENT, HOWEVER AN ODOR WAS PRESENT IN THE CABIN. THE CREW DECLARED AN EMERGENCY AND RETURNED TO FIELD. THE AIRCRAFT LANDED WITHOUT INCIDENT AND TA
- [SDR CHQA201100496](https://openairdocs.org/sdr/CHQA201100496.md): Wire · damaged · Dec 22, 2011 · N563RP · Emb EMB145LR · Engine Oil System Wiring
  > CREW REPORTED THAT DURING CLIMB, AT 17,000 FEET, THEY RECEIVED A HIGH OIL PRESSURE INDICATION FOR THE NUMBER 2 ENGINE. AFTER LEVELING, THE CREW RAN THE QUICK REFERENCE HANDBOOK AND SET THE NUMBER 2 ENGINE TO IDLE THRUST. THE ENGINE OIL PRESSURE STOPPED INCRE
- [SDR CHQA201100489](https://openairdocs.org/sdr/CHQA201100489.md): Battery · discharged · Dec 15, 2011 · N563RP · Emb EMB145LR · Emergency Lighting
  > DURING INSPECTION, THE EMERGENCY LIGHT POWER SUPPLY IN POSITION 4 FAILED THE FUNCTIONAL CHECK. MAINTENANCE REPLACED THE NUMBER 4 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.
- [SDR CHQA201100265](https://openairdocs.org/sdr/CHQA201100265.md): Floor Support · cracked · Jul 4, 2011 · N563RP · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING INSPECTION, A CRACK WAS FOUND ON THE LEFT OMEGA BEAM BETWEEN FRAMES 23 AND 24 IN CENTER FUSE I. MAINTENANCE REPAIRED THE LEFT OMEGA BEAM BETWEEN FRAME 14 AND FRAME 25 IN ACCORDANCE WITH ETD2011-145-101741.
- [SDR CHQA201100262](https://openairdocs.org/sdr/CHQA201100262.md): Spar Cap · cracked · Jul 3, 2011 · N563RP · Emb EMB145LR · Wing Spar
  > DURING INSPECTION, A CRACK WAS FOUND ON THE RIGHT WING FRONT SPAR LOWER CAP FROM THE CAP EDGE THROUGH THE SCREW HOLE. THE AIRCRAFT IS CURRENTLY IN C-CHECK INSPECTION.
- [SDR CHQA201100042](https://openairdocs.org/sdr/CHQA201100042.md): Inverter · inoperative · Feb 23, 2011 · N563RP · Emb EMB145LR · Emergency Lighting
  > DURING INSPECTION, THE FORWARD OVERWING EXIT LOCATOR LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT INVERTER FOR THE FORWARD OVERWING EXIT LIGHT LOCATOR. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.
- [SDR CHQA201000007](https://openairdocs.org/sdr/CHQA201000007.md): Battery · discharged · Jan 13, 2010 · N563RP · Emb EMB145LR · Emergency Lighting
  > DURING INSPECTION THE LAST 4 EMERGENCY LIGHT STRIPS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NR 4 EMERGENCY LIGHT BATTERY IAW AMM 33-50-04 AND THE EMERGENCY LIGHTS OPERATED NORMALLY.
- [SDR CHQA200900138](https://openairdocs.org/sdr/CHQA200900138.md): Connector · loose · Jun 8, 2009 · N563RP · Emb EMB145LR · Light System Wiring
  > DURING INSPECTION, THE EMERGENCY LIGHT OVER THE MAIN DOOR AND FRONT SIDE OF THE EXIT ROW SIGN WERE INOP WHEN TESTED. MAINTENANCE RE-SECURED ALL CONNECTORS ON THE EMERGENCY LIGHT BATTERY PACKS PER AMM 33-50-00, ALL LIGHTS OPS CHECKED GOOD.
- [SDR CHQA200900085](https://openairdocs.org/sdr/CHQA200900085.md): Seal · leaking · Mar 19, 2009 · N563RP · Emb EMB145LR · Passenger/Crew Doors
  > FLIGHT 6123, MKE TO CVG - CREW REPORTED THAT THE AUTO PRESSURIZATION SYSTEM WAS INOP, BUT DID NOT TRY THE MANUAL MODE BEFORE RETURNING TO MKE. THEY ALSO REPORTED THAT THE MAIN ENTRY DOOR WAS SQUEALING IN FLIGHT. THE AIRCRAFT WAS PRESSURIZED ON THE GROUND AND
- [SDR CHQA200800156](https://openairdocs.org/sdr/CHQA200800156.md): Control Unit · faulty · Jul 29, 2008 · N563RP · Emb EMB145LR · Stabilizer Control System
  > FLIGHT 6349, CVG TO LIT. DURING INITIAL CLIMB THE FLIGHT CREW RECEIVED A PTRIM MAIN INOP MESSAGE ON EICAS. THE CREW PERFORMED THE APROPRIATE QRH CHECKLIST ITEMS AND THE ACFT LANDED WITHOUT INCIDENT BACK AT CVG. MAINTENANCE TROUBLESHOT THE FAULT TO THE HORIZ
- [SDR CHQA200800036](https://openairdocs.org/sdr/CHQA200800036.md): Engine · making metal · Feb 20, 2008 · N563RP · Emb EMB145LR · Engine (Turbine/Turboprop)
  > CVG TO GSP - AFTER TAKEOFF, THE FLIGHT CREW REPORTED SMOKE IN THE CABIN AND THE AUTO SHUTDOWN OF ENGINE NR 1. THE AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE CHECKED THE CMC FOR FAULT CODES AND FOUND MESSAGES FOR OIL DEBRIS, CONTROL S
- [SDR CHQA200600130](https://openairdocs.org/sdr/CHQA200600130.md): Battery · discharged · Oct 3, 2006 · N563RP · Emb EMB145LR · Emergency Lighting
  > EMERGENCY LIGHTS IN BACK HALF OF AIRPLANE (INSIDE) WERE ON WHEN ARRIVED AT THE AIRCRAFT. AIRPLANE WAS COMPLETELY POWERED DOWN. REMOVED AND REPLACED EMERGENCY BATTERIES.
- [SDR CHQA200600007](https://openairdocs.org/sdr/CHQA200600007.md): Bulb · burned out · Jan 15, 2006 · N563RP · Emb EMB145LR · Emergency Lighting
  > RIGHT AFT EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED BULB ON RIGHT AFT EMERGENCY LIGHT IAW EMB MM 33-50-10.
- [SDR CHQA200500174](https://openairdocs.org/sdr/CHQA200500174.md): Static Inverter · inoperative · Oct 6, 2005 · N563RP · Emb EMB145LR · Emergency Lighting
  > LEFT OVERWING EMERGENCY EXIT MARKER LIGHT INOPERATIVE. REMOVED AND REPLACED NR 4 STATIC INVERTER IAW EMB 145 MM 33-50-11. 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 = 'N563RP' AND deregistration_id = 'N563RP-2018-07-11'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N563RP-2018-07-11/reports

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