# Service difficulty reports: N15527

A list on [N15527](https://openairdocs.org/aircraft/N15527.md).

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

- [SDR ASOA201701234002](https://openairdocs.org/sdr/ASOA201701234002.md): Engine · flamed out · Jan 23, 2017 · N15527 · Emb EMB135LR · Engine (Turbine/Turboprop)
  > IAH - FLIGHT 4231, THE CREW REPORTED ENG NR 2 OUT IN FLIGHT. THE AIRCRAFT LANDED IN IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NUMBER 2 ENGINE, OPERATIONALLY TESTED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA201610164076](https://openairdocs.org/sdr/ASOA201610164076.md): Metering Unit · inoperative · Oct 11, 2016 · N15527 · Emb EMB135LR · Engine (Turbine/Turboprop)
  > FLIGHT 4193, THE CREW REPORTED THAT IMMEDIATELY AFTER TAKEOFF, THE NR 2 ENGINE SHUTDOWN, WITH NO N2 OR FUEL FLOW, AND RECEIVED E2 NO DISP, E2 CTL FAIL, SPOILER FAIL, AND RUD HDOV PROT FAIL MESSAGES. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT
- [SDR ASOA201610164075](https://openairdocs.org/sdr/ASOA201610164075.md): Fadec · inoperative · Oct 11, 2016 · N15527 · Emb EMB135LR · Engine (Turbine/Turboprop)
  > FLIGHT 4193, THE CREW REPORTED THAT IMMEDIATELY AFTER TAKEOFF, THE NR 2 ENGINE SHUTDOWN, WITH NO N2 OR FUEL FLOW, AND RECEIVED E2 NO DISP, E2 CTL FAIL, SPOILER FAIL, AND RUD HDOV PROT FAIL MESSAGES. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDEN
- [SDR ASOA201610164074](https://openairdocs.org/sdr/ASOA201610164074.md): Fadec · malfunctioned · Oct 11, 2016 · N15527 · Emb EMB135LR · Engine (Turbine/Turboprop)
  > FLIGHT 4193, THE CREW REPORTED THAT IMMEDIATELY AFTER TAKEOFF, THE NR 2 ENGINE SHUTDOWN, WITH NO N2 OR FUEL FLOW, AND RECEIVED E2 NO DISP, E2 CTL FAIL, SPOILER FAIL, AND RUD HDOV PROT FAIL MESSAGES. THE AIRCRAFT RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDEN
- [SDR ASOA20160905070H](https://openairdocs.org/sdr/ASOA20160905070H.md): Light · inoperative · Sep 5, 2016 · N15527 · Emb EMB135LR · Emergency Lighting
  > THE CREW REPORTED THAT THE FIRST SEGMENT OF AISLE PATH LIGHTING WAS INOPERATIVE. MAINTENANCE R & R THE AFFECTED LIGHT STRIP, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20160404015](https://openairdocs.org/sdr/ASOA20160404015.md): Frame · cracked · Apr 4, 2016 · N15527 · Emb EMB135LR · Fuselage Main, Frame
  > DURING C-CHECK. RT FRAME 10 IS CRACKED. REPLACED RT FRAME 10 IAW SRM 51-40-02. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20150424039](https://openairdocs.org/sdr/ASOA20150424039.md): Unknown · odor · Apr 24, 2015 · N15527 · Emb EMB135LR · Air Distribution System
  > THE CREW REPORTED THAT THE GASPER FAN HAD A BURNING ODOR WITH PACK NR 2 AND NOT RUNNING THE NR 2 RECIRCULATION FAN. ACFT WAS APPROVED FOR RETURN TO SERVICE. MAINTENANCE INSPECTED THE ACFT AND OPERATIONALLY TESTED BOTH RECIRCULATING FANS WITH NO DEFECTS OR O
- [SDR ASOA20150424039H](https://openairdocs.org/sdr/ASOA20150424039H.md): Fan · failed · Apr 24, 2015 · N15527 · Emb EMB135LR · Air Distribution Fan
  > THE CREW REPORTED THAT THE GASPER FAN HAD A BURNING ODOR WITH PACK NR 2 AND NOT RUNNING THE NR 2 RECIRCULATION FAN. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20131211215](https://openairdocs.org/sdr/ASOA20131211215.md): Drag Angle · cracked · Dec 11, 2013 · N15527 · Emb EMB135LR · Fuselage Miscellaneous Structure
  > DURING 1A INSPECTION, THE RT FWD DRAG ANGLE, PROFILE, WAS FOUND TO BE CRACKED AT FRAME 76. MAINTENANCE R & R THE AFFECTED DRAG ANGLE, PROFILE, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA201311274](https://openairdocs.org/sdr/ASOA201311274.md): Sill · corroded · Nov 27, 2013 · N15527 · Emb EMB135LR · Fuselage Miscellaneous Structure
  > DURING C-CHECK, CENTER SERVICE DOOR SILL CORRODED. MAINTENANCE R & R DOOR SILL IAW SRM 51-40-02. RETURNED TO SERVICE.
- [SDR ASOA20131127273](https://openairdocs.org/sdr/ASOA20131127273.md): Threshold · corroded · Nov 27, 2013 · N15527 · Emb EMB135LR · Fuselage Miscellaneous Structure
  > DURING C-CHECK CARGO DOOR LOWER THRESHOLD CORRODED. MAINTENANCE REPAIRED THRESHOLD IAW SRM 51-40-02. RETURNED TO SERVICE.
- [SDR ASOA20131127272](https://openairdocs.org/sdr/ASOA20131127272.md): Shear Tie · cracked · Nov 27, 2013 · N15527 · Emb EMB135LR · Fuselage Internal Mounting Structure
  > DURING C-CHECK SHEAR TIE AT FRAME 75, S2L-2R CORRODED. MX R & R SHEAR TIE IAW EC5310-01317. RETURNED TO SERVICE.
- [SDR ASOA20130313029](https://openairdocs.org/sdr/ASOA20130313029.md): Inverter · inoperative · Mar 13, 2013 · N15527 · Emb EMB135LR · Emergency Lighting
  > DURING ROUTINE MX THE EMERGENCY LIGHT ABOVE THE F/A SEAT FAILED TO ILLUMINATE WHEN TESTED. MX REPLACED THE EMERGENCY LIGHT INVERTER, OPERATIONALLY TESTED THE SYS AND CLEARED THE DISCREPANCY.
- [SDR CHQA201100223](https://openairdocs.org/sdr/CHQA201100223.md): Unknown · odor · Jun 13, 2011 · N15527 · Emb EMB135LR · Pneumatic Distribution System
  > CREW REPORTED, SHORTLY AFTER TAKEOFF A SMOKE ODOR IN THE CABIN AND THE COCKPIT. A LAVATORY SMOKE INDICATION THEN APPEARED ON THE EICAS. REPORTED THAT AFTER APPROXIMATELY 30 SECONDS THE ODOR AND THE INDICATION BOTH WENT AWAY. THE AIRCRAFT LANDED WITHOUT INCI
- [SDR CHQA201100197](https://openairdocs.org/sdr/CHQA201100197.md): Light · inoperative · May 28, 2011 · N15527 · Emb EMB135LR · Emergency Lighting
  > DURING INSPECTION, THE RIGHT AFT EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE EMERGENCY LIGHTS WITH NO DEFECTS NOTED.
- [SDR CHQA201100072](https://openairdocs.org/sdr/CHQA201100072.md): Carbon Seal · worn · Mar 22, 2011 · N15527 · Emb EMB135LR · Turbine Engine Oil System
  > CREW REPORTED THAT UPON TAKEOFF, AT APPROXIMATELY 400 FEET, CREW BECAME AWARE OF SMOKE IN THE COCKPIT AND CABIN. AFTER LEVELING OFF AT 4000 FEET, THE SMOKE RAPIDLY DISSIPATED AND WENT AWAY WITH POWER REDUCTION AND THE RECIRCULATION FANS TURNED OFF. CREW DECL
- [SDR CHQA201000202](https://openairdocs.org/sdr/CHQA201000202.md): Pressure Switch · faulty · Oct 22, 2010 · N15527 · Emb EMB135LR · Rudder Control System
  > CREW REPORTED THAT ON CLIMB-OUT FROM MKE, RECEIVED A RUDDER SYS 1-2 INOP MESSAGE ALONG WITH A YAW DAMP FAIL MESSAGE ON EICAS. THE QRH WAS FOLLOWED AND THE MESSAGE CLEARED, BUT RETURNED AFTER ABOUT 5 MINUTES. THE QRH WAS FOLLOWED AGAIN AND THE MESSAGE CLEARED
- [SDR CHQA201000095](https://openairdocs.org/sdr/CHQA201000095.md): Transducer · failed · May 10, 2010 · N15527 · Emb EMB135LR · Landing Gear Brake System
  > AFTER LANDING THE CREW REPORTED THAT HIGH SPEED BRAKING WAS INEFFECTIVE. BOTH BRAKE PEDALS WENT TO THE FLOOR WITH LITTLE EFFECT. CREW ALSO REPORTED THAT BRAKING SEEMED TO IMPROVE AT LOWER SPEEDS. MAINTENANCE FOUND FAULTS ON THE CMC FOR BRAKE PPTAN 3 FAIL AN
- [SDR CHQA200900216](https://openairdocs.org/sdr/CHQA200900216.md): Solenoid Valve · deteriorated · Oct 8, 2009 · N15527 · Emb EMB135LR · Landing Gear Retraction/Extension System
  > AFTER TAKEOFF WHEN A POSITIVE RATE OF CLIMB WAS ESTABLISHED, THE GEAR HANDLE WAS SELECTED TO THE UP POSITION, AND AFTER A FEW SECONDS THE CREW RECEIVED A RED GEAR DOWN INDICATION AND MASTER WARNING ON EICAS OF LG/DISAGREE. THE QRH WAS FOLLOWED AND THE AIRCRAF
- [SDR CHQA200900214](https://openairdocs.org/sdr/CHQA200900214.md): Electronic Unit · faulty · Oct 2, 2009 · N15527 · Emb EMB135LR · Landing Gear Retraction/Extension System
  > FLIGHT 1206, IND TO MKE. AFTER TAKEOFF, THE CREW SELECTED THE GEAR UP AND RECEIVED A 3 RED INDICATION SHOWING DOWN IN ADDITION TO LG LEVER DISAGREE ON EICAS. THE QRH WAS FOLLOWED AND THE FAULT DID NOT CLEAR. THE AIRCRAFT RETURNED TO IND AND LANDED WITHOUT I
- [SDR CHQA200900206](https://openairdocs.org/sdr/CHQA200900206.md): Unknown · malfunctioned · Sep 20, 2009 · N15527 · Emb EMB135LR · Landing Gear Retraction/Extension System
  > FLIGHT 1119, MKE TO SDF. CREW REPORTED THAT AFTER DEPARTURE THE LANDING GEAR FAILED TO RETRACT ALONG WITH A LANDING GEAR LEVER DISAGREE MESSAGE. THE CREW RAN THE QRH PROCEDURE WITH NO SUCCESS. THE AIRCRAFT THEN RETURNED TO MKE AND LANDED WITHOUT INCIDENT.
- [SDR C2XA07IA206](https://openairdocs.org/sdr/C2XA07IA206.md): Control Handle · defective · Sep 14, 2007 · N15527 · Emb EMB135LR · Landing Gear Selector
  > IAH - FLIGHT 2206, THE CREW REPORTED LANDING GEAR DOES NOT RETRACT PROPERLY, LANDING GEAR HANDLE SELECTED UP GEAR INDICATION 3 DOWN FOR 5 - 10 SEC THEN IN TRANSIT AND THEN GEAR UP. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED LANDIN
- [SDR C2XA07IA086](https://openairdocs.org/sdr/C2XA07IA086.md): Unknown · unknown · Apr 12, 2007 · N15527 · Emb EMB135LR · Main Landing Gear
  > IAH - FLIGHT 2922 AFTER TAKEOFF, THE CREW SELECTED GEAR LEVER TO UP POSTION BUT GEAR DID NOT RETRACT, CYCLED LEVER BACK DOWN THEN UP RETRACTED NORMAL. THE AIRCRAFT CONTINUED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED EXTENSION AND RETRACT
- [SDR C2XA07IA012](https://openairdocs.org/sdr/C2XA07IA012.md): Indication Sys · malfunctioned · Jan 11, 2007 · N15527 · Emb EMB135LR · Landing Gear Position and Warning
  > IAH - FLIGHT 3109, THE CREW REPORTED AFTER T/O THE GEAR STARTED TO RETRACT, GOT AMBER THEN RED INDICATIONS WITH LANDING GEAR LEVER DISAGREE MESSAGE. THE GEAR STOWED AT 1300 FT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPE
- [SDR C2XA05IA104](https://openairdocs.org/sdr/C2XA05IA104.md): Light · inoperative · Sep 10, 2005 · N15527 · Emb EMB135LR · Emergency Lighting
  > LRD - FLIGHT 2359, DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT BOTH SIDE PANEL EXIT LIGHTS AT THE OVERWING EXITS WERE INOPERATIVE. THE CREW RESET THE EMERGENCY LIGHT SYSTEM, OPERATIONALLY CHECK WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN
- [SDR C2XA05SH096](https://openairdocs.org/sdr/C2XA05SH096.md): Firewall · cracked · Aug 9, 2005 · N15527 · Emb EMB135LR · APU Cowling/Containment
  > SHV - DURING C-CHECK APU FIRE WALL CRACK AROUND NUT PLATE FASTENERS AT 3 O`CLOCK POSITION. MAINTENANCE REPAIRED APU FIREWALL AT 3 O`CLOCK POSITION IAW EC 5330-01483. THE AIRCRAFT WAS APPROVED TO CONTINUED FOR SERVICE.
- [SDR C2XA05SH101](https://openairdocs.org/sdr/C2XA05SH101.md): Floor Support · corroded · May 11, 2005 · N15527 · Emb EMB135LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK CORROSION ON RT OMEGA BEAM AT FR 18. MAINTENANCE REPAIRED RT OMEGA BEAM AT FR 18 IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA04TY099](https://openairdocs.org/sdr/C2XA04TY099.md): Threshold · corroded · Jun 23, 2004 · N15527 · Emb EMB135LR · Fuselage Miscellaneous Structure
  > DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE PASSENGER ENTRY DOOR THRESHOLD PLATE. MAINTENANCE REMOVED AND REPLACED THE THRESHOLD PLATE IAW EMB SRM 51-21-00. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.
- [SDR C2XA04IA022](https://openairdocs.org/sdr/C2XA04IA022.md): Proximity Switch · faulty · Mar 1, 2004 · N15527 · Emb EMB135LR · Landing Gear Position and Warning
  > DURING CLIMB THE NOSE GEAR DOORS DID NOT RETRACT AFTER THE NOSE LANDING GEAR WAS UP AND LOCKED. THE AIRCRAFT RETURNED TO XNA AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS FERRIED TO IAH WHERE MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR UPLOCK PROX
- [SDR C2XA03BT115](https://openairdocs.org/sdr/C2XA03BT115.md): Controller · faulty · Dec 7, 2003 · N15527 · Emb EMB135LR · Cabin Pressure Controller
  > CREW REPORTED, AUTO PRESSURIZATION FAILED DURING DESCENT. AIRCRAFT WAS RELEASED IAW MEL 21-31-03/1 CONTROL NUMBER 037305. AIRCRAFT RETURNED TO SERVICE. MAINTENANCE REMOVED AND REPLACED DIGITAL PRESSURIZATION CONTROLLER IAW EMB135 AMM 21-31-01. OPS CHECKED
- [SDR C2XA03CL189](https://openairdocs.org/sdr/C2XA03CL189.md): Light · inoperative · Nov 18, 2003 · N15527 · Emb EMB135LR · Emergency Lighting
  > CLE FLIGHT 2051 THE CREW REPORTED THE RIGHT OVERWING EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE RIGHT WING AFT EMERGENCY LIGHT. OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA03CL117](https://openairdocs.org/sdr/C2XA03CL117.md): Charger · faulty · Jul 2, 2003 · N15527 · Emb EMB135LR · Emergency Lighting
  > DURING ROUTINE MAINTENANCE THE EMERGENCY AISLE PATH LIGHTS WERE DIM. MAINTENANCE REPLACED THE NR 2 EMERGENCY BATTERY CHARGER. OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA03TY050](https://openairdocs.org/sdr/C2XA03TY050.md): Handle · shorted · Apr 16, 2003 · N15527 · Emb EMB135LR · Extinguishing System
  > TYS- DURING A SCHEDULED 1-C INSPECTION THE FIRE HANDLE NR 2 WOULD NOT LIGHT UP DURING THE FIRE DETECTION TEST. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE FIRE SHUTOFF AND EXTINGUISHING HANDLE. OPS CHECK WAS GOOD. A/C WILL BE RELEASED UPON COMPLETION OF AL
- [SDR C2XA03TY049](https://openairdocs.org/sdr/C2XA03TY049.md): Shear Tie · bent · Apr 15, 2003 · N15527 · Emb EMB135LR · Fuselage Main, Structure
  > TYS, DURING A SCHEDULED INSPECTION A DENT WAS FOUND ON THE LEFT FORWARD FUSELAGE BETWEEN FRAMES 10 AND 11 AND BETWEEN STRINGERS 13L AND 15L. MAINTENANCE REMOVED THE DAMAGED SHEAR CLIP, RESTORED SKIN AND INSTALLED A NEW SHEAR CLIP IAW EC5330-01246. THE REPAIR
- [SDR C2XA03TY048](https://openairdocs.org/sdr/C2XA03TY048.md): Floorbeam · corroded · Apr 15, 2003 · N15527 · Emb EMB135LR · Fuselage Main, Floor Beam
  > TYS, DURING A SCHEDULED INSPECTION THE FORWARD DIGITAL PLATE WAS FOUND CORRODED AFT OF THE COCKPIT STEP IN THE GALLEY. MAINTENANCE REMOVED AND REPLACED THE CENTER FORWARD DIGITAL IAW EMB-145 SRM 53-21-10, 51-40-02, 51-21-04/05 AND 06. THE REPAIR WAS SATISFAC
- [SDR C2XA03TY047](https://openairdocs.org/sdr/C2XA03TY047.md): Stringer · bent · Apr 15, 2003 · N15527 · Emb EMB135LR · Fuselage Main, Longeron/Stringer
  > TYS, DURING A SCHEDULED INSPECTION A TEMPORARY REPAIR BETWEEN FRAMES 24 AND 25 AT STRINGER 12R, WAS MADE PERMANENT. REMOVED THE OLD REPAIR STRINGER 12R, CUT OUT A SECTION OF FR 24 AND INSTALLED A FRAME SPLICE, DOUBLER AND STRINGER IAW SRM 53-00-04, 53-22-01,
- [SDR C2XA02CL235](https://openairdocs.org/sdr/C2XA02CL235.md): Wire Harness · faulty · Nov 30, 2002 · N15527 · Emb EMB135LR · Landing Gear Position and Warning
  > CLE FLIGHT#3141 THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE DURING FLIGHT ASSOCIATED WITH "THUMP" NOISE UNDER NOSE.THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT.MAINTENANCE REPLACED THE LEFT MAIN LANDING GEAR WOW PROXIMITY SWITCH WIRE HARNESS W510.
- [SDR C2XA02CL162](https://openairdocs.org/sdr/C2XA02CL162.md): Receptacle · burned · Aug 4, 2002 · N15527 · Emb EMB135LR · Buffet/Galleys
  > SLP - FLIGHT 4153, THE CREW REPORTED A STRONG SMELL OF BURNING RUBBER FROM THE NR 2 COFFEE JUG. THE AIRCRAFT WAS RELEASED IAW 25-60-02/3D. MAINTENANCE REPLACED THE COFFEE POT RECEPTACLE IN THE GALLEY. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASE
- [SDR C2XA02CL136](https://openairdocs.org/sdr/C2XA02CL136.md): Fire Loop · chafed · Jun 27, 2002 · N15527 · Emb EMB135LR · Fire Detection
  > DTW FLIGHT 3318 THE CREW REPORTED A NR 2 FIRE DETECT FAIL MESSAGE ON TAKEOFF. THE TAKEOFF WAS ABORTED AND AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED AND REPLACED THE NR 2 ENGINE FIRE LOOP DETECTOR AND CLEANED THE NR 2 ENGINE FIRE BOTTLE CANNON PLUG
- [SDR C2XA02CL081](https://openairdocs.org/sdr/C2XA02CL081.md): Module · faulty · Mar 24, 2002 · N15527 · Emb EMB135LR · Emergency Lighting
  > CLE FLIGHT 3029 THE CREW REPORTED THE EMERGENCY LIGHTS WOULD NOT GO OUT. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED THE EMERGENCY LIGHT CONTROL MODULE. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.
- [SDR C2XA01CL247](https://openairdocs.org/sdr/C2XA01CL247.md): Control Handle · intermittent · Dec 17, 2001 · N15527 · Emb EMB135LR · Landing Gear Selector
  > CLE FLIGHT 3064 THE CREW REPORTED THE LANDING GEAR DID NOT RETRACT. RECYCLED AND IT WAS SLOW TO RETRACT. MAINTENANCE REPLACED THE LANDING GEAR HANDLE ASSEMBLY. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.
- [SDR C2XA01CL185](https://openairdocs.org/sdr/C2XA01CL185.md): Firewall · cracked · Jul 28, 2001 · N15527 · Emb EMB135LR · Fuselage Main, Bulkhead
  > CLE MAINTENANCE DURING ACCOMPLISHMENT OF SB 145-49-0009 AND 145-49-0018 MAINTENANCE FOUND THE APU FIREWALL CRACKED IN SEVERAL PLACES. THE AIRCRAFT WAS RELEASED IAW EMBRAER AUTHORIZATION GST 2630/01. MAINTENANCE REPLACED THE APU FIRE WALL. OPERATIONAL CHECKS
- [SDR C2XA01CL118](https://openairdocs.org/sdr/C2XA01CL118.md): Control Handle · defective · May 24, 2001 · N15527 · Emb EMB135LR · Landing Gear Selector
  > CLE FLIGHT 3678 THE CREW REPORTED THE NOSE GEAR WAS SLOW TO RETRACT. RECEIVED A L/G GEAR LEVER DISAGREEMENT. THE MESSAGE CLEARED ON ITS OWN. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LANDING GEAR CONTROL HANDLE. OPERATIONAL C
- [SDR C2XA01IA234](https://openairdocs.org/sdr/C2XA01IA234.md): Landing Gear · malfunctioned · Apr 29, 2001 · N15527 · Emb EMB135LR · Landing Gear Retraction/Extension System
  > BPT - DURING TRAINING FLIGHT 838, THE CREW REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE PERFORMED OPERATIONAL CHECKS ON THE LANDING GEAR EXTENSION / RETRACTION SYSTEM WITH NO DEFECTS NOTED, AN

## 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 = 'N15527' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N15527/reports

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