# Service difficulty reports: N29917

A list on [N29917](https://openairdocs.org/aircraft/N29917.md).

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

Page 1 of 2 · 73 reports

- [SDR ASOA201907125085](https://openairdocs.org/sdr/ASOA201907125085.md): Inverter · inoperative · Jul 12, 2019 · N29917 · Emb EMB145LR · Emergency Lighting
  > DURING MX INSPECTION THE AFT EMERGENCY LIGHT STRIPS 6,7, AND 8 INOP. MX R&R #6 INVERTER WITH OPERATIONAL CHECK GOOD. A/C WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA201903157032](https://openairdocs.org/sdr/ASOA201903157032.md): Skin · dented · Mar 15, 2019 · N29917 · Emb EMB145LR · Wing, Plate/Skin
  > TYS A/C IS IN C-CHECK WHEN A FUR 5700-01510,DEFECT BO27891 RT L/E 1 WAS DENTED AND REQUIRED A PERMANENT REPAIR. MAINTENANCE CUT OUT THE DAMAGE AREA,FABRICATED A FILLER(.071) AND A DOUBLER OF SAME MATERIAL AND INSTALLED IAW SRM 57-40-00. ALL WORK ACCOMPLISHED
- [SDR ASOA201706064042](https://openairdocs.org/sdr/ASOA201706064042.md): Display · shorted · Jun 6, 2017 · N29917 · Emb EMB145LR · Attitude and Direction Data System
  > THE CREW REPORTED THAT EICAS FAIL IN FLIGHT WITH ODOR OF BURNING ELECTRICAL. THE AIRCRAFT DIVERTED WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, AND MAINTENANCE REMOVED AND REPLACED THE DEFECTIVE DISPLAY UNIT, OPERATIONALLY TESTED WITH
- [SDR ASOA201701305009](https://openairdocs.org/sdr/ASOA201701305009.md): Unknown · odor · Jan 30, 2017 · N29917 · Emb EMB145LR · Air Distribution System
  > PILOT REPORTED BURNING ODOR COMING FROM GALLEY ABOVE THE COFFEE POTS. MX PERFORMED OPERATIONAL CHECK OF COFFEEMAKERS WITH NO BURNING ODOR NOTED AT THIS TIME. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20160423021](https://openairdocs.org/sdr/ASOA20160423021.md): Fitting · cracked · Apr 23, 2016 · N29917 · Emb EMB145LR · Engine Mount Section
  > DURING C-CHECK, THE RT ENGINE LOWER FWD MOUNT YOKE FITTING WAS FOUND TO BE CRACKED. MAINTENANCE R & R THE FITTING IAW EC5450-01199. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20160408017V](https://openairdocs.org/sdr/ASOA20160408017V.md): Skin · cracked · Apr 8, 2016 · N29917 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > DURING C-CHECK THE LT AFT SKIN WAS FOUND TO BE CRACKED AROUND FASTENERS AT FRAME 75 STR 1L-2L. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EC5330-03099. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20160408016](https://openairdocs.org/sdr/ASOA20160408016.md): Skin · cracked · Apr 8, 2016 · N29917 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > DURING C-CHECK THE RT AFT SKIN WAS FOUND TO BE CRACKED AROUND FASTENERS AT FRAME 75 AND STRINGERS 2R-3R. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EC5330-03099. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20150730041](https://openairdocs.org/sdr/ASOA20150730041.md): Oil System · leaking · Jul 30, 2015 · N29917 · Emb EMB145LR · Turbine Engine Oil System
  > CREW REPORTED AN OIL ODOR COMING FROM NR 1 ENGINE BLEED. MAINTENANCE R & R NR 1 ENGINE. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20150726041](https://openairdocs.org/sdr/ASOA20150726041.md): Duct · dirty · Jul 26, 2015 · N29917 · Emb EMB145LR · Air Distribution System
  > THE CREW REPORTED A VERY STRONG ODOR OF OIL IN FLIGHT. STRONGER IN DESCENT. MAINTENANCE INSPECTED AND CLEANED AIR DUCTS IAW 21-20-00. NO ODOR WAS NOTED AND ACFT RETURNED TO SERVICE.
- [SDR ASOA20140807086](https://openairdocs.org/sdr/ASOA20140807086.md): Flashlight · inoperative · Aug 6, 2014 · N29917 · Emb EMB145LR · Emergency Equipment
  > CREW REPORTED THE AFT CABIN FLASHLIGHT WAS INOPERATIVE. INTIALLY WAS PLACED ON MEL 25-60-05. MAINTENANCE R & R THE FLASHLIGHT WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140624143](https://openairdocs.org/sdr/ASOA20140624143.md): Gusset · corroded · Jun 24, 2014 · N29917 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING C-CHECK, CORROSION WAS FOUND AROUND TWO NUTPLATES ON CENTER OMEGA BEAM GUSSET, Y-0.0, BETWEEN FRAMES 14 & 18. R & R GUSSET IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140624142](https://openairdocs.org/sdr/ASOA20140624142.md): Threshold · corroded · Jun 24, 2014 · N29917 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING C-CHECK, CARGO DOOR THRESHOLD FOUND CORRODED AT NUTPLATE HOLES. MAINTENANCE R & R THRESHOLD IAW SRM 51-40-02 AND CPM 51-21-04. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140520088V](https://openairdocs.org/sdr/ASOA20140520088V.md): Nut Plate · corroded · May 20, 2014 · N29917 · Emb EMB145LR · Fuselage Main, Attach Fittings
  > DURING C-CHECK, CORROSION AROUND TWO NUTPLATES ON CENTER OMEGA BEAM GUSSET, Y-0.0, BETWEEN FRAMES 14 AND 18 AS MARKED IN CENTER FUSELAGE I. MAINTENANCE R & R GUSSETT AND 3 EA DOUBLERS ON FWD CENTER BEAM NR FRAME 14 IAW SRM 51-40-02, APPLIED PRIMER AND TOPCOA
- [SDR ASOA20140520087](https://openairdocs.org/sdr/ASOA20140520087.md): Threshold · corroded · May 20, 2014 · N29917 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING C-CHECK, CARGO DOOR THRESHOLD HAS CORROSION, AT NUTPLATES HOLES. R & R CARGO DOOR THRESHOLD IAW SRM 51-40-02 AND CPM 51-21-04. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140517086V](https://openairdocs.org/sdr/ASOA20140517086V.md): Floor Support · corroded · May 17, 2014 · N29917 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING C-CHECK, RT FLOOR SUPPORT AT FRAME 53 HAS CORROSION. MAINTENANCE R & R RT FLOOR SUPPORT IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140517085V](https://openairdocs.org/sdr/ASOA20140517085V.md): Floor Support · corroded · May 17, 2014 · N29917 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING C-CHECK, CORROSION AROUND NUTPLATE ON CENTER OMEGA BEAM, Y=0.0, GUSSET AT FRAME 20. MAINTENANCE BLENDED CORROSION AROUND NUTPLATE ON CENTER OMEGA BEAM GUSSET AT FRAME 20, MATERIAL LOSS IS WITHIN LIMITS IAW SRM 53-21-10. PREPPED, ALODINED, PRIMED AND T
- [SDR ASOA20140517084](https://openairdocs.org/sdr/ASOA20140517084.md): Floor Support · corroded · May 17, 2014 · N29917 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING C-CHECK RT FLOOR SILL IN CARGO AREA FRAMES 61-63 IS CORRODED. MAINTENANCE R & R FLOOR SILL AND SPLICE IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140517083](https://openairdocs.org/sdr/ASOA20140517083.md): Floor Support · corroded · May 17, 2014 · N29917 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING C-CHECK, CORROSION AROUND NUTPLATE BOTH NUTPLATES ON GUSSETT AT RT OMEGA BEAM, Y+479.0, FRAME 22. MAINTENANCE DETERMINED CORROSION AROUND NUTPLATE HAS 100 PERCENT MATERIAL LOSS, R & R RT GUSSETT IAW SRM 41-40-02. THE ACFT WAS APPROVED FOR RETURN TO SE
- [SDR ASOA20140517082](https://openairdocs.org/sdr/ASOA20140517082.md): Floor Support · corroded · May 17, 2014 · N29917 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING C-CHECK, FOUND CORROSION AROUND NUTPLATE ON GUSSETT RT OMEGA BEAM, Y=479.0, FRAME 20. MAINTENANCE DETERMINED CORROSION AROUND NUTPLATE IN GUSSETT IS 100 PERCENT MATERIAL LOSS, R & R RT GUSSETT IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SER
- [SDR ASOA20140517081](https://openairdocs.org/sdr/ASOA20140517081.md): Floor Support · corroded · May 17, 2014 · N29917 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING C-CHECK LAVATORY UNDER FLOOR OMEGA BEAM CAP IS CORRODED, LOCAL LEVEL 2, AS MARKED ON RT SIDE AROUND NUTPLATE. MAINTENANCE BLENDED CORROSION AROUND NUTPLATE 100 NR MATERIAL LOSS, R & R OMEGA BEAM CAP IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN T
- [SDR ASOA20140517080V](https://openairdocs.org/sdr/ASOA20140517080V.md): Firewall · cracked · May 16, 2014 · N29917 · Emb EMB145LR · APU Cowling/Containment
  > DURING C-CHECK, THE APU FIREWALL WAS FOUND TO BE CRACKED INBD OF STRINGER 12L WHERE THE APU CONTROL HARNESS CONNECTS. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW SRM 53-32-10. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140517079V](https://openairdocs.org/sdr/ASOA20140517079V.md): Floorbeam · corroded · May 16, 2014 · N29917 · Emb EMB145LR · Fuselage Main, Floor Beam
  > DURING C-CHECK THE CENTER AISLE CROSSBEAM AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE R & R THE BEAM IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140517078](https://openairdocs.org/sdr/ASOA20140517078.md): Shear Tie · corroded · May 16, 2014 · N29917 · Emb EMB145LR · Fuselage Internal Mounting Structure
  > DURING C-CHECK THE FRAME 65 SHEAR CLIP WAS FOUND TO BE CORRODED BETWEEN STRINGERS 15-16L. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A SPLICE REPAIR IAW SRM 53-31-04. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140517077](https://openairdocs.org/sdr/ASOA20140517077.md): Frame · corroded · May 16, 2014 · N29917 · Emb EMB145LR · Fuselage Main, Frame
  > DURING C-CHECK, FRAME 65 WAS FOUND TO BE CORRODED BETWEEN STRINGERS 16-17L. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW SRM 53-31-04. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140516074](https://openairdocs.org/sdr/ASOA20140516074.md): Bearing Cap · corroded · May 16, 2014 · N29917 · Emb EMB145LR · Nose/Tail Landing Gear
  > DURING C-CHECK CORROSION FOUND ON LT AND RT NLG BEARING CAPS. MAINTENANCE REPLACED LT AND RT NLG BEARING CAPS AND SHIMMED IAW AMM 32-20-01, FOR INSTALLATION SEE W04249, TASK 7021. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140516073](https://openairdocs.org/sdr/ASOA20140516073.md): Partition · corroded · May 16, 2014 · N29917 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING C-CHECK CORROSION ON RT WALL DOUBLER AT FRAME 61 AT FLOOR LEVEL. MAINTENANCE DETERMINED CORROSION 100 PERCENT MATERIAL LOSS, REMOVED WALL DOUBLER, LOCATED, DRILLED, ALODINED AND INSTALLED NEW RT WALL DOUBLER AT FRAME 61 IAW SRM 51-20-03 AND SRM 51-40-0
- [SDR ASOA20140516072](https://openairdocs.org/sdr/ASOA20140516072.md): Floor Support · corroded · May 16, 2014 · N29917 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING C-CHECK LAVATORY UNDER FLOOR OMEGA BEAM CAP IS CORRODED AS MARKED ON LT SIDE AROUND NUT PLATE. MAINTENANCE DETERMINED CORROSION ON OMEGA BEAM CAP LT SIDE FRAMES 59-61 IS 100 PERCENT MATERIAL LOSS IAW SRM 53-24-10. MAINTENANCE R & R LT GUSSET IAW SRM 5
- [SDR ASOA20140516071](https://openairdocs.org/sdr/ASOA20140516071.md): Floor Support · corroded · May 16, 2014 · N29917 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING C-CHECK, CARGO UNDERFLOOR SUPPORT 65-68 LT SIDE UNDER FLOORBOARD 271FF HAS CORROSION. MAINTENANCE R & R FLOOR SUPPORT IAW SRM 51-40-02 AND 53-31-10. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140516070V](https://openairdocs.org/sdr/ASOA20140516070V.md): Partition · damaged · May 16, 2014 · N29917 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING C-CHECK, BOTH SHOT BOLT HOLES FOR LT COCKPIT PARTION ARE ELONGATED. MAINTENANCE REMOVED CHAFED UPPER PIN GUIDE FABRICATED, LOCATED AND DRILLED UPPER PIN GUIDE DOUBLER IAW EC5320-017018. INSTALLED AND TOP COATED UPPER AND LOWER PIN GUIDES IAW EC5320-0
- [SDR ASOA20140516069](https://openairdocs.org/sdr/ASOA20140516069.md): Stringer · cracked · May 16, 2014 · N29917 · Emb EMB145LR · Fuselage Main, Longeron/Stringer
  > DURING C-CHECK, STRINGER 3L AT FRAME 20 IS CRACKED. MAINTENANCE R & R STRINGER IAW SRM 51-40-02. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140516068](https://openairdocs.org/sdr/ASOA20140516068.md): Access Panel · corroded · May 16, 2014 · N29917 · Emb EMB145LR · Wing, Plate/Skin
  > DURING C-CHECK RT WING ACCESS PANEL 532AB FOUND CORRODED ON BACKSIDE AROUND FASTENER HOLES. MAINTENANCE BLENDED CORROSION AND REMAINED WITHIN ALLOWABLE LIMITS IAW EC5720-01178. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140516067](https://openairdocs.org/sdr/ASOA20140516067.md): Access Panel · corroded · May 16, 2014 · N29917 · Emb EMB145LR · Wing, Plate/Skin
  > DURING C-CHECK, RT WING ACCESS PANEL 632AB FOUND CORRODED ON BACKSIDE AROUND FASTENER HOLES. MAINTENANCE BLENDED CORROSION. REMAINED WITHIN ALLOWABLE LIMITS IAW EC5720-01178. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140516066V](https://openairdocs.org/sdr/ASOA20140516066V.md): Frame · broken · May 16, 2014 · N29917 · Emb EMB145LR · Fuselage Main, Frame
  > DURING C-CHECK, FRAME 10 BENEATH CO-PILOT'S DV WINDOW BROKEN. MAINTENANCE REMOVED BROKEN FRAME 10, LOCATED, DRILLED, ALODINED, AND INSTALLED NEW FRAME 10 IAW SRM 51-20-03, 51-40-03 AND CPM 51-14-05. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140516065](https://openairdocs.org/sdr/ASOA20140516065.md): Frame · broken · May 16, 2014 · N29917 · Emb EMB145LR · Fuselage Main, Frame
  > FRAME 10 BENEATH PILOT'S DV WINDOW BROKEN. MAINTENANCE REMOVED BROKEN FRAME 10, LOCATED, DRILLED, ALODINED AND INSTALLED NEW FRAME 10 IAW SRM 53-00-04, 51-40-02, AND CPM 51-21-04. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20131104079](https://openairdocs.org/sdr/ASOA20131104079.md): Check Valve · leaking · Nov 4, 2013 · N29917 · Emb EMB145LR · Aircraft Fuel Distribution System
  > THE CREW REPORTED FUEL LEAK ON TAKOFF FOR FIRST FIVE MINUTES THEN WHEN AT 10,000 FT AND REDUCED PITCH NO LEAK WAS NOTICED. MAINTENANCE INSPECTED AND REPLACED THE LEFT WING FUEL CHECK VALVE AT RIB 19. OPS CHECKED GOOD. NO LEAKS NOTED.
- [SDR ASOA06012013316](https://openairdocs.org/sdr/ASOA06012013316.md): Yoke · cracked · Jun 1, 2013 · N29917 · Emb EMB145LR · Engine Mount Section
  > ACFT WAS IN FOR A 5A CHECK, WHEN INSPECTION FOUND NTHE LT FWD LWR ENGINE YOKE CRACKED. MX R & R THE ENGINE YOKE IAW EC 5450-01013. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.
- [SDR ASOA20130221015](https://openairdocs.org/sdr/ASOA20130221015.md): Control Module · odor · Feb 21, 2013 · N29917 · Emb EMB145LR · Passenger Compartment Lighting
  > ELECTRICAL BURNING ODOR REPORTED COMING FROM FRONT OF CABIN. R & R THE PASSENGER CABIN LIGHTS CONTROL MODULE ASSY WITH OPS CHECK SUCCESSFUL. ACFT WAS APRROVED FOR RETURN TO SERVICE.
- [SDR ASOA201302150101](https://openairdocs.org/sdr/ASOA201302150101.md): Wire Harness · faulty · Feb 15, 2013 · N29917 · Emb EMB145LR · Light System Wiring
  > THE CREW REPORTED A ELECTRICAL BURN ODOR COMING FROM SEAT 1A AREA. MX INSPECTED AND FOUND LIGHT SOCKET SHORTED OUT AT LOCATION SIDEWALL PANEL ABOVE SEAT 1A. THE POWER SUPPLY BALLAST WAS DISCONNECTED. THE LT SIDEWALL LIGHT HARNESS ASSY WAS REPLACED AT SEAT
- [SDR C2XA11IA109](https://openairdocs.org/sdr/C2XA11IA109.md): Outflow Valve · malfunctioned · Jun 10, 2011 · N29917 · Emb EMB145LR · Pressure Regulator/Outflow Valve
  > DURING CRUISE THE CREW REPORTED THAT THE AUTO-PRESSURIZATION FAILED AND DECLARED AN EMERGENCY. DIVERTING TO AEX WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE OUTFLOW VALVE, PERFORMED OPERATIONAL CHECKS AND CLEARED THE DISCREPANCY.
- [SDR C2XA11IA108](https://openairdocs.org/sdr/C2XA11IA108.md): Outflow Valve · intermittent · Jun 10, 2011 · N29917 · Emb EMB145LR · Pressure Regulator/Outflow Valve
  > DURING CRUISE THE CREW REPORTED THAT THE AUTO-PRESSURIZATION FAILED AND DECLARED AN EMERGENCY DIVERTING TO AEX WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE PNEUMATIC OUTFLOW VALVE, PERFORMED OPERATIONAL CHECKS AND CLEARED THE DISCREPAN
- [SDR C2XA11CL079](https://openairdocs.org/sdr/C2XA11CL079.md): Key · shorted · Mar 24, 2011 · N29917 · Emb EMB145LR · Fire Detection
  > CLE FLT 2043 - THE CREW REPORTED A NR 1 ENGINE FIRE INDICATION ON LANDING. THE CREW FOLLOWED MEMORY ITEMS THEN QRH. MESSAGE REMAINED AND EVSC PROCEDURE WAS FOLLOWED. THE ENGINE FIRE BOTTLES WERE BLOWN. MAINTENANCE INSPECTED AND NO ENGINE FIRE WAS DETECTED.
- [SDR C2XA11SH063](https://openairdocs.org/sdr/C2XA11SH063.md): Skin Panel · damaged · Mar 11, 2011 · N29917 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > AC N29917 FERRIED INTO SHV BECAUSE OF GROUND DAMAGE BY LAVATORY TRUCK. SKIN PANEL AT FRAME 61-66 STRINGER 16R TO 19L HAS DAMAGE. FERRY FLIGHT CONDITIONS WERE TO "SECURE BOTH OUTFLOW VALVES, TRIM JAGGED MATERIAL FROM AROUND PUNCTURED AREAS, RE-CONTOUR PUNCTUR
- [SDR C2XA1`0IA283](https://openairdocs.org/sdr/C2XA1%600IA283.md): Ahrs · inoperative · Nov 8, 2010 · N29917 · Emb EMB145LR · Integrated Flight System
  > IAH - FLIGHT 2945, THE CREW REPORTED A AHRS NR 1 FAIL MESSAGE IN FLIGHT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 AHRS UNIT, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED F
- [SDR C2XA10IA187](https://openairdocs.org/sdr/C2XA10IA187.md): Selector · out of position · Jul 4, 2010 · N29917 · Emb EMB145LR · Landing Gear Selector
  > MTY - FLIGHT 2151DURING CLIMB THE CREW RECEIVED A LANDING GEAR DISAGREE MESSAGE AND THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT DIVERTED TO NTY WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE FREE FALL SELECT
- [SDR C2XA10SH223](https://openairdocs.org/sdr/C2XA10SH223.md): Skin · cracked · Jun 29, 2010 · N29917 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > SHV - DURING C CHECK THE RT AFT SKIN WAS FOUND TO BE CRACKED AROUND FASTENERS (4 EACH) BETWEEN FRAMES 78-79 AND STRINGERS 3L-5L. MAINTENANCE REMOVED THE CRACKS AND PERFORMED BUSHING REPAIRS IAW EC5330-02162. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10SH222](https://openairdocs.org/sdr/C2XA10SH222.md): Beam · corroded · Jun 29, 2010 · N29917 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK THE CARGO DOOR CUTOUT LOWER BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10SH200](https://openairdocs.org/sdr/C2XA10SH200.md): Relay · failed · Jun 10, 2010 · N29917 · Emb EMB145LR · Airfoil Anti/De-ice System
  > AIRCRAFT 29917 - FLT 2056 IAH-MCI DIVERT TO SHV - WING ANTI-ICE FAIL MSG DURING TEST. FLIGHT DIVERTED DURING CRUISE. SHV MAINTENANCE REMOVED AND REPLACED RELAY K0528 IAW EMB-145 AMM 20-13-12, PERFORMED ANTI-ICE OPERATIONAL CHECK IAW EMB-145 AMM 30-00-00, OPE
- [SDR C2XA10RI069](https://openairdocs.org/sdr/C2XA10RI069.md): Hose · leaking · May 24, 2010 · N29917 · Emb EMB145LR · Cabin Cooling System
  > FLIGHT 2038 - EWR - FLIGHT CREW REPORTED PACK NR 2 FAIL IN CLIMB. CREW PERFORMED AIR RETURN AND LANDED ACFT UNEVENTFULLY. EWR MX REMOVED AND REPLACED PACK HOSE AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.
- [SDR C2XA10IA056](https://openairdocs.org/sdr/C2XA10IA056.md): Battery · overtemp · Feb 7, 2010 · N29917 · Emb EMB145LR · Battery/Charger System
  > IAH - FLIGHT 2705, DURING TAKEOFF THE CREW REPORTED A BATTERY ONE OVERTEMP INDICATION. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE MAIN BATTERY, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE
- [SDR C2XA09IA327](https://openairdocs.org/sdr/C2XA09IA327.md): Strut · low · Dec 26, 2009 · N29917 · Emb EMB145LR · Nose/Tail Landing Gear
  > IAH - FLIGHT 2573, THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE AND A ENG 1-2 REV DISAGREE MESSAGE ON CLIMB. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE NOSE LANDING GEAR TO REQUI

Next page: https://openairdocs.org/aircraft/N29917/reports.md?page=2

## 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 = 'N29917' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N29917/reports

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