# Service difficulty reports: N13992

A list on [N13992](https://openairdocs.org/aircraft/N13992.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 · 84 reports

- [SDR ASOA201908197097](https://openairdocs.org/sdr/ASOA201908197097.md): Shear Tie · corroded · Aug 19, 2019 · N13992 · Emb EMB145LR · Fuselage Internal Mounting Structure
  > CORROSION ON SHEAR CLIP AT FRAME 61 STRINGER 20R-18R. REMOVED AND REPLACED CORRODED SHEAR CLIP IAW SRM 51-40-02.
- [SDR ASOA201803205084](https://openairdocs.org/sdr/ASOA201803205084.md): Bulb · inoperative · Mar 20, 2018 · N13992 · Emb EMB145LR · Emergency Lighting
  > DURING MX INSPECTION, THE LT OVERWING EMERGENCY LIGHT WAS INOPERATIVE. MX R & R THE BULB, OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA201706273216](https://openairdocs.org/sdr/ASOA201706273216.md): Seat Track · corroded · Jun 27, 2017 · N13992 · Emb EMB145LR · Fuselage, Seat/Cargo Attach Fittings
  > CABIN SEAT TRACK CORRODED RIGHT OTBD NR 3. REPLACED THE SEAT TRACK IAW 53-01-06-400
- [SDR ASOA201706273215](https://openairdocs.org/sdr/ASOA201706273215.md): Seat Track · corroded · Jun 27, 2017 · N13992 · Emb EMB145LR · Fuselage, Seat/Cargo Attach Fittings
  > CABIN NR 6 SEAT TRACK CORRODED. REPLACED IAW SRM 53-01-06-400.
- [SDR ASOA201706263211](https://openairdocs.org/sdr/ASOA201706263211.md): Skin · cracked · Jun 26, 2017 · N13992 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > LEFT FUSELAGE SKIN CRACKED AT FRAME 75, STRINGER 2L. CRACK FOUND DURING NDT INSPECTION. LEFT FUSELAGE SKIN REPAIRED WITH DOUBLER (11" X 9") IAW SRM 53-31-01, ITEM 11, FIG 219, SHEET 1.
- [SDR ASOA201706263210](https://openairdocs.org/sdr/ASOA201706263210.md): Trunnion · cracked · Jun 26, 2017 · N13992 · Emb EMB145LR · Wing, Landing Gear Attach Fittings
  > LEFT MAIN LANDING GEAR AFT UPPER TRUNNION CRACKED. THE TRUNNION WAS REPLACED IAW T1-145-14-018 REV E, AND ETD-2017-145-053707.
- [SDR ASOA201706263209](https://openairdocs.org/sdr/ASOA201706263209.md): Channel · corroded · Jun 26, 2017 · N13992 · Emb EMB145LR · Service Doors
  > SERVICE DOOR CHANNEL CORRODED. SERVICE DOOR CHANNEL REPLACED IAW SRM 51-40-02
- [SDR ASOA201706223208](https://openairdocs.org/sdr/ASOA201706223208.md): Beam · corroded · Jun 22, 2017 · N13992 · Emb EMB145LR · Fuselage Main, Structure
  > CENTER FUSELAGE 4 FLOOR STRUCTURE CENTER BEAM CORRODED AROUND ANCHOR NUT. CENTER BEAM REPAIRED AROUND ANCHOR NUT WITH DOUBLER IAW SRM 53-24-10 ITEM 3 FIG 202.
- [SDR ASOA201706223207](https://openairdocs.org/sdr/ASOA201706223207.md): Gusset · corroded · Jun 22, 2017 · N13992 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > CENTER FUSELAGE FLOOR STRUCTURE LEFT GUSSET UNDER CARBON BEAM CORRODED. LEFT GUSSET BETWEEN FRAME 59 AND 61 REPLACED IAW SRM 51-40-02.
- [SDR ASOA201706223206](https://openairdocs.org/sdr/ASOA201706223206.md): Gusset · corroded · Jun 22, 2017 · N13992 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > CENTER FUSELAGE 4 FLOOR STRUCTURE MID GUSSET CORRODED. MID GUSSET WAS REPLACED IAW SRM 51-40-02.
- [SDR ASOA201706223205](https://openairdocs.org/sdr/ASOA201706223205.md): Window Frame · cracked · Jun 22, 2017 · N13992 · Emb EMB145LR · Fuselage Main, Structure
  > FRAME CRACKED TOP FORWARD CO-PILOT SLIDING WINDOW. SLIDING WINDOW UPPER LATERAL FRAME WAS REPLACED AS PER SRM 51-40-02.
- [SDR ASOA201706223204](https://openairdocs.org/sdr/ASOA201706223204.md): Trunnion · cracked · Jun 22, 2017 · N13992 · Emb EMB145LR · Wing, Landing Gear Attach Fittings
  > RIGHT MAIN GEAR AFT UPPER TRUNNION CRACKED. THE TRUNNION WAS REPLACED IAW T1-145-14-018R/H, AND ETD 2017-145-67014-608.
- [SDR ASOA201704305070](https://openairdocs.org/sdr/ASOA201704305070.md): Lamp · inoperative · Apr 30, 2017 · N13992 · Emb EMB145LR · Emergency Lighting
  > DURING MX INSPECTION, THE CABIN OVERHEAD LIGHT AT ROW 7 WAS INOPERATIVE. MX REPLACED THE LAMPS AND OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA201704055035](https://openairdocs.org/sdr/ASOA201704055035.md): Cradle · burned · Apr 5, 2017 · N13992 · Emb EMB145LR · Emergency Equipment
  > CREW REPORTED A BURNING ODOR, FOLLOWED BY LOSS OF CA'S AIRSPEED INDICATOR, ALTIMETER, AND SPS. ADVANCED ON EICAS DURING FLIGHT. MX FOUND BURNING ODOR TO BE F/A'S FWD FLASHLIGHT BURNED AND BROKEN. REMOVED AND REPLACED THE FLASHLIGHT HOLDER.
- [SDR ASOA201610234078](https://openairdocs.org/sdr/ASOA201610234078.md): Acm · frozen · Oct 23, 2016 · N13992 · Emb EMB145LR · Cabin Cooling System
  > FLIGHT 3888 THE CREW REPORTED SMOKE IN THE CABIN IN CRUISE FLIGHT AT FL250. THE SMOKE DISSIPATED AFTER APPROXIMATELY 15 SECONDS. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE L
- [SDR ASOA20160406015](https://openairdocs.org/sdr/ASOA20160406015.md): Fmu · failed · Apr 6, 2016 · N13992 · Emb EMB145LR · Fuel Controlling System
  > PILOT REPORTED A NR 2 ENGINE OUT MESSAGE ENGINE UNCOMMANDED SHUTDOWN, DID NOT INDICATE ON GROUND OR IN FLIGHT. MAINTENANCE INSPECTED AND FOUND DEBRIS IN FUEL FILTER AND BOWL THEN R & R ENGINE NR 2 FMPU WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SER
- [SDR ASOA20150621031R](https://openairdocs.org/sdr/ASOA20150621031R.md): Light · inoperative · Jun 21, 2015 · N13992 · Emb EMB145LR · Emergency Lighting
  > DURING MAINTENANCE INSPECTION, THE FLOOR EMERGENCY LIGHT STRIP AT SEATS 7 & 8A WAS FOUND INOPERATIVE. MAINTENANCE R & R THE LIGHT STRIP WITH OPS CHECK GOOD. AIRCRAFT WAS APRROVED FOR RETURN TO SERVICE.
- [SDR ASOA20150413094](https://openairdocs.org/sdr/ASOA20150413094.md): Rib · cracked · Apr 13, 2015 · N13992 · Emb EMB145LR · Wing, Rib/Bulkhead
  > DURING C-CHECK, RIB 21 ON RT WING INSIDE PANEL 651CB IS CRACKED. MAINTENANCE REPAIRED RT WING RIB 21 IAW EC 5720-01201. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20150409092](https://openairdocs.org/sdr/ASOA20150409092.md): Skin · corroded · Apr 9, 2015 · N13992 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > DURING C-CHECK, FUSELAGE SKIN CORRODED BETWEEN FRAME 57-58, STR 20R-19R. REPAIRED SKIN IAW EC5330-03001. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20150409091](https://openairdocs.org/sdr/ASOA20150409091.md): Door Sill · corroded · Apr 9, 2015 · N13992 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING C-CHECK, SERVICE DOOR AFT SILL CORRODED. REPAIRED SERVICE DOOR SILL IAW SRM 53-21-10. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20150409090](https://openairdocs.org/sdr/ASOA20150409090.md): Skin · cracked · Apr 9, 2015 · N13992 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > DURING C-CHECK, SKIN CRACKS AROUND RIVETS FRAME 75 STR 2R-3R. REPAIRED SKIN CRACKS IAW EC5330-02997. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20150409089](https://openairdocs.org/sdr/ASOA20150409089.md): Skin · cracked · Apr 9, 2015 · N13992 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > DURING C-CHECK, SKIN CRACKS AROUND RIVETS FRAME 78, STR 3L-5L. REPAIRED SKIN CRACKS AROUND RIVETS IAW EC 5330-03000. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20150409088](https://openairdocs.org/sdr/ASOA20150409088.md): Frame · cracked · Apr 9, 2015 · N13992 · Emb EMB145LR · Fuselage Main, Frame
  > DURING C-CHECK, FRAME 25 CRACKED AT STR 15R-16R. REPAIRED FRAME 25 IAW SRM 53-00-04. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140626086](https://openairdocs.org/sdr/ASOA20140626086.md): Smoke Warning · false activation · Jun 26, 2014 · N13992 · Emb EMB145LR · Smoke Detection
  > DURING DESCENT THE CREW REPORTED A LAVATORY SMOKE WARNING ON EICAS WITH NO SIGN OF SMOKE IN LAVATORY. THE CREW DEACTIVATED TWO CIRCUIT BREAKERS IAW THE QRH AND THE ACFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE ACFT WITH NO SIGN OF SMOKE OR ODOR DET
- [SDR ASOA20130720076](https://openairdocs.org/sdr/ASOA20130720076.md): Transducer · faulty · Jul 20, 2013 · N13992 · Emb EMB145LR · Landing Gear Position and Warning
  > CREW REPORTED THE RT BRAKES NOT WORKING ON LANDING, ACFT PULLED TO THE LEFT AND TOWER SAW SMOKE FROM THE RT MLG DURING LANDING. MX R & R NR 3 WHEEL SPEED TRANSDUCER AND HUB CAP ASSY. HIGH SPEED TAXI AND OPS CHECKS SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO
- [SDR ASOA20130607318](https://openairdocs.org/sdr/ASOA20130607318.md): Flap System · out of rig · Jun 7, 2013 · N13992 · Emb EMB145LR · Trailing Edge Flap Control System
  > FLAP FAIL MESSAGE INFLIGHT. PERFORMED FLAP RIGGING. OPS CHECK GOOD, ACFT RELEASED AND RETURNED TO SERVICE.
- [SDR ASOA20130421134](https://openairdocs.org/sdr/ASOA20130421134.md): Shear Tie · corroded · Apr 19, 2013 · N13992 · Emb EMB145LR · Fuselage Internal Mounting Structure
  > DURING C-CHECK THE FRAME 65 SHEAR TIE AT THE CARGO DOOR CUTOUT WAS FOUND TO BE CORRODED. MX REMOVED THE CORROSION AND PERFORMED A SPLICE REPAIR IAW EC5320-01494. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130421133](https://openairdocs.org/sdr/ASOA20130421133.md): Frame · corroded · Apr 19, 2013 · N13992 · Emb EMB145LR · Fuselage Main, Frame
  > DURING C-CHECK, FRAME 65 WAS FOUND TO BE CORRODED BETWEEN STRINGERS 15L-16L. MX REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5310-01505. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130421132V](https://openairdocs.org/sdr/ASOA20130421132V.md): Beam · corroded · Apr 19, 2013 · N13992 · Emb EMB145LR · Fuselage Main, Structure
  > DURING C-CHECK, THE CARGO DOOR LOWER BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 65-68 AND STRINGERS 15L-16L. MX R & R THE BEAM IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130315016C](https://openairdocs.org/sdr/ASOA20130315016C.md): Fan · faulty · Mar 15, 2013 · N13992 · Emb EMB145LR · Air Distribution Fan
  > THE CREW REPORTED A ELECTRICAL BURNING ODOR IN THE CABIN. MX INSPECTED AND REPLACED THE NR 1 PACK RECIRCULATION FAN. OPS CHECKS WERE GOOD.
- [SDR ASOA20120813111](https://openairdocs.org/sdr/ASOA20120813111.md): Inverter · inoperative · Aug 13, 2012 · N13992 · Emb EMB145LR · Emergency Lighting
  > DURING MX INSPECTION, THE AISLE PATH LIGHTING FROM ROW 3 TO 7 WERE FOUND TO BE INOPERATIVE. MX R & R THE NR 3 EMERGENCY LIGHT INVERTER, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA11CL133](https://openairdocs.org/sdr/C2XA11CL133.md): Smoke Detector · faulty · May 22, 2011 · N13992 · Emb EMB145LR · Smoke Detection
  > ORD FLT 5904 THE CREW REPORTED A LAV SMOKE INOPERATIVE MESSAGE. MAINTENANCE INSPECTED AND REPLACED THE LAV SMOKE DETECTOR. OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA11TY054](https://openairdocs.org/sdr/C2XA11TY054.md): Door Frame · damaged · May 1, 2011 · N13992 · Emb EMB145LR · Fuselage Main, Structure
  > SERVICE DOOR STRUCTURE FOR DOOR STOPS 3.9 AND 3.10 REQUIRE MOUNT HOLES TO BE REWORKED FOR SB145-53-0031. SERVICE DOOR FRAME STOP BACKUP STRUCTURE POSITION 3.9 AFT AND 3.10 AFT HOLE ELONGATED. REMOVED AND REPLACED DAMAGED SECTION OF FRAME 22 AND BACKUP STRUCT
- [SDR C2XA11TY032](https://openairdocs.org/sdr/C2XA11TY032.md): Smoke Detector · defective · Mar 19, 2011 · N13992 · Emb EMB145LR · Smoke Detection
  > THE FORWARD SMOKE DETECTOR IN CARGO HAS A STEADY LIGHT ON. REMOVED AND REPLACED DETECTOR IAW EMB 145 AMM 26-15-01. OPS CHECK GOOD.
- [SDR C2XA11TY026](https://openairdocs.org/sdr/C2XA11TY026.md): A/C Pack · overheated · Mar 2, 2011 · N13992 · Emb EMB145LR · Cabin Cooling System
  > DURING TAXI PACK 1 OVERHEAT RESULTED IN SMOKE IN THE CABIN. PLACED PACK 1 ON MEL.
- [SDR C2XA11CL066](https://openairdocs.org/sdr/C2XA11CL066.md): Acm · failed · Mar 2, 2011 · N13992 · Emb EMB145LR · Cabin Cooling System
  > BNA FLT 6097 THE CREW REPORTED PACK NR 1 OVERHEAT AND SMOKE IN THE CABIN. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED AND PLACED NR 1 PACK ON MEL. ON 3/10 MAINTENANCE REPLACED THE NR 1 AIR CYCLE MACHINE. OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA10CL166](https://openairdocs.org/sdr/C2XA10CL166.md): Light · inoperative · Nov 1, 2010 · N13992 · Emb EMB145LR · Emergency Lighting
  > DURING ROUTINE MAINTENANCE THE EMERGENCY AISLE PATH LIGHT STRIP AT SEAT 12A WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE LIGHT STRIP AT SEAT 12A.OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA10IA218](https://openairdocs.org/sdr/C2XA10IA218.md): Light · inoperative · Aug 3, 2010 · N13992 · Emb EMB145LR · Emergency Lighting
  > IAH - FLIGHT 2044, DURING PREFLIGHT INSPECTION THE CREW REPORTED THE EMERGENCY LIGHT STRIP AT ROW 12A WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO
- [SDR C2XA10CL065](https://openairdocs.org/sdr/C2XA10CL065.md): Engine · faulty · May 1, 2010 · N13992 · Emb EMB145LR · Engine (Turbine/Turboprop)
  > MHT-CLE FLT 2582 THE CREW REPORTED A PUNGENT ODOR FROM THE PACKS THROUGHOUT THE ENTIRE FLIGHT. MAINTENANCE REPLACED THE NR 1 ENGINE AND OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA10RI043](https://openairdocs.org/sdr/C2XA10RI043.md): Fadec · defective · Mar 17, 2010 · N13992 · Emb EMB145LR · Fuel Control/Turbine Engines
  > FLIGHT 2882 - FLIGHT CREW REPORTED PARTIAL LOSS OF POWER ON ENGINE 1, 2 TIMES IN FLIGHT. DURING CRUISE, N1 WENT DOWN TO 67 PERCENT, IGN A AND B CAME ON AND RESTORED POWER ALSO ENGINE 1 SHORT DISPATCH ON EICAS. EWR MX REMOVED FADEC 1A AND 1B AND PERFORMED OPE
- [SDR C2XA10RI042](https://openairdocs.org/sdr/C2XA10RI042.md): Fadec · defective · Mar 17, 2010 · N13992 · Emb EMB145LR · Fuel Control/Turbine Engines
  > FLIGHT 2882 - FLIGHT CREW REPORTED PARTIAL LOSS OF POWER ON ENGINE 1, 2 TIMES IN FLIGHT. DURING CRUISE, N1 WENT DOWN TO 67 PERCENT, IGN A AND B CAME ON AND RESTORED POWER ALSO ENGINE 1 SHORT DISPATCH ON EICAS. EWR MX REMOVED FADEC 1A AND 1B AND PERFORMED OPE
- [SDR C2XA10IA098](https://openairdocs.org/sdr/C2XA10IA098.md): Fadec · malfunctioned · Mar 14, 2010 · N13992 · Emb EMB145LR · Fuel Control/Turbine Engines
  > IAW - FLIGHT 2758, THE CREW REPORTED THAT ENGINE 1 SURGES IN FLIGHT. CRUISE THRUST N1 FLUCTUATES =/-15 PERCENT WITH AN ITT RISE AND FALL; N1 REQUEST CARAT ALSO FLUCTUATES =/- 15 PERCENT, AND THE CRZ THRUST SETTING AUTO ADVANCED TO TO1. ENGINE 1 FADEC AUTO AL
- [SDR C2XA09CL162](https://openairdocs.org/sdr/C2XA09CL162.md): Wire Harness · burned · Dec 13, 2009 · N13992 · Emb EMB145LR · Light System Wiring
  > SDF FLT 2343 THE CREW REPORTED UPON LANDING NOTICED ELECTRICAL/SMOKE SMELL COMING FROM OVERHEAD PANEL AT SEAT 1A. MAINTENANCE INSPECTED AND REPLACED THE SIDEWALL LIGHT HARNESS AT SEAT 1A. OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA09CL125](https://openairdocs.org/sdr/C2XA09CL125.md): Apu · malfunctioned · Sep 28, 2009 · N13992 · Emb EMB145LR · APU Core Engine
  > CLE FLT 2698 - THE CREW REPORTED A PLASTIC BURNING SMELL IN THE CABIN DURING CLIMB. MAINTENANCE INSPECTED AND REPLACED THE APU. OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA09RI165](https://openairdocs.org/sdr/C2XA09RI165.md): Unknown · odor · Sep 19, 2009 · N13992 · Emb EMB145LR · Air Distribution System
  > FLIGHT 2393 - EWR - FLIGHT CREW REPORTED STRONG ODOR WHEN PACKS ARE ON IN COCKPIT. EWR MX PERFORMED OPERATIONAL CHECK FOR PACK SYSTEM IAW EMB-145 AMM 21-51-00 AND OPERATIONAL CHECK FOR APU AND ENGINE BLEED SYSTEM IAW EMB-145 AMM 36-00-00 OPERATION CHECK GOOD.
- [SDR C2XA09SH173](https://openairdocs.org/sdr/C2XA09SH173.md): Beam · corroded · Jun 12, 2009 · N13992 · Emb EMB145LR · Fuselage Main, Structure
  > SHV. DURING C-CK. CARGO DOOR LOWER CUTOUT BEAM HAS CORROSION. REMOVED AND REPLACED CARGO DOOR LOWER CUTOUT BEAM IAW EMB 145 SRM 51-40-02. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09SH172](https://openairdocs.org/sdr/C2XA09SH172.md): Floor Support · corroded · Jun 12, 2009 · N13992 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV. DURING C-CHECK. RT OMEGA BEAM HAS CORROSION AT FR 22. REPAIRED RT OMEGA BEAM AT FR 22 IAW IC2009-145/04543. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09CL043](https://openairdocs.org/sdr/C2XA09CL043.md): Turbine Wheel · cracked · Apr 11, 2009 · N13992 · Emb EMB145LR · Turbine Section
  > DURING COMPLIANCE OF SB AE3007A-72-368 ON THE NR 1 ENGINE A CRACK INDICATION OF THE 2ND STAGE HIGH PRESSURE TURBINE WHEEL WAS FOUND WHILE PERFORMING THE ULTRASOUND INSPECTION. THE NR 1 ENGINE WAS REPLACED.
- [SDR C2XA09CL021](https://openairdocs.org/sdr/C2XA09CL021.md): Indicator · faulty · Feb 23, 2009 · N13992 · Emb EMB145LR · Fuel Flow Indicating
  > CLE FLIGHT 2341 - THE CREW REPORTED A ENGINE NR 1 FUEL IMPENDING BYPASS INDICATION ON CLIMBOUT. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 1 ENGINE FUEL FILTER AND THE NR 1 ENGINE FUEL IMPENDING BYPASS
- [SDR C2XA09RI001](https://openairdocs.org/sdr/C2XA09RI001.md): Bleed Valve · inoperative · Jan 2, 2009 · N13992 · Emb EMB145LR · Compressor Bleed Valve
  > BNA - FLIGHT 2573 - FLIGHT CREW REPORTED ENGINE NR 1 BLEED VALVE CLOSED IN FLIGHT AND THEY WERE UNABLE TO REOPEN. CREW PERFORMED AIR RETURN AND LANDED ACFT UNEVENTFULLY. MX R&R ENGINE BLEED VALVE AND PERFORMED OPS CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RET

Next page: https://openairdocs.org/aircraft/N13992/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 = 'N13992' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N13992/reports

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