# Service difficulty reports: N153GL

A list on [N153GL](https://openairdocs.org/aircraft/N153GL.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 · 96 reports

- [SDR GLBA2016060100590](https://openairdocs.org/sdr/GLBA2016060100590.md): Downlock Switch · inoperative · May 31, 2016 · N153GL · Beech 1900D · Landing Gear Position and Warning
  > PILOT REPORTED THAT THEY HAD NO NLG INDICATIONS ON GEAR EXTENSION, RAN ABNORMAL CHECKLIST, DECLARED AN EMER & LANDED WITHOUT INCIDENT. R & R THE NOSE GEAR DRAG BRACE DOWN LOCK SWITCH IAW TC 1900-3220.0 REV 1 STEPS 3,4, & 21. PERFORMED GEAR SWING, OPERATIONS
- [SDR GLBA2016041400580](https://openairdocs.org/sdr/GLBA2016041400580.md): Unknown · malfunctioned · Apr 14, 2016 · N153GL · Beech 1900D · Propeller Feathering/Reversing
  > PILOT REPORTED THAT THEY HAD UNSCHEDULED AUTOFEATHER CYCLING ON FINAL. PERFORMED AUTOFEATHER OPERATIONAL CHECKS & COULD NOT DUPLICATE DISCREPANCY SIGNED OFF USING REF 1900DMM 61-21-00. OPERATIONS CHECKED GOOD.
- [SDR GLBA2015010800490](https://openairdocs.org/sdr/GLBA2015010800490.md): Skin · damaged · Jan 8, 2015 · N153GL · Beech 1900D · Elevator, Plate/Skin
  > DURING A SCHEDULED INSPECTION FOUND A BURN HOLE IN THE RT ELEVATOR TOP OTBD SKIN TE 1.5 INCH WIDE BY.75 INCHES LONG IN AN EXISTING PATCH. HOLE IS 4.5 INCHES FROM OTBD TIP &.5 INCHES FROM THE TE. REPAIRED IAW EO 14-120-53-002.
- [SDR GLBA2014122400486](https://openairdocs.org/sdr/GLBA2014122400486.md): Strut · low pressure · Dec 22, 2014 · N153GL · Beech 1900D · Passenger/Crew Doors
  > THE CABIN DOOR SNUBBER IS READING 200 PSI LOW & THE DOOR IS HARD TO CLOSE. SERVICED THE CABIN DOOR STRUT AS NEEDED IAW AIM 3 4 0 STEP 23. OPERATIONS CHECKED GOOD.
- [SDR GLBA2014112400468](https://openairdocs.org/sdr/GLBA2014112400468.md): Skin · dented · Nov 23, 2014 · N153GL · Beech 1900D · Horizontal Stabilizer, Plate/Skin
  > MAJOR REPAIR. DURING A SCHEDULED INSPECTION FOUND DENT IN THE RT HORIZONTAL STAB LE 3.25 INCHES BY 1.375 INCHES, DENT AT HSS 58.00, DENT LOCATED AT RIB AREA, SMALLER DENT OTBD OF DENT AT HSS 58.00, APPROX AT HSS 61.00, 2 INCHES BY 1.5 INCHES, DUE TO BIRD STR
- [SDR GLBA2014021400384](https://openairdocs.org/sdr/GLBA2014021400384.md): Frame · cracked · Feb 13, 2014 · N153GL · Beech 1900D · Fuselage Main, Frame
  > DURING A SCHEDULED INSPECTION MAINTENANCE FOUND A CRACK AT FS 456 LT SIDE LOWER FRAME, 1.5 INCHES IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-53-011.
- [SDR GLBA2014021000377](https://openairdocs.org/sdr/GLBA2014021000377.md): Door Frame · cracked · Feb 8, 2014 · N153GL · Beech 1900D · Fuselage Main, Structure
  > DURING A SCHEDULED INSPECTION MX FOUND A CRACK IN THE CARGO DOOR AFT LOWER FRAME AT FS 509.50 AT THE INTERSECTION OF THE LOWER SILL, 1" IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-53-006.
- [SDR GLBA2013121600360](https://openairdocs.org/sdr/GLBA2013121600360.md): Unknown · odor · Dec 15, 2013 · N153GL · Beech 1900D · Air Distribution System
  > PILOT REPORTED THAT THERE WAS A HOT ELEC SMELL COMING FROM THE FIRST OFFICER'S SIDE OF THE COCKPIT, POSSIBLE FROM THE CB PANEL. INSPECTED BEHIND THE CB PANEL, PULLED UP FLOORBOARDS, RAN ENG NO DISCREPANCIES OR ABNORMAL ODORS NOTED.
- [SDR GLBA2013100400335](https://openairdocs.org/sdr/GLBA2013100400335.md): Structure · cracked · Oct 4, 2013 · N153GL · Beech 1900D · Horizontal Stabilizer Structure
  > DURING A SCHEDULED INSPECTION, FOUND CRACK IN THE HORIZONTAL STABILIZER LT LOWER TEE SECTION AT HSS 0.00,.5" IN LENGTH. REPAIRED IAW EO 13-1900-55-024.
- [SDR GLBA2013100200332](https://openairdocs.org/sdr/GLBA2013100200332.md): Frame · cracked · Oct 1, 2013 · N153GL · Beech 1900D · Fuselage Main, Frame
  > DURING A SCHEDULED INSPECTION, FOUND A CRACK IN THE FUSELAGE FRAME ANGLE IN THE BEND RADIUS AT FS 451 AND STRINGER 10R,.875 INCH IN LENGTH. REPAIRED IAW EO 13-1900-53-068. MAJOR REPAIR.
- [SDR GLBA2013100200330](https://openairdocs.org/sdr/GLBA2013100200330.md): Frame · cracked · Oct 1, 2013 · N153GL · Beech 1900D · Fuselage Main, Frame
  > DURING A SCHEDULED INSPECTION FOUND A CRACK BS 107 AND STRINGER 8R FRAME, 0.5 INCH IN LENGTH. REPAIRED IAW EO 13-1900-53-070. MAJOR REPAIR.
- [SDR GLBA2013100200331](https://openairdocs.org/sdr/GLBA2013100200331.md): Frame · cracked · Oct 1, 2013 · N153GL · Beech 1900D · Fuselage Main, Frame
  > DURING A SCHEDULED INSPECTION, FOUND A CRACK IN THE FRAME LT SIDE OF FS 107 BY STRINGER 8L,.125 INCH IN LENGTH. REPAIRED IAW EO 13-1900-53-069. MAJOR REPAIR.
- [SDR GLBA2013100200333](https://openairdocs.org/sdr/GLBA2013100200333.md): Frame · cracked · Oct 1, 2013 · N153GL · Beech 1900D · Fuselage Main, Frame
  > DURING A SCHEDULED INSPECTION FOUND TWO CRACKS IN FUSELAGE FRAME, STRINGER 8L BS 438.25,.999 INCH IN LENGTH. REPAIRED IAW EO 13-1900-53-067. MAJOR REPAIR.
- [SDR GLBA2013100200329](https://openairdocs.org/sdr/GLBA2013100200329.md): Skin · cracked · Oct 1, 2013 · N153GL · Beech 1900D · Fuselage Main, Plate/Skin
  > DURING A SCHEDULED INSPECTION, FOUND TWO CRACKS IN FUSELAGE SKIN, PROTRUDING OUT OF 2 RIVETS AT FS 150.6 STRINGER 1, 0.5 INCH IN LENGTH. REPAIRED IAW EO 13-1900-53-071. MAJOR REPAIR.
- [SDR GLBA2013100200328](https://openairdocs.org/sdr/GLBA2013100200328.md): Frame · cracked · Oct 1, 2013 · N153GL · Beech 1900D · Fuselage Main, Frame
  > DURING A SCHEDULED INSPECTION, FOUND TWO CRACKS IN THE FUSELAGE FRAME ON EITHER SIDE OF STRINGER 2L AT FS 378.25, ONE INCH IN LENGTH. REPAIRED IAW EO 13-1900-53-072. MAJOR REPAIR.
- [SDR GLBA2013100200327](https://openairdocs.org/sdr/GLBA2013100200327.md): Spar Cap · cracked · Oct 1, 2013 · N153GL · Beech 1900D · Horizontal Stabilizer, Spar/Rib
  > DURING A SCHEDULED INSPECTION, FOUND A CRACK IN THE RT FWD SPAR CAP ANGLE ON THE VERTICAL STAB 2ND FROM TOP RIVET,.125 INCHES IN LENGTH. REPAIRED IAW EO 13-1900-55-023. MAJOR REPAIR.
- [SDR GLBA2013100200326](https://openairdocs.org/sdr/GLBA2013100200326.md): Structure · cracked · Sep 30, 2013 · N153GL · Beech 1900D · Emergency Exits
  > DURING A SCHEDULED INSPECTION, FOUND A CRACK IN THE EXIT DOOR 4C, UPPER FWD CORNER, 1.5 INCHES IN LENGTH. REPAIRED IAW EO 13-1900-52-002. MAJOR REPAIR.
- [SDR GLBA2013031900214](https://openairdocs.org/sdr/GLBA2013031900214.md): Web · cracked · Mar 19, 2013 · N153GL · Beech 1900D · Horizontal Stabilizer Structure
  > DURING A SCHEDULED ROUTINE INSPECTION, FOUND TWO CRACKS IN THE HORIZONTAL STAB AFT WEB AT THE 10 & 2 O'CLOCK POSITION AROUND THE ACCESS HOLE,.15" IN LENGTH. REPAIRED IAW EO 13-1900-55-007. MAJOR REPAIR.
- [SDR GLBA2013031800213](https://openairdocs.org/sdr/GLBA2013031800213.md): Spar Cap · cracked · Mar 18, 2013 · N153GL · Beech 1900D · Vertical Stabilizer, Spar/Rib
  > DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE VERTICAL STABILIZER LT SPAR CAP ANGLE AT 20 PERCENT CHORD AT FSS 84.10, GOING THROUGH THE THIRD FASTENER FROM THE TOP (SECOND FASTENER BELOW THE HAT SECTION) IN THE AREA OF THE HORIZONTAL STAB ATTACH
- [SDR GLBA2013021500177](https://openairdocs.org/sdr/GLBA2013021500177.md): Bulb · inoperative · Feb 14, 2013 · N153GL · Beech 1900 · Emergency Lighting
  > PILOT REPORTED THAT THE EMERGENCY LIGHTS ON THE F/O'S SIDE DO NOT ILLUMINATE AND ARE ALSO INOPERATIVE IN INDIRECT LIGHT MODE. MX REPLACED THE BULBS AND SECURED WIRING, OPS CHECKED GOOD.
- [SDR GLBA2012122600144](https://openairdocs.org/sdr/GLBA2012122600144.md): Wire · broken · Dec 25, 2012 · N153GL · Beech 1900D · Light System Wiring
  > PILOT REPORTED THE THE F/O'S EMERGENCY LIGHTS ARE INOPERATIVE. MX REPLACED THE BULB AND REPAIRED A WIRE, OPS CHECKED GOOD.
- [SDR GLBA2012101800080](https://openairdocs.org/sdr/GLBA2012101800080.md): Warning Light · illuminated · Oct 18, 2012 · N153GL · Beech 1900D · Door Warning System
  > PILOT REPORTED THAT THE CARGO DOOR CAME OPEN IN FLIGHT, LANDED SAFELY. MAINTENANCE REPLACED ALL PARTS AND FRAMES REQ IAW SRM, OPS CHECKED FLIGHT SAT.
- [SDR GLBA2012100500076](https://openairdocs.org/sdr/GLBA2012100500076.md): Structure · damaged · Oct 5, 2012 · N153GL · Beech 1900D · Wing Main, Frame Structure
  > BIRD STRIKE ON LT OTBD WING FROM WS 192.74 TO APPROX 201.74, APPROX.5" IN DEPTH. REPAIRED IAW EO 12-1900-57-011. MAJOR REPAIR
- [SDR GLBA2012091000049](https://openairdocs.org/sdr/GLBA2012091000049.md): Spar Cap · cracked · Sep 7, 2012 · N153GL · Beech 1900D · Horizontal Stabilizer, Spar/Rib
  > DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE VERTICAL STAB LT SPAR CAP ANGLE AT 20 PERCENT CHORD AT VSS 84.10,.75" IN LENGTH. REPAIRED IAW FR-CO002516R1, STEP 1. MAJOR REPAIR.
- [SDR GLBA2012070500010](https://openairdocs.org/sdr/GLBA2012070500010.md): Rib · cracked · Jul 5, 2012 · N153GL · Beech 1900D · Wing, Rib/Bulkhead
  > DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE LT INBD WING AUX RIB AT WS 29.00 AND FS 288, 1.1" IN LENGTH. REPAIRED THE AFFECTED AREA IAW EO 12-1900-57-006.
- [SDR GLBA2012062700007](https://openairdocs.org/sdr/GLBA2012062700007.md): Skin · cracked · Jun 27, 2012 · N153GL · Beech 1900D · Fuselage Main, Plate/Skin
  > DURING A SCHEDULED ROUTINE INSPECTION FOUND THE SKIN CRACKED IN THE UPPER CABIN FUSELAGE AT FS 273.25, BETWEEN STRINGER 1 AND 2R, CRACK IS ALONG A ROW OF FASTENERS, 3.65" IN LENGTH. REPAIRED THE AFFECTED AREA IAW EO12-1900-53-037.
- [SDR GLBA2012062600006](https://openairdocs.org/sdr/GLBA2012062600006.md): Skin · cracked · Jun 26, 2012 · N153GL · Beech 1900D · Fuselage Main, Plate/Skin
  > DURING A SCHEDULED ROUTINE INSPECTION, FOUND THE SKIN CRACKED AT THE EMERGENCY EXIT DOOR 6C SKIN AT THE LWR AFT CORNER, 2" IN LENGTH. REPAIRED THE AFFECTED AREA IAW EO 12-1900-52-001.
- [SDR GLBA2012062600005](https://openairdocs.org/sdr/GLBA2012062600005.md): Skin · cracked · Jun 26, 2012 · N153GL · Beech 1900D · Fuselage Main, Plate/Skin
  > DURING A SCHEDULED ROUTINE INSP, FOUND A CRACK IN THE BELLY SKIN AT FS 303, IB 2.5" FROM SKIN EDGE, 4.25" IN LENGTH. REPAIRED THE AFFECTED AREA IAW EO 12-1900-53-036.
- [SDR GLBA2012062500002](https://openairdocs.org/sdr/GLBA2012062500002.md): Door Frame · cracked · Jun 25, 2012 · N153GL · Beech 1900D · Fuselage Main, Structure
  > DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE UPPER CARGO DOOR FRAME ON THE FWD SIDE AT APPROX FS 459, 3" IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 12-1900-53-033. MATERIALS UTILIZED ARE INCLUDED IN
- [SDR GLBA201206250004](https://openairdocs.org/sdr/GLBA201206250004.md): Pressure Blkhd · cracked · Jun 25, 2012 · N153GL · Beech 1900D · Fuselage Main, Bulkhead
  > DURING A SCHEDULED ROUTINE INSP, FOUND A CRACK IN THE FWD LWR LT PRESSURE BULKHEAD AT FS 84, 2" IN LENGTH. REPAIRED THE AFFECTED AREA IAW EO 12-1900-53-034.
- [SDR GLBA2012062500003](https://openairdocs.org/sdr/GLBA2012062500003.md): Bulkhead · cracked · Jun 25, 2012 · N153GL · Beech 1900D · Fuselage Main, Bulkhead
  > DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE FWD LWR RT PRESSURE BULKHEAD AT FS 84, 1" IN LENGTH. REPAIRED THE AFFECTED AREA IAW EO 12-1900-53-035.
- [SDR GLBA2012062500001](https://openairdocs.org/sdr/GLBA2012062500001.md): Door Frame · cracked · Jun 25, 2012 · N153GL · Beech 1900D · Fuselage Main, Structure
  > DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE UPPER CARGO DOOR FRAME ON THE FWD SIDE AT APPROX FS 459, 3" IN LENGTH.
- [SDR GLBA2012040201](https://openairdocs.org/sdr/GLBA2012040201.md): Engine · failed · Apr 1, 2012 · N153GL · Beech 1900D · Engine (Turbine/Turboprop)
  > PILOT REPORTED THAT AFTER TAKEOFF AT 5000 FT, NR 1 ENGINE SHUTDOWN, RAN CHECKLIST, DECLARED EMERGENCY, RETURNED TO DEPARTURE, MANUALLY FEATHER NR 1 PROP. MX R & R LT ENGINE, PWR SEC AND GAS GENERATOR, IAW TC 1900-7100-00, OPS CHECKED GOOD.
- [SDR GLBA20111114F](https://openairdocs.org/sdr/GLBA20111114F.md): Pressure Switch · inoperative · Nov 12, 2011 · N153GL · Beech 1900D · Propeller Feathering/Reversing
  > RIGHT AUTOFEATHER WILL NOT TEST DURING RUN UP. MX REPLACED THE RT ENGINE AUTOFEATHER LOW PRESSURE SWITCH.
- [SDR GLBA20111101G](https://openairdocs.org/sdr/GLBA20111101G.md): Pump · leaking · Oct 30, 2011 · N153GL · Beech 1900D · Fuel Boost Pump
  > PILOT REPORTED THAT THERE WAS A FUEL LEAK ON THE LT ENGINE. MX REPLACED THE LP FUEL PUMP.
- [SDR GLBA20111017H](https://openairdocs.org/sdr/GLBA20111017H.md): Line · leaking · Oct 15, 2011 · N153GL · Beech 1900D · Aircraft Fuel Distribution System
  > PILOT REPORTED THAT FUEL WAS LEAKING FROM THE BOTTOM OF THE ENGINE. MX TIGHTED A LOOSE FUEL LINE, LEAK AND OPS CHECKED GOOD.
- [SDR GLBA20110926G](https://openairdocs.org/sdr/GLBA20110926G.md): Pcb · inoperative · Sep 23, 2011 · N153GL · Beech 1900D · Propeller Feathering/Reversing
  > PILOT REPORTED THAT DURING THE PROP OVERSPEED TEST ON THE RT SIDE THE AFX DISABLE LIGHT ILLUMINATED. MX REPLACED THE AFX PCB IAW MI 24-01 AND BMM 61-21-00, PN: 129-364091-9 SN: 742-D-96, OPS CK GOOD.
- [SDR GLBA20110919F](https://openairdocs.org/sdr/GLBA20110919F.md): Life Vest · torn · Sep 16, 2011 · N153GL · Beech 1900D · Life Jacket
  > PILOT REPORTED THAT THE CAPT'S LIFE PRESERVER POUCH IS RIPPED. MX REPLACE THE PRESERVER.
- [SDR GLBA20110831H](https://openairdocs.org/sdr/GLBA20110831H.md): Fire Warning · illuminated · Aug 30, 2011 · N153GL · Beech 1900D · Fire Detection
  > PILOT REPORTED THAT WHILE CLIMBING THE MASTER WARNING AND NR 2 T-HANDLE ILLUMINATED, EMERGENCY DECLARED, NR 2 ENGINE WAS SHUTDOWN, LANDED WITHOUT INCIDENT. MX REPLACED PCB E173 IAW MI 24-01 PN: 129-364037-1 SN: 657-I-86 AND FWD & AFT FIRELOOPS IAW 26-10-01 PN
- [SDR GLBA20110830G](https://openairdocs.org/sdr/GLBA20110830G.md): Exhaust Stack · cracked · Aug 30, 2011 · N153GL · Beech 1900D · Engine Collector/Tailpipe/Nozzle
  > "SUP" - SIG EVENT - PILOT REPORTED THAT THE NR2 T-HANDLE ILLUMINATED IN FLIGHT, NO INDICATION OF A FIRE WAS VISIBLE, WITH NO ABNORMAL ENGINE INDICATIONS NOTED. MX FOUND EVIDENCE OF AN EXHAUST LEAK ON THE FIRE LOOP NEAR THE EXHAUST MOUNTING FLANGE, RR EXHAUST
- [SDR GLBA20110829A](https://openairdocs.org/sdr/GLBA20110829A.md): Connector · loose · Aug 29, 2011 · N153GL · Beech 1900D · Fire Protection System Wiring
  > NR 2 T-HANDLE ILLUMINATED IN FLIGHT. ENGINE SECURED, FIRE EXTINGUISHER ACTIVATED, T-HANDLE REMAINED ILLUMINATED. LIGHT EXTINGUISHED SHORTLY BEFORE TOUCHDOWN. NO OTHER INDICATION OF FIRE. PROP WAS VISUALLY VERIFED TO HAVE FEATHERED. MX INSPECTED FIRE LOOP SY
- [SDR GLBA20110830F](https://openairdocs.org/sdr/GLBA20110830F.md): Ground Wire · loose · Aug 29, 2011 · N153GL · Beech 1900D · Fire Protection System Wiring
  > "SUP" - SIG EVENT - PILOT REPORTED THAT THE NR 2 TEE HANDLE ILLUMINATED, SHUTDOWN RT ENGINE AND ACTUATED EXTINGUISHER, VISUALLY CHECKED THAT ENGINE WAS FEATHERED. MX INSPECTED FIRE LOOP SYS, FOUND LOOSE GROUND ON AFT CONNECTOR, REPAIRED GROUND REF AIM 14.3.0,
- [SDR GLBA2011082911F](https://openairdocs.org/sdr/GLBA2011082911F.md): Snubber · leaking · Aug 28, 2011 · N153GL · Beech 1900D · Passenger/Crew Doors
  > PILOT REPORTED THAT THE CABIN DOOR SNUBBER IS AT 700LBS. MX REPLACED THE DOOR SNUBBER DUE TO LEAKING SEALS IAW BMM 52-10-01, OPS CHECKED GOOD.
- [SDR GLBA20110817F](https://openairdocs.org/sdr/GLBA20110817F.md): Uplock Switch · inoperative · Aug 16, 2011 · N153GL · Beech 1900D · Landing Gear Position and Warning
  > PILOT REPORTED THAT WITH GEAR IN UP POSITION AND AUTO FEATHER SWITCH IN OFF POSITION. AUTO FEATHER OFF ANNUNCIATOR ILLUMINATED. MX REPLACED THE LT UPLOCK SWITCH, IAW TC 1900-3260.00, OPS CHECKED GOOD.
- [SDR GLBA20110817G](https://openairdocs.org/sdr/GLBA20110817G.md): Snubber · low pressure · Aug 16, 2011 · N153GL · Beech 1900D · Passenger/Crew Doors
  > PILOT REPORTED THAT THE AIRSTAIR DOOR SNUBBER PSI WAS BELOW 1000 PSI. MX SERVICED THE SYS IAW BMM 12-10-00, SYS WITHIN LIMITS.
- [SDR GLBA20110811H](https://openairdocs.org/sdr/GLBA20110811H.md): Bulb · inoperative · Aug 10, 2011 · N153GL · Beech 1900D · Propeller Feathering/Reversing
  > PILOT REPORTED THAT THE BULB IN THE LT AUTOFEATHER ANNC IS BURNED OUT. MX REPLACED THE BULB IAW BMM 33-10-01, OPS CHECKED GOOD.
- [SDR GLBA20110721F](https://openairdocs.org/sdr/GLBA20110721F.md): Propeller · malfunctioned · Jul 20, 2011 · N153GL · Beech 1900D · Propeller Feathering/Reversing
  > PILOT REPORTED THAT DURING APPROACH THE LT PROP WAS CYCLING IN AND OUT OF FEATHER WITH ABOUT 500LBS OF TORQUE. R & R LT & RT LOW PRESSURE AUTO FEATHER SWITCHES & RIGGED LT & RT ENG TORQUE IAW CH 7, SECTION 7.5 & BMM 61-21-01, OPS CHECKED GOOD.
- [SDR GLBA20110715H](https://openairdocs.org/sdr/GLBA20110715H.md): Pcb · inoperative · Jul 14, 2011 · N153GL · Beech 1900D · Propeller Feathering/Reversing
  > DURING THE OVERSPEED TEST ON THE RT ENGINE THE AUTOFEATHER DISABLE ANNUNCIATOR ILLUMINATED. MX REPLACED THE AFX PCB IAW MI 24-01, OPS CHECKED GOOD.
- [SDR GLBA20110630F](https://openairdocs.org/sdr/GLBA20110630F.md): Switch · inoperative · Jun 28, 2011 · N153GL · Beech 1900D · Propeller Feathering/Reversing
  > PILOT REPORTED THAT WHILE REDUCING POWER FROM 1200 LBS TORQUE TO IDLE NR1 ENGINE TRIED TO AUTOFEATHER. MX R & R LT & RT LOW PRESSURE AUTOFEATHER SWITCHES & RIGGED LT & RT ENGINE TORQUE IAW AIM CH 7, SECTION 7.5 & BMM 61-21-01, OPS CK GOOD.
- [SDR GLBA20110628G](https://openairdocs.org/sdr/GLBA20110628G.md): Connector · loose · Jun 27, 2011 · N153GL · Beech 1900D · Propeller/Propulsor System Wiring
  > PILOT REPORTED THAT WHEN THEY REDUCED POWER FROM 1200 TO IDLE THE LT ENGINE TRIED TO AUTOFEATHER, DISENGAGED AUTOFEATHER AND LANDED. MX RESECURED THE CONNECTOR PLUG ON THE LT LOW PRESSURE AFX SWITCH, OPS CK GOOD.

Next page: https://openairdocs.org/aircraft/N153GL/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 = 'N153GL' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N153GL/reports

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