# Service difficulty reports: N154GL

A list on [N154GL](https://openairdocs.org/aircraft/N154GL.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 · 58 reports

- [SDR GLBA2014091100437](https://openairdocs.org/sdr/GLBA2014091100437.md): Skin · damaged · Sep 11, 2014 · N154GL · Beech 1900D · Elevator, Plate/Skin
  > DURING A SCHEDULED INSPECTION MAINTENANCE FOUND A LIGHTNING STRIKE ON THE OTBD RT ELEVATOR TE JUST OTBD OF THE OTBD MOST STATIC WICK CAUSING DAMAGE TO THE FIBERGLASS TIP, THE ADJACENT SHEET METAL & AN EXISTING PATCH. THERE ARE.060 INCH DIAMETER &.225 INCH D
- [SDR GLBA2014012300373](https://openairdocs.org/sdr/GLBA2014012300373.md): Spar · cracked · Jan 22, 2014 · N154GL · Beech 1900D · Horizontal Stabilizer, Spar/Rib
  > DURING A SCHEDULED INSPECTION MX ACCOMPLISH PROACTIVE REPAIR TO THE RT VERTICAL SPAR CAP ANGLE IAW EO 14-1900-55-001. SUPPLEMENTAL INFORMATION WILL BE SUBMITTED UPON COMPLETION OF THE REPAIR & RETENTION OF THE PAPERWORK.
- [SDR GLBA2014011600371](https://openairdocs.org/sdr/GLBA2014011600371.md): Skin · dented · Jan 15, 2014 · N154GL · Beech 1900D · Fuselage Main, Plate/Skin
  > DURING A SCHEDULED INSPECTION, MX FOUND THE LT AFT SKIN DENTED AT BS 446 BETWEEN STRINGERS 11-12L. REPAIREDS IAW EO 14-1900-53-005.
- [SDR GLBA2014011300368](https://openairdocs.org/sdr/GLBA2014011300368.md): Frame · cracked · Jan 13, 2014 · N154GL · Beech 1900D · Fuselage Main, Frame
  > DURING A SCHEDULED INSPECTION FOUND A CRACK AT BS 183 & STRINGER 9R FRAME ANGLE,.375 INCHES IN LENGTH. REPAIRED IAW EO 14-1900-53-003.
- [SDR GLBA2014011300367](https://openairdocs.org/sdr/GLBA2014011300367.md): Door Frame · cracked · Jan 13, 2014 · N154GL · Beech 1900D · Fuselage Main, Structure
  > DURING A SCHEDULED INSPECTION, FOUND A CRACK IN THE PAX DOOR CUTOUT LOWER FRAME AT APPROXIMATELY FS 172 LOWER AFT CORNER, 1 INCH IN LENGTH. REPAIRED IAW EO 13-1900-53-002.
- [SDR GLBA2014011300370](https://openairdocs.org/sdr/GLBA2014011300370.md): Skin · cracked · Jan 13, 2014 · N154GL · Beech 1900D · Fuselage Main, Plate/Skin
  > DURING A SCHEDULED INSPECTION, FOUND TWO CRACKS AT BS 150 & STRINGER 1 EXTERIOR FUSELAGE SKIN PROTRUDING OUT OF RIVETS ON EITHER SIDE OF STRINGER,.25 INCHES IN LENGTH. REPAIRED IAW EO 13-1900-53-004.
- [SDR GLBA2014011300369](https://openairdocs.org/sdr/GLBA2014011300369.md): Door · cracked · Jan 13, 2014 · N154GL · Beech 1900D · Emergency Exits
  > DURING A SCHEDULED INSPECTION, FOUND THE EMERGENCY DOOR CRACKED, 4C AT THE RT FWD ASSEMBLY, 1.125 INCHES IN LENGTH. REPAIRED IAW EO 13-1900-52-001.
- [SDR GLBA2013090900307](https://openairdocs.org/sdr/GLBA2013090900307.md): Wire · damaged · Sep 6, 2013 · N154GL · Beech 1900D · Fire Protection System Wiring
  > PILOT REPORTED THAT THE RT FIRE LOOP AND TEE HANDLE ANNUNCIATORS FLICKERED DURING CLIMB OUT. MAINTENANCE TROUBLESHOT SYSTEM, NO FAULTS FOUND MEGGED WIRE W16A22 FROM J410 T. HRU S16 SWITCH TO PIN 3 OF P157 AND FOUND SHORT TO GROUND. R & R SWITCH S16 IAW AIM 1
- [SDR GLBA2013070500269](https://openairdocs.org/sdr/GLBA2013070500269.md): Blower · odor · Jul 3, 2013 · N154GL · Beech 1900D · Air Distribution Fan
  > PILOT REPORTED A FOUL ODOR EMINATING FROM THE ENVIROMENTAL SYS WITH A NOTIABLE VIBRATION IN THE BACK OF THE ACFT. MX CLEANED THE ENVIRO VENT BLOWER AND SECURED THE PANEL, OPS CHECKED GOOD, NO ODOR NOTED.
- [SDR GLBA2012082300037](https://openairdocs.org/sdr/GLBA2012082300037.md): Attach Angle · cracked · Aug 23, 2012 · N154GL · Beech 1900D · Fuselage Main, Attach Fittings
  > DURING A SCHEDULED ROUTINE INSPECTION FOUND TWO CRACKS AT THE RT ANGLE AT FS 107.00 AS IT ATTACHES TO THE LONGERON, RT ANGLE AT THE UPPER END OF THE BEND RADIUS,.5" IN LENGTH, AND AT THE UPPER FASTENER AREA,.375" IN LENGTH. REPAIRED THE AFFECTED AREA IAW E
- [SDR GLBA2012082300038](https://openairdocs.org/sdr/GLBA2012082300038.md): Attach Angle · cracked · Aug 23, 2012 · N154GL · Beech 1900D · Fuselage Main, Attach Fittings
  > DURING A SCHEDULED ROUTINE INSPECTION, FOUND CRACK ON THE LT SIDEWALL AT FS 107.00, LT ANGLE UPPER INBD FLANGE PORTION IN THE BEND RADIUS AS IT ATTACHED TO THE LONGERON,.75" IN LENGTH. REPAIRED THE AFFECTED AREA IAW EO 12-1900-53-047.
- [SDR GLBA2012082300036](https://openairdocs.org/sdr/GLBA2012082300036.md): Longeron · cracked · Aug 23, 2012 · N154GL · Beech 1900D · Fuselage Main, Longeron/Stringer
  > DURING A SCHEDULED ROUTINE INSPECTION, FOUND THE RT LONGERON AT JUNCTION WITH RT ANGLE AT FS 107.00 CRACKED FROM THE INBD FLANGE AT THE LONGERON TO THE BEND RADIUS,.75" IN LENGTH. REPAIRED THE AFFECTED AREA IAW EO 12-1900-53-048. MAJOR REPAIRE.
- [SDR GLBA2012082100035](https://openairdocs.org/sdr/GLBA2012082100035.md): Spar Cap · cracked · Aug 20, 2012 · N154GL · Beech 1900D · Vertical Stabilizer, Spar/Rib
  > DURING A SCHEDULED ROUTINE INSPECTION FOUND VERT STAB LT SPAR CAP ANGLE AT THE 20 PERCENT CHORD IS CRACKED AT THE UPPER END AT VSS 84.10, BEGINNING AT THE TOP EDGE AND RADIATES DOWNWARD, THE CRACK IS ON THE FWD FAIRING PORTION OF THE ANGLE, 4.25" IN LENGTH.
- [SDR GLBA2012082100034](https://openairdocs.org/sdr/GLBA2012082100034.md): Pressure Blkhd · cracked · Aug 20, 2012 · N154GL · Beech 1900D · Fuselage Main, Bulkhead
  > DURING A SCHEDULED ROUTINE INSPECTION FOUND RT LWR FWD PRESSURE BULKHEAD CRACKED AROUND FASTENERS ALONG THE BULKHEADS INBD EDGE, FOUND 2 CRACKS APPROX.1 INCH IN LENGTH THAT RADIATES FROM FASTENER HOLES AT FS 84.0. REPAIRED IAW EO 12-1900-53-045.
- [SDR GLBA2012082100033](https://openairdocs.org/sdr/GLBA2012082100033.md): Pressure Blkhd · cracked · Aug 20, 2012 · N154GL · Beech 1900D · Fuselage Main, Bulkhead
  > DURING A SCHEDULED INSPECTION, FOUND LT LWR FWD PRESSURE BULKHEAD IS CRACKED ALONG THE INBD EDGE DOUBLE ROW OF FASTENER, 3 CRACKS.2 INCHES IN LENGTH RADIUS FROM FASTENER HOLES AT FS 84. REPAIRED IAW EO 12-1900-53-045.
- [SDR GLBA2012061900001](https://openairdocs.org/sdr/GLBA2012061900001.md): Web · cracked · Jun 19, 2012 · N154GL · Beech 1900D · Horizontal Stabilizer Structure
  > DURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE HORIZONTAL STAB AFT WEB AT HSS 0.00, 2" IN LENGTH. REPAIRED THE AFFECTED AREA IAW EO 12-1900-55-017.
- [SDR GLBA20111227F](https://openairdocs.org/sdr/GLBA20111227F.md): Switch · dirty · Dec 24, 2011 · N154GL · Beech 1900D · Door Warning System
  > CABIN DOOR ANNUNCIATOR ILLUMINATED ON DESCENT THEN EXTINGUISHED SHORTLY AFTER. MX CLEANED THE SWITCH, OPS CHECKED GOOD.
- [SDR GLBA20111109F](https://openairdocs.org/sdr/GLBA20111109F.md): Wire · damaged · Nov 8, 2011 · N154GL · Beech 1900D · Door System Wiring
  > PILOT REPORTED THEAT THE CABIN DOOR ANNUNCIATOR EXTINGUISHES WHEN DOOR IS OPEN AND HANDLE IS CLOSED. MX REPAIRED SPLICE D436, OPS CHECKED GOOD.
- [SDR GLBA20111003J](https://openairdocs.org/sdr/GLBA20111003J.md): Circuit Board · malfunctioned · Oct 2, 2011 · N154GL · Beech 1900D · Propeller Feathering/Reversing
  > PILOT REPORTED THAT DURING RUNUP THE AFX DISABLE ANNUNCIATOR WON'T ILLUMINATE ON THE RT AUTOFEATHER TEST. MX RERACKED THE A123 PCB IAW MI 24-01, OPS CHECKED GOOD.
- [SDR GLBA20110906F](https://openairdocs.org/sdr/GLBA20110906F.md): Switch · inoperative · Sep 2, 2011 · N154GL · Beech 1900D · Door Warning System
  > PILOT REPORTED THAT THE CABIN DOOR ANNUNCIATOR DOES NOT EXTINGUISH. MX REPAIRED MULTIPLE WIRES TO SPLICE D436, REPLACED FWD MICROSWITCH REF 14.12.10, RIGGED SWITCH IAW BMM 52-70-01, OPS CHECK GOOD.
- [SDR GLBA201108081](https://openairdocs.org/sdr/GLBA201108081.md): Valve · failed · Aug 7, 2011 · N154GL · Beech 1900D · Landing Gear Retraction/Extension System
  > LANDING GEAR FAILED TO EXTEND ON APPROACH. DID NOT HEAR THE PUMP TURN ON WHEN MOVING THE LANDING GEAR CONTROL HANDLE. PUMPED GEAR DOWN MANUALLY, HAD ALL 5 GREEN LIGHTS AND IN TRANSIT LIGHT WAS EXTINGUISHED. MX REPLACED THE LG SERVICE VALVE IAW BMM 32-30-16,
- [SDR GLBA20110706H](https://openairdocs.org/sdr/GLBA20110706H.md): Support · failed · Jul 5, 2011 · N154GL · Beech 1900D · Passenger/Crew Doors
  > PILOT REPORTED THAT THE CABIN DOOR STRAP SUPPORT ON THE LT SIDE IS COMING APART. MX REINSTALLED A FASTENER ON THE LT CABIN DOOR STRAP SUPPORT IAW BMM 52-10-60, ALL CHECKS GOOD.
- [SDR GLBA20110519F](https://openairdocs.org/sdr/GLBA20110519F.md): Skin · debonded · May 19, 2011 · N154GL · Beech 1900D · Passenger/Crew Doors
  > MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION MAINTENANCE FOUND THE AS DOOR SKIN DEBONDED AT THE LOWER BOTTOM, DEBONDED FROM FORWARD EDGE TO THE AFT EDGE, FROM LOWER EDGE TO 5" UPWARD. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RI
- [SDR GLBA20110518F](https://openairdocs.org/sdr/GLBA20110518F.md): Skin · cracked · May 17, 2011 · N154GL · Beech 1900D · Fuselage Main, Plate/Skin
  > MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION MAINTENANCE FOUND A CRACK IN THE BELLY SKIN AT FS 300 AND RT WING IB BULK HEAD, 1" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-53-035. MATERIAL
- [SDR GLBA20110516L](https://openairdocs.org/sdr/GLBA20110516L.md): Frame · cracked · May 16, 2011 · N154GL · Beech 1900D · Fuselage Main, Frame
  > MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION MAINTENANCE FOUND CRACKS AT F.S. 456 BETWEEN STRINGERS 3L AND 4L AT THE UPPER IB NUTPLATE AREA, 1.9" IN LENGTH, 7 CRACKS. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW
- [SDR GLBA20110516K](https://openairdocs.org/sdr/GLBA20110516K.md): Frame · cracked · May 16, 2011 · N154GL · Beech 1900D · Fuselage Main, Frame
  > MAJOR REPAIR. DURING A SCHEDULED ROUTINE INSPECTION MAINTENANCE FOUND A CRACK IN THE FRAME AT FS 456 AND S10R,.5" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-53-034. MATERIALS UTILIZED ARE INCL
- [SDR GLBA20100904A](https://openairdocs.org/sdr/GLBA20100904A.md): Tube · leaking · Sep 4, 2010 · N154GL · Beech 1900D · Air Distribution System
  > PILOT REPORTED THAT THEY NOTICED SMOKE/FUMES IN THE CABIN PRIOR TO TAKEOFF, SUSPECT VAPOR CYCLE SYSTEM LEAK. MAINTENANCE REPLACED THE TUBE FROM RECEIVER-DRIER TO CONDENSOR IAW BMM 21-52-00, REPLACED CONDENSER BLOWER IAW BMM 21-52-03, AND SERVICED SYSTEM IAW BM
- [SDR GLBA20100805FA](https://openairdocs.org/sdr/GLBA20100805FA.md): Engine · overtorqued · Aug 3, 2010 · N154GL · Beech 1900D · Engine (Turbine/Turboprop)
  > PILOT REPORTED THAT UPON APPROACH, RT POWER LEVER STUCK WITH AN OVERTORQUE INDICATION, PERFORMED PRECAUTIONARY RT ENGINE SHUTDOWN. RT PROPELLER CONTINUED TO WINDMILL AFTER ENGINE SHUTDOWN. MX PERFORMED AN INSPECTION ON RT ENGINE POWER CONTROL LINKAGE, CABLE, C
- [SDR GLBA2010051601](https://openairdocs.org/sdr/GLBA2010051601.md): Bearing · failed · May 16, 2010 · N154GL · Beech 1900D · Starter-Generator
  > PILOTS REPORTED, WHILE PERFORMING A 2ND START FOR NR 2 ENG. NR 2 STARTER SEEMED TO TURN ON & OFF VERY QUICKLY WHEN IGNITION & ENG START SWITCH IN ON. DURING ENG START, N1 DOES NOT CLIMB ABOVE 6 %. ON 3RD ATTEMPT TO START, NOTICED NR 2 ENG ACCY SECTION HAD VI
- [SDR GLBA20091116F](https://openairdocs.org/sdr/GLBA20091116F.md): Brace · chafed · Nov 12, 2009 · N154GL · Beech 1900D · Main Landing Gear Strut/Axle/Truck
  > MX DISCOVERED THAT THERE WAS CHAFING ON THE FWD RT SIDE OF THE RT MLG BRACE CTR TUBE APPROX 11 INCHES FROM TOP. CHAFE IS APPROX AT A 45 DEGREE ANGLE AND MEASURES.5 INCHES LONG,.310 INCHES WIDE AND.020 INCHES MAX DEPTH. CHAFE ON FWD RT SIDE OF THE MLG BRAC
- [SDR GLBA20090909H](https://openairdocs.org/sdr/GLBA20090909H.md): Skin · cracked · Sep 8, 2009 · N154GL · Beech 1900D · Fuselage Main, Plate/Skin
  > MAJOR REPAIR - DURING ROUTINE SCHEDULED MAINTENANCE A CRACK WAS FOUND ON THE BELLY SKIN AT B.L. 29.0 AND F.S. 303.25. CRACK IS APPROXIMATELY 2.250" IN LENGTH. MAINTENANCE REPAIRED THE BELLY SKIN AT F.S. 303.25 AND B.L 29.0 IAW EO 09-1900-53-016. RII INSPECTIO
- [SDR GLBA20090502A](https://openairdocs.org/sdr/GLBA20090502A.md): Circuit Board · loose · May 2, 2009 · N154GL · Beech 1900D · Air Conditioning System Wiring
  > RIGHT ENVIRO FAIL ANNUNCIATOR ILLUMINATED DURING TAKEOFF WITH TAKEOFF POWER AND BLEED AIR VALVES CLOSED. MAINTENANCE RE-SEATED THE PRINTED CIRCUIT BOARD AND OPERATIONAL CHECKS WERE GOOD.
- [SDR GLBA20090424B](https://openairdocs.org/sdr/GLBA20090424B.md): Generator · failed · Apr 24, 2009 · N154GL · Beech 1900D · DC Generating System
  > PILOTS REPORTED THE THE LEFT DC GENERATOR FELL OFFLINE ON TAKEOFF ROLL. MAINTENANCE PERFORMED AN OPERATIONAL CHECK PER MM 24-00-00-001. NO FAULTS WERE FOUND AND THE AIRCRAFT WAS RETURNED TO SERVICE.
- [SDR GLBA20090312A](https://openairdocs.org/sdr/GLBA20090312A.md): Relay · deteriorated · Mar 12, 2009 · N154GL · Beech 1900D · Trailing Edge Flap Control System
  > PILOTS REPORTED THAT THE FLAPS STUCK INTERMITTENTLY AT 17 DEGREES AND EVENTUALLY CAME UP UPON LANDING. MAINTENANCE REMOVED AND REPLACED FLAP RELAY I.A.W. BMM 27-50-05 OPERATIONAL CHECKS WERE GOOD PART NUMBER ON/OFF. SM50B7 CLEARED MEL AND PLACARDS WERE REMOVE
- [SDR GLBA20090301B](https://openairdocs.org/sdr/GLBA20090301B.md): Indicator · worn · Mar 1, 2009 · N154GL · Beech 1900D · Airspeed/Mach Indicator
  > FLIGHT 5014- NO AIRSPEED INDICATION ON CA AIRSPEED ON T/O ROLL. MAINTENANCE REMOVED AND REPLACED THE NR 1 AIRSPEED INDICATOR IAW TASKCARD 1900.3411.00-1. OPERATIONAL CHECK WAS GOOD.
- [SDR GLBA20061099](https://openairdocs.org/sdr/GLBA20061099.md): Skin · damaged · May 2, 2008 · N154GL · Beech 1900D · Fuselage Main, Plate/Skin
  > RT UPPER ICE SHIELD DIVIDED INTO (2) PIECES AT APPROXIMATE LOCATION OF STRINGER 8R FROM F.S. 183.25 TO F.S. 220.75. MAINT REPLACED THE RT UPPER ICE SHILED IAW. SRM 51-40. RII INSP COMPLIED WITH IAW TASKCARD 8.2.1.
- [SDR GLBA20061098](https://openairdocs.org/sdr/GLBA20061098.md): Frame · cracked · May 1, 2008 · N154GL · Beech 1900D · Fuselage Main, Frame
  > FUSELAGE FRAME AT FS 177.3 CRACKED AT STRINGER 9R CUTOUT. CRACK APPROXIMATELY.6 INCH IN LENGTH. MAINTENANCE REPAIRED FUSELAGE FRAME AT FS 177.3 AT STRINGER 9R RELIEF HOL IAW. SRM 51-70. REPAIR APPROXIMATELY 5 INCH BY 2.5 INCH. 2024-T3.071. RII INSPECTION CO
- [SDR GLBA20061097](https://openairdocs.org/sdr/GLBA20061097.md): Frame · cracked · May 1, 2008 · N154GL · Beech 1900D · Fuselage Main, Frame
  > FUSELAGE FRAME CRACK AT FS 163.97 AT STRINGER 9R CUTOUT. CRACK APPROXIMATELY.5 INCH IN LENGTH. MAINT REPAIRED FUSELAGE FRAME AT FS 163.97 AT STRINGER 9R RELIEF HOLE IAW. SRM 51-70. REPAIR APPROXIMATELY 5.5 INCH BY 2.5 INCH. 2024-T3.071. RII INSPECTION COMP
- [SDR GLBA20061096](https://openairdocs.org/sdr/GLBA20061096.md): Frame · cracked · May 1, 2008 · N154GL · Beech 1900D · Fuselage Main, Frame
  > FUSELAGE FRAME AT FS 451 CRACKED ON THE TOP SIDEOF STRINGER 10R. CRACK APPROXIMATELY 1.1 INCH LENGTH. MAINT REPAIRED FUSELAGE FRAME FLANGE AT FS 451 STRINGER 10R IAW SRM 51-70. REPAIR APPROXIMATELY 6 INCH BY 2 INCH. 2024-T3.071. RII INSPECTIONS COMPLIED WITH
- [SDR GLBA20061095](https://openairdocs.org/sdr/GLBA20061095.md): Stringer · cracked · May 1, 2008 · N154GL · Beech 1900D · Fuselage Main, Longeron/Stringer
  > STRINGER 10R CRACKED AT F.S. 451. CRACK LENGTH APPROXIMATELY.5 INCH. MAINT REPAIRED STRINGER 10R FLANGE AT F.S. 451 I.A.W. BEECH 1900D SRM 51-70. REPAIR DIMENSION APPROX 7.5 INCH BY 1 INCH. 2024-T3.050 INCH. RII INSPECTION COMPLIED WITH IAW TASKCARD 8.2.1.
- [SDR GLBA20061054](https://openairdocs.org/sdr/GLBA20061054.md): Engine · deteriorated · Jan 30, 2008 · N154GL · Beech 1900D · Engine (Turbine/Turboprop)
  > ENGINE SHUTDOWN, FLT 5041 ENROUTE 10 MILES OUT ON FINAL THE NR1 ENGINE FEATHERED INFLIGHT AND THE PILOTS PERFORMED THE ENG SECURE PROCEDURES AND SHUTDOWN THE ENG MAINT REMOVED AND REPLACED THE NR1 ENG ASSY IAW TASKCARD NR 1900-7100.00. RII INSP COMPLIED WITH.
- [SDR GLBA20060961](https://openairdocs.org/sdr/GLBA20060961.md): Torquemeter · malfunctioned · Jul 2, 2007 · N154GL · Beech 1900D · Engine BMEP/Torque Indicating
  > ABORTED TAKEOFF, FLIGHT 5063, UPON TAKEOFF PILOTS REPORTED THAT THE LT TORQUE INDICATOR STUCK AND WOULD NOT WORK CORRECTLY. AIRCRAFT RETURNED TO GATE. MAINTENANCE REMOVED AND REPLACED THE LT TORQUE GAUGE IAW MM 33-10. OPERATIONAL CHECK OF THE SYSTEM GOOD.
- [SDR 20030785](https://openairdocs.org/sdr/20030785.md): Spar · cracked · Jan 26, 2005 · N154GL · Beech 1900D · Horizontal Stabilizer, Spar/Rib
  > DURING ROUTINE STRUCTURAL "I" INSPECTION, FOUR CRACKS WERE IDENTIFIED EMANATING FROM THE DE-ICE HOLE ON THE HORIZONTAL CENTER MAIN SPAR CENTER WEB SKIN APPROX 1" LONG EACH UNDER PANEL 332 ATC. REPAIR WAS MADE AND AIRCRAFT RETURNED TO SERVICE.
- [SDR GLBA20030683](https://openairdocs.org/sdr/GLBA20030683.md): Skin · cracked · Jul 29, 2004 · N154GL · Beech 1900D · Fuselage Main, Plate/Skin
  > CRACK IN FUSELAGE SKIN FWD AND LEFT OF LWR COMM ANTENNA, PERFORMED MAJOR REPAIR TO FUSELAGE SKIN.
- [SDR GLBA20030652](https://openairdocs.org/sdr/GLBA20030652.md): Compressor · stalled · Jun 22, 2004 · N154GL · Beech 1900D · Engine (Turbine/Turboprop)
  > NR 1 ENG COMPRESSOR STALLS, SHUT DOWN ENG IN FLT RETURNED TO DEN. REMOVED AND REPLACED ENG PN PT6A-67D.
- [SDR GLBA20030598](https://openairdocs.org/sdr/GLBA20030598.md): Wire · broken · Mar 28, 2004 · N154GL · Beech 1900D · Flight Control System Wiring
  > LOOSE WIRE CAUSED SPARK ON F.O. YOKE, REMOVED BROKEN WIRE OPS CK GOOD
- [SDR GLBA20030594](https://openairdocs.org/sdr/GLBA20030594.md): Indicator · frozen · Mar 21, 2004 · N154GL · Beech 1900D · Engine RPM Indicating System
  > RT N1 INDICATOR SPIKED & FROZE AT 98 PERCENT, PREFORMED OPS CK FOUND NO DEFECTS SWAPPED GAUGES PN 130-380044-5 CND
- [SDR GLBA20030527](https://openairdocs.org/sdr/GLBA20030527.md): Flap · stuck · Jan 7, 2004 · N154GL · Beech 1900D · Trailing Edge Flap Control System
  > FLAPS STUCK AT 17 DEG, PENDING CORRECTIVE ACTION
- [SDR GLBA2003527](https://openairdocs.org/sdr/GLBA2003527.md): Flap · stuck · Jan 7, 2004 · N154GL · Beech 1900D · Trailing Edge Flap Control System
  > FLAPS STUCK AT 17 DEG, PENDING CORRECTIVE ACTION
- [SDR GLBA2003153](https://openairdocs.org/sdr/GLBA2003153.md): Indicator · malfunctioned · Nov 20, 2003 · N154GL · Beech 1900D · Engine EGT/TIT Indicating System
  > LT ENGINE ITT EXCEEDED 900C ON ADVANCEMENT OF POWER ON TAKE OFF ROLL, REMOVED AND REPLACED LT ITT GAUGE.

Next page: https://openairdocs.org/aircraft/N154GL/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 = 'N154GL' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N154GL/reports

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