# Service difficulty reports: N198GA

A list on [N198GA](https://openairdocs.org/aircraft/N198GA.md).

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

- [SDR TIMA20240105002](https://openairdocs.org/sdr/TIMA20240105002.md): Unknown · odor · Jan 5, 2024 · N198GA · Beech 1900C · Air Distribution System
  > ON ROTATION SMELL OF SMOKE IN COCKPIT AND I REQUESTED IMMEDIATE TURN BACK TO THE APPROACH. FLAP CIRCUIT BREAKER WAS POPPED.
- [SDR TIMA20200613003](https://openairdocs.org/sdr/TIMA20200613003.md): Engine · malfunctioned · Jun 13, 2020 · N198GA · Beech 1900C · Engine (Turbine/Turboprop)
  > AIRCRAFT DEPARTED DEN AND SHORTLY AFTER CLIMBOUT, LEVELING OUT AT 10K', THE PILOT BEGAN PULLING BACK POWER AND EXPERIENCED THE RIGHT ENGINE PROPELLER BECAME "JERKY" AND SPORADIC WITHOUT ANT PROPELLER LEVER INPUTS. SOON AFTER, THE RIGHT ENGINE ITT CLIMBED TO 11
- [SDR TIMA20180206002](https://openairdocs.org/sdr/TIMA20180206002.md): Trim System · malfunctioned · Jan 29, 2018 · N198GA · Beech 1900C · Elevator Tab Control System
  > ELECTRIC ELEVATOR TRIM ACTUATED UN-COMMANDED. THE PILOT PRESSED THE 'TRIM DISCONNECT' BUTTON WHICH STOPPED THE ELECTRIC TRIM OPERATION.
- [SDR TIMA20151127009](https://openairdocs.org/sdr/TIMA20151127009.md): Computer · faulty · Nov 27, 2015 · N198GA · Beech 1900C · Stall Warning System
  > STALL WARNING HORN SOUNDED CONTINUOUSLY FROM THE TIME THE ACFT TOOK OFF. PILOT ELECTED TO RETURN TO TAKEOFF AIRFIELD FOR AN UNEVENTFUL LANDING. SUBSEQUENT INSPECTION REVEALED THE LIFT DETECTOR COMPUTER WAS FAULTY.
- [SDR TIMA20151120008](https://openairdocs.org/sdr/TIMA20151120008.md): Terminal · corroded · Nov 20, 2015 · N198GA · Beech 1900C · Landing Gear Retraction/Extension System
  > AFTER TAKEOFF, WHEN GEAR SELECTED UP, THEY FAILED TO RETRACT. PILOT RETURNED TO TAKEOFF AIRFIELD FOR UNEVENTFUL LANDING. SUBSEQUENT INSPECTION FOUND THE LG POWER CB POPPED & CORROSION ON THE CB TERMINALS.
- [SDR TIMA20140422019](https://openairdocs.org/sdr/TIMA20140422019.md): Skin · debonded · Apr 22, 2014 · N198GA · Beech 1900C · Wing, Plate/Skin
  > LEFT WING DEBOND. UPPER SKIN OF BONDED PANEL IN AREA AROUND FUEL BAY ACCESS OVAL PANEL DEBONDED FROM FUEL ACCESS DISH & HONEYCOMB CORE.
- [SDR 2002F00863](https://openairdocs.org/sdr/2002F00863.md): Angle · cracked · Feb 15, 2002 · N198GA · Beech 1900C · Nacelle/Pylon, Main Frame
  > ANGLE LOCATED ABOVE THE ICE DOOR HINGE, THIS ANGLE HOLDS THE LOWER FIRE SEAL BULKHEAD. WHEN THIS ANGLE CRACKS, IT ALLOWS THE OUTSIDE COWL RIVETS TO WORK LOOSE, AND THIS CAUSES THE COWL SIDE SKIN TO CRACK. (M)
- [SDR 20001017AP004](https://openairdocs.org/sdr/20001017AP004.md): Panel · shorted · Jun 26, 2000 · N198GA · Beech 1900C · AC Power Distribution System
  > FLT 9449 - RSW-TPA - DURING TAXI, HEARD AND SAW ELECTRICAL ARC ON MAIN CIRCUIT BREAKER PANEL, THERE WAS A SMELL OF ELECTRICAL SMOKE. REMOVED AND REPLACED LUMINESCENT PANEL IAW BEECHCRAFT MM CHAP 33. OPERATIONAL CHECK NORMAL. (M)
- [SDR 98ZZZX3822](https://openairdocs.org/sdr/98ZZZX3822.md): Cable · broken · Sep 22, 1998 · N198GA · Beech 1900C · Passenger/Crew Doors
  > MIA/MCO - FLT 9380 - FORWARD CABIN DOOR WILL NOT OPEN WHEN HANDLE IS ROTATED. REMOVED AND REPLACED BROKEN DOOR CABLE.
- [SDR 98ZZZM237](https://openairdocs.org/sdr/98ZZZM237.md): Bracket · corroded · Jan 23, 1998 · N198GA · Beech 1900C · Elevator Structure
  > AT SCHEDULED EMPENNAGE INSPECTION, DETERMINED LEFT ELEVATOR OUTBOARD AND CENTER HINGE ATTACH BRACKETS TO HAVE INTERGRANULAR CORROSION. REMOVE AND REPLACED OUTBOARD AND CENTER HINGE, ATTACH BRACKETS. (M)
- [SDR 98ZZZM236](https://openairdocs.org/sdr/98ZZZM236.md): Spar Cap · corroded · Jan 23, 1998 · N198GA · Beech 1900C · Elevator, Spar/Rib
  > AT SCHEDULED, EMPENNAGE INSPECTION DETERMINED LEFT ELEVATOR UPPER AND LOWER SPAR CAPS TO HAVE INTERGRANULAR CORROSION THE LAST FOUR INCHES OUTBOARD. REPLACED LEFT ELEVATOR UPPER AND LOWER SPAR CAPS PART NR 'S 101-920014-45, AND 101-620014-47. (M)
- [SDR 98ZZZM218](https://openairdocs.org/sdr/98ZZZM218.md): Hinge · corroded · Jan 23, 1998 · N198GA · Beech 1900C · Horizontal Stabilizer Structure
  > AT SCHEDULED EMPENNAGE INSPECTION DETERMINED LEFT ELEVATOR, OUTBOARD AND CENTER HINGE ATTACH BRACKETS TO HAVE INTERGRANULAR CORROSION. REMOVED AND REPLACED OUTBOARD AND CENTER HINGE, ATTACH BRACKETS. (M)
- [SDR 98ZZZM217](https://openairdocs.org/sdr/98ZZZM217.md): Spar Cap · corroded · Jan 23, 1998 · N198GA · Beech 1900C · Elevator, Spar/Rib
  > AT SCHEDULED EMPENNAGE INSPECTION DETERMINED LEFT ELEVATOR UPPER AND LOWER SPAR CAPS TO HAVE INTERGRANULAR CORROSION THE LAST FOUR INCHES OUTBOARD. REPLACED LEFT ELEVATOR UPPER AND LOWER SPAR CAPS, P/N'S 101-920014-45, AND 101-620014-47. (M)
- [SDR 98ZZZM231](https://openairdocs.org/sdr/98ZZZM231.md): Circuit Board · failed · Dec 13, 1997 · N198GA · Beech 1900C · Landing Gear Retraction/Extension System
  > FLT 7383 - MIA-MCO - CIRCUIT BREAKER POPPED AND WOULD NOT RESET. GEAR WAS MANUALLY EXTENDED. SECURED PRINTED CIRCUIT BOARD, E173, CONNECTOR. SYSTEM CHECED GOOD ON JACKS. (M)
- [SDR 98ZZZM220](https://openairdocs.org/sdr/98ZZZM220.md): Circuit Board · damaged · Dec 13, 1997 · N198GA · Beech 1900C · Landing Gear Retraction/Extension System
  > FLT 7299 - NAS-MIA - WHILE IN FLIGHT, LANDING GEAR HANDLE WOULD NOT EXTEND GEAR. EXTENDED GEAR MANUALLY. A/C LANDED SAFELY. REMOVED AND REPLACED PRINTED CIRCUIT BOARD. (M)
- [SDR 98ZZZM230](https://openairdocs.org/sdr/98ZZZM230.md): Uplock Switch · out of adjust · Dec 12, 1997 · N198GA · Beech 1900C · Landing Gear Retraction/Extension System
  > FLT 7251 - MCO-EYW - ON APPROACH INTO EYW, WITH GEAR HANDLE DOWN. CIRCUIT BREAKER POPPED WOULD NOT RESET. DIVERTED TO MIA AND MANUALLY EXTENDED GEAR. AIRCRAFT LANDED SAFELY. ADJUSTED LEFT UPLOCK SWITCH. SYSTEM CHECKED GOOD ON JACKS. (M)
- [SDR 97ZZZX3858](https://openairdocs.org/sdr/97ZZZX3858.md): Engine · failed · May 19, 1997 · N198GA · Beech 1900C · Engine (Turbine/Turboprop)
  > MIA/NAS - FLT 7156 - RIGHT ENGINE QUIT ON CLIMB-OUT. REMOVED AND REPLACED RIGHT ENGINE. (X)
- [SDR 97ZZZM560](https://openairdocs.org/sdr/97ZZZM560.md): Fire Loop · out of position · Apr 9, 1997 · N198GA · Beech 1900C · Fire Detection
  > FLT 7485 - NAS-FLL - RIGHT FIREWALL FUEL VALVE HANDLE ILLUMINATED FOR ABOUT 20 SECONDS AND EXTINGUISHED AT IDLE DURING TAXI. REPOSITIONED RIGHT ENGINE FIRE LOOP TO PROPER POSITION. PERFORMED OPERATIONAL CHECK OF THE SYSTEM WITH TEST SWITCH. (M)
- [SDR 97ZZZM526](https://openairdocs.org/sdr/97ZZZM526.md): Switch Wire · loose · Mar 21, 1997 · N198GA · Beech 1900C · Landing Gear Position and Warning
  > FLT 396 - MCO/MIA - GEAR HORN AND HANDLE LIGHT WILL NOT ILLUMINATE WHEN POWER LEVERS ARE RETARDED OR FLAPS ARE LOWERED PAST APPROACH. SECURED WIRE AT LEFT POWER LEVER MICROSWITCH WITH AIRCRAFT ON JACKS. CYCLED GEAR SEVERAL TIMES. NO DEFECTS NOTED. (M)
- [SDR 96ZZZM1064](https://openairdocs.org/sdr/96ZZZM1064.md): O-Ring · pinched · Jun 14, 1996 · N198GA · Beech 1900C · Turbine Engine Oil System
  > FLT - 477 - FLL/NAS - LEFT ENGINE LOST OIL PRESSURE THEN THE ENGINE SHUTDOWN ITSELF. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO MIA AND LANDED WITHOUT INCIDENT. INSPECTED AND DETERMINED THAT THE LEFT OIL FILTER COVER O-RING WAS PINCHED ALLOWING L
- [SDR 96ZZZM1008](https://openairdocs.org/sdr/96ZZZM1008.md): Wire · chafed · May 23, 1996 · N198GA · Beech 1900C · Landing Gear System Wiring
  > FLT 169 - TPA-MIA - LANDING GEAR INDICATION CIRCUIT BREAKER POPS DURING RETRACTION CYCLED ONLY. REPAIRED CHAFED WIRE UNDER CENTER FLOOR AT PLUG P313. OPS CHECK GOOD ON GEAR SWINGS, OPS CHECK GOOD ON TEST FLIGHT. (M)
- [SDR 96ZZZM813](https://openairdocs.org/sdr/96ZZZM813.md): Skin · cracked · Apr 23, 1996 · N198GA · Beech 1900C · Wing, Plate/Skin
  > AT SCHEDULED INSPECTION, THE RIGHT UPPER WING SKIN WAS DETERMINED TO BE CRACKED, ZONE 632. REMOVED DAMAGED AREA, INSTALLED FILLER DOUBLER IAW BEECH SRM CHAPTER 51-70-00, FIGURE 15. (M)
- [SDR 96ZZZM812](https://openairdocs.org/sdr/96ZZZM812.md): Skin · cracked · Apr 23, 1996 · N198GA · Beech 1900C · Wing, Plate/Skin
  > AT SCHEDULED INSPECTION, THE LEFT UPPER WING SKIN CRACKED, ZONE 532. REMOVED DAMAGED AREA, INSTALLED FILLER AND DOUBLER IAW BEECH SRM 51-70-00, FIGURE 15. (M)
- [SDR 95ZZZW805](https://openairdocs.org/sdr/95ZZZW805.md): Oil Syst · over serviced · Jul 15, 1995 · N198GA · Beech 1900C · Turbine Engine Oil System
  > MIA-ELH - FLT 465 - SMOKE IN CABIN, AC RETURNED TO MIA WITHOUT FURTHER INCIDENT. DETERMINED RT ENGINE TO BE OVER SERVICED. DRAINED OIL TO PROPER LEVEL. AC WAS TEST FLOWN WITH SATISFACTORY RESULTS AND RELEASED FOR SERVICE.
- [SDR 95ZZZW732](https://openairdocs.org/sdr/95ZZZW732.md): Breaker · tripped · May 8, 1995 · N198GA · Beech 1900C · Landing Gear Retraction/Extension System
  > FLT 487A - MCO-MIA - LANDING GEAR CIRCUIT BREAKER POPPED ON RETRACT OUT OF MCO. TROUBLE SHOT SYSTEM WIRING. PERFORMED SEVERAL GEAR SWINGS. OPS CHECK GOOD, COULD NOT DUPLICATE.

## 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 = 'N198GA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N198GA/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.