# Service difficulty reports: N153GA

A list on [N153GA](https://openairdocs.org/aircraft/N153GA.md).

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

- [SDR TIMA202207130008](https://openairdocs.org/sdr/TIMA202207130008.md): Engine · shutdown · Jul 12, 2022 · N153GA · Beech 1900C · Powerplant System
  > PS NORMAL THROUGH 10,000 FT. CLIMBING THROUGH ABOUT 10500 FT THE PILOT NOTICED THE RH TORQUE GAUGE BEGIN TO FALL, THEN THE RH OIL PRESSURE LIGHT CAME ON. PILOT FELT A YAW, WAITED ABOUT THIRTY SECONDS TO CONFIRM FAILURE, SECURED THE ENGINE AND RETURNED BACK TO
- [SDR TIMA20211220002](https://openairdocs.org/sdr/TIMA20211220002.md): Unknown · unknown · Dec 7, 2021 · N153GA · Beech 1900C · Air Conditioning System
  > GOT SMOKE/HAZE IN THE COCKPIT ONCE LEVELED IN CRUISE. TURNED BACK TO BIL AND SHUT OFF THE BLEED VALVES. ONCE BLEED VALVES WERE OFF THE COCKPIT CLEARED. LANDED AND TAXIED WITH NO ISSUES.
- [SDR TIMA20161213019](https://openairdocs.org/sdr/TIMA20161213019.md): Windshield · cracked · Dec 13, 2016 · N153GA · Beech 1900C · Flight Compartment Windows
  > THE PILOT’S SIDE WINDSHIELD CRACKED DURING FLIGHT. THERE WAS A 3 INCH WIDE BAND OF SHATTERING OF THE OUTER LAYER THAT RAN FROM THE TOP TO THE BOTTOM OF THE WINDSHIELD ON THE INBOARD EDGE NEXT TO THE CENTER POST.
- [SDR TIMA20130830009](https://openairdocs.org/sdr/TIMA20130830009.md): Skin · corroded · Aug 30, 2013 · N153GA · Beech 1900C · Fuselage Main, Plate/Skin
  > CORROSION FOUND ON BELLY OF ACFT UNDER ADF ANTENNA BS 183.25. REPAIRED.
- [SDR KGBR507Y201105250](https://openairdocs.org/sdr/KGBR507Y201105250.md): Skin Panel · cracked · May 25, 2011 · N153GA · Beech 1900C · Trailing Edge Flaps
  > CRACK IN SKIN PANEL.5 INCH FWD OF THE TRAILING EDGE, 4.5 INCHES TO 10.5 INCHES FROM THE INBOARD EDGE OF THE FLAP. ALSO ARE 2 CRACKS IN THE AREA OF THE INBOARD ATTACH BRACKET AREA AT THE OUTBOARD ACCESS HOLE, 13 INCHES OUTBOARD OF THE INBOARD EDGE, EACH AT AP
- [SDR TIMA2010000011](https://openairdocs.org/sdr/TIMA2010000011.md): Seat Track · corroded · Mar 10, 2010 · N153GA · Beech 1900C · Fuselage, Seat/Cargo Attach Fittings
  > LEFT SIDE SEAT RAIL CORRODED.
- [SDR TIM2005F00000](https://openairdocs.org/sdr/TIM2005F00000.md): Blade · broken · Dec 28, 2004 · N153GA · Beech 1900C · Turbine Engine Compressor Section
  > AIRCRAFT DEPARTED AT CRUISE. THE LT ENGINE HAD AN EXPLOSIVE NOISE AND THE LT ENGINE SEIZED. PRE-INSPECTION OF ENGINE INDICATES LOSS OF CT BLADE. (K)
- [SDR 2005FA0000006](https://openairdocs.org/sdr/2005FA0000006.md): Blade · broken · Dec 28, 2004 · N153GA · Beech 1900C · Engine (Turbine/Turboprop)
  > AIRCRAFT DEPARTED, AT CRUISE, THE LT ENGINE HAD AN EXPLOSIVE NOISE AND THE LEFT ENGINE SEIZED. PRE INSPECTION OF ENGINE INDICATES LOSS OF CT BLADE. (K)
- [SDR 2005FA0000005](https://openairdocs.org/sdr/2005FA0000005.md): Cable · broken · Nov 16, 2004 · N153GA · Beech 1900C · Passenger/Crew Doors
  > ON CLIMBOUT THE AIRSTAIR DOOR OPENED. AC RETURNED, WHEN AIRSTAIR DOOR OPENED IN FLIGHT, DOOR DAMPER BROKE AND SUPPORT CHAINS BROKE. CHAIN HIT PROPELLER AND CAUSED NOTICEABLE DAMAGE. DOOR ANNUNCIATOR LIGHT WAS NOT ILLUMINATED SO NO INDICATION OF ANY PROBLEM
- [SDR TIM2001F00010](https://openairdocs.org/sdr/TIM2001F00010.md): Bulkhead · cracked · Oct 15, 2001 · N153GA · Beech 1900C · Engine Cowling System
  > THE RIGHT ENGINE COWLING BULKHEAD AT STATION 238.18 THAT THE LOWER FRONT ENGINE COWLING ATTACHES TO WAS CRACKED ON THE RIGHT LOWER SIDE. THIS LOCATION IS WERE ONE OF THE FOUR BOLTS SECURE THE LOWER COWL TO THE BULKHEAD. (PICTURES INCLUDED)
- [SDR 2001F00624](https://openairdocs.org/sdr/2001F00624.md): Shaft · damaged · Oct 4, 2001 · N153GA · Beech 1900C · Trailing Edge Flap Control System
  > INSPECTION OF THE FLAP CABLES AS OUTLINED IN BEECH S/B 27-3397 PER AD 2001-18-07 REVEALED THE CABLES DIAGONAL WRAP TO BE UNWINDING. CONTINUED INSPECTION REVEALED THAT THREE OF THE FOUR CABLES TO BE UNWINDING. THE CABLES WERE INSTALLED IN THE CORRECT FASHION.
- [SDR 2001F00622](https://openairdocs.org/sdr/2001F00622.md): Shaft · damaged · Oct 4, 2001 · N153GA · Beech 1900C · Trailing Edge Flap Control System
  > INSPECTION OF THE FLAP CABLES AS OUTLINED IN BEECH S/B 27-3397 PER AD 2001-18-07 REVEALED THE CABLES DIAGONAL WRAP TO BE UNWINDING. CONTINUED INSPECTION REVEALED THAT THREE OF THE FOUR CABLES TO BE UNWINDING. THE CABLES WERE INSTALLED IN THE CORRECT FASHION.
- [SDR 2001F00621](https://openairdocs.org/sdr/2001F00621.md): Shaft · damaged · Oct 4, 2001 · N153GA · Beech 1900C · Trailing Edge Flap Control System
  > INSPECTION OF THE FLAP CABLES AS OUTLINED IN BEECH S/B 27-3397 PER AD 2001-18-07 REVEALED THE CABLES DIAGONAL WRAP TO BE UNWINDING. CONTINUED INSPECTION REVEALED THAT THREE OF THE FOUR CABLES TO BE UNWINDING. THE CABLES WERE INSTALLED IN THE CORRECT FASHION.
- [SDR TIM2001F00008](https://openairdocs.org/sdr/TIM2001F00008.md): Motor · shorted · Sep 6, 2001 · N153GA · Beech 1900C · Air Distribution Fan
  > AIRCRAFT FILLED WITH SMOKE, CREW MADE AN EMERGENCY LANDING. CHECK OF AIRCRAFT SYSTEMS FOUND THE FORWARD EVAPORATOR MOTOR SHORTED. AIRCRAFT WAS FURTHER INSPECTED FOR DAMAGE, NONE FOUND.
- [SDR 20010507CW019](https://openairdocs.org/sdr/20010507CW019.md): Stringer · corroded · Mar 7, 2001 · N153GA · Beech 1900C · Fuselage Main, Longeron/Stringer
  > INSPECTION REVEALED A.6 INCH SECTION OF FUSELAGE STRINGER 14L CORRODED AT APPROX F.S. 250 FUSELAGE SKIN WAS NOT DAMAGED.
- [SDR 20010507CW015](https://openairdocs.org/sdr/20010507CW015.md): Bracket · corroded · Mar 7, 2001 · N153GA · Beech 1900C · Elevator Structure
  > INSPECTION DISCOVERED SIGNIFICANT CORROSION ON 2 RT ELEVATOR HINGE BRACKETS.
- [SDR 20010507CW014](https://openairdocs.org/sdr/20010507CW014.md): Bracket · corroded · Mar 7, 2001 · N153GA · Beech 1900C · Elevator Structure
  > INSPECTION DISCOVERED SIGNIFICANT CORROSION ON 2 RT ELEVATOR HINGE BRACKETS.
- [SDR 20010507CW008](https://openairdocs.org/sdr/20010507CW008.md): Floor Support · corroded · Mar 7, 2001 · N153GA · Beech 1900C · Fuselage Miscellaneous Structure
  > 4 FLOOR SUPPORT BRACKETS WERE FOUND WITH SIGNIFICANT CORROSION ON THE TOP SURFACE WHERE THEY ARE IN CONTACT WITH THE HONEYCOMB FLOOR PANEL.
- [SDR 20010507CW007](https://openairdocs.org/sdr/20010507CW007.md): Floor Support · corroded · Mar 7, 2001 · N153GA · Beech 1900C · Fuselage Miscellaneous Structure
  > 4 FLOOR SUPPORT BRACKETS WERE FOUND WITH SIGNIFICANT CORROSION ON THE TOP SURFACE WHERE THEY ARE IN CONTACT WITH THE HONEYCOMB FLOOR PANEL.
- [SDR 20010507CW006](https://openairdocs.org/sdr/20010507CW006.md): Bracket · worn · Mar 7, 2001 · N153GA · Beech 1900C · Trailing Edge Flaps
  > INSPECTION FOUND ALL FLAP TRACK BRACKETS WORN BEYOND ACCEPTABLE LIMITS.
- [SDR 20010507CW005](https://openairdocs.org/sdr/20010507CW005.md): Bracket · worn · Mar 7, 2001 · N153GA · Beech 1900C · Trailing Edge Flaps
  > INSPECTION FOUND ALL FLAP TRACK BRACKETS WORN BEYOND ACCEPTABLE LIMITS.
- [SDR 20001228AP001](https://openairdocs.org/sdr/20001228AP001.md): Fire Loop · shorted · Aug 28, 2000 · N153GA · Beech 1900C · Fire Detection
  > FLT 9141 - TPA-RSW - DURING FLIGHT, LEFT ENGINE FIRE INDICATION OCCURRED. PRECAUTIONARY SHUTDOWN AND DISCHARGE OF ENGINE FIRE BOTTLE CARRIED OUT. REMOVED AND REPLACED LEFT ENGINE FORWARD FIRE LOOP DUE TO SHORT. REPLACED LEFT ENGINE FIRE BOTTLE. (M)
- [SDR 20000725AP005](https://openairdocs.org/sdr/20000725AP005.md): Hinge · corroded · Apr 19, 2000 · N153GA · Beech 1900C · Elevator Structure
  > DURING SCHEDULED MAINTENANCE, LEFT OUTBOARD ELEVATOR HINGE BRACKET MOUNTED ON THE STABILIZER SHOWED SIGNS OF INTERGRANULAR CORROSION. REMOVED AND REPLACED LEFT ELEVATOR OUTBOARD HINGE. (M)
- [SDR 20000427AP008](https://openairdocs.org/sdr/20000427AP008.md): Engine · failed · Feb 8, 2000 · N153GA · Beech 1900C · Powerplant System
  > FLT 9330 - TPA-JAX - WHILE IN DESCENT INTO JACKSONVILLE AT 10,000 FT, A LOUD SQUEALING NOISE WAS HEARD. LEFT ENGINE INDICATED ITT AND TORQUE FLUCTUATIONS. PILOT MADE THE DETERMINATION TO SHUT THE LEFT ENGINE DOWN. REMOVED ENGINE ASSEMBLY AND ROUTED TO PRATT
- [SDR 98ZZZX2870](https://openairdocs.org/sdr/98ZZZX2870.md): Switch · failed · May 24, 1998 · N153GA · Beech 1900C · Landing Gear Retraction/Extension System
  > TPA/MIA - FLT 7485 - LANDING GEAR INDICATOR CIRCUIT BOARD TRIPS WHEN GEAR RETRACTS AND WILL NOT RESET UNTIL GEAR IS DOWN AND LOCKED. REMOVED AND REPLACED GEAR UP LIMIT SWITCH. (X)
- [SDR 99ZZZX733](https://openairdocs.org/sdr/99ZZZX733.md): Switch · out of ajdust · Jun 22, 1997 · N153GA · Beech 1900C · Landing Gear Position and Warning
  > FPO/MIA - FLT 7410 - PILOT REPORT: CANNOT SILENCE WARNING HORN FOR GEAR. ADJUSTED BOTH LEFT AND RIGHT POWER LEVER SWITCHES. (X)
- [SDR 97ZZZM729](https://openairdocs.org/sdr/97ZZZM729.md): Relay · shorted · May 27, 1997 · N153GA · Beech 1900C · Landing Gear Retraction/Extension System
  > FLT 7168 - MCO-FLL, UNABLE TO LOWER GEAR, BREAKER POPPED, HYDRAULIC FLUID LOW LIGHT ILLUMINATED. MANUAL EXTENSION ACCOMPLISHED. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED LANDING GEAR POWER PACK RELAY. GEAR SWINGS ON JACKS SATISFACTORY. (M)
- [SDR 97ZZZM527](https://openairdocs.org/sdr/97ZZZM527.md): Switch · intermittent · Mar 3, 1997 · N153GA · Beech 1900C · Landing Gear Position and Warning
  > FLT 398 - TCB/FLL - LANDING GEAR LIGHT (INTRANSIT) WOULD NOT GO OFF WHEN LANDING GEAR WAS RETRACTED. NO EMERGENCY DECLARED. AIRCRAFT LANDED WITHOUT INCIDENT. AIRCRAFT FERRIED TO MIA. REPLACED LEFT MAIN LANDING GEAR DOWNLOCK SWITCH. OP ERATIONAL CHECKS SAT
- [SDR 97ZZZM150](https://openairdocs.org/sdr/97ZZZM150.md): Brakes · inoperative · Dec 25, 1996 · N153GA · Beech 1900C · Landing Gear Brake System
  > FLT 437 - TPA-MIA - RIGHT BRAKE INOP, SLIPS. CLEANED AND SERVICED BRAKES. OK FOR SERVICE. (M)
- [SDR 96ZZZX5988](https://openairdocs.org/sdr/96ZZZX5988.md): Warning Light · malfunctioned · Nov 1, 1996 · N153GA · Beech 1900C · Landing Gear Position and Warning
  > EYW/MIA - FLT 403 - PILOT REPORT: WHEELS WARNING LIGHT WILL NOT COME ON IN-FLIGHT. SYSTEM FUNCTIONS PROPERLY WHEN RETARDING POWER LEVERS BACK TO ACTUATE WARNING HORN.

## 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 = 'N153GA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N153GA/reports

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