# Service difficulty reports: N172GA

A list on [N172GA](https://openairdocs.org/aircraft/N172GA.md).

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

- [SDR KGBR20200313001](https://openairdocs.org/sdr/KGBR20200313001.md): Tube · chafed · Mar 13, 2020 · N172GA · Beech 1900C · Fuel Storage
  > FOUND FUEL TANK INTERCONNECT TUBES IN LEFT AND RIGHT MAIN LANDING GEAR WELLS TO BE CHAFED WHERE THE TUBES PASS THROUGH THE OUT BOARD KEEL BEAM. THE RIGHT HAND SIDE WORN TO OVER 90% OF THE WALL THICKNESS. THE LEFT HAND SIDE WAS WORN TO APPROX 75% OF THE WALL T
- [SDR TIMA2018052230001](https://openairdocs.org/sdr/TIMA2018052230001.md): Bolt · broken · Apr 30, 2018 · N172GA · Beech 1900C · Main Landing Gear
  > RIGHT MAIN LANDING DRAG BRACE DISCONNECTED FROM WING ATTACH POINT. LANDING GEAR STRUT RETRACED THE AFT CONTACTING WING STRUCTURE. INVESTIGATION FOUND DRAG BRACE ATTACH BOLT BROKEN AT GREASE GALLEY.
- [SDR TIMA20170223003](https://openairdocs.org/sdr/TIMA20170223003.md): Switch · failed · Feb 23, 2017 · N172GA · Beech 1900C · Door Warning System
  > DURING TAKEOFF ROLL BAGGAGE DOOR ANNUNCIATION ILLUMINATED. PILOT ABORTED TAKEOFF. INSPECTION REVEALED THE NOSE BAGGAGE DOOR SWITCH HAD FAILED.
- [SDR TIMA20150915004](https://openairdocs.org/sdr/TIMA20150915004.md): Seat Track · corroded · Sep 15, 2015 · N172GA · Beech 1900C · Fuselage, Seat/Cargo Attach Fittings
  > DURING MX, THE RT SIDE SEAT RAIL WAS FOUND TO BE CORRODED.
- [SDR TIMA20150715003](https://openairdocs.org/sdr/TIMA20150715003.md): Seat Track · corroded · Sep 15, 2015 · N172GA · Beech 1900C · Fuselage, Seat/Cargo Attach Fittings
  > DURING MX INSPECTION, THE LT SIDE SEAT RAIL WAS FOUND TO BE CORRODED.
- [SDR TIMA20140402018](https://openairdocs.org/sdr/TIMA20140402018.md): Spar Cap · corroded · Apr 2, 2014 · N172GA · Beech 1900C · Wing Spar
  > INSPECTION REVEALED CORROSION DEVELOPING ON THE LT UPPER MAIN SPAR CAP UNDER THE VORTEX GENERATORS.
- [SDR TIMA20140312017](https://openairdocs.org/sdr/TIMA20140312017.md): Skin · cracked · Mar 12, 2014 · N172GA · Beech 1900C · Wing, Plate/Skin
  > SEVERAL CRACKS DEVELOPED IN THE SKIN OTBD OF THE LT NACELLE & AFT OF THE MAIN SPAR ORIGINATING FROM VARIOUS RIVETS.
- [SDR TIMA20140312016](https://openairdocs.org/sdr/TIMA20140312016.md): Skin · debonded · Mar 12, 2014 · N172GA · 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 TIMA20140312015](https://openairdocs.org/sdr/TIMA20140312015.md): Skin · debonded · Mar 12, 2014 · N172GA · Beech 1900C · Wing, Plate/Skin
  > RIGHT WING DEBOND. UPPER SKIN OF BONDED PANEL IN AREA AROUND FUEL BAY ACCESS OVAL PANEL DEBONDED FROM FUEL ACCESS DISH & HONEYCOMB CORE.
- [SDR TIMA20130617007](https://openairdocs.org/sdr/TIMA20130617007.md): Rib · cracked · Jun 17, 2013 · N172GA · Beech 1900C · Vertical Stabilizer, Spar/Rib
  > TWO CRACKS WERE DISCOVERED IN THE VERTICAL STABILIZER RIB AT CSS 69. REPAIRED IAW SRM 51-10-21.
- [SDR TIMA20130605006](https://openairdocs.org/sdr/TIMA20130605006.md): Doubler · cracked · Jun 5, 2013 · N172GA · Beech 1900C · Horizontal Stabilizer, Spar/Rib
  > A CRACK WAS DISCOVERED IN THE LT HORIZONTAL STABILIZER FWD SPAR DOUBLER. THE LT HORIZONTAL STABILIZER FORWARD SPAR DOUBLER WAS REPLACED WITH A NEW PART.
- [SDR TIMA20130531005](https://openairdocs.org/sdr/TIMA20130531005.md): Spar Cap · cracked · May 31, 2013 · N172GA · Beech 1900C · Vertical Stabilizer, Spar/Rib
  > A CRACK WAS DISCOVERED IN THE LT FWD SPAR CAP OF THE VERTICAL STABILIZER ABOVE CSS 61. REPAIRED IAW FR-CO-02599, REV 1.
- [SDR TIMA20130718004](https://openairdocs.org/sdr/TIMA20130718004.md): Tee Fitting · cracked · May 30, 2013 · N172GA · Beech 1900C · Horizontal Stabilizer Structure
  > DURING AN INSPECTION, A CRACK IN THE LT HORIZONTAL STABILIZER LOWER TEE EXTRUSION WAS DISCOVERED. REPAIRED THE CRACKED TEE EXTRUSION BY SPLICING IN A NEW SECTION IAW REPAIR FR-CO-02598. TWO REPAIR ANGLES WERE FABRICATED USING A SECTION OF A NEW TEE.
- [SDR TIMA2010000010](https://openairdocs.org/sdr/TIMA2010000010.md): Actuator · cracked · Mar 4, 2010 · N172GA · Beech 1900C · Landing Gear Actuator
  > MAIN LANDING GEAR ACTUATOR ROD END CAP FOUND CRACKED DURING NDT INSPECTION TO C/W AD 2009-23-01.
- [SDR TIMA20090002](https://openairdocs.org/sdr/TIMA20090002.md): Skin · corroded · Apr 3, 2009 · N172GA · Beech 1900C · Fuselage Main, Plate/Skin
  > WHILE CLEANING LITE CORROSION ON SURFACE OF BELLY AFT OF WINGS, NOTICED SOME APPARENT BLISTERING OF THE SKIN. INVESTIGATION REVEALED THERE WAS CORROSION BETWEEN THE SKIN AND THE FUSELAGE FRAME. AFFECTED SKIN WAS CUT OUT AND REPLACED AS A COVER PATCH IN ACCOR
- [SDR 2006FA0000837](https://openairdocs.org/sdr/2006FA0000837.md): Fire Loop · broken · Jun 7, 2006 · N172GA · Beech 1900C · Fire Detection
  > PILOT EXPERIENCED A FIRE WARNING ANNUNCIATION DURING TAKEOFF ROLL. PILOT ABORTED TAKEOFF. MAINTENANCE FOUND THAT ONE FIRELOOP HAD FAILED AND CAUSED THE FALSE FIRE INDICATION. (K)
- [SDR TIMR74](https://openairdocs.org/sdr/TIMR74.md): Skin · cracked · Jul 9, 2002 · N172GA · Beech 1900C · Horizontal Stabilizer, Plate/Skin
  > LEADING EDGE OF STABILIZER DISBONDED ON LOWER SIDE AND A CRACK FORMED JUST OFF THE END CAP AND COMPOSITE JOINT. (CONTROL NR 74)
- [SDR TIM2002F00010](https://openairdocs.org/sdr/TIM2002F00010.md): Angle · broken · Feb 15, 2002 · N172GA · Beech 1900 · Nacelle/Pylon, Main Frame
  > ANGLE LOCATED ABOVE THE ICE DOOR HINGE. THIS ANGLE HOLDS THE LOWER FIRE SEAL BULK HEAD WHEN THIS ANGLE CRACKS, IT ALLOWS THE OUTSIDE COWL RIVETS TO WORK LOOSE, AND THIS CAUSES THE COWL SIDE SKIN TO CRACK.
- [SDR TIM2002F00009](https://openairdocs.org/sdr/TIM2002F00009.md): Bolt · corroded · Jan 16, 2002 · N172GA · Beech 1900 · Nose/Tail Landing Gear Strut/Axle
  > BOLT PN 908200115, CONNECTING NOSE GEAR DRAG BRACE TO NOSE STRUT, AND BOLT PN 908200111 CONNECTING THE TWO DRAG BRACE HALVES WAS FOUND WITH PITTING TYPE CORROSION.
- [SDR TIM2002F00004](https://openairdocs.org/sdr/TIM2002F00004.md): Cable · broken · Dec 4, 2001 · N172GA · Beech 1900 · Entrance Stairs
  > AIRSTAIR DOOR CABLE BROKE, ALLOWING ONE SIDE OF THE DOOR TO REMAIN UNLOCKED.
- [SDR TIM2001F00011](https://openairdocs.org/sdr/TIM2001F00011.md): Wire · broken · Oct 16, 2001 · N172GA · Beech 1900 · Ice/Rain Protection System Wiring
  > THE ICE VANE CONTROL WIRE NUMBER 20A20 BROKE AT THE TERMINAL END UNDER THE PANEL AT INST ZONE 245 CAUSING A SHORT WHICH CAUSED SMOKE IN THE COCKPIT.
- [SDR 2001F00623](https://openairdocs.org/sdr/2001F00623.md): Shaft · defective · Oct 4, 2001 · N172GA · Beech 1900 · Trailing Edge Flap Control System
  > INSPECTION OF FLAP CABLES AS OUTLINED IN BEECH S/B 27-3397 PER AD 2001-18-07 REVEALED THE RIGHT OUTBOARD FLAP CABLE DEFECTIVE. THE INNER SHAFT RETAINER WAS NOT ATTACHED TO THE FERRULE AS REQUIRED. (M)
- [SDR TIM2001F00006](https://openairdocs.org/sdr/TIM2001F00006.md): B-Nut · loose · May 22, 2001 · N172GA · Beech 1900 · Engine Oil Distribution (Airframe Furnished)
  > OIL LINE TO THE TORQUE MANIFOLD, B-NUT CAME LOOSE, OIL PRESSURE FLUCTUATED AND ENGINE SHUT DOWN. AIRCRAFT LANDED. ENGINE WAS INSPECTED AS PER MM, LOW OIL PRESSURE PROCEDURE. NO DAMAGE FOUND - OIL SERVICED AND ENGINE TEST RUN PER P/W CHECK.
- [SDR 20010613CW015](https://openairdocs.org/sdr/20010613CW015.md): B-Nut · loose · May 22, 2001 · N172GA · Beech 1900C · Engine Oil Distribution (Airframe Furnished)
  > OIL LINE TO THE TORQUE MANIFOLD B-NUT CAME LOOSE. OIL PRESSURE FLUCTUATED AND ENGINE SHUT DOWN. AIRCRAFT LANDED. ENGINE WAS INSPECTED AS PER PWA MM. LOW OIL PRESSURE PROCEDURE, NO DAMAGE FOUND. OIL SERVICED AND ENGINE TEST RUN, PER PWA CHECK.
- [SDR 20010507CW013](https://openairdocs.org/sdr/20010507CW013.md): Cap · corroded · Apr 4, 2001 · N172GA · Beech 1900C · Horizontal Stabilizer Structure
  > LOWER CAP LEFT STABILIZER OUTER 6 IS CORRODED.
- [SDR 20010507CW011](https://openairdocs.org/sdr/20010507CW011.md): Trim Tab · corroded · Apr 4, 2001 · N172GA · Beech 1900C · Aileron Tab Control System
  > LEFT AILERON TRIM TAB HORN CORRODED.
- [SDR 20010509CW006](https://openairdocs.org/sdr/20010509CW006.md): Spar Cap · corroded · Apr 2, 2001 · N172GA · Beech 1900C · Horizontal Stabilizer, Spar/Rib
  > FOUND THE OUTBOARD 6 INCHES LOWER RIGHT REAR SPAR CAP EXTRUSION CORRODED. CORROSION WAS FOUND WHILE REPLACING A CORRODED OUTBOARD ELEVATOR HINGE BRACKET.
- [SDR 20010509CW005](https://openairdocs.org/sdr/20010509CW005.md): Intercostal · cracked · Apr 2, 2001 · N172GA · Beech 1900C · Fuselage Miscellaneous Structure
  > P43 INSPECTION FOUND A.8 INCH CRACK IN THE OUTDBOARD FLANGE RADIUS OF THE INTERCOSTAL AT THE UPPER CARGO DOOR FRAME AT FS 494.
- [SDR 20010509CW004](https://openairdocs.org/sdr/20010509CW004.md): Hinge Bracket · corroded · Apr 2, 2001 · N172GA · Beech 1900C · Elevator Structure
  > DURING INSPECTION, THE RIGHT OUTBOARD AND THE RIGHT MIDDLE ELEVATOR HINGE BRACKET WERE FOUND TO BE CORRODED.
- [SDR 20001103AP007](https://openairdocs.org/sdr/20001103AP007.md): Block · worn · May 22, 2000 · N172GA · Beech 1900C · Propeller System
  > FLT 9410 - MIA/EYW - AFTER ROTATION, RIGHT PROP RPM DROPPED TO APPROXIMATELY 1200 RPM. RETURNED TO MIA. DETERMINED RIGHT BETA BLOCK TO BE WORN. REPLACED RIGHT BETA BLOCK AND RIGGED. (M)
- [SDR 20000619AP012](https://openairdocs.org/sdr/20000619AP012.md): Nozzle · loose · Mar 20, 2000 · N172GA · Beech 1900C · Engine Collector/Tailpipe/Nozzle
  > FLT 9209 - ON CLIMB-OUT FROM TAMPA, RIGHT T-HANDLE FIRE WARNING ILLUMINATED. PILOT SHUT DOWN ENGINE, DECLARED EMERGENCY AND RETURNED TO TAMPA. AIRCRAFT LANDED WITHOUT INCIDENT. INSPECTED RIGHT ENGINE. NO EVIDENCE OF FIRE. DETERMINED TO BE HOT AIR LEAKING

## 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 = 'N172GA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N172GA/reports

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