# Service difficulty reports: N69549, cancelled Mar 5, 2022

A list on [N69549, cancelled Mar 5, 2022](https://openairdocs.org/deregistered/N69549-2022-03-05.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 · 79 reports

- [SDR 29GA94953061512](https://openairdocs.org/sdr/29GA94953061512.md): Skin · corroded · Jun 15, 2012 · N69549 · Beech 1900D · Fuselage Main, Plate/Skin
  > DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED FUSELAGE SKIN CORROSION AT STRINGER 15L AND 15R FS 408.25 TO FS 456.00. REMOVED DAMAGED AREA BETWEEN STRINGER 15R AND STRINGER 16 AT FS 423.25 AND INSTALLED REPAIR FILLER AND EXTERNAL DOUBLER REPAIR.
- [SDR 29GA94971081911A](https://openairdocs.org/sdr/29GA94971081911A.md): Truss · damaged · Aug 19, 2011 · N69549 · Beech 1900D · Engine Mount Section
  > REPORT: DURING MAGNETIC PARTICLE INSPECTION DISCOVERED ENGINE TRUSS TUBE DAMAGED. PERFORMED ENGINE TRUSS REPAIR IN ACCORDANCE WITH FAA APPROVED DATA CONTAINED IN DRAWING 1005272-7, 8110-3, DERT-510208-CE.
- [SDR 29GA94957081711A](https://openairdocs.org/sdr/29GA94957081711A.md): Skin · corroded · Aug 17, 2011 · N69549 · Beech 1900D · Wing, Plate/Skin
  > REPORT: DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED RIGHT WING UPPER SKIN TRAILING EDGE CORROSION AND DEBOND INBOARD OF WING STATION 209.97 DAMAGE 5/16 X 1/8 HOLE. REMOVED DAMAGED SKIN AND INSTALLED AN EXTERNAL REPAIR DOUBLER.
- [SDR 29GA94932081311A](https://openairdocs.org/sdr/29GA94932081311A.md): Unknown · malfunctioned · Aug 13, 2011 · N69549 · Beech 1900D · Landing Gear Retraction/Extension System
  > FLIGHT: 9180 EYW/TPA PILOT REPORTED LANDING GEAR WILL NOT RETRACT RETURNED EYW LANDED WITHOUT INCIDENT. UNABLE TO DUPLICATE OPERATIONAL CHECK NORMAL.
- [SDR 29GA94971062811A](https://openairdocs.org/sdr/29GA94971062811A.md): Truss · cracked · Jun 28, 2011 · N69549 · Beech 1900D · Engine Mount Section
  > DURING MAGNETIC PARTICLE INSPECTION DISCOVERED ENGINE TRUSS COWLING ATTACH BRACKETS WELD AREA CRACKS AND RIGHT FORWARD LOWER ENGINE MOUNT ATTACH POINT WELD AREA CRACK. PERFORMED WELD REPAIR TO ENGINE TRUSS ATTACH BRACKETS WELD AREAS AND RIGHT FORWARD LOWER EN
- [SDR GUUA94955040511B](https://openairdocs.org/sdr/GUUA94955040511B.md): Stringer · cracked · Apr 5, 2011 · N69549 · Beech 1900D · Vertical Stabilizer, Spar/Rib
  > DURING SCHEDULED ROUTINE INSP, DISCOVERED VERTICAL STAB RT SIDE APPEARS TO HAVE CRACKS AT EACH OF THE 3 CHORD STRINGERS AT CSS 54.026. STOP DRILLED CRACKS AND INSTALLED REPAIR STRAPS THREE EACH.
- [SDR GUUA94955040511A](https://openairdocs.org/sdr/GUUA94955040511A.md): Rib · cracked · Apr 5, 2011 · N69549 · Beech 1900D · Vertical Stabilizer, Spar/Rib
  > DURING SCHEDULED ROUTINE INSP, DISCOVERED VERTICAL STABILIZER LT SIDE, 1 CRACK AT CSS 54.026. STOP DRILLED CRACK AND INSTALLED REPAIR STRAP.
- [SDR GUUA94932032411A](https://openairdocs.org/sdr/GUUA94932032411A.md): Relay · shorted · Mar 24, 2011 · N69549 · Beech 1900D · Landing Gear Retraction/Extension System
  > PILOT REPORTED LANDING GEAR WILL NOT RETRACT. CONTINUED, LANDED WITHOUT INCIDENT. REPLACED K3 RELAY LANDING GEAR OPS CHECK GOOD.
- [SDR GUUA94952012011B](https://openairdocs.org/sdr/GUUA94952012011B.md): Cable · broken · Jan 20, 2011 · N69549 · Beech 1900D · Passenger/Crew Doors
  > PILOT REPORTED RT CABLE ON AIRSTAIR DOOR BROKEN. REPLACED RT AIRSTAIR DOOR CABLE ASSY.
- [SDR GUUA94952012011A](https://openairdocs.org/sdr/GUUA94952012011A.md): Control Cable · broken · Jan 20, 2011 · N69549 · Beech 1900D · Passenger/Crew Doors
  > PILOT REPORTED LT CABLE ON AIRSTAIR DOOR BROKEN. REPLACED FWD LOWER CABLE CONTROL ASSY OPS CHECK NORMAL.
- [SDR GUUA94952062910A](https://openairdocs.org/sdr/GUUA94952062910A.md): Hand Rail · out of position · Jun 29, 2010 · N69549 · Beech 1900D · Passenger/Crew Doors
  > FLIGHT 9174 PILOT REPORTED DURING PREFLIGHT FOUND CABIN DOOR HARD TO OPEN. REPOSITIONED CABIN DOOR TOP HANDRAIL CABLE OPERATIONAL CHECKED GOOD.
- [SDR GUUA94952061910A](https://openairdocs.org/sdr/GUUA94952061910A.md): Door · binding · Jun 19, 2010 · N69549 · Beech 1900D · Passenger/Crew Doors
  > PILOT REPORTED CABIN DOOR DIFFICULT TO OPEN. CLEANED EXCESS GREASE FROM LOCKING MECHANISM, OPS CK GOOD.
- [SDR GUUA94952061710A](https://openairdocs.org/sdr/GUUA94952061710A.md): Cable Assy · frayed · Jun 17, 2010 · N69549 · Beech 1900D · Entrance Stairs
  > DURING SCHEDULED ROUTINE MX DISCOVERED AIRSTAIR DOOR LWR FWD CABLE FRAYED. REPLACED AIRSTAIR DOOR LOWER FWD CABLE.
- [SDR GUUA94934053010A](https://openairdocs.org/sdr/GUUA94934053010A.md): Altimeter · intermittent · May 30, 2010 · N69549 · Beech 1900D · Altimeter, Barometric/Encoder
  > CAPT'S ALTIMETER WORKING INTERMITTENTLY THROUGHOUT CLIMB. R & R CAPTAIN'S ALTIMETER. OPS CHECKS SATISFACTORY AT THIS TIME.
- [SDR GUUA94932050410A](https://openairdocs.org/sdr/GUUA94932050410A.md): Indicator · inoperative · May 4, 2010 · N69549 · Beech 1900D · Landing Gear Position and Warning
  > PILOT REPORTED "HH" LANDING GEAR ANNUNCIATOR INOPERATIVE. REPLACED LANDING GEAR INDICATOR ASSY, OPS CHECK GOOD.
- [SDR GUUA94957041210A](https://openairdocs.org/sdr/GUUA94957041210A.md): Skin · corroded · Apr 12, 2010 · N69549 · Beech 1900D · Wing, Plate/Skin
  > DURING SCHEDULED ROUTINE INSP DISCOVERED LT WING T/E BY THE NR 1 FLAP, 2 SPOTS OF SURFACE CORROSION. DURING CLEANING OF SURFACE CORROSION DISCOVERED UPPER WING SKIN CORROSION BETWEEN LWS 136 THROUGH 196. REMOVED DAMAGED SKIN AND INSTALLED AN EXTERNAL REPAIR
- [SDR GUUA94957121009A](https://openairdocs.org/sdr/GUUA94957121009A.md): Stringer · corroded · Dec 10, 2009 · N69549 · Beech 1900D · Wing, Longeron/Stringer
  > DURING REMOVAL OF MINOR CORROSION FROM LT WING COLLECTOR TANK J STRINGER, DISCOVERED CORROSION OUT OF LIMITS BETWEEN WS 114.25 TO WS 124.25. REMOVED CORROSION AND INSTALLED EXTERNAL REPAIR STRAP.
- [SDR GUUA94953120809A](https://openairdocs.org/sdr/GUUA94953120809A.md): Skin · corroded · Dec 8, 2009 · N69549 · Beech 1900D · Fuselage Main, Plate/Skin
  > DURING SCHEDULED ROUTINE INSP, DISCOVERED CORROSION ON ACFT BELLY SKIN AT FS 243.280 TO 258.280. REMOVED DAMAGED SKIN AND INSTALLED AN EXTERNAL DOUBLER REPAIR.
- [SDR GUUA94957120109B](https://openairdocs.org/sdr/GUUA94957120109B.md): Stringer · corroded · Dec 1, 2009 · N69549 · Beech 1900D · Wing, Longeron/Stringer
  > DURING SCHEDULED RT WING X-RAY INSP, DISCOVERED SPOTS OF CORROSION ON FWD BONDED STRINGER OTBD OF WS 124.25. REMOVED CORROSION AND INSTALLED AN EXTERNAL REPAIR STRAP.
- [SDR GUUA94957120109A](https://openairdocs.org/sdr/GUUA94957120109A.md): Spar · corroded · Dec 1, 2009 · N69549 · Beech 1900D · Wing Spar
  > DURING SCHEDULED LT WING X-RAY INSP, DISCOVERED SURFACE CORROSION ON MAIN SPAR AFT FLANGE BETWEEN WS 114.25 TO 124.25. REMOVED CORROSION AND INSTALLED AN INTERNAL REPAIR STRAP AND EXTERNAL DOUBLER REPAIR.
- [SDR GUUA94957113009A](https://openairdocs.org/sdr/GUUA94957113009A.md): Skin · corroded · Nov 30, 2009 · N69549 · Beech 1900D · Wing, Plate/Skin
  > DURING SCHEDULED ROUTINE INSP, DISCOVERED RT WING UPPER SKIN T/E CORROSION AND DEBOND BETWEEN WS 133.86 TO WS 173.50. REMOVED DAMAGE AND INSTALLED EXTERNAL DOUBLER REPAIR.
- [SDR GUUA94952102009A](https://openairdocs.org/sdr/GUUA94952102009A.md): Latch · damaged · Oct 20, 2009 · N69549 · Beech 1900D · Entrance Stairs
  > PILOT REPORTED AIRSTAIR DOOR ONCE CLOSED, LATCH DIFFICULT TO TURN AND LOCK. RIGGED LATCH POST. OPS CHECK GOOD.
- [SDR GUUA94952101709A](https://openairdocs.org/sdr/GUUA94952101709A.md): Hinge · damaged · Oct 17, 2009 · N69549 · Beech 1900D · Entrance Stairs
  > PILOT REPORTED WHEN CLOSING MAIN CABIN DOOR, UPPER LT CAM LOCK SCRAPES AGAINST LOCK. REPLACED AIRSTAIR DOOR TOP AND BOTTOM HINGES.
- [SDR GUUA94952101609A](https://openairdocs.org/sdr/GUUA94952101609A.md): Door · out of adjust · Oct 16, 2009 · N69549 · Beech 1900D · Passenger/Crew Doors
  > PILOT REPORTED CABIN DOOR VERY HARD TO CLOSE. LUBRICATED CAMS AND REPOSITIONED DOOR CABLES. OPS CHECK GOOD.
- [SDR GUUA94957091409A](https://openairdocs.org/sdr/GUUA94957091409A.md): Access Panel · leaking · Sep 14, 2009 · N69549 · Beech 1900D · Wing, Plate/Skin
  > DURING SCHEDULED ROUTINE INSP DISCOVERED RT WING COLLECTOR TANK FUEL ACCESS PANEL 632 AT, FUEL LEAK. FABRICATED AND INSTALLED EXTERNAL DOUBLER RING FOR RT UPPER WING FUEL ACCESS PANEL 632 AT.
- [SDR GUUA94927081309B](https://openairdocs.org/sdr/GUUA94927081309B.md): Horn · corroded · Aug 13, 2009 · N69549 · Beech 1900D · Elevator Control System
  > DURING SCHEDULED ROUTINE INSP, DISCOVERED LT ELEVATOR TRIM TAB INBD CONTROL HORN EXFOLIATED. REPLACED LT ELEVATOR TRIM TAB ASSY.
- [SDR GUUA94927081309A](https://openairdocs.org/sdr/GUUA94927081309A.md): Torque Tube · corroded · Aug 13, 2009 · N69549 · Beech 1900D · Elevator Control System
  > DURING SCHEDULED INSP, DISCOVERED LT ELEVATOR TORQUE TUBE SHOW SIGNS OF EXFOLIATION. REPLACED LT ELEVATOR TORQUE TUBE.
- [SDR GUUA94921072609A](https://openairdocs.org/sdr/GUUA94921072609A.md): Unknown · odor · Jul 26, 2009 · N69549 · Beech 1900D · Air Distribution System
  > AFTER TAKEOFF WHEN BLEED AIR VALVES TURNED TO OPEN BURNING ODOR FROM PANEL VENTS WAS DETECTED. PERFORMED ENGINE RUN AT TAKEOFF AND CRUISE POWER SETTINGS OPENED BOTH BLEEDS NO BURNING ODOR OR SMOKE PRESENT.
- [SDR GUUA94952030509A](https://openairdocs.org/sdr/GUUA94952030509A.md): Cable Assy · frayed · Mar 5, 2009 · N69549 · Beech 1900D · Entrance Stairs
  > DURING SCHEDULED ROUTINE INSP, DISCOVERED AIRSTAIR DOOR COUNTER BALANCE CABLE ASSEMBLY FRAYED. REPLACED AIRSTAIR DOOR COUNTER BALANCE CABLE ASSY.
- [SDR GUUA94952020509A](https://openairdocs.org/sdr/GUUA94952020509A.md): Door · stiff · Feb 5, 2009 · N69549 · Beech 1900D · Emergency Exits
  > DURING SCHEDULED ROUTINE MX DISCOVERED RT AFT EMERGENCY EXIT DOOR DIFFICULT TO OPEN. LUBRICATED RT AFT EMERGENCY EXIT DOOR INTERIOR LOCKING MECHANISM.
- [SDR GUUA10130801](https://openairdocs.org/sdr/GUUA10130801.md): Dampener · cracked · Oct 13, 2008 · N69549 · Beech 1900D · Passenger/Crew Doors
  > DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED AIRSTAIR DOOR COUNTER BALANCE SUPPORT ASSEMBLY DAMPENER CRACK. REPLACED AIRSTAIR DOOR COUNTER BALANCE UPPER SUPPORT ASSEMBLY DAMPENER.
- [SDR GUUA10100803](https://openairdocs.org/sdr/GUUA10100803.md): Lock · lack of lube · Oct 10, 2008 · N69549 · Beech 1900D · Emergency Exits
  > AT SCHEDULED ROUTINE MAINT, DISCOVERED RT AFT EMERGENCY EXIT FROZEN AND WILL NOT OPEN, APPLIED LUBRICANT TO RT AFT EMERGENCY EXIT LOCKING ASSY. OPERATIONAL CHECK NORMAL.
- [SDR GUUA10100802](https://openairdocs.org/sdr/GUUA10100802.md): Lock · lack of lube · Oct 10, 2008 · N69549 · Beech 1900D · Emergency Exits
  > AT SCHEDULED ROUTINE MAINT DISCOVERED LT AFT EMERGENCY EXIT FROZEN AND WILL NOT OPEN. APPLIED LUBRICANT TO LT AFT EMERGENCY EXIT LOCKING ASSY. OPS CHECK NORMAL.
- [SDR GUU2008F00055](https://openairdocs.org/sdr/GUU2008F00055.md): Relay · failed · Sep 24, 2008 · N69549 · Beech 1900D · Landing Gear Retraction/Extension System
  > FLIGHT 9132 MIA/TPA PILOT DISCREPANCY. DURING APPROACH WHEN LANDING GEAR CONTROL SELECTED DOWN CIRCUIT BREAKER POPPED. HAD TO RESET SEVERAL TIMES BEFORE ALL GEAR CAME DOWN AND LOCKED 3 GREEN. C/A REPLACED LANDING GEAR RELAY. OPS CHECK NORMAL. TEST FLIGHT
- [SDR GUU2008F00052](https://openairdocs.org/sdr/GUU2008F00052.md): Circuit Breaker · popped · Sep 21, 2008 · N69549 · Beech 1900D · Landing Gear Retraction/Extension System
  > FLIGHT 9130 FPO/FLL PILOT DISCREPANCY DURING APPROACH, WHEN LANDING GEAR HANDLE SELECTED DOWN THE LANDING GEAR CIRCUIT BREAKER POPPED. RESET THE CIRCUIT BREAKER AND THE LANDING GEAR EXTENDED NORMALLY. C/A TROUBLE SHOT LANDING GEAR SYSTEM. NO DEFECTS NOTED.
- [SDR GUU2008F00040](https://openairdocs.org/sdr/GUU2008F00040.md): Hinge Bracket · corroded · Aug 9, 2008 · N69549 · Beech 1900D · Elevator Structure
  > AT SCHEDULED ROUTINE MAINTENANCE DISCOVERED LT INBOARD ELEVATOR HINGE BRACKET EXFOLIATED. REPLACED LT INBOARD ELEVATOR HINGE BRACKET. (S)
- [SDR GUU2008F00038](https://openairdocs.org/sdr/GUU2008F00038.md): Hinge Bracket · corroded · Aug 9, 2008 · N69549 · Beech 1900D · Elevator Structure
  > AT SCHEDULED ROUTINE MAINTENANCE DISCOVERED RT OUTBOARD ELEVATOR HINGE BRACKET EXFOLIATED. REPLACED RT OUTBOARD ELEVATOR HINGE BRACKET. (S)
- [SDR GUU2008F00037](https://openairdocs.org/sdr/GUU2008F00037.md): Hinge Bracket · corroded · Aug 9, 2008 · N69549 · Beech 1900D · Elevator Structure
  > AT SCHEDULED ROUTINE MAINTENANCE DISCOVERED LT CENTER ELEVATOR HINGE BRACKET EXFOLIATED. REPLACED LT CENTER ELEVATOR HINGE BRACKET. (S)
- [SDR GUUA11110701](https://openairdocs.org/sdr/GUUA11110701.md): Valve · intermittent · Nov 11, 2007 · N69549 · Beech 1900D · Landing Gear Retraction/Extension System
  > FLIGHT: 9276 EYW/FLL AFTER TAKEOFF THE LANDING GEAR REQUIRED RECYCLING FOUR TIMES TO RETRACT. REPLACED THE LANDING GEAR SERVICE VALVE. LANDING GEAR OPERATIONAL CHECK NORMAL.
- [SDR GUUA11100702](https://openairdocs.org/sdr/GUUA11100702.md): Control Handle · intermittent · Nov 10, 2007 · N69549 · Beech 1900D · Landing Gear Selector
  > FLIGHT: 9131, AFTER TAKEOFF LANDING GEAR DID NOT RETRACT WHEN LANDING GEAR SELECTED UP. RETURNED TO TPA. LANDED WITHOUT INCIDENT. REPLACED LANDING GEAR CONTROL HANDLE. LANDING GEAR EXTENSION AND RETRACTION OPERATIONAL CHECK NORMAL.
- [SDR GUUA11040701](https://openairdocs.org/sdr/GUUA11040701.md): Valve · misrigged · Nov 4, 2007 · N69549 · Beech 1900D · Landing Gear Retraction/Extension System
  > FLIGHT: 9279 DURING APPROACH, LANDING GEAR WOULD NOT EXTEND. MANUALLY EXTENDED LANDING GEAR. LANDED WITHOUT INCIDENT. FOUND LANDING GEAR GROUND SERVICE VALVE IN THE UP POSITION PLACED IN THE DOWN POSITION. LANDING GEAR EXTENSION AND RETRACTION OPERATIONAL CHE
- [SDR GUUA11020701](https://openairdocs.org/sdr/GUUA11020701.md): Squat Switch · out of adjust · Nov 2, 2007 · N69549 · Beech 1900D · Landing Gear Position and Warning
  > FLIGHT: 9128 AFTER TAKEOFF THE LANDING GEAR WOULD NOT RETRACT. RETURNED TO DEPARTURE. LANDED WITH OUT INCIDENT. READJUSTED RT MAIN LANDING GEAR SQUAT SWITCH.
- [SDR GUUA09130702](https://openairdocs.org/sdr/GUUA09130702.md): Handle · failed · Sep 13, 2007 · N69549 · Beech 1900D · Landing Gear Selector
  > DURING APPROACH LANDING GEAR DID NOT EXTEND ON THE FIRST AND SECOND SELECTION OF THE GEAR SELECTOR KNOB TO THE DOWN POSITION. RETURNED TO FLL LANDED WITHOUT INCIDENT. REPLACED LANDING GEAR HANDLE. OPERATIONAL CHECK NORMAL.
- [SDR GUUA09110702](https://openairdocs.org/sdr/GUUA09110702.md): Relay · failed · Sep 11, 2007 · N69549 · Beech 1900D · Landing Gear Position and Warning
  > AFTER TAKEOFF LANDING GEAR WOULD NOT RETRACT. REPLACED MLG RELAY, COULD NOT DUPLICATE OPERATIONAL CHECK NORMAL.
- [SDR GUUA08190701](https://openairdocs.org/sdr/GUUA08190701.md): Unknown · unknown · Aug 19, 2007 · N69549 · Beech 1900D · Landing Gear Retraction/Extension System
  > DURING APPROACH LANDING, GEAR WOULD NOT EXTEND WHEN GEAR HANDLE SELECTED DOWN, DIVERTED. MANUALLY EXTENDED LANDING GEAR. LANDED WITHOUT INCIDENT. TROUBLESHOT SYSTEM COULD NOT DUPLICATE OPERATIONAL CHECK NORMAL.
- [SDR GUUA07140701](https://openairdocs.org/sdr/GUUA07140701.md): Unknown · unknown · Jul 14, 2007 · N69549 · Beech 1900D · Landing Gear System
  > DURING APPROACH LANDING GEAR WOULD NOT EXTEND WITH THE GEAR HANDLE DOWN, CYCLED LANDING GEAR AND THE RT GEAR EXTENDED PARTIALLY THEN 10 SECONDS LATER ALL GEARS EXTENDED. INSPECTED LANDING GEAR SYSTEM NO DEFECTS NOTED. LANDING GEAR OPERATIONAL TEST NORMAL. TES
- [SDR GUUA03180701](https://openairdocs.org/sdr/GUUA03180701.md): Hinge Bracket · corroded · Mar 18, 2007 · N69549 · Beech 1900D · Horizontal Stabilizer Structure
  > AT SCHEDULED ROUTINE MAINTENANCE LT OB ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REPLACED LT OB ELEVATOR HINGE BRACKET.
- [SDR GUUA94957060206A](https://openairdocs.org/sdr/GUUA94957060206A.md): Spar Cap · damaged · Jun 2, 2006 · N69549 · Beech 1900D · Wing Spar
  > RT WING REAR SPAR LOWER CAP AFT FLANGE DEFLECTED.046 INCHES UPWARD. LOCATED AT WS 104.50. HAND FORMED SPAR FLANGE BACK TO ORIGINAL PROFILE, PERFORMED NDT EDDY CURRENT INSP BY A QUALIFIED LEVEL III INSPECTOR NO CRACK INDICATIONS NOTED. FABRICATED AND INSTALL
- [SDR GUUA05210602](https://openairdocs.org/sdr/GUUA05210602.md): Spar Cap · damaged · May 21, 2006 · N69549 · Beech 1900D · Wing Spar
  > FLIGHT: 9137 SAQ/FLL RT LANDING GEAR COLLAPSE BACKWARDS ON LANDING FOUND RT WING REAR SPAR LOWER CAP AFT FLANGE DEFLECTED.046 INCHES UP. HAND FORMED SPAR FLANGE BACK TO ORIGINAL PROFILE PERFORMED NDT EDDY CURRENT INSPECTION BY A QUALIFIED LEVEL III INSPECTOR
- [SDR GUUA05210601](https://openairdocs.org/sdr/GUUA05210601.md): Bolt · broken · May 21, 2006 · N69549 · Beech 1900D · Landing Gear Retraction/Extension System
  > FLIGHT: 9137 SAQ/FLL DURING APPROACH RT MLG UNSAFE INDICATION. RT LANDING GEAR COLLAPSE BACKWARDS ON LANDING. FOUND RT MLG DRAG BRACE ATTACH BOLT BROKEN.

Next page: https://openairdocs.org/deregistered/N69549-2022-03-05/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 = 'N69549' AND deregistration_id = 'N69549-2022-03-05'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N69549-2022-03-05/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.