# Service difficulty reports: N16729, cancelled Oct 25, 2007

A list on [N16729, cancelled Oct 25, 2007](https://openairdocs.org/deregistered/N16729-2007-10-25.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 · 73 reports

- [SDR C2XA01IA397](https://openairdocs.org/sdr/C2XA01IA397.md): Landing Gear · malfunctioned · Nov 8, 2001 · N16729 · Emb EMB120ER · Landing Gear Retraction/Extension System
  > ROW - CREW REPORTED THAT THE LANDING GEAR SYSTEM FAILED TO EXTEND WHILE ON APPROACH. THE CREW PERFORMED A MANUAL EXTENSION OF THE GEAR AND LANDED AT ROW WITHOUT FURTHER INCIDENT. AWAITING A MAINTENANCE ACTION TO COMPLETE THIS REPORT.
- [SDR C2XA01IA312](https://openairdocs.org/sdr/C2XA01IA312.md): Pump · faulty · Aug 3, 2001 · N16729 · Emb EMB120ER · Engine Fuel Pump
  > IAH - FLIGHT 3050, THE CREW REPORTED THAT THE NUMBER TWO ENGINE EXPERIENCED A SUDDEN POWER LOSS DURING CLIMBOUT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO ENGINE DRIVEN FUEL PUMP, AND THE A
- [SDR C2XA01IA311](https://openairdocs.org/sdr/C2XA01IA311.md): Hmu · unserviceable · Aug 3, 2001 · N16729 · Emb EMB120ER · Engine Fuel and Control
  > IAH - FLIGHT 3050, THE CREW REPORTED THAT THE NUMBER TWO ENGINE EXPERIENCED A SUDDEN POWER LOSS ON CLIMBOUT. THE AIRCRAFT RETURNED TO IAH WITHOUT INCIDENT WHER MAINTENANCE REMOVED AND REPLACED THE AFFECTED HYDROMECHANICAL METERING UNIT IN ACCORDANCE WITH PW118
- [SDR C2XA01IA296](https://openairdocs.org/sdr/C2XA01IA296.md): A/C Pack · malfunctioned · Jul 13, 2001 · N16729 · Emb EMB120ER · Cabin Cooling System
  > BPT- FLIGHT 3083, AFTER TAKEOFF THE CREW NOTED SMOKE IN THE CABIN, THE LAV SMOKE ALARM ACTIVATED, (RT PACK FAIL FIVE MINUTES PRIOR TO SMOKE), AND THE AIRCRAFT RETURNED TO BPT WITHOUT INCIDENT. BPT- MAINTENANCE INSPECTED THE AIRCRAFT AND THE RIGHT PACK WAS PLA
- [SDR C2XA01IA270](https://openairdocs.org/sdr/C2XA01IA270.md): Battery Pack · discharged · Jun 19, 2001 · N16729 · Emb EMB120ER · Emergency Lighting
  > IAH - DURING A-CHECK INSPECTION, THE AISLE PATH EMERGENCY EXIT LIGHTS WERE FOUND TO BE MALFUNCTIONING. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY PACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA01IA269](https://openairdocs.org/sdr/C2XA01IA269.md): Control Cable · frayed · Jun 18, 2001 · N16729 · Emb EMB120ER · Elevator Control System
  > IAH - DURING "A" CHECK INSPECTION, THE LEFT HAND INBOARD ELEVATOR CABLE WAS FOUND TO HAVE SEVERAL BROKEN STRANDS IN THE CARGO COMPARTMENT. MAINTENANCE REMOVED AND REPLACED THE EFFECTED CABLE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA01A015](https://openairdocs.org/sdr/C2XA01A015.md): Frame · cracked · Jan 8, 2001 · N16729 · Emb EMB120ER · Nacelle/Pylon, Frame/Spar/Rib
  > SHV - DURING MAINTENANCE INSPECTIN, THE LEFT NACELLE HALF FRAME FOR THE LEFT MAIN LANDING GEAR AFT OUTBOARD DOOR FORWARD HINGE POINT WAS FOUND TO BE CRACKED. THE AIRCRAFT WAS FERRIED TO IAH WHERE IT LANDED WITHOUT INCIDENT, AND MAINTNANCE PERFORMED A DOUBLER
- [SDR C2XA01IA029](https://openairdocs.org/sdr/C2XA01IA029.md): Frame · cracked · Jan 8, 2001 · N16729 · Emb EMB120ER · Nacelle/Pylon, Frame/Spar/Rib
  > IAH - DURING MAINTENANCE INSPECTION, THE LEFT NACELLE HALF FRAME FOR THE AFT OUTBOARD GEAR DOOR HINGE POINT WAS FOUND TO BE CRACKED. MAINTENANCE PERFORMED A DOUBLER REPAIR, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA01IA067](https://openairdocs.org/sdr/C2XA01IA067.md): Wire · chafed · Dec 5, 2000 · N16729 · Emb EMB120ER · Light System Wiring
  > IAH - DURING MAINTENANCE INSPECTION, THE FORWARD SECTION OF AISLE PATH EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPOSITIONED A CHAFED WIRE IN ACCORDANCE WITH EMB120 W/M 20-00-00, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA00IA437](https://openairdocs.org/sdr/C2XA00IA437.md): Power Supply · inoperative · Dec 4, 2000 · N16729 · Emb EMB120RT · Emergency Lighting
  > LCH - DURING POST FLIGHT INSPECTION, THE CREW REPORTED THAT THE FIRST HALF OF THE AISLE PATH EMERGENCY LIGHTING WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 2 EMERGENCY LIGHT POWER SUPPLY IAW EMB120 MM 33-50-02, AND THE AIRCRAFT WAS APPROVED FOR R
- [SDR C2XA01IA072](https://openairdocs.org/sdr/C2XA01IA072.md): Wire · broken · Dec 1, 2000 · N16729 · Emb EMB120ER · Light System Wiring
  > IAH - DURING POST-FLIGHT INSPECTION, THE CREW REPORTED THAT THE FORWARD SECTION OF AISLE PATH EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE IN THE STRIP, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XAOOIA403](https://openairdocs.org/sdr/C2XAOOIA403.md): Wire · broken · Nov 7, 2000 · N16729 · Emb EMB120RT · Light System Wiring
  > IAH-DURING POST FLIGHT INSPECTION, CREW REPORTED SEVERAL EMERGENCY LIGHTS TO BE INOPERATIVE. MX REPAIRED A BROKEN WIRE. A/C WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA00IA269](https://openairdocs.org/sdr/C2XA00IA269.md): Battery Pack · discharged · Aug 17, 2000 · N16729 · Emb EMB120RT · Emergency Lighting
  > EFD - DURING MAINTENANCE INSPECTION, THE AFT AISLE PATH EMERGENCY LIGHT BATTERY PACK WAS FOUND TO BE DISCHARGED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BATTERY PACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)
- [SDR C2XA00IA179](https://openairdocs.org/sdr/C2XA00IA179.md): Battery Pack · discharged · Jun 24, 2000 · N16729 · Emb EMB120RT · Emergency Lighting
  > IAH - DURING MAINTENANCE INSPECTION, THE AFT EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 3 EMERGENCY LIGHT BATTERY PACK IAW EMB120 MM 33-50-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)
- [SDR C2XA00IA129](https://openairdocs.org/sdr/C2XA00IA129.md): Strap · corroded · May 8, 2000 · N16729 · Emb EMB120RT · Fuselage Miscellaneous Structure
  > DURING CONTINENTAL EXPRESS C-CHECK, THE RIGHT BUTT STRAP WAS FOUND TO BE CORRODED FROM FRAME 13 TO JUST PAST FRAME 14. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF BUTT STRAP IAW EMB120 SRM 53-10-10, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SER
- [SDR C2XA00IA128](https://openairdocs.org/sdr/C2XA00IA128.md): Seat Track · corroded · May 8, 2000 · N16729 · Emb EMB120RT · Fuselage, Seat/Cargo Attach Fittings
  > DURING CONTINENTAL EXPRESS C-CHECK, THE LEFT SEAT TRACK WAS FOUND TO BE CORRODED FROM FRAME 33 TO FRAME 39. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF SEAT TRACK IAW EMB120 SRM 53-20-11, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)
- [SDR C2XA00IA127](https://openairdocs.org/sdr/C2XA00IA127.md): Frame · cracked · May 8, 2000 · N16729 · Emb EMB120RT · Nacelle/Pylon, Main Frame
  > DURING CONTINENTAL EXPRESS C-CHECK, THE RIGHT NACELLE FRAME ONE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FRAME IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5410-01034, AND THE AIRCRAFT WAS APPROVED FOR RE
- [SDR C2XA99CL096](https://openairdocs.org/sdr/C2XA99CL096.md): Pressurization · failed · Aug 23, 1999 · N16729 · Emb EMB120RT · Cabin Pressure Control System
  > AZO - FLT 3019 - THE CREW REPORTED A BURNING SMELL IN CLIMB BEFORE THE PRESSURIZATION FAILED. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED OPERATIONAL CHECKS OF THE AIRCONDITIONER SYSTEM BOTH PACKS OPERATED NORMAL IAW EMB120MM 21-00-00
- [SDR C2XA99CL094](https://openairdocs.org/sdr/C2XA99CL094.md): Light · inoperative · Aug 22, 1999 · N16729 · Emb EMB120RT · Emergency Lighting
  > CLE-SDF - FLT 3285 - THE CREW REPORTED THE LAST FIVE EMERGENCY LIGHT IN THE CABIN AISLE ARE INOPERATIVE. THE AIRCRAFT WAS AT THE GATE, NO FURTHER INCIDENTS REPORTED. MAINTENANCE PERFORMED OPERATIONAL CHECKS OF THE SYSTEM IAW EMB120MM 33-50-00, NO DEFECTS WER
- [SDR C2XA99CL046](https://openairdocs.org/sdr/C2XA99CL046.md): Pack · smoking · Jun 9, 1999 · N16729 · Emb EMB120RT · Cabin Cooling System
  > CLE - THE CREW REPORTED SMOKE IN THE CABIN AND COMING FROM THE RIGHT PACK, THE AIRCRAFT WAS TAXIING TO THE MAINTENANCE HANGAR FOR OTHER MAINTENANCE. MAINTENANCE PERFORMED OPERATIONAL CHECKS ON THE PACK SYSTEM IAW EMB-120 MM 21-00-00, NO DEFECTS WERE NOTED DUR
- [SDR C2XA99CL045](https://openairdocs.org/sdr/C2XA99CL045.md): Retract Mech · malfunctioned · Jun 9, 1999 · N16729 · Emb EMB120RT · Landing Gear Retraction/Extension System
  > DTW - THE LEFT MAIN LANDING GEAR WOULD NOT EXTEND, CREW USED THE MANUAL GEAR EXTENSION SYSTEM TO GET THE GEAR DOWN AND LOCKED. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. THE AIRCRAFT WAS FERRY FLIGHTED TO CLEVELAND FOR REPAIRS. MAINTENANCE PERFORMED SEVE
- [SDR C2XA99CL044](https://openairdocs.org/sdr/C2XA99CL044.md): Transducer · leaking · Jun 9, 1999 · N16729 · Emb EMB120RT · Hydraulic Pressure Sensor
  > DTW - DURING FLIGHT THE CREW LOST THE GREEN SYSTEM HYDRAULIC PRESSURE AND QUANTITY INDICATIONS. THE AIRCRAFT DIVERTED TO DTW WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE PRESSURE TRANSDUCER IAW EMB-120 MM 29-30-09. OPERATIONAL CHECKS OF TH
- [SDR C2XA98IA543](https://openairdocs.org/sdr/C2XA98IA543.md): Frame · corroded · Dec 18, 1998 · N16729 · Emb EMB120RT · Fuselage Main, Frame
  > DURING C-CHECK INSPECTION, FOUND THE RIGHT OUTBOARD CROSS FRAME AT FRAME 40 HEAVILY CORRODED. REMOVED AND REPLACED CROSS FRAME. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)
- [SDR C2XA98IA542](https://openairdocs.org/sdr/C2XA98IA542.md): Bracket · cracked · Dec 18, 1998 · N16729 · Emb EMB120RT · Trailing Edge Flaps
  > DURING C-CHECK INSPECTION, FOUND THE RIGHT WING INBOARD FLAP HINGE PANEL OUTBOARD ROLLER BRACKET CRACKED. REMOVED AND REPLACED ROLLER BRACKET. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)
- [SDR C2XA98IA541](https://openairdocs.org/sdr/C2XA98IA541.md): Support · corroded · Dec 18, 1998 · N16729 · Emb EMB120RT · Fuselage Miscellaneous Structure
  > DURING C-CHECK INSPECTION, FOUND THE LEFT OUTBOARD FLOOR SUPPORT BETWEEN FRAMES 44 AND 46 CORRODED. REMOVED AND REPLACED THE FLOOR SUPPORT. THE AIRCRAFT WAS APPROVED FOR RETURNED TO SERVICE. (M)
- [SDR C2XA98IA540](https://openairdocs.org/sdr/C2XA98IA540.md): Support · corroded · Dec 18, 1998 · N16729 · Emb EMB120RT · Fuselage Miscellaneous Structure
  > DURING C-CHECK INSPECTION, FOUND THE RIGHT OUTBOARD FLOOR SUPPORT FROM FRAME 40 TO 44 CORRODED. REMOVED AND REPLACED THE FLOOR SUPPORT. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)
- [SDR C2XA98IA539](https://openairdocs.org/sdr/C2XA98IA539.md): Support · corroded · Dec 18, 1998 · N16729 · Emb EMB120RT · Fuselage Miscellaneous Structure
  > DURING C-CHECK INSPECTION, FOUND THE RIGHT OUTBOARD FLOOR SUPPORT BETWEEN FRAMES 45-46 CORRODED. REMOVED AND REPLACED THE FLOOR SUPPORT. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)
- [SDR C2XA98IA538](https://openairdocs.org/sdr/C2XA98IA538.md): Strap · corroded · Dec 18, 1998 · N16729 · Emb EMB120RT · Fuselage Miscellaneous Structure
  > DURING C-CHECK INSPECTION, FOUND THE RIGHT BUTT STRAP CORRODED BETWEEN FRAMES 38 AND 40. REMOVED AND REPLACED BUTT STRAP. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)
- [SDR C2XA98IA537](https://openairdocs.org/sdr/C2XA98IA537.md): Strap · corroded · Dec 18, 1998 · N16729 · Emb EMB120RT · Fuselage Miscellaneous Structure
  > DURING C-CHECK INSPECTION, FOUND THE RIGHT INBOARD FLOOR FLANGE CORRODED BETWEEN FRAMES 33 AND 35. REMOVED AND REPLACED BUTT STRAPS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)
- [SDR C2XA98IA536](https://openairdocs.org/sdr/C2XA98IA536.md): Exhaust Nozzle · cracked · Dec 18, 1998 · N16729 · Emb EMB120RT · Engine Collector/Tailpipe/Nozzle
  > DURING C-CHECK INSPECTION, FOUND THE RIGHT EXHAUST DUCT CRACKED INBOARD ABOVE ATTACH MOUNT BRACKET. REMOVED AND REPLACED RIGHT EXHAUST PIPE. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)
- [SDR C2XA98IA535](https://openairdocs.org/sdr/C2XA98IA535.md): Tail Pipe · cracked · Dec 18, 1998 · N16729 · Emb EMB120RT · Engine Collector/Tailpipe/Nozzle
  > DURING C-CHECK INSPECTION, FOUND CRACK IN AFT OUTBOARD MOUNT FLANGE ON LEFT TAIL PIPE. REMOVED AND REPLACED LEFT TAIL PIPE. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)
- [SDR C2XA98IA534](https://openairdocs.org/sdr/C2XA98IA534.md): Stiffener · chafed · Dec 18, 1998 · N16729 · Emb EMB120RT · Nacelle/Pylon Structure
  > DURING C-CHECK INSPECTION, FOUND THE RIGHT NACELLE AFT END CENTER FLAP WELL LOWER STRUCTURE CHAFED. REMOVED AND REPLACED STIFFENER. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)
- [SDR C2XA98IA533](https://openairdocs.org/sdr/C2XA98IA533.md): Panel · chafed · Dec 18, 1998 · N16729 · Emb EMB120RT · Nacelle/Pylon, Plate/Skin
  > DURING C-CHECK INSPECTION, FOUND THE NACELLE ACCESS PANEL 432BB HAD SMALL CHAFE MARKS TO INNER SURFACE. LOCATED AND DRILLED NEW PANEL. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)
- [SDR C2XA98IA532](https://openairdocs.org/sdr/C2XA98IA532.md): Panel · broken · Dec 18, 1998 · N16729 · Emb EMB120RT · Nacelle/Pylon, Plate/Skin
  > DURING C-CHECK INSPECTION, FOUND ACCESS PANEL 442BB HAD SEVERAL FASTENER HOLES CRACKED AND BROKEN OUT. LOCATED AND DRILLED PANEL. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)
- [SDR C2XA98IA531](https://openairdocs.org/sdr/C2XA98IA531.md): Hat Section · damaged · Dec 18, 1998 · N16729 · Emb EMB120RT · Nacelle/Pylon Structure
  > DURING C-CHECK INSPECTION, AFTER LEFT WING NACELLE FLAP REMOVAL, FOUND LOWER HAT SECTION DAMAGED (HOLE) IN FLAP WELL. REMOVED AND REPLACED LOWER DAMAGED HAT SECTION. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)
- [SDR C2XA98IA530](https://openairdocs.org/sdr/C2XA98IA530.md): Fitting · cracked · Dec 18, 1998 · N16729 · Emb EMB120RT · Nacelle/Pylon Structure
  > DURING C-CHECK INSPECTION, FOUND THE RIGHT MLG INBOARD DOOR ACTUATOR FORWARD SUPPORT FITTING CRACKED. REMOVED AND REPLACED FITTING. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)
- [SDR C2XA98IA529](https://openairdocs.org/sdr/C2XA98IA529.md): Fitting · cracked · Dec 18, 1998 · N16729 · Emb EMB120RT · Nacelle/Pylon Structure
  > DURING C-CHECK INSPECTION, FOUND THE RIGHT MLG FORWARD OUTBOARD DOOR ACTUATOR FORWARD FITTING CRACKED. REMOVED AND REPLACED FITTING. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)
- [SDR C2XA98IA528](https://openairdocs.org/sdr/C2XA98IA528.md): Skin · cracked · Dec 18, 1998 · N16729 · Emb EMB120RT · Nacelle/Pylon, Plate/Skin
  > DURING C-CHECK INSPECTION, FOUND THE RIGHT MLG AFT INBOARD DOOR FORWARD HINGE ATTACH POINT NACELLE SKIN CRACKED AT RIVET. STOP DRILLED AND FABRICATED DOUBLER REPAIR. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)
- [SDR C2XA98IA527](https://openairdocs.org/sdr/C2XA98IA527.md): Fitting · broken · Dec 18, 1998 · N16729 · Emb EMB120RT · Landing Gear Doors
  > DURING C-CHECK INSPECTION, FOUND THE RIGHT MLG AFT INBOARD DOOR AFT HINGE FITTING BROKEN. REMOVED AND REPLACED HINGE FITTING. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)
- [SDR C2XA98IA526](https://openairdocs.org/sdr/C2XA98IA526.md): Flange · chafed · Dec 18, 1998 · N16729 · Emb EMB120RT · Landing Gear Doors
  > DURING C-CHECK INSPECTION, FOUND THE LEFT OUTBOARD FORWARD LANDING GEAR DOOR NACELLE HINGE ATTACH POINT CHAFED. REMOVED AND REPLACED LEFT OUTBOARD FORWARD LANDING GEAR DOOR NACELLE HINGE ATTACH POINT. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)
- [SDR C2XA97IA165](https://openairdocs.org/sdr/C2XA97IA165.md): Frame · cracked · May 24, 1997 · N16729 · Emb EMB120RT · Nacelle/Pylon, Frame/Spar/Rib
  > IAH - DURING C-CHECK INSPECTION, THE LEFT NACELLE COWLING SUPPORT FRAME WAS FOUND TO BE CRACKED. MAINTENANCE REPAIRED THE FRAME IAW CONTINENTAL EXPRESS EC 5420-01011, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)
- [SDR C2XA97IA145](https://openairdocs.org/sdr/C2XA97IA145.md): Spring · broken · Apr 20, 1997 · N16729 · Emb EMB120RT · Cabin Cooling System
  > IAH - FLT 3959 - THE PILOT REPORTED THAT DURING CLIMB, CABIN FILLED WITH SMOKE AND A SMOKE WARNING INDICATION WAS ILLUMINATED. THE CREW TURNED THE AIR CONDITIONING PACK SWITCHES TO LOW AND THE SMOKE INDICATION LIGHT EXTINGUISHED. THE AIRCRAFT RETURNED TO IAH
- [SDR C2XA97IA134](https://openairdocs.org/sdr/C2XA97IA134.md): Duct Assembly · broken valve · Apr 3, 1997 · N16729 · Emb EMB120RT · Pneumatic Distribution System
  > IAH - FLT 3793 - PILOT REPORTED DURING CLIMB, THERE WAS SMOKE IN CABIN. THE AIRCRAFT RETURNED AND LANDED TO IAH WITHOUT INCIDENT. MAINTENANCE FOUND THE RIGHT RAM AIR VALVE BROKEN AND THE AIRCRAFT WAS DISPATCHED UNDER MEL 21-51-1C. TO CLEAR THE DISCREPANCY,
- [SDR C2XA96CL025](https://openairdocs.org/sdr/C2XA96CL025.md): Switch · out of adjust · Sep 2, 1996 · N16729 · Emb EMB120RT · Landing Gear Steering System
  > CLE - FLT 3070 - CREW REPORTED, THAT THE NOSE WHEEL STEERING DISCONNECTS WHEN MAKING FULL LEFT TURNS USING THE TILLER. MAINTENANCE INSPECTED AIRCRAFT AND ADJUSTED THE NOSE WHEEL STEERING TILLER MICROSWITCH IAW EMB-120 MM 32-50-00. OPS CHECKS WERE GOOD, AIRCRA
- [SDR C2XA96CL024](https://openairdocs.org/sdr/C2XA96CL024.md): Steering Handle · worn · Aug 30, 1996 · N16729 · Emb EMB120RT · Landing Gear Steering System
  > CLE - FLT 3216 - CREW REPORTED, THAT THE NOSE WHEEL STEERING DISCONNECTS WHEN MAKING FULL LEFT TURNS WITH THE TILLER AND RUDDER PEDALS. MAINTENANCE INSPECTED AIRCRAFT AND REMOVED AND REPLACED THE STEERING HANDLE IAW EMB-120 MM 32-50-01, OPERATIONAL CHECKS WER
- [SDR C2XA96IA091](https://openairdocs.org/sdr/C2XA96IA091.md): Wheel · failed · Apr 10, 1996 · N16729 · Emb EMB120RT · Wheel/Ski/Float
  > IAH - FLT 3950 - DURING POST-FLIGHT INSPECTION, PILOT REPORTED THE NR 4 MAIN TIRE WAS BLOWN. MAINTENANCE FOUND THE WHEEL RIM HAD FAILED, REMOVED AND REPLACED THE WHEEL ASSEMBLY, AND APPROVED THE AIRCRAFT FOR RETURN TO SERVICE. AIRCRAFT TOTAL TIME, 13,896.1
- [SDR C2XA95IA435](https://openairdocs.org/sdr/C2XA95IA435.md): Support · cracked · Dec 28, 1995 · N16729 · Emb EMB120RT · Wing Miscellaneous Structure
  > IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB 21, UPPER NR 2 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET, AND THE AIRCAFT WAS APPROVED FOR RETURN TO SERVICE. (M)
- [SDR C2XA95IA434](https://openairdocs.org/sdr/C2XA95IA434.md): Support · cracked · Dec 28, 1995 · N16729 · Emb EMB120RT · Wing Miscellaneous Structure
  > IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB NR 16, UPPER NR 2 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)
- [SDR C2XA95IA433](https://openairdocs.org/sdr/C2XA95IA433.md): Support · cracked · Dec 28, 1995 · N16729 · Emb EMB120RT · Wing Miscellaneous Structure
  > IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB NR 16, UPPER NR 1 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)
- [SDR C2XA95IA432](https://openairdocs.org/sdr/C2XA95IA432.md): Support · cracked · Dec 28, 1995 · N16729 · Emb EMB120RT · Wing Miscellaneous Structure
  > IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB 22, LOWER NR 2 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Next page: https://openairdocs.org/deregistered/N16729-2007-10-25/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 = 'N16729' AND deregistration_id = 'N16729-2007-10-25'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N16729-2007-10-25/reports

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