# Service difficulty reports: N47722, cancelled Mar 7, 2012

A list on [N47722, cancelled Mar 7, 2012](https://openairdocs.org/deregistered/N47722-2012-03-07.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 · 54 reports

- [SDR C2XA01IA063](https://openairdocs.org/sdr/C2XA01IA063.md): Proximity Switch · inoperative · Feb 5, 2001 · N47722 · Emb EMB120ER · Landing Gear Position and Warning
  > IAH - FLIGHT 3580, THE CREW REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT MAIN LANDING GEAR WEIGHT ON WHEELS PROXIMITY SWITCH, AND THE AIRCRAFT WAS
- [SDR C2XA00IA476](https://openairdocs.org/sdr/C2XA00IA476.md): Connector · bent · Dec 22, 2000 · N47722 · Emb EMB120RT · Landing Gear Position and Warning
  > TYR - FLT 4379 - THE CREW REPORTED THAT ON TAKEOFF ROLL RECEIVED ELECTRIC AND DOOR WARNINGS AND LOST NOSE WHEEL STEERING. THE CREW ABORTED TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. THE AIRCRAFT WAS RELEASED FOR FERRY FLIGHT TO IAH. MAINTENANCE FOUN
- [SDR C2XAOOIA396](https://openairdocs.org/sdr/C2XAOOIA396.md): Heater · damaged · Oct 30, 2000 · N47722 · Emb EMB120RT · Fuel Heater
  > DURING TAKE-OFF ROLL CREW REPORTED A FUEL LOW PRESSURE LIGHT ON #2 ENGINE. TAKE-OFF WAS ABORTED WITHOUT INCIDENT, AND THE CREW NOTICED FUEL LEAKING OUT OF #2 NACELLE. #2 ENGINE WAS SHUT DOWN, MX INSPECTED A/C AND FOUND TWO STUDS PULLED OUT OF THE FUEL HEATER B
- [SDR C2XA00IA268](https://openairdocs.org/sdr/C2XA00IA268.md): Bulb · inoperative · Sep 6, 2000 · N47722 · Emb EMB120RT · Emergency Lighting
  > IAH - DURING A CHECK INSPECTION, TWO AISLE PATH EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT BULBS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)
- [SDR C2XA00IA192](https://openairdocs.org/sdr/C2XA00IA192.md): Door · disconnected · Jul 4, 2000 · N47722 · Emb EMB120RT · Landing Gear Doors
  > IAH - FLT 3581 - THE CREW REPORTED THAT THE LEFT FORWARD NOSE GEAR DOOR WOULD NOT CLOSE AND A LOUD NOISE COMING FROM THE NOSE LANDING GEAR COMPARTMENT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE RECONNECTED THE LEFT FORWARD NLG DOOR AND OPERATI
- [SDR C2XA00IA131](https://openairdocs.org/sdr/C2XA00IA131.md): Wire · broken · May 19, 2000 · N47722 · Emb EMB120RT · Light System Wiring
  > EFD - DURING MAINTENANCE INSPECTION, SEVERAL AISLE PATH EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE ON THE LIGHT TRACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)
- [SDR C2XA00IA124](https://openairdocs.org/sdr/C2XA00IA124.md): Battery Pack · discharged · May 13, 2000 · N47722 · Emb EMB120RT · Emergency Lighting
  > IAH - DURING 1A INSPECTION, THE RIGHT UPPER OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BATTERY PACK IAW EMB120MM 33-50-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)
- [SDR C2XA00IA114](https://openairdocs.org/sdr/C2XA00IA114.md): Battery Pack · discharged · May 5, 2000 · N47722 · Emb EMB120RT · Emergency Lighting
  > IAH - DURING SERVICE CHECK INSPECTION, THE AFT EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY PACK IAW EMB120 MM 33-50-02, AND THE AICRAFT WAS APPROVED FOR RETURN TO SERVICE. (X)
- [SDR C2XA00IA048](https://openairdocs.org/sdr/C2XA00IA048.md): Proximity Switch · misaligned · Mar 2, 2000 · N47722 · Emb EMB120RT · Landing Gear Position and Warning
  > IAH - FLIGHT 3664 - THE CREW REPORTED THAT THE RIGHT MAIN LANDING GEAR POSITION A LIGHT ILLUMINATED INFLIGHT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE ADJUSTED THE AFFECTED UPLOCK PROXIMITY SWITCH, AND THE AIRCRAFT WAS APPRO
- [SDR C2XAOOIA045](https://openairdocs.org/sdr/C2XAOOIA045.md): Frame · cracked · Feb 20, 2000 · N47722 · Emb EMB120RT · Nacelle/Pylon, Frame/Spar/Rib
  > DURING CONTINENTAL EXPRESS AIRLINES C-CHECK, FOUND LT NACELLE NR 1 FRAME CRACKED. REMOVED AND REPLACED NR 1 FRAME IAW EC5410-01034. AIRCRAFT APPROVED FOR RETURN TO SERVICE (M)
- [SDR C2XA99IA589](https://openairdocs.org/sdr/C2XA99IA589.md): Relay Box · inoperative · Nov 3, 1999 · N47722 · Emb EMB120RT · Landing Gear Retraction/Extension System
  > IAH - FLT 3455, THE CREW REPORTED THAT THE LANDING GEAZR WOULD NOT RETRACT. THE AIRCRAFT CONTINUED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR RELAY BOX IAW EMB120 MM 32-31-02, AND THE AIRCRAFT WAS APPROVED FOR
- [SDR C2XA99IA384](https://openairdocs.org/sdr/C2XA99IA384.md): Battery Pack · discharged · Jul 23, 1999 · N47722 · Emb EMB120RT · Emergency Lighting
  > IAH - A-CHECK INSPECTION, THE AFT FOUR EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY PACK IAW EMB120 MM 33-50-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X)
- [SDR C2XA99IA181](https://openairdocs.org/sdr/C2XA99IA181.md): Lens · broken · Mar 4, 1999 · N47722 · Emb EMB120RT · Emergency Lighting
  > IAH - DURING POST-FLT INSPECTION, A RED EMERGENCY AISLE PATH EMERGENCY LIGHT WAS FOUND TO BE BROKEN. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LENS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)
- [SDR C2XA99IA179](https://openairdocs.org/sdr/C2XA99IA179.md): Wire · broken · Mar 4, 1999 · N47722 · Emb EMB120RT · Light System Wiring
  > IAH - DURING PREFLIGHT INSPECTION, THE CREW REPORTED SEVERAL EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)
- [SDR C2XA98CL072](https://openairdocs.org/sdr/C2XA98CL072.md): Fuse · failed · Nov 6, 1998 · N47722 · Emb EMB120RT · Emergency Lighting
  > CLE - FLT 3351 - CREW REPORTED THE EMERGENCY ESCAPE FLOOR LIGHTS DO NOT WORK FROM ROW 9 TO ROW 11. MAINTENANCE INSPECTED THE EMERGENCY LIGHTING SYSTEM THEN REMOVED AND REPLACED A FUSE AND ALSO REPAIRED A WIRE FOR PRECAUTIONARY REASON. THE EMERGENCY LIGHTING
- [SDR C2XA98IA211](https://openairdocs.org/sdr/C2XA98IA211.md): Battery Pack · discharged · Jun 17, 1998 · N47722 · Emb EMB120RT · Emergency Lighting
  > IAH - DURING C-CHECK INSPECTION, THE FORWARD FLOOR EMERGENCY LIGHTS FAILED TO ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK FOR THE AFFECTED LIGHTS IAW EMB120 MM CH 33-50-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA98IA210](https://openairdocs.org/sdr/C2XA98IA210.md): Crease Beam · corroded · Jun 17, 1998 · N47722 · Emb EMB120RT · Fuselage Miscellaneous Structure
  > IAH - DURING C-CHECK INSPECTION, THE RIGHT CREASE BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 39 AND 44. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF BUTTSTRAP IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)
- [SDR C2XA98IA209](https://openairdocs.org/sdr/C2XA98IA209.md): Buttstrap · corroded · Jun 17, 1998 · N47722 · Emb EMB120RT · Fuselage Miscellaneous Structure
  > IAH - DURING C-CHECK INSPECTION, THE RIGHT CENTER BUTTSTRAP WAS FOUND TO BE CORRODED BETWEEN FRAMES 38-44. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF BUTTSTRAP IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)
- [SDR C2XA98IA208](https://openairdocs.org/sdr/C2XA98IA208.md): Buttstrap · corroded · Jun 17, 1998 · N47722 · Emb EMB120RT · Fuselage Miscellaneous Structure
  > IAH - DURING C-CHECK INSPECTION, THE RIGHT CENTER BUTTSTRAP BETWEEN FRAMES 34 AND 38 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE EFFECTED SECTION OF BUTTSTRAP IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M
- [SDR C2XA98IA207](https://openairdocs.org/sdr/C2XA98IA207.md): T-Profile · corroded · Jun 17, 1998 · N47722 · Emb EMB120RT · Fuselage Miscellaneous Structure
  > IAH - DURING C-CHECK INSPECTION, THE T-PROFILE AT FRAME 40 RIGHT WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE EFFECTED T-PROFILE IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)
- [SDR C2XA98IA206](https://openairdocs.org/sdr/C2XA98IA206.md): Tee · corroded · Jun 17, 1998 · N47722 · Emb EMB120RT · Fuselage Miscellaneous Structure
  > IAH - DURING C-CHECK INSPECTION, THE T-PROFILE AT FRAME 38 RIGHT WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE EFFECTED T-PROFILE IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)
- [SDR C2XA98IA205](https://openairdocs.org/sdr/C2XA98IA205.md): Seat Track · corroded · Jun 17, 1998 · N47722 · Emb EMB120RT · Fuselage, Seat/Cargo Attach Fittings
  > IAH - DURING C-CHECK INSPECTION, THE RIGHT AFT FLOOR SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMVOED AND REPLACED THE EFFECTED SEAT TRACK IAW EMBL-120 SRM 51-21-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)
- [SDR C2XA98IA204](https://openairdocs.org/sdr/C2XA98IA204.md): Support · cracked · Jun 17, 1998 · N47722 · Emb EMB120RT · Wing Miscellaneous Structure
  > IAH - DURING C-CHECK INSPECTION, THE RIGHT WING NUMBER TWO UPPER SKIN SUPPORT AT RIB 21 WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE EFFECTED SKIN SUPPORT IAW EMB-120 SRM 51-40-02 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)
- [SDR C2XA98IA200](https://openairdocs.org/sdr/C2XA98IA200.md): Angle · cracked · Jun 17, 1998 · N47722 · Emb EMB120RT · Vertical Stabilizer
  > IAH - DURING C-CHECK INSPECTION, THE LEFT DRAG ANGLE ON THE VERTICLE STABILIZER WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED THE DAMAGED SECTION OF THE DRAG ANGLE AND INSTALLED A REPAIR SPLICE IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATIO
- [SDR C2XA98IA199](https://openairdocs.org/sdr/C2XA98IA199.md): Support · cracked · Jun 17, 1998 · N47722 · Emb EMB120RT · Fuselage Miscellaneous Structure
  > IAH - DURING C-CHECK INSPECTION, THE RIGHT VERTICLE SUPPORT AT FRAME 13 WAS FOUND TO BE CRACKED. MAINTENANCE STOP DRILLED THE CRACK AND INSTALLED A DOUBLER REPAIR IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)
- [SDR C2XA98IA198](https://openairdocs.org/sdr/C2XA98IA198.md): Support · cracked · Jun 17, 1998 · N47722 · Emb EMB120RT · Fuselage Miscellaneous Structure
  > IAH - DURING C-CHECK INSPECTION, THE LEFT VERTICLE SUPPORT AT FRAME 13 WAS FOUND TO BE CRACKED. MAINTENANCE STOP DRILLED THE CRACK AND INSTALLED A DOUBLER IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)
- [SDR C2XA97CL048](https://openairdocs.org/sdr/C2XA97CL048.md): Engine · failure · Apr 30, 1997 · N47722 · Emb EMB120RT · Engine (Turbine/Turboprop)
  > CLE - FLT 3184 - CREW REPORTED WHILE CLIMBING THROUGH 6,000 FEET, RIGHT HAND ENGINE NP INCREASED AND THE OIL PRESSURE DROPPED TO ZERO. CREW ATTEMPTED A SHUTDOWN, BUT THE PROPELLER WOULD NOT FEATHER. THE ENGINE CONTINUED TO OPERATE WHILE THE ITT WENT TO APPRO
- [SDR C2XA97CL021](https://openairdocs.org/sdr/C2XA97CL021.md): Actuator · failed · Mar 10, 1997 · N47722 · Emb EMB120RT · Trailing Edge Flap Actuator
  > PIT - FLT 3610 - CREW REPORTED, RECEIVED A FLAP CONTROL FAULT IN FLIGHT WHICH WOULD NOT RESET. AIRCRAFT LANDED IN PIT WITHOUT INCIDENT. THE AIRCRAFT WAS MAINTENANCE FERRIED TO CLE, WHERE MAINTENANCE REMOVED AND REPLACED THE RIGHT INBOARD FLAP ACTUATOR IAW EM
- [SDR C2XA96IA292](https://openairdocs.org/sdr/C2XA96IA292.md): Stringer · cracked · Dec 2, 1996 · N47722 · Emb EMB120RT · Wing, Longeron/Stringer
  > IAH - DURING C-CHECK INSPECTION, THE RIGHT WING STRINGER NR 10 WAS FOUND TO BE CRACKED. MAINTENANCE REPAIRED THE AFFECTED PORTION OF STRINGER AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE STRINGER REPAIR WAS ACCOMPLISHED IAW CONTINENTAL EXPRESS EN
- [SDR C2XA96CL009](https://openairdocs.org/sdr/C2XA96CL009.md): Actuator · sticking · Jan 31, 1996 · N47722 · Emb EMB120RT · Trailing Edge Flap Control System
  > CLT - FLT NR 3340 - CREW REPORTED, THAT AFTER TAKEOFF AND FLAP RETRACTION, THE LEFT AND RIGHT OUTBOARD FLAPS STAYED AT 15 DEGREES WITHOUT RECEIVING A DISAGREEMENT INDICATION. MAINTENANCE INSPECTED AIRCRAFT AND REMOVED AND REPLACED THE RIGHT OUTBOARD FLAP ACTU
- [SDR C2XA96CL008](https://openairdocs.org/sdr/C2XA96CL008.md): Control Unit · failed · Jan 30, 1996 · N47722 · Emb EMB120RT · Trailing Edge Flap Control System
  > CLE - FLIGHT NR 3286 - CREW REPORTED THAT ON APPROACH WHEN THE FLAPS WERE SELECTED TO 25 DEGREES FROM 15 DEGREES, THE LEFT AND RIGHT OUTBOARD FLAPS STAYED AT 15 DEGREES AND THE NACELLE AND INBOARD FLAPS WENT TO 25 DEGREES WITHOUT A WARNING INDICATION ON THE MA
- [SDR C2XA96CL007](https://openairdocs.org/sdr/C2XA96CL007.md): Actuator · linkage binding · Jan 30, 1996 · N47722 · Emb EMB120RT · Trailing Edge Flap Actuator
  > ROC - FLIGHT NR 3113 - CREW REPORTED THAT ON APPROACH WITH FLAPS SELECTED TO 15 DEGREES, A FLAP ASYMMETRY OCCURRED THEN CHANGED TO A FLAP DISAGREEMENT. THE CREW ALSO REPORTED THAT THEY DID NOT RECEIVE A FLAP LIGHT ON THE MAP OR A DISAGREEMENT LIGHT ON THE FLA
- [SDR C2XA96CL006](https://openairdocs.org/sdr/C2XA96CL006.md): Control Unit · failed · Jan 28, 1996 · N47722 · Emb EMB120RT · Trailing Edge Flap Control System
  > CLT - FLT NR 3372 - CREW REPORTED, THAT DURING APPROACH THEY RECEIVED A FLAP CONTROL FAULT, THE CREW RESET THE SYSTEM BUT RECEIVED ANOTHER FLAP CONTROL FAULTY WHEN FLAPS WERE EXTENDED TO 25 DEGREES. MAINTENANCE INSPECTED AIRCRAFT AND REMOVED AND REPLACED THE
- [SDR C2XA96CL005](https://openairdocs.org/sdr/C2XA96CL005.md): Control Unit · failed · Jan 25, 1996 · N47722 · Emb EMB120RT · Trailing Edge Flap Control System
  > ROC - FLT NR 3113 - CREW REPORTED THAT DURING LANDING WHEN THE FLAPS WERE SELECTED TO 15 DEGREES, THE RIGHT OUTBOARD EXTENDED TO 10 DEGREES AND THE LEFT OUTBOARD EXTENDED TO 45 DEGREES CAUSING A FLAP ASYMMETRY. MAINTENANCE INSPECTED AIRCRAFT AND REMOVED AND R
- [SDR C2XA95CL116](https://openairdocs.org/sdr/C2XA95CL116.md): Engine · failed · Sep 23, 1995 · N47722 · Emb EMB120RT · Engine (Turbine/Turboprop)
  > FLT NR 3230 - DAY - CLE - RIGHT POWER LEVER HAD VERY NOTICEABLE VIBRATION WITH PROPELLER IN FEATHER AND MINIMUM RPM. MAINTENANCE REMOVED AND REPLACED RIGHT ENGINE IAW MAINTENANCE DIRECTIVE NR 7 AND NR 8. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR C2XA95IA180](https://openairdocs.org/sdr/C2XA95IA180.md): T-Cap · corroded · Aug 8, 1995 · N47722 · Emb EMB120RT · Fuselage Miscellaneous Structure
  > IAH - DURING C-CHECK INSPECTION, FOUND THE T-CAP AT FRAME 40 TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED T-CAP, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)
- [SDR C2XA95IA179](https://openairdocs.org/sdr/C2XA95IA179.md): Cross Beam · corroded · Aug 8, 1995 · N47722 · Emb EMB120RT · Fuselage Miscellaneous Structure
  > IAH - DURING C-CHECK INSPECTION, FOUND THE CROSS BEAM BETWEEN FRAMES 35 TO 38, TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PORTION OF CROSSBEAM, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)
- [SDR C2XA95IA178](https://openairdocs.org/sdr/C2XA95IA178.md): Crossbeam · corroded · Aug 8, 1995 · N47722 · Emb EMB120RT · Fuselage Miscellaneous Structure
  > IAH - DURING C-CHECK INSPECTION, FOUND CROSSBEAM AT FRAME 16 TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF CROSSBEAM, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)
- [SDR C2XA95IA177](https://openairdocs.org/sdr/C2XA95IA177.md): Skin Support · cracked · Aug 8, 1995 · N47722 · Emb EMB120RT · Wing Miscellaneous Structure
  > IAH - DURING C-CHECK INSPECTION, FOUND LEFT WING LOWER NR 4 SKIN SUPPORT CRACKED AT RIB NR 16. MAINTENANCE REMOVED AND REPLACED THE SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M)
- [SDR C2XA95IA175](https://openairdocs.org/sdr/C2XA95IA175.md): Skin Support · cracked · Aug 8, 1995 · N47722 · Emb EMB120RT · Wing Miscellaneous Structure
  > IAH - DURING C-CHECK INSPECTION, FOUND LEFT WING LOWER NR 2 SKIN SUPPORT CRACKED AT RIB NR 16. MAINTENANCE REMOVED AND REPLACED THE SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M)
- [SDR C2XA95IA174](https://openairdocs.org/sdr/C2XA95IA174.md): Skin Support · cracked · Aug 8, 1995 · N47722 · Emb EMB120RT · Wing Miscellaneous Structure
  > IAH - DURING C-CHECK INSPECTION, FOUND LEFT WING UPPER NR 3 SKIN SUPPORT CRACKED AT RIB NR 16. MAINTENANCE REMOVED AND REPLACED THE SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M)
- [SDR C2XA95IA173](https://openairdocs.org/sdr/C2XA95IA173.md): Skin Support · cracked · Aug 8, 1995 · N47722 · Emb EMB120RT · Wing Miscellaneous Structure
  > IAH - DURING C-CHECK INSPECTION, FOUND LEFT WING LOWER NR 5 SKIN SUPPORT CRACKED AT RIB NR 15. MAINTENANCE REMOVED AND REPLACED THE SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M)
- [SDR C2XA95IA172](https://openairdocs.org/sdr/C2XA95IA172.md): Skin Support · cracked · Aug 8, 1995 · N47722 · Emb EMB120RT · Wing Miscellaneous Structure
  > IAH - DURING C-CHECK INSPECTION, FOUND LEFT WING LOWER NR 3 SKIN SUPPORT CRACKED AT RIB NR 15. MAINTENANCE REMOVED AND REPLACED THE SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M)
- [SDR C2XA95IA171](https://openairdocs.org/sdr/C2XA95IA171.md): Skin Support · cracked · Aug 8, 1995 · N47722 · Emb EMB120RT · Wing Miscellaneous Structure
  > IAH - DURING C-CHECK INSPECTION, FOUND LEFT WING LOWER NR 2, AND NR 4 SKIN SUPPORTS CRACKED AT RIB NR 15. MAINTENANCE REMOVED AND REPLACED THE SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M)
- [SDR C2XA95IA170](https://openairdocs.org/sdr/C2XA95IA170.md): Skin Support · cracked · Aug 8, 1995 · N47722 · Emb EMB120RT · Wing Miscellaneous Structure
  > IAH - DURING C-CHECK INSPECTION, FOUND RT WING NR 1 UPPER SKIN SUPPORT CRACKED AT RIB NR 21. MAINTENANCE REMOVED AND REPLACED THE SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M)
- [SDR C2XA95IA169](https://openairdocs.org/sdr/C2XA95IA169.md): Skin Support · cracked · Aug 8, 1995 · N47722 · Emb EMB120RT · Wing Miscellaneous Structure
  > IAH - DURING C-CHECK INSPECTION, FOUND RT WING LOWER NR 2 SKIN SUPPORT CRACKED AT RIB NR 16. MAINTENANCE REMOVED AND REPLACED THE SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M)
- [SDR C2XA95IA168](https://openairdocs.org/sdr/C2XA95IA168.md): Skin Support · cracked · Aug 8, 1995 · N47722 · Emb EMB120RT · Wing Miscellaneous Structure
  > IAH - DURING C-CHECK INSPECTION, FOUND RT WING NR 4 LOWER SKIN SUPPORT CRACKED AT RIB NR 15. MAINTENANCE REMOVED AND REPLACED THE SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M)
- [SDR C2XA95IA167](https://openairdocs.org/sdr/C2XA95IA167.md): Skin Support · cracked · Aug 8, 1995 · N47722 · Emb EMB120RT · Wing Miscellaneous Structure
  > IAH - DURING C-CHECK INSPECTION, FOUND RT WING NR 3 LOWER SKIN SUPPORT CRACKED AT RIB NR 15. MAINTENANCE REMOVED AND REPLACED THE SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M)
- [SDR C2XA95IA166](https://openairdocs.org/sdr/C2XA95IA166.md): Skin Support · cracked · Aug 8, 1995 · N47722 · Emb EMB120RT · Wing Miscellaneous Structure
  > IAH - DURING C-CHECK INSPECTION, FOUND RT WING LOWER SKIN SUPPORT NR 2 CRACKED AT RIB NR 15. MAINTENANCE REMOVED AND REPLACED THE SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M)
- [SDR C2XA5IA176](https://openairdocs.org/sdr/C2XA5IA176.md): Skin Support · cracked · Aug 8, 1995 · N47722 · Emb EMB120RT · Wing Miscellaneous Structure
  > IAH - DURING C-CHECK INSPECTION, FOUND LEFT WING LOWER NR 3 SKIN SUPPORT CRACKED AT RIB NR 16. MAINTENANCE REMOVED AND REPLACED THE SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M)

Next page: https://openairdocs.org/deregistered/N47722-2012-03-07/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 = 'N47722' AND deregistration_id = 'N47722-2012-03-07'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N47722-2012-03-07/reports

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