# Service difficulty reports: N8790A

A list on [N8790A](https://openairdocs.org/aircraft/N8790A.md).

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

- [SDR REXA2014030800285](https://openairdocs.org/sdr/REXA2014030800285.md): Connector · detached · Mar 8, 2014 · N8790A · Cndair CL6002B19 · Equipment/Furnishings Wiring
  > ON ELT CONNECTOR FOUND PINS 7 & 11 DETACHED FROM WIRES. DEFERRED, MORE INFORMATION TO COME.
- [SDR REXA2013062901320](https://openairdocs.org/sdr/REXA2013062901320.md): Priority Valve · malfunctioned · Jun 29, 2013 · N8790A · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > DURING FUNCTIONAL TEST OF EXTENTION & RETRACTRACTION SYS, GEAR DISAGREE WARNING WITH NLG SLOW TO RETRACT ON SINGLE PUMP OPERATION. R & R NLG PRIORITY VALVE. OPS & LEAK CHECKED GOOD IAW AMM 32-33-15. FUNCTIONAL TEST OF EXTENTION AND RETRACTION SYS FOR ALL GE
- [SDR REXA2013061301182](https://openairdocs.org/sdr/REXA2013061301182.md): Flap System · unknown · Jun 13, 2013 · N8790A · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS HALF SPEED.
- [SDR REXA2013060301056](https://openairdocs.org/sdr/REXA2013060301056.md): Life Vest · unserviceable · Jun 3, 2013 · N8790A · Cndair CL6002B19 · Life Jacket
  > OBS LIFE VEST HAS HOLE IN BAG, R & R OTBD LIFE VEST IAW AMM 25-61-03.
- [SDR REXA2013050900880](https://openairdocs.org/sdr/REXA2013050900880.md): Strap · broken · May 9, 2013 · N8790A · Cndair CL6002B19 · Emergency Equipment
  > PILOT'S EMERGENCY FLASHLIGHT INDICATOR STRAP BROKEN. REPLACED BATTERY IAW CMM 25-60-02 AND REINSTALLED FLASHLIGHT IAW AMM 25-61-02.
- [SDR REXA2013040700729](https://openairdocs.org/sdr/REXA2013040700729.md): Selector Valve · malfunctioned · Apr 7, 2013 · N8790A · Cndair CL6002B19 · Landing Gear Selector
  > ON FLIGHT 3672 (ROC TO DTW) ON APPROACH INTO DTW RECEIVED GEAR DISAGREE ON ARRIVAL NOSE GEAR DOWN AND LOCKED. MAIN GEAR BOTH WHITE INDICATIONS UP. CREW RAN QRH AND PULLED EMERGENCY HANDLE - MANUAL EXTENSION INDICATED 3 GREEN DOWN AND LOCKED. COMPLIED WITH P
- [SDR REXA2013010900058](https://openairdocs.org/sdr/REXA2013010900058.md): Frame · cracked · Jan 7, 2013 · N8790A · Cndair CL6002B19 · Fuselage Main, Frame
  > FOUND THE 280 FRAME CRACKED AT RBL 9 LOWER ANGLE. REPAIRED IAW BOMBARDIER REO 601R-53-11-171.
- [SDR REXA2013010300142](https://openairdocs.org/sdr/REXA2013010300142.md): Drag Angle · cracked · Jan 3, 2013 · N8790A · Cndair CL6002B19 · Passenger/Crew Doors
  > DURING HEAVY CHECK FOUND PASSENGER DOOR AFT DRAG ANGLE CRACKED (AIRCRAFT IN HEAVY CHECK 1/2/2013 - 1/13/2013). REPAIRED PASSENGER DOOR AFT DRAG ANGLE IAW REO 601R-52-11-513.
- [SDR REXA2012102701434](https://openairdocs.org/sdr/REXA2012102701434.md): Hydraulic System · contaminated · Oct 27, 2012 · N8790A · Cndair CL6002B19 · Hydraulic System, Main
  > ON FLIGHT 3771 (DTW - CAK) HAD A GEAR DISAGREE ON APPROACH INTO CAK. BOTH MAIN GEARS DID NOT COME DOWN, CREW RAN QRH AND CYCLED HANDLE GEAR DID NOT FALL THE SECOND TIME. CREW PULLED MANUAL RELEASE HANDLE AND THE GEAR FELL. CREW REPORTED RECEIVING GEAR DISAG
- [SDR REXA2012101401405](https://openairdocs.org/sdr/REXA2012101401405.md): Light · inoperative · Oct 14, 2012 · N8790A · Cndair CL6002B19 · Emergency Lighting
  > LEFT EMERGENCY LIGHT BY EMERGENCY EXIT INOPERABLE. REMOVED AND REPLACED LEFT EMERGENCY LIGHT IAW CRJ 200 AMM 33-51-21. OPS CHECKS GOOD.
- [SDR REXA2012082501293](https://openairdocs.org/sdr/REXA2012082501293.md): Light · inoperative · Aug 25, 2012 · N8790A · Cndair CL6002B19 · Emergency Lighting
  > RIGHT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED LIGHT IAW AMM 33-51-21. OPS CHECKED GOOD.
- [SDR REXA2012081601269](https://openairdocs.org/sdr/REXA2012081601269.md): Container · damaged · Aug 16, 2012 · N8790A · Cndair CL6002B19 · Life Jacket
  > OBSERVER`S AND FLIGHT ATTENDANTS LIFE VEST BAGS DAMAGED. REMOVED AND REPLACED OBSERVER`S AND FLIGHT ATTENDANTS LIFE VEST IAW AMM 25-61-03.
- [SDR REXA2012061801001](https://openairdocs.org/sdr/REXA2012061801001.md): Control Unit · malfunctioned · Jun 18, 2012 · N8790A · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAIL CAUTION MESSAGE. REMOVED AND REPLACED FECU PER AMM 27-51-05. RIG AND OPS CHECKED GOOD. AIRCRAFT OK FOR SERVICE.
- [SDR REXA2012051400728](https://openairdocs.org/sdr/REXA2012051400728.md): Switch · dirty · May 14, 2012 · N8790A · Cndair CL6002B19 · Engine Thrust Reverser
  > LT ENGINE THRUST REVERSER WOULD NOT ENGAGE OR DEPLOY. CLEANED DEPLOY SWITCH, PERFORMED OPS CHECK IAW AMM 78-30-00. OK FOR SERVICE.
- [SDR REXA2012051000718](https://openairdocs.org/sdr/REXA2012051000718.md): Thrust Reverser · malfunctioned · May 10, 2012 · N8790A · Cndair CL6002B19 · Engine Thrust Reverser
  > LEFT THRUST REVERSER WILL NOT DEPLOY. PERFORMED OPERATIONAL CHECK OF LT TRUST REV IAW AMM 71-00-00. ALL CHECKED GOOD. AIRCRAFT OK FOR SERVICE.
- [SDR REXA2012051000717](https://openairdocs.org/sdr/REXA2012051000717.md): Thrust Reverser · malfunctioned · May 10, 2012 · N8790A · Cndair CL6002B19 · Engine Thrust Reverser
  > LEFT THRUST REVERSER WOULD NOT DEPLOY ON LANDING. PERFORMED MUTIPLE OPERATIONAL CHECKS, COULD NOT DUPLICATE. OPS CHECKED GOOD IAW AMM 78-30-00. OK FOR SERVICE.
- [SDR REXA2012050800614](https://openairdocs.org/sdr/REXA2012050800614.md): Unknown · malfunctioned · May 8, 2012 · N8790A · Cndair CL6002B19 · Engine Thrust Reverser
  > LEFT THRUST REVERSER WOULD NOT DEPLOY AFTER LANDING. T/S PER FIM 78-30-00. PERFORMED OPS CHECK OF LEFT THRUST REVERSER IAW GROUND RUN MANUAL 71-00-00. OPS CHECK GOOD.
- [SDR REXA2012042700584](https://openairdocs.org/sdr/REXA2012042700584.md): Connector · damaged · Apr 27, 2012 · N8790A · Cndair CL6002B19 · Engine Exhaust System Wiring
  > LEFT THRUST REVERSER WILL NOT STOW. FOUND PIN DAMAGED IN CONNECTOR, REPAIRED IAW 20-00-00. NO DEFECTS NOTED. OPS CHECKED GOOD IAW AMM 78-30-00 NO DEFECTS NOTED. OK FOR SERVICE
- [SDR REXA2012021800199](https://openairdocs.org/sdr/REXA2012021800199.md): Skin · punctured · Feb 17, 2012 · N8790A · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN JUST AFT OF BS 319 AND BETWEEN S23-24L TO BE PUNCTURED. THE DAMAGE WAS CUT OUT LEAVING A 1.75 INCH DIAMETER HOLE. REPAIRED IAW EA CRJ253-00378 AND CORRESPONDING 8110-3.
- [SDR REXA201100865](https://openairdocs.org/sdr/REXA201100865.md): Inverter · inoperative · Nov 23, 2011 · N8790A · Cndair CL6002B19 · Emergency Lighting
  > BACK FOUR EMERGENCY ROW STRIPS OUT. REMOVED AND REPLACED NR 4 INVERTER IAW 33-51-07. OPS CHECK GOOD. VERFIED PART EFFECITIVTY.
- [SDR REXA201100831](https://openairdocs.org/sdr/REXA201100831.md): Light · inoperative · Nov 9, 2011 · N8790A · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY FLOOR LIGHT NOT WORKING AFT OF EXIT ROW. PERFORMED OPS CHECK OF EMERGENCY LIGHTS IAW AMM 33-51-00. CHECKS GOOD, NO DEFECTS NOTED.
- [SDR REXA201100692](https://openairdocs.org/sdr/REXA201100692.md): Coalescer Bag · dirty · Oct 8, 2011 · N8790A · Cndair CL6002B19 · Humidity Control System
  > STRONG ODOR OF RAW JET FUEL ON FLT DECK WHEN OPEN MAIN CABIN DOOR AND FROM APU SHUT DOWN. REMOVED AND REPLACED LT AND RT COALESCER BAGS IAW AMM 21-51-13. VERIFIED PARTS EFFECTIVITY.
- [SDR REXA201100637](https://openairdocs.org/sdr/REXA201100637.md): Connector · defective · Sep 30, 2011 · N8790A · Cndair CL6002B19 · Light System Wiring
  > CABIN EMERGENCY LIGHT ROW 8-12 INOP. REMOVED AND REPLACED EMERGENCY LIGHTS FLOOR TRACK AFT ELECTRICAL CONNECTOR IAW AMM 33-51-01. VERIFIED PART EFFECTIVITY. OPC GOOD, A/C OK FOR SVC.
- [SDR REXA201100597](https://openairdocs.org/sdr/REXA201100597.md): Strut · low pressure · Sep 25, 2011 · N8790A · Cndair CL6002B19 · Nose/Tail Landing Gear Strut/Axle
  > GEAR DISAGREE UPON GEAR RETRACTION. MSG CLEAR AFTER FLAPS RETRACTED. SVCD NOSE STRUT IAW AMM 12-12-32 COMPLIED WITH PA05-018B GEAR DISAGREE EVENT PROCEDURE AND AMM 32-30-00. NO DEFECTS NOTED OK FOR SVC.
- [SDR REXA201100665](https://openairdocs.org/sdr/REXA201100665.md): Angle · damaged · Sep 21, 2011 · N8790A · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 559 BULKHEAD CAP ANGLE HAS INDICATION NOTED AT LBL 18 APPROX 0.2" IN LENGTH 50 PERCENT FSH AND RT WEB AT WL59.10 APPROX 0.3" IN LENGTH 80 PERCENT FSH. REPAIRED IAW BOMBARDIER REOS REO 601R-53-41-260 REV E, REO 601R-53-41-609, AND REO 601R-53-41-1480 REV A.
- [SDR REXA201100550](https://openairdocs.org/sdr/REXA201100550.md): Bulkhead · cracked · Sep 12, 2011 · N8790A · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 559 SEMI-PRESSURE BULKHEAD FOUND CRACKED. REPAIR IAW BOMBARDIER REO 601R-53-41-260 REV E AND 601R-53-41-609 REV B.
- [SDR REXA201100445](https://openairdocs.org/sdr/REXA201100445.md): Strut · low · Jul 12, 2011 · N8790A · Cndair CL6002B19 · Nose/Tail Landing Gear Strut/Axle
  > NLG DISAGREE SERVICED NOSE IAW AMM 12-12-32 STRUT AND C/W PA 05-018B AND GEAR SWING CHECKS GOOD IAW AMM 32-30-00, OK FOR SERVICE.
- [SDR REXA201100289A](https://openairdocs.org/sdr/REXA201100289A.md): Warning Light · illuminated · May 12, 2011 · N8790A · Cndair CL6002B19 · Landing Gear Position and Warning
  > ON APPROACH INTO DTW CREW GOT GEAR DISAGREE. RAN QRH, LANDED WITHOUT INCIDENT. DID NOT DECLARE EMERGENCY.
- [SDR REXA201100288A](https://openairdocs.org/sdr/REXA201100288A.md): Warning System · activated · May 11, 2011 · N8790A · Cndair CL6002B19 · Landing Gear Position and Warning
  > GEAR DISAGREE ON APPROACH INTO JFK DEFERRED PER MEL 32-30-01.
- [SDR REXA201100285](https://openairdocs.org/sdr/REXA201100285.md): Warning System · activated · May 11, 2011 · N8790A · Cndair CL6002B19 · Landing Gear Position and Warning
  > GEAR DISAGREE ON APPROACH INTO JFK DEFERRED PER MEL 32-30-01.
- [SDR REXA201000217](https://openairdocs.org/sdr/REXA201000217.md): Idg · low · Oct 17, 2010 · N8790A · Cndair CL6002B19 · AC Generator-Alternator
  > GEN 2 OFF CAUTION EMP 53228 FLT 4299. SERVICED NR 2 IDG IAW AMM 12-13-24. RECONNECTED NR 2 IDG OPC NR 2 IDG IAW AMM 24-11-01. OPC GOOD. THIS CLEARS DM NR 30785. PLACARD REMOVED.
- [SDR REXA200600075](https://openairdocs.org/sdr/REXA200600075.md): Flap System · malfunctioned · Jul 19, 2006 · N8790A · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAP FAIL ON TAXI. RESET SYSTEM AND PLACED ON 72 HOUR WATCH PER AD 98-20-01.
- [SDR REXA200500138](https://openairdocs.org/sdr/REXA200500138.md): Flap System · malfunctioned · Nov 15, 2005 · N8790A · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAIL AT ZERO WHEN SELECTED TO TWENTY. QRH FOLLOWED, ZERO FLAP LANDING PERFORMED. SYSTEM REST AND PLACED ON 72 HOUR WATCH PER AD98-20-01.
- [SDR REXA04008](https://openairdocs.org/sdr/REXA04008.md): G Switch · failed · Apr 7, 2004 · N8790A · Cndair CL6002B19 · Emergency Locator Beacon
  > ELT FAILS G-SWITCH TEST DURING 12 MONTH ELT INSPECTION. REMOVED ELT FOR MAINTENANCE IAW FAR 91.207. THIS FAILURE IS THE 9TH OCCURRENCE OF THIS MODEL ELT FAILING THE G-SWITCH ON ITS FIRST 12 MONTH INSPECTION. PINNACLE AIRLINES REACHED THE 12 MONTH INVERVAL O

## 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 = 'N8790A' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8790A/reports

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