# Service difficulty reports: N8946A

A list on [N8946A](https://openairdocs.org/aircraft/N8946A.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 REXA2021022200068](https://openairdocs.org/sdr/REXA2021022200068.md): Bulkhead Web · cracked · Feb 10, 2021 · N8946A · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUND FS 559 RT BULKHEAD WEB HAS 2 INDICATIONS NOTED 1) I/B OF RBL18 WL 59.10.500 LONG 70% FSH AND 2) O/B OF RBL 9 WL 54.10.300 LONG 50% FSH BOTH FAILED NDT INSPECTION. COMPLIED WITH 559 BULKHEAD REPAIR IAW EO NR P53025 AND MHIRJ REO 601R-53-41-2858 REV A D
- [SDR REXA2021022200066](https://openairdocs.org/sdr/REXA2021022200066.md): Angle · corroded · Feb 1, 2021 · N8946A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 280.00 FWD J ANGLE HAS MULTIPLE SPOTS OF CORROSION. REMOVED AND REPLACED FS 280 FWD J ANGLE IAW CRJ 200 SRM'S 51-40-11, 51-42-06 AND 51-42-21. "
- [SDR REXA2021022200065](https://openairdocs.org/sdr/REXA2021022200065.md): Angle · corroded · Feb 1, 2021 · N8946A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SERVICE DOOR SILL ANGLE CORRODED IN MULTIPLE SPOTS. REPAIRED CORRODED AREAS OF SERVICE DOOR SILL ANGLE CLIPS IAW CRJ 200 SRM 51-21-06 AND 53-00-00. REMOVED AND REPLACED CORRODED SERVICE DOOR SILL ANGLE IAW CRJ 200 SRM'S 51-40-11, 51-42-06 AND 51-42-21. "
- [SDR REXA2019082951278](https://openairdocs.org/sdr/REXA2019082951278.md): Seat Track · damaged · Aug 25, 2019 · N8946A · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CO PILOTS OB SEAT TRACK WEAR STRIP 4 FROM FRONT RETAINING RIVET SHEARED. COMPLIED WITH REO 601R-53-11-1093.
- [SDR REXA2019082951277](https://openairdocs.org/sdr/REXA2019082951277.md): Seat Track · damaged · Aug 25, 2019 · N8946A · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > PILOTS IB SEAT TRACK WEAR STRIP 1 2 AN 3 FROM FRONT RETAINING RIVETS SHEERED AND FWD SECTION OF WEAR STRIP CAN BE LIFTED UP UNBONDED. COMPLIED WITH REO 601R-53-11-1093.
- [SDR REXA2019082951276](https://openairdocs.org/sdr/REXA2019082951276.md): Seat Track · damaged · Aug 25, 2019 · N8946A · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > PILOTS OTBD SEAT TRACK WEAR STRIP NR 2 AND 4 FROM FRONT RETAINING RIVETS SHEARED. COMPLIED WITH REO 601R-53-11-1093 TEMPORARY DISPOSTITION INITATED PWI WITHIN 6000 FHS SEE N705634
- [SDR REXA2018082410716](https://openairdocs.org/sdr/REXA2018082410716.md): Oxygen Mask · no test · Aug 21, 2018 · N8946A · Cndair CL6002B19 · Crew Oxygen System
  > CAPTAIN`S OXYGEN MASK FAILS TO TEST. PREFORMED AN OPS CHECK IAW AMM 35-11-12. OPS CHK GOOD. NO FURTHER DEFECTS NOTED.
- [SDR REXA2018030900181](https://openairdocs.org/sdr/REXA2018030900181.md): Lamp · inoperative · Mar 9, 2018 · N8946A · Cndair CL6002B19 · Emergency Lighting
  > RIGHT WING AFT EMERGENCY LIGHT OUT. REPLACED THE LAMPS IAW AMM 33-51-21. OPS TESTED GOOD.
- [SDR REXA2018022300169](https://openairdocs.org/sdr/REXA2018022300169.md): Skin · chafed · Feb 23, 2018 · N8946A · Cndair CL6002B19 · Wing, Plate/Skin
  > RIGHT WING LOWER SKIN CHAFED. REPAIRED THE WING SKIN IAW REO 60IR-57-21-2749.
- [SDR REXA2018022300167](https://openairdocs.org/sdr/REXA2018022300167.md): Access Panel · damaged · Feb 23, 2018 · N8946A · Cndair CL6002B19 · Wing, Plate/Skin
  > RIGHT WING INBD FLAP VANE, INBD ACCESS PANEL 684DT HAS ELONGATED SCREW HOLE. LOCATED & DRILLED A NEW ACCESS PANEL IAW SRM 51-40-11.
- [SDR REXA2018022300166](https://openairdocs.org/sdr/REXA2018022300166.md): Support · cracked · Feb 23, 2018 · N8946A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PILOTS SIDE LOWER SIDE POST SUPPORT BELOW PILOT WINDOW IS CRACKED BETWEEN BS 220 AND 235, BELOW WL 110. REMOVED AND REPLACED THE SUPPORT IAW SRM 51-42-06, AND SRM 51-42-21 AAR SM-58
- [SDR REXA2018022200165](https://openairdocs.org/sdr/REXA2018022200165.md): Step · cracked · Feb 22, 2018 · N8946A · Cndair CL6002B19 · Passenger/Crew Doors
  > WHILE REMOVING CORROSION ON PAX DOOR STEP, FOUND A CRACK. LOCATED, AND DRILLED A NEW STEP IAW SRM 51-40-11.
- [SDR REXA2018022100168](https://openairdocs.org/sdr/REXA2018022100168.md): Stiffener · cracked · Feb 21, 2018 · N8946A · Cndair CL6002B19 · Engine Collector/Tailpipe/Nozzle
  > NR 1 ENGINE EXHAUST CONE 436AL HAS CRACKED STIFFENER. REPAIRED THE STIFFENER IAW CMM 78-11-00, PG 6043.
- [SDR REXA2018022100164](https://openairdocs.org/sdr/REXA2018022100164.md): Attach Angle · cracked · Feb 21, 2018 · N8946A · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > RIGHT WINDSHIELD SIDE SUPPORT POST, LOWER OTBD ATTACH ANGLE CRACKED. REMOVED THE ATTACH ANGLE, LOCATED, DRILLED, AND INSTALLED A NEW ATTACH ANGLE IAW SRM 51-52-21.
- [SDR REXA2018021700170](https://openairdocs.org/sdr/REXA2018021700170.md): Post · cracked · Feb 17, 2018 · N8946A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > VERTICAL POST AT LBL 27 ON THE BULKHEAD AT BS 409+128. FOUND TO HAVE A ONE INCH CRACK AT BOTTOM OF INBD CHANNEL. REPAIRED THE POST IAW REO 601R-53-41-056.
- [SDR REXA2018021700163](https://openairdocs.org/sdr/REXA2018021700163.md): Attach Angle · cracked · Feb 17, 2018 · N8946A · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > LEFT WINDSHIELD, SIDE SUPPORT POST LOWER OTBD ATTACH ANGLE CRACKED. REMOVED AND REPLACED THE ATTACH ANGLE IAW SRM 51-42-21.
- [SDR REXA2018021500161](https://openairdocs.org/sdr/REXA2018021500161.md): Attach Angle · cracked · Feb 15, 2018 · N8946A · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > INTERCOSTAL INBD ATTACH ANGLE CRACKED AT LBL 36, BS 484. REPLACED THE ATTACH ANGLE IAW SRM 51-42-21.
- [SDR REXA2018021400162](https://openairdocs.org/sdr/REXA2018021400162.md): Support Angle · cracked · Feb 14, 2018 · N8946A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SUPPORT AT BS 473.15 ON THE RT UNDEFLOOR LONGERON IS CRACKED. REMOVED AND REPLACED THE SUPPORT ANGLE IAW SRM 51-40-06.
- [SDR REXA2018021400160](https://openairdocs.org/sdr/REXA2018021400160.md): Hinge · cracked · Feb 14, 2018 · N8946A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CARGO DOOR THRESHOLD HINGED PROTECTOR PLATE, THREE PIANO HINGE SEGMENTS CRACKED AND/OR WORN AT HINGE PIN LUGS. REPLACED THE PIANO HINGES ON THE CARGO DOOR THRESHOLD PLATE IAW IAW SRM 51-42-06.
- [SDR REXA2018021300159](https://openairdocs.org/sdr/REXA2018021300159.md): Angle · cracked · Feb 13, 2018 · N8946A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INBD ANGLE ON STRINGER 3L IS CRACKED JUST AFT OF FRAME BS 280, IN THE CABIN. REMOVED AND REPLACED THE ANGLE IAW SRM 51-42-06, AND 51-42-21.
- [SDR REXA2018012800052](https://openairdocs.org/sdr/REXA2018012800052.md): Lamp · inoperative · Jan 28, 2018 · N8946A · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHTS SWITCH LIGHT, BULBS INOPERATIVE. REPLACED THE LAMPS IAW ESPM 20-24-00.
- [SDR REXA2018011700024](https://openairdocs.org/sdr/REXA2018011700024.md): Light · inoperative · Jan 17, 2018 · N8946A · Cndair CL6002B19 · Emergency Lighting
  > FWD RT OVERWING EMERGENCY LIGHT INOP. RELAMPED FWD RT OVERWING EMERGENCY LIGHT IAW AMM 33-51-21. OPS GOOD. P/N OFF/ON: 1317
- [SDR REXA2017121301243](https://openairdocs.org/sdr/REXA2017121301243.md): Oxygen Mask · leaking · Dec 13, 2017 · N8946A · Cndair CL6002B19 · Crew Oxygen System
  > CA SIDE O2 MASK LEAKS DURING TEST. R/R'D CPT SIDE O2 MASK IAW AMM 35-11-12. OPC GOOD, OK FOR SVC.
- [SDR REXA2017052200633](https://openairdocs.org/sdr/REXA2017052200633.md): Oxygen Mask · leaking · May 22, 2017 · N8946A · Cndair CL6002B19 · Crew Oxygen System
  > OBSERVER OXYGEN MASK LEAKS. R & R THE OBSERVER`S OXYGEN MASK IAW AMM 35-11-12. PERFORMED OPS CHECK AND FOUND GOOD.
- [SDR REXA2017051100581](https://openairdocs.org/sdr/REXA2017051100581.md): Defibrillator · inoperative · May 11, 2017 · N8946A · Cndair CL6002B19 · Emergency Equipment
  > BOTH DEFIBRILLATOR`S POWER INOPERATIVE NOT GREEN. REMOVED AND REPLACED IAW CRJ 200 AMM 25-60-00.
- [SDR REXA2017041600524](https://openairdocs.org/sdr/REXA2017041600524.md): Bulb · inoperative · Apr 16, 2017 · N8946A · Cndair CL6002B19 · Emergency Lighting
  > LEFT EMERGENCY LIGHT FWD OF EMERGENCY EXIT DOOR IS INOPERATIVE. EXTERIOR EMERGENCY LIGHT 5. REMOVED AND REPLACED THE BULBS IAW AMM 33-51-21, OPS CHECKED GOOD.
- [SDR REXA2017041400505](https://openairdocs.org/sdr/REXA2017041400505.md): Flashlight · inoperative · Apr 14, 2017 · N8946A · Cndair CL6002B19 · Emergency Equipment
  > FA FLASHLIGHT INOPERATIVE. R & R THE FLASHLIGHT IAW AMM 25-61-02. OK FOR SERVICE.
- [SDR REXA2017020600185](https://openairdocs.org/sdr/REXA2017020600185.md): Oxygen Mask · inoperative · Feb 6, 2017 · N8946A · Cndair CL6002B19 · Crew Oxygen System
  > OBSERVER'S OXYGEN MASK FAILED TEST. HARNESS EITHER STAYS INFLATED OR STAYS DEFLATED. BUT IT WON'T BOTH. REMOVED & REPLACED THE OXYGEN MASK IAW AMM 35-11-12. OPS TEST AND LEAK CHECKED GOOD.
- [SDR REXA2017020300167](https://openairdocs.org/sdr/REXA2017020300167.md): Oxygen Mask · inoperative · Feb 3, 2017 · N8946A · Cndair CL6002B19 · Crew Oxygen System
  > FO OXYGEN MASK TEST FAIL. FOUND FO'S O2 MASK INOP. REMOVED FO'S 02 MASK AND SWAPPED WITH OBSERVER'S O2 MASK IAW AMM 35-11-12. PERFORMED OPS CHECK OF FO'S 02 MASK IAW AMM 35-100-00 AND 23-51-00. OPS CHECK GOOD AT THIS TIME. DEFERRED OBS O2 SYS IAW MEL 35-10-01
- [SDR REXA2017010800012](https://openairdocs.org/sdr/REXA2017010800012.md): Defibrillator · inoperative · Jan 8, 2017 · N8946A · Cndair CL6002B19 · Emergency Equipment
  > AED BATTERY IS DEAD. REMOVED AND REPLACED AED IAW AMM 25-60-00. MM02.
- [SDR REXA2016120402344](https://openairdocs.org/sdr/REXA2016120402344.md): Motor · inoperative · Dec 4, 2016 · N8946A · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR DOES NOT CLOSE. REMOVED AND REPLACED PASS DOOR POWER ASSIST MOTOR IAW AMM 52-11-08. OPS CHECK OK. REMOVED AND REPLACED PASS DOOR PRESS VENT-FLAP ICE BREAK CABLE ASSY IAW AMM 52-11-15. OPS CHECK OK.
- [SDR REXA2016101001922](https://openairdocs.org/sdr/REXA2016101001922.md): Bracket · bent · Oct 10, 2016 · N8946A · Cndair CL6002B19 · Landing Gear Position and Warning
  > GEAR DISAGREE ON TAKE OFF. NOSE GEAR REMAINED DOWN. QRH PERFORMED SATISFACTORILY AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED TARGET AND BRACKET FOR NLG CENTERED, EXTENDED PROXIMITY SENSOR IAW CMM 32-20-04 EXTENSION AND RETRACTION OF NLG GOOD IAW AMM 32-
- [SDR REXA2016100801916](https://openairdocs.org/sdr/REXA2016100801916.md): Angle · cracked · Oct 8, 2016 · N8946A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT BS 621 OBLIQUE ANGLE AT STRINGER 14L IS CRACKED. REMOVED & REPLACED THE ANGLE IAW SRM 51-42-06 & 51-42-21. LEAK CHECKED GOOD IAW AMM 52-31-07-720-801.
- [SDR REXA2016100401911](https://openairdocs.org/sdr/REXA2016100401911.md): Attach Angle · cracked · Oct 4, 2016 · N8946A · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > THE ATTACH ANGLE AT AFT SIDE OF BS 621 BULKHEAD IS CRACKED. REMOVED AND REPLACED THE ATTACH ANGLE IAW SRM 51-42-06.
- [SDR REXA2016100401909](https://openairdocs.org/sdr/REXA2016100401909.md): Attach Angle · cracked · Oct 4, 2016 · N8946A · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > ANGLE AT AFT SIDE OF BS 621 BULKHEAD IS CRACKED. REMOVED AND REPLACED THE ANGLE IAW SRM 51-42-06.
- [SDR REXA2016100401908](https://openairdocs.org/sdr/REXA2016100401908.md): Angle · cracked · Oct 4, 2016 · N8946A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > ANGLE AT AFT SIDE OF FS621 BULKHEAD IS CRACKED. REMOVED AND REPLACED IAW SRM 51-42-06.
- [SDR REXA2016100401906](https://openairdocs.org/sdr/REXA2016100401906.md): Attach Angle · cracked · Oct 4, 2016 · N8946A · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > ANGLE AT AFT SIDE OF BS 621 BULKHEAD IS CRACKED. REMOVED & REPLACED THE ANGLE IAW SRM 51-42-06.
- [SDR REXA2016100401900](https://openairdocs.org/sdr/REXA2016100401900.md): Angle · bent · Oct 4, 2016 · N8946A · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR FWD HAND RAIL STOW ANGLE MISSING. ALSO AFT HANDRAIL STOW ANGLE IS BENT. REMOVED AND REPLACED THE ANGLE IAW SRM 51-42-06.
- [SDR REXA2016100301904](https://openairdocs.org/sdr/REXA2016100301904.md): Floor Support · corroded · Oct 3, 2016 · N8946A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > IN AFT CARGO BAY BS 621 - 589 LBL 28 FLOOR SUPPORT CORRODED. REMOVED & REPLACED FLOOR SUPPORT IAW SRM 51-42-21.
- [SDR REXA2016100101910](https://openairdocs.org/sdr/REXA2016100101910.md): Intercostal · cracked · Oct 1, 2016 · N8946A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INTERCOSTAL AT AFT SIDE OF BS 621 BULKHEAD IS CRACKED. REMOVED & REPLACED INTERCOSTAL IAW SRM 51-42-21 & 51-42-22.
- [SDR REXA2016100101907](https://openairdocs.org/sdr/REXA2016100101907.md): Intercostal · cracked · Oct 1, 2016 · N8946A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INTERCOSTAL AT AFT SIDE OF FS621 BULKHEAD IS CRACKED. REMOVED & REPLACED THE INTERCOSTAL IAW SRM 51-42-21 & 51-42-22.
- [SDR REXA2016100101905](https://openairdocs.org/sdr/REXA2016100101905.md): Intercostal · cracked · Oct 1, 2016 · N8946A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INTERCOSTAL AT AFT SIDE OF BS 621 BULKHEAD AND L 13 IS CRACKED. REMOVED & REPLACED INTERCOSTAL IAW SRM 51-42-21 & 51-42-22.
- [SDR REXA2016092901915](https://openairdocs.org/sdr/REXA2016092901915.md): Isolator · cracked · Sep 29, 2016 · N8946A · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > IN AFT CARGO, FWD FACE OF AFT PRESSURE BULKHEAD HAS TWO ISOLATOR MOUNTS THAT ARE BROKEN. REMOVED AND REPLACED THE ISOLATOR IAW SRM 51-42-06.
- [SDR REXA2016092801898](https://openairdocs.org/sdr/REXA2016092801898.md): Seat Track · corroded · Sep 28, 2016 · N8946A · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK FROM BS 409+126 - 559 HAS SEVERAL AREAS OF CORROSION AND GOUGES. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11.
- [SDR REXA2016092701914](https://openairdocs.org/sdr/REXA2016092701914.md): Bulkhead · cracked · Sep 27, 2016 · N8946A · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 621 BULKHEAD CRACKED AROUND LINTEL FITTING. REPAIRED IAW REO 601R-53-61-1230. REV. F.
- [SDR REXA2016092701913](https://openairdocs.org/sdr/REXA2016092701913.md): Floor Support · corroded · Sep 27, 2016 · N8946A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > IN THE AFT CARGO BAY, BS 589 - 621 LBL 26 FLOOR SUPPORT HAS CORROSION. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. REPAIRED IAW EA CRJ253-04790.
- [SDR REXA2016092701912](https://openairdocs.org/sdr/REXA2016092701912.md): Floor Support · corroded · Sep 27, 2016 · N8946A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > IN AFT CARGO BAY BS 589 - 621 LBL 9 FLOOR SUPPORT CORRODED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. REPAIRED THE FLOOR SUPPORT IAW EA CRJ253-04792.
- [SDR REXA2016092401899](https://openairdocs.org/sdr/REXA2016092401899.md): Seat Track · corroded · Sep 24, 2016 · N8946A · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK FROM BS 559 TO 559+80 HAS SEVERAL AREAS OF CORROSION AND GOUGES. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11, REO 601R-53-00-485, AND AMM 53-01-11.
- [SDR REXA2016092401895](https://openairdocs.org/sdr/REXA2016092401895.md): Seat Track · corroded · Sep 24, 2016 · N8946A · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK FROM BS 559 TO 559+80 HAS SEVERAL AREAS OF CORROSION AND GOUGES. REMOVED AND REPLACED THE SEAT TRACK AMM 53-01-11, AND AMM 53-01-11.
- [SDR REXA2016092301903](https://openairdocs.org/sdr/REXA2016092301903.md): Attach Angle · cracked · Sep 23, 2016 · N8946A · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > FLT CONTROL CABLE FAIRLEAD INTERCOSTAL AT BS 484, RBL 27 TO 34 INBD ATTACH ANGLE CRACKED. REMOVED & REPLACED THE ATTACH ANGLE IAW SRM 51-42-06.

Next page: https://openairdocs.org/aircraft/N8946A/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 = 'N8946A' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8946A/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.