# Service difficulty reports: N8828D

A list on [N8828D](https://openairdocs.org/aircraft/N8828D.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 · 62 reports

- [SDR SWIA2018100545121](https://openairdocs.org/sdr/SWIA2018100545121.md): Fitting · cracked · Sep 15, 2018 · N8828D · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CRACKS ON LOWER FITTING OF WINDSHIELD CENTER POST. (C-CHECK) RO: 10/04/2018 DRILLED AND INSTALLED 2EA NEW WINDSHIELD CENTER POST LOWER FITTINGS P/N: 601R33237-1S AND 601R33237-2S IAW SRM.
- [SDR SWIA2018100545127](https://openairdocs.org/sdr/SWIA2018100545127.md): Floor Panel · corroded · Sep 13, 2018 · N8828D · Cndair CL6002B19 · Fuselage Floor Panel
  > LT PRESSURE FLOOR PANEL HAS CORROSION FROM FS409+128 TO FS559.00. (C-CHECK) RO: 10/04/2018 REMOVED CORROSION AND REPAIRED 17EA SPOTS ON LT FLOOR SILL PANEL FROM FS409+128 TO FS559.00 IAW REO. PERFORMED A PRESSURE CHECK OF REWORKED AREA IAW AMM. (PRESSURE CHEC
- [SDR SWIA2018100545126](https://openairdocs.org/sdr/SWIA2018100545126.md): Skin · corroded · Sep 13, 2018 · N8828D · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > CORROSION COMMON TO THE INNER SURFACE OF THE FUSELAGE SKIN AT APPROX. FS574.0 AT STR 27, AROUND THE ANTENNA CUT OUT, (C-CHECK) RO: 10/04/2018 REMOVED CORROSION ON FUSELAGE AT FS574 AT STR27 AROUND ANTENNA CUTOUT IAW REO. OPS CHECK GOOD AT THIS TIME.
- [SDR SWIA2018100545125](https://openairdocs.org/sdr/SWIA2018100545125.md): Strap · corroded · Sep 12, 2018 · N8828D · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LT FLOOR STRAP STRUCTURE AT FS559 BETWEEN LBL27 TO LBL45 HAS CORROSION. (C-CHECK) RO: 10/04/2018 REPLACED THE LT FLOOR STRAP AT FS.559.00 BETWEEN LBL.27 AND LBL.45 IAW SRM.
- [SDR SWIA2018100545124](https://openairdocs.org/sdr/SWIA2018100545124.md): Strap · corroded · Sep 12, 2018 · N8828D · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT FLOOR STRAP STRUCTURE AT FS559 BETWEEN RBL27 TO RBL45 HAS CORROSION. (C-CHECK) RO: 10/04/2018 REPLACED THE RT FLOOR STRAP AT FS.559.00 BETWEEN RBL.27 AND RBL.45 IAW SRM.
- [SDR SWIA2018100545123](https://openairdocs.org/sdr/SWIA2018100545123.md): Web · corroded · Sep 12, 2018 · N8828D · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR FWD WEB HAS MULTIPLE SPOTS OF CORROSION. (C-CHECK) RO: 10/04/2018 REMOVED CORROSION LOCATED ON PAX DOOR FWD WEB. ALL STEPS C/W IAW REO.
- [SDR SWIA2018100545122](https://openairdocs.org/sdr/SWIA2018100545122.md): Web · corroded · Sep 12, 2018 · N8828D · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR AFT WEB HAS MULTIPLE SPOTS OF CORROSION. (C-CHECK) RO: 10/04/2018 REMOVED PAX DOOR AFT WEB CORROSION. COMPLIED WITH ALL STEPS OF REO AND SRM.
- [SDR SWIA201642309](https://openairdocs.org/sdr/SWIA201642309.md): Engine · failed · Jul 8, 2016 · N8828D · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > DURING CRUISE, HEARD A LOUD BANG FROM RT ENGINE AND THEN A LOSS OF POWER. ALSO HEARD A VERY LOUD WHINING NOISE. RECEIVED HIGH N1 VIBRATION. PULLED BACK TO IDLE AND THEN FOLLOWED QRH FOR IN FLIGHT SHUTDOWN. R&R RT ENGINE.
- [SDR REXA2015012000059](https://openairdocs.org/sdr/REXA2015012000059.md): Cover · broken · Jan 20, 2015 · N8828D · Cndair CL6002B19 · Emergency Lighting
  > WHILE INSPECTING FLOOR TRACK EMER LIGHTING FOUND FLOOR TRACK LIGHTING COVER BROKEN, CRACKED & DETACHED. R & R FLOOR TRACK LIGHTING COVER IAW AMM 33-51-01. OPERATIONS CHECKED GOOD AT THIS TIME.
- [SDR REXA2015011100023](https://openairdocs.org/sdr/REXA2015011100023.md): Cover · loose · Jan 11, 2015 · N8828D · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHT COVER LOOSE. RESECURED EMERGENCY LIGHT COVER IAW AMM 33-51-01.
- [SDR REXA2014090900886](https://openairdocs.org/sdr/REXA2014090900886.md): Bpsu · failed · Sep 9, 2014 · N8828D · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAIL CAUTION MSG. PERFORMED TROUBLESHOOTING IAW FIM CHAPTER 27-580-00 REV 47 IAW AD 2009-06-12 PARAGRAPH H 6 I AMOC DATED APRIL 22,2014 & TS001100-2014 FIM TECHNICAL SUPPLEMENT. TROUBLE SHOT WRING IAW FIM, CHANGED RT BPSU IAW 27-51-10. FLAP FAIL CODES
- [SDR REXA2014081100808](https://openairdocs.org/sdr/REXA2014081100808.md): Ulb · failed · Aug 11, 2014 · N8828D · Cndair CL6002B19 · Audio/Video Monitoring
  > CVR ULB FAILED FUNCTIONAL TEST. R & R CVR ULB IAW AMM 23-71-03. FUNCTIONAL CHECK GOOD IAW AMM 23-71-03-720-801.
- [SDR REXA2014081100805](https://openairdocs.org/sdr/REXA2014081100805.md): Cover · broken · Aug 11, 2014 · N8828D · Cndair CL6002B19 · Emergency Lighting
  > FLOOR TRACK EMER LIGHT STRIP COVER & BASE IS BROKEN IN MULTIPLE PLACES. REPAIRED FLOOR TRACK EMER LIGHT STRIP IAW AMM 33-51-01. OPERATIONS CHECKED GOOD IAW AMM 33-51-00-710-801.
- [SDR REXA2014080900758](https://openairdocs.org/sdr/REXA2014080900758.md): Skin · corroded · Aug 8, 2014 · N8828D · Cndair CL6002B19 · Wing, Plate/Skin
  > RIGHT WING PLANK CORRODED AT LANDING FOR PANEL 640BB AT WS 54.897. REPAIRED IAW REO 601R-57-21-030.
- [SDR REXA2014080900759](https://openairdocs.org/sdr/REXA2014080900759.md): Skin · corroded · Aug 7, 2014 · N8828D · Cndair CL6002B19 · Wing, Plate/Skin
  > RIGHT WING PLANK CORRODED AROUND LANDING FOR FUEL ACCESS PANEL 610AB AT WS 12.245. REPAIRED IAW REO 601R-57-21-030.
- [SDR REXA2014080700757](https://openairdocs.org/sdr/REXA2014080700757.md): Skin · chafed · Aug 7, 2014 · N8828D · Cndair CL6002B19 · Wing, Plate/Skin
  > FOUND CHAFE DAMAGE TO THE RT WING LOWER AFT WING PLANK AT THE WING JACK POINT WS 144.00 AUX SPAR DATUM. REPAIRED IAW EA CRJ257-02801.
- [SDR REXA2014080700510](https://openairdocs.org/sdr/REXA2014080700510.md): Skin · chafed · Aug 7, 2014 · N8828D · Cndair CL6002B19 · Wing, Plate/Skin
  > FOUND CHAFE DAMAGE TO THE LT WING LOWER AFT WING PLANK AT THE WING JACK POINT WS 144.00, AUX SPAR DATUM. REPAIRED IAW EA CRJ257-02800.
- [SDR REXA2014080700509](https://openairdocs.org/sdr/REXA2014080700509.md): Skin · dented · Aug 7, 2014 · N8828D · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FOUND A DENT TO THE LT FUSELAGE SKIN AT FS 356.00 AT STRINGER 23L. REPAIRED IAW EA CRJ253-02782.
- [SDR REXA2014081000762](https://openairdocs.org/sdr/REXA2014081000762.md): Skin · corroded · Aug 6, 2014 · N8828D · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > SKIN CORRODED AT FS 605 BETWEEN STRINGER 26 & 26R MEASURING 7 INCHES X 4.5 INCHES X 0.033 INCHES DEEP. REPAIRED IAW REO 601R-53-61-5321.
- [SDR REXA2014081000761](https://openairdocs.org/sdr/REXA2014081000761.md): Bulkhead · chafed · Aug 6, 2014 · N8828D · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FORWARD FACE OF FS 621 BULKHEAD CHAFED FROM SCREW HEADS IN 13 PLACES. REPAIRED IAW REO 601R-53-61-2155.
- [SDR REXA2014080600756](https://openairdocs.org/sdr/REXA2014080600756.md): Spar · gouged · Aug 4, 2014 · N8828D · Cndair CL6002B19 · Nacelle/Pylon, Frame/Spar/Rib
  > LEFT ENG PYLON BOX FRAME FWD ENG YOKE MOUNT SPAR GOUGED IN THREE PLACES. REPAIRED IAW REO 601R-54-51-341.
- [SDR REXA2014080500755](https://openairdocs.org/sdr/REXA2014080500755.md): Fitting · cracked · Aug 1, 2014 · N8828D · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT OTBD CLIP OF FS 280 BULKHEAD CRACKED. REPAIRED IAW REO 601R-53-11-171.
- [SDR REXA2014080100506](https://openairdocs.org/sdr/REXA2014080100506.md): Frame · corroded · Aug 1, 2014 · N8828D · Cndair CL6002B19 · Fuselage Main, Frame
  > FOUND CORROSION ON THE LOWER FRAME SECTOR AT FS 605.00 BETWEEN STRINGER 25R & 26L. REPAIRED IAW EA CRJ253-02772.
- [SDR REXA2014080100505](https://openairdocs.org/sdr/REXA2014080100505.md): Skin · dented · Aug 1, 2014 · N8828D · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FOUND A DENT IN THE LT FUSELAGE SKIN AT FS 615.00. REPAIRED IAW EA CRJ253-02758.
- [SDR REXA2013111602257](https://openairdocs.org/sdr/REXA2013111602257.md): Selector Valve · faulty · Nov 16, 2013 · N8828D · Cndair CL6002B19 · Landing Gear Selector
  > GEAR DISAGREE WARNING MESSAGE WHEN PULLED LG DOWN ON FINAL RST RW 13 6 NM OUT AT 3000' 180 KISA. QRH COMPLETE WITH MANUAL GEAR EXTENSION FULL UP, GEAR CAME DOWN WITH ALL 3 GREEN LANDED NORMAL. R & R PSEU IAW AMM 32-61-01, NO HELP. R & R MLG SELECTOR VLV IAW
- [SDR REXA2013071701374](https://openairdocs.org/sdr/REXA2013071701374.md): Container · damaged · Jul 17, 2013 · N8828D · Cndair CL6002B19 · Life Jacket
  > FO`S LIFE VEST HAS A HOLE IN BAG. R & R F/O`S LIFE VEST IAW AMM 25-61-03.
- [SDR REXA2013032500593](https://openairdocs.org/sdr/REXA2013032500593.md): Life Vest · unserviceable · Mar 25, 2013 · N8828D · Cndair CL6002B19 · Life Jacket
  > CAPTAIN LIFE VEST BAG TORN. REMOVED AND REPLACED CAPTAIN'S LIFE VEST IAW AMM 25-61-03.
- [SDR REXA2013022400425](https://openairdocs.org/sdr/REXA2013022400425.md): Light · inoperative · Feb 24, 2013 · N8828D · Cndair CL6002B19 · Emergency Lighting
  > FORWARD OVERHEAD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED FWD EMERGENCY LIGHT IAW AMM 33-51-16. OPS CHECKED GOOD, ACFT OK FOR SERVICE.
- [SDR REXA2013020300083](https://openairdocs.org/sdr/REXA2013020300083.md): Skin · cracked · Feb 2, 2013 · N8828D · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN AT FS 780.00 DENTED BETWEEN S-25L AND S-26L AND CRACKED. REPAIRED IAW EA CRJ253-01255A AS APPROVED BY 8110-3 DATED FEBRUARY 1, 2013.
- [SDR REXA2013020300087](https://openairdocs.org/sdr/REXA2013020300087.md): Bulkhead · cracked · Feb 1, 2013 · N8828D · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD AT FS 621 CRACKED AT THE LINTEL FITTING LOWER EDGE. REPAIRED IAW BOMBARDIER REO 601R-53-61-1230.
- [SDR REXA2013020300086](https://openairdocs.org/sdr/REXA2013020300086.md): Stiffener · cracked · Feb 1, 2013 · N8828D · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > Z-STIFFENER CRACKED AT WL 47 ON AFT SIDE OF FS 202 BULKHEAD ON LEFT SIDE NEAR PARKING BRAKE CABLE FEED THRU. REPLACED IAW SRM 51-24-00.
- [SDR REXA2013020300085](https://openairdocs.org/sdr/REXA2013020300085.md): Bulkhead · cracked · Feb 1, 2013 · N8828D · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > PRESSURE BULKHEAD AT FS 202.75 AT LL 23.75 CRACKED. REPAIRED IAW BOMBARDIER REO 601R-53-11-563.
- [SDR REXA2013012000212](https://openairdocs.org/sdr/REXA2013012000212.md): Door · lack of lube · Jan 20, 2013 · N8828D · Cndair CL6002B19 · Emergency Exits
  > DURING HEAVY CHECK RIGHT OVERWING EMERGENCY EXIT DOOR FAILED FUNCTIONAL CHECK. (AIRCRAFT WAS IN HEAVY CHECK 1/19/2013 THROUGH 2/3/2013). PERFORMED LUBE OF RT OVERWING EMERGENCY EXIT IAW CRJ 200 AMM 12-20-52 PERFORMED FUNCTIONAL CHECK OF RT EMERGENCY EXIT I
- [SDR REXA2013010800119](https://openairdocs.org/sdr/REXA2013010800119.md): Striker · damaged · Jan 8, 2013 · N8828D · Cndair CL6002B19 · Passenger/Crew Doors
  > EXTREMELY HIGH PITCH NOISE COMING FROM THE MAIN CABIN DOOR IN FLIGHT. NOISE STOPPED AS WE STARTED THE DESCENT. REPAIRED PASSENGER DOOR STRIKER IN 2 SPOTS ON THE AFT PORTION IAW REO601R-53-22-033.
- [SDR REXA2013010300110](https://openairdocs.org/sdr/REXA2013010300110.md): Light · shorted · Jan 3, 2013 · N8828D · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHT FLOOR STRIP ROW 2 SHORTED OUT. REPLACED FLOOR LIGHT STRIP IAW AMM 33-51-01.
- [SDR REXA2012111801687](https://openairdocs.org/sdr/REXA2012111801687.md): Inverter · inoperative · Nov 18, 2012 · N8828D · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY FLOOR STRIPS 6 TO 8 INOPERABLE. REMOVED AND REPLACED NR 3 INVERTER AND NR 8 FLOOR TRACK STRIP IAW AMM 33-51-07 AND AMM 33-51-01. OPS CHECK GOOD.
- [SDR REXA2012101401407](https://openairdocs.org/sdr/REXA2012101401407.md): Light · inoperative · Oct 14, 2012 · N8828D · Cndair CL6002B19 · Emergency Lighting
  > FORWARD EMERGENCY LIGHT STRIP AT ROW 11 RIGHT INOPERABLE. REPLACED EMERGENCY LIGHT STRIP IAW CRJ-200 AMM 33-51-01. OPS CHECK GOOD.
- [SDR REXA2012101401401](https://openairdocs.org/sdr/REXA2012101401401.md): Strip · out of position · Oct 14, 2012 · N8828D · Cndair CL6002B19 · Emergency Lighting
  > ORANGE STRIP AT SEAT 8C FOR EMERGENCY EXIT FLOOR PATH LIGHTING STRIP IS LOCATED AT SEAT 10C. RELOCATED EMERGENCY ORANGE STRIP TO SEAT 8C, OPS CHECK GOOD IAW AMM 33-51-01.
- [SDR REXA2012082101289](https://openairdocs.org/sdr/REXA2012082101289.md): Power Supply · inoperative · Aug 21, 2012 · N8828D · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAILED AT 0' 200 KTS ON APPROACH. PERFORMED TROUBLESHOOTING PER FIM REV 43 IAW AD 2009-06-12 (H)(6)(I) AMOC DATED APRIL 2012 AND PA 27-05H. FOUND LT BPSU BAD, REMOVED AND REPLACED LT BPSU IAW CRJ 200 AMM 27-51-01. ALL CHECKED GOOD.
- [SDR REXA2012080701244](https://openairdocs.org/sdr/REXA2012080701244.md): Sensor · out of adjust · Aug 7, 2012 · N8828D · Cndair CL6002B19 · Landing Gear Position and Warning
  > AFTER TAKEOFF, FLIGHT 4093, GEAR HANDLE IN THE UP POSITION RECEIVED A NOSE GEAR WARNING ALONG WITH GEAR DISAGREE. DID NOT DECLARE AN EMERGENCY. PERFORMED AN AIR RETURN. COMPLIED WITH PA 05-018 REV G. FOUND NLG OLEO CENTERING EXTENDED SENSOR (PS14GA) TO TAR
- [SDR REXA2012071001064](https://openairdocs.org/sdr/REXA2012071001064.md): Bpsu · out of adjust · Jul 10, 2012 · N8828D · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAILED AT 30 DEGREES ON APPROACH. PERFORMED TROUBLESHOOTING PER FIM REV 39 IAW AD 2009-06-12 PARAGRAPH (H)(6)(I). AMOC DATED MARCH 27, 2009, TR NR 27-012 PER AMOC DECEMBER 18, 2009 AND PA AD27-052G. FOUND LEFT BPSU OUT OF ADJUSTMENT. ADJUSTED LEFT BPS
- [SDR REXA2012071001063](https://openairdocs.org/sdr/REXA2012071001063.md): Cover · damaged · Jul 10, 2012 · N8828D · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHT COVER HAS SEVERAL DAMAGED AREAS AND STRIP IS PULLING AWAY FROM FLOORBOARD IN AFT CABIN. REMOVED AND REPLACED SECTIONS OF LIGHT COVER IAW AMM 33-51-01.
- [SDR REXA2012040800485](https://openairdocs.org/sdr/REXA2012040800485.md): Pbe · damaged · Apr 8, 2012 · N8828D · Cndair CL6002B19 · Portable Oxygen System
  > COCKPIT PBE IS MUSHY AND INDICATOR IS NOT LIGHT BLUE. REMOVED & REPLACED COCKPIT PBE IAW CMM PRM-01 AND AMM 35-30-00, OK FOR SERVICE.
- [SDR REXA201200120](https://openairdocs.org/sdr/REXA201200120.md): Light · damaged · Jan 14, 2012 · N8828D · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY FLOOR TRACK LIGHTING FIRST ONE DAMAGED. REMOVED AND REPLACED EMERGENCY FLOOR TRACK LIGHTING STRIP IAW AMM 33-51-01.
- [SDR REXA201100818](https://openairdocs.org/sdr/REXA201100818.md): Bulkhead · cracked · Nov 17, 2011 · N8828D · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > THE 559 SEMI-PRESSURE BULKHEAD CRACKED IN WEB ANGLE AT LBL 9 AND RBL 9. REPAIRED IAW PA53-025 IAW REO 601R-53-41-260 REV E AND 601R-53-41-609 REV B.
- [SDR REXA201100735](https://openairdocs.org/sdr/REXA201100735.md): Flashlight · inoperative · Oct 18, 2011 · N8828D · Cndair CL6002B19 · Emergency Equipment
  > FA FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY TO FA FLASHLIGHT IAW AMM 25-61-04. NO FIX 'VERIFIED PART EFFECTIVITY'. REMOVED AND REPLACED FA EMERGENCY FLASHLIGHT ASSY IAW AMM 25-61-04. OPC GOOD. "VERIFIED PART EFFECTIVITY".
- [SDR REXA201100595](https://openairdocs.org/sdr/REXA201100595.md): Circuit Breaker · tripped · Sep 13, 2011 · N8828D · Cndair CL6002B19 · Fuel Transfer Valve
  > APU XFLOW MSG FOUND CBP 1 N10 XFLOW/APU FUEL CB OUT AND PERFORMED RESET NO DEFECTS NOTED. OPS CHECK GOOD IAW AMM 28-24-01.
- [SDR REXA201100472](https://openairdocs.org/sdr/REXA201100472.md): Steering Sys · malfunctioned · Jul 19, 2011 · N8828D · Cndair CL6002B19 · Landing Gear Steering System
  > NOSE WHEEL STEERING INOP INSPECT NWS SYSTEM IAW AMM 32-51-10 AND OPS CHECKED IAW AMM 32-51-00, NO DEFECTS NOTED AT THIS TIME. A/C OK FOR SERVICE.
- [SDR REXA201100032](https://openairdocs.org/sdr/REXA201100032.md): Skin · damaged · Jan 6, 2011 · N8828D · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > THERE IS A LIFE LIMITED SKIN REPAIR BETWEEN FS 587.00 AND FS 605.00 FROM STRINGER 22R TO 26R. PERFORMED A MAJOR REPAIR TO THE FUSELAGE SKIN BETWEEN FS 587 AND FS 605 FROM STRINGER 22R TO 26R IN ACCORDANCE WITH BOMBARDIER AEROSPACE REPAIR ENGINEERING ORDER 601
- [SDR REXA201100031](https://openairdocs.org/sdr/REXA201100031.md): Floor Support · corroded · Jan 6, 2011 · N8828D · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 280 FORWARD FLOOR SUPPORT ANGLE P/N 600-34017-351 CORRODED. REMOVED AND REPLACED SUPPORT ANGLE IAW CRJ 200 SRM 51-42-06.

Next page: https://openairdocs.org/aircraft/N8828D/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 = 'N8828D' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8828D/reports

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