# Service difficulty reports: N8944B

A list on [N8944B](https://openairdocs.org/aircraft/N8944B.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 · 74 reports

- [SDR REXA2017090400960](https://openairdocs.org/sdr/REXA2017090400960.md): Flap System · malfunctioned · Sep 4, 2017 · N8944B · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAIL CAUTION DURING DESCENT ON THE APPROACH AT 200 KIAS, FULL SPOILER, THRUST FLIGHT IDLE,AUTOPILOT ON + COUPLED TO THE ILS,TRIED TO EXTEND FLAPS FROM 0 TO 8.FLAPS REMAINED AT O.OAT ON THE GROUND WAS 27 C.NO TURBULANCE.APU ON.35MIN INTO FLIGHT. INFLI
- [SDR REXA2017083100951](https://openairdocs.org/sdr/REXA2017083100951.md): Oxygen Mask · leaking · Aug 31, 2017 · N8944B · Cndair CL6002B19 · Crew Oxygen System
  > CAPTAIN`S OXYGEN MASK LEAKING AT LINE SWIVEL. REMOVED AND REPLACED THE CAPTAIN`S OXYGEN MASK IAW AMM 35-11-12-400-801. OPS AND LEAK CHECKED GOOD. SERVICED TO 1840 PSI.
- [SDR REXA2017042800557](https://openairdocs.org/sdr/REXA2017042800557.md): Smoke Detector · inoperative · Apr 28, 2017 · N8944B · Cndair CL6002B19 · Smoke Detection
  > TOILET SMOKE CAUTION AFTER FA DUMPED COFFEE ONTO TOILET. THE CAUTION CLEARED. LAV SMOKE DETECTOR WOULD NOT RE-TEST AFTER. PERFORMED OPERATIONAL TEST OF THE LAV FIRE DETECTOR AS PER AMM 26-16-01. OPS CHECK GOOD. NO DEFECTS NOTED. OK FOR SVC.
- [SDR REXA2017012100086](https://openairdocs.org/sdr/REXA2017012100086.md): Bpsu · out of rig · Jan 21, 2017 · N8944B · Cndair CL6002B19 · Trailing Edge Flap Control System
  > EICAS MESSAGE RECEIVED FLAPS FAIL IN FLIGHT, 2 MINUTES AFTER TAKEOFF DURING FLAP RETRACTION. FLAPS FAILED AT 20 DEG DURING RETRACTION. AIRSPEED WAS 160 AND OAT WAS 12 DEG C. RESET FLAPS PER FIM 27-50-00 CYCLED FLAPS 5 TIMES NO DEFECTS NOTED. PERFORMED TROUBL
- [SDR REXA2017010800014](https://openairdocs.org/sdr/REXA2017010800014.md): Oxygen Bottle · empty · Jan 8, 2017 · N8944B · Cndair CL6002B19 · Emergency Equipment
  > PORTABLE OXYGEN BOTTLE EMPTY. R & R PORTABLE OXYGEN BOTTLE IAW AMM 35-30-00. OK FOR SERVICE.
- [SDR REXA2016121602552](https://openairdocs.org/sdr/REXA2016121602552.md): Control Unit · inoperative · Dec 16, 2016 · N8944B · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAILED AT 20 DEGREES. RESET FLAP CIRCUIT BREAKERS. FLAPS CYCLED FIVE TIMES NORMALLY. PERFORMED TROUBLESHOOTING IAW FIM REV. 51 FOUND AND ADJUSTED THE LT & RT BPSU. REMOVED & REPLACED TEH FECU. COMPLETED RIGGING IAW AMM 27-51-10.
- [SDR REXA2016010400020](https://openairdocs.org/sdr/REXA2016010400020.md): Angle · cracked · Jan 4, 2016 · N8944B · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LOWER CAP ANGLE AT LBL 18, FS 559.0, IS CRACKED IN RADIUS. IDENTIFIED DURING SDI FS 559.0 IAW NDTM PT 6 53-41-201. REPAIRED LOWER CAP ANGLE IAW P35025 REO601R-53-41-260 REV E & REO 601R-53-41-609 REV B.
- [SDR REXA2016010200019](https://openairdocs.org/sdr/REXA2016010200019.md): Skin Panel · cracked · Jan 2, 2016 · N8944B · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > SKIN BELOW AFT LATCH FOR PANEL 211AL IS CRACKED. R & R PANEL IAW SRM 51-42-06 PAR 6, 51-42 -10 PAR 8 & 51-42-21 PAR 6.
- [SDR REXA2015122701266](https://openairdocs.org/sdr/REXA2015122701266.md): Fitting · cracked · Dec 27, 2015 · N8944B · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT FUSELAGE COMPARTMENT, REAR PRESS BULKHEAD AFT SIDE CLIP ON INTERCOSTAL IS CRACKED, FS 621, STRINGER 14A LT AT FUSELAGE SKIN. R & R CRACKED CLIP WITH A SERVICEABLE FORMED CLIP AT FS 621, STRINGER 14A IAW REO 601R-53-61-5265 SRM 51-42-21.
- [SDR REXA2015122701263](https://openairdocs.org/sdr/REXA2015122701263.md): Floorbeam · cracked · Dec 27, 2015 · N8944B · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CLIP AT FS 280, FLOORBEAM OTBD OF RBL 9 IS CRACKED. R & R CLIP IAW REO 601R-53-11-171.
- [SDR REXA2015122701261](https://openairdocs.org/sdr/REXA2015122701261.md): Floorbeam · cracked · Dec 27, 2015 · N8944B · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FS 280, FLOORBEAM OTBD OF LBL 9, IS CRACKED AT UPPER & LOWER FLANGE. REPAIRED FS 280 FLOORBEAM IAW REO 601R-53-11-171 & REO 601R-53-11-136.
- [SDR REXA2015122601265](https://openairdocs.org/sdr/REXA2015122601265.md): Fitting · cracked · Dec 26, 2015 · N8944B · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT FUSELAGE COMPARTMENT, REAR PRESS BULKHEAD VERTICAL STIFFENER LOWER CLIP IS CRACKED, FS 621, STRINGER 24A LT. R & R CRACK CLIP WITH A SERVICEABLE CLIP IAW SRM 51-42-21.
- [SDR REXA2015122601264](https://openairdocs.org/sdr/REXA2015122601264.md): Fitting · cracked · Dec 26, 2015 · N8944B · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT FUSELAGE COMPARTMENT, REAR PRESS BULKHEAD AFT SIDE CLIP ON INTERCOSTAL IS CRACKED, FS 621, STRINGER 13A LT AT FUSELAGE SKIN. R & R CRACKED CLIP WITH A SERVICEABLE CLIP IAW REO 601R-53-61-100 & SRM 51-42-21 & REO 601R-53-61-5265.
- [SDR REXA2015122601262](https://openairdocs.org/sdr/REXA2015122601262.md): Floorbeam · cracked · Dec 26, 2015 · N8944B · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FS 280, FLOORBEAM OTBD OF RBL 9 IS CRACKED AT UPPER & LOWER FLANGE. REPAIRED FS 280 FLOORBEAM IAW REO 601R-53-11-171 & 601R-53-11-2847.
- [SDR REXA2015122301274](https://openairdocs.org/sdr/REXA2015122301274.md): Door Sill · cracked · Dec 23, 2015 · N8944B · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 621 FLOOR SUPPORT STRUCTURE AT RT FLOOR SILL IS CRACKED. R & R CRACKED SECTION OF FLOOR SILL IAW REO 601R-53-61-117 & SRM 51-42-06.
- [SDR REXA2015122301267](https://openairdocs.org/sdr/REXA2015122301267.md): Seat Track · corroded · Dec 23, 2015 · N8944B · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK NR 3 ON RBL 9, HAS SEVERAL AREAS OF CORROSION. R & R SEAT TRACK NR 3, STATION 412 - 525 IAW AMM 53-01-11.
- [SDR REXA2015122201277](https://openairdocs.org/sdr/REXA2015122201277.md): Angle · cracked · Dec 22, 2015 · N8944B · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR POWER ASSIST MOTOR LOWER MOUNT ANGLE CRACKED. R & R PAX DOOR POWER ASSIST MOTOR LOWER MOUNT ANGLE IAW SRM 51-42-06.
- [SDR REXA2015122201276](https://openairdocs.org/sdr/REXA2015122201276.md): Drag Angle · cracked · Dec 22, 2015 · N8944B · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR AFT DRAG ANGLE CRACKED. REPAIRED DRAG ANGLE IAW 601R-52-11-513.
- [SDR REXA2015122101280](https://openairdocs.org/sdr/REXA2015122101280.md): Fitting · cracked · Dec 21, 2015 · N8944B · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CLIP AT FS 265 & STRINGER 3L IS CRACKED. R & R FS 265 CLIP, STRINGER 3L IAW SRM 51-42-21.
- [SDR REXA2015122101279](https://openairdocs.org/sdr/REXA2015122101279.md): Fitting · cracked · Dec 21, 2015 · N8944B · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CLIP AT FS 265 & STRINGER 3R IS CRACKED. R & R FS 265 & STRINGER 3R IAW SRM 51-42-21.
- [SDR REXA2015122101278](https://openairdocs.org/sdr/REXA2015122101278.md): Bracket · cracked · Dec 21, 2015 · N8944B · Cndair CL6002B19 · Wing, Attach Fittings
  > LOWER OTBD CORNER OF FUEL SERVICING BRACKET IS CRACKED. R & R FUEL SERVICING BRACKET IAW SRM 51-41-02 & 51-40-11.
- [SDR REXA2015122101275](https://openairdocs.org/sdr/REXA2015122101275.md): Bulkhead · cracked · Dec 21, 2015 · N8944B · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FORWARD FACE OF REAR PRESS BULKHEAD IS CRACKED AT LINTEL FITTING INBD EDGES. REPAIRED FWD PRESS BULKHEAD FWD FACE AT LINTEL FITTING IAW REO 601R-53-61-1230.
- [SDR REXA2015121901273](https://openairdocs.org/sdr/REXA2015121901273.md): Fitting · cracked · Dec 19, 2015 · N8944B · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AFT FUSELAGE COMPARTMENT, REAR PRESS BULKHEAD AFT SIDE CLIP IS CRACKED, FS 621, STRINGER 13A RT, AT FUSELAGE SKIN. R & R CLIP IAW SRM 51-42-06 PAR 6 & 51-42-21 PAR 6.
- [SDR REXA2015121901272](https://openairdocs.org/sdr/REXA2015121901272.md): Fitting · cracked · Dec 19, 2015 · N8944B · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AFT FUSELAGE COMPARTMENT REAR PRESS BULKHEAD AFT SIDE CLIP IS CRACKED, FS 621 & STRINGER 14A. R & R CLIP IAW SRM 51-42-21.
- [SDR REXA2015121901271](https://openairdocs.org/sdr/REXA2015121901271.md): Seat Track · corroded · Dec 19, 2015 · N8944B · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT SIDE SEAT TRACK HAS SEVERAL AREAS OF CORROSION, FROM FS 449 - 499. R & R CORRODED RT SIDE SEAT TRACK WITH A NEW RT SIDE SEAT TRACK PN 601R38312-115, TAG 69381 IAW AMM 53-01-11.
- [SDR REXA2015121901270](https://openairdocs.org/sdr/REXA2015121901270.md): Fitting · cracked · Dec 19, 2015 · N8944B · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CLIP AT FS 484, OTBD OF RBL 27 IS CRACKED. REMOVED DAMAGED CLIP & INSTALLED NEW CLIP IAW SRM 51-42-20.
- [SDR REXA2015121901268](https://openairdocs.org/sdr/REXA2015121901268.md): Fitting · cracked · Dec 19, 2015 · N8944B · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CLIP AT FS 484, OTBD OF LBL 27 IS CRACKED. REMOVED DAMAGED CLIP & INSTALLED NEW CLIP IAW SRM 51-40-20. "
- [SDR REXA2015121901260](https://openairdocs.org/sdr/REXA2015121901260.md): Fitting · cracked · Dec 19, 2015 · N8944B · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT FUSELAGE COMPARTMENT, REAR PRESS BULKHEAD, AFT SIDE CLIP IS CRACKED, FS 621, STRINGER 16A RT AT FUSELAGE SKIN. R & R CLIP IAW SRM 51-42-21 & 51-42-01.
- [SDR REXA2015121901259](https://openairdocs.org/sdr/REXA2015121901259.md): Fitting · cracked · Dec 19, 2015 · N8944B · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CLIP AT FS 484, INBD OF LBL 36, IS CRACKED. REMOVED DAMAGED CLIP, INSTALLED NEW CLIP IAW SRM 51-42-20&51-40-20.
- [SDR REXA2015121901258](https://openairdocs.org/sdr/REXA2015121901258.md): Fitting · cracked · Dec 19, 2015 · N8944B · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT FUSELAGE COMPARTMENT, REAR PRESS BULKHEAD AFT SIDE CLIP IS CRACKED, FS 621 & STRINGER 15A RT AT FUSELAGE SKIN. R & R CLIP IAW SRM 51-42-21 & 51-42-06.
- [SDR REXA2015122801257](https://openairdocs.org/sdr/REXA2015122801257.md): Fitting · cracked · Dec 18, 2015 · N8944B · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT FUSELAGE COMPARTMENT, REAR PRESS BULKHEAD VERTICAL STIFFENER LOW ER CLIP IS CRACKED FS 621, STRINGER 25A LT. R & R AFT PRESS BULKHEAD, VERTICAL STIFFENER LOWER CLIP AT FS 621, STRINGER 25A LT IAW SRM 51-42-21.
- [SDR REXA2015121301269](https://openairdocs.org/sdr/REXA2015121301269.md): Intercostal · cracked · Dec 13, 2015 · N8944B · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CARGO DOOR FWD TRACK SUPPORT INTERCOSTAL IS CRACKED. R & R CRACKED INTERCOSTAL IAW SRM 51-42-06 & 51-42-20.
- [SDR REXA2015102300987](https://openairdocs.org/sdr/REXA2015102300987.md): Light · inoperative · Oct 23, 2015 · N8944B · Cndair CL6002B19 · Emergency Lighting
  > CABIN EMER LIGHT CEILING FLOOD LIGHT INOPERATIVE, 2ND FLOOD FROM FRONT. R & R EMER LIGHT IAW AMM 33-51-16. THIS CLEARS MEL 33-51-11. REMOVED FROM MM02.
- [SDR REXA2015071800721](https://openairdocs.org/sdr/REXA2015071800721.md): Priority Valve · faulty · Jul 18, 2015 · N8944B · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > GEAR DISAGREE WARNING MSG INFLIGHT, QRH COMPLETED. GEAR STATUS NOSE GEAR DOWN BOTH MAINS UP MANUAL RELEASE HANDLE WAS REQUIRED TO EXTEND THE GEAR, SPEED 210 KTS ALTITUDE 3500 FT FLT SPLRS WERE DEPLOYED. R & R MLG PRIORITY VLV IAW AMM 32-32-15. OPERATIONS CH
- [SDR REXA2014072200728](https://openairdocs.org/sdr/REXA2014072200728.md): Life Vest · unserviceable · Jul 22, 2014 · N8944B · Cndair CL6002B19 · Life Jacket
  > ONE INFANT LIFE VEST BAG TORN. R & R INFANT LIFE VEST IAW PA25-096A.
- [SDR REXA2014052800532](https://openairdocs.org/sdr/REXA2014052800532.md): Target · loose · May 28, 2014 · N8944B · Cndair CL6002B19 · Landing Gear Position and Warning
  > GEAR DISAGREE MASTER WARNING BRINGING GEAR UP AFTER TAKEOFF. DISAGREE WITH LT MAIN. DEFER LG SYS IAW MEL 32-30-01. PLACARD INSTALLED ENTERED IN MM02. FOUND LT MLG UP LOCK PROX SENSOR TARGET LOOSE CAUSING GEAR DISAGREE. R & R LT MLG UP LOCK ASSEMBLY IAW AMM
- [SDR REXA2014052800530](https://openairdocs.org/sdr/REXA2014052800530.md): Warning System · activated · May 28, 2014 · N8944B · Cndair CL6002B19 · Landing Gear Position and Warning
  > GEAR DISAGREE, LT MAIN GEAR. DEFERRED MORE INFORMATION TO COME.
- [SDR REXA2014021800212](https://openairdocs.org/sdr/REXA2014021800212.md): Life Vest · unserviceable · Feb 18, 2014 · N8944B · Cndair CL6002B19 · Life Jacket
  > FLIGHT ATTENDANT'S LIFE VEST BAG TORN;. R & R FLIGHT ATTENDANT'S LIFE VEST IAW AMM 25-61-03.
- [SDR REXA2014012600135](https://openairdocs.org/sdr/REXA2014012600135.md): Warning System · false activation · Jan 26, 2014 · N8944B · Cndair CL6002B19 · Engine Oil Pressure
  > AFTER TAKEOFF FROM CMH AT ABOUT 26000 FT, LT ENG OIL PRESS WARNING MESSAGE ILUMINATED. OIL PRESS WAS FLUCTUATING BETWEEN 23 - 32 PSI, APPROXIMATELY 4 - 5 MIN LATER PRESS FELL BELOW 25 & STAYED IN THE RED. COMPLETED QRH & SHUT DOWN LT ENG. DIVERTING TO DTW D
- [SDR REXA2014012000126](https://openairdocs.org/sdr/REXA2014012000126.md): Life Vest · unserviceable · Jan 20, 2014 · N8944B · Cndair CL6002B19 · Life Jacket
  > INFANT LIFE VEST BAG TORN. REPLACED ONE TORN INFANT LIFE VEST IAW PA28-096A.
- [SDR REXA2014011900122](https://openairdocs.org/sdr/REXA2014011900122.md): Battery · discharged · Jan 19, 2014 · N8944B · Cndair CL6002B19 · Emergency Equipment
  > CAPTAIN`S EMERGENCY FLASHLIGHT FAILS RED LED TEST. REPLACED CAPTAIN`S FLASHLIGHT BATTERY, OPERATIONS CHECKED GOOD IAW AMM 25-61-00-02.
- [SDR REXA2014010300105](https://openairdocs.org/sdr/REXA2014010300105.md): Smoke Warning · false activation · Jan 3, 2014 · N8944B · Cndair CL6002B19 · Smoke Detection
  > SMOKE, TOILET CAUTION MESSAGE. OPERATIONS CHECKED LAVATORY SMOKE DETECTION SYS IAW 26-16-00 AMM. OPERATIONS CHECKED NORMAL. INSPECTED LAVATORY FIRE EXTINGUISHER NO DISCHARGE, INSPECTED LAVATORY TRASH BIN NO FIRE NOTED. OK FOR SERVICE.
- [SDR REXA2013111502256](https://openairdocs.org/sdr/REXA2013111502256.md): Smoke Detector · faulty · Nov 15, 2013 · N8944B · Cndair CL6002B19 · Smoke Detection
  > SMOKE TOILET MESSAGE AFTER TAKEOFF. R & R LAVATORY SMOKE DETECTOR IAW AMM 26-61-01, OPERATIONS CHECKED NORMAL. COMPLIED WITH MIN WORK SCOPE SMOKE & FUMES IN CABIN, FLIGHT DECK, SMOKE TOILET MESSAGE, NO DEFECTS NOTED. ACFT READY FOR SERVICE.
- [SDR REXA2013091701738](https://openairdocs.org/sdr/REXA2013091701738.md): Coalescer Bag · dirty · Sep 17, 2013 · N8944B · Cndair CL6002B19 · Humidity Control System
  > DURING TAKEOFF BURNED ODOR FROM AIR CONDIONER PACKS. POSSIBLE PACK FILTER, REMOVED LT AND RT COALESCERS AND INSTALLED SERVICE UNITS NO ABNORMAL ODORS NOTED WHILE ACMS RUNNING FROM APU AND ENG BLEEDS IAW MM 21-51-13.
- [SDR REXA2013042200759](https://openairdocs.org/sdr/REXA2013042200759.md): Battery Pack · discharged · Apr 22, 2013 · N8944B · Cndair CL6002B19 · Emergency Lighting
  > LEFT AND RIGHT NR 1 EMERGENCY LIGHTS (EXTERIOR) INOPERABLE. REMOVED AND REPLACED BATTERY PACK IAW AMM 33-51-04. OPERATIONS CHECK GOOD.
- [SDR REXA2013021000287](https://openairdocs.org/sdr/REXA2013021000287.md): Life Vest · unserviceable · Feb 10, 2013 · N8944B · Cndair CL6002B19 · Life Jacket
  > 1 INFANT LIFE VEST BAG TORN. REMOVED AND REPLACED INFANT LIFE VEST IAW PA 25-096A.
- [SDR REXA2012042200078](https://openairdocs.org/sdr/REXA2012042200078.md): Hinge · worn · Apr 22, 2012 · N8944B · Cndair CL6002B19 · Fuselage, Door Hinge
  > PAX DOOR HINGE WORN (FUSELAGE HINGE). REMOVED AND REPLACED WORN HINGE IAW CRJ-200 SRM 53-21-23.
- [SDR REXA2012041900077](https://openairdocs.org/sdr/REXA2012041900077.md): Floor Support · corroded · Apr 19, 2012 · N8944B · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 280.00 AFT COCKPIT FLOOR PANEL LANDING CORRODED. DOT A247 021. REMOVED DAMAGED COCKPIT FLOOR PANEL LANDING AT FS 280.00 AND INSTALLED NEW IAW CRJ -200 SRM 51-42-06. CR3213-5-4 TAG B97282, 600-34017-3515 TAG B11214 B0203013-08 TAG B03442, HST1DA65-4 TAG B
- [SDR REXA2012041900076](https://openairdocs.org/sdr/REXA2012041900076.md): Beam · corroded · Apr 19, 2012 · N8944B · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > COCKPIT FLOOR 280 BEAM WEB BL 0 EXFOLIATED. REPAIRED COCKPIT FLOOR 280 BEAM AT BL 0 IAW REO 601R-53-111-2309 T/N B46967 P/N MS2047AD5-6, T/N B97100 P/N MS2047AD5-5, T/N 09073 P/N PG6W2-202, T/N B12170 P/N PS870B1/2-TU AAR SM-28.
- [SDR REXA2012041900075](https://openairdocs.org/sdr/REXA2012041900075.md): Fitting · cracked · Apr 19, 2012 · N8944B · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > TWO EACH LBL 9 AND RBL 9 AT 280, EVIDENCE OF CRACKING. REMOVED DAMAGED 2 EA LBL 9 AND RBL 9 AT 280 CLIPS AND INSTALLED NEW IAW CRJ-200 SRM 51-41-21 HST10A65-4 TAG B10430 HST10A65-2 TAG B01346, B0203013-03 TAG B11523 HST10A65-2 TAG B07178 AAR SM-28.

Next page: https://openairdocs.org/aircraft/N8944B/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 = 'N8944B' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8944B/reports

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