# Service difficulty reports: N8416B

A list on [N8416B](https://openairdocs.org/aircraft/N8416B.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 · 60 reports

- [SDR REXA2015010300002](https://openairdocs.org/sdr/REXA2015010300002.md): Smoke Detector · malfunctioned · Jan 3, 2015 · N8416B · Cndair CL6002B19 · Smoke Detection
  > RECEIVED AN INTERMITTENT SMOKE TOILET CAUTION MESSAGE, SIX TIMES. THE LAVATORY SMOKE ALARM ALSO WENT OFF, BUT NOT AT THE SAME TIMES AS THE SMOKE TOILET CAUTION MESSAGE. REMOVED & RESEATED SMOKE DETECTOR, OPS CHECKED GOOD IAW AMM 26-16-00.
- [SDR REXA2014121401190](https://openairdocs.org/sdr/REXA2014121401190.md): Wire Harness · defective · Dec 14, 2014 · N8416B · Cndair CL6002B19 · Landing Gear System Wiring
  > AIR RETURN DUE TO NOSE DOOR OPEN & NOSE GEAR DISAGREE WARNING MSG. R & R PROX SENSOR HARNESS IAW AMM 32-61-25. SERVICED GEAR IAW AMM 12-12-32. PERFORMED EXTENSION & RETRACTION, CHECKED IAW AMM 32-30-00. ALL CHECKED NORMAL. NO DEFECTS NOTED.
- [SDR REXA2014071100685](https://openairdocs.org/sdr/REXA2014071100685.md): Selector Valve · inoperative · Jul 11, 2014 · N8416B · Cndair CL6002B19 · Landing Gear Selector
  > GEAR DISAGREE WARNING MSG ON FINAL. NOSE DOOR OPEN WARNING MSG A SECOND LATER. MAINS TURNED DOWN & LOCKED GREEN. A SECOND LATER MSG WENT OUT & NOSE TURNED DOWN & LOCKED GREEN, MSG STAYED OUT. DEFERRED LG RETRACTION SYS IAW MEL 32-30-01. ENTERED INTO DMR PL
- [SDR REXA2014062900640](https://openairdocs.org/sdr/REXA2014062900640.md): Life Vest · unserviceable · Jun 29, 2014 · N8416B · Cndair CL6002B19 · Life Jacket
  > CAPTAIN`S LIFE VEST BAG TORN. R & R CAPTAIN LIFE VEST IAW AMM 25-61-03.
- [SDR REXA2014040100345](https://openairdocs.org/sdr/REXA2014040100345.md): Elt · defective · Apr 1, 2014 · N8416B · Cndair CL6002B19 · Emergency Locator Beacon
  > ELT FAILS G SWITCH TEST DURING CL600-2B19 ELT 12 MONTH CHECK. REMOVED ELT 110-4 PN - 453-0150 SN - 70146 IAW DDG 25-62-01- IAW CRJ AMM 25-62-01. TRANSFERRED TO DEFERRAL LIST IAW MEL 25-62-01 CAT A. INSTALLED PLACARD & UPDATED MM02.
- [SDR REXA2014031500292](https://openairdocs.org/sdr/REXA2014031500292.md): Torque Link · disconnected · Mar 15, 2014 · N8416B · Cndair CL6002B19 · Nose/Tail Landing Gear Strut/Axle
  > GEAR DISAGREE WARNING MSG WHEN PUTTING THE GEAR IN THE UP POSITION. UPON LANDING WE HAD NO NOSE WHEEL STEERING. UPON INSPECTION TORQUE LINKS WERE DISCONNECTED. IAW AML 2319634, DISC NR 1 FOR NLG CHANGE.
- [SDR REXA2014031500291](https://openairdocs.org/sdr/REXA2014031500291.md): Unknown · malfunctioned · Mar 15, 2014 · N8416B · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > ON DEPARTURE 100KTS GOT HYD 3 LOW PRESS CAUTION, ONCE IN THE AIR THE GEAR WOULD NOT GO TO UP POSITION, AFTER ABOUT 2-3 MIN GEAR WENT UP. BEFORE COMPLETING QRH WE ALSO HAD GEAR DISAGREE & ANTI-SKID WARNING. QRH COMPLETED & RETURN TO A SAFE LANDING IN YW. DEF
- [SDR REXA2014031100287](https://openairdocs.org/sdr/REXA2014031100287.md): Torque Link · disconnected · Mar 11, 2014 · N8416B · Cndair CL6002B19 · Nose/Tail Landing Gear Strut/Axle
  > AIRCRAFT TOOK OFF & GOT A LG DISAGREE MESSAGE. MLG RETRACTED NORMAL, NLG DID NOT RETRACT. LANDED & CREW NOTED A NOSE WHEEL SHIMMY & GND CREW NOTED NLG TORQUE LINK WAS DISCONNECTED. NLG TIRES DISPLAYED EXCESSIVE WEAR BUT NOT BLOWN. OPERATIONS TOWED ACFT TO
- [SDR REXA2014022600240](https://openairdocs.org/sdr/REXA2014022600240.md): Control Valve · defective · Feb 26, 2014 · N8416B · Cndair CL6002B19 · Landing Gear Brake System
  > CREW REPORTS BRAKE PRESS BLEEDS DOWN FAST. R & R BRAKE CONTROL VLV IAW AMM 32-43-06, OPERATIONS CHECKED GOOD, ACFT OK FOR SERVICE.
- [SDR REXA2014020400177](https://openairdocs.org/sdr/REXA2014020400177.md): Sign · cracked · Feb 4, 2014 · N8416B · Cndair CL6002B19 · Emergency Lighting
  > GALLEY OVERHEAD EMERGENCY EXIT SIGN CRACKED. R & R GALLEY OVERHEAD EMERGENCY EXIT SIGN IAW AMM 33-51-14
- [SDR REXA2014013000151](https://openairdocs.org/sdr/REXA2014013000151.md): Life Vest · unserviceable · Jan 30, 2014 · N8416B · Cndair CL6002B19 · Life Jacket
  > CAPTAIN`S LIFE VEST BAG TORN. R & R CAPTAIN`S LIFE VEST IAW AMM 25-61-03.
- [SDR REXA2013072001380](https://openairdocs.org/sdr/REXA2013072001380.md): Selector Valve · failed · Jul 20, 2013 · N8416B · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > GEAR DISAGREE MASTER WARNING ON DEPARTURE. TOOK APPROX 1.5-2 MINUTES FOR GEAR TO COME UP. VIOLENT BANGING NOISE THROUGHOUT THIS PROCESS. SWUNG GEAR AND DUPLICATED PROBLEM. NOSE GEAR DOOR STAYED OPEN. PSEU CODES WERE S30 FAR, S31 FAR, S32 FAR. REPLACED NLG
- [SDR REXA2013060600696](https://openairdocs.org/sdr/REXA2013060600696.md): Link · twisted · Jun 5, 2013 · N8416B · Cndair CL6002B19 · Fuselage, Wing Attach Fittings
  > RIGHT, FS 513, WING TO FUSELAGE PICK UP LINK TWISTED WITH A GAP OF 0.003" ON INBD SIDE AND 0.020" GAP ON OTBD SIDE. LEFT, FS 513, WING TO FUSELAGE PICK UP LINK TWISTED WITH A GAP OF 0.003" ON INBD SIDE AND 0.016" GAP ON OTBD SIDE. REPAIRED IAW REO 601R-53-41
- [SDR REXA2013060500694](https://openairdocs.org/sdr/REXA2013060500694.md): Fitting · cracked · Jun 5, 2013 · N8416B · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS621 FORWARD FACE TOP OF LINTEL FITTING TOWARDS INBD CORNER IS CRACKED. REPAIRED IAW REO 601R-53-61-1230.
- [SDR REXA2013060500693](https://openairdocs.org/sdr/REXA2013060500693.md): Fitting · cracked · Jun 5, 2013 · N8416B · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > BATH TUB FITTING AT RBL9 FS461 CRACKED 1" AT FLANGE SECURING INTERCOSTAL FROM RBL9 TO RBL27. R & R IAW SRM 51-42-21.
- [SDR REXA2013060500692](https://openairdocs.org/sdr/REXA2013060500692.md): Fitting · cracked · Jun 5, 2013 · N8416B · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CLIP CRACKED AT FS484 LBL36. REPAIRED IAW REO 601R-53-41-059.
- [SDR REXA2013060500691](https://openairdocs.org/sdr/REXA2013060500691.md): Fitting · cracked · Jun 5, 2013 · N8416B · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CLIP CRACKED AT FS484, RBL36. REPAIRED IAW REO 601R-53-41-059.
- [SDR REXA2013060300690](https://openairdocs.org/sdr/REXA2013060300690.md): Frame · corroded · May 30, 2013 · N8416B · Cndair CL6002B19 · Fuselage Main, Frame
  > LOWER FS349 FRAME CORRODED IN AVIONICS BAY BETWEEN S-26L AND S-26R. REPAIRED IAW SRM 51-21-06.
- [SDR REXA2013052900676](https://openairdocs.org/sdr/REXA2013052900676.md): Frame · corroded · May 26, 2013 · N8416B · Cndair CL6002B19 · Fuselage Main, Frame
  > LOWE FS333, FRAME CORRODED BETWEEN S-26L AND S-26R. REPAIRED IAW SRM 51-21-06.
- [SDR REXA2013052900680](https://openairdocs.org/sdr/REXA2013052900680.md): Beam · chafed · May 25, 2013 · N8416B · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBD FLAP CENTER VANE ACTUATOR SLIDING BEAM IS CHAFED AND WORN 0.002" DEEP. REPAIRED IAW REO 601R-57-52-1979.
- [SDR REXA2013052900679](https://openairdocs.org/sdr/REXA2013052900679.md): Beam · chafed · May 25, 2013 · N8416B · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBD FLAP, INBD VANE ACTUATOR SLIDING BEAM IS CHAFED AND WORN 0.003" DEEP. REPAIRED IAW REO 601R-57-52-1979.
- [SDR REXA2013052900678](https://openairdocs.org/sdr/REXA2013052900678.md): Beam · chafed · May 25, 2013 · N8416B · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > VERTICAL BEAM AT BL0 ON FS621 BULKHEAD IS CHAFED 0.003" DEEP. REPAIRED IAW REO 601R-53-61-1523.
- [SDR REXA2013052900677](https://openairdocs.org/sdr/REXA2013052900677.md): Structure · damaged · May 25, 2013 · N8416B · Cndair CL6002B19 · Horizontal Stabilizer Miscellaneous Structure
  > TOOL MARK DAMAGE ON LOWER SIDE OF HORIZONTAL STABILIZER AT FWD OTBD CORNER OF CUTOUT FOR PANEL 342AB, FOUND TO BE 0.007" DEEP. BLENDED IAW SRM 55-11-31.
- [SDR REXA2013030700548](https://openairdocs.org/sdr/REXA2013030700548.md): Light · inoperative · Mar 7, 2013 · N8416B · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHT COVER CAME OFF AND LIGHT UNDERNEATH LOOKED DISCONNECTED. R & R FLOOR TRACK EMERGENCY LIGHT AT ROW 1 IAW AMM 33-51-01.
- [SDR REXA2013030300430](https://openairdocs.org/sdr/REXA2013030300430.md): Connector · dirty · Mar 3, 2013 · N8416B · Cndair CL6002B19 · Light System Wiring
  > FRONT SECTION OF EMERGENCY FLOOR LIGHTS TURN UP ORANGE INOPERABLE. REMOVED, CLEANED AND RESET CABIN FLOOR EMERGENCY LIGHT CONNECTION. OPS CHECK GOOD AMM 33-50-00. OK FOR SERVICE AT THIS TIME.
- [SDR REXA2013022300364](https://openairdocs.org/sdr/REXA2013022300364.md): Life Vest · unserviceable · Feb 23, 2013 · N8416B · Cndair CL6002B19 · Life Jacket
  > CAPTAIN LIFE VEST BAG TORN. REMOVED AND REPLACED VEST IAW AMM 25-61-03.
- [SDR REXA2013012300178](https://openairdocs.org/sdr/REXA2013012300178.md): Bpsu · failed · Jan 23, 2013 · N8416B · Cndair CL6002B19 · Trailing Edge Flap Control System
  > ON FLIGHT 4259 (DTW TO PWM) RECEIVED FLAPS FAIL MESSAGE DURING FLIGHT WITH THE FLAPS EXTENDED AT ZERO DEGREE, AIRSPEED 195 KTS, OAT -19*C, NO SKEW DETECTION LIGHTS. CREW DECLARED EMERGENCY LANDING. PERFORMED TROUBLESHOOTING PER BOMBARDIER FIM REV 44 IAW AD 2
- [SDR REXA2012120501729](https://openairdocs.org/sdr/REXA2012120501729.md): Medical Kit · unserviceable · Dec 3, 2012 · N8416B · Cndair CL6002B19 · Emergency Equipment
  > SEALS BROKEN ON EMK ON LAST FLIGHT. REMOVED AND REPLACED EMK IAW 25-61-00.
- [SDR REXA2012111101506](https://openairdocs.org/sdr/REXA2012111101506.md): Sill · corroded · Oct 21, 2012 · N8416B · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT FLOOR SILL BETWEEN FS 349 AND FS 364 FOUND CORRODED. CORROSION REMOVED AND FOUND TO BE WITHIN LIMITS OF SRM 53-00-00.
- [SDR REXA2012111101505](https://openairdocs.org/sdr/REXA2012111101505.md): Hand Rail · corroded · Oct 21, 2012 · N8416B · Cndair CL6002B19 · Passenger/Crew Doors
  > AFT PAX DOOR HANDRAIL RECEPTACLE HAS CORROSION. REMOVED CORROSION IAW SRM 53-00-00.
- [SDR REXA2012111101504](https://openairdocs.org/sdr/REXA2012111101504.md): Hand Rail · corroded · Oct 21, 2012 · N8416B · Cndair CL6002B19 · Passenger/Crew Doors
  > FORWARD PAX DOOR HANDRAIL RECEPTACLE HAS CORROSION. REMOVED CORROSION IAW SRM 53-00-00.
- [SDR REXA2012081901272](https://openairdocs.org/sdr/REXA2012081901272.md): Drain · leaking · Aug 19, 2012 · N8416B · Cndair CL6002B19 · Fuel Storage
  > FUEL LEAK FROM UNDER THE RIGHT WING NEAR FUEL DRAIN AND AT ROOT NEAR WHEEL. RESEATED FUEL DRAIN FOR RIGHT WING AS REQUIRED. ALL CHECKED GOOD. CLEANED RESIDUAL FUEL AS REQUIRED. NO LEAKS NOTED, REF CRJ 200 AMM CHAPTER 28-10-00.
- [SDR REXA2012080201217](https://openairdocs.org/sdr/REXA2012080201217.md): Container · torn · Aug 2, 2012 · N8416B · Cndair CL6002B19 · Life Jacket
  > OBSERVERS LIFE VEST BAG TORN. REMOVED AND REPLACED OBSERVERS LIFE VEST IAW AMM 25-61-03.
- [SDR REXA2012051300705](https://openairdocs.org/sdr/REXA2012051300705.md): Sign · broken · May 13, 2012 · N8416B · Cndair CL6002B19 · Emergency Lighting
  > SERVICE DOOR EMERGENCY EXIT SIGN FOUND BROKEN. REMOVED & REPLACED THE SERVICE DOOR EMERGENCY EXIT SIGN HOUSING ASSEMBLY IAW AMM 33-51-13. OPS CHECK GOOD. A/C OK FOR SERVICE.
- [SDR REXA2012030100296](https://openairdocs.org/sdr/REXA2012030100296.md): Controller · malfunctioned · Mar 1, 2012 · N8416B · Cndair CL6002B19 · Pitot/Static Anti-Ice System
  > AFTER TAKEOFF PASSING 200 AGL TAT PROBE HEAT, R AOA HEAT, R STATIC HEAT, R PITOT HEAT CAUTION MESSAGES. QRH COMPLETED AND NO REST. REMOVED AND REPLACED RIGHT AIR DATA SENSOR HEAT CONTROLLER (2A1HD) IAW AMM 30-31-15. OPC GOOD. OK FOR SERVICE.
- [SDR REXA201200129](https://openairdocs.org/sdr/REXA201200129.md): Unknown · malfunctioned · Jan 18, 2012 · N8416B · Cndair CL6002B19 · Fuel Indicating System
  > FLIGHT DIVERTED DUE TO AUTO XFLOW INHIB STATUS RIGHT TANK AND TOTAL FUEL GAUGES NOW INOP. PERFORMED OPS CHECK OF GRAVITY CROSSFLOW IAW AMM 28-13-16. FUEL QTY CHECKS GOOD IAW AMM 28-14-00. OK FOR SVC.
- [SDR REXA201200088](https://openairdocs.org/sdr/REXA201200088.md): Unknown · malfunctioned · Jan 3, 2012 · N8416B · Cndair CL6002B19 · Stabilizer Control System
  > UNCOMMANDED STAB TRIM MOVEMENT FROM 7.6 TO 9.4 ON TAXI OUT. NO CLACKER HEARD DURING UNCOMMANDED MOVEMENT. C/W GROUND MAINTENANCE TEST OF THE HSTCU IAW AMM 27-41-00. NO FAULTS NOTED. NO CHANNEL FAILURES WERE FOUND IN LRU FAULT HISTORY. SWITCHES ARE FREE OF
- [SDR REXA201100325](https://openairdocs.org/sdr/REXA201100325.md): Sill · corroded · May 25, 2011 · N8416B · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LT PRESSURE FLOOR SILL ASSY BETWEEN FS 409+128 AND FS 559 HAS AREAS OF CORROSION ON FLOOR SILL PANEL AND FLOOR SILL ANGLE. REPAIRED IAW BOMBARDIER REO 601R-53-41-666 REV A.
- [SDR REXA201100324](https://openairdocs.org/sdr/REXA201100324.md): Sill · corroded · May 25, 2011 · N8416B · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT PRESSURE FLOOR SILL ASSY BETWEEN FS 409+128 AND FS 559 HAS AREAS OF CORROSION ON FLOOR SILL PANEL AND FLOOR SILL ANGLE. REPAIRED IAW BOMBARDIER REO 601R-53-41-666 REV A.
- [SDR REXA201100323](https://openairdocs.org/sdr/REXA201100323.md): Skin · corroded · May 23, 2011 · N8416B · Cndair CL6002B19 · Wing, Plate/Skin
  > LT LOWER WING PLANK FUEL PANEL CUTOUT FOR 550FB HOLE 14 AT WS 274.319 HAS MINOR FRETTING CORROSION ON THE OUTBOARD END NON-CRITICAL REGION APPROX 1" LONG X 0.030" WIDE X 0.003" DEEP. REPAIRED IAW BOMBARDIER REO 601R-57-21-030 REV H.
- [SDR REXA201100322](https://openairdocs.org/sdr/REXA201100322.md): Skin · corroded · May 23, 2011 · N8416B · Cndair CL6002B19 · Wing, Plate/Skin
  > LT LOWER WING PLANK FUEL PANEL CUTOUT FOR 550BB HOLE 10 AT WS 188.040 HAS MINOR FRETTING CORROSION IN THE NON-CRITICAL REGION OUTBAORD END APPROX 6" LONG X 0.25" WIDE X 0.005" DEEP. REPAIRED IAW BOMBARDIER REO 601R-57-21-030 REV H.
- [SDR REXA201100321](https://openairdocs.org/sdr/REXA201100321.md): Skin · corroded · May 23, 2011 · N8416B · Cndair CL6002B19 · Wing, Plate/Skin
  > LT LOWER WING PLANK FUEL PANEL CUTOUT FOR 550AB (HOLE 4) AT WS 163.00 HAS MINOR FRETTING CORROSION ON THE OUTBOARD END IN THE NON-CRITICAL REGION APPROX 1" LONG X 0.25" WIDE X 0.002" DEEP. REPAIRED IAW BOMBARDIER REO 601R-57-21-030 REV H.
- [SDR REXA201100320](https://openairdocs.org/sdr/REXA201100320.md): Skin · corroded · May 23, 2011 · N8416B · Cndair CL6002B19 · Wing, Plate/Skin
  > LT LOWER WING PLANK FUEL PANEL CUTOUT FOR 540FB (HOLE 8) WS 136.676 HAS MINOR FRETTING CORROSION ON OUTBOARD END IN NON-CRITICAL REGION APPROXIMATELY 1" LONG X 0.25" WIDE X 0.002" DEEP. REPAIRED IAW BOMBARDIER REO 601R-57-21-030 REV H.
- [SDR REXA201100310](https://openairdocs.org/sdr/REXA201100310.md): Skin · corroded · May 23, 2011 · N8416B · Cndair CL6002B19 · Wing, Plate/Skin
  > LT LOWER WING PLANK FUEL PANEL CUTOUT FOR PANEL 550CB HOLE 11 AT WS 209.040 HAS MINOR CORROSION IN THE CRITICAL AND NON-CRITICAL REGIONS. MEASURES 2" X.25" X 0.003". REPAIRED IAW BOMBARDIER REO 601R-57-21-030 REV H.
- [SDR REXA201100309](https://openairdocs.org/sdr/REXA201100309.md): Skin · corroded · May 23, 2011 · N8416B · Cndair CL6002B19 · Wing, Plate/Skin
  > LT LOWER WING PLANK FUEL PANEL CUTOUT FOR 550EB HOLE 13 AT WS 253.022 HAS MINOR FRETTING CORROSION IN THE CRITICAL AND NON-CRITICAL REGIONS. REPAIRED IAW BOMBARDIER REO 601R-57-21-030 REV H.
- [SDR REXA201100308](https://openairdocs.org/sdr/REXA201100308.md): Skin · corroded · May 23, 2011 · N8416B · Cndair CL6002B19 · Wing, Plate/Skin
  > LT LOWER WING PLANK FUEL PANEL CUTOUT 540DB (HOLE NR 6) AT WS 95.950 HAS MINOR FRETTING CORROSION ON OUTBOARD END IN NON-CRITICAL REGION APPROX 1" LONG X.25" WIDE X 0.003". REPAIRED IAW BOMBARDIER REO 601R-57-21-030 REV H.
- [SDR REXA201100307](https://openairdocs.org/sdr/REXA201100307.md): Skin · corroded · May 23, 2011 · N8416B · Cndair CL6002B19 · Wing, Plate/Skin
  > LT LOWER WING PLANK FUEL CUTOUT FOR 540BB HOLE NR 1 AT WS 54.897 HAS MINOR FRETTING CORROSION ON I/B AND O/B ENDS IN NON-CRITICAL REGION APPROX 2" LONG X.25" WIDE X 0.003" DEEP. REPAIRED IAW BOMBARDIER REO 601R-57-21-030 REV H.
- [SDR REXA201100306](https://openairdocs.org/sdr/REXA201100306.md): Rib · damaged · May 23, 2011 · N8416B · Cndair CL6002B19 · Nacelle/Pylon, Frame/Spar/Rib
  > FRETTING DAMAGE ON RT RISER OF ENGINE PYLON OUTBOARD RIB. REPAIRED IAW BOMBARDIER REO'S 601R-54-50-036 AND 601R-71-22-026.
- [SDR REXA201100305](https://openairdocs.org/sdr/REXA201100305.md): Floorbeam · corroded · May 23, 2011 · N8416B · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > RBL 27 FLOORBEAM CAP HAS CORROSION AROUND NUT PLATE HOLES BETWEEN FS 621 AND FS 574. REPAIRED IAW SRM 51-21-06 AND 53-00-43 STEPS 5A(1) THROUGH 5A(12) ALUMINUM FLOORBEAM FLANGE REPAIR.
- [SDR REXA201100304](https://openairdocs.org/sdr/REXA201100304.md): Web · cracked · May 23, 2011 · N8416B · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 280 WEB CRACKED 2 INCHES OUTBOARD OF RBL 9. REPAIRED IAW BOMBARDIER REO 601R-53-11-926 REV B AND BOMBARDIER SERVICES CORPORATION STANDARD REPAIR 601R-53-0107.

Next page: https://openairdocs.org/aircraft/N8416B/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 = 'N8416B' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8416B/reports

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