# Service difficulty reports: N8869B

A list on [N8869B](https://openairdocs.org/aircraft/N8869B.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 3 · 125 reports

- [SDR REXA2022081101833](https://openairdocs.org/sdr/REXA2022081101833.md): Splice · cracked · Aug 6, 2022 · N8869B · Cndair CL6002B19 · Flight Compartment Windows
  > WINDSHIELD CENTER POST AT FS 202.75 THE LH SPLICE FITTING IS CRACKED REMOVED AND REPLACED LH SPLICE FITTING FOR WINDSHIELD CENTER POST IAW SRM 51-77-00
- [SDR REXA2022081101832](https://openairdocs.org/sdr/REXA2022081101832.md): Splice Angle · cracked · Aug 6, 2022 · N8869B · Cndair CL6002B19 · Flight Compartment Windows
  > WINDSHIELD CENTER POST AT FS 202.75 THE RH SPLICE FITTING IS CRACKED REMOVED AND REPLACED RH SPLICE FITTING FOR WINDSHIELD CENTER POST IAW SRM 51-77-00
- [SDR REXA2022071401592](https://openairdocs.org/sdr/REXA2022071401592.md): Inverter · inoperative · Jul 9, 2022 · N8869B · Cndair CL6002B19 · Emergency Lighting
  > ROWS 2-5 FLOOR TRACK EMERGENCY LIGHTING INOP. REMOVED & REPLACED INVERTER #2 IAW CRJ 200 AMM 33-51-07. P/N ON/OFF: 5925-7. OPS CHECK GOOD.
- [SDR REXA2022070101438](https://openairdocs.org/sdr/REXA2022070101438.md): Charger · inoperative · Jun 24, 2022 · N8869B · Cndair CL6002B19 · Emergency Lighting
  > LEFT OVERWING EXIT EMERGENCY EXIT LIGHT IS NOT ILLUMINATING. (LOWER GREEN SIGN) REPLACED CHARGER BA5-0933-901 STATION 450L IAW MM 33-51-05-04 AND TEST IAW MM 33-51-04 CHECKS GOOD MC NOTIFIED 96575
- [SDR REXA2021100700858](https://openairdocs.org/sdr/REXA2021100700858.md): Battery · inoperative · Oct 7, 2021 · N8869B · Cndair CL6002B19 · Emergency Lighting
  > "MULTIPLE EMER. LIGHTS INOP. "REPLACED BATTERY PACK (PS1LF) IAW CRJ 200 AMM 33-51-04. OPS CHECK GOOD. P/N ON/OFF 2013-1ASMI S/N ON 13502 S/N OFF 11614. "
- [SDR REXA2019061860910](https://openairdocs.org/sdr/REXA2019061860910.md): Light · detached · Jun 16, 2019 · N8869B · Cndair CL6002B19 · Emergency Lighting
  > EMER LIGHTING STRIP IN CABIN IS PULLED UP. R&R'D EMER. LIGHTING STRIP @ 7A IAW AMM 33-51-01. OPC GOOD. OK FOR SVC
- [SDR REXA201904085418](https://openairdocs.org/sdr/REXA201904085418.md): Light · inoperative · Apr 5, 2019 · N8869B · Cndair CL6002B19 · Emergency Lighting
  > INTERIOR EMERGENCY EXIT LIGHT AT 8 A NOT ILLUMINATING. REPLACED EMERGENCY LIGHT AT SEAT 8 A OPS CHECK GOOD IAW AMM 33-51-10, OPS CHECKED GOOD
- [SDR REXA2019030500253](https://openairdocs.org/sdr/REXA2019030500253.md): Lens · damaged · Mar 5, 2019 · N8869B · Cndair CL6002B19 · Emergency Lighting
  > EMER LIGHT STRIP UNATTACHED BY 12C. FOUND DAMAGE TO EMERGENCY LIGHTS LENS BASE AND LIGHT BASE ASSY. REMOVED AND REPLACED LENS, BASE AND LIGHT BASE ASSY IN THE AFT SECTION IAW AMM 33-51-01. OPS CHECK GOOD. LIGHT STRIP AT 12C IS SECURE.
- [SDR REXA2019012100056](https://openairdocs.org/sdr/REXA2019012100056.md): Floorbeam · corroded · Jan 21, 2019 · N8869B · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOORBEAM FS559+112- FS 589 IS CORRODED LBL27. REPAIRED FLOORBEAM AT LBL27 FS559+112 TO FS589 IAW REO 601R-53-61-6839.
- [SDR REXA2019011900054](https://openairdocs.org/sdr/REXA2019011900054.md): Fitting · corroded · Jan 19, 2019 · N8869B · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR FITTING LBL 27 FS 605-621 IS CORRODED ON PANEL LANDING. REPAIRED FLOOR FITTING AT LBL27 IAW EA 253-08237 REV IR.
- [SDR REXA2019011700061](https://openairdocs.org/sdr/REXA2019011700061.md): Floorbeam · corroded · Jan 17, 2019 · N8869B · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOORBEAM LBL 27 O/B AND I/B FLOOR LANDINGS HAS CORROSION SPOTS BETWEEN FS 559+112 THRU FS 621, IN THE CARGO BAY BELOW THE FLOOR. REMOVED FLOORBEAM CAP AND INSTALLED NEW FLOORBEAM CAP IAW SRM 51-24-36, 51-42-21 AND 51-42-22 FS559+118 TO FS609. CORROSION FS559+
- [SDR REXA2019011700055](https://openairdocs.org/sdr/REXA2019011700055.md): Drag Angle · cracked · Jan 17, 2019 · N8869B · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR AFT STEP RISER DRAG ANGLE CRACKED. REPAIRED CRACKED DRAG ANGLE IAW REO 601R-52-11-513 REV B DATED 07/05/2015 REPAIR TYPE I.
- [SDR REXA2019011300058](https://openairdocs.org/sdr/REXA2019011300058.md): Fitting · cracked · Jan 13, 2019 · N8869B · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > ANGLE CLIP IS CRACKED ON THE O/B SIDE OF LBL 27 AT FS 484, IN THE CABIN BELOW THE FLOOR. REMOVED/REPLACED ANGLE CLIP O/B SIDE LBL27@ FS484 IAW SRM 51-42-21.
- [SDR REXA2019011300057](https://openairdocs.org/sdr/REXA2019011300057.md): Fitting · cracked · Jan 13, 2019 · N8869B · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > ANGLE CLIP IS CRACKED ON THE I/B SIDE OF RBL 36 AT FS 484, IN THE CABIN BELOW THE FLOOR. REMOVED/REPLACED ANGLE CLIP I/B SIDE RBL36 @ FS484 IAW REO 601R-53-41- AND SRM 51-42-21.
- [SDR REXA2019011100065](https://openairdocs.org/sdr/REXA2019011100065.md): Skin Panel · cracked · Jan 11, 2019 · N8869B · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > SKIN PANEL ABOVE NOSE HYDRAULIC COMPARTMENT CRACKED AT DOOR LATCH. REPAIRED SKIN PNL ABOVE NOSE HYDRAULIC COMPARTMENT @ DOOR LATCH IAW EA 253-08205.
- [SDR REXA2019010900064](https://openairdocs.org/sdr/REXA2019010900064.md): Fitting · cracked · Jan 9, 2019 · N8869B · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > WHILE DOING BUY BACK ON THE 280 FWD FLOOR STRUCTURE NOTICED THAT THE I/B ANGLE CLIP IS CRACKED AT THE I/B SIDE OF LBL 9 AND AFT SIDE OF BEAM 280, IN THE CABIN BELOW THE FLOOR. REMOVED CRACKED ANGLE AT FS280 ON I/B SIDE OF LBL 9 LONGITUDIUAL BEAM FABRICATED/INS
- [SDR REXA2019010900063](https://openairdocs.org/sdr/REXA2019010900063.md): Access Panel · cracked · Jan 9, 2019 · N8869B · Cndair CL6002B19 · APU Cowling/Containment
  > APU ENCLOSURE CRACKED ON AFT SURFACE OF ACCESS PANEL FLANGE, NEAR PREVIOUS REPAIR. (AFT OF EXHAUST). REMOVED CRACKED AREA APU INSTALLED NEW FABRICATED BRACKETS IAW REO 601R-49-11-071.
- [SDR REXA2019010800062](https://openairdocs.org/sdr/REXA2019010800062.md): Support Bracket · cracked · Jan 8, 2019 · N8869B · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT MLG WW HYD SYS 3B PRESSURE TRANSDUCER SUPPORT BRACKET CRACKED. REMOVED AND REPLACED RT WHEEL WELL HYDRAULIC SYSTEM 3B PRESSURE TRANSDUCER SUPPORT BRACKET IAW SRM 51-42-06 AND SRM 51-41-02.889241.
- [SDR REXA2019010500066](https://openairdocs.org/sdr/REXA2019010500066.md): Bulkhead · cracked · Jan 5, 2019 · N8869B · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD IS CRACKED AT BL0 APPROX WL112. DOT 262A001 REPAIRED AFT PRESSURE BULKHEAD AT BL0, APPROXIMATELY WL112 IAW REO 601R-53-61-1285.
- [SDR REXA2018120101176](https://openairdocs.org/sdr/REXA2018120101176.md): Light · inoperative · Dec 1, 2018 · N8869B · Cndair CL6002B19 · Emergency Lighting
  > NR 3 CEILING EMERGENCY FLOOD LIGHT INOP. R&R NR 3 CEILING EMERGENCY FLOOD LIGHT BULB IAW AMM 33-51-16. OPS CK'S GOOD. OK FOR SERVICE.
- [SDR REXA2018072400642](https://openairdocs.org/sdr/REXA2018072400642.md): Flashlight · inoperative · Jul 20, 2018 · N8869B · Cndair CL6002B19 · Emergency Equipment
  > RED LIGHT NOT BLINKING ON FLIGHT ATTENDANT FLASHLIGHT. REMOVED AND REPLACED F/A FLASHLIGHT IN WARDROBE, OPS CK GOOD, REF AMM 25-61-02.
- [SDR REXA2018020800107](https://openairdocs.org/sdr/REXA2018020800107.md): Wire Harness · damaged · Feb 8, 2018 · N8869B · Cndair CL6002B19 · Landing Gear System Wiring
  > GEAR DISAGREE AFTER TAKEOFF. WHEN HANDLE SELECTED UP, MAIN WHEELS RETRACTED, NOSE WHEEL REMAINED DOWN AND LOCKED. RAN QRH, PULLED MANUAL GEAR EXTENTION AND MAIN LANDING GEAR BECAME DOWN AND LOCKED AS WELL. RETURNED TO DEPARTURE. STEERING WAS AVAILABLE ON LAND
- [SDR REXA2017101701102](https://openairdocs.org/sdr/REXA2017101701102.md): Oxygen Mask · leaking · Oct 17, 2017 · N8869B · Cndair CL6002B19 · Portable Oxygen System
  > THE LPM MASK, FLOW INDICATOR LEAKS. REMOVED AND REPLACED PORTABLE OXYGEN BOTTLE MASK IAW AMM 35-31-01. CHECKED GOOD.
- [SDR REXA2017092401026](https://openairdocs.org/sdr/REXA2017092401026.md): Bpsu · faulted · Sep 24, 2017 · N8869B · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAIL CAUTION MESSAGE WHILE CLIMBING THROUGH FL180 AT 290 KIAS. PERFORMED TROUBLESHOOTING IAW FIM 27-50-00, REV 53, IAW AD 2009-06-12, PARAGRAPH (H) (6) (I). REPLACED THE LEFT BPSU IAW AMM 27-51-10. OPS AND FUNCTIONAL CHECKED GOOD.
- [SDR REXA2017083100957](https://openairdocs.org/sdr/REXA2017083100957.md): Light · inoperative · Aug 31, 2017 · N8869B · Cndair CL6002B19 · Emergency Lighting
  > FLOOR EMERGENCY LIGHT INOPERATIVE FROM SEATS 1C - 5C, ALL OTHER EMERGENCY LIGHTS BOTH INTERNAL AND EXTERNAL WORK. INSPECTED EMERGENCY LIGHT STRIP IAW AMM 33-51-01. CLEANED CONNECTORS, GREEN LIGHTS ILLUMINATED. UNABLE TO GET MOST FWD SECTION OF AMBER LIGHTS
- [SDR REXA2017061300710](https://openairdocs.org/sdr/REXA2017061300710.md): Selector Valve · inoperative · Jun 13, 2017 · N8869B · Cndair CL6002B19 · Nose/Tail Landing Gear Strut/Axle
  > NOSE GEAR DISAGREE ON LANDING MESSAGE, PROCEEDED WITH A GO AROUND RAN QRH PROBLEM APPEAR TO BE FIXED ON THE SECOND APPROACH MESSAGE PERSISTED. FOLLOWED WITH A GO AROUND COMPLETED QRH AND FOLLOWED WITH FLY BY FOLLOWED TO A LANDING. PURGED NOSE SHOCK STRUT OF O
- [SDR REXA2017031100345](https://openairdocs.org/sdr/REXA2017031100345.md): Light · inoperative · Mar 11, 2017 · N8869B · Cndair CL6002B19 · Emergency Lighting
  > FWD EMERGENCY FLOOD LIGHT INOPERATIVE. R & R THE FLOOD LIGHT IAW AMM 33-51-16. OPS CHECKED GOOD. OK FOR SERVICE.
- [SDR REXA2016121902489](https://openairdocs.org/sdr/REXA2016121902489.md): Stringer · corroded · Dec 19, 2016 · N8869B · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > STRINGER 27 HAS SEVERAL CORROSION SPOTS BETWEEN FRAMES 349 - 333, IN THE FWD E & E BAY. REPAIRED THE STRINGER IAW EA CRJ253-05149.
- [SDR REXA2016121702486](https://openairdocs.org/sdr/REXA2016121702486.md): Door Frame · corroded · Dec 17, 2016 · N8869B · Cndair CL6002B19 · Fuselage Main, Structure
  > PAX DOOR FWD FRAME CORRODED INSIDE INSPECTION ACCESS PANEL 832HL EXTENDING UPWARD UNDER INNER HANDLE ASSY IN ACCESS PANEL 832GL. REMOVED AND REPLACED PAX DOOR FWD FRAME IAW SRM 51-42-06 AND SRM 51-42-21 AND 51-42-10.
- [SDR REXA2016121702487](https://openairdocs.org/sdr/REXA2016121702487.md): Fairing · chafed · Dec 17, 2016 · N8869B · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT STUB FAIRING OTBD SKIN IS CHAFED AT SEVERAL SPOTS. REPAIRED STUB FAIRING O/B SKIN IAW EA CRJ253-05135.
- [SDR REXA2016121402484](https://openairdocs.org/sdr/REXA2016121402484.md): Trunnion · gouged · Dec 14, 2016 · N8869B · Cndair CL6002B19 · Fuselage, Landing Gear Attach Fittings
  > RIGHT AFT MLG TRUNNION BORE GOUGED AT 12;00 POSITION. REPAIRED IAW REO 601R-57-21-003.
- [SDR REXA2016121402485](https://openairdocs.org/sdr/REXA2016121402485.md): Channel · cracked · Dec 14, 2016 · N8869B · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CARGO DOOR FORWARD TRACK LOWER CHANNEL CRACKED IN TWO LOCATIONS. REMOVED & REPLACED THE CHANNEL IAW SRM 51-42-06.
- [SDR REXA2016121302446](https://openairdocs.org/sdr/REXA2016121302446.md): Vane · chafed · Dec 13, 2016 · N8869B · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT WING INBD FLAP VANE LE IS CHAFED IN MULTIPLE AREAS. REMOVED & REPLACED THE RIGHT WING I/B FLAP VANE L/E SKIN IAW SRM 51-42-13. REMOVED DAMAGE IN THREE AREAS THE MID AN OTBD AREAS STAYED IN LIMITS INBD AREA OUT OF LIMITS IAW REO 601R-57-52-004.
- [SDR REXA2016121302482](https://openairdocs.org/sdr/REXA2016121302482.md): Panel · cracked · Dec 13, 2016 · N8869B · Cndair CL6002B19 · Elevator, Plate/Skin
  > TAIL PANEL 334AB IS GOUGED AND CRACKED. LOCATED AND DRILLED NEW PANEL IAW SRM 51-40-11.
- [SDR REXA2016121302483](https://openairdocs.org/sdr/REXA2016121302483.md): Bracket · cracked · Dec 13, 2016 · N8869B · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > RIGHT ACM DIS VALVE MOUNT BRACKET CRACKED. REMOVED AND REPLACED MOUNT BRACKET IAW SRM 51-42-06.
- [SDR REXA2016121102437](https://openairdocs.org/sdr/REXA2016121102437.md): Channel · cracked · Dec 11, 2016 · N8869B · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CHANNEL AT BS 625 AND STRINGR 14L IS CRACKED. REMOVED AND REPLACED THE CHANNEL IAW SRM 51-42-06 AND SRM 51-42-21.
- [SDR REXA2016121102438](https://openairdocs.org/sdr/REXA2016121102438.md): Stringer · cracked · Dec 11, 2016 · N8869B · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > STRINGER 3L CRACKED AT BS 379 AFT END OF PAX DOOR LINTEL. REPAIRED THE STRINGER IAW SRM 53-00-03.
- [SDR REXA2016121102443](https://openairdocs.org/sdr/REXA2016121102443.md): Stringer · cracked · Dec 11, 2016 · N8869B · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > STRINGER 3L CRACKED AT BS 379 AFT END OF PAX DOOR LINTEL. REPAIRED THE STRINGER IAW SRM 53-00-03.
- [SDR REXA2016121102444](https://openairdocs.org/sdr/REXA2016121102444.md): Channel · cracked · Dec 11, 2016 · N8869B · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > CHANNEL AT BS 625 AND STRINGER 15L IS CRACKED. REMOVED AND REPLACED THE CHANNEL5 IAW SRM 51-42-06 AND SRM 51-42-21.
- [SDR REXA2016121102445](https://openairdocs.org/sdr/REXA2016121102445.md): Rub Strip · chafed · Dec 11, 2016 · N8869B · Cndair CL6002B19 · Nacelle/Pylon, Main Frame
  > LEFT ENGINE COWL PANEL 432AB TRAILING EDGE RUB STRIP IS CHAFED. REMOVED AND REPLACED THE RUB STRIP IAW IAW CMM 71-14-01.
- [SDR REXA2016121002434](https://openairdocs.org/sdr/REXA2016121002434.md): Angle · cracked · Dec 10, 2016 · N8869B · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > OBLIQUE ANGLE AT BS 625 AND STRINGER 14R IS CRACKED. REMOVED & REPLACED THE ANGLE IAW SRM 51-42-06.
- [SDR REXA2016121002435](https://openairdocs.org/sdr/REXA2016121002435.md): Support Bracket · cracked · Dec 10, 2016 · N8869B · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT OVERWING PANEL SUPPORT BRACKET IS CRACKED AT BS 449.85. REMOVED AND REPLACED SUPPORT BRACKET IAW SRM 51-42-06.
- [SDR REXA2016121002436](https://openairdocs.org/sdr/REXA2016121002436.md): Bracket · cracked · Dec 10, 2016 · N8869B · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT OVERWING PANEL SUPPORT BRACKET AT BS 449.85 IS CRACKED. REMOVED AND REPLACED THE SUPPORT BRACKET IAW SRM 51-42-06.
- [SDR REXA2016120902433](https://openairdocs.org/sdr/REXA2016120902433.md): Angle · cracked · Dec 9, 2016 · N8869B · Cndair CL6002B19 · Fuselage Main, Frame
  > FLT DECK LT SIDE FRAME AT BS 220 APPROX WL 100 CRACKED AT CUTOUT. REMOVED AND REPLACED FRAME IAW SRM 51-42-06.
- [SDR REXA2016120902439](https://openairdocs.org/sdr/REXA2016120902439.md): Rub Strip · cracked · Dec 9, 2016 · N8869B · Cndair CL6002B19 · Nacelle/Pylon, Main Frame
  > RIGHT ENGINE COWL PANEL 442AT TRAILING EDGE RUB STRIP IS KNIFED EDGES AND CRACKED. REMOVED AND REPLACED RUB STRIP IAW CMM 71-14-01.
- [SDR REXA2016120802554](https://openairdocs.org/sdr/REXA2016120802554.md): Bracket · cracked · Dec 8, 2016 · N8869B · Cndair CL6002B19 · Wing Miscellaneous Structure
  > RT WING PRESSURE REFUEL BRACKET IS CRACKED ON OTBD LWR END. REMOVED & REPLACED REFUEL BRACKET IAW SRM 51-42-06, & SRM 51-41-02.
- [SDR REXA2016120802429](https://openairdocs.org/sdr/REXA2016120802429.md): Seat Track · corroded · Dec 8, 2016 · N8869B · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT NR 7 SEAT TRACK HAS CORROSION FROM BS 551 - 559+10. REMOVED AND REPLACED THE SEAT TRACK IAW AMM-53-01-11, AND SRM 53-21-49.
- [SDR REXA2016120802430](https://openairdocs.org/sdr/REXA2016120802430.md): Seat Track · corroded · Dec 8, 2016 · N8869B · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT NR 3 SEAT TRACK SECTION HAS CORROSION FROM BS 409+68 - 409+104. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11, AND SRM 53-21-49.
- [SDR REXA2016120802431](https://openairdocs.org/sdr/REXA2016120802431.md): Seat Track · corroded · Dec 8, 2016 · N8869B · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT NR 4 SEAT TRACK SECTION HAS CORROSION FROM BS 409+112 - 498 AT MULTIPLE LOCATIONS. REMOVED AND REPLACED THE SEAT TRACK IAW AMM-53-01-11 AND SRM CRJ-200 53-21-49.
- [SDR REXA2016120802432](https://openairdocs.org/sdr/REXA2016120802432.md): Seat Track · corroded · Dec 8, 2016 · N8869B · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT NR 3 SEAT TRACK SECTION HAS CORROSION BETWEEN BS 409+8 AND 409+100 AT MULTIPLE LOCATIONS. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11, AND SRM 53-21-49.

Next page: https://openairdocs.org/aircraft/N8869B/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 = 'N8869B' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8869B/reports

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