# Service difficulty reports: N8894A

A list on [N8894A](https://openairdocs.org/aircraft/N8894A.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 · 112 reports

- [SDR REXA2022060200974](https://openairdocs.org/sdr/REXA2022060200974.md): Plug · inoperative · May 17, 2022 · N8894A · Cndair CL6002B19 · Emergency Lighting
  > FLOOD EMERGENCY LIGHTS NEAR PAX DOOR INOP FOUND BROKEN WIRE AT CONNECTOR TO FLOOR LEVEL, AT PAX DOOR, FLOOD LIGHT. PINNED WIRE WITH CONNECTOR PLUG KIT PN OFF AND ON: 48-7190. OPS CK GOOD IAW ESPM 20-16-00 AND AMM 33-51-19
- [SDR REXA2022050600830](https://openairdocs.org/sdr/REXA2022050600830.md): Lamp · inoperative · May 2, 2022 · N8894A · Cndair CL6002B19 · Emergency Lighting
  > THE EMERGENCY EXIT SIGN ON THE LEFT WALL AS SOON AS YOU ENTER THE MAIN CABIN DOOR HAS NUMEROUS BULBS BURNED OUT. RE-LAMPED EMERG EXIT SIGN IAW AMM 33-51-10.OPS TEST GOOD.
- [SDR REXA2021012100039](https://openairdocs.org/sdr/REXA2021012100039.md): Light · inoperative · Jan 14, 2021 · N8894A · Cndair CL6002B19 · Emergency Lighting
  > RT FWD CENTER EMERGENCY LIGHT OUT. REMOVED AND INSTALLED RT FWD CENTER EMERGENCY LIGHT, IAW CRJ 200 AMM 33-51-01. OPERATIONS CHECK EMERGENCY LIGHT. OPERATIONS CHECK GOOD. P/N ON/OFF: 1317
- [SDR REXA2020072000600](https://openairdocs.org/sdr/REXA2020072000600.md): Battery Pack · inoperative · Jul 15, 2020 · N8894A · Cndair CL6002B19 · Emergency Lighting
  > CREW REPORTED ALL EMERGENCY LIGHTS INOPERATIVE. R & R 4 EMERGENCY LIGHT BATTERY PACKS IAW AMM 33-51-04. OPS CHECKED GOOD.
- [SDR REXA2019051200697](https://openairdocs.org/sdr/REXA2019051200697.md): Light · inoperative · May 12, 2019 · N8894A · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY FLOOR LIGHT STRIP NOT LIGHTING. REMOVED AND REPLACED 8CD EMERGENCY FLOOR TRACK LIGHT STRIP IAW AMM 33-51-01. OPS CHECK GOOD.
- [SDR REXA2019042270491](https://openairdocs.org/sdr/REXA2019042270491.md): Bulkhead Web · cracked · Apr 17, 2019 · N8894A · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD CRACK AT CARGO DOOR TRACK LBL 27.5, AND DENT NEXT TO REPAIR AREA LBL 18.0 - W.L 121.9 - 137.5. REPAIRED AFT BULKHEAD IAW REO 601R-53-61-6927 OPS CK GOOD OF CARGO DOOR WARNING SYS IAW AMM 52-70-02-710-801. OPS CK GOOD OF CARGO DOOR IAW A
- [SDR REXA2019042250490](https://openairdocs.org/sdr/REXA2019042250490.md): Retainer · cracked · Apr 15, 2019 · N8894A · Cndair CL6002B19 · Nacelle/Pylon, Main Frame
  > DURING SEAL REPLACEMENT ON PANEL 412AB, FOUND RETAINER TO BE CRACKED AND BROKEN. REMOVED OLD SEAL RETAINER/REPLACED WITH NEW SEAL ON PNL 412AB IAW 51-42-06.
- [SDR REXA2019042211488](https://openairdocs.org/sdr/REXA2019042211488.md): Attach Bracket · cracked · Apr 11, 2019 · N8894A · Cndair CL6002B19 · Flight Compartment Windows
  > WINDSHIELD CTR POST LWR RH MACHINED ATTACH BRACKET CRACKED. REMOVED/REPLACED WINDSHIELD POST LWR RH ATTACH BRACKET IAW CRJ 200 SRM 51-42-21 AAR SM 33
- [SDR REXA2019042210487](https://openairdocs.org/sdr/REXA2019042210487.md): Drag Angle · cracked · Apr 10, 2019 · N8894A · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR AFT DRAG ANGLE IS CRACKED. REMOVED UNSERVICEABLE DRAG ANGLE/REPLACED WITH NEW SERVICEABLE DRAG ANGLE IAW BOMBA REO 601R-52-11-513 REV B AAR SM 107
- [SDR REXA2019042210486](https://openairdocs.org/sdr/REXA2019042210486.md): Handle · cracked · Apr 10, 2019 · N8894A · Cndair CL6002B19 · Electrical/Electronic Compartment Doors
  > AVIONICS DOOR HANDLE HOUSING IS CRACKED AT BASE. REMOVED/REPLACED AVIONICS DOOR HANDLE HOUSING IAW CRJ 200 SRM 51-42-21 OPS CK GOOD IAW AMM 52-70-08-710-801.
- [SDR REXA2019042210485](https://openairdocs.org/sdr/REXA2019042210485.md): Seat Track · corroded · Apr 10, 2019 · N8894A · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LH FLOOR SEAT RAIL LBL9 STICK 4 HAS CORROSION. REMOVED CORROSION ON LBL9 FLOOR SEAT TRACK STICK #4 FOUND TO BE OUT OF LIMITS. REMOVED CORRODED SEAT TRACK/INSTALLED NEW FLOOR SEAT TRACK IAW SRM 51-21-06, 53-41-49, EA DWG S6487 REV A, AMM 53-01-11.
- [SDR REXA2019042210484](https://openairdocs.org/sdr/REXA2019042210484.md): Seat Track · corroded · Apr 10, 2019 · N8894A · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LH FLOOR SEAT RAIL LBL9 STICK 3 HAS CORROSION. REMOVED CORROSION ON LBL9 FLOOR SEAT TRACK #3 FOUND TO BE OUT OF LIMITS. INSTALLED NEW LBL9 STICK #3 FLOOR SEAT TRACK IAW SRM 51-21-06, 53-41-49, EA DWG S6487 REV A, AMM 53-01-11.
- [SDR REXA2019042210483](https://openairdocs.org/sdr/REXA2019042210483.md): Seat Track · corroded · Apr 10, 2019 · N8894A · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RH FLOOR SEAT RAIL RBL9 STICK 3 HAS CORROSION. EVALUATED CORROSION ON RBL9 FLOOR SEAT TRACK STICK #3 AND FOUND TO BE OUT OF LIMITS REMOVED CORRODED SEAT TRACK AND INSTALLED NEW FLOOR SEAT TRACK IAW CRJ 200 SRM 53-41-49, EA DWG S6487 REV A, CRJ 200 AMM 53-01-1
- [SDR REXA2019042210482](https://openairdocs.org/sdr/REXA2019042210482.md): Seat Track · corroded · Apr 10, 2019 · N8894A · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RH FLOOR SEAT RAIL RBL9 STICK 2 HAS CORROSION. REMOVED/REPLACED SEAT RAIL IAW AMM 53-01-11.
- [SDR REXA2019042210481](https://openairdocs.org/sdr/REXA2019042210481.md): Fitting · worn · Apr 10, 2019 · N8894A · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR CUTOUT, AFT PULL IN CAM IS WORN. FOUND PAX DOOR OPENING AFT PULL IN CAM WORN BEYOND SERVICEABLE LIMITS AND INSTALLED NEW CAM IAW SRM 51-42-21 OPS CKS PERFORMED IAW AMM 33-22-00-710-801 CK GOOD.
- [SDR REXA201904229480](https://openairdocs.org/sdr/REXA201904229480.md): Attach Angle · cracked · Apr 9, 2019 · N8894A · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > FAIRLEAD SUPPORT OTBD ATTACH ANGLE FS 484.0 LBL36 CRACKED. REMOVED/REPLACED ATTACH ANGLE IAW BOMBARDIER REO 601R-53-41-059 REV B AAR SM 33
- [SDR REXA2019040600479](https://openairdocs.org/sdr/REXA2019040600479.md): Attach Angle · cracked · Apr 6, 2019 · N8894A · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > FAIRLEAD SUPPORT INTERCOSTAL INBD ATTACH CLIP CRACKED AT FS 484 RBL 27. REMOVED/REPLACED ATTACH CLIP IAW BOMBARDIER REO 601R-53-41-059 REV B AAR SM 33
- [SDR REXA201904226477](https://openairdocs.org/sdr/REXA201904226477.md): Floor Support · corroded · Apr 6, 2019 · N8894A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AFT CARGO FLOOR SUPPORT STRUCTURE HAS LBL9 CORRODED BETWEEN FS605.0 AND FS621. REPAIRED AFT CARGO FLOOR SUPPORT STRUCTURE ON LBL9 FS 605-FS 621 IAW EA 253-08758.
- [SDR REXA2019042240489](https://openairdocs.org/sdr/REXA2019042240489.md): Floor Support · corroded · Apr 4, 2019 · N8894A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT BEAM LBL27 OTBD FLANGE HAS CORROSION AT FLOOR PNL ATTACH HDWR FS 575.0 TO FS605. REMOVED/REPLACED FLOOR BEAM CAP WITH NEW LOCATED/DRILLED CAP IAW ENDEAVOR AIR EA CRJ 253-08651.
- [SDR REXA2019042240468](https://openairdocs.org/sdr/REXA2019042240468.md): Mount · corroded · Apr 4, 2019 · N8894A · Cndair CL6002B19 · Wing, Attach Fittings
  > RIGHT WING OUTBOARD LEADING EDGE PANEL INBOARD PICCOLO TUBE MOUNT HAS CORROSION REMOVED AND REPLACED R/H WING OB L/E PANEL I/B PICOLO TUBE MOUNT (RIB) IAW CK 200 SRM 51-42-06 AND SRM 51-42-10. AAR R SM 4
- [SDR REXA2019042230470](https://openairdocs.org/sdr/REXA2019042230470.md): Rib · cracked · Apr 3, 2019 · N8894A · Cndair CL6002B19 · Wing, Rib/Bulkhead
  > L/H WING LEADING EDGE PANEL 530KL HAS I/B END CAP CORRODED. REMOVED AND REPLACED WITH NEW END CAP RIB IAW SRM 51-42-06 AND CRJ 200 SRM 51-42-13. AAR SM 58
- [SDR REXA20190422478](https://openairdocs.org/sdr/REXA20190422478.md): Angle · cracked · Apr 2, 2019 · N8894A · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > AFT EQUIPMENT BAY DOOR LH SURROUND FRAME CLIP AT FS700 CRACKED. REMOVED/REPLACED FS700 FRAME CLIP IAW CRJ 200 SRM 51-42-06 AAR SM 58
- [SDR REXA201904220475](https://openairdocs.org/sdr/REXA201904220475.md): Attach Angle · cracked · Apr 2, 2019 · N8894A · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > FAIR LEAD SUPPORT OTBD ATTACH ANGLE FS 484.0 LBL27 CRACKED. REMOVED/REPLACED ATTACH ANGLE IAW CRJ 200 SRM 53-41-43 AAR SM 33
- [SDR REXA20190422469](https://openairdocs.org/sdr/REXA20190422469.md): Bracket · chafed · Apr 2, 2019 · N8894A · Cndair CL6002B19 · Wing Miscellaneous Structure
  > LEFT WING HINGE FAIRING 597BB HAS A CHAFED BRACKET. REMOVED/REPLACED WITH NEW BRACKET ON LH WING HINGE FAIRING 597BB IAW CRJ 200 SRM 51-42-06 AAR SM 58
- [SDR REXA201904220467](https://openairdocs.org/sdr/REXA201904220467.md): Floor Support · corroded · Apr 2, 2019 · N8894A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LH FLOOR SUPPORT SILL AT CARGO DOOR THRESHOLD HAS CORROSION FS 574.0 TO FS 621.0. REPAIRED LH FLOOR SUPPORT SILL @ FS574 TO FS621 IAW CRJ 200 SRM 51-42-06. FOR OPS / RIG CHECK REFER TO 1016818 2000-0217. AAR SM 107
- [SDR REXA201904221476](https://openairdocs.org/sdr/REXA201904221476.md): Angle · cracked · Apr 1, 2019 · N8894A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > ANGLE CLIP ON THE FWD SIDE OF FRAME 589 JUST UNDER THE LH FLOOR SILL IS CRACKED, IN THE CARGO BAY BELOW THE FLOOR. REMOVED/REPLACED ANGLE CLIP ON FWD SIDE OF FS589 UNDER LH FLOOR SILL IAW CRJ 200 SRM 51-42-21 AAR SM 107
- [SDR REXA201904229472](https://openairdocs.org/sdr/REXA201904229472.md): Seat Track · corroded · Mar 29, 2019 · N8894A · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RH FLOOR SEAT RAIL RBL9 STICK 4 HAS CORROSION. REMOVED DAND REPLACED SEAT TRACK IAW CRJ 200 AMM 53-01-11. AAR SM 58
- [SDR REXA2019042229471](https://openairdocs.org/sdr/REXA2019042229471.md): Seat Track · corroded · Mar 29, 2019 · N8894A · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LH FLOOR SEAT RAIL LBL9 STICK 2 HAS CORROSION. REMOVED AND REPLACED SEAT TRACK IAW CRJ 200 AMM 53-01-11. AAR SM 58
- [SDR REXA201904227474](https://openairdocs.org/sdr/REXA201904227474.md): Seat Track · corroded · Mar 27, 2019 · N8894A · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RH FLOOR SEAT RAIL RBL9 STICK 1 HAS CORROSION. REMOVED AND REPLACED WITH NEW SEAT TRACK I.A.W. CRJ-200 AMM 53-01-11-420-01. AAR SM 58
- [SDR REXA2019042226473](https://openairdocs.org/sdr/REXA2019042226473.md): Seat Track · corroded · Mar 26, 2019 · N8894A · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LH FLOOR SEAT RAIL LBL9 STICK 1 HAS CORROSION. REMOVE AND REPLACE NEW SEAT TRACK IAW AMM 53-01-11-420-01. AAR SM 58
- [SDR REXA2019042250466](https://openairdocs.org/sdr/REXA2019042250466.md): Mount · chafed · Mar 25, 2019 · N8894A · Cndair CL6002B19 · Engine Mount Section
  > NR 2 ENG FWD MOUNT FWD AFT AND UPPER LUG SMALL NICK AND MINOR CHAFF C/W BOMBARDIER REO 601R-54-51-194 TO REMOVE CHAFE DAMAGE ROTO PEEN SURFACE FAND RESTORE FINISH (.003: MAX MATERIAL LOSS) AAR SM 39
- [SDR REXA2018071100607](https://openairdocs.org/sdr/REXA2018071100607.md): Pin · not seated · Jul 8, 2018 · N8894A · Cndair CL6002B19 · Light System Wiring
  > ENTRANCE DOOR 'EXIT' LIGHT INOP. FOUNBD PIN IN WIRING NOT INSTALLED ALL OF THE WAY CAUSING DISRUPTION IN ELECTRICITY. REINSTALLED PIN AND OPS CHECKED GOOD IAW AMM 33-51-10.
- [SDR REXA2018052200404](https://openairdocs.org/sdr/REXA2018052200404.md): Oxygen Bottle · empty · May 22, 2018 · N8894A · Cndair CL6002B19 · Portable Oxygen System
  > DURING MORNING PREFLIGHT BY FLIGHT ATTENDANT FOUND PORTABLE 02 BOTTLE TO BE ON AND EMPTY. REMOVED AND REPLACED PORTABLE 02 BOTTLE WITH NEW UNIT. PN ON & OFF 5500-C1A-Y0EE SN ON 191291 SN OFF 174826 IAW AMM 35-31-01.
- [SDR REXA2018051870388](https://openairdocs.org/sdr/REXA2018051870388.md): Bulkhead Web · dented · May 17, 2018 · N8894A · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > WHILE COMPLYING WITH JC 53-310-600, A DETAILED INSPECTION OF THE REAR PRESSURE BULKHEAD, VERTICAL STIFFENERS AND WEB. A SMOOTH DENT WAS FOUND IN THE WEB LOCATED BETWEEN LBL 27.5 - LBL 18 AND BELOW WL 137.5 - WL121.9. THERE ARE NO SHARP EDGES OR CREASES. AN
- [SDR REXA2018051760385](https://openairdocs.org/sdr/REXA2018051760385.md): Post · cracked · May 16, 2018 · N8894A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > VERTICAL POST, RBL 27, HAS A.75 INCH CRACK ORIGINATING AT THE BOTTOM INBD CHANNEL & EXTENDING UPWARDS UP TO & PAST THE FIRST RIVET, ENDING HALFWAY BETWEEN FIRST & SECOND RIVETS, BS 409+128. REPAIRED IAW REO 601R-53-41-0056. MAJOR REPAIR.
- [SDR REXA2018043000333](https://openairdocs.org/sdr/REXA2018043000333.md): Light · inoperative · Apr 30, 2018 · N8894A · Cndair CL6002B19 · Emergency Lighting
  > LEFT OVERWING EMERGENCY LIGHT OUT. R&R LIGHT BULB IAW AMM 33-51-21. OPS CHECK GOOD NO DEFECTS.
- [SDR REXA2018042900332](https://openairdocs.org/sdr/REXA2018042900332.md): Sign · inoperative · Apr 29, 2018 · N8894A · Cndair CL6002B19 · Emergency Lighting
  > LIGHTED FLOOR LEVEL EXIT SIGN FOUND INOP. R&R FLOOR LEVEL EXIT SIGN IAW AMM 33-51-10 OPS CHECK GOOD NO FURTHER DEFECTS NOTED AT THIS TIME PN ON/OFF 6020-6 NON SERIALIZED PART.
- [SDR REXA2017050100568](https://openairdocs.org/sdr/REXA2017050100568.md): Selector Valve · inoperative · May 1, 2017 · N8894A · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > GEAR DISAGREE WARNING MESSAGE WHEN GEAR EXTENDED. PERFORMED GO AROUND, WHEN SPEED INCREASED, THE MESSAGE WENT AWAY. RAN QRH AND LANDED. INSPECTED NLG AREA AND FOUND NO DEFECTS. INTERROGATED PSEU FOR CODES, PLACED GEAR EXTENSION AND RETRACTION SYSTEM ON M
- [SDR REXA2016122902541](https://openairdocs.org/sdr/REXA2016122902541.md): Uplock Target · loose · Dec 29, 2016 · N8894A · Cndair CL6002B19 · Landing Gear Position and Warning
  > GEAR DISAGREE WARNING AFTER T/O LEFT MAIN GEAR INDICATED RED, NOSE & MAIN INDICATED UP RAN QRH PERFORMED MEL MAINTENANCE PROCEDURES, DEFERRED LANDING GEAR RETRACTION SYSTEM IAW MEL 32-30-01. T/S IAW FIM 32-00-00. CODES FROM PSEU AS FOLLOWS: S30 FAR, S31 FAR, S
- [SDR REXA2016111902252](https://openairdocs.org/sdr/REXA2016111902252.md): Light · inoperative · Nov 19, 2016 · N8894A · Cndair CL6002B19 · Emergency Lighting
  > NR 3 EXTERNAL E LIGHT RIGHT SIDE INOP. R&R NR 3 EXTERNAL E-LIGHT ON RIGHT SIDE IAW AMM 33-51-21, OPS CHECK IAW AMM 33-51-00 OPS CHECK GOOD.
- [SDR REXA2016100201847](https://openairdocs.org/sdr/REXA2016100201847.md): Skin · damaged · Oct 2, 2016 · N8894A · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > DURING LIGHTNING STRIKE INSPECTION, FOUND DAMAGE TO FUSELAGE SKIN AT BS 409+65 ALONG STRINGER 14R. BLENDED THE DAMAGED AREA IAW SRM 51-12-00 AND INSTALLED FABRICATED REPAIR DOUBLER IAW EA CRJ253-04870.
- [SDR REXA2016062901217](https://openairdocs.org/sdr/REXA2016062901217.md): Frame · corroded · Jun 29, 2016 · N8894A · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME CORRODED AT BS 574 BETWEEN STRINGERS 25L-26R. REPAIRED FRAME IAW EA CRJ253-04482.
- [SDR REXA2016062801219](https://openairdocs.org/sdr/REXA2016062801219.md): Riser · cracked · Jun 28, 2016 · N8894A · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR LOWER STEP AFT RISER IS CRACKED. REPAIRED THE RISER IAW REO 601R-52-11-702. OPS CHECKED GOOD.
- [SDR REXA2016062601218](https://openairdocs.org/sdr/REXA2016062601218.md): Skin · dented · Jun 26, 2016 · N8894A · Cndair CL6002B19 · Spoilers
  > LT FLIGHT SPOILER IS DENTED. REPAIRED IAW CRJ257-04486
- [SDR REXA2016062001212](https://openairdocs.org/sdr/REXA2016062001212.md): Attach Bracket · damaged · Jun 20, 2016 · N8894A · Cndair CL6002B19 · Wing, Attach Fittings
  > LEFT WING L/E ATTACH BRACKET ANGLE IS CRACKED/CHAFED, LOCATED BETWEEN MIDDLE AND OTBD L/E WS 260. R & R LT WING L/E BRACKET WS 260 IAW SRM 51-42-06 LEAK CHECK TRANSFERRED TO SN 4715690, W/O 1013044-5000-0058.
- [SDR REXA2016061901216](https://openairdocs.org/sdr/REXA2016061901216.md): Attach Angle · cracked · Jun 19, 2016 · N8894A · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > LT OVERWING TO FUSELAGE PANEL ATTACH ANGLE BS 449.85 IS CRACKED. REMOVED & REPLACED THE ATTACH ANGLE IAW SRM 51-42-06.
- [SDR REXA2016061901215](https://openairdocs.org/sdr/REXA2016061901215.md): Floorbeam · cracked · Jun 19, 2016 · N8894A · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > MAIN CABIN FLOORBEAM HAS A CRACKED ANGLE AT BS 280 LBL 9. REMOVED & REPLACED THE ANGLE IAW SRM 51-42-21.
- [SDR REXA2016061701214](https://openairdocs.org/sdr/REXA2016061701214.md): Angle · cracked · Jun 17, 2016 · N8894A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INTERCOSTAL ANGLE AT BS 621 AND STRINGER 13L IS CRACKED. REMOVED AND REPLACED THE INTERCOSTAL ANGLE IAW SRM 51-42-06, & 51-42-21.
- [SDR REXA2016061701213](https://openairdocs.org/sdr/REXA2016061701213.md): Floorbeam · corroded · Jun 17, 2016 · N8894A · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOORBEAM CORRODED AT BS 559+80, RBL 27. REPAIRED FLOORBEAM IAW SRM 53-00-43 FIG 203.
- [SDR REXA2016061601222](https://openairdocs.org/sdr/REXA2016061601222.md): Floorbeam · cracked · Jun 16, 2016 · N8894A · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > MAIN CABIN FLOOR STRUCTURE HAS A CRACKED ANGLE AT BS 280 RBL 9. REMOVED & REPLACED ANGLE IAW SRM 51-42-21.

Next page: https://openairdocs.org/aircraft/N8894A/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 = 'N8894A' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8894A/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.