# Service difficulty reports: N8847A

A list on [N8847A](https://openairdocs.org/aircraft/N8847A.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 · 106 reports

- [SDR REXA2020072000601](https://openairdocs.org/sdr/REXA2020072000601.md): Battery Pack · inoperative · Jul 16, 2020 · N8847A · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY CEILING LIGHT DS4LY INOPERATIVE. REPLACED PS1LF BATTERY ASSY IAW AMM 33-51-04. PN OFF 2013-1A. SN OFF 119527. PN ON 2013-1ASMI. SN ON 12497. MINIMUM CHARGE TIME OF 6 HOURS WAS ACCOMPLISED PER CMM 25-60-03. DS4LY CEILING LIGHT OPS CHECKS GOOD IAW CRJ
- [SDR REXA2019101081415](https://openairdocs.org/sdr/REXA2019101081415.md): Rivet · sheared · Oct 8, 2019 · N8847A · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > DURING FLIGHT DECK CARPET REPLACEMENT, NOTED TWO FORWARD ALIGNMENT RIVETS ON OUTBOARD CA SEAT RAIL MISSING. PERFORMED TEMPORARY REPAIR IAW REO #601R-53-11-1093. SEE NRWC #728465 FOR PERMANENT REPAIR PWI ON FORWARD TWO ALIGNMENT RIVETS ON OUTBOARD CA SEAT RAIL
- [SDR REXA2019050400615](https://openairdocs.org/sdr/REXA2019050400615.md): Battery Pack · discharged · May 4, 2019 · N8847A · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHT STRIP LIGHT FROM ROW 6CD TO 8CD ARE ILLUMINATING. REMOVED AND REPLACED BATTERY PACK 3 AND BATTERY PACK 3 INVERTER (INVERTER FIX PROBLEM IAW AMM 33-51-04 AND AMM 33-51-07.
- [SDR REXA2019020150113](https://openairdocs.org/sdr/REXA2019020150113.md): Bracket · cracked · Jan 25, 2019 · N8847A · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR OPENING AFT WIRE HARNESS BRACKET J1MB IS CRACKED AT THE I/B SIDE OF THE LOWER LONGERON, IN THE CABIN BELOW THE FLOOR. INSTALLED NEW BRACKET IAW CRJ 200 SRM 51-42-06 AND IAW CRJ 200 SRM 51-41-00. AAR SM 11
- [SDR REXA2019020150111](https://openairdocs.org/sdr/REXA2019020150111.md): Angle · cracked · Jan 25, 2019 · N8847A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > ANGLE CLIP IS CRACKED ON THE I/B SIDE OF LBL 36 AT FS 484, IN THE CABIN BELOW THE FLOOR REMOVED AND REPLACED ANGLE CLIP AT I/B SIDE OF LBL36 AT FS484 IAW BOMBARDIER REI 601R-53-52-059. AAR SM 107
- [SDR REXA2019020140112](https://openairdocs.org/sdr/REXA2019020140112.md): Vane · chafed · Jan 24, 2019 · N8847A · Cndair CL6002B19 · Trailing Edge Flaps
  > LH WING INBD FLAP VANE ACTUATOR ACCESS PNL584CB CHAFED AT L/E. REMOVED CHAFED PANEL AND REPLACED WITH NEW PANEL IAW CRJ 200 SRM TR-51-42 AAR SM 58
- [SDR REXA2019020120114](https://openairdocs.org/sdr/REXA2019020120114.md): Rib · cracked · Jan 22, 2019 · N8847A · Cndair CL6002B19 · Trailing Edge Flaps
  > L/H I/B FLAP HAS A CRACKED RIB AT T/E JUST O/B OF I/B JACKSCREW. [INTERNAL] REPAIRED CRACKED RIBON L/H I/B FLAP AT T/E IAW EA# CRJ257-08167 REV A DATE 1-16-19. AAR SM 107
- [SDR REXA2019020160109](https://openairdocs.org/sdr/REXA2019020160109.md): Support Bracket · bent · Jan 16, 2019 · N8847A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR FWD TRACK CENTER SUPPORT BRACKET IS BENT REPALCED DOOR TRACK SUPPORT IAW CRJ-200-SRM-51-42-06. AAR SM 51
- [SDR REXA2019020150110](https://openairdocs.org/sdr/REXA2019020150110.md): Support Bracket · bent · Jan 15, 2019 · N8847A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR FWD TRACK LWR SUPPORT BRACKETS BENT REMOVED AND REPLACED BOTH AFT CAREGO DOOR FWD TRACK LWR SUPPORT BRACKETS IAW CRJ-200 SRM 51-42-06 DUE TO NO ALLOWABLE DAMAGE IAW CRJ-200 SRM 53-61-23. AAR SM 58
- [SDR REXA2019020150108](https://openairdocs.org/sdr/REXA2019020150108.md): Fitting · cracked · Jan 15, 2019 · N8847A · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > BATH TUB FITTING AT THE O/B SIDE OF RBL 9 IS CRACKED AT FS 461, IN THE CABIN BELOW THE FLOOR REMOVED AND REPALCED BATHTUB FITTING AT F.S 461 RBL IAW CRJ 200 SRM 51-42-06 AND CRJ-200 SRM 51-42-21. AAR SM 107
- [SDR REXA2019020140107](https://openairdocs.org/sdr/REXA2019020140107.md): Seat Track · corroded · Jan 14, 2019 · N8847A · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LH SIDEWALL SEAT TRACK STICK 5 HAS CORROSION SPOTS BETWEEN FS 449.85 THE CABIN. REMOVED AND REPLACED WITH NEW SEAT TRACK I.A.W. CRJ-200 CMM 53-01-11 AAR AP 225
- [SDR REXA2019020140105](https://openairdocs.org/sdr/REXA2019020140105.md): Seat Track · corroded · Jan 14, 2019 · N8847A · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RH SIDEWALL SEAT TRACK STICK 2 HAS CORROSION SPOTS BETWEEN FS 364 THRU FS 409+16, IN THE CABIN. REMOVED AND REPLACED WITH NEW TRACK I.A.W. CRJ-200 AMM 53-01-11 AAR SM 58
- [SDR REXA2019020140104](https://openairdocs.org/sdr/REXA2019020140104.md): Seat Track · corroded · Jan 14, 2019 · N8847A · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LH AISLE SEAT TRACK STICK 3 HAS CORROSION SPOTS BETWEEN FS 409+112 THRU FS 559, IN THE CABIN. REMOVED AND REPLACED SEAT TRACK I.A.W. CRJ-200 AMM 53-01-11 AAR SM 58
- [SDR REXA2019020140103](https://openairdocs.org/sdr/REXA2019020140103.md): Seat Track · corroded · Jan 14, 2019 · N8847A · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RH SIDEWALL SEAT TRACK STICK 3 HAS CORROSION SPOTS BETWEEN FS 409+16 THRU FS 409+112, IN THE CABIN. REMOVED AND REPLACED WITH NEW SEAT TRACK I.A.W. CRJ-200 AMM 53-01-11 AAR SM 58
- [SDR REXA2019020140102](https://openairdocs.org/sdr/REXA2019020140102.md): Seat Track · corroded · Jan 14, 2019 · N8847A · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LH SIDEWALL SEAT TRACK STICK 2 HAS CORROSION SPOTS BETWEEN FS 364 THRU FS 409+16, IN THE CABIN. REMOVED AND REPLACED WITH NEW SEAT TRACK I.A.W. CRJ-200 AMM 53-01-11 AAR AP 225
- [SDR REXA2019020140101](https://openairdocs.org/sdr/REXA2019020140101.md): Strap · corroded · Jan 14, 2019 · N8847A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR STRAP AT FS 559 HAS CORROSION SPOTS BETWEEN LBL 27 AND THE LH FLOOR SILL, IN THE CABIN BELOW THE FLOOR. EVALUATED CORROSION OUT OF LIMITS, REMOVED STRAP AND INSTALLED NEW STRAP I.A.W. CRJ-200 SRM 51-42-06 AAR AP 377
- [SDR REXA2019020110106](https://openairdocs.org/sdr/REXA2019020110106.md): Angle · cracked · Jan 11, 2019 · N8847A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > ANGLE CLIP IS CRACKED ON THE O/B SIDE OF RBL 27 AT FS 484, IN THE CABIN BELOW THE FLOOR. REMOVED AND REPLACED ANGLE CLIP AT F.S. 484 O/B SIDE OF RBL 27. I.A.W. CRJ-200 SRM 51-42-21 AAR SM 33
- [SDR REXA2018101500957](https://openairdocs.org/sdr/REXA2018101500957.md): Apu · smoke · Oct 12, 2018 · N8847A · Cndair CL6002B19 · APU Core Engine
  > IN FLIGHT HEAVY SMOKE BEGAN TO ENTER CABIN. WE RECIEVED APU OIL PRESS CAUTION MSG RAN QRH FOR THAT AS WELL AS SMOKE OM CABIN. WE SHUT DOWN APU. NO AUTO SHUTDOWN. COMPLIED WITH WORK SCOPE (CABIN SMOKE) AND REFER TO AML 3354481-1 FOR THE REPLACEMENT OF THE APU.
- [SDR REXA2018091100818](https://openairdocs.org/sdr/REXA2018091100818.md): Sign · inoperative · Sep 9, 2018 · N8847A · Cndair CL6002B19 · Emergency Lighting
  > OVERWING EMER EXIT SIGN NOT FUNCTIONING AIRCRAFT RIGHT. R&R LOWER RT EMERGENCY FLOOR LEVEL LIGHT SIGN IN EMERGENCY EXIT ROW IAW AMM 33-51-10 OPS CK GOOD. P/N OFF ON 6020-5.
- [SDR REXA2018080300665](https://openairdocs.org/sdr/REXA2018080300665.md): Warning System · activated · Jul 31, 2018 · N8847A · Cndair CL6002B19 · Landing Gear Position and Warning
  > AFTER T/O WE CALLED FOR GEAR UP THEN WE RECEIVED GEAR DISAGREE WARNING & NOSE DOOR OPEN WARNING. THE NOSE WHEEL APPEARED TO NOT COME UP, WOW INPUT CAUTION NOSEWHEEL STEERING CAUTION AND OUTPUT STATUS FAIL MESSAGE SHOWED. RAN QRH PULLED MANUAL RELEASE HANDLE HA
- [SDR REXA2018030900180](https://openairdocs.org/sdr/REXA2018030900180.md): Sensor · inoperative · Mar 9, 2018 · N8847A · Cndair CL6002B19 · Landing Gear Position and Warning
  > ENROUTE AND AFTER TAKEOFF, GEAR WAS SLOW TO SHOW NORMALLY. RECEIVED A NOSE GEAR DISAGREE. MESSAGE WENT OUT BEFORE QRH COULD BE RAN. TROUBLESHOT THE GEAR DISAGREE IAW FAULT TABLE IN FIM 30-60-09-01. FOUND NOSE GEAR CENTERING AND NR 2 WOW PROX SENSORS OUT OF
- [SDR REXA2018030400175](https://openairdocs.org/sdr/REXA2018030400175.md): Proximity Sensor · out of rig · Mar 4, 2018 · N8847A · Cndair CL6002B19 · Landing Gear Position and Warning
  > GEAR DISAGREE WARNING ABOUT ONE MINUTE AFTER RAISING GEAR. MESSAGE WENT AWAY AFTER ONE SECOND. NOSE GEAR INDICATION WHILE WARNING WAS POSTED. HAD AMBER DASHES, AFTER MESSAGE WENT AWAY, ALL INDICATIONS NORMAL. PERFORMED RIGGING OF THE PSEU PROXIMITY SENSOR
- [SDR REXA2018012300043](https://openairdocs.org/sdr/REXA2018012300043.md): Downlock Sensor · defective · Jan 23, 2018 · N8847A · Cndair CL6002B19 · Landing Gear Position and Warning
  > NOSE DISAGREE IN THE DOWN POSITION. R & R THE NR 1 AND 2 DOWNLOCK PROXIMITY SENSORS IAW AMM 32-21-05.
- [SDR REXA2017121101232](https://openairdocs.org/sdr/REXA2017121101232.md): Oxygen Mask · leaking · Dec 11, 2017 · N8847A · Cndair CL6002B19 · Crew Oxygen System
  > OBSERVERS OXYGEN MASK LEAKING AT REGULATOR/HEADSTRAP CONNECTION REMOVED AND REPLACED OBSERVERS OXYGEN MASK W/SERV ASSY IAW CRJ AMM 35-11-12-400-802. OPS AND LEAK CHECKS GOOD.
- [SDR REXA2017082100922](https://openairdocs.org/sdr/REXA2017082100922.md): Hydraulic System · contaminated · Aug 21, 2017 · N8847A · Cndair CL6002B19 · Hydraulic System, Main
  > UP RECIEVED, HYD 3 LOW PRESSURE CAUTION, AND MAIN GEAR DISAGREE WARNING MESSAGES. NOSE GEAR WAS UP, NOSE DOOR WAS OPEN, BOTH MAIN GEAR INDICATED RED. ON HYD PAGE, HYD QTY FOR SYS 3 INDICATED 100% AND BOTH 3A & 3B LINES WERE YELLOW AND SHOWED 300 PSI. WE VERIF
- [SDR REXA2017031200346](https://openairdocs.org/sdr/REXA2017031200346.md): Battery Pack · inoperative · Mar 12, 2017 · N8847A · Cndair CL6002B19 · Emergency Equipment
  > DURING INSPECTION, NOTED F/A EMERGENCY FLASHLIGHT INDICATOR LED NOT BLINKING. REMOVED AND REPLACED THE BATTERY PACK IAW AMM 25-61-00. OPS CHECKED GOOD.
- [SDR REXA2016103102099](https://openairdocs.org/sdr/REXA2016103102099.md): Oxygen Mask · leaking · Oct 31, 2016 · N8847A · Cndair CL6002B19 · Crew Oxygen System
  > FO OXYGEN MASK LEAKING. R & R THE OXYGEN MASK IAW AMM 35-11-12. OPS TESTED GOOD.
- [SDR REXA2016100601887](https://openairdocs.org/sdr/REXA2016100601887.md): Bulb · inoperative · Oct 6, 2016 · N8847A · Cndair CL6002B19 · Emergency Lighting
  > LEFT FWD EXTERIOR EMERGENCY LIGHT INOPERATIVE. R & R THE BULB IAW AMM 33-51-21. OPS CHECKED NORMAL.
- [SDR REXA2016090301710](https://openairdocs.org/sdr/REXA2016090301710.md): Seat Track · corroded · Sep 3, 2016 · N8847A · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT SEAT TRACK NR 7 BS 544 - 559+80 HAS CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 51-01-11 PARA A(4)-(9) & REO 601R-53-00-055.
- [SDR REXA2016090301689](https://openairdocs.org/sdr/REXA2016090301689.md): Door Sill · corroded · Sep 3, 2016 · N8847A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT FLOOR SILL AT CARGO DOOR CUTOUT HAS CORROSION FROM FS 587 TO FS 619. R & R LT FLOOR SILL AT CARGO DOOR IAW REO 601R-53-61-593 AND SRM 51-40-11.
- [SDR REXA2016090201697](https://openairdocs.org/sdr/REXA2016090201697.md): Fairing · chafed · Sep 2, 2016 · N8847A · Cndair CL6002B19 · Aerodynamic Fairings
  > RIGHT STUB FAIRING HAS CHAFE DAMAGE. REPAIRED IAW REO 601R-53-82-003.
- [SDR REXA2016090201690](https://openairdocs.org/sdr/REXA2016090201690.md): Hinge · corroded · Sep 2, 2016 · N8847A · Cndair CL6002B19 · Fuselage, Door Hinge
  > AFT CARGO DOOR SILL GUARD HAS A CORRODED HINGE. R & R HINGES ON AFT CARGO DOOR SILL GUARD IAW SRM 51-42-06.
- [SDR REXA2016083101714](https://openairdocs.org/sdr/REXA2016083101714.md): Connector · inoperative · Aug 31, 2016 · N8847A · Cndair CL6002B19 · Oxygen System Wiring
  > PASSENGER OXYGEN MASKS FAILED TO DROP AT SEATS 3CD, 5AB AND LAVATORY. RESEATED CONNECTORS J5 AS SEAT 3CD PSU, RESEATED PIN 4 IN CONNECTOR J5 AS SEAT 5AB PSU IAW ESPM 20-17-51. ADJUSTED LAVATORY 02 BOX DOOR IAW CMM 25-40-43. DISASSEMBLY STEP G.(1) AND ASSEMB
- [SDR REXA2016083001706](https://openairdocs.org/sdr/REXA2016083001706.md): Attach Angle · cracked · Aug 30, 2016 · N8847A · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > DURING REMOVAL OF LT SIDE WINDSHIELD SIDE POST SUPPORT LOWER WEB FOUND ATTACH ANGLE CRACKED. REPLACED THE ATTACH ANGLE IAW SRM 51-42-06 AND 51-40-11.
- [SDR REXA2016083001705](https://openairdocs.org/sdr/REXA2016083001705.md): Support · cracked · Aug 30, 2016 · N8847A · Cndair CL6002B19 · Fuselage Main, Structure
  > LEFT WINDSHIELD SIDE POST SUPPORT LOWER WEB CRACKED. REMOVED AND REPLACED THE SUPPORT IAW SRM 51-42-06.
- [SDR REXA2016083001702](https://openairdocs.org/sdr/REXA2016083001702.md): Attach Fitting · cracked · Aug 30, 2016 · N8847A · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > RIGHT WING TO FUSELAGE PANEL ATTACH FITTING BS 470 FOUND CRACKED. REMOVED AND REPLACED ATTACH FITTING IAW SRM 51-42-06.
- [SDR REXA2016083001701](https://openairdocs.org/sdr/REXA2016083001701.md): Attach Fitting · cracked · Aug 30, 2016 · N8847A · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > RIGHT WING TO FUSELAGE PANEL ATTACH FITTING BS 449.85. IS CRACKED. REMOVED AND REPLACED THE ATTACH FITTING IAW SRM 51-42-06.
- [SDR REXA2016083001700](https://openairdocs.org/sdr/REXA2016083001700.md): Attach Fitting · cracked · Aug 30, 2016 · N8847A · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > LEFT WING TO FUSELAGE PANEL ATTACH FITTING BS 461 FOUND CRACKED. REMOVED & REPLACED THE ATTACH FITTING IAW SRM 51-42-06.
- [SDR REXA2016083001699](https://openairdocs.org/sdr/REXA2016083001699.md): Attach Fitting · cracked · Aug 30, 2016 · N8847A · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > LEFT WING TO FUSELAGE PANEL ATTACH FITTING BS 449.85 IS CRACKED. REMOVED & REPLACED THE ATTACH FITTING IAW SRM.
- [SDR REXA2016083001698](https://openairdocs.org/sdr/REXA2016083001698.md): Attach Fitting · cracked · Aug 30, 2016 · N8847A · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > LEFT WING TO FUSELAGE PANEL ATTACH FITTING BS 470.00 IS CRACKED. REMOVED AND REPLACED THE ATTACH FITTING IAW SRM 51-42-06.
- [SDR REXA2016082701695](https://openairdocs.org/sdr/REXA2016082701695.md): Vertical Beam · cracked · Aug 27, 2016 · N8847A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > BS 409+128, LBL 18 VERTICAL BEAM IS CRACKED AT THE LOWER O/B RADIUS. REPAIRED IAW REO 601R-53-41-889 REV. A, REO 601R-53-41-056 REV. F AND SRM 51-42-06.
- [SDR REXA2016082701694](https://openairdocs.org/sdr/REXA2016082701694.md): Stringer · cracked · Aug 27, 2016 · N8847A · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > STRINGER 4R AT BS 379 IS CRACKED. REPAIRED THE STRINGER IAW SRM 53-00-03.
- [SDR REXA2016082501696](https://openairdocs.org/sdr/REXA2016082501696.md): Seal · torn · Aug 25, 2016 · N8847A · Cndair CL6002B19 · Nacelle/Pylon, Main Frame
  > TRANS COWL 444AT OTBD SEAL IS TORN. REMOVED & REPLACED THE SEAL IAW SRM 51-42-06 & 51-42-16.
- [SDR REXA2016082401693](https://openairdocs.org/sdr/REXA2016082401693.md): Bulkhead · gouged · Aug 24, 2016 · N8847A · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > BS 621 AFT PRESSURE BULKHEAD FWD FACE LT HALF HAS DAMAGED AREA IN SKIN WL 78 LBL 24. REPAIRED THE BULKHEAD IAW REO 601R-53-61-5800.
- [SDR REXA2016082201713](https://openairdocs.org/sdr/REXA2016082201713.md): Seat Track · corroded · Aug 22, 2016 · N8847A · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > NR 4 SEAT TRACK HAS CORROSION AND IS GOUGED AT BS 478. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11.
- [SDR REXA2016082001692](https://openairdocs.org/sdr/REXA2016082001692.md): Bulkhead · cracked · Aug 20, 2016 · N8847A · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > APB IS CRACKED JUST ABOVE CARGO DOOR TRACK UPPER PORTION. PERFORMED REPAIR TO AFT PRESSURE BULKHEAD WEB LBL27-50 IAW REO NR 601R-53-61-1541, REV: F.
- [SDR REXA2016081901691](https://openairdocs.org/sdr/REXA2016081901691.md): Bracket · cracked · Aug 19, 2016 · N8847A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CARGO DOOR CROSSBEAM AFT LOWER BRACKET AT STA 621 APB IS CRACKED. R & R BRACKET IAW SRM 51-42-21.
- [SDR REXA2016081801704](https://openairdocs.org/sdr/REXA2016081801704.md): Angle · cracked · Aug 18, 2016 · N8847A · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT EQUIPMENT BAY BS 621 BULKHEAD AFT SIDE ANGLE AT STRINGER 14 IS CRACKED. REMOVED & REPLACED THE ANGLE IAW SRM 51-42-06 & 51-42-21.
- [SDR REXA2016081801703](https://openairdocs.org/sdr/REXA2016081801703.md): Angle · cracked · Aug 18, 2016 · N8847A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AFT EQUIPMENT BAY BS 621 BULKHEAD AFT SIDE ANGLE AT STRINGER 13L IS CRACKED. REMOVED & REPLACED THE ANGLE IAW SRM 51-42-06 & 51-42-21.
- [SDR REXA2016081601712](https://openairdocs.org/sdr/REXA2016081601712.md): Seat Track · corroded · Aug 16, 2016 · N8847A · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT SEAT TRACK NR 6 FROM BS 484 - 544 HAS CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11.

Next page: https://openairdocs.org/aircraft/N8847A/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 = 'N8847A' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8847A/reports

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