# Service difficulty reports: N8877A

A list on [N8877A](https://openairdocs.org/aircraft/N8877A.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 · 117 reports

- [SDR REXA2022060601074](https://openairdocs.org/sdr/REXA2022060601074.md): Lamp · inoperative · Jun 1, 2022 · N8877A · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHTING FLOOR STRIP AT ROW 9DC INOP. REPLACED FLOOR-TRACK EMERGENCY LIGHT AT ROW 9 DC IAW AMM 33-51-01. OPS TEST GOOD. P/N OFF/ON 36378-2.
- [SDR REXA2022052601037](https://openairdocs.org/sdr/REXA2022052601037.md): Connector · loose · May 21, 2022 · N8877A · Cndair CL6002B19 · Emergency Lighting
  > FFOD CABIN PREFLIGHT CHECK REVEALED EMERGENCY FLOOR TRACK LIGHTING DOES NOT ILLUMINATE FROM EXIT ROW TO AFT OF CABIN SECURED CONNECTORS IAW AMM 33-51-01. ALL CHECKS GOOD. PN 48-7190, 48-7191.
- [SDR REXA2021032900182](https://openairdocs.org/sdr/REXA2021032900182.md): Floor Support · corroded · Mar 21, 2021 · N8877A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LBL 27 FLOOR BEAM IS CORRODED BETWEEN F.S. 589 TO F.S. 605. REPAIRED LBL 27 FLOORBEAM AT FS 589 TO FS 605 IAW ENDEAVOR EA CRJ253-11304 REV A, DATED 3/14/2021.
- [SDR REXA2021032900181](https://openairdocs.org/sdr/REXA2021032900181.md): Handle · cracked · Mar 18, 2021 · N8877A · Cndair CL6002B19 · Electrical/Electronic Compartment Doors
  > FOUND MAIN AVIONICS DOOR HANDLE HOUSING HAS MULTIPLE INDICATIONS NOTED IN RADIUS AROUND ENTIRE BASE 90 % FSH, FAILED NDT INSPECTION
- [SDR REXA2021032900184](https://openairdocs.org/sdr/REXA2021032900184.md): Bulkhead Web · cracked · Mar 17, 2021 · N8877A · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUND REAR PRESSURE BULKHEAD WEB HAS 3 AREAS THAT HAVE MULTIPLE INDICATIONS NOTED. 1)LBL 18.00, WL 132 3"LONG 60% FSH; 2) BL 0.0, WL 127 7"LONG 100% FSH AND 3) BL 0.0, WL 112 3"LONG 50% FSH. ALL 3 AREAS FAILED NDT INSPECTION. REPAIRED FS 621 BULKHEAD IAW BOMB
- [SDR REXA2021032900185](https://openairdocs.org/sdr/REXA2021032900185.md): Bulkhead Web · cracked · Mar 16, 2021 · N8877A · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUND REAR PRESSURE BULKHEAD WEB HAS 3 CHAFED AREAS WL 103, LBL 27.50,.200 LONG X.200 WIDE; LBL 18.00 ON PREVIOUS REPAIR ON TRIPLER.200 LONG X.200 WIDE AND RBL 36.20 ON PREVIOUS REPAIR ON TRIPLER.200 LONG X.200 WIDE. ALL 3.003 DEEP. REMOVED CHAFE DAMAG
- [SDR REXA2021032900183](https://openairdocs.org/sdr/REXA2021032900183.md): Seat Track · corroded · Mar 16, 2021 · N8877A · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LBL 9 FLOOR SEAT TRACK IS CORRODED BETWEEN FS 574 TO FS 559+12. "REMOVED, FABRICATED AND INSTALLED SEAT TRACK AT LBL9, FS 574 TO FS 559+12 IAW REO 601R-53-00-485. "
- [SDR REXA2020121500835](https://openairdocs.org/sdr/REXA2020121500835.md): Connector · damaged · Dec 13, 2020 · N8877A · Cndair CL6002B19 · Light System Wiring
  > EMERGENCY EXIT LIGHT IN MAIN CABIN DOORWAY DOES NOT ILLUMINATE. REPAIRED CONNECTOR, PER ESPM 20-17-31. OPERATIONS TEST EMERGENCY LIGHT NORMAL, IAW AMM 33-50-00. A/C OK FOR SERVICE.
- [SDR REXA2020121500833](https://openairdocs.org/sdr/REXA2020121500833.md): Battery Pack · inoperative · Dec 3, 2020 · N8877A · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHTS WILL NOT STAY ILLUMINATED. REMOVED & REPLACED EMERGENCY BATTERIES AT POSITION PS1LF, PS4LF, PS2LF & PS3LF, IAW CRJ 200 JOB CARD 33-900-701. OPERATIONS CHECK GOOD, A/C OK FOR SERVICE. PN: 2013-1A, 2013-1ASMI, AD-2013-1A.
- [SDR REXA2020070600581](https://openairdocs.org/sdr/REXA2020070600581.md): Charger · inoperative · Jun 1, 2020 · N8877A · Cndair CL6002B19 · Emergency Lighting
  > RIGHT OVERWING EXIT FWD LIGHT INOP. FOUND EMERGENCY BATT CHARGER 2 W-BLOWN FUSE/RESISTOR. REMOVED AND REPLACED BATT CHARGER 2 P2LF IAW AMM 33-51-05. OPS CHECK GOOD, OK FOR SVC.
- [SDR REXA2019102541560](https://openairdocs.org/sdr/REXA2019102541560.md): Light · inoperative · Oct 24, 2019 · N8877A · Cndair CL6002B19 · Emergency Lighting
  > SMALL STRIP OF EMERGENCY FLOOR TRACK LIGHTING INOP IN FRONT REMOVED AND REPLACED INOP FLOOR TRACK LIGHTING PN 36262-4 IAW CRJ200 AMM 33-51-01
- [SDR REXA2019091001284](https://openairdocs.org/sdr/REXA2019091001284.md): Light · missing · Sep 6, 2019 · N8877A · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY TRACK LIGHT MISSING AT SEATS 1D AND C. INSTALLED NEW TRACK LIGHT AT SEATS 1D AND C IAW AMM 33-51-01. OPS CHECK GOOD. P/N ON: 36491-1.
- [SDR REXA2019080101143](https://openairdocs.org/sdr/REXA2019080101143.md): Light · inoperative · Aug 1, 2019 · N8877A · Cndair CL6002B19 · Emergency Lighting
  > TWO FRONT EMERGENCY LIGHTS ON FLOOR INOPERATIVE. REPLACED THE EMERGENCY LIGHT STRIP IAW AMM 33-51-01. OPS CHECKED GOOD.
- [SDR REXA2019041200458](https://openairdocs.org/sdr/REXA2019041200458.md): Light · inoperative · Apr 12, 2019 · N8877A · Cndair CL6002B19 · Emergency Lighting
  > RIGHT EXTERIOR EMERGENCY LIGHT INOP. R&R EXTERIOR EMERGENCY LIGHT IAW CRJ200 AMM 33-51-21-000-801. OPS CHECK GOOD AT THIS TIME.
- [SDR REXA2019031900339](https://openairdocs.org/sdr/REXA2019031900339.md): Support Bracket · cracked · Mar 19, 2019 · N8877A · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR HANDLE FWD SUPPORT BRACKET IS CRACKED. REMOVED AND REPLACED FWD PAX DOOR HANDRAIL SUPPORT BRACKET PER SRM 51-42-21.
- [SDR REXA2019031800338](https://openairdocs.org/sdr/REXA2019031800338.md): Door Frame · damaged · Mar 18, 2019 · N8877A · Cndair CL6002B19 · Service Doors
  > AFTER REMOVAL OF HI-LITES IN SPIGOT FOUND 2EA HOLES OVER SIZED IN AFT LOWER SPIGOT, FRAME SECTION AND INNER T SUPPORT REPAIR SERVICE DOOR LOWER FRAME SECTION IAW EA 252-08423.
- [SDR REXA2019031600334](https://openairdocs.org/sdr/REXA2019031600334.md): Angle · corroded · Mar 16, 2019 · N8877A · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > LBL9 FLOORBEAM ATTACHMENT TO THE REAR PRESSURE BULKHEAD HAS CORROSION. REPAIRED FLOOR ANGLE IAW EA CRJ 253-08552.
- [SDR REXA2019031400337](https://openairdocs.org/sdr/REXA2019031400337.md): Attach Bracket · cracked · Mar 14, 2019 · N8877A · Cndair CL6002B19 · Flight Compartment Windows
  > RIGHT SIDE LOWER CENTER POST ATTACH BRACKET ON FWD WINDSHIELD IS CRACKED. REMOVED AND REPLACED RT SIDE LOWER CENTERPOST BRACKET IAW SRM 51-42-21 OPS TEST GOOD IAW AMM 31-61-01 AND AMM 34-14-01.
- [SDR REXA2019031400335](https://openairdocs.org/sdr/REXA2019031400335.md): Floor Support · corroded · Mar 14, 2019 · N8877A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LBL9 FLOOR SUPPORT LANDING FS621 CORRODED. REPAIRED IAW EA CRJ253-08552 REV IR.
- [SDR REXA2019031200330](https://openairdocs.org/sdr/REXA2019031200330.md): Angle · cracked · Mar 12, 2019 · N8877A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > REFERENCE REJECTED CARD NO- 1016887-1000-0021 S/N 6965331. " FINAL ACTION REJECTED, ANGLE CLIP RBL-27 FS-484 WAS FABRICATED FROM INCORRECT MATERIAL. ORIG. DISC. AS FOLLOWS... ANGLE CLIP ON O/B SIDE OF RBL 27 AT FS 484 IS CRACKED, IN THE CABIN BELOW THE FLOOR
- [SDR REXA2019031100336](https://openairdocs.org/sdr/REXA2019031100336.md): Attach Fitting · cracked · Mar 11, 2019 · N8877A · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR FWD HAND RAIL SUPPORT ACTUATING ROD ATTACH FITTING AT THRESHOLD CRACKED. REMOVED CRACKED ATTACH FITTINGS AND INSTALLED NEW FITTINGS IAW SRM 51-41-02 AND SRM TR 51-42.
- [SDR REXA2019030700332](https://openairdocs.org/sdr/REXA2019030700332.md): Floor Support · corroded · Mar 7, 2019 · N8877A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LBL27 FLOOR SUPPORT HAS CORROSION BETWEEN FS574.0 AND FS609.0. REMOVED AND REPLACED FLOOR SUPPORT BEAM IAW SRM 51-42-21.
- [SDR REXA2019030700329](https://openairdocs.org/sdr/REXA2019030700329.md): Fitting · corroded · Mar 7, 2019 · N8877A · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > LBL27 FLOORBEAM ATTACHMENT TO REAR PRESSURE BULKHEAD HAS CORROSION. REPAIRED LBL 27 FLOORBEAM FITTING IAW EA CRJ 253-08537 REV IR.
- [SDR REXA2019030500333](https://openairdocs.org/sdr/REXA2019030500333.md): Angle · cracked · Mar 5, 2019 · N8877A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > ANGLE CLIP ON THE I/B SIDE OF LBL 36 AT FS 484 IS CRACKED, IN THE CABIN BELOW THE FLOOR. REMOVED CRACKED ANGLE CLIP IN I/B SIDE OF LBL36 FS 484 AND INSTALLED NEW ANGLE CLIP IAW SRM 51-42-06, 51-42-21, 53-41-43 51-24-36 TR-51-42 AND 601R-53-41-059.
- [SDR REXA2019030300328](https://openairdocs.org/sdr/REXA2019030300328.md): Plate · cracked · Mar 3, 2019 · N8877A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CARGO DOOR OPENING FWD TRACK LOWER PLATE IS CRACKED, JUST ABOVE LIGHT SWITCH. REMOVED CARGO DOOR FWD TRACK LOWER PLATE AND INSTALLED NEW PLATE IAW SRM 51-42-06.
- [SDR REXA2019030100331](https://openairdocs.org/sdr/REXA2019030100331.md): Frame · cracked · Mar 1, 2019 · N8877A · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME 605 IS CRACKED ON THE FWD SIDE JUST BELOW STGR 9L, IN THE CARGO BAY. REPAIRED 605 FRAME IAW REO 601R-53-61-5214 REV A.
- [SDR REXA2019022700326](https://openairdocs.org/sdr/REXA2019022700326.md): Seat Track · corroded · Feb 27, 2019 · N8877A · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RBL9 SEAT TRACK BETWEEN FS559.0 AND FS559.0+80 HAS CORROSION. REMOVED AND REPLACED WITH NEW SEAT TRACK IAW AMM 53-01-11 FORMAT ID REF W/O 1016887-1000-0063 S/N 6965447.
- [SDR REXA2019022300325](https://openairdocs.org/sdr/REXA2019022300325.md): Scuff Plate · corroded · Feb 23, 2019 · N8877A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > R1 DOOR SCUFF PLATE HAS CORROSION ON THE WHOLE LEADING EDGE. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00 MATCH DRILLED NE SCUFF PLATE AND CAP SEALED NUTPLATED IAW SRM 51-40-11 TR 51-42 AND SRM 51-23-00.
- [SDR REXA2019010200327](https://openairdocs.org/sdr/REXA2019010200327.md): Doubler · corroded · Jan 2, 2019 · N8877A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SUPPORT STRUCTURE STA 331 RBL 6 (APPROX) CORRODED. REMOVED AND REPLACED FLOOR SUPPORT DOUBLER AT FS331 RBL 6 IAW SRM 51-42-06, AND 51-42-13.
- [SDR REXA2018101500962](https://openairdocs.org/sdr/REXA2018101500962.md): Angle · cracked · Oct 15, 2018 · N8877A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > VERTICAL POST ANGLE AT FS 409.00+128 AT RBL 27.00, IB ANGLE CRACKED. REPAIRED FS 409+128 RBL 27 VERTICAL POST ON BULKHEAD IAW REO 601R-53-41-056.
- [SDR REXA2018092000866](https://openairdocs.org/sdr/REXA2018092000866.md): Oxygen Mask · unwanted deploy · Sep 18, 2018 · N8877A · Cndair CL6002B19 · Passenger Oxygen System
  > PASSENGER 02 MASKS ABOVE SEATS 12 C&D HAVE FALLEN DOWN. INSPECTED AND RESTOWED 02 MASK IAW AMM 35-21-09.
- [SDR REXA2018082800720](https://openairdocs.org/sdr/REXA2018082800720.md): Hose · cut · Aug 28, 2018 · N8877A · Cndair CL6002B19 · Portable Oxygen System
  > PORTABLE OXYGEN MASK HOSE WAS CUT. REMOVED AND REPLACED THE OXYGEN MASK IAW AMM 35-30-00-02.
- [SDR REXA2017050300569](https://openairdocs.org/sdr/REXA2017050300569.md): Torque Link · disconnected · May 3, 2017 · N8877A · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > ON TAKEOFF RECIEVED MSGS: NOSE DOOR OPEN (RED) GEAR DISAGREE (RED) NOSE WHEEL STEERING INOP (YELLOW) WOW INPUT (YELLOW). RAN QRH AND RETURNED TO DEPARTURE AND LANDED. GROUND PERSONNEL REPORTED TORQUE LINKS WERE DISCONNECTED. PERFORMED OPS CHECK OF THE LANDI
- [SDR REXA2017021600239](https://openairdocs.org/sdr/REXA2017021600239.md): Relay · inoperative · Feb 15, 2017 · N8877A · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHTS FAILED OPERATIONAL CHECK. REMOVED AND REPLACED AC ESSENTIAL BUSS SENSE RELAY IAW AMM 21-51-27-000-801. OPS TESTED GOOD IAW AMM 24-51-27-700-801, AND AMM 33-51-00-710-801.
- [SDR REXA2017020700225](https://openairdocs.org/sdr/REXA2017020700225.md): Intercostal · cracked · Feb 7, 2017 · N8877A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INTERCOSTAL CRACKED AT AFT PRESSURE BULKHEAD BS 621 STRINGER 16L. REMOVED & REPLACED THE INTERCOSTAL IAW SRM 51-42-06, & 51-42-21.
- [SDR REXA2017020700224](https://openairdocs.org/sdr/REXA2017020700224.md): Intercostal · cracked · Feb 7, 2017 · N8877A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INTERCOSTAL CRACKED AT APB FS 621 STRINGER 15L. REMOVED & REPLACED THE INTERCOSTAL IAW SRM 51-42-06, & 51-42-21.
- [SDR REXA2017020700223](https://openairdocs.org/sdr/REXA2017020700223.md): Intercostal · cracked · Feb 7, 2017 · N8877A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INTERCOSTAL CRACKED AT APB STRINGER 14L. REMOVED & REPLACED THE INTERCOSTAL IAW SRM 51-42-06 & 51-42-21.
- [SDR REXA2017020700222](https://openairdocs.org/sdr/REXA2017020700222.md): Intercostal · cracked · Feb 7, 2017 · N8877A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INTERCOSTAL CRACKED AT APB LT SIDE STRINGER 13L. REMOVED & REPLACED THE INTERCOSTAL IAW SRM 51-42-06 AND SRM 51-42-21.
- [SDR REXA2017020700203](https://openairdocs.org/sdr/REXA2017020700203.md): Pulley Bracket · cracked · Feb 7, 2017 · N8877A · Cndair CL6002B19 · Passenger/Crew Doors
  > CRACKED PAX DOOR PULLEY BRACKET. REMOVED AND REPLACED PAX DOOR PULLEY BRACKET IAW SRM 51-42-06.
- [SDR REXA2017020600229](https://openairdocs.org/sdr/REXA2017020600229.md): Channel · cracked · Feb 6, 2017 · N8877A · Cndair CL6002B19 · Engine Collector/Tailpipe/Nozzle
  > NR 2 ENGINE TAIL PIPE CHANNEL CRACKED, THIRD ANGLE FROM FRONT. REPAIRED THE CHANNEL AND OUTER SKIN IAW CMM 78-11-00, REPAIRS SRS025 AND SRS 042.
- [SDR REXA2017020600228](https://openairdocs.org/sdr/REXA2017020600228.md): Bulkhead · gouged · Feb 6, 2017 · N8877A · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 621, RBL 36.2, WL 103 IS GOUGED OUT OF LIMITS. REMOVED THE DAMAGE AND REPAIRED THE AREA IAW REO 601R-53-61-1285 REV.E.
- [SDR REXA2017020600227](https://openairdocs.org/sdr/REXA2017020600227.md): Bulkhead · gouged · Feb 6, 2017 · N8877A · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 621 AFT PRESSURE BULKHEAD LBL 18, WL 103 IS GOUGED OUT OF LIMITS. REMOVED THE DAMAGE AND REPAIRED THE AREA IAW REO 601R-53-61-1285 REV E.
- [SDR REXA2017020500220](https://openairdocs.org/sdr/REXA2017020500220.md): Drag Angle · cracked · Feb 5, 2017 · N8877A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT MLG BAY DRAG ANGLE CRACKED. REMOVED AND REPLACED THE DRAG ANGLE IAW SRM 51-41-00.
- [SDR REXA2017020500216](https://openairdocs.org/sdr/REXA2017020500216.md): Stringer · cracked · Feb 5, 2017 · N8877A · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > PASSENGER CABIN LT SIDE FWD END OF STRINGER 3L HAS EVIDENCE OF A CRACK FWD SIDE OF BS 379. REPAIRED THE STRINGER IAW SRM 53-00-03.
- [SDR REXA2017020400219](https://openairdocs.org/sdr/REXA2017020400219.md): Doubler · cracked · Feb 4, 2017 · N8877A · Cndair CL6002B19 · Engine Collector/Tailpipe/Nozzle
  > NR 2 ENGINE TAIL PIPE FAIRING STIFFENER PREVIOUS REPAIR DOUBLER CRACKED AT SECOND ANGLE FROM FWD EDGE. REMOVED AND REPLACED THE REPAIR DOUBLER IAW CMM 78-11-00.
- [SDR REXA2017020400214](https://openairdocs.org/sdr/REXA2017020400214.md): Seat Track · corroded · Feb 4, 2017 · N8877A · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT SIDEWALL SEAT TRACK HAS CORROSION BS 499 - 541. REPLACED THE SEAT TRACK IAW AMM 53-01-11 AND SRM 53-21-49.
- [SDR REXA2017020400213](https://openairdocs.org/sdr/REXA2017020400213.md): Seat Track · corroded · Feb 4, 2017 · N8877A · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT SIDEWALL SEAT TRACK HAS CORROSION BS 449+85 - 499. REPLACED THE SEAT TRACK IAW AMM 53-01-11 AND SRM 53-21-49.
- [SDR REXA2017020400212](https://openairdocs.org/sdr/REXA2017020400212.md): Seat Track · corroded · Feb 4, 2017 · N8877A · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT SIDEWALL SEAT TRACK HAS CORROSION BS 409+18 - 409+113. REPLACED THE SEAT TRACK IAW AMM 53-01-11, SRM 51-40-11, 51-21-16, 51-25-06, 51-25-16, AND REO 601R-53-00-485.
- [SDR REXA2017020400211](https://openairdocs.org/sdr/REXA2017020400211.md): Seat Track · corroded · Feb 4, 2017 · N8877A · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RT SIDEWALL SEAT TRACK STICK 2 HAS CORROSION IN CABIN FS364 - FS409+18. REPLACED NR 2 RT SIDEWALL SEAT TRACK IAW AMM 53-01-11 AND SRM 53-21-49.
- [SDR REXA2017020400207](https://openairdocs.org/sdr/REXA2017020400207.md): Seat Track · corroded · Feb 4, 2017 · N8877A · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LT SIDEWALL SEAT TRACK STICK 3 HAS CORROSION IN CABIN FS409+18 - FS409+113. REPLACED NR 3 LT SIDE SEAT TRACK IAW AMM 53-01-11, SRM 51-40-11, 51-21-16, 51-25-06, 51-25-16 AND REO 601R-53-00-485.

Next page: https://openairdocs.org/aircraft/N8877A/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 = 'N8877A' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8877A/reports

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