# Service difficulty reports: N922XJ

A list on [N922XJ](https://openairdocs.org/aircraft/N922XJ.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 4 · 191 reports

- [SDR REXA2026092501880](https://openairdocs.org/sdr/REXA2026092501880.md): Lug · damaged · Sep 2, 2026 · N922XJ · Cndair CL6002D24 · Ailerons
  > FOUND L/H AILERON SIDE LUG LABELED G TO BE OVERSIZED. COMPLIED WITH STEP F(8) OF REO 670-57-61-237 REV. --, FABRICATED (QTY. 1) O/S AILERON BUSHING. LPI PERFORMED IAW STEP F(9) OF REO 670-57-61-237 REV--. NO INDICATIONS NOTED. APPLIED BRUSH CAD-PLATING T
- [SDR REXA2026092501879](https://openairdocs.org/sdr/REXA2026092501879.md): Lug · damaged · Sep 2, 2026 · N922XJ · Cndair CL6002D24 · Ailerons
  > FOUND LT AILERON SIDE LUG LABELED B TO BE OVERSIZED. FABRICATED (QTY. 1) O/S AILERON BUSHING. LPI PERFORMED IAW STEP F(9) OF REO 670-57-61-237 REV. --. NO INDICATIONS NOTED. APPLIED BRUSH CAD-PLATING TO NEW BUSHING LABELED B IAW STEP F(8) OF REO 670-57-61-
- [SDR REXA2026092501876](https://openairdocs.org/sdr/REXA2026092501876.md): Lug · damaged · Sep 2, 2026 · N922XJ · Cndair CL6002D24 · Ailerons
  > FOUND LT AILERON SIDE LUG LABELED I TO BE OVERSIZED. COMPLIED WITH SECTION I UPPER LUG ONLY IAW STEPS 1-3 OF REO 690-57-61-556 REV --(P2). PERFORMED EDDY CURRENT OF LT AILERON LUG IAW REO 690-57-61-556 REV -- P2. NO INDICATIONS NOTED. COMPLIED WITH SECTION I
- [SDR REXA2026092501875](https://openairdocs.org/sdr/REXA2026092501875.md): Lug · damaged · Sep 2, 2026 · N922XJ · Cndair CL6002D24 · Ailerons
  > FOUND L/H AILERON SIDE LUG LABELED -H- TO BE OVERSIZED. COMPLIED WITH SECTION LOWER LUG ONLY IAW STEPS 1-3 OF REO 690-57-61-556 REV --(P2). PERFORMED EDDY CURRENT OF LT AILERON LUG LABEL H IAW REO 690-57-61-556 REV -- P2. NO INDICATIONS NOTED. COMPLIED WITH
- [SDR REXA2026092501834](https://openairdocs.org/sdr/REXA2026092501834.md): Bushing · damaged · Sep 2, 2026 · N922XJ · Cndair CL6002D24 · Ailerons
  > FOUND LT AILERON SIDE LUG LABELED -C- TO BE OVERSIZED. COMPLIED WITH STEP F(7) OF REO 670-57-61-237 REV-, FABRICATED O/S AILERON BUSHING. THE LT AILERON SIDE LUG HAD AN INTERNAL DIAMETER OF (0.7511").COMPLIED WITH REMAINING STEPS F(10)-F(13) AND STEP G OF R
- [SDR REXA2026082501639](https://openairdocs.org/sdr/REXA2026082501639.md): Former · cracked · Aug 24, 2026 · N922XJ · Cndair CL6002D24 · Emergency Exits
  > R/H FWD OVERWING EMERGENCY EXIT DOOR UPPER FORMER CRACKED AROUND AFT LUG. COMPLIED WITH MHIRJ REO 670-52-21-103 REV-- DATE 2024-11-06.
- [SDR REXA2026082401632](https://openairdocs.org/sdr/REXA2026082401632.md): Former · cracked · Aug 23, 2026 · N922XJ · Cndair CL6002D24 · Emergency Exits
  > R/H AFT OVERWING EMERGENCY EXIT DOOR UPPER FORMER CRACKED AROUND AFT LUG. COMPLIED WITH MHIRJ REO 670-52-21-103 REV-- DATE 2024-11-06.
- [SDR REXA2026090801780](https://openairdocs.org/sdr/REXA2026090801780.md): Floor Support · corroded · Aug 20, 2026 · N922XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > RIGHT FLOOR SUPPORT IS CORRODED BETWEEN FS310 AND FS319. ON FURTHER INVESTIGATION FOUND TO BE HEAVILY CORRODED TO THE POINT WHERE THERE IS CHUNKS OF MATERIAL MISSING AT BS 319. REMOVED & REPLACED THE FLOOR SUPPORT BETWEEN FS280 - FS319 IAW SRM 51- 42-21-001-0
- [SDR REXA2026091001797](https://openairdocs.org/sdr/REXA2026091001797.md): Door · cracked · Aug 15, 2026 · N922XJ · Cndair CL6002D24 · Emergency Exits
  > L/H AFT OVERWING EMERGENCY EXIT DOOR UPPER FORMER CRACKED AROUND AFT LUG COMPLIED WITH ALL STEPS OF REO 670-52-21-103 REV -- DATE 2024-11-06 ON L/H AFT OVERWING EMERGENCY EXIT DOOR UPPER FORMER AFT LUG. INSTALLED THE LH AFT EMERGENCY EXIT LINER PANEL 835AZ IAW
- [SDR REXA2025052800594](https://openairdocs.org/sdr/REXA2025052800594.md): Lamp · inoperative · May 22, 2025 · N922XJ · Cndair CL6002D24 · Emergency Lighting
  > ONE BULB IN FLOOR LEVEL EMERGENCY FLOODLIGHT NEAR PAX DOOR INOP REMOVED AND REPLACED LIGHT BULB IAW AMM 33-51-11. OPS CHECK GOOD. P/N OFF/ON: OL3071BPE/GPL
- [SDR REXA2022040500257](https://openairdocs.org/sdr/REXA2022040500257.md): Unknown · inoperative · Mar 9, 2023 · N922XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > MAIN CABIN DOOR IS STUCK CLOSED. COULD NOT MOVE DOOR LEVER IN EITHER DIRECTION. FOUND AFT UPPER TENSION FITTING ON PAX DOOR TO BE RUBBING HARD ON TENSION BUTTON. ADJUSTED AFT UPPER TENSION FITTING ON PAX DOOR IAW CRJ900 AMM 52-11-19-820-801-A01. ADJUSTED COUNT
- [SDR REXA2022112102571](https://openairdocs.org/sdr/REXA2022112102571.md): Coaming · chafed · Nov 14, 2022 · N922XJ · Cndair CL6002D24 · Engine Thrust Reverser
  > RH LOWER TRANSCOWL INNER COAMING CHAFED AT FORWARD LATCH INSTALLED NEW 1 EA. COAMING P/N C/N624-2060-209, 2 EA. BEARING PAD P/N CN624-2130-201, 1 EA. CHANNEL P/N CN624-2049-201 & 1 EA. DOUBLER P/N CN624-2068-209 ON R/H LOWER TRANSCOWL, REF. CRJ900 SRM 51-42-06
- [SDR REXA2022112102568](https://openairdocs.org/sdr/REXA2022112102568.md): Retainer · chafed · Nov 14, 2022 · N922XJ · Cndair CL6002D24 · Engine Thrust Reverser
  > LH UPPER TRANSCOWL HAS 4EA CHAFED RETAINERS BLENDED CHAFE ON LH UPPER TRANSCOWL RETAINERS AND FOUND 3EA WITHIN LIMITS. 1EA OUT OF LIMITS AND REPLACED
- [SDR REXA2022112102567](https://openairdocs.org/sdr/REXA2022112102567.md): Seat Track · corroded · Nov 14, 2022 · N922XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION NOTED ON LH SIDE SEAT RAIL BETWEEN APPROX FS672.00 AND FS720 REMOVED AND REPLACED THE LH SIDE SEAT RAIL P/N SH690-36284-1 REF CRJ 900 AMM 53-00-49-400-801-A19
- [SDR REXA2022113002603](https://openairdocs.org/sdr/REXA2022113002603.md): Retainer · chafed · Nov 10, 2022 · N922XJ · Cndair CL6002D24 · Engine Thrust Reverser
  > RIGHT LWR TRANSCOWL HAD TWO RETAINERS CHAFED. REPLACED THE RETAINERS.
- [SDR REXA2022112102585](https://openairdocs.org/sdr/REXA2022112102585.md): Bracket · cracked · Nov 10, 2022 · N922XJ · Cndair CL6002D24 · Engine Thrust Reverser
  > R/H LWR TRANSCOWL INBD 'A" BRACKET IS CRACKED REPLACED ANGLE (BRACKET)
- [SDR REXA2022112102584](https://openairdocs.org/sdr/REXA2022112102584.md): Bracket · cracked · Nov 10, 2022 · N922XJ · Cndair CL6002D24 · Engine Thrust Reverser
  > R/H LWR TRANSCOWL OTBD "A" BRACKET IS CRACKED REPLACED ANGLE (BRACKET)
- [SDR REXA2022111102527](https://openairdocs.org/sdr/REXA2022111102527.md): Skin · cracked · Nov 9, 2022 · N922XJ · Cndair CL6002D24 · Engine Thrust Reverser
  > L/H LOWER TRANSCOWL Z STIFFENER HAS CRACK AND SHEARED RIVETS. COMPLIED WITH EA CRJ754-14795 REV A DATED 11/07/2022
- [SDR REXA2022112102578](https://openairdocs.org/sdr/REXA2022112102578.md): Stringer · corroded · Nov 8, 2022 · N922XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER 27 AND MULTIPLE RIVETS ON STGR27 BETWEEN FS265 -FS250 HAS CORROSION REPLACED STRINGER
- [SDR REXA2022111102525](https://openairdocs.org/sdr/REXA2022111102525.md): Web · corroded · Nov 8, 2022 · N922XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > LH FS280.00 LOWER WEB HAS INTERGRANULAR IN AREA BENEATH CROSSBEAM REPAIRED LH LOWER BULKHEAD WEB AT FS280 REF CRJ-900 SRM 53-11-10-201-004-A01
- [SDR REXA2022111102524](https://openairdocs.org/sdr/REXA2022111102524.md): Web · corroded · Nov 8, 2022 · N922XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > RH FS280.00 LOWER WEB HAS INTERGRANULAR IN AREA BENEATH CROSSBEAM REPAIRED RH LOWER BULKHEAD WEB AT FS280 REF CRJ-900 SRM 53-11-10-201-004-A01
- [SDR REXA2022112102582](https://openairdocs.org/sdr/REXA2022112102582.md): Housing · worn · Nov 7, 2022 · N922XJ · Cndair CL6002D24 · Engine Thrust Reverser
  > L/H LWR TRANSCOWL LATCH DOOR HINGE HALF COWL SIDE IS WORN. REPLACED HINGE HOUSING
- [SDR REXA2022112102581](https://openairdocs.org/sdr/REXA2022112102581.md): Bracket · cracked · Nov 7, 2022 · N922XJ · Cndair CL6002D24 · Engine Thrust Reverser
  > L/H LWR TRANSCOWL INBD "A" BRACKET CRACKED REPLACED ANGLE (BRACKET)
- [SDR REXA2022112102580](https://openairdocs.org/sdr/REXA2022112102580.md): Latch · chafed · Nov 7, 2022 · N922XJ · Cndair CL6002D24 · Engine Thrust Reverser
  > L/H LWR TRANSCOWL LATCH DOOR INNER SURFACE CHAFED REPLACED LATCH DOOR
- [SDR REXA2022111102523](https://openairdocs.org/sdr/REXA2022111102523.md): Torque Box · cracked · Nov 7, 2022 · N922XJ · Cndair CL6002D24 · Engine Thrust Reverser
  > DURING REMOVAL OF C-DUCT FOUND CRACK AT APPROX 12 O'CLOCK AT CASCADE ATTACH POINT REPAIRED PER EA: CRJ954-14767 REV B 11/6/2022
- [SDR REXA2022111102522](https://openairdocs.org/sdr/REXA2022111102522.md): Angle · damaged · Nov 7, 2022 · N922XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > OUTBD. "L" ANGLE @ FS280.00 AND LBL9.0 HAS ELONGATED HOLES REPLACED ANGLE
- [SDR REXA2022111102521](https://openairdocs.org/sdr/REXA2022111102521.md): Skin · corroded · Nov 7, 2022 · N922XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > UPON REMOVAL OF PAX DOOR FWD AND AFT WEBS FOUND AREAS OF CORROSION ON PAX DOOR INNER SKIN REPLACED THE PAX DOOR INNER SKIN
- [SDR REXA2022111102520](https://openairdocs.org/sdr/REXA2022111102520.md): Crossbeam · corroded · Nov 7, 2022 · N922XJ · Cndair CL6002D24 · Fuselage Main, Structure
  > AFTER REMOVAL OF THE COCKPIT FLOOR AFT SUPPORT ANGLE FOUND THE RH FS280 CROSSBEAM TO BE EXFOLIATED AT UPPER FORWARD CORNER APPROX. RBL6 REPLACE CROSSBEAM
- [SDR REXA2022111102519](https://openairdocs.org/sdr/REXA2022111102519.md): Crossbeam · corroded · Nov 7, 2022 · N922XJ · Cndair CL6002D24 · Fuselage Main, Structure
  > AFTER REMOVAL OF THE COCKPIT FLOOR AFT SUPPORT ANGLE FOUND THE LH FS280 CROSSBEAM TO BE EXFOLIATED AT UPPER FORWARD CORNER APPROX. LBL6 REPLACE CROSSBEAM
- [SDR REXA2022111102518](https://openairdocs.org/sdr/REXA2022111102518.md): Striker · chafed · Nov 7, 2022 · N922XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FORWARD BAGGAGE BAY DOOR SURROUND – LOWER SEAL STRIKER HAS CHAFING AT THE FORWARD AND AFT CORNERS; SH670-34126-7 AND SH670-34126-8 REPAIRED PER EA: CRJ953-14709 & CRJ953-14710
- [SDR REXA2022111102517](https://openairdocs.org/sdr/REXA2022111102517.md): Floorbeam · corroded · Nov 7, 2022 · N922XJ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > FLOOR SUPPORT ON THE FORWARD SIDE OF THE 280 BEAM BETWEEN LBL9 & RBL9 IS CORRODED REPLACED COCKPIT FLOOR SUPPORT ANGLE
- [SDR REXA2022113002602](https://openairdocs.org/sdr/REXA2022113002602.md): Hinge · excess play · Nov 3, 2022 · N922XJ · Cndair CL6002D24 · Engine Thrust Reverser
  > RIGHT UPPER TRANSCOWL LATCH DOOR HAS EXCESSIVE PLAY. REPLACED HINGE HOUSING
- [SDR REXA2022112102579](https://openairdocs.org/sdr/REXA2022112102579.md): Pad · chafed · Nov 2, 2022 · N922XJ · Cndair CL6002D24 · Engine Thrust Reverser
  > LH UPPER TRNASCOWL 2 EA LATCH DOOR BEARING PADS ARE WORN REPLACED PAD
- [SDR REXA2022111002433](https://openairdocs.org/sdr/REXA2022111002433.md): Flap · cracked · Nov 1, 2022 · N922XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > PASSENGER DOOR EXTERNAL HANDLE FLAP IS CRACKED IN THE FORWARD AND AFT LOWER CORNERS REPLACED PAX DOOR HANDLE FLAP
- [SDR REXA2022111002479](https://openairdocs.org/sdr/REXA2022111002479.md): Beam · cracked · Oct 30, 2022 · N922XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > BEAM FOR AFT WEB GAS SPRING CRACKED ON PAX DOOR REPLACED BEAM
- [SDR REXA2022111002434](https://openairdocs.org/sdr/REXA2022111002434.md): Angle · cracked · Oct 30, 2022 · N922XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR AFT WEB DRAG ANGLE CRACKED REPLACED ANGLE
- [SDR REXA2022112102583](https://openairdocs.org/sdr/REXA2022112102583.md): Coaming · chafed · Oct 29, 2022 · N922XJ · Cndair CL6002D24 · Engine Thrust Reverser
  > R/H UPPER TRANSCOWL INNER COAMING CHAFED @ FWD LATCH REPAIRED COMPLIED WITH REO 670-54-21-1028 REV NC DATE 2009-06-15
- [SDR REXA2022112102570](https://openairdocs.org/sdr/REXA2022112102570.md): Spigot · chafed · Oct 28, 2022 · N922XJ · Cndair CL6002D24 · Engine Thrust Reverser
  > R/H UPPER TRANSCOWL LATCH SPIGOT WORN REPLACED SPIGOT
- [SDR REXA2022112102569](https://openairdocs.org/sdr/REXA2022112102569.md): Tab · chafed · Oct 28, 2022 · N922XJ · Cndair CL6002D24 · Engine Thrust Reverser
  > R/H UPPER TRANSCOWL LATCH DOOR SPRING REACTION TAB CHAFED REPLACED TAB
- [SDR REXA2022111002477](https://openairdocs.org/sdr/REXA2022111002477.md): Stringer Splice · corroded · Oct 25, 2022 · N922XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER SPLICE AT FS333 STR 22R HAD DEEP PITTING CORROSION REPLACED STRINGER SPLICE
- [SDR REXA2022111002453](https://openairdocs.org/sdr/REXA2022111002453.md): None · cracked · Oct 25, 2022 · N922XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR OUTER HANDLE PRESSURE BOX ASSY. P/N 601R31766-7 IS CRACKED COMPLIED WITH THE TEMP REPAIR REO 690-52-11-787 REV -- DATE 2022-10-25
- [SDR REXA2022111002436](https://openairdocs.org/sdr/REXA2022111002436.md): Angle · corroded · Oct 25, 2022 · N922XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR ANGLE P/N 601R317052-1 AND CLIP P/N 601R318058-1 COMMON TO DD7A INTERCOSTAL ARE CORRODED REPLACED ANGLE & CLIP
- [SDR REXA2022110102370](https://openairdocs.org/sdr/REXA2022110102370.md): Seat Track · corroded · Oct 25, 2022 · N922XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FLOOR SEAT TRACK AT RBL9 HAS CORROSION BETWEEN FS364 AND FS379 AND IS GOUGED AT FS437 REMOVED AND REPLACED SEAT TRACK.
- [SDR REXA2022110202379](https://openairdocs.org/sdr/REXA2022110202379.md): Cleat · worn · Oct 24, 2022 · N922XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > HOLES ON CLEAT ARE ELONGATED F.S.295.00 STR 23R REPLACED CLEAT
- [SDR REXA2022110102372](https://openairdocs.org/sdr/REXA2022110102372.md): Angle · corroded · Oct 24, 2022 · N922XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > ANGLE ON FS319 STRG22R HAS CORROSION REPLACED ANGLE
- [SDR REXA2022110102363](https://openairdocs.org/sdr/REXA2022110102363.md): Skin · chafed · Oct 24, 2022 · N922XJ · Cndair CL6002D24 · Cargo/Baggage Doors
  > FWD BAGGAGE BAY LOWER, FWD INNER SKIN IS CHAFED COMPLIED WITH EA CRJ952-14722 REV IR 10/22/2022
- [SDR REXA2022111002468](https://openairdocs.org/sdr/REXA2022111002468.md): Frame · corroded · Oct 23, 2022 · N922XJ · Cndair CL6002D24 · Fuselage Main, Frame
  > FRAME AT F.S.295.00 IS CORRODED BETWEEN STR26L AND 25R REPLACED FRAME
- [SDR REXA2022111002464](https://openairdocs.org/sdr/REXA2022111002464.md): Stringer · corroded · Oct 23, 2022 · N922XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > STR 19R HAS DEEP PITTING AT SEVERAL LOCATIONS REPLACED STRINGER
- [SDR REXA2022111002463](https://openairdocs.org/sdr/REXA2022111002463.md): Retainer · chafed · Oct 23, 2022 · N922XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR LOWER SEAL RETAINER P/N 601R318087-3 IS CHAFED REPLACED RETAINER
- [SDR REXA2022110202381](https://openairdocs.org/sdr/REXA2022110202381.md): Panel · corroded · Oct 23, 2022 · N922XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR ACCESS PANEL 832AL AND 832EL HAS EXFOLIATED CORROSION REPLACED ACCESS PANELS 832AL & 832EL, PNS 601R31902-463 & 600-3190

Next page: https://openairdocs.org/aircraft/N922XJ/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 = 'N922XJ' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N922XJ/reports

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