# Service difficulty reports: N181GJ

A list on [N181GJ](https://openairdocs.org/aircraft/N181GJ.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 2 · 68 reports

- [SDR REXA2025102700964](https://openairdocs.org/sdr/REXA2025102700964.md): Lock · inoperative · Oct 22, 2025 · N181GJ · Cndair CL6002D24 · Fixed Inner Doors
  > CA WENT TO USE BATHROOM AND COMING BACK THE FLIGHT DECK DOOR WOULD NOT OPEN. CA TRIED TO SHIMMY THE DOOR AND IT DID NOT OPEN SO WE HAD TO TAKE THE HINGE PIN OUT. R/R COCKPIT DOOR LOCK ASSY IAW CMM 25-17-03 OPC GOOD
- [SDR REXA2025032400350](https://openairdocs.org/sdr/REXA2025032400350.md): Diaphragm · damaged · Mar 17, 2025 · N181GJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > UPON LOCATING OF NEW RBL 36 BEAM, WE HAVE DISCOVERED DIAPHRAGM @ FS 792 ON RIGHT HAND SIDE TO HAVE MULTIPLE ELONGATED HOLES COMMON TO SILL DECK AND DIAPHRAGM. THESE HOLES ARE ONLY ELONGATED IN THE DIAPHRAGM, NOT ELONGATED IN THE SILL DECK SKIN. COMPLIED WITH
- [SDR REXA2024103001208](https://openairdocs.org/sdr/REXA2024103001208.md): Intercostal · corroded · Mar 20, 2024 · N181GJ · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR DD6 MID INTERCOSTAL CORRODED. LOCATED DRILLED AND INSTALLED NEW INTERCOSTAL IAW CRJ900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
- [SDR REXA2024051700388](https://openairdocs.org/sdr/REXA2024051700388.md): Handle · cracked · Mar 18, 2024 · N181GJ · Cndair CL6002D24 · Electrical/Electronic Compartment Doors
  > MAIN AVIONICS DOOR HANDLE HOUSING HAS CRACK INDICATIONS FOUND AROUND CIRCUMFERENCE OF HANDLE BASE. FAILED NDT. REMOVED DOOR HANDLE HOUSING FROM MAIN AVIONICS COMPARTMENT DOOR IAW CRJ900 AMM 52-42-03-000-801-A01 AND SRM 51-42-21-001-001-A01. INSTALLED NEW SERVI
- [SDR REXA2024040200326](https://openairdocs.org/sdr/REXA2024040200326.md): Angle · corroded · Mar 17, 2024 · N181GJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > SERVICE DOOR ANGLE MOUNTING HAS HEAVY CORROSION. REMOVED ANGLE MOUNTING (P/N:SH670-31996-3) IAW CRJ900 SRM 51-21-06-001-001-A01. INSTALLED ANGLE LOWER SILL (P/N:SH670-31986-1) IAW CRJ900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01. LOCATED AND DRIL
- [SDR REXA2024040200325](https://openairdocs.org/sdr/REXA2024040200325.md): Door Frame · cracked · Mar 17, 2024 · N181GJ · Cndair CL6002D24 · Fuselage Main, Structure
  > R/H AFT EMERGENCY EXIT DOOR S/N: SB0830 - 1 (EA.) TOP FORMER CRACKED BY THE SWITCH TARGET. REPAIRED IAW ENDEAVOR AIR EA# CRJ952-16162, REV IR, DATED 3/25/24.
- [SDR REXA2024040200324](https://openairdocs.org/sdr/REXA2024040200324.md): Door Frame · cracked · Mar 17, 2024 · N181GJ · Cndair CL6002D24 · Fuselage Main, Structure
  > R/H FWD. EMERGENCY EXIT DOOR S/N: SB0836 - 1 (EA.) TOP FORMER CRACKED BY THE SWITCH TARGET. REPAIRED IAW ENDEAVOR AIR EA# CRJ952-16164, REV IR, DATED 3/28/2024.
- [SDR REXA2024040200323](https://openairdocs.org/sdr/REXA2024040200323.md): Door Frame · cracked · Mar 17, 2024 · N181GJ · Cndair CL6002D24 · Fuselage Main, Structure
  > L/H AFT EMERGENCY EXIT DOOR S/N: SB0834 - 1 (EA.) TOP FORMER CRACKED BY THE SWITCH TARGET. REPAIRED IAW ENDEAVOR AIR EA# CRJ952-16163, REV IR, DATED 3/25/2024.
- [SDR REXA2024032600311](https://openairdocs.org/sdr/REXA2024032600311.md): Striker · corroded · Mar 17, 2024 · N181GJ · Cndair CL6002D24 · Service Doors
  > SERVICE DOOR SEAL STRIKER AFT SIDE HAS LIGHT CORROSION AROUND SCREW HOLES. REMOVED CORROSION IAW CRJ-900 SRM 51-21-06-001-001-A01 ORIGINAL MATERIAL THICKNESS 0.120 REMOVED.066, REMAINING MATERIAL THICKNESS 0.054, SEAL STRIKER IS OUT OF LIMITS DUE TO MO
- [SDR REXA2024103001206](https://openairdocs.org/sdr/REXA2024103001206.md): Coaming · deformed · Mar 16, 2024 · N181GJ · Cndair CL6002D24 · Engine Thrust Reverser
  > UPPER L/H TRANSCOWL LATCH DOOR COAMING, AND DOUBLER FOUND TO BE CHAFED AND SPIGOT HOLES ENLARGED. REMOVED UPPER L/H TRANSCOWL FWD LATCH TO F.O.M IAW CRJ900 SRM 51-41-02-001-001-A01 REMOVED FWD UPPER LATCH STIFFENER TO F.O.M IAW CRJ900 SRM 51-42-13-001-001-A01
- [SDR REXA2024103001205](https://openairdocs.org/sdr/REXA2024103001205.md): Skin · chafed · Mar 16, 2024 · N181GJ · Cndair CL6002D24 · Landing Gear Doors
  > "RIGHT MLG DOOR INNER SKIN AFT SIDE IS CHAFED APPROX..5""W X 4""L X.010""D UPON FURTHER INVESTIGATION, CHAFE DAMAGE IS LOCATED ON R/H MLG DOOR INNER SKIN FILLER ON FWD SIDE. CHAFE IS APPROX. 0.010"" D AND RUNS ACROSS ENTIRE LENGTH OF PART. REMOVED DAMAGED FI
- [SDR REXA2024040200322](https://openairdocs.org/sdr/REXA2024040200322.md): Door Frame · corroded · Mar 16, 2024 · N181GJ · Cndair CL6002D24 · Fuselage Main, Structure
  > PAX DOOR FWD FORMER IS CORRODED ON INNER SIDE. REMOVED DAMAGED FORMER, LOCATED, DRILLED AND INSTALLED SERVICEABLE PAX DOOR FWD FORMER, P/N 601R318031-5S IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01,51-42-21-001-001-A01 AND 51-40-11-001-001
- [SDR REXA2024032500307](https://openairdocs.org/sdr/REXA2024032500307.md): Bulkhead Web · cracked · Mar 16, 2024 · N181GJ · Cndair CL6002D24 · Fuselage Main, Bulkhead
  > LH FS 280 BULKHEAD LOWER WEB AT LBL11 WL 72 IS CORRODED. L/H FS 280 LOWER WEB IS CORRODED ON MORE THAN ONE ELEMENT, DEPTH OF CORROSION IS.017 AND IS OUT OF LIMITS IAW CRJ 900 SRM 53-11-10-201-003-A01.COMPLIED WITH STEPS 5.B.(1 THRU 3) REMOVE SPLICE PLATE,
- [SDR REXA2024103001202](https://openairdocs.org/sdr/REXA2024103001202.md): Angle · corroded · Mar 15, 2024 · N181GJ · Cndair CL6002D24 · Landing Gear Doors
  > SEVERAL AREAS OF CORROSION ON LH LNBOARD MLG DOOR REMOVED LIGHT CORROSION FROM EXPOSED SURFACE OF ANGLE P/N CC670-10563-3 PER CRJ 900 SRM 51-21-06-001-001-A01. RECEIVED AND COMPLIED WITH ALL STEPS OF ENDEAVOR AIR EA CRJ952-16169 REV IR DATED 3/18/2024.
- [SDR REXA2024103001201](https://openairdocs.org/sdr/REXA2024103001201.md): Drain Pan · deformed · Mar 15, 2024 · N181GJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FS 280 RH DRAIN PAN HAS SEVERAL ELONGATED HOLES AND POPPED RIVETS. REPAIRED IAW ENDEAVOR AIR EA CRJ953-16255 REV A DATED 3/25/2024.
- [SDR REXA2024103001200](https://openairdocs.org/sdr/REXA2024103001200.md): Bulkhead Web · corroded · Mar 14, 2024 · N181GJ · Cndair CL6002D24 · Fuselage Main, Bulkhead
  > RH FS280.00 BULKHEAD LOWER WEB IS CORRODED ON AFT FACE AT RBL 42, WL 72. REPAIRED RH FS280 LOWER WEB IAW CRJ 900 SRM 53-11-10-201-004-A01
- [SDR REXA2024103001199](https://openairdocs.org/sdr/REXA2024103001199.md): Floorbeam · corroded · Mar 14, 2024 · N181GJ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > R/H FS 280 CROSSBEAM IS CORRODED BETWEEN BL0 AND RBL 5 REPLACED RH FS280 CROSSBEAM IAW CRJ 900 SRM 51-40-11-001-001-A01,51-42-06-001-001-A01, 51-42-13-001-001-A01 AND 51-42-21-001-001-A01.
- [SDR REXA2024103001198](https://openairdocs.org/sdr/REXA2024103001198.md): Floorbeam · corroded · Mar 14, 2024 · N181GJ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > FS280 CROSSBEAM FWD J-ANGLE IS CORRODED AROUND FASTENER RECEPTACLES. LOCATED AND DRILLED NEW J-ANGLE P/N CC670-34095-1SB LOCATED AT FS 280 BETWEEN RBL 12 TO LBL 12 IAW CRJ-900 SRM 51-40-11-001-001-A01 INSTALLED NEW J-ANGLE IAW CRJ-900 SRM 51-42-06-001-001-A01
- [SDR REXA2024040100317](https://openairdocs.org/sdr/REXA2024040100317.md): Fitting · worn · Mar 14, 2024 · N181GJ · Cndair CL6002D24 · Rudder Structure
  > "MID LOWER RUDDER FITTING BOTTOM HALF BEARING BORE IS WORN. DEPTH SHOULD BE.286"" BORE IS AT.3185"" FITTING REQUIRES REPLACEMENT. LOCATED AND DRILLED FASTENER HOLES IN NEW SERVICEABLE FITTING PN AV670-21081-013 IAW CRJ 900 SRM 51-40-11-001-001-A01. R
- [SDR REXA2024032600310](https://openairdocs.org/sdr/REXA2024032600310.md): Skin · corroded · Mar 14, 2024 · N181GJ · Cndair CL6002D24 · Landing Gear Doors
  > SEVERAL AREAS OF CORROSION ON THE RIGHT MLG DOOR SKIN ON FORWARD INBOARD EDGE. REMOVED CORROSION FROM R/H MLG I/B DOOR FWD EDGE MEMBER (CC670-10524-4 0.063"") IAW CRJ-900 SRM 51-21-06-001-001-A01. NO DAMAGE ALLOWED IAW CRJ-900 SRM 52-82-02-101-001-A01. ENGI
- [SDR REXA2024032600309](https://openairdocs.org/sdr/REXA2024032600309.md): Floorbeam · corroded · Mar 14, 2024 · N181GJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "L/H FS 280 CROSSBEAM IS CORRODED BETWEEN BL0 AND LBL 5 UPON CLEANING UPPER FLANGE AND VERTICAL WEB OF FS280.00 FLOOR BEAM FROM BL 0 TO LBL 11 PER CRJ 900 SRM 51-26-00-001-001-A01, FOUND ADDITIONAL CORROSION ON UPPER FLANGE BETWEEN LBL 8 AND LBL 11. BEGAN REM
- [SDR REXA2024103001197](https://openairdocs.org/sdr/REXA2024103001197.md): Floor Support · corroded · Mar 13, 2024 · N181GJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > RH FLOOR SILL IS CORRODED AT FS 280. REMOVED CORROSION ON R/H FLOOR SILL BETWEEN FS 280 TO FS 319 IAW CRJ-900 SRM 51-21-06-001-001-A01.
- [SDR REXA2024103001196](https://openairdocs.org/sdr/REXA2024103001196.md): Former · cracked · Mar 12, 2024 · N181GJ · Cndair CL6002D24 · Emergency Exits
  > L/H FWD. EMERGENCY EXIT DOOR S/N: SB0835 - 2 (EA.) TOP FORMERS CRACKED BY THE SWITCH TARGET. REPAIRED IAW MHIRJ REO 690-52-162.
- [SDR REXA2024103001195](https://openairdocs.org/sdr/REXA2024103001195.md): Bushing · damaged · Mar 12, 2024 · N181GJ · Cndair CL6002D24 · Ailerons
  > UPON REMOVAL OF L/H AILERON SIDE PCU BUSHINGS, BUSHING LUGS FOUND TO BE PREVIOUSLY OVERSIZED REPAIRED LH AILERON PCU BUSHING LUGS IAW REO 670-57-6-237 REV - - DATED 2017-07-25
- [SDR REXA2024103001192](https://openairdocs.org/sdr/REXA2024103001192.md): Web · cracked · Mar 11, 2024 · N181GJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FWD EQUIPMENT COMPARTMENT L/H FLOOR WEB IS CRACKED AT F.S.193. INSTALLED NEW FRAME CLEAT @ FS193 PER REPAIR IAW CRJ900 SRM 53-11-43-201-001-A01 AND CRJ900 SRM 51-42-06-001-001-A01. INSTALLED REPAIR PARTS IAW CRJ900 SRM 53-11-43-201-001-A01 AND CRJ900 SRM 51-42
- [SDR REXA2024080500609](https://openairdocs.org/sdr/REXA2024080500609.md): Drag Angle · cracked · Mar 11, 2024 · N181GJ · Cndair CL6002D24 · Vertical Stabilizer
  > RH FWD VERTICAL DRAG ANGLE HAS A POSSIBLE CRACK. REPAIRED RH FWD VERTICAL DRAG ANGLE IAW CRJ 900 SRM 55-31-00-201-001-A01.
- [SDR REXA2024061400434](https://openairdocs.org/sdr/REXA2024061400434.md): Drag Angle · cracked · Mar 11, 2024 · N181GJ · Cndair CL6002D24 · Vertical Stabilizer
  > RH AFT VERTICAL DRAG ANGLE HAS A POSSIBLE CRACK. INSTALLED RH AFT DRAG ANGLE (PN:AV670-21186-004) IAW CRJ 900 SRM 51-42-22-001-001-A01, 51-42-21-001-001-A01, AND 51-42-13-001-001-A01.
- [SDR REXA2024061400433](https://openairdocs.org/sdr/REXA2024061400433.md): Drag Angle · cracked · Mar 11, 2024 · N181GJ · Cndair CL6002D24 · Vertical Stabilizer
  > LH FWD VERTICAL DRAG HAS A POSSIBLE CRACK REPAIRED LH FWD DRAG ANGLE IAW CRJ-900 SRM 55-31-00-201-001-A01.
- [SDR REXA2024032500305](https://openairdocs.org/sdr/REXA2024032500305.md): Angle · cracked · Mar 11, 2024 · N181GJ · Cndair CL6002D24 · Passenger/Crew Doors
  > AFT STEP PANEL. CRACKS AT RIVET. MARKED WITH ORANGE TAPE. NEXT TO PULLEY BRACKET. REMOVED, LOCATED, DRILLED AND INSTALLED SERVICEABLE PAX DOOR AFT DRAG ANGLE, P/N 601R31772-5, IAW CRJ 900 SRM 51-40-11-001-001-A041 AND 51-42-06-001-001-A01UPON FURTHER INVESTIG
- [SDR REXA2020100700680](https://openairdocs.org/sdr/REXA2020100700680.md): Angle · corroded · Sep 29, 2020 · N181GJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > PASSENGER DOOR LOWER SILL ANGLE IS CORRODED AT FS 333.00. REMOVED PAX DOOR LOWER SILL ANGLE THAT WAS CORRODED AT FS 333.00, IAW CRJ 900 SRM 51-42-00-001-001-A01 AND 51-42-21-001-001-A01 AND INSTALLED NEW SERVICEABLE PAX DOOR LOWER SILL ANGLE AT FS 333.00 P/N:
- [SDR REXA2020100700679](https://openairdocs.org/sdr/REXA2020100700679.md): Doubler · corroded · Sep 29, 2020 · N181GJ · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > TCAS DOUBLER IS CORRODED. REMOVED AND REPLACED TCAS DOUBLER, IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
- [SDR REXA2020100700688](https://openairdocs.org/sdr/REXA2020100700688.md): Seat Track · corroded · Sep 28, 2020 · N181GJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > PAX FLOOR SEAT TRACK BETWEEN FS 661+32 AND FS 672.00 LBL 9 IS CORRODED. REMOVED, FABBED, AND INSTALLED SEAT TRACK, IAW BOMBARDIER REO 670-53-00-343 AND AMM 53-00-49-000/400-801-A13.
- [SDR REXA2020100700685](https://openairdocs.org/sdr/REXA2020100700685.md): Seat Track · corroded · Sep 28, 2020 · N181GJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > FLOOR SEAT TRACK CORRODED AT RBL 9 BETWEEN FS 847+51 TO FS 977. FABBED AND INSTALLED NEW SEAT TRACK, IAW BOMBARDIER REO 670-53-343 AND CRJ 900 AMM 53-00-49-000/400-801-A13.
- [SDR REXA2020100700682](https://openairdocs.org/sdr/REXA2020100700682.md): Seat Track · corroded · Sep 27, 2020 · N181GJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN FLOOR SEAT RAIL AT LBL 9 IS CORRODED BETWEEN FS 409 & FS 485.00. REMOVED CORRODED CABIN FLOOR SEAT RAIL AT LBL 9 BETWEEN FS 409 TO FS485. FABRICATED, LOCATED, DRILLED & INSTALLED A NEW SERVICEABLE SEAT RAIL FROM P/N N126-2075, IAW CRJ 900 SRM 53-00
- [SDR REXA2020100700681](https://openairdocs.org/sdr/REXA2020100700681.md): Seat Track · corroded · Sep 27, 2020 · N181GJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN FLOOR SEAT RAIL AT RBL 9 IS CORRODED FS 349.00 TO FS 485.00. REMOVED CORRODED CABIN FLOOR SEAT RAIL AT RBL 9 BETWEEN FS 349 TO FS 485. FABRICATED, LOCATED, DRILLED AND REINSTALLED A NEW SERVICEABLE SEAT RAIL FROM P/N N126-2075, IAW CRJ 900 SRM 53-00-4
- [SDR REXA2020100700691](https://openairdocs.org/sdr/REXA2020100700691.md): Seat Track · corroded · Sep 24, 2020 · N181GJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > PAX FLOOR SEAT TRACK BETWEEN FS 485.00 AND FS 581 RBL 9 IS CORRODED. FABRICATED SEAT TRACK P/N: SH690-33407-1 FROM EXT 20276-288-0-0A, IAW MHIRJ REO 670-53-00-589 REV A DATED 2020-07-14. REPAIR B REWORKED AND INSTALLED NEW FABRICATED SEAT TRACK, IAW MHIRJ R
- [SDR REXA2020100700690](https://openairdocs.org/sdr/REXA2020100700690.md): Seat Track · corroded · Sep 23, 2020 · N181GJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > PAX FLOOR SEAT TRACK BETWEEN FS 581.00 AND FS 661+32 LBL 9 IS CORRODED. FABBED SEAT TRACK AND INSTALLED, IAW BOMBARDIER GREO 670-53-00-589..
- [SDR REXA2020100400689](https://openairdocs.org/sdr/REXA2020100400689.md): Seat Track · corroded · Sep 23, 2020 · N181GJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > PAX FLOOR SEAT TRACK BETWEEN FS 581.00 AND FS 661+32 RBL 9 IS CORRODED. FABBED SEAT TRACK AND INSTALLED, IAW BOMBARDIER GREO 670-53-00-589.
- [SDR REXA2020100700687](https://openairdocs.org/sdr/REXA2020100700687.md): Seat Track · corroded · Sep 22, 2020 · N181GJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > PAX FLOOR SEAT TRACK BETWEEN FS 661+32 & FS 672.00 RBL 9 IS CORRODED. FABBED AND INSTALLED NEW SEAT TRACK, IAW BOMBARDIER REO 670-53-00-343.
- [SDR REXA2020100700686](https://openairdocs.org/sdr/REXA2020100700686.md): Seat Track · corroded · Sep 22, 2020 · N181GJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > FLOOR SEAT TRACK CORRODED AT LBL 9 BETWEEN FS 847+51 AND FS 977. FAB NEW SEAT TRACK AND INSTALLED, IAW BOMBARDIER GREO 670-53-00-343.
- [SDR REXA2020100700684](https://openairdocs.org/sdr/REXA2020100700684.md): Seat Track · corroded · Sep 22, 2020 · N181GJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > FLOOR SEAT TRACK AT RBL 9 CORRODED BETWEEN FS 672 TO FS 836.50. FABRICATED SEAT TRACK P/N BA690-41125-26 FROM EXT, MATERIAL 20276-288-0-0A PO W5158, IAW MHIRJ REO 690-53-00-445 REV DATED 2020-09-14. REMOVED, INSTALLED, & FABRICATED TRACK AT RBL 9 BETWEEN FS
- [SDR REXA2020100700678](https://openairdocs.org/sdr/REXA2020100700678.md): Plate · damaged · Sep 21, 2020 · N181GJ · Cndair CL6002D24 · Fuselage Main, Structure
  > FWD CARGO CEILING ANCHORING BRACKET FOR PANEL 151KLC HAS HOLES DRILLED INTO IT AT FS 501 AND APPROXIMATELY LBL 18. REPAIRED DAMAGE IN CROSSBEAM AT FS 501 LBL 18, IAW ENDEAVOR AIR EA CRJ 953-10861 REV A DATED 09/14/20. REPLACED 2 EA ANCHORING BRACKETS FOR PAN
- [SDR REXA2020100700693](https://openairdocs.org/sdr/REXA2020100700693.md): Crossbeam · damaged · Sep 18, 2020 · N181GJ · Cndair CL6002D24 · Fuselage Main, Structure
  > DAMAGE FOUND IN CROSS BEAM BETWEEN LBL 9 & LBL 27 AT FS 469. DAMAGE FOUND IN CROSS BEAM BETWEEN LBL 9 & LBL 27 AT FS 469. ENDEAVOR AIR EA CRJ953-10837 REV IR DATED 09/15/20. FABRICATED AND INSTALLED A NEW NUTPLATE STRAP, IAW CRJ 900 SRM 51-42-06-001-001-A01
- [SDR REXA2020100700695](https://openairdocs.org/sdr/REXA2020100700695.md): Angle · cracked · Sep 16, 2020 · N181GJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FOUND INDICATION ON RT OUTBOARD ANGLE FS 280 APPROXIMATELY.625 LONG 100% FSA AT RADIUS FAILS NDT. LOCATED, DRILLED, AND INSTALLED NEW SERVICEABLE ANGLE P/N CC670-34269- 4S AT FS 280 RBL 9 OUTBOARD SIDE, IAW CRJ 900 SRM 51-40-11-001-001-A01 AND 51-42-21-001-0
- [SDR REXA2020100700694](https://openairdocs.org/sdr/REXA2020100700694.md): Drain · corroded · Sep 16, 2020 · N181GJ · Cndair CL6002D24 · Fuselage Main, Structure
  > INTERCOSTAL CORRODED AT STR 21L BETWEEN FS 319.70 AND FS 333.00. REMOVED 1EA CORRODED BACK UP SILL. LOCATED, DRILLED, AND INSTALLED 1EA NEW BAUR UP SILL P/N SH670-31822-1, IAW CRJ 900 SRM 51-40-06-001-001- A01, 51-40-11-001-001-A01, 51-42-21-001-001-A01, AND
- [SDR REXA2020100700692](https://openairdocs.org/sdr/REXA2020100700692.md): Seat Track · corroded · Sep 16, 2020 · N181GJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > RT SIDE SEAT RAIL LOCATED BETWEEN FS 785-FS 847+16 HAS MULTIPLE AREAS OF CORROSION. REMOVED AND REPLACED RT SIDE SEAT RAIL FS 785-FS 847+16, IAW CRJ 900 SRM 51-41-02-001-001-A01 AND AMM 20-21-00-00-910-801 AND AMM 53-00-49-600-801-A07.
- [SDR REXA2020100700683](https://openairdocs.org/sdr/REXA2020100700683.md): Stiffener · cracked · Sep 16, 2020 · N181GJ · Cndair CL6002D24 · Fuselage Main, Attach Fittings
  > PAX DOOR ASSIST MOTOR LOWER BRACKET CRACKED. REMOVED CRACKED BRACKET LOCATED, DRILLED & INSTALLED 1 EA NEW PAX DOOR ASSIST MOTOR LOWER BRACKET, IAW CRJ 900 SRM 51-40-06-001-001-A01, 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-13-001-001-A01, P/N 601R317
- [SDR REXA2020073100606](https://openairdocs.org/sdr/REXA2020073100606.md): Resistor · inoperative · Jul 27, 2020 · N181GJ · Cndair CL6002D24 · Emergency Lighting
  > LH OVERWING FWD EMERGENCY LIGHT INOPERATIVE. R & R THE DIODE/RESISTOR IAW CMM 25-28-62 AND WM 91-11-00. OPS CHECKED GOOD.
- [SDR N6WA20191206402](https://openairdocs.org/sdr/N6WA20191206402.md): Pressure Switch · failed · Dec 4, 2019 · N181GJ · Cndair CL6002D24 · Hydraulic System, Main
  > NW STEERING INOP ON T/O FROM EWR. R/R # 3 HYDRAULIC SYSTEM PUMP PRESSURE SWITCH MT 129 IAW CRJ 900 AMM 29-34-01 PERFORMED OPS CHECK OF NOSEWHEEL STEERING SYSTEM IAW CRJ 900 AMM 32-51-00 OPS CHECK GOOD P/N ON/OFF 967008-1 S/N OFF 5274 S/N ON HYD13250
- [SDR N6WA20191206401](https://openairdocs.org/sdr/N6WA20191206401.md): Warning Message · illuminated · Dec 4, 2019 · N181GJ · Cndair CL6002D24 · Landing Gear Steering System
  > NW STEERING INOP ON T/O FROM STL. RESET SYS IAW CRJ 900AMM 32-51-00 NO DEFECTS NOTED AT THIS TIME.

Next page: https://openairdocs.org/aircraft/N181GJ/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 = 'N181GJ' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N181GJ/reports

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