# Service difficulty reports: N183GJ

A list on [N183GJ](https://openairdocs.org/aircraft/N183GJ.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 · 80 reports

- [SDR REXA2025082600838](https://openairdocs.org/sdr/REXA2025082600838.md): Charger · inoperative · Aug 23, 2025 · N183GJ · Cndair CL6002D24 · Emergency Lighting
  > EMERGENCY LIGHTS ON WITH THE SWITCH IN THE OFF POSITION R/R EMERGENCY LIGHT SWITCH IAW CRJ900 ESPM 20-45-51. FAILED OPS CHECK OF EMERGENCY LIGHT SWITCH. R/R EMERGENCY LIGHTS POWER SENSE RELAY IAW CRJ900 ANN 33-51-19 FAILED OPS CHECK. R/R EMERGENCY BATT ASSYS
- [SDR REXA2025052900627](https://openairdocs.org/sdr/REXA2025052900627.md): Battery Pack · inoperative · May 28, 2025 · N183GJ · Cndair CL6002D24 · Emergency Lighting
  > DURING L/C FOUND PS37 BATTERY INOP AND EMER LIGHTS WONT TURN ON R/R PS37 IAW AMM 33-51-17 OPS CKS GOOD.
- [SDR REXA2025052900626](https://openairdocs.org/sdr/REXA2025052900626.md): Charger · inoperative · May 28, 2025 · N183GJ · Cndair CL6002D24 · Emergency Lighting
  > EMERGENCY EXIT LIGHTS STAYS ON WHILE SWITCH IS IN THE OFF POSITION AND COMES OFF IN THE ARM POSITION. R/R PS35 BATTERY CHARGER IAW AMM 33-51-17 OPS CHECK GOOD. NO FURTHER DEFECTS NOTED.
- [SDR REXA2025052100592](https://openairdocs.org/sdr/REXA2025052100592.md): Sign · inoperative · May 17, 2025 · N183GJ · Cndair CL6002D24 · Emergency Lighting
  > OVERWING CEILING EMERGENCY LOCATING SIGN FACING AFT IS INOP RECHARGED EMERGENCY LIGHTS BATTERIES IAW CMM 26-60-03. OPS CHECKS GOOD IAW AMM 33-51-00.
- [SDR REXA2025042400473](https://openairdocs.org/sdr/REXA2025042400473.md): Latch · inoperative · Apr 19, 2025 · N183GJ · Cndair CL6002D24 · Passenger/Crew Doors
  > PASSENGER DOOR JAMMED, WOULD NOT OPEN. R/R PASSENGER DOOR (OUTER) DOOR LATCH SPIGOT ASSY IAW AMM 53-21-23. OPS CHECK GOOD
- [SDR REXA2025032800363](https://openairdocs.org/sdr/REXA2025032800363.md): Charger · inoperative · Mar 27, 2025 · N183GJ · Cndair CL6002D24 · Emergency Lighting
  > DURING WAKE-UP FOUND PAX DOOR EXTERIOR EMERGENCY LIGHT INOP, & OVERHEAD LH & RH GALLEY EXIT SIGN INOP. FOUND 0 VOLTS PRESENT ON PLUG P336 PINS 1 & 2 ON CEILING PANEL. REMOVED & REPLACED BATTERY CHARGER ASSY IN PS35 POSITION IAW 900 AMM 33-51-17. P/N ON/OFF:
- [SDR REXA2025032400351](https://openairdocs.org/sdr/REXA2025032400351.md): Battery Pack · inoperative · Mar 23, 2025 · N183GJ · Cndair CL6002D24 · Emergency Lighting
  > DURING LINE CHECK FOUND FWD EMERGENCY EXIT SIGN ON DIVIDER INOP. R/R PS35 BATTERY AND BATTERY CHARGER IAW J.C 33-900-701. OPS CHECK GOOD. A/C OK FOR SVC.
- [SDR REXA2025030600284](https://openairdocs.org/sdr/REXA2025030600284.md): Hinge · cracked · Mar 3, 2025 · N183GJ · Cndair CL6002D24 · Fuselage, Door Hinge
  > CRACK ON AFT HINGE OF FLAP STEP PLATE AT AFT BAGGAGE BAY DOOR CUTOUT AFT HINGE OF FLAP STEP PLATE AT AFT BAGGAGE BAY DOOR CUTOUT WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01
- [SDR REXA2025030600283](https://openairdocs.org/sdr/REXA2025030600283.md): Hinge · cracked · Mar 3, 2025 · N183GJ · Cndair CL6002D24 · Fuselage, Door Hinge
  > CRACK ON MIDDLE HINGE OF FLAP STEP PLATE AT AFT BAGGAGE BAY DOOR CUTOUT MID HINGE OF FLAP STEP PLATE AT AFT BAGGAGE BAY DOOR CUTOUT WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01
- [SDR REXA2025030600282](https://openairdocs.org/sdr/REXA2025030600282.md): Stop · cracked · Mar 3, 2025 · N183GJ · Cndair CL6002D24 · Cargo/Baggage Doors
  > CRACK ON FWD STOPPER OF FLAP STEP PLATE AT AFT BAGGAGE BAY DOOR CUTOUT FWD STOPPER OF FLAP STEP PLATE AT AFT BAGGAGE BAY DOOR CUTOUT WAS REPLACED PER CRJ900 AMM 53-62-34 (CONFIG A01)
- [SDR REXA2025030600281](https://openairdocs.org/sdr/REXA2025030600281.md): Hinge · cracked · Mar 3, 2025 · N183GJ · Cndair CL6002D24 · Fuselage, Door Hinge
  > CRACK ON FWD HINGE OF FLAP STEP PLATE AT AFT BAGGAGE BAY DOOR CUTOUT FWD HINGE OF FLAP STEP PLATE AT AFT BAGGAGE BAY DOOR CUTOUT WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01
- [SDR REXA2025030600280](https://openairdocs.org/sdr/REXA2025030600280.md): Stop · cracked · Mar 3, 2025 · N183GJ · Cndair CL6002D24 · Cargo/Baggage Doors
  > CRACK ON AFT STOPPERS OF FLAP STEP PLATE AT AFT BAGGAGE BAY DOOR CUTOUT AFT STOPPER OF FLAP STEP PLATE AT AFT BAGGAGE BAY DOOR CUTOUT WAS REPLACED PER CRJ900 AMM 53-62-34 (CONFIG A01)
- [SDR REXA2025030300251](https://openairdocs.org/sdr/REXA2025030300251.md): Bracket · corroded · Mar 3, 2025 · N183GJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON LIGHT BRACKET (ON FUSELAGE SKIN) AT WATER WASTE PANEL LIGHT BRACKET WAS FABRICATED PER EA CRJ953-18254 REV IR AND REPLACED PER CRJ900 AMM 38-31-08 (CONFIG A01)
- [SDR REXA2026072701164](https://openairdocs.org/sdr/REXA2026072701164.md): Support · cracked · Feb 12, 2025 · N183GJ · Cndair CL6002D24 · Fuselage Main, Structure
  > CRACK IN CORNER OF JB6 SUPPORT BASE IN FWD EQUIPMENT COMPARTMENT. JB6 SUPPORT BASE IN FWD EQUIPMENT COMPARTMENT WAS REPLACED PER SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01
- [SDR REXA2025030600278](https://openairdocs.org/sdr/REXA2025030600278.md): Drag Angle · cracked · Feb 11, 2025 · N183GJ · Cndair CL6002D24 · Vertical Stabilizer Miscellaneous Structure
  > CRACK ON RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD DRAG ANGLE 67.5% REAR SPAR DATUM. RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD DRAG ANGLE 67.5% REAR SPAR DATUM WAS REPAIRED PER CRJ-900 SRM 55-31-00-201-001-A01
- [SDR REXA2025030300250](https://openairdocs.org/sdr/REXA2025030300250.md): Angle · corroded · Feb 11, 2025 · N183GJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > COROSION ON LOWER SILL ANGLE BTW FS 319.00/FS349.00 COROSION ON LOWER SILL ANGLE BTW FS 319.00/FS349.00 WAS EVALUATED OUT LIMITS PER CRJ-900 SRM 53-21-23-101-002-A01 THEREFORE WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-34-001-001-A01
- [SDR REXA2026072701169](https://openairdocs.org/sdr/REXA2026072701169.md): Lug · corroded · Feb 6, 2025 · N183GJ · Cndair CL6002D24 · Wing, Control Surface Attach Fittings
  > CORROSION WAS FOUND ON LUGS BORES R1, R2, R5 AND R6 AT RH AILERON CENTER FITTING AND ON LOWER LUG BORE AT RH AILERON OUTBOARD FITTING LUGS BORES R1, R2, R5 & R6 AT RH AILERON CENTER FITTING WERE REPAIRED PER REO 670-57-61-237 REV - - AND LWR LUG BORE OUTBD FIT
- [SDR REXA2026072701165](https://openairdocs.org/sdr/REXA2026072701165.md): Lug · corroded · Feb 6, 2025 · N183GJ · Cndair CL6002D24 · Wing, Control Surface Attach Fittings
  > CORROSION ON INB LUGS AT AILERON HINGE NO.4 AND HINGE NO.1 ON REAR SPAR RH WING INB LUGS AT AILERON HINGE NO.4 WAS CLEANED PER CRJ 900 SRM TASK 51-26-00-001-001-A01 AND GVI WAS PERFORMED PER CRJ900 SRM 51-11-00-001-001-A01 AND NOT DAMAGE FOUND AND HINGE NO.1 O
- [SDR REXA2025030600274](https://openairdocs.org/sdr/REXA2025030600274.md): Angle · corroded · Feb 4, 2025 · N183GJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > DURING SILL REMOVAL IN REF NRC 093, CORROSION ON ANGLE MID CAP WAS FOUND CORROSION ON ANGLE MID CAP WAS EVALUATED OUT LIMITS PER CRJ-900 SRM 53-21-23-101-002-A02 THEREFORE WAS REPLACED ON NRC 0093
- [SDR REXA2025030600273](https://openairdocs.org/sdr/REXA2025030600273.md): Seat Track · corroded · Feb 3, 2025 · N183GJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON PASSENGER SEAT RAILS RBL9 AND LBL9 BTW FS 661.00+90 AND 693.00 AT PASSENGER CABIN. DUE TO EXCESIVE CORROSION AT SEAT TRACK 9RBL AND 9LBL OF FS 661 TO FS 693 AT PASSENGER CABIN WERE REPLACED PER CRJ-900 SRM53-21-49-101-001-A01 AND CRJ-900 AMM 53-00
- [SDR REXA2025030600272](https://openairdocs.org/sdr/REXA2025030600272.md): Beam · corroded · Feb 3, 2025 · N183GJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON UPPER FACE AT TRANSVERSE BEAM FS 333.00 BTW LBL 9 TO LBL 27 UPPER FACE AT TRANSVERSE BEAM FS 333.00 BTW LBL 9 TO LBL 27 WAS REPAIRED PER REO 690-53-21-1887 REV --
- [SDR REXA2025030600271](https://openairdocs.org/sdr/REXA2025030600271.md): Seat Track · corroded · Feb 2, 2025 · N183GJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RH/LH SEAT TRACK FS349-FS379 9RBL AND FS374-FS384 9LBL AT PASSENGER CABIN CORROSION AT SEAT TRACK FS349-FS484 9RBL AND FS- 374-FS485 9LBL AT PASSENGER CABIN WAS EVALUATED OUT LIMITS PER CRJ-900 SRM 53-21-49-101-001-A01, THEREFORE WERE REPLACED PER
- [SDR REXA2026072701141](https://openairdocs.org/sdr/REXA2026072701141.md): Strap · corroded · Feb 1, 2025 · N183GJ · Cndair CL6002D24 · Fuselage Main, Structure
  > CORROSION ON FRAME STRAP AT FS 319.00 OF THE SERVICE DOOR SURROUND STRUCTURE. CORROSION ON FRAME STRAP AT FS 319.00 OF THE SERVICE DOOR SURROUND STRUCTURE WAS EVALUATED OUT LIMITS PER CRJ-900 SRM 51-10-06-001-001-A01 THEREFORE WAS REPLACED PER CRJ-900 SRM 51-
- [SDR REXA2026072801168](https://openairdocs.org/sdr/REXA2026072801168.md): Transcowl · corroded · Jan 31, 2025 · N183GJ · Cndair CL6002D24 · Engine Thrust Reverser
  > CORROSION ON INBD SLIDER AT RT ENGINE LOWER AND UPPER TRANSCOWL. DUE TO NOT ALLOWABLE DAMAGE ON INBD SLIDER AT RT ENGINE, LOWER TRANSCOWL (P/N: CN624-2001-011 S/N: SB1009) AND UPPER TRANSCOWL (P/N: CN624-2001-012 S/N: SB1006) WERE REPLACED BY RT SERVICIABLE LO
- [SDR REXA2026072801167](https://openairdocs.org/sdr/REXA2026072801167.md): Transcowl · corroded · Jan 31, 2025 · N183GJ · Cndair CL6002D24 · Engine Thrust Reverser
  > CORROSION ON INBOARD SLIDER AT RH ENGINE LOWER AND UPPER TRANSCOWL. DUE TO NOT ALLOWABLE DAMAGE ON INBOARD SLIDER AT RH ENGINE, LOWER TRANSCOWL (P/N: CN624-2001-011 S/N: SB1009) AND UPPER TRANSCOWL (P/N: CN624-2001-012 S/N: SB1006) WERE REPLACED BY RH SERVICIA
- [SDR REXA2025030600270](https://openairdocs.org/sdr/REXA2025030600270.md): Drag Angle · cracked · Jan 31, 2025 · N183GJ · Cndair CL6002D24 · Vertical Stabilizer Miscellaneous Structure
  > CRACK ON RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 61.56% STRG DATUM TO 67.5% REAR SPAR DATUM RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 61.56% STRG DATUM TO 67.5% REAR SPAR DATUMWAS REPAIRED PER CRJ-900 SRM 55-31-0
- [SDR REXA2025030600269](https://openairdocs.org/sdr/REXA2025030600269.md): Angle · cracked · Jan 31, 2025 · N183GJ · Cndair CL6002D24 · Vertical Stabilizer
  > CRACK ON LH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 61.56% STRG DATUM TO 67.5% REAR SPAR DATUM LH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 61.56% STRG DATUM TO 67.5% REAR SPAR DATUM WAS REPAIRED PER CRJ-900 SRM 55-31
- [SDR REXA2025030600268](https://openairdocs.org/sdr/REXA2025030600268.md): Diaphragm · cracked · Jan 31, 2025 · N183GJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK IN LH FAIRING SUPPORT DIAPHRAGM IN STA. FS= 797 TO FS= 807 AND 35RBL/LBL AT LH MLG WHEEL WELL. LH FAIRING SUPPORT DIAPHRAGM IN STA. FS= 797 TO FS= 807 AND 35RBL/LBL AT LH MLG WHEEL WELL WERE REPLACED PER CRJ900 SRM 51-41-02-001-001-A01
- [SDR REXA2025030600267](https://openairdocs.org/sdr/REXA2025030600267.md): Diaphragm · cracked · Jan 31, 2025 · N183GJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK IN RH FAIRING SUPPORT DIAPHRAGM IN STA. FS= 797 TO FS= 807 AND 35RBL/LBL AT RH MLG WHEEL WELL. RH FAIRING SUPPORT DIAPHRAGM IN STA. FS= 797 TO FS= 807 AND 35RBL/LBL AT RH MLG WHEEL WELL WERE REPLACED PER CRJ900 SRM 51-41-02-001-001-A01
- [SDR REXA2025030600266](https://openairdocs.org/sdr/REXA2025030600266.md): Fairing · corroded · Jan 31, 2025 · N183GJ · Cndair CL6002D24 · Aerodynamic Fairings
  > CORROSION ON SETTLEMENT AREA OF THE WING TO FUSELAGE FAIRING 195AL, 195DL, 196AR AND 196DR. CORROSION ON SETTLEMENT AREA OF THE WING TO FUSELAGE FAIRING 195AL, 195DL, 196AR AND 196DR WAS EVALUATED WITHIN LIMITS PER CRJ-900 SRM 53-00-01-101-001 AND SRM 53-51-01
- [SDR REXA2025030600265](https://openairdocs.org/sdr/REXA2025030600265.md): Door Sill · corroded · Jan 31, 2025 · N183GJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON LOWER SILL AT SERVICE DOOR EXTERNAL SURROUND STRUCTURE. CORROSION ON LOWER SILL AT SERVICE DOOR EXTERNAL SURROUND STRUCTURE WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01 AND WAS EVALUATED OUT LIMITS PER CRJ-900 SRM 53-21-23-101-002-A02 THEREFO
- [SDR REXA2025030600264](https://openairdocs.org/sdr/REXA2025030600264.md): Stiffener · cracked · Jan 31, 2025 · N183GJ · Cndair CL6002D24 · Leading Edge Devices
  > AFTER REMOVAL OF ACCESS PANEL 621AT CRACK WAS FOUND ON SUPPORT BRACKET CRACK ON STIFFENER SS 21.50 WAS REPAIRED PER CRJ 900 SRM 51-71-59-001-001-A01
- [SDR REXA2025030600263](https://openairdocs.org/sdr/REXA2025030600263.md): Door Sill · corroded · Jan 31, 2025 · N183GJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON LOWER SILL AT PASSENGER DOOR SURROUND STRUCTURE. LOWER SILL AT PASSENGER DOOR SURROUND STRUCTURE WAS REPLACED PER CRJ900 SRM 51-42-21-001-001-A01
- [SDR REXA2025030600262](https://openairdocs.org/sdr/REXA2025030600262.md): Structure · corroded · Jan 30, 2025 · N183GJ · Cndair CL6002D24 · Static Discharge System
  > IN REF TO: DURING INSPECTION OF THE TASK CARD 900-57-900-300 IT WAS DETECTED CORROSION ON STATIC DISCHARGE BASE (4EAS) BTW AILERON AND WING EXTENSION TRAILING EDGE WS370.25 TO WS398.939 AFT OF THE REAR SPAR AT LH/RH WING. CORROSION ON STATIC DISCHARGE BASE (4E
- [SDR REXA2025030600261](https://openairdocs.org/sdr/REXA2025030600261.md): Structure · corroded · Jan 30, 2025 · N183GJ · Cndair CL6002D24 · Static Discharge System
  > IN REF TO: DURING INSPECTION OF THE TASK CARD 900-57-900-300 IT WAS DETECTED CORROSION ON STATIC DISCHARGE BASE (4EAS) BTW AILERON AND WING EXTENSION TRAILING EDGE WS370.25 TO WS398.939 AFT OF THE REAR SPAR AT LH/RH WING. CORROSION ON STATIC DISCHARGE BASE (4E
- [SDR REXA2025012200071](https://openairdocs.org/sdr/REXA2025012200071.md): Lamp · inoperative · Jan 22, 2025 · N183GJ · Cndair CL6002D24 · Emergency Lighting
  > EMERGENCY LIGHT AFT OF PAX DOOR INOP R/R EMERGENCY LIGHT AFT OF PAX DOOR IN REF AMM 33-51-15 P/N ON/OFF: 8GH002473-08
- [SDR REXA2024120901565](https://openairdocs.org/sdr/REXA2024120901565.md): Charger · inoperative · Dec 8, 2024 · N183GJ · Cndair CL6002D24 · Emergency Lighting
  > EMER. LTS IN LOWER FWD GALLEY AND ENTRANCE COMPARTMENT INOP. REMOVED AND REPLACED CHARGER ASSY, BATTERY PER AMM 33-51-17. ALL CHECKS GOOD. P/N OFF/ON 11-0049 S/N OFF 26323 S/N ON 26250
- [SDR REXA2024103001209](https://openairdocs.org/sdr/REXA2024103001209.md): Seat Track · corroded · Jun 11, 2024 · N183GJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK RBL 9 FS 693- 837 IS CORRODED WITH CORRODED HARDWARE THROUGHOUT. REMOVED AND REPLACED IAW CRJ-900 SRM 53-00-49-201-002-A01.
- [SDR REXA2024062400474](https://openairdocs.org/sdr/REXA2024062400474.md): Seat Track · corroded · Jun 11, 2024 · N183GJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK LBL 9 FS 693- 837 IS CORRODED WITH CORRODED HARDWARE THROUGHOUT. REMOVED AND REPLACED IAW CRJ-900 SRM 53-00-49-201-002-A01.
- [SDR REXA20240701487](https://openairdocs.org/sdr/REXA20240701487.md): Frame · cracked · Jun 10, 2024 · N183GJ · Cndair CL6002D24 · Emergency Exits
  > R/H AFT EMERGENCY EXIT DOOR HAS A VISIBLE CRACK ABOVE AFT UPPER DUG LUG, PN# SH670-36600 SN# SB0863 REPAIRED RH AFT EMERGENCY EXIT IAW ENDEAVOR AIR EA CRJ952-16767 REV IR DATED 6/13/2024, REF, ENDEAVOR AIR DTA # 916531,
- [SDR REXA20240701486](https://openairdocs.org/sdr/REXA20240701486.md): Door · cracked · Jun 10, 2024 · N183GJ · Cndair CL6002D24 · Emergency Exits
  > L/H AFT EMERGENCY EXIT DOOR HAS A VISIBLE CRACK BELOW AFT UPPER LUG, PN# SH670-36600 SN# SB0862 REPAIRED LH AFT EMERGENCY EXIT IAW ENDEAVOR AIR EA CRJ952-16766 REV IR DATED 6/13/2024, REF, ENDEAVOR AIR DTA # 916532,
- [SDR REXA2021080600550](https://openairdocs.org/sdr/REXA2021080600550.md): Bracket · cracked · Jul 23, 2021 · N183GJ · Cndair CL6002D24 · Cargo Compartment Lighting
  > THE CENTER CARGO COMPARTMENT LIGHT FIXTURE HAS A CRACKED BRACKET - REMOVED AND REPLACED CENTER CARGO COMPARTMENT LIGHT FIXTURE BRACKET IAW CRJ 900 SRM 51-41-02.
- [SDR REXA2021080600548](https://openairdocs.org/sdr/REXA2021080600548.md): Lintel · cracked · Jul 21, 2021 · N183GJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > F.S. 280-295 DOOR LINTEL STR 3L IS CRACKED JUST AFT OF F.S. 280 - REFERANCE EO# R53568 (WILL SUBMIT ADDITIONAL FORM WITH CORRECTIVE ACTION)
- [SDR REXA2021080600547](https://openairdocs.org/sdr/REXA2021080600547.md): Door Frame · nicked · Jul 21, 2021 · N183GJ · Cndair CL6002D24 · Passenger/Crew Doors
  > CENTER BAGGAGE BAY SURROUND LOCK/LATCH RECEIVERS HAVE SMALL KNICKS FROM LATCHES JC: 900-500-810-306 - BLENDED OUT DAMAGE ON LATCH RECEIVERS OF CENTER BAGGAGE BAY SURROUND LOCK IAW CRJ 900 SRM 51-12-00 AND CHECKED LIMITS FOUND TO BE WITHIN LIMITS IAW CRJ 900 SR
- [SDR REXA2021080600540](https://openairdocs.org/sdr/REXA2021080600540.md): Attach Fitting · chafed · Jul 21, 2021 · N183GJ · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR FORWARD LOWER TUBE ATTACHMENT FITTING CHAFFED FORWARD PULLING LEVER - REMOVED AND REPLACED PAX DOOR FWD LWR TUBE ATTACHMENT PULL-IN LEVER FITTING IAW BOMBARDIER CRJ 900 AMM 52-11-02.
- [SDR REXA2021080600537](https://openairdocs.org/sdr/REXA2021080600537.md): Stringer · corroded · Jul 21, 2021 · N183GJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER 25L BETWEEN FS295 AND FS310 IS CORRODED JC:900-53-140-500 - REMOVED & REPLACED STGR 25L BTW FS 280 TO FS 333 IAW CRJ 900 SRM 51-42-06- &51-42-20
- [SDR REXA2021080600536](https://openairdocs.org/sdr/REXA2021080600536.md): Stringer Splice · corroded · Jul 21, 2021 · N183GJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER SPLICE AT 26L AT FS333 IS CORRODED JC: 900-53-140-500 - REMOVED & REPLACED STGR SPLICE @ 26L @ FS333 IAW CRJ900 SRM 51-42-06
- [SDR REXA2021080600535](https://openairdocs.org/sdr/REXA2021080600535.md): Stringer Splice · corroded · Jul 21, 2021 · N183GJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER SPLICE @25L @FS333 IS CORRODED JC: 900-53-140-500 - REMOVED @ REPLACED STRG SPLICE @25L @FS333 IAW CRJ900 SRM 51-42-06.
- [SDR REXA2021080600533](https://openairdocs.org/sdr/REXA2021080600533.md): Intercostal · corroded · Jul 14, 2021 · N183GJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INTERCOSTAL RIGHT OF STRINGER 27 BETWEEN FS.349 AND FS364 HAS CORROSION IOB CODE:900-53-140-500 - REMOVED & REPLACED RIGHT INTERCOSTAL OF STRINGER 27 BETWEEN FS349 & FS 364 IAW CRJ900 SRM51.42.06 & SRM51.42.20.
- [SDR REXA2021080600542](https://openairdocs.org/sdr/REXA2021080600542.md): Housing · cracked · Jul 13, 2021 · N183GJ · Cndair CL6002D24 · Electrical/Electronic Compartment Doors
  > AVIONICS BAY DOR HANDLE HOUSING CRACKED, VERIFIED BY NDT JC: 900-52-810-901 - REPLACED AVIONICS BAY DOOR HANDLE HOUSING IAW CRJ900 SRM 51-42-00 AND CRJ900 AMM 52-42-03

Next page: https://openairdocs.org/aircraft/N183GJ/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 = 'N183GJ' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N183GJ/reports

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