# Service difficulty reports: N931XJ

A list on [N931XJ](https://openairdocs.org/aircraft/N931XJ.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 · 138 reports

- [SDR REXA2024103101323](https://openairdocs.org/sdr/REXA2024103101323.md): None · none · Apr 17, 2024 · N931XJ · Cndair CL6002D24 · Standard Practices/Structures
  > "THE L/H AILERON HAS PREVIOUSLY O/S LUG BORES LABELED ""C"" & ""F"". FABRICATION OF (QTY. #2) O/S BUSHINGS IS REQUIRED. REPAIRED IAW BOMBARDIER REO 670-57-61-237 REV -- DATED 2017-07-25. "
- [SDR REXA2024070800509](https://openairdocs.org/sdr/REXA2024070800509.md): Handle · cracked · Apr 17, 2024 · N931XJ · Cndair CL6002D24 · Emergency Exits
  > CREW ESCAPE HATCH HANDLE HOUSING IS CRACKED. REMOVED AND REPLACED CREW ESCAPE HATCH HANDLE HOUSING (P/N: H3419-35) IAW CRJ900 SM 51-42-06-001-001-A01, 51-40-11-001-001-A01. DISPLACED AND REINSTALLED INSULATION FOR ACCESS IAW CRJ900 AMM 25-81-01-000/400
- [SDR REXA2024103101262](https://openairdocs.org/sdr/REXA2024103101262.md): Intercostal · corroded · Apr 16, 2024 · N931XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR DD6 MID INTERCOSTAL CORRODED. REMOVED PAX DOOR INTERCOSTAL AT DD6IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01, RECEIVED NEW INTERCOSTAL P/N 601R318057-1, LOCATED AND DRILLED AND INSTALLED NEW INTERCOSTAL IAW CRJ SRM 900 51-40-1
- [SDR REXA2024103101322](https://openairdocs.org/sdr/REXA2024103101322.md): Former · corroded · Apr 15, 2024 · N931XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR FWD FORMER IS CORRODED IN SEVERAL AREAS. REPLACED FWD PAX DOOR FORMER P/N 601R318031-5 IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-40-11-001-001-A01 AND 51-42-21-001-001-A01
- [SDR REXA2024103101261](https://openairdocs.org/sdr/REXA2024103101261.md): Former · corroded · Apr 15, 2024 · N931XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR FWD FORMER IS CORRODED IN SEVERAL AREAS. REPLACED FWD PAX DOOR FORMER P/N 601R318031-5 IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-40-11-001-001-A01 AND 51-42-21-001-001-A01
- [SDR REXA2024103101260](https://openairdocs.org/sdr/REXA2024103101260.md): Stringer · corroded · Apr 14, 2024 · N931XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STGR 21R FOUND TO BE CORRODED THROUGH BETWEEN F.S. 364 AND F.S. 379. REPAIRED IAW CRJ900 SRM 53-00-03-201-001-A02.
- [SDR REXA2024042200359](https://openairdocs.org/sdr/REXA2024042200359.md): Stringer · corroded · Apr 14, 2024 · N931XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STGR 21R FOUND TO BE CORRODED THROUGH BETWEEN F.S. 364 AND F.S. 379. REPAIRED IAW CRJ900 SRM 53-00-03-201-001-A02.
- [SDR REXA2024103101321](https://openairdocs.org/sdr/REXA2024103101321.md): Frame · corroded · Apr 13, 2024 · N931XJ · Cndair CL6002D24 · Fuselage Main, Frame
  > FS379 FRAME SEGMENT FROM STR 25R TO STR 21R CORRODED REPLACE FRAME SEGMENT IAW CRJ 900 SRM 51-42-06-001-001-A01.
- [SDR REXA2024103101320](https://openairdocs.org/sdr/REXA2024103101320.md): Stringer Splice · corroded · Apr 10, 2024 · N931XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > "STGR 19R SPLICE IS CORRODED BETWEEN F.S. 677 TO F.S. 669.40. DISPLACED WIRE HARNESS BETWEEN FS 661+90 - FS 693 REMOVED FASTENERS AT AFFECTED LOCATIONS FOR ACCESS IAW CRJ 900 SRM 51-42-06/21-001-001-A01. REMOVED CORROSION FROM FWD SIDE OF STGR 19R SPLICE (P/N
- [SDR REXA2024080500619](https://openairdocs.org/sdr/REXA2024080500619.md): Diaphragm · corroded · Apr 10, 2024 · N931XJ · Cndair CL6002D24 · Fluid Service Doors
  > STRUCTURE INSIDE FWD TOILET SERVICE DOOR IS CORRODED. REMOVED AND REPLACED DIAPHRAGMS AND BRACKET IAW CRJ 900SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.
- [SDR REXA2024070800508](https://openairdocs.org/sdr/REXA2024070800508.md): Floorbeam · corroded · Apr 10, 2024 · N931XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "FOUND RH FS 280 CROSSBEAM TO HAVE CORROSION. REMOVED AND REPLACED RH FS 280 CROSSBEAM PN: CC670-34094-2 IAW CRJ 900 SRM 51-42-06-001-00-A01, 51-42-13-001-001-A01, 51-42-21-001-001-A01, AND 51-42-22-001-001-A01, 51-40-11-001-001-A01. PAINTED RH FS 280 CROS
- [SDR REXA2024070800507](https://openairdocs.org/sdr/REXA2024070800507.md): Floorbeam · corroded · Apr 10, 2024 · N931XJ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > FOUND LH FS 280 CROSSBEAM TO HAVE CORROSION. REMOVED AND REPLACED LH FS 280 CROSSBEAM PN: CC670-34094-1 IAW CRJ 900 SRM 51-42-06-001-00-A01, 51-42-13-001-001-A01, 51-42-21-001-001-A01, AND 51-42-22-001-001-A01, 51-40-11-001-001-A01. PAINTED LH FS 280 CROSS
- [SDR REXA2024103101319](https://openairdocs.org/sdr/REXA2024103101319.md): Fitting · unknown · Feb 14, 2024 · N931XJ · Cndair CL6002D24 · Standard Practices/Structures
  > WHILE PERFORMING SB 670BA-53-044 REV G PART B & C - PRIMARY STRUCTURE FS 144 TO FS 280 - REINFORCEMENT OF THE LH & RH SIDES OF THE FS 202.75 BULKHEAD ABOVE THE FLOOR AND NLG BOX WE FOUND THE R/H STRINGER 12A FITTING CC670-33562-001SB WILL ONLY PICK UP TWO FAST
- [SDR REXA2024032100293](https://openairdocs.org/sdr/REXA2024032100293.md): Lug · cracked · Feb 10, 2024 · N931XJ · Cndair CL6002D24 · Emergency Exits
  > R/H FWD EMERGENCY EXIT UPPER AFT LUG POSIBLE CRACK, REPAIRED IAW MHIRJ REO 690-52-21-155 REV -- DATED 2024-02-15,
- [SDR REXA2024032100292](https://openairdocs.org/sdr/REXA2024032100292.md): Lug · cracked · Feb 10, 2024 · N931XJ · Cndair CL6002D24 · Emergency Exits
  > L/H AFT EMERGENCY EXIT UPPER AFT LUG POSIBLE CRACK, REPAIRED IAW MHIRJ REO 690-52-21-154 REV -.
- [SDR REXA2024021300187](https://openairdocs.org/sdr/REXA2024021300187.md): Wire Harness · inoperative · Feb 1, 2024 · N931XJ · Cndair CL6002D24 · Landing Gear System Wiring
  > AFTER TAKEOFF RECEIVED BRAKE OVHT WARNING INDICATION FOR RIGHT INBOARD BRAKE. RETURNED TO ATL. REMOVED AND REPLACED PROXIMITY SENSOR HARNESS ASSEMBLY IAW AMM 32-61-05. OPS TEST DONE IAW AMM 32-61-00, OPS TEST GOOD. ALSO REMOVED AND REPLACED BRAKE TEMPERATURE S
- [SDR REXA2022120602675](https://openairdocs.org/sdr/REXA2022120602675.md): Battery · inoperative · Dec 5, 2022 · N931XJ · Cndair CL6002D24 · Emergency Lighting
  > FOUND FWD EMERGENCY LIGHTS INOP R&R EPSU BATTERY IAW AMM 33-51-17 OPS CHECK GOOD.
- [SDR REXA2021122701189](https://openairdocs.org/sdr/REXA2021122701189.md): None · inoperative · Dec 27, 2021 · N931XJ · Cndair CL6002D24 · Emergency Lighting
  > EPSU BATTERY CHARGER FAILED OPS CHECK WHEN REPLACING EPSU BATTERY PACK @PS37. R&R EPSU BATTERY CHARGER @PS37. OPS CHECK IS GOOD. IAW AMM 33-51-17 PN ON & OFF: 11-0049. SN ON: 27237 SN OFF: 23106
- [SDR REXA2020113000800](https://openairdocs.org/sdr/REXA2020113000800.md): Wire · pulled · Nov 20, 2020 · N931XJ · Cndair CL6002D24 · Light System Wiring
  > EMERGENCY LIGHT ON RT OVERWING PANEL 172CRJ IS INOPERABLE. INVESTIGATED AND FOUND WIRE PULLED OUT OF CONTACT AT LIGHT. INSTALLED SERVICEABLE CONTACT ON WIRE AND CONNECTED TO EMERGENCY LIGHT ON PANEL 172CR, IAW CRJ 900 ESPM 20-26-00. OPERATIONS TEST GOOD, IA
- [SDR REXA2020113000799](https://openairdocs.org/sdr/REXA2020113000799.md): Skin · dented · Nov 16, 2020 · N931XJ · Cndair CL6002D24 · Rudder, Plate/Skin
  > INTERNAL RUDDER BAYS, BELOW PCU ATTACH POINTS PAINT DISBONDED FROM INTERNAL SURFACES DUE TO SKYDROL EXPOSURE. REPAIRED RUDDER, IAW MHIRJ EO NR CC670-22001-SNIEO-S01, ENDEAVOR AIRLINES EA'S NR CRJ955-10925, CRJ955-10926, CRJ955-10927 AND CRJ955-10928 REV IR DA
- [SDR REXA2020113000798](https://openairdocs.org/sdr/REXA2020113000798.md): Floor Support · corroded · Nov 15, 2020 · N931XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > AFT CARGO LT OUTBOARD FLOOR SILL BETWEEN FS 985.00 TO FS 1000 IS CORRODED IN SEVERAL LOCATIONS, LT SIDE. CW ENDEAVOR AIR EA CRJ953-10919 REV IR DATED 10-28-20 FOR AFT CARGO OUTBOARD FLOOR SILL BETWEEN FS 985.00 TO FS 1000.
- [SDR REXA2020113000797](https://openairdocs.org/sdr/REXA2020113000797.md): Seat Track · corroded · Nov 15, 2020 · N931XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > FLOOR SEAT RAIL AT RBL 9 BEGINNING AT APPROXIMATLEY FS 661.00+32 CORRODED IN 4 LOCATIONS. REMOVED & INSTALLED NEW SEAT TRACK AT FS 661.00+32 RBL 9, IAW REO 670-53-00-342 CRJ 900 SRM 51-40-11, 57-42-02 TASK 51-41-02-001-A01 &CRJ 900 AMM 53-00-17-400-801-A07.
- [SDR REXA2020113000789](https://openairdocs.org/sdr/REXA2020113000789.md): Seat Track · corroded · Nov 12, 2020 · N931XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > FLOOR SEAT RAIL AT LBL 9 BEGINNING AT APPROX FS 693.00 CORRODED IN 3 LOCATIONS. REMOVED, REPLACED AND FABRICATED NEW SEAT TRACK AT LBL 9, FS 693.00-830.40 WITH PART NR 20276-288-0-0A, IAW REO 670-53-00-343 REV N DATED 07/16/19 AND CRJ 900 SRM 51-40-11-001-00
- [SDR REXA2020113000788](https://openairdocs.org/sdr/REXA2020113000788.md): Seat Track · corroded · Nov 12, 2020 · N931XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > FLOOR SEAT TRACK ON LBL 27 BETWEEN FS 409 AND FS 477.40 GOUGED AND CHAFED IN SEVERAL LOCATIONS. DAMAGE EXCEEDS ALLOWABLE LIMITS AT FS 409-FS 477, IAW CRJ 900 SRM 53-21-49-101-001-A01. LOCATED AND DRILLED SEAT TRACK, IAW CRJ 900 SRM 51-40-11-001-001-A01. INS
- [SDR REXA2020113000785](https://openairdocs.org/sdr/REXA2020113000785.md): Intercostal · corroded · Nov 12, 2020 · N931XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > AVIONICS BAY DOOR SURROUND STRUCTURE, FWD INTERCOSTAL BETWEEN FS 349 AND FS 364 AT STGR 27L CORRODED. REMOVED AND INSTALLED NEW INTERCOSTAL AT FS 349-364 AT STR 27L, IAW CRJ 900 SRM 51-42-21-001-001-A01. OPERATIONS CHECK GOOD.
- [SDR REXA2020113000796](https://openairdocs.org/sdr/REXA2020113000796.md): Bracket · corroded · Nov 1, 2020 · N931XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FWD BAGGAGE BAY DOOR SURROUND STRUCTURE MACHINED BRACKET CORRODED AT APPROX FS 565.00 AND LBL 24.0. REMOVED MACHINED BRACKET AT FS 565 STR LBL 24, IAW CRJ 900 SRM 51-42-22-001-001-A01 AND 51-42-21-001-001-A01. LOCATED AND DRILLED SERVICEABLE MACHINED BRACKET
- [SDR REXA2020113000794](https://openairdocs.org/sdr/REXA2020113000794.md): Bracket · corroded · Nov 1, 2020 · N931XJ · Cndair CL6002D24 · Trailing Edge Flaps
  > RT INBOARD FLAP PANEL 684ET IS CHAFED. REPLACED PANEL 684ET, LOCATED HOLES, PER CRJ 900 SRM 51-40-11-001-001-A01.
- [SDR REXA2020113000793](https://openairdocs.org/sdr/REXA2020113000793.md): Plate · corroded · Nov 1, 2020 · N931XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FWD BAGGAGE BAY DOOR PLATE CORRODED AT FS 557 AND LBL 3.4. REPLACED FWD BAGGAGE BAY DOOR PLATE, IAW CRJ900 SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01.
- [SDR REXA2020113000792](https://openairdocs.org/sdr/REXA2020113000792.md): Bracket · corroded · Nov 1, 2020 · N931XJ · Cndair CL6002D24 · Fuselage Main, Attach Fittings
  > FWD BAGGAGE BAY STRUCUTRE, MACHINED BRACKET CORRODED AT LBL 2.6 AND APPROXIMATELY FS 565. REMOVED & REPLACED MACHINED BRACKET, IAW CRJ900 SRM 51-40-11-001-001-A01, 51-42-21-001-001-A01, & 51-42-22-001-001-A01.
- [SDR REXA2020113000791](https://openairdocs.org/sdr/REXA2020113000791.md): Angle · chafed · Oct 31, 2020 · N931XJ · Cndair CL6002D24 · Fuselage Main, Attach Fittings
  > TWO BRACKETS ON AFT CARGO DOOR TRACKS AREA CHAFED AND GOUGED AT FS 985 AND FS 1047. REMOVED AND FABRICATED NEW FWD AND AFT CLIPS ON AFT CARGO DOOR TRACKS, IAW DWG MM670-35514 AND MM 670-35518 AND SRM 51J-42-21-001-010-A01.
- [SDR REXA2020113000790](https://openairdocs.org/sdr/REXA2020113000790.md): Angle · chafed · Oct 31, 2020 · N931XJ · Cndair CL6002D24 · Fuselage Main, Attach Fittings
  > TWO BRACKETS ON AFT CARGO DOOR TRACKS AREA CHAFED AND GOUGED AT FS 985 AND FS 1047. REMOVED AND FABRICATED NEW FWD AND AFT CLIPS ON AFT CARGO DOOR TRACKS, IAW DWG MM670-35514 AND MM 670-35518 AND SRM 51J-42-21-001-010-A01.
- [SDR REXA2020113000787](https://openairdocs.org/sdr/REXA2020113000787.md): Intercostal · corroded · Oct 28, 2020 · N931XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > AVIONICS BAY DOOR SURROUND STRUCTURE, AFT INTERCOSTAL BETWEEN FS 379 AND FS 394 AT STGR 27L CORRODED. DAMAGED INTERCOSTAL BETWEEN FS 394 AND FS 394 STR 27L EXCEEDS ALLOWABLE LIMITS, IAW CRJ 900 SRM 53-21-23-101-003-A02. REMOVED INTERCOSTAL AT STR 27L BETWEE
- [SDR REXA2020113000786](https://openairdocs.org/sdr/REXA2020113000786.md): Intercostal · corroded · Oct 28, 2020 · N931XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > AVIONICS BAY DOOR SURROUND STRUCUTRE, AFT INTERCOSTAL BETWEEN FS 379 AND FS 394 AT STGR 27R. DAMAGED INTERCOSTAL BETWEEN FS 394 AND FS 409 STR 27R EXCEEDS ALLOWABLE LIMITS, IAW CRJ 900 SRM 53-21-23-101-003-A02. LOCATED AND DRILLED NEW INTERCOSTAL AT STR 27R
- [SDR REXA2020113000795](https://openairdocs.org/sdr/REXA2020113000795.md): Angle · corroded · Oct 26, 2020 · N931XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > SERVICE DOOR SEAL ANGLE CORRODED BETWEEN FS 319.70 AND 349 AT WL 72. REPLACED CORRODED SERVICE DOOR SEAL STRIKER, IAW CRJ 900 SRM 51-42-06-001-001-A01.
- [SDR REXA2020113000784](https://openairdocs.org/sdr/REXA2020113000784.md): Seat Track · corroded · Oct 26, 2020 · N931XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > FLOOR SEAT RAIL AT RBL 9 BEGINNING AT APPROXIMATELY FS 581.00 CORRODED IN THREE LOCATIONS. REMOVED SEAT TRACK AT RBL 9 FS 581.00. FABRICATED AND INSTALLED NEW SEAT TRACK, IAW BOMBARDIER REO 670-53-00-343, REV N DATED 7/16/19 AND IAW CRJ 900 AMM 53-00-49-400-
- [SDR REXA2020113000783](https://openairdocs.org/sdr/REXA2020113000783.md): Angle · corroded · Oct 26, 2020 · N931XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FOUND FWD J ANGLE TO BE CORRODED. FWD J CHANNEL FOUND TO BE HEAVILY PITTED AND CORRODED AND REQUIRED REPLACEMENT. REMOVED FWD J CHANNEL, IAW CRJ 900 SRM 51-42-06-001-001-A01. LOCATED AND DRILLED NEW J CHANNEL, IAW CRJ 900 SRM 51-40-11-001-001-A01. INSTALLE
- [SDR REXA2020113000782](https://openairdocs.org/sdr/REXA2020113000782.md): Door Sill · corroded · Oct 21, 2020 · N931XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR LOWER SILL HAS MULTIPLE AREAS OF CORROSION. REMOVED AND INSTALLED NEW LOWER SILL, IAW CRJ 900 SRM 51-42-21-001-001-A01, 51-42-06-001-001-A01, 51-42-13-001-001-A01 AND 51-41-02-001-001- A01.
- [SDR REXA2018071600620](https://openairdocs.org/sdr/REXA2018071600620.md): Stowage Box · broken · Jul 11, 2018 · N931XJ · Cndair CL6002D24 · Crew Oxygen System
  > PILOT OXYGEN MASK QUICK-RELEASE DOOR BROKEN. SWAPPED CA OXYGEN MASK STOWAGE BOX WITH OBSERVER OXYGEN MASK BOX PER A MM 35-11-15. OPS CHECK GOOD. REMOVED AND REPLACED OBSERVERS MASK STOWAGE BOX AND OXYGEN MASK IAW AMM 35-11-15 & 35-11-12. PERFORMED OPERATIONAL
- [SDR REXA2018011500020](https://openairdocs.org/sdr/REXA2018011500020.md): Warning Message · false activation · Jan 15, 2018 · N931XJ · Cndair CL6002D24 · Landing Gear Steering System
  > ON APPROACH WITH GEAR DOWN, RECEIVED A STEERING INOPERATIVE CAUTION MESSAGE. AFTER LANDING PERFORMED RESET PROCEDURE AND TAXIED TO THE GATE. MDC CHECKED IAW FIM 32-51-50-810- 802. NO FAULT REPORTED. OPS TESTED IAW AMM 32-51-00. OPS CHECKED GOOD.
- [SDR REXA2018011100017](https://openairdocs.org/sdr/REXA2018011100017.md): Oxygen Bottle · empty · Jan 11, 2018 · N931XJ · Cndair CL6002D24 · Portable Oxygen System
  > AFT PORTABLE OXYGEN BOTTLE DEPLETED. REMOVED & REPLACED THE OXYGEN BOTTLE IAW 35-31-61.
- [SDR REXA2017120301216](https://openairdocs.org/sdr/REXA2017120301216.md): Flashlight · inoperative · Dec 3, 2017 · N931XJ · Cndair CL6002D24 · Emergency Equipment
  > CAPTAINS SIDE EMERGENCY FLASHLIGHT INOP. REPLACED CAPTAINS SIDE EMER FLASHLIGHT OPS CK GOOD REF AMM 25-61-00.
- [SDR REXA2017113001213](https://openairdocs.org/sdr/REXA2017113001213.md): Battery Pack · inoperative · Nov 30, 2017 · N931XJ · Cndair CL6002D24 · Emergency Lighting
  > LEFT AFT OVERWING EMERGENCY LIGHT INOPERATIVE AND RT FWD OVERWING EMERGENCY LIGHT INOPERATIVE AND CABIN FWD EMERGENCY DOOR LOWER ON BOTH SIDES AND OVERHEAD OVERWING FWD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REMOVED THE PS38 BATTERY PACK IAW JC 33-900-701.
- [SDR REXA2017112101185](https://openairdocs.org/sdr/REXA2017112101185.md): Strap · broken · Nov 21, 2017 · N931XJ · Cndair CL6002D24 · Emergency Equipment
  > AFT FA EMER FLASHLIGHT WIRE BROKEN. REPLACED EMERGENCY AFT FLASHLIGHT STRAP IAW AMM 25-61-02. FLASHLIGHT CHECKS GOOD.
- [SDR REXA2017111201168](https://openairdocs.org/sdr/REXA2017111201168.md): Wire · damaged · Nov 12, 2017 · N931XJ · Cndair CL6002D24 · Light System Wiring
  > EMERGENCY LIGHTS FAILED AN OPS CHECK. REPAIRED A WIRE IAW ESPM 20-44-00. OPS TESTED THE ESPU. CHECKED GOOD IAW AMM 33-51-17-710-801. OPS TESTED THE EMERGENCY LIGHT. CHECKED GOOD IAW AMM 33-51-00-710-802.
- [SDR REXA2017110201173](https://openairdocs.org/sdr/REXA2017110201173.md): Bearing · worn · Nov 2, 2017 · N931XJ · Cndair CL6002D24 · Rudder Structure
  > RUDDER CENTER LOWER HINGE BEARING HAS EXCESSIVE PLAY. REMOVED AND INSTALLED A NEW BEARING IAW CMM 55-41-27, AND SRM 51-42-21.
- [SDR REXA2017110101172](https://openairdocs.org/sdr/REXA2017110101172.md): Skin · chafed · Nov 1, 2017 · N931XJ · Cndair CL6002D24 · Rudder, Plate/Skin
  > LEFT LE OF RUDDER CHAFED ABOVE CENTER HINGE AREA. REMOVED AND REPLACED THE RUDDER SKIN IAW SRM 51-42-06.
- [SDR REXA2017110101141](https://openairdocs.org/sdr/REXA2017110101141.md): Flashlight · damaged · Nov 1, 2017 · N931XJ · Cndair CL6002D24 · Emergency Equipment
  > 3RD F/A FLASHLIGHT ASSY ON FWD FACE IS DAMAGED. REMOVED AND REPLACED 3RD F/A FLASHLIGHT ASSY IAW AMM 25-61-02-400-801-A10.
- [SDR REXA2017103001171](https://openairdocs.org/sdr/REXA2017103001171.md): Skin · dented · Oct 30, 2017 · N931XJ · Cndair CL6002D24 · Trailing Edge Flaps
  > LEFT WING INBD FLAP SKIN IS DENTED ON THE LOWER SURFACE 7 INCHES FROM THE TE EDGE, AND 18 INCHES FROM THE INBD EDGE. REPAIRED THE FLAP SKIN IAW SRM 57-52-01-201-001-A01, TYPE IV.
- [SDR REXA2017103001170](https://openairdocs.org/sdr/REXA2017103001170.md): Skin · dented · Oct 30, 2017 · N931XJ · Cndair CL6002D24 · Trailing Edge Flaps
  > LEFT WING INBD FLAP DENTED ON THE LOWER SURFACE 15 INCHES FROM THE TE EDGE, AND 18 INCHES FROM THE INBD EDGE. REPAIRED THE LEFT FLAP SKIN IAW SRM 57-52-01-201-001-A01, TYPE IV.
- [SDR REXA2017103001169](https://openairdocs.org/sdr/REXA2017103001169.md): Skin · dented · Oct 30, 2017 · N931XJ · Cndair CL6002D24 · Trailing Edge Flaps
  > LEFT WING, INBD FLAP IS DENTED ON LOWER SURFACE 9 INCHES FROM THE OTBD EDGE AND 11INCHES FROM THE TE. REPAIRED THE FLAP SKIN IAW SRM 57-52-01-200-001-A01 TYPE IV.

Next page: https://openairdocs.org/aircraft/N931XJ/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 = 'N931XJ' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N931XJ/reports

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