# Service difficulty reports: N904FJ

A list on [N904FJ](https://openairdocs.org/aircraft/N904FJ.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 7 · 308 reports

- [SDR MASA2022102700251](https://openairdocs.org/sdr/MASA2022102700251.md): Battery Pack · discharged · Oct 27, 2022 · N904FJ · Cndair CL6002D24 · Emergency Equipment
  > MEGAPHONE WILL NOT TEST PROPERLY. R/R BATTERY, OPS CHK GOOD.
- [SDR MASA2022102700250](https://openairdocs.org/sdr/MASA2022102700250.md): Battery Pack · discharged · Oct 27, 2022 · N904FJ · Cndair CL6002D24 · Emergency Equipment
  > AFT FA FLASH LIGHT IS NOT BLINKING. R/R BATTERY, OPS CHK GOOD.
- [SDR MASA2022091900233](https://openairdocs.org/sdr/MASA2022091900233.md): Bulb · inoperative · Sep 19, 2022 · N904FJ · Cndair CL6002D24 · Emergency Lighting
  > ROW 14 D/F MID LVL EXIT SIGN (2) BULBS INOP REPLACED BULBS
- [SDR MASA2022080700205](https://openairdocs.org/sdr/MASA2022080700205.md): None · none · Aug 7, 2022 · N904FJ · Cndair CL6002D24 · Emergency Lighting
  > CEILING LEVEL EMERGENCY FLOOD LIGHT AT ROW 18 INOP. PLACED ON MEL.
- [SDR MASA2022072400197](https://openairdocs.org/sdr/MASA2022072400197.md): None · none · Jul 24, 2022 · N904FJ · Cndair CL6002D24 · Air Conditioning System
  > L PACK ODOR - DEFERRED LH PACK
- [SDR MASA2022060400154](https://openairdocs.org/sdr/MASA2022060400154.md): None · none · Jun 4, 2022 · N904FJ · Cndair CL6002D24 · Emergency Lighting
  > PAX ENTRY SIDEWALL EMER EXIT LIGHT INOP (FLOODLIGHT). PLACED ON MEL.
- [SDR MASA2022051500145](https://openairdocs.org/sdr/MASA2022051500145.md): Bulb · inoperative · May 16, 2022 · N904FJ · Cndair CL6002D24 · Emergency Lighting
  > 13F LWR LVL EXIT SIGN 2 BULBS INOP REPLACED BULBS
- [SDR MASA20220413204](https://openairdocs.org/sdr/MASA20220413204.md): Skin · corroded · Apr 13, 2022 · N904FJ · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN AT STGR 21R AND BETWEEN STA 305 TO 315 WS FOUND TO HAVE CORROSION DAMAGE. PERFORMED PERM REPAIR IAW CRJ900 STRUCTURAL REPAIR MANUAL (SRM) 53-21-01-001-002-A01, FIGURE 53-21.-01-991-802, ITEM 1.
- [SDR MASA20220413203](https://openairdocs.org/sdr/MASA20220413203.md): Transcowl · cracked · Apr 13, 2022 · N904FJ · Cndair CL6002D24 · Engine Thrust Reverser
  > THE RH UPPER TRANSCOWL WAS FOUND TO HAVE CRACK DAMAGE TO THE OUTER SKIN. PERFORMED PERM REPAIR IAW CRJ?00/900 STRUCTURAL REPAIR MANUAL (SRM) 54-21-05, FIGURE 54-21-05-991-801, ITEM 1 (REV.38 DATED JUL. 25, 2020).
- [SDR MASA20220413202](https://openairdocs.org/sdr/MASA20220413202.md): None · cracked · Apr 13, 2022 · N904FJ · Cndair CL6002D24 · Service Doors
  > THE REPAIR AFT IAW SERVICE CRJ?00/900 DOOR PLUG STRUCTURAL INNER SKIN REPAIR (P/N: MANUAL CC690-38511-1) (SRM) WAS 53-51-01-001-005-A01 FOUND TO HAVE ITEM (2) 2, "SKIN, CRACKS. AFT PERFORMED SERVICE DOOR PERM PLUG-STRUCTURAL IDENTIFICATION" (REV.38 DATED JUL.
- [SDR MASA20220413201](https://openairdocs.org/sdr/MASA20220413201.md): None · none · Apr 13, 2022 · N904FJ · Cndair CL6002D24 · Passenger/Crew Doors
  > THE L 1 DOOR ACCESS PANEL 832AT BOTTOM STEP WAS FOUND WITH WEAR DAMAGE IN THE SETTLEMENT AREA. PERFORMED PERM REPAIR IAW CRJ700/900 STRUCTURAL REPAIR MANUAL (SRM) 52-11-04-001-001-A01 ITEM 30 (REV.38 DATED JUL.25, 2020).
- [SDR MASA20220413200](https://openairdocs.org/sdr/MASA20220413200.md): Exhaust Cone · dented · Apr 13, 2022 · N904FJ · Cndair CL6002D24 · Fuselage Structure (General)
  > MAINTENANCE DISCOVERED TWO DENTS AFFECTING THE SKIN AFT CONE (P/N: WA670-30701-1). PERFORMED PERM REPAIR IAW CRJ700/900 STRUCTURAL REPAIR MANUAL (SRM) 53-85-00-001-002-A01, ITEM 1.
- [SDR MASA20220413199](https://openairdocs.org/sdr/MASA20220413199.md): None · dented · Apr 13, 2022 · N904FJ · Cndair CL6002D24 · Trailing Edge Flaps
  > THE INBOARD FLAP LOWER SKIN OF THE RH WING WAS FOUND WITH A DENT AT FLS 48.00. PERFORMED PERM REPAIR IAW CRJ700/900 STRUCTURAL REPAIR MANUAL (SRM) 57-52-01, ITEM 28A, D (REV.38 DATED JULY 9TH, 2021).
- [SDR MASA20220413198](https://openairdocs.org/sdr/MASA20220413198.md): None · none · Apr 13, 2022 · N904FJ · Cndair CL6002D24 · Nacelle/Pylon, Plate/Skin
  > THE RH LOWER FAN COWL DOOR WAS FOUND TO HAVE 10 EA. ELONGATED COUNTERSINKS AND FASTENER HOLES ALONG THE EDGE OF THE OUTER SKIN PANEL AND AFT EDGE MEMBER. PERFORMED PERM REPAIR IAW CRJ700/900 STRUCTURAL REPAIR MANUAL (SRM) 54-14-01, FIGURE 54-14-01-991-801, ITE
- [SDR MASA20220413197](https://openairdocs.org/sdr/MASA20220413197.md): None · corroded · Apr 13, 2022 · N904FJ · Cndair CL6002D24 · Leading Edge Devices
  > SLAT TRACKS 3-1 (P/N: CC670-12072-7) AND TRACK 3-2 (P/N: CC670-12081-9) ON THE LH WING WAS FOUND TO HAVE CORROSION DAMAGE ON THE UPPER FACES. PERFORMED PERM REPAIR IAW CRJ900 ILLUSTRATED PARTS CATALOG (IPG) 27-81-41, FIGURE 10, ITEM15,AND 90 (REV. 70 DATED 10
- [SDR MASA20220413196](https://openairdocs.org/sdr/MASA20220413196.md): None · corroded · Apr 13, 2022 · N904FJ · Cndair CL6002D24 · Leading Edge Devices
  > SLAT TRACKS 2-3 (P/N: CC670-12062-7) ON THE LH WING WAS FOUND TO HAVE CORROSION DAMAGE ON THE UPPER FACES. PERFORMED PERM REPAIR IAW CRJ900 ILLUSTRATED PARTS CATALOG (IPC) 27-81-41, FIGURE 5, ITEM 105,(REV. 70 DATED, 10 AUG 2021).
- [SDR MASA20220413195](https://openairdocs.org/sdr/MASA20220413195.md): None · corroded · Apr 12, 2022 · N904FJ · Cndair CL6002D24 · Leading Edge Devices
  > SLAT TRACKS 1-1 (P/N: CC670-12010-5} AND 1-2 (P/N: CC670-12021-9) AND 1-3 (P/N: CC670-12030-3} ON THE LH WING WERE_ FOUND TO HAVE CORROSION DAMAGE ON THE UPPER AND /OR LOWER SURFACES. PERFORMED PERM REPAIR IAW CRJ900 ILLUSTRATED PARTS CATALOG (IPC) 27-81-41, F
- [SDR MASA20220413194](https://openairdocs.org/sdr/MASA20220413194.md): None · corroded · Apr 12, 2022 · N904FJ · Cndair CL6002D24 · Leading Edge Devices
  > SLAT TRACKS 3-1 (P/N: CC670-12070-3) AND 3-2 (P/N: CC670-12081-7) ON THE RH WING WERE FOUND TO HAVE CORROSION DAMAGE ON THE UPPER AND /OR LOWER SURFACES. PERFORMED PERM REPAIR IAW CRJ900 ILLUSTRATED PARTS CATALOG (IPC) 27-81-41, FIGURE 10, ITEM 10A AND 85 (R
- [SDR MASA20220413193](https://openairdocs.org/sdr/MASA20220413193.md): None · corroded · Apr 12, 2022 · N904FJ · Cndair CL6002D24 · Leading Edge Devices
  > SLAT TRACKS 2-1 (P/N: CC670-12040-3) AND 2-2 (P/N: CC670-12051-9) ON THE RH WING WERE FOUND TO HAVE CORROSION DAMAGE ON THE UPPER AND /OR LOWER SURFACES. PERFORMED PERM REPAIR IAW CRJ900 ILLUSTRATED PARTS CATALOG (IPC) 27-81-41, FIGURE 5, ITEM 15 AND 85 (REV
- [SDR MASA20220413192](https://openairdocs.org/sdr/MASA20220413192.md): None · corroded · Apr 12, 2022 · N904FJ · Cndair CL6002D24 · Leading Edge Devices
  > SLAT TRACKS 1-1 (P/N: CC670-12010-5) AND 1-2 (P/N: CC670-12021-9) AND 1-3 (P/N:CC670-12030-3) ON THE RH WING WERE FOUND TO HAVE CORROSION DAMAGE ON THE UPPER AND /OR LOWER SURFACES. PERFORMED PERM REPAIR IAW CRJ900 ILLUSTRATED PARTS CATALOG (IPC) 27-81-41, FIG
- [SDR MASA20220413191](https://openairdocs.org/sdr/MASA20220413191.md): None · none · Apr 12, 2022 · N904FJ · Cndair CL6002D24 · Ice/Rain Protection System
  > THE WING ANTI ICE (WAI) RH SUPPLY DUCT SHIELD (PN-9911996-102) EXTERIOR SURFACE. PERFORMED PERM REPAIR IAW_ CRJ900 AIRCRAFT ILLUSTRATED PARTS CATALOG (AIPC) 30-11-04-01, FIGURE 1, ITEM 30 & 33 (REV71 DATED 1/17/2022).
- [SDR MASA20220413190](https://openairdocs.org/sdr/MASA20220413190.md): None · corroded · Apr 12, 2022 · N904FJ · Cndair CL6002D24 · Nacelle/Pylon, Main Frame
  > THE LH INLET COWL LIPSKIN WAS FOUND TO HAVE EROSION DAMAGE AND WAS BLENDED OUT PER SRM 54-11-05-101-001-A01. PERFORM PERM REPAIR IAW CRJ7/9 STRUCTURAL REPAIR MANUEL (SRM) 54-11-05, FIGURE 54-11-05-991-801, ITEM 1 (REV.37 DATED AUG. 15, 2019).
- [SDR MASA20220413189](https://openairdocs.org/sdr/MASA20220413189.md): Skin · corroded · Apr 7, 2022 · N904FJ · Cndair CL6002D24 · Fuselage Main, Structure
  > IN REF NRC S/N 00352, DURING STRINGER 21RH REMOVAL, CORROSION ON INTERNAL FUSELAGE SKIN WAS FOUND BTW FS 305-315 (SETTLEMENT AREA OF STRG 21R). IT WAS REPAIRED PER EA 81-2022-044 REV. IR
- [SDR MASA20220426208](https://openairdocs.org/sdr/MASA20220426208.md): Stringer · corroded · Apr 3, 2022 · N904FJ · Cndair CL6002D24 · Fuselage Structure (General)
  > CORROSION ON STRINGER 23 RH BTW FS319.5-FS333, AT MAIN E/E COMPARTMENT. STRINGER 23 RH BTW FS319.5-FS333, AT MAIN E/E COMPARTMENT WAS REPAIRED PER CRJ-900 SRM 53-00-03-201-001-A02
- [SDR MASA20220426207](https://openairdocs.org/sdr/MASA20220426207.md): Stringer · corroded · Apr 3, 2022 · N904FJ · Cndair CL6002D24 · Fuselage Structure (General)
  > CORROSION ON STRINGER 21 RH BTW FS295-FS333, AT MAIN E/E COMPARTMENT. STRINGER 21 RH BTW FS280 TO FS333 WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-20-001-001-A01
- [SDR MASA20220411182](https://openairdocs.org/sdr/MASA20220411182.md): None · corroded · Apr 3, 2022 · N904FJ · Cndair CL6002D24 · Fuselage Structure (General)
  > CORROSION ON STRINGER 19RH BTW FS295-FS330, AT MAIN E/E COMPARTMENT. CORRECTIVE ACTION: STRINGER 19RH BTW FS295-FS330 WAS REPLACED PER CRJ900 SRM 53-00-03-201-001-A02.
- [SDR MASA20220401162](https://openairdocs.org/sdr/MASA20220401162.md): None · none · Apr 1, 2022 · N904FJ · Cndair CL6002D24 · Engine Thrust Reverser
  > THE RH ENGINE UPPER TRANSCOWL LATCH DOOR (PN-CN624-2021-901) WAS FOUND TO HAVE WEAR ON THE SURROUND LANDING AT THE FREE EDGE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 (SRM) TASK 54-21-05-003-A01, (REV. 38 DATED 9JUL2021). (SUPPLEMENTAL)
- [SDR MASA20220331162](https://openairdocs.org/sdr/MASA20220331162.md): None · corroded · Mar 31, 2022 · N904FJ · Cndair CL6002D24 · Engine Thrust Reverser
  > THE RH ENGINE UPPER TRANSCOWL LATCH DOOR (PN-CN624-2021-901) WAS FOUND TO HAVE CORROSION ON THE SURROUND LANDING AT THE FREE EDGE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 (SRM) TASK 54-21-05-003-A01, (REV. 38 DATED 9JUL2021).
- [SDR MASA20220329161](https://openairdocs.org/sdr/MASA20220329161.md): None · none · Mar 29, 2022 · N904FJ · Cndair CL6002D24 · Service Doors
  > THE AFT SERVICE DOOR LOWER BEAM WAS FOUND WITH WEAR DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ700/900 SRM 52-46-06-001-001-A01 ITEM 45 (REV. 38 DATED JUL. 25, 2020).
- [SDR MASA20220329160](https://openairdocs.org/sdr/MASA20220329160.md): None · none · Mar 29, 2022 · N904FJ · Cndair CL6002D24 · Ailerons
  > THE RH AILERON CENTER HINGE ASSEMBLY WAS DISCOVERED TO HAVE TOOL MARKS DURING THE REMOVAL OF THE PCU ATTACH LINK BOLT AT AS343.53. PERFORMED PERMANANT REPAIR IAW CRJ700/900 ILLUSTRATED PARTS CATALOG {IPC) 57-60-00, FIGURE 1, ITEM 146 (REV.37 DATED AUG. 15, 201
- [SDR MASA20220324119](https://openairdocs.org/sdr/MASA20220324119.md): Flap · dented · Mar 24, 2022 · N904FJ · Cndair CL6002D24 · Trailing Edge Flaps
  > A DENT WAS FOUND AFFECTING THE SKIN THE LOWER SKIN ON LEFT OUTBOARD FLAP ALONG THE AFT EDGE..PERFORMED A PERMANENT REPAIR IAW CRJ900 SRM 57-52-01, FIGURE 57-53-01-001-001-A01, ITEM 3. DEFECT LOCATION: LH WING, FS235.96-245.84
- [SDR MASA20220324118](https://openairdocs.org/sdr/MASA20220324118.md): None · dented · Mar 24, 2022 · N904FJ · Cndair CL6002D24 · Nacelle/Pylon, Plate/Skin
  > EIGHT DENTS WERE REPORTED AFFECTING THE LH ENGINE INBOARD INLET COWL AT THE 5 TO 7 O'CLOCK POSITION LOOKING FORWARD ON THE OUTER INBOARD SKIN. PERFORMED A PERMANENT REPAIR IAW CRJ700/900 SRM 54-11-01-001-002-A01 FIGURE 54-11-01-991-802 ITEM (REV. 37 DATED 24 F
- [SDR MASA20220411177](https://openairdocs.org/sdr/MASA20220411177.md): Tripler · worn · Mar 22, 2022 · N904FJ · Cndair CL6002D24 · Fuselage Structure (General)
  > WEAR ON TRIPLER SKIN SKIN (PREVIOUS REPAIR) LOCATED BTW FS969-985 FS969 & SGTR 26L-26R, REAR FUSELAGE (4 LOCATIONS). CORRECTIVE ACTION: TRIPLER SKIN SKIN (PREVIOUS REPAIR) LOCATED BTW FS969-985 FS969 & SGTR 26L-26R, REAR FUSELAGE WERE REPAIRED PER REO 690-5
- [SDR MASA20220411176](https://openairdocs.org/sdr/MASA20220411176.md): None · corroded · Mar 22, 2022 · N904FJ · Cndair CL6002D24 · Fuselage Structure (General)
  > PITTING CORROSION ON SLAT TRACKS: 1-1, 1-3, 3-1 AT UPPER SURFACE; SLAT TRACK 1-2 & 2-2 AT LOWER SURFACE; SLAT TRACK 2-1 & 3-2 AT UPPER/LOWER SURFACE FOR RH WING.| CORRECTIVE ACTION: SLAT TRACKS WAS PERFORMED PER EA 81-2022-038 REV IR.EA 81-2022-039 REV IR AND
- [SDR MASA20220411175](https://openairdocs.org/sdr/MASA20220411175.md): None · corroded · Mar 22, 2022 · N904FJ · Cndair CL6002D24 · Fuselage Structure (General)
  > PITTING CORROSION ON SLAT TRACK: 1-1, 1-2, 1-3 & 2-3 AT UPPER/LOWER SURFACE; SLAT TRACK 2-3, 3-1 & 3-2 AT UPPER SURFACE, FOR LH WING |CORRECTIVE ACTION: SLAT TRACKS WAS PERFORMED PER EA 81-2022-040 REV IR, EA 81-2022-041 REV IR AND EA 81-2022-042 REV IR
- [SDR MASA20220411174](https://openairdocs.org/sdr/MASA20220411174.md): None · cracked · Mar 22, 2022 · N904FJ · Cndair CL6002D24 · Fuselage Main, Structure
  > INITIAL INSPECTION: CRACK ON COCKPIT FLOOR LONGITUDINAL BEAMS (LBL 12/RBL 12) TO CROSSBEAM FS 280. FLOOR STRUCTURE BELOW FLIGHT COMPARTMENT | BEAMS (LBL 12/RBL 12) TO CROSSBEAM FS 280. FLOOR STRUCTURE BELOW FLIGHT COMPARTMENT WAS REPAIRED PER CRJ 900 SRM 53-11
- [SDR MASA20220411184](https://openairdocs.org/sdr/MASA20220411184.md): None · corroded · Mar 20, 2022 · N904FJ · Cndair CL6002D24 · Fuselage Structure (General)
  > CORROSION ON FLOOR SEAT RAIL AT LBL 27.00 BETWEEN FS 349.50 - FS 485.00| FLOOR SEAT RAIL AT LBL 27.00 BETWEEN FS 349.50 - FS 485.00 AS REPLACED PER CRJ900 AMM 53-00-49
- [SDR MASA20220411183](https://openairdocs.org/sdr/MASA20220411183.md): None · corroded · Mar 20, 2022 · N904FJ · Cndair CL6002D24 · Fuselage Structure (General)
  > CORROSION ON LH SIDE SEAT RAIL AT WL 85.25 BETWEEN FS 847.00+14 - FS 907.00| H SIDE SEAT RAIL AT WL 85.25 BETWEEN FS 847.00+14 - FS 907.00 WAS REPLACED PER CRJ 900 SRM 53-0044
- [SDR MASA20220411173](https://openairdocs.org/sdr/MASA20220411173.md): None · corroded · Mar 20, 2022 · N904FJ · Cndair CL6002D24 · Fuselage Structure (General)
  > CORROSION ON LH SIDE SEAT RAIL AT WL 85.25 BETWEEN FS 743.00 - FS 763.00. LH SIDE SEAT RAIL AT WL 85.25 BETWEEN FS 743.00 - FS 763.00 WAS REPLACED PER CRJ900 AMM 53-00-49
- [SDR MASA20220411172](https://openairdocs.org/sdr/MASA20220411172.md): None · corroded · Mar 20, 2022 · N904FJ · Cndair CL6002D24 · Fuselage Structure (General)
  > CORROSION ON LH SIDE SEAT RAIL AT WL 85.25 BETWEEN FS 672.00 - FS 772.00 |LH SIDE SEAT RAIL AT WL 85.25 BETWEEN FS 672.00 - FS 772.00 WAS REPLACED PER CRJ900 AMM 53-00-49
- [SDR MASA20220411171](https://openairdocs.org/sdr/MASA20220411171.md): None · corroded · Mar 20, 2022 · N904FJ · Cndair CL6002D24 · Fuselage Structure (General)
  > CORROSION ON LH SIDE SEAT RAIL AT WL 85.25 BETWEEN FS 661.00+90 - FS 672.00 | LH SIDE SEAT RAIL AT WL 85.25 BETWEEN FS 661.00+90 - FS 672.00 WAS REPLACED PER CRJ-900 AMM 53-00-49
- [SDR MASA20220411170](https://openairdocs.org/sdr/MASA20220411170.md): None · corroded · Mar 20, 2022 · N904FJ · Cndair CL6002D24 · Fuselage Structure (General)
  > CORROSION ON LH SIDE SEAT RAIL AT WL 85.25 BETWEEN FS 573.00 - FS 661.00+14 | LH SIDE SEAT RAIL AT WL 85.25 BETWEEN FS 573.00 - FS 661.00+14 WAS INSTALLED PER CRJ900-AMM-53-00-49
- [SDR MASA20220411169](https://openairdocs.org/sdr/MASA20220411169.md): None · corroded · Mar 20, 2022 · N904FJ · Cndair CL6002D24 · Fuselage Structure (General)
  > CORROSION ON LH SIDE SEAT RAIL AT WL 85.25 BETWEEN FS 483.00 - FS 573.00 | LH SIDE SEAT RAIL AT WL 85.25 BETWEEN FS 483.00 - FS 573.00 WAS REPLACED PER CRJ-900 AMM 53-00-49
- [SDR MASA20220411168](https://openairdocs.org/sdr/MASA20220411168.md): None · corroded · Mar 20, 2022 · N904FJ · Cndair CL6002D24 · Fuselage Structure (General)
  > CORROSION ON LH SIDE SEAT RAIL AT WL 85.25 BETWEEN FS 379.00 - FS 483.00 |LH SIDE SEAT RAIL AT WL 85.25 BETWEEN FS 379.00 - FS 483.00. WAS REPLACED PER CRJ-900 AMM 53-00-49
- [SDR MASA20220411167](https://openairdocs.org/sdr/MASA20220411167.md): None · corroded · Mar 20, 2022 · N904FJ · Cndair CL6002D24 · Fuselage Structure (General)
  > CORROSION ON RH SIDE SEAT RAIL AT WL 85.25 BETWEEN FS 573.00 - FS 661.00+14. RH SIDE SEAT RAIL AT WL 85.25 BETWEEN FS 573.00 - FS 661.00+14 WAS REPLACED PER CRJ900 AMM 53-00-49
- [SDR MASA20220411166](https://openairdocs.org/sdr/MASA20220411166.md): None · corroded · Mar 20, 2022 · N904FJ · Cndair CL6002D24 · Fuselage Structure (General)
  > CORROSION ON RH SIDE SEAT RAIL AT WL 85.25 BETWEEN FS 483.00 - FS 573.00. RH SIDE SEAT RAIL AT WL 85.25 BETWEEN FS 483.00 - FS 573.00 WAS REPLACED PER CRJ900 AMM 53-00-49
- [SDR MASA20220411165](https://openairdocs.org/sdr/MASA20220411165.md): None · corroded · Mar 20, 2022 · N904FJ · Cndair CL6002D24 · Fuselage Structure (General)
  > CORROSION ON RH SIDE SEAT RAIL AT WL 85.25 BETWEEN FS 379.00 - FS 483.00. | CORRECTIVE ACTION: SIDE SEAT RAIL AT WL 85.25 BETWEEN FS 379.00 - FS 483.00 WAS REPLACED PER CRJ 900 AMM 53-00-49
- [SDR MASA20220413188](https://openairdocs.org/sdr/MASA20220413188.md): Plate · corroded · Mar 19, 2022 · N904FJ · Cndair CL6002D24 · Fuselage Structure (General)
  > CORROSION AND GOUGE ON ACCESS PANEL 814FZ (SERVICE DOOR LATCH COVER) ACTION ACCESS PANEL 814FZ WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01
- [SDR MASA20220426206](https://openairdocs.org/sdr/MASA20220426206.md): None · corroded · Mar 18, 2022 · N904FJ · Cndair CL6002D24 · Fuselage Structure (General)
  > CORROSION ON INTERNAL FUSELAGE SKIN WAS FOUND BTW FS 305-315 (SETTLEMENT AREA OF STRG 21R) CORROSION ON INTERNAL FUSELAGE SKIN WAS FOUND BTW FS 305-315 (SETTLEMENT AREA OF STRG 21R) WAS REPAIRED PER EA 81-2022-044 REV. IR
- [SDR MASA20220412185](https://openairdocs.org/sdr/MASA20220412185.md): None · corroded · Mar 18, 2022 · N904FJ · Cndair CL6002D24 · Fuselage Structure (General)
  > CORROSION ON RH SIDE SEAT RAIL AT WL 85.25 BETWEEN FS 847.00+14 - FS 867.00 | RH SIDE SEAT RAIL AT WL 85.25 BETWEEN FS 847.00+14 - FS 867.00 WAS REPLACED PER CRJ 900-53-00-49

Next page: https://openairdocs.org/aircraft/N904FJ/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 = 'N904FJ' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N904FJ/reports

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