# Service difficulty reports: N902FJ

A list on [N902FJ](https://openairdocs.org/aircraft/N902FJ.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 · 317 reports

- [SDR MASA2024030100018](https://openairdocs.org/sdr/MASA2024030100018.md): Light · inoperative · Mar 1, 2024 · N902FJ · Cndair CL6002D24 · Emergency Lighting
  > CEILING EMER LIGHT AT ROW 18 INOP. PLACED ON MEL.
- [SDR MASA2024030100017](https://openairdocs.org/sdr/MASA2024030100017.md): Light · inoperative · Mar 1, 2024 · N902FJ · Cndair CL6002D24 · Emergency Lighting
  > CEILING EMER LIGHT AT ROW 3 INOP. PLACED ON MEL
- [SDR MASA2023100800132](https://openairdocs.org/sdr/MASA2023100800132.md): Bulb · burned out · Oct 8, 2023 · N902FJ · Cndair CL6002D24 · Emergency Lighting
  > ROW 18 EMERGENCY FLOOD LIGHT BULB INOP PLACED ON MEL RELAMP, OPS CHECK GOOD.
- [SDR MASA2023070400088](https://openairdocs.org/sdr/MASA2023070400088.md): Unknown · unknown · Jul 4, 2023 · N902FJ · Cndair CL6002D24 · Landing Gear System
  > NLG/STEERING DISAGREE CURRENTLY TROUBLESHOOTING, FOUND NLG STRUT COLLAPSED AFTER LANDING, NEEDS A STRUT RE-PACK.
- [SDR MASA2023022300038](https://openairdocs.org/sdr/MASA2023022300038.md): Battery Pack · discharged · Feb 23, 2023 · N902FJ · Cndair CL6002D24 · Emergency Lighting
  > ALL EMER BATT LTS DRAINED/SW LEFT IN ON POSITION CREW ALOWED EMER BATTERIES TO CHARGE, OPS CK GD
- [SDR MASA2023021800035](https://openairdocs.org/sdr/MASA2023021800035.md): Bulb · inoperative · Feb 18, 2023 · N902FJ · Cndair CL6002D24 · Emergency Lighting
  > FWD ROW 13 EMER LIGHT INOP RELAMPED FWD ROW 13 EMER LIGHT OPS CHECK GOOD
- [SDR MASA2023021600032](https://openairdocs.org/sdr/MASA2023021600032.md): Bulb · inoperative · Feb 16, 2023 · N902FJ · Cndair CL6002D24 · Emergency Lighting
  > ROW 17 CEILING EMER FLOOD LIGHT INOP REPLACED BULB
- [SDR MASA2023012170015](https://openairdocs.org/sdr/MASA2023012170015.md): Battery Pack · discharged · Jan 17, 2023 · N902FJ · Cndair CL6002D24 · Emergency Lighting
  > EMERGENCY LIGHTS INOPERATIVE. CHARGED BATTERIES, OPS CHECK GOOD
- [SDR MASA2022090100222](https://openairdocs.org/sdr/MASA2022090100222.md): None · none · Sep 2, 2022 · N902FJ · Cndair CL6002D24 · Emergency Lighting
  > ROW 15 CEILING LEVEL FLOOD LIGHT INOP. REPLACED BULB.
- [SDR MASA2021122900352](https://openairdocs.org/sdr/MASA2021122900352.md): Bulb · inoperative · Dec 30, 2021 · N902FJ · Cndair CL6002D24 · Emergency Lighting
  > SVC DR LWR AFT FLOODLIGHT 1 BULB OUT REPLACED BULB
- [SDR MASA2021122400348](https://openairdocs.org/sdr/MASA2021122400348.md): None · none · Dec 24, 2021 · N902FJ · Cndair CL6002D24 · Emergency Lighting
  > DOOR EXIT LT FWD EDGE 1 BULB INOP. RELAMP, OPS CHK GD
- [SDR MASA2021122400347](https://openairdocs.org/sdr/MASA2021122400347.md): None · none · Dec 24, 2021 · N902FJ · Cndair CL6002D24 · Emergency Lighting
  > EMER ZONE INDICATOR LIGHTS 1,3,9 INOP. RESECURED CONNECTOR, OPS CHK GOOD
- [SDR MASA20211213605](https://openairdocs.org/sdr/MASA20211213605.md): None · damaged · Dec 10, 2021 · N902FJ · Cndair CL6002D24 · Leading Edge Devices
  > THE RH WING SLAT 1 RIB AT SS 196.66 WAS FOUND WITH EXISTING MATERIAL REMOVAL COMMON TO THE SLAT DISCONNECT SENSOR STRIKE PIN. PERFORMED PERMANENT REPAIR IAW SRM 57-41-12-995-801, ITEM 28B (REV. 38 DATED JUL. 25, 2020).
- [SDR MASA20211213604](https://openairdocs.org/sdr/MASA20211213604.md): None · none · Dec 10, 2021 · N902FJ · Cndair CL6002D24 · Fuselage Main, Structure
  > THE FORWARD AND AFT SEAL CARRIERS OF THE AFT SERVICE DOOR PLUG WAS FOUND TO HAVE (2) GOUGES. PERFORMED PERMANENT REPAIR IAW CRJ7/9 IAW SRM 53-51-07-001-005-A01 FIG. 53-51-07-991-801, ITEMS 3 AND 4 (REV. 38 DATED JULY 9, 2021).
- [SDR MASA20211213603](https://openairdocs.org/sdr/MASA20211213603.md): None · none · Dec 10, 2021 · N902FJ · Cndair CL600* · Fuselage Floor Panel
  > A FLOOR SILL STRUCTURE WAS FOUND WITH SEVERAL DAMAGES MAKING THE SILL INOPERABLE. PERFORMED PERMANENT REPAIR IAW CRJ7/9 53-21-45-001-A02, ITEM 1 (REV. 38 DATED JUL. 25, 2020).
- [SDR MASA20211213610](https://openairdocs.org/sdr/MASA20211213610.md): Beam · corroded · Dec 9, 2021 · N902FJ · Cndair CL6002D24 · Fuselage Structure (General)
  > THE CENTER FLOOR BEAM WAS FOUND WITH CORROSION DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ7/9 53-31-43, FIG. 53-31-43-991-801, ITEM 6 (REV. 38 DATED JUL. 25, 2020). DEFECT LOCATION: FS 621.00-661.00+22.50, LBL 9.00
- [SDR MASA20211213609](https://openairdocs.org/sdr/MASA20211213609.md): None · corroded · Dec 9, 2021 · N902FJ · Cndair CL6002D24 · Doors
  > THE SERVICE DOOR SURROUND STRUCTURE SEAL STRIKER WAS FOUND WITH CORROSION DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ7/9 SRM 51-21-16 AND PER CMM 516-02 FIG. 1 DETAILS.
- [SDR MASA20211213608](https://openairdocs.org/sdr/MASA20211213608.md): None · none · Dec 9, 2021 · N902FJ · Cndair CL6002D24 · Wing Structure
  > THE L/H WING T/E STRUCTURE SUPPORT FITTING AT SPS 43.60 WAS FOUND WITH WEAR DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ7/9 REO 670-57-51-341 AND SRM 51-26-00, 51-12-00.
- [SDR MASA20211213607](https://openairdocs.org/sdr/MASA20211213607.md): None · corroded · Dec 9, 2021 · N902FJ · Cndair CL6002D24 · Fuselage Structure (General)
  > THE CENTER FLOOR BEAM AT PAX CABIN WAS FOUND WITH CORROSION DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ7/9 SRM 53-00-41-201-001-A03 (FLOORBEAMS FS 280.00 -FS 1098.20 REPAIRS), FIG. 53-00-41-995-829 (REV. 38 DATED JUL. 25, 2020).
- [SDR MASA20211213606](https://openairdocs.org/sdr/MASA20211213606.md): None · corroded · Dec 9, 2021 · N902FJ · Cndair CL6002D24 · Fuselage Structure (General)
  > HE RBL9.00 CENTER FLOOR BEAM AT PAX CABIN WAS FOUND WITH CORROSION DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ7/9 SRM 53 -31-43-101-A03 AND 53-00-41-201-001-A03 (FLOORBEAMS FS 280.00 -FS 1098.20 REPAIRS), FIG 53-00-41-995-829 (REV. 38 DATED JUL. 25, 2020).
- [SDR MASA20211213620](https://openairdocs.org/sdr/MASA20211213620.md): None · dented · Dec 8, 2021 · N902FJ · Cndair CL6002D24 · Fuselage Structure (General)
  > THE LH FUSELAGE SKIN PANEL WAS FOUND WITH A DENT. PERFORMED PERMANENT REPAIR IAW CRJ7/9 53-11-01, FIG. 53-11-01-991-806, ITEM 1 (REV. 38 DATED 9 JUL. 2021). DEFECT LOCATION: FS 278.00 BETWEEN STRG. 22L AND STRG. 23L
- [SDR MASA20211213619](https://openairdocs.org/sdr/MASA20211213619.md): None · dented · Dec 8, 2021 · N902FJ · Cndair CL6002D24 · Fuselage Structure (General)
  > THE FUSELAGE LOWER SKIN PANEL WAS FOUND WITH A DENT. PERFORMED PERMANENT REPAIR IAW CRJ?/9 53-61-01. DEFECT LOCATION: FS 1047-FS 1051, STGR. 22L - STGR. 23L
- [SDR MASA20211213618](https://openairdocs.org/sdr/MASA20211213618.md): None · corroded · Dec 8, 2021 · N902FJ · Cndair CL6002D24 · Fuselage Structure (General)
  > THE UPPER CAP AFT FLOOR BEAM FOUND WITH CORROSION DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ7/9 53-31-43-991-801, ITEM 7 (REV. 33 DATED JUN.25, 2017).
- [SDR MASA20211213617](https://openairdocs.org/sdr/MASA20211213617.md): None · eroded · Dec 8, 2021 · N902FJ · Cndair CL6002D24 · Empennage Structure
  > THE VERTICAL STABILIZER BULLET FAIRING UPPER PANEL ASSEMBLY WAS FOUND HAVING EROSION DAMAGE. PERFORMED PERMANENT REPAIR JAW CRJ7/9 SRM 51-74-02-201-001-A01, (REV. DATED 7-9-2021). DEFECT LOCATION: VERTICAL STABILIZER BULLET FAIRING UPPER PANEL
- [SDR MASA20211130592](https://openairdocs.org/sdr/MASA20211130592.md): None · none · Dec 8, 2021 · N902FJ · Cndair CL6002D24 · Nacelle/Pylon Structure
  > OUTER SKIN PANEL OF THE LOWER RH FAN COWL DOOR WAS FOUND TO HAVE WEAR DAMAGE AT THE UPPER AFT CORNER. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 54-14-01, FIGURE 54-14-01-991-801, ITEM 1A, EA 72-2021-219.
- [SDR MASA20211213611](https://openairdocs.org/sdr/MASA20211213611.md): None · corroded · Dec 8, 2021 · N902FJ · Cndair CL6002D24 · Fuselage Structure (General)
  > THE UPPER CAP OF THE LBL9.00 CENTER FUSELAGE FLOOR BEAM BETWEEN FS661+16-FS661+32 WAS FOUND TO HAVE CORROSION DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ7/9 SRM 53-31-43-001-A03, FIG. 53-61-43-991-801, ITEM 2A (REV. 33 DATED JUN. 25, 2017). DEFECT LOCATION: FS
- [SDR MASA20211213616](https://openairdocs.org/sdr/MASA20211213616.md): None · corroded · Dec 7, 2021 · N902FJ · Cndair CL6002D24 · Fuselage Structure (General)
  > CENTER FLOOR BEAM AT PAX CABIN WAS FOUND WITH CORROSION DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ7/9 SRM TASK 53-00-41-201-001-A03, SRM 53-31-43-991-801, ITEMS 4 (REV.38 DATED JUL. 25, 2020).
- [SDR MASA20211213615](https://openairdocs.org/sdr/MASA20211213615.md): None · dented · Dec 7, 2021 · N902FJ · Cndair CL6002D24 · Fuselage Structure (General)
  > LOWER FUSELAGE SKIN PANEL WAS FOUND TO HAVE A DENT. PERFORMED PERMANENT REPAIR IAW CRJ7/9 SRM 53-21-01-001-002-A01, ITEMS 1 AND E (REV. 37 DATED 15 AUG 2019). DEFECT LOCATION: FS295.00-FS310.00 ANO STGR.18R-STGR. 19R
- [SDR MASA20211213614](https://openairdocs.org/sdr/MASA20211213614.md): None · dented · Dec 7, 2021 · N902FJ · Cndair CL6002D24 · Wing Structure
  > THE RH WING OUTBOARD RIB AT WS 281.50 WAS FOUND WITH A DENT AT THE LOWER FLANGE OF THE RIB. PERFORMED PERMANENT REPAIR IAW CRJ7/9 SRM 51-26-01, SRM 57-53-02-101-001-A01/57-53-01-101-001
- [SDR MASA20211213613](https://openairdocs.org/sdr/MASA20211213613.md): None · none · Dec 7, 2021 · N902FJ · Cndair CL6002D24 · Fuselage Structure (General)
  > FOUND PREVIOUS BLENDOUTS AT FUSELAGE LH SKIN PANEL BETWEEN FS661+32 & BETWEEN STGR15L & STGR17L. PERFORMED PERMANENT REPAIR IAW CRJ?/9 SRM 53-31-01, FIG. 53-31-0.1-995-804, ITEM 1 (REV. 38 DATED 9 JUL 2021).
- [SDR MASA20211213612](https://openairdocs.org/sdr/MASA20211213612.md): None · dented · Dec 7, 2021 · N902FJ · Cndair CL6002D24 · Wing Structure
  > DENT DAMAGE WAS FOUND ON RH WING OTBD FLAP LOWER SKIN. DENT WAS LOCATED ON OTBD AFT END AT WS 281.50 & MEASURED 7.779" LONG X 3.228" WIDE X0.120". PERFORMED PERMANENT REPAIR IAW CRJ7/9 SRM 57-53-01-201-001-A01 TYPE II REPAIR-OUTBOARD FLAP SKINS-FLUSH REPAIRS.
- [SDR MASA20211130593](https://openairdocs.org/sdr/MASA20211130593.md): None · none · Nov 30, 2021 · N902FJ · Cndair CL6002D24 · Doors
  > AFT BAGGAGE BAY DOOR OUTER SKIN WAS FOUND TO HAVE EIGHT NICKS. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 52-31-01-001-001-A01 FIGURE 52-31-01-991-801, ITEM 2A, EA 79-2021-266.
- [SDR MASA20211130591](https://openairdocs.org/sdr/MASA20211130591.md): None · none · Nov 30, 2021 · N902FJ · Cndair CL6002D24 · Fuselage Structure (General)
  > FUSELAGE LOWER SKIN PANEL BETWEEN FS 485 -FS 517, STR 24R -STR 26R WAS FOUND WITH SIX AREAS OF DAMAGE DUE TO LIGHTNING STRIKE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-31-01-001-003-A02, "SKIN, LOWER PANEL FS477.40 TO FS693.00 -STRUCTURAL IDENTIFICATI
- [SDR MASA20211130590](https://openairdocs.org/sdr/MASA20211130590.md): None · none · Nov 30, 2021 · N902FJ · Cndair CL600* · Nacelle/Pylon, Longeron/Stringer
  > WEAR DAMAGE WAS FOUND ON THE L/H ENGINE AFT CORE COWL INBOARD SKIN, THE DAMAGE IS LOCATED AT THE INTERFACE OF THE PYLON FAIRING SEAL. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 54-13-00, EA 20-2021-202.
- [SDR MASA20211130589](https://openairdocs.org/sdr/MASA20211130589.md): None · none · Nov 30, 2021 · N902FJ · Cndair CL600* · Fuselage Floor Panel
  > FUSELAGE SKIN AT FS285.00 - FS295.00 & STGR24R - STGR26R WAS FOUND TO HAVE 3 DENTS. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-21-01, FIGURE 53-21-01-991-802, ITEM 1M, EA 72-2021-210. FS28S.00 • FS295.00 & STGR2AR • STGR:26R
- [SDR MASA20211130588](https://openairdocs.org/sdr/MASA20211130588.md): None · none · Nov 30, 2021 · N902FJ · Cndair CL600* · Fuselage Floor Panel
  > FUSELAGE LOWER SKIN PANEL WAS FOUND WITH DAMAGE BETWEEN FS295.00-FS333.00 & STGR21R, THE DAMAGE CONSISTS OF TWELVE PROTRUDING DENTS. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-21-01-001-002-A01, FIGURE 53-21-01-991-802, ITEM 1, EA 81-2021-089.
- [SDR MASA20211130587](https://openairdocs.org/sdr/MASA20211130587.md): None · none · Nov 30, 2021 · N902FJ · Cndair CL600* · Fuselage Floor Panel
  > FLOOR SILL STRUCTURE WAS FOUND WITH SEVERAL DAMAGES MAKING THE SILL INOPERABLE. PERFORMED PERMANENT REPAIR IAW CR700/900 SRM 53-21-45-001-001-A02, ITEM 31, EA 80-2021-159.
- [SDR MASA20211129586](https://openairdocs.org/sdr/MASA20211129586.md): None · dented · Nov 29, 2021 · N902FJ · Cndair CL600* · Fuselage Structure (General)
  > FUSELAGE LOWER SKIN PANEL BETWEEN FS1047.0- FS1051.0, STR. 22L- STR. 23L WAS FOUND WITH A DENT. PERFOMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-61-01, EA 20-2021-198.
- [SDR MASA20211129585](https://openairdocs.org/sdr/MASA20211129585.md): None · dented · Nov 29, 2021 · N902FJ · Cndair CL600* · Fuselage Floor Panel
  > FUSELAGE LOWER SKIN PANEL WAS FOUND WITH A PROTRUDING DENT BETWEEN FS349 - FS364 AND STGR20R - STGR21R. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-21-01, FIGURE 53-21-01-991-806, ITEM 1, EA 72-2021-205.
- [SDR MASA20211129584](https://openairdocs.org/sdr/MASA20211129584.md): None · none · Nov 29, 2021 · N902FJ · Cndair CL600* · Fuselage Structure (General)
  > FUSELAGE LH SKIN PANEL BETWEEN FS501 & FS525 AND STGR14L & STGR15L WAS FOUND TO HAVE PREVIOUS BLENDOUTS. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-31-01, FIGURE 53-31-01-99-804, ITEM 1, EA 85-2021-003.FS501 & FS525 / STGR14L & STGR15L
- [SDR MASA20211129583](https://openairdocs.org/sdr/MASA20211129583.md): None · dented · Nov 29, 2021 · N902FJ · Cndair CL600* · Fuselage Floor Panel
  > LH FUSELAGE LOWER SKIN PANEL BETWEEN FS319.70 - FS333.0 & STR22L - STR23L WAS FOUND WITH TWO DENTS. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-21-01, FIGURE 53-21-01-991-802, ITEM 1, EA69-2021-195.
- [SDR MASA20211129579](https://openairdocs.org/sdr/MASA20211129579.md): None · none · Nov 25, 2021 · N902FJ · Cndair CL600* · Fuselage Floor Panel
  > RH FUSELAGE SKIN PANEL WAS FOUND WITH DAMAGE BETWEEN FS 645.00 AND 661.00 AT STGR 17R. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-21-01-001-005-A01, FIGURE 53-21-01-991-805, ITEM 1A, EA.81-2021-091
- [SDR MASA20211124575](https://openairdocs.org/sdr/MASA20211124575.md): None · none · Nov 24, 2021 · N902FJ · Cndair CL6002D24 · Fuselage Floor Panel
  > FUSELAGE LOWER SKIN PANEL AT FS453 AND STGR27R & STGR26L WAS FOUND TO HAVE A PREVIOUS BLENDOUT. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-11-01, FIGURE 53-21-01-99-807, ITEM 1, EA 72-2021-218.
- [SDR MASA20211124578](https://openairdocs.org/sdr/MASA20211124578.md): None · corroded · Nov 23, 2021 · N902FJ · Cndair CL6002D24 · Fuselage Structure (General)
  > UPPER CAP OF THE RBL9.00 AFT FLOOR BEAM AT FS693.00 WAS FOUND TO HAVE CORROSION DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-31-43-001-001-A03, FIGURE 53-31-43-991-801, ITEM 7, EA 79-2021-260.
- [SDR MASA20211124577](https://openairdocs.org/sdr/MASA20211124577.md): None · none · Nov 23, 2021 · N902FJ · Cndair CL6002D24 · Fuselage Structure (General)
  > FUSELAGE LOWER SKIN PANEL BETWEEN FS565 & FS581 AND STGR21R AND STGR22R WAS FOUND TO HAVE A PREVIOUS BLENDOUT. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-31-01, FIGURE 53-31-01-99-806, ITEM 1, EA 72-2021-217.
- [SDR MASA20211124576](https://openairdocs.org/sdr/MASA20211124576.md): None · none · Nov 23, 2021 · N902FJ · Cndair CL6002D24 · Fuselage Structure (General)
  > FUSELAGE LOWER SKIN PANEL BETWEEN FS597 & FS629 AND STGR20L & STGR22L WAS FOUND TO HAVE PREVIOUS BLENDOUTS. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-31-01, FIGURE 53-31-01-99-806, ITEM 1, EA 72-2021-216.
- [SDR MASA20211123574](https://openairdocs.org/sdr/MASA20211123574.md): None · dented · Nov 22, 2021 · N902FJ · Cndair CL6002D24 · Fuselage Floor Panel
  > FUSELAGE SKIN BETWEEN FS 421 - FS 437, STR 19L - STR 20L, WAS FOUND WITH A DENT. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-21-01-991-859, EA 20-2021-205.
- [SDR MASA20211123573](https://openairdocs.org/sdr/MASA20211123573.md): None · none · Nov 22, 2021 · N902FJ · Cndair CL6002D24 · Fuselage Structure (General)
  > FUSELAGE SKIN BETWEEN FS897.00 - FS927.00, STGR27, WAS FOUND WITH (2) PREVIOUS BLEND OUTS. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-51-01-001-003-A02, FIGURE 53-51-01-991-806, ITEM 1, D, EA 79-2021-257.
- [SDR MASA20211123572](https://openairdocs.org/sdr/MASA20211123572.md): None · dented · Nov 22, 2021 · N902FJ · Cndair CL6002D24 · Nacelle/Pylon Structure
  > LH ENGINE THRUST REVERSER FORWARD CORE COWL UPPER INBOARD FACING SHEET WAS FOUND WITH (6) MINOR DENTS. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 54-23-05-001-001-A01, EA 12-2021-268.
- [SDR MASA20211123571](https://openairdocs.org/sdr/MASA20211123571.md): None · none · Nov 22, 2021 · N902FJ · Cndair CL6002D24 · Fuselage Floor Panel
  > FUSELAGE SKIN LOWER PANEL BETWEEN FS280.00 -FS295.00 AND STGR24R -STGR26R WAS FOUND WITH CORROSION DAMAGE AND 4EA DENTS. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-21-01-001-002-A01, ITEM 1, D, E, EA 79-2021-251.

Next page: https://openairdocs.org/aircraft/N902FJ/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 = 'N902FJ' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N902FJ/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.