# Service difficulty reports: JASC 5541

A list on [JASC 5541](https://openairdocs.org/jasc/5541.md).

Reports filed under 5541 · Rudder, Spar/Rib, newest first.

Page 1 of 6 · 277 reports

- [SDR HNAA2026081400712](https://openairdocs.org/sdr/HNAA2026081400712.md): Rib · damaged · Aug 1, 2026 · N942LL · Emb EMB145LR
  > F143997 RUDDER I TOP RIB DAMAGED DURING REMOVAL OF HORIZONTAL STABILIZER. PERFORMED RE-CONTOUR AND SPLICE REPAIR TO THE RUDDER I TOP RIB IAW EMB ETD2026-145-01327 REV. A, AND EO1-55-26-0370
- [SDR 2025FA0000758](https://openairdocs.org/sdr/2025FA0000758.md): Spar · cracked · Nov 14, 2025 · N4981W · Gulstm 114
  > CRACK EMANATING FROM UPPER LEFT CORNER OF THE RUDDER SPAR AND DOWN BEHIND THE HINGE CONNECTION PLATE FOR APPROXIMATELY 3.5" AND THEN TURNS INBOARD FOR A DISTANCE OF 1/2 THE WIDTH OF THE SPAR. THE CRACK WAS FOUND DURING THE REMOVAL OF THE RUDDER TO CHANGE THE B
- [SDR SWIA2025F01379](https://openairdocs.org/sdr/SWIA2025F01379.md): Rib · corroded · Jul 27, 2025 · N461SW · Cndair CL6002B19
  > RUDDER BOTTOM RIB HAS CORROSION ON UPPER SIDE, HN00255797 (C-CHECK RO 09/24/2025)REMOVED CORROSION AND RESTORED FINISH ON REWORKED AREAS AT RUDDER BOTTOM RIB ON UPPER SIDE, COMPLIED TO ALL STEPS REO 601R-55-41-310 REV -- DATE: 2025-08-04 ( SEE CONTINUATION
- [SDR AALA202504151358](https://openairdocs.org/sdr/AALA202504151358.md): Frame · corroded · Apr 15, 2025 · N923NN · Boeing 737823
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION TO RUDDER CONDUCTIVE FRAME FROM RUDDER STA 257.9 TO STA 276. ACCOMPLISHED SPLICE REPAIR PER SRM 55-40-01-2R AND EA 363604.
- [SDR JJBA20250403019](https://openairdocs.org/sdr/JJBA20250403019.md): Rib · cracked · Mar 27, 2025 · N24128 · Emb EMB145XR
  > RUDDER II, FWD ON FRONT SPAR, UPPER RIB CRACKED AT UPPER MID HINGE FITTING. RUDDER II, FWD OF FRONT SPAR UPPER MID HINGE FITTING UPPER RIB REPLACED.
- [SDR TSAA2024112600019](https://openairdocs.org/sdr/TSAA2024112600019.md): Frame · corroded · Nov 23, 2024 · N301KH · Boeing 737330
  > CORROSION (19.0" X 1.0") RH SIDE CONDUCTIVE FRAME TRAILING EDGE AT RUD STA 233~252. CORROSION REMOVED LEVEL 1 AT RH SIDE CONDUCTIVE FRAME TRAILING EDGE AT RUD STA 233~252 FROM PN 65C31496-4 AFTER REMOVED SKIN THROUGH REPLACED CONDUCTIVE FRAME I.A.W B737-300 S
- [SDR NACA2024070500009](https://openairdocs.org/sdr/NACA2024070500009.md): Frame · corroded · Jul 5, 2024 · N405YK · Boeing 737436
  > CORROSION AT RH SIDE RUDDER CONDUCTIVE FRAME AT RUDDER STA 234. REMOVED CORROSION AND REPLACED CONDUCTIVE FRAME IAW SRM 55-40-01 AND CMM 55-40-12
- [SDR NACA2024070500008](https://openairdocs.org/sdr/NACA2024070500008.md): Frame · corroded · Jul 5, 2024 · N405YK · Boeing 737436
  > CORROSION AT LH SIDE RUDDER CONDUCTIVE FRAME AT RUDDER STA 234. REMOVED CORROSION AND REPLACED CONDUCTIVE FRAME IAW SRM 55-40-01 AND CMM 55-40-12
- [SDR AALA202311309908](https://openairdocs.org/sdr/AALA202311309908.md): Frame · peeling · Nov 27, 2023 · N867NN · Boeing 737823
  > AIRCRAFT WAS GROUNDED: SHEET METAL PEELING UP ON TOP AFT OF RUDDER. REPAIRED RUDDER CONDUCTIVE FRAME PER AARD 55-40-01, SEE NON ROUTINE WORK RECORD 1023003.
- [SDR AALA202307187153](https://openairdocs.org/sdr/AALA202307187153.md): Frame · cracked · Jul 13, 2023 · N800NN · Boeing 737823
  > AIRCRAFT IN BASE MAINTENANCE: CRACK IN RUDDER SKIN CONDUCTIVE FRAME LOCATED AT RUDDER STA 282. REPAIRED FRAME PER SRM 55-40-01-2R PROCEDURE 2 REPAIR 2.
- [SDR WX0A2022091674247](https://openairdocs.org/sdr/WX0A2022091674247.md): None · none · Sep 15, 2022 · N289NV · Airbus A320214
  > REF. W/O 463019-2 PERMANENT REPAIR OF RUDDER DAMAGE REQUIRES REPAIR/PERFORMED RUDDER SKIN REPAIR AROUND TRAILING EDGE SCREW LINE IN THE GFRP AREA UP TO STEP 2.A.2 H.13 SRM 55-41-13-300-025.COMPLETED RUDDER SKIN REPAIR AROUND TRIALING EDGE SCREW IN GFRP AREA FR
- [SDR SWIA202266637](https://openairdocs.org/sdr/SWIA202266637.md): None · worn · Sep 14, 2022 · N779SK · Cndair CL6002C10
  > RUDDER ASS'Y FAILED BACKLASH CHECK, V-STAB REAR SPAR RUDDER HINGE FITTING #2 (UPR MIDDLE) SPHERICAL BEARING HAS EXCESSIVE PLAY (C-CHECK RO 10/24/2022) REMOVED AND REPLACED WORN SPHERICAL BEARING AT V-STAB REAR SPAR RUDDER HINGE FITTING #2 (UPR MIDDLE) W
- [SDR SWAA2022082539485](https://openairdocs.org/sdr/SWAA2022082539485.md): Rib · cracked · Aug 7, 2022 · N264LV · Boeing 7377H4
  > CRACK DORSAL FIN PANEL 321A RIB AT BS 867 AT VERTICAL STABILIZER 2022-423338 / [01] TOOL USED:CALIPER P/N 4996A52 S/N 201219744 CAL DUE DATE 22 FEB 23.;[02] REPLACED RIB AND FASTENERS LOCATED ON DORSAL FIN PANEL 321A RIB AT BS 867 AT VERTICAL STABILIZER IAW B7
- [SDR REXA2022032400492](https://openairdocs.org/sdr/REXA2022032400492.md): Spar · deformed · Mar 10, 2022 · N8970D · Cndair CL6002B19
  > RUDDER LEADING EDGE HAS DAMAGE TO LIGHTING HOLE AT FRONT SPAR LOWER SECTION JC:55-320-519 EMP#:2006BRT REPAIRED RUDDER L/E LIGHTING HOLE @ FRONT SPAR IAW ENDEAVOR E.A. CRJ255-13042
- [SDR SWIA202265153](https://openairdocs.org/sdr/SWIA202265153.md): None · grooved · Mar 1, 2022 · N103SY · Emb ERJ170200LR
  > RUDDER #1 HINGE BOLT AND FLOATING BUSHING ARE GROOVED. (C CHECK RO 3-21-22) REPLACED RUDDER #1 HINGE BOLT AND FLOATING BUSHING. REFERENCE CP 24320822 FOR FINAL INSTALL. REF EMB 175 AMM 27-21-05
- [SDR SWIA202265152](https://openairdocs.org/sdr/SWIA202265152.md): None · grooved · Mar 1, 2022 · N103SY · Emb ERJ170200LR
  > RUDDER #2 HINGE BOLT IS GROOVED. (C CHECK RO 3-21-22) REPLACED RUDDER #2 HINGE BOLT ON RACK. REFERENCE CP 24320822 FOR FINAL INSTALL. REF EMB 175 AMM 27-21-05
- [SDR SWIA202265151](https://openairdocs.org/sdr/SWIA202265151.md): None · grooved · Mar 1, 2022 · N103SY · Emb ERJ170200LR
  > RUDDER #3 HINGE BOLT AND FLOATING BUSHINGS ARE GROOVED. (C CHECK RO 3-21-22) REPLACED RUDDER #3 HINGE BOLT AND FLOATING BUSHINGS ON RACK. REFERENCE CP 24320822 FOR FINAL INSTALL. REF EMB 175 AMM 27-21-05
- [SDR SWIA202265155](https://openairdocs.org/sdr/SWIA202265155.md): None · worn · Feb 28, 2022 · N103SY · Emb ERJ170200LR
  > LATE FIND-LH ELEVATOR #1 HINGE BOLT AND BUSHING WORN (C CHECK RO 3-21-22) REPLACED LH ELEVATOR #1 HINGE BOLT AND BUSHING ON RACK. REFERENCE CP 24320802 FOR FINAL INSTALL. REF EMB 175 AMM 27-31-05
- [SDR SWIA202265154](https://openairdocs.org/sdr/SWIA202265154.md): None · worn · Feb 28, 2022 · N103SY · Emb ERJ170200LR
  > LATE FIND-LH ELEVATOR #3 HINGE BOLT AND NUT WORN (C CHECK RO 3-21-22) REPLACED LH ELEVATOR #3 HINGE BOLT AND NUT ON RACK. REFERENCE CP 24320802 FOR FINAL INSTALL. REF EMB 175 AMM 27-31-05
- [SDR SWIA202163253](https://openairdocs.org/sdr/SWIA202163253.md): None · damaged · Nov 16, 2021 · N773SK · Cndair CL600*
  > R/H AILERON AFT SPAR #2 I/B HINGE FITTING BUSHING BORE IS PITTED (C-CHECK RO 12/26/2021) REMOVED AND REPLACED R/H AILERON AFT SPAR #2 I/B HINGE FITTING BUSHING. COMPLIED WITH REO 670-57-51-464 REV-- DATED 2021-11-24. / COMPLIED WITH SKYWEST TASKCARD 51-
- [SDR SWIA202162727](https://openairdocs.org/sdr/SWIA202162727.md): None · misaligned · Oct 23, 2021 · N774SK · Cndair CL600*
  > VERTICAL STABILIZER TRAILING EDGE RUDDER MIDDLE LOWER HINGE DOES NOT LINE UP CORRECTLY. (C-CHECK RO 11-20-2021) REMOVED MIDDLE LOWER HINGE ON VERTICAL STABILIZER TRAILING EDGE REF. CRJ700 SRM 51-42-21-001-001-A01 AND INSTALLED MIDDLE LOWER HINGE ON VERTIC
- [SDR LR7A2021070802870](https://openairdocs.org/sdr/LR7A2021070802870.md): Stiffener · cracked · Jul 8, 2021 · N401LC · Lkheed 382G
  > SUPPLEMENTAL INFORMATION DURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5511, FOUND THE RUDDER LOWER INTERIOR STRUCTURE WITH CRACKED MAIN BEAM STIFFENER AT FS1150, RBL6, VSS33. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-19. NR# 1000461150.
- [SDR LR7A2021070902870](https://openairdocs.org/sdr/LR7A2021070902870.md): Stiffener · cracked · Jul 8, 2021 · N401LC · Lkheed 382G44K30
  > DURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5511, FOUND THE RUDDER LOWER INTERIOR STRUCTURE WITH CRACKED MAIN BEAM STIFFENER AT FS1150, RBL6, VSS33. / REPAIRED IAW LAC MEA 382-55-21-031. NR# 1000461150.
- [SDR SIMA20210113004](https://openairdocs.org/sdr/SIMA20210113004.md): Skin · cracked · Jan 13, 2021 · N908AE · Emb EMB145LR
  > RUDDER II FWD SPAR SKIN APPEARS TO HAVE A CRACK PROTRUDING FROM A HIGH LOCK FOR THE MIDDLE LOWER ATTACH POINT. VIEWED THREW ACCESS PANEL 327 BL. C/A: R & R RUDDER, IAW AMM 27-20-02, REF NON-ROUTINES E839469, E839910 AND E839976 FOR GAP CHECKS, FCF AND BACKLA
- [SDR AALA202012219002](https://openairdocs.org/sdr/AALA202012219002.md): Frame · damaged · Dec 20, 2020 · N883NN · Boeing 737823
  > AIRCRAFT IN BASE MAINTENANCE. RUDDER LEFT UPPER CONDUCTIVE FRAME UNDERNEATH LOWER STATIC WICK BASE HAS HOLE AT RSTA 282.12. REMOVED FRAME AND DAMAGED SKIN. REPAIRED IAW B737NG SRM 55-40-01-2R-2, B737NG SRM 51-70-10, AND B737NG SRM 51-70-04-2R-1.
- [SDR KCSA202006261098](https://openairdocs.org/sdr/KCSA202006261098.md): Rib · cracked · Jun 26, 2020 · N741CK · Boeing 7474H6
  > UPPER RUDDER HAS A 17 INCH CRACK ON INTERSPAR RIB AT RUDDER STA 146.7 UNDER PANEL 326AL
- [SDR SIMA2020040702007](https://openairdocs.org/sdr/SIMA2020040702007.md): Rib · dented · Apr 2, 2020 · N607AE · Emb EMB145LR
  > RUDDER 1 LEADING EDGE RIB BELOW CENTER HINGE FITTINGS (ZV=1897.0) IS DENTED.-C/A-REMOVED AND REPLACED RIB AT ZV=1897.0 FOR RUDDER LEADING EDGE BELOW CENTER HINGE FITTING IAW SRM 51-40-02.
- [SDR SIMA2020040602004](https://openairdocs.org/sdr/SIMA2020040602004.md): Rib · bent · Apr 2, 2020 · N607AE · Emb EMB145LR
  > RUDDER 1 SKIN SUPPORT FLANGE (RIB) AT THE LOWER CENTER HINGE IS BENT.-C/A-REMOVED AND REPLACED RIB IAW EMB SRM 51-40-02.
- [SDR SIMA2020040602003](https://openairdocs.org/sdr/SIMA2020040602003.md): Rib · bent · Apr 2, 2020 · N607AE · Emb EMB145LR
  > RUDDER 1 SUPPORT FLANGE SKIN AT THE UPPER CENTER HINGE IS BENT.-C/A-REMOVED AND REPLACED RIB IAW EMB SRM 51-40-02.
- [SDR SIMA2020040602005](https://openairdocs.org/sdr/SIMA2020040602005.md): Rib · damaged · Apr 2, 2020 · N607AE · Emb EMB145LR
  > RUDDER 1 LEADING EDGE RIB ABOVE CENTER HINGE FITTINGS (ZV=2312.0) HAS DAMAGED FLANGE ON INTERIOR SIDE.-C/A- REMOVED AND REPLACED RIB AT ZV=2312.0 IAW EMB SRM 51-40-02.
- [SDR SWAA2021081732667](https://openairdocs.org/sdr/SWAA2021081732667.md): Frame · deformed · Mar 5, 2020 · N947WN · Boeing 7377H4
  > TRANSFERRED FROM DIS# 1105520 DURING WALK AROUND CHECK; FOUND RUDDER LEFT SIDE CON DUCTIVE FRAME WAS DEFORMED. DAMAGE IS 6 IN LONG X 3 IN WIDE / REMOVED & REINSTALLED RUDDER (P/N 173A0103-10; S/N CASA-1318) PER M/M 27-21-11. REFERENCE RO # 0550042-70R FOR REP
- [SDR ASAA2019122431666](https://openairdocs.org/sdr/ASAA2019122431666.md): Spar · punctured · Dec 14, 2019 · N526VA · Airbus A319112
  > RUDDER FWD SPAR FRONT FACE LOWER R/H CORNER PUNCTURED JUST ABOVE #1 ATTACH FITTING GROUNDED - YES. REPAIR RUDDER FWD SPAR FRONT FACE LOWER R/H CORNER PUNCTURE IAW A319-111 SRM: 51-42-00, 51-77-11-911-008, 51-75-12, 54-42-21, 55-31-11-300-017, NTM: 51-90-00, 51
- [SDR 7C7A2019110800518](https://openairdocs.org/sdr/7C7A2019110800518.md): Spar · gouged · Nov 8, 2019 · N892EA · Dhav DHC8106
  > GOUGE DAMAGE TOO FORE RUDDER, FRONT SPAR ON R/H SIDE AT RIB# 25. THE PERMANENT REPAIR FOR GOUGE DAMAGE TO FORE RUDDER, FRONT SPAR ON THE R/H SIDE AT RIB#25 WILL BE ACCOMPLISHED IAW DEHAVILLAND AIRCRAFT OF CANADA LIMITED RD 8-55-3406 ISSUE 1 DATED 08 NOVEMBER
- [SDR JGVR20190919006](https://openairdocs.org/sdr/JGVR20190919006.md): Rib · cracked · Sep 19, 2019 · N376QS · Cessna 680CE
  > REPAIRED RUDDER BY REPLACING CRACKED LOWER AFT RIB AND CLIP WITH NEW RIB P/N 6933160-3 AND CLIP P/N 6933160-2 PER SRM 51-40-03, 51-40-06, 51-40-09, AND CSPM 20-40-20.
- [SDR LR7A2019062401961](https://openairdocs.org/sdr/LR7A2019062401961.md): Frame · corroded · Jun 24, 2019 · N409LC · Lkheed 382G
  > DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5511, FOUND THE RUDDER LOWER FRAME WEB CORRODED BEYOND LIMITS AT SEVERAL PLACES. FS1128-1200, LBL12-RBL12, WL286. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6270.
- [SDR AALA201905239022](https://openairdocs.org/sdr/AALA201905239022.md): Frame · peeling · May 21, 2019 · N768AA · Boeing 777223
  > AIRCRAFT WAS GROUNDED: RUDDER TOP RIGHT HAND SURFACE CONDUCTIVE FRAME LOWER CORNER PEELING. REPAIRED CONDUCTIVE FRAME PER AARD 55-40-00-1.
- [SDR CA190308014](https://openairdocs.org/sdr/CA190308014.md): Rib · corroded · Mar 8, 2019 · Aerosp ATR42500
  > (CAN) UPPER RUDDER MACHINED RIB CORRODED.
- [SDR RAIA2019020400002](https://openairdocs.org/sdr/RAIA2019020400002.md): Rib · damaged · Jan 24, 2019 · N31131 · Emb EMB145XR
  > RUDDER #2 2ND NOSE RIB FROM BOTTOM DAMAGED AT L/H NUTPLATE- REMOVED DAMAGED RIB ON #2 RUDDER NOSE BOTTOM AT L/H AND STARTED LOCATING FASTNER HOLES. DRILLED UP AND INSTALLED NEW RIB ON RUDDER, PAINT REQUIRED. REMOVED & REPLACED #2 RUDDER 2ND LWR NOSE R
- [SDR CA190321002](https://openairdocs.org/sdr/CA190321002.md): Rib · cracked · Jan 15, 2019 · Cessna 152
  > (CAN) LOWER RIB PART NUMBER 043301015 WAS FOUND CRACKED DURING INSPECTION.
- [SDR V6NA201902192019](https://openairdocs.org/sdr/V6NA201902192019.md): Rib · cracked · Dec 18, 2018 · N255SL · Lear 60LEAR
  > AT SCHEDULED INSPECTION, DISCOVERED RUDDER RIB AT WL 126.0 TO BE CRACKED. RIB REPAIRED WITH DOUBLER PER LEARJET 60 STRUCTURAL REPAIR MANUAL SECTION 55-40-01.
- [SDR ASOA2018102485275](https://openairdocs.org/sdr/ASOA2018102485275.md): Rib · corroded · Oct 18, 2018 · N783CA · Cndair CL6002B19
  > REF: CO 7315618 JOB 7731568 OP 36: RUDDER BOTTOM RIB P/N 600-22032 HAS EVIDENCE OF CORROSION. C/A:REPAIRED DAMAGE IAW SRM 51-21-06, 55-40-00, 51-25-01, STS EA 32-2018-208 AND EC/TC EA 32-2018-208 WO#559076.
- [SDR DXTA2018FA0000361](https://openairdocs.org/sdr/DXTA2018FA0000361.md): Spar Web · damaged · Sep 11, 2018 · N338QS · Cessna 680CE
  > REPAIR OF RUDDER FWD SPAR LIGHTENING HOLE DAMAGED FLANGE. ENGINEERING REPAIR LETTER DQ1562M1 DATED SEPTEMBER 6, 2018.
- [SDR EBVR20170406001](https://openairdocs.org/sdr/EBVR20170406001.md): Rib · corroded · Apr 6, 2017 · N672QS · Cessna 560XL
  > CORROSION FOUND ON LOWER RIB OF THE RUDDER AT THE BONDING POINT. REPAIRED EXISTING LOWER RUDDER TORQUE TUBE RIB PER AQRD ERO-891028 REV IR. ATTACHED NEW REPAIR DOUBLER TO LOWER RIB OF RUDDER WET WITH PS870B1/2 LOT# 70540 AND CR3213-4-2 RIVETS.
- [SDR QXEA2017030100093](https://openairdocs.org/sdr/QXEA2017030100093.md): Rib · corroded · Feb 24, 2017 · N404QX · Bombdr DHC8402
  > FORE RUDDER, NOSE RIB 9 CORRODED. NOSE RIB 9 AND STRAP REMOVED IAW SRM 51-42-05. NEW NOSE RIB 9 AND STRAP INSTALLED IAW SRM 51-42-05.
- [SDR 7C7A2017013100283](https://openairdocs.org/sdr/7C7A2017013100283.md): Rib · cracked · Jan 31, 2017 · N884EA · Dhav DHC8106
  > TRAILING RUDDER, CENTER HINGE, TOP LEADING EDGE RIB CRACKED
- [SDR 4AER20161102007](https://openairdocs.org/sdr/4AER20161102007.md): Frame · corroded · Sep 17, 2016 · N285XA · Boeing 7374Q8
  > RIGHT HAND RUDDER UPPER AFT CORNER CONDUCTIVE FRAME AT RUDDER STATION 234.89 HAS CORROSION.
- [SDR IPXA2016101109236](https://openairdocs.org/sdr/IPXA2016101109236.md): Rib · corroded · Sep 16, 2016 · N258UP · Doug MD11F
  > INSPECTION TYPE: 3C, RIB CORRODED INSIDE UPPER FWD RUDDER. REMOVED, FABRICATED, AND INSTALLED A REPLACEMENT RIB IAW DWG AMC7292 AND SRM 51-35-01.
- [SDR IGXR20160921004](https://openairdocs.org/sdr/IGXR20160921004.md): Trim Tab · cracked · Sep 7, 2016 · N657QS · Cessna 560XL
  > THE LOWER AFT CORNER OF THE RUDDER TRIM HAS A CRACK MEASURING 0.76 INCHES LONG. PERFORMED PERMANENT REPAIR USING APPROVED ENGINEERING ORDER ERO-859505.
- [SDR JJBA20160514008](https://openairdocs.org/sdr/JJBA20160514008.md): Rib · damaged · May 14, 2016 · N839CA · Dhav DHC8311
  > DAMAGE FOUND ON TOP OF TRAILING RUDDER. REMOVED DAMAGE ON TOP OF TRAILING RUDDER.
- [SDR DALA2016051203953](https://openairdocs.org/sdr/DALA2016051203953.md): Tab · unknown · May 11, 2016 · N964DN · Doug MD9030
  > FLAME SPRAY COAT ON RUDDER CONTROL TAB. REPAIRED IAW SRM 55-41-01.

Next page: https://openairdocs.org/jasc/5541/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 jasc_code = '5541'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/jasc/5541/reports

---
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