JASC 5544

Service difficulty reports · 270

Reports filed under 5544 · Rudder Miscellaneous Structure, newest first.

Query with SQL
duckdb -csv -c "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 = '5544'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR SWIA2026082176937Angle · crackedFOUND A CRACK IN RUDDER SUPPORT STRUCTURE ON ANGLE, CONNECTING TO SUPPORT MEMBER AT RS 40.458 ON ITEM 167 STATION RIB IAW SRM 55-40-00, FIG 1, SHEET 13. MANUFACTURED AND INSTALLED REPLACEMENT RUDDER SUPPORT STRUCTURE ANGLE(RHS) LOCATED AT RS40.458 BY COMPLYAug 21, 2026 · N459SW · Cndair CL6002B19SDR UIEA2026061700516Web · crackedRUDDER STA 207.6 THE WEB FOUND CRACKED, 3CM LENGTH AT LT FWD CORNER. WEB REPAIRED IAW RI-55-40-18393 REV A. NO FURTHER DEFECTS NOTED.Jul 29, 2026 · N485MC · Boeing 74745EFSDR HNAA2026101500992Nut Plate · missing824 PROTRACTOR NUTPLATE MISSING ON FORE RUDDER LH SIDE. REPAIRED IAW SRM 55-41-01Jul 21, 2026 · N650AE · Emb EMB145LRSDR HNAA2026081400717Fitting · damagedRUDDER I LOWER ACTUATOR FITTING UPPER DOUBLE HAT BUSHING UPPER HAT BUSHING FITS LOOSE IN FITTING. REMOVED AND REPLACED 2 HAT BUSHINGS WITH 2 OVERSIZE HAT BUSHINGS, REAMED RUDDER I LOWER ACTUATOR FITTING UPPER DOUBLE HAT BUSHING HOLE TO (.7543") TO ACCOMODATE Jul 9, 2026 · N942LL · Emb EMB145LRSDR AALA202607150605Balance Weight · corrodedAIRCRAFT IN BASE MAINTENANCE: RUDDER BALANCE WEIGHT SHOW SIGN OF CORROSION . MAINTENANCE REPLACED RUDDER BALANCE WEIGHTI AW B737-NG AMM 55-40-00-000-801C1 AND B737-NG-AMM-55-40-00-400-801C1. IPC VERIFIED IAW B737-NG-AIPC-27-21-11-22.Jun 24, 2026 · N807NN · Boeing 737823SDR SWAA2026061510784Balance Weight · corrodedRUDDER COUNTER BALANCE WEIGHT CORRODED AND ERODED. REPLACED THE RUDDER BALANCE WEIGHT IAW CMM 55-40-09.Jun 10, 2026 · N287WN · Boeing 7377H4SDR 4VAA202605130015Mount · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE RUDDER FRONT SPAR LEFT HAND AND RIGHT HAND LEADING EDGE PANEL MOUNT SCREW HOLES. IT WAS REPAIRED IN ACCORDANCE WITH SAAB STATEMENT 2000SDS060677.May 12, 2026 · N749SA · Saab 2000SAABSDR HNAA2026061700514Bracket · gougedRUDDER 2 LOWER SECTION INTERNAL BRACKET IS GOUGED. REMOVED AND REPLACED INTERNAL BRACKET ON RUDDER 2 LOWER SECTION PER SRM 51-40-02.May 7, 2026 · N657AE · Emb EMB145LRSDR SWAA2026033184022Frame · debondedRUDDER LT CONDUCTIVE FRAME DEBONDED. REMOVED DAMAGED CONDUCTIVE FRAME PER SRM 51-10-02 GENERAL ; AND FASTENERS PER SRM 51-40-02. ACCOMPLISHED PERMANENT REPAIR OF CONDUCTIVE FRAME ZONE 3. IAW SRM 55-40-01-1A-3 ALLOWABLE DAMAGE 3. RUDDER BALANCE ACCOMPLISHED ONMar 28, 2026 · N248WN · Boeing 7377H4SDR SWIA2026031175964Angle · crackedAFT RUDDER QUADRANT SUPPORT STRUCTURE LT FWD ANGLE IS CRACKED AT VERTICAL STAB MID SPAR (VS 43.75%). REMOVED AND REPLACED THE AFT RUDDER QUADRANT SUPPORT STRUCTURE LH FWD ANGLE AT VERTICAL STAB MID SPAR (VS 43.75%) IN REFRERENCE WITH THE SRM 51-42-06 AND SRM Mar 11, 2026 · N915SW · Cndair CL6002B19SDR JJBA20260217038Pulley Bracket · corrodedAFT WET AREA 1EA RUDDER CABLE PULLEY IB BRACKET AT FR 61 HAS CORROSION. REMOVED AND REPLACED AFT WET AREA 1 EACH RUDDER CABLE PULLEY INBD BRACKET AT FR61Feb 12, 2026 · N14168 · Emb EMB145XRSDR JJBA20250217037Pulley Bracket · corrodedAFT WET AREA 1EA RUDDER CABLE PULLEY OB BRACKET AT FR 61 HAS CORROSION. REMOVED AND REPLACED AFT WET AREA 1 EACH RUDDER CABLE PULLEY OUTBD BRACKET AT FR61Feb 12, 2026 · N14168 · Emb EMB145XRSDR SWAA2026021269215Balance Weight · corrodedRUDDER BALANCE WEIGHT HAS PAINT PEELING DOWN TO BARE METAL AND SIGNS OF CORROSION IN AND AROUND THE FOUR FORWARD BOLT HOLES. REMOVED & REPLACED RUDDER BALANCE WEIGHT IAW CMM 55-40-09.Feb 10, 2026 · N8846Q · Boeing 7378SDR JJBA20260217040Frame Angle · corrodedAFT WET AREA 1EA RUDDER CABLE PULLEY IB FWD FRAME CLIP AT FR 60 HAS CORROSION. REMOVED AND REPLACED AFT WET AREA 1 EACH RUDDER CABLE PULLEY INBD FWD FRAME CLIP AT FR60Feb 7, 2026 · N14168 · Emb EMB145XRSDR JJBA20260217039Pulley Bracket · corrodedAFT WET AREA 1EA RUDDER CABLE PULLEY OB FWD FRAME CLIP AT FR 60 HAS CORROSION. REMOVED AND REPLACED AFT WET AREA 1 EACH RUDDER CABLE PULLEY OUTBD FWD FRAME CLIP AT FR60Feb 7, 2026 · N14168 · Emb EMB145XRSDR SWAA2025121050129Frame · debondedLEFT CONDUCTIVE FRAME AT RUDDER WAS DISBONDED REF TLD 25-155-03112 TTG8Q018TDJK. REMOVED 6.125 IN. SECTION OF DISBONDED LOWER CONDUCTIVE FRAME AT RUDDER TE IAW SRM 55-40-01-1A-3. REMOVED SIX RIVETS AT RUDDER TE TO FOM IAW SRM 51-40-02. PERFORMED PERMANENT Dec 6, 2025 · N8324A · Boeing 7378H4SDR AALA202512189616Strip · splitAIRCRAFT IN BASE MAINTENANCE: RUDDER APEX STRIP FOUND TO BE SPLITTING IN TWO AREAS. APPROXIMATELY 2 FEET AND 4 FEET FROM BOTTEM EDGE. MAINTENANCE REPAIRED RUDDER PER SRM 55-41-19-300-011.Nov 30, 2025 · N117UW · Airbus A320214SDR AALA202512039616Structure · splitAIRCRAFT IN BASE MAINTENANCE: RUDDER APEX STRIP FOUND TO BE SPLITTING IN TWO AREAS. APPROXIMATELY 2 FEET AND 4 FEET FROM BOTTEM EDGE. **SUPPLEMENTAL REPORT WILL BE SUBMITTED ** (OPEN)Nov 30, 2025 · N117UW · Airbus A320214SDR DALA2025120108759Hinge Arm · corrodedVERTICAL STABILIZER, RUDDER HINGE ARM #4 THE FASTENER HOLE WITH CORROSION. CORRECTIVE ACTION: COMPLIED QITH ER/A 630371-14. (1325852).Nov 28, 2025 · N354NB · Airbus A319114SDR DALA2025120108758Hinge Arm · corrodedVERTICAL STABILIZER, RUDDER HINGE ARM #3 THE FASTENER HOLE WITH CORROSION. COMPLIED WITH ER/A 630371-14. (1325843).Nov 28, 2025 · N354NB · Airbus A319114SDR DALA2025101707585Hinge Arm · corrodedVERTICAL STABILIZER RUDDER HINGE ARM BR3 CRACKED HOLE. REPAIRED PER ER/A 629756-14. (1255486)Oct 16, 2025 · N324NB · Airbus A319114SDR AALA202510133934Strip · splitAIRCRAFT IN BASE MAINTENANCE: TRAILING EDGE OF RUDDER ON THE LOWER CORNER IS SPLITTING AND HAS A PULLED RIVET. REPAIRED RUDDER APEX STRIP PER SRM 55-41-19-300-004.Sep 20, 2025 · N155NN · Airbus A321231SDR SWIA2025120800919Hinge Fitting · looseRUDDER CENTER HINGES BEARING (TOP & BOTTOM) ON VERTICAL STABILIZER SIDE HAS EXCESSIVE PLAY. INSTALLED NEW UPPER AND LOWER RUDDER CENTER HINGE FITTINGS P/N AV670-21081-015 AND (1EA) AND P/N AV670-21081-013 (1EA) PER DWG.AV670-21200 REV H AND REF.CRJ/700 SRM. Sep 19, 2025 · N633SK · Cndair CL6002C10SDR SWAA2025100614847Seal · debondedRUDDER BLADE SEAL 324AAL DISBONDED. REPLACED RUDDER BLADE SEAL 324AAL ON SHELF IAW AIPC 55-30-00-21 ITEM 30 PG. 6.Sep 16, 2025 · N966WN · Boeing 7377H4SDR SWAA2025100614848Seal · debondedRUDDER BLADE SEAL 324ABL DISBONDED. REPLACED RUDDER BLADE SEAL 324ABL ON SHELF IAW AIPC 55-30-00-21 ITEM 25 PG. 6.Sep 16, 2025 · N966WN · Boeing 7377H4SDR SWAA2025100614849Seal · debondedRUDDER BLADE SEAL 324RL DISBONDED. REMOVED AND REPLACED ON SHELF REF IPC 55-30-00-31 ITEM 75.Sep 16, 2025 · N966WN · Boeing 7377H4SDR SWAA2025100614850Seal · debondedDOT A24-16 RUDDER BLADE SEAL 324ZL DISBONDED. REPLACED RUDDER BLADE SEAL 324ZL ON SHELF IAW AIPC 55-30-00-21 ITEM 35 PG. 7.Sep 16, 2025 · N966WN · Boeing 7377H4SDR AALA202507251794Strip · delaminatedAIRCRAFT IN BASE MAINTENANCE: BOTTOM OF RUDDER TRAILING EDGE DELAMED AT APEX STRIP. REPAIRED APEX STRIP PER SRM 55-41-19-300-004 AND SRM 51-75-12.Jul 23, 2025 · N544UW · Airbus A321231SDR REXA2025063000702Hinge Fitting · chafedVERTICAL STABILIZER MID LOWER HINGE ASSY., LOWER HINGE HALF P/N AV670-21140-001 HAS AN EXCESSIVELY WORN BEARING LANDING. COMPLIED WITH MHIRJ REO 670-55-31-192 REV-- DATED 2025-06-20. INSTALLED NEW SERVICABLE LOWER HINGE P/N AV670-21081-013.Jun 30, 2025 · N340CA · Cndair CL6002C10SDR CALA2025060505291Access Panel · crackedRUDDER HINGE ACCESS PANEL 324CL COMPOSITE IS DISBONDED. EVALUATED RUDDER HINGE ACCESS PANEL 324CL AND FOUND 3EA DAMAGED FASTENER HOLES REQUIRING REPAIR IAW UAL B757-200 SRM 55-30-01-1A -1 ALLOWABLE DAMAGE 1. REPAIRED IAW B757-200 SRM 55-30-01-2R-3, SRM 51-70May 30, 2025 · N12114 · Boeing 757224SDR UIEA2024071500675Structure · chafedLWR RUDDER L/H LWR CHORD FOUND CHAFING(<P>LWR CHORD CHAFING AREA REPAIRED AS PER RI-55-40-17002 REV.B. NO FURTHER DEFECTS NOTED.Jul 17, 2024 · N487MC · Boeing 74745EFSDR JGVR20230324002Unknown · unknownREPLACED CORRODED RUDDER FAIRING INNER SUPPORT RIB P/N UNKNOWN WITH NEW TEXTRON P/N 6912670-5 PER CESSNA 680A SRM 51-40-05 AND 51-40-11 AND DUNCAN AVIATION PROCESS GPP-0105 REV. 9.Mar 24, 2023 · N535QS · Cessna 680ASDR AALA202208049351Balance Weight · corrodedAIRCRAFT WAS GROUNDED: RUDDER BALANCE WEIGHT HAS SMALL AREA OF CORROSION ON LEFT SIDE. **SUPPLEMENTAL REPORT FOR AALA202207199351: REPLACED BALANCE WEIGHT PER CMM 55-40-09.** (CLOSED)Jul 16, 2022 · N891NN · Boeing 737SDR AALA202207199351Balance Weight · corrodedAIRCRAFT WAS GROUNDED: RUDDER BALANCE WEIGHT HAS SMALL AREA OF CORROSION ON LEFT SIDE. **SUPPLEMENTAL REPORT REQUIRED** (OPEN)Jul 16, 2022 · N891NN · Boeing 737823SDR AALA202204299436Hinge Arm · wornAIRCRAFT IN BASE MAINTENANCE: WHILE ACCOMPLISHING THE RUDDER HINGE LINE MODIFICATION EO 5520Y001, FOUND HOLES ON THE #2 HINGE ARM FITTING ELONGATED. REPAIRED HINGE ARM FITTING PER EA 335807Apr 28, 2022 · N191UW · Airbus A300*SDR DATA2022040800001Torque Tube · corrodedRUDDER TORQUE TUBE SHOWS CORROSION BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED TORQUE TUBE WITH A SERVICEABLE PART.Apr 5, 2022 · N360AB · Stbros SD360SDR DATA2021101201Torque Tube · corrodedRUDDER BOTTOM TORQUE TUBE CORRODED. REMOVED AND REPLACED RUDDER BOTTOM TORQUE TUBE WITH A NEW PART.Oct 5, 2021 · N4498Y · Stbros SD360SDR AALA202110069821Rudder · corrodedAIRCRAFT WAS GROUNDED: CORROSION ON RUDDER RIGHT HAND LOWER TRAILING EDGE. REMOVED CORROSION AND REPLACED APEX STRIP PER SRM 51-41-19-300-006.Oct 2, 2021 · N8009T · Airbus A319115SDR SWAA2021101418446Balance Weight · corrodedRUDDER BEAM ARM BALANCE WEIGHT CORRODED.(PICS IN ATTACHMENTS) ; / [01] REMOVED AND REPLACED RUDDER BALANCE ARM WEIGHT PER REF CMM55-40-09 / SRM51-60-07; [02] REMOVED AND REPLACED RUDDER BALANCE ARM WEIGHT PER REF CMM55-40-09 / SRM51-60-07Sep 15, 2021 · N904WN · Boeing 7377H4SDR SWAA2021110917669None · delaminatedRUDDER L/E BY CENTER AREA WEIGHT BALANCE PANEL DELAMINATED ; / [01] REMOVED RUDDER WEIGHTBALANCE AS PER B737-700 CMM 55-40-09; [02] PERFORMED WIEGHT THE REMOVED BALANCE WEIGHT FOUND WEIGHT= 43.40 LBS; [03] PERFORMED WIEGHT THE NEW SERVISEABLE RUDDER BALANCE WESep 13, 2021 · N783SW · Boeing 737*SDR IPXA2020041554220Mount Fitting · gougedINSPECTION TYPE:3CLOWER AFT RUDDER EYE BOLT MOUNT FITTING WAS FOUND GOUGED.REPAIRED LOWER AFT RUDDER EYE BOLT MOUNT FITTING IAW VT-SAA EA 011-5540-01-A8101 REV. I/R AND UPS EO MD11-5540-76126-A. (MINOR)Mar 17, 2020 · N278UP · Doug MD11FSDR IPXA2020040853996Attach Fitting · gougedINSPECTION TYPE:3CUPPER AFT RUDDER UPPER ATTACH FITTING IS GOUGED.REPAIRED GOUGED UPPER AFT RUDDER UPPER ATTACH FITTING IAW VT-SAA EA 011-5542-01-A8111 REV. IR AND UPS EO MD11-5540-76080-A (MINOR)Mar 13, 2020 · N278UP · Doug MD11FSDR IPXA2020040853998Fitting · gougedINSPECTION TYPE:3CLOWER AFT RUDDER LOWER MOUNT FITTING IS GOUGED.REPAIRED GOUGED LOWER AFT RUDDER LOWER MOUNT FITTING IAW VT-SAA EA 011-5542-01-A8110 REV IR AND UPS EO MD11-5540-76078-A. (MINOR)Mar 13, 2020 · N278UP · Doug MD11FSDR IPXA2020040853997Lug · gougedINSPECTION TYPE:3CLOWER AFT RUDDER UPPER MOUNT FITTING LUGS ARE GOUGED.REPAIRED GOUGED LOWER AFT RUDDER UPPER MOUNT FITTING LUGS IAW VT-SAA EA 011-5542-01-A8110 REV IR AND UPS EO MD11-5540-76078-A. (MINOR)Mar 13, 2020 · N278UP · Doug MD11FSDR SIMA2020032310007Plate · damagedRUDDER #1 HAS AREA OF CHAFEING DAMAGE-C/A-COMPLIED WITH IAW ERS-EM-55MR-830 01Mar 10, 2020 · N610AE · Emb EMB145LRSDR SIMA20200306001Fitting · out of toleranceRUDDER 2 LOWER ROD FITTING UPPER FLANGE FAILED DIMENSIONAL CHECK, FITTING REQUIRES REPLACEMENT.-C/A-REMOVED AND REPLACED LOWER ROD FITTING ASSY IAW SRM 55-40-02Mar 6, 2020 · N610AE · Emb EMB145LRSDR UIEA2020030900417Angle · crackedCLOSE OUT ANGLE UNDER RUDDER HAS CRACK AT LEFT END OF ANGLE.(<P>REMOVED AND REPLACED CRACKED CLOSE OUT ANGLE UNDER RUDDER IAW BOEING DOCUMENT #173T1215 AND B767-200 SRM 51-40-02.</P>)Mar 4, 2020 · N659GT · Boeing 767281SDR SWIA2020041050107Fastener · corrodedRUDDER POSITION POTENTIOMETER LINKAGE HAS CORRODED HARDWARE AND THE LINKAGE IS HARD TO MOVE AT THE VERTICLE STABILIZER LOWER REAR SPAR. (C-CHECK) RO 4/9/2020 REMOVED AND REPLACED HARDWARE ON RUDDER POSITION POTENTIOMETER LINKAGE IAW CRJ200 AMM. TORQUE WRENJan 17, 2020 · N975SW · Cndair CL6002B19SDR DALA2019090305119Housing · corrodedCORROSION ON BEARING HOUSING OF RUDDER TORQUE TUBE AFT FUSELAGE AREA (A&P). NRC 00586: CORROSION LEVEL 2, BEARING HOUSING OF RUDDER TORQUE TUBE AFT FUSELAGE AREA WAS REPLACED PER AMM 27-21-01 AND SRM 51-41-02-0G. (LP #1252777)Sep 2, 2019 · N947AT · Boeing 717200SDR DALA2019071304238Support Bracket · corrodedCORROSION WAS FOUND ON SUPPORT BRACKET OF RUDDER YOKE BEARING ASSEMBLY IN REF 2720-2004 (EHV). NRC 00253: CORROSION LEVEL 2, SUPPORT BRACKET OF RUDDER YOKE BEARING ASSEMBLY WAS REPLACED PER SRM 51-41-02-0G AND DWG #5913121 REV D. (LP #1168559)Jul 12, 2019 · N944AT · Boeing 717200
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