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 C2XA08SHAttach Fitting · damagedSHV - DURING C-CHECK RUDDER 1 UPPER ACTUATOR ATTACHMENT LOWER HINGE UPPER HAT BUSHING MIGRATED.Dec 2, 2008 · N13955 · Emb EMB145LRSDR USAA2008122392311Structure · debondedSAL - C19 - MAJOR REPAIR - NR 6135795 - DEBOND OF TRAILING EDGE OF RUDDER STA 233.09 +12 INCHES. REPAIRED RUDDER TRAILING EDGE IAW B737 SRM 51-20-05-06.Dec 1, 2008 · N303AW · Boeing 7373G7SDR C2XA08SH145Attach Bracket · wornSHV - DURING C-CHECK THE RUDDER UPPER CENTER ATTACHMENT BRACKET WAS FOUND TO BE WORN AND THE HAT BUSHINGS MIGRATED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 145 SRM 55-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Nov 11, 2008 · N14952 · Emb EMB145LRSDR CA080813007Cover Plate · damaged(CAN) PILOT INDICATES RUDDER MOVEMENT STIFF. MORE RT RUDDER REQUIRED AT TAKE-OFF. INSP BY MAINT REVEALED THAT THE COVER PLATE AT THE BOTTOM OF THE RUDDER WAS BENT OUT OF SHAPE CAUSING INTERFERENCE WITH THE RUDDER MOVEMENT. INSP OF OTHER ACFT REVEALS THAT THISAug 12, 2008 · Pilats PC1245SDR 08FDEA01003Fitting · damagedRUDDER; LEFT SIDE LEADING EDGE; BR 4 UPPER HINGE BLOCK REPAIR AREA HAS 1 EACH MISSED DRILLED HOLE. COMPLIED WITH EA 65540-118461.Mar 17, 2008 · N425FE · Airbus A310203SDR WRLA2008038Panel · damagedDURING C-CHECK INSPECTION FOUND UPPER RUDDER PANEL 376RL 2EA SCREW HOLES DAMAGED. REPAIRED UPPER RUDDER PANEL 376RL SCREW HOLES PER ECRA 242NW-55-DC10-014, 242NW-55-DC10-015.Mar 7, 2008 · N138WA · Doug DC1030SDR WRLA2008037Panel · damagedDURING C-CHECK INSPECTION FOUND UPPER FWD RUDDER PANEL 376VL HAS 2EA SCREW HOLES ELONGATED. REPAIRED UPPER FWD RUDDER PANEL 376VL SCREW HOLES PER ECRA 242NW-55-DC10-014 AND ECRA, 242NW-55-DC10-015.Mar 7, 2008 · N138WA · Doug DC1030SDR 08FDEA00769Strap · corrodedRUDDER L/E PANEL NR 326 EL BRIDGING STRAPS ARE CORRODED UNDER THE NUT PLATES. REMOVED AND REPLACED THE BRIDGING STRAPS REFERENCE A310-200 SRM 51-40-21; PARA 5.Mar 6, 2008 · N425FE · Airbus A310203SDR CALA0800279Structure · damagedRUDDER TRAILING EDGE HAS EXPOSED COMPOSITE APPROXIMATELY 8 INCHES FROM BOTTOM, RT SIDE. REPAIRED DAMAGE TO SUBJECT RUDDER IAW CONTINENTAL EC/RA NO 5540-01246.Mar 5, 2008 · N18350 · Boeing 7373T0SDR UPS08851404Doubler · crackedINSPECTION TYPE:C2 INTERNAL DOUBLER CRACKED ON LOWER EYEBOLT ACCESS HOLE ON RUDDER. REMOVED, FABRICATED AND REPLACED INTERNAL DOUBLER PER DWG 5655077 AND SRM 51-1-21.Dec 30, 2007 · N718UP · Doug DC871FSDR CA071029007Bearing · damaged(CAN) RUDDER BEARING FOUND DAMAGED ON C-CHECK. THE BEARING WAS INCORPORATED BY SB ON WINTER WORK 2005-2006 AND CUMULATE 421 HOURS SINCE INSTALLATION. A/C HOURS 2141 CYCLES 1316 DROPS 11678 (TC NR 20071029007)Oct 29, 2007 · Cndair CL2156B11215SDR ABXR070395Hinge Bracket · crackedUPPER RUDDER HINGE BRACKET CRACKED RIGHT SIDE. REMOVED AND REPLACED BRACKET IAW DC9 MM 27-20-1 AND DAC DWG 5910254.Oct 5, 2007 · N784TW · Doug DC915SDR CA071003006Mount · cracked(CAN) DURING RIGGING OF LOWER RUDDER ACTUATOR SPRING STRUT, NOTICED ACTUATOR ADAPTOR FLEXING. ADAPTOR FOUND TO BE CRACKED FROM OUTER FLANGE HORIZONTALLY ACROSS RADIUS TO INNER FLANGE. ADAPTOR REPLACED. (TC NR 20071003006)Oct 2, 2007 · Dhav DHC8102SDR 2007FA0000915Hinge Bracket · corrodedLT OB HINGE BRACKET BROKE OFF DURING AILERON REMOVAL. APPEARS TO HAVE FAILED DUE TO CORROSION. (K)Oct 1, 2007 · N52FT · Cessna S550SDR C2XA07TY043Bushing · wornTYS DURING A CURRENT 2C INSPECTION THE MIDDLE BUSHION ON THE RUDDER 2 WAS FOUND WORN. MAINTENANCE REMOVED AND REPLACED THE BRACKET WITH A NEW BUSHION IAW EMB 135/145 SRM 51-40-02 AND EC 5540-01028. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OFAug 15, 2007 · N14993 · Emb EMB145LRSDR C2XA07TY041Bracket · damagedTYS - DURING A CURRENT C-CHECK INSPECTION, ELONGATED HOLES WERE FOUND ON NR 2 RUDDER AT SPAR 1. HOLES MEASURED (1) .249 (2) .228 AND (3) .338. HOLES WERE REAMED IAW EC5540-01074. ALODINED PRIMED HOLES. INSTALL NEW BUSHIONS IN THE NR 3 HOLE. ALL WORK WAS ACAug 5, 2007 · N13994 · Emb EMB145LRSDR UPS07850472Web · crackedINSPECTION TYPE:C2 RUDDER HAS 1.5 INCH CRACK IN LWR STRUCTURE JUST AFT OF TORQUE TUBE MOUNTING. REMOVED CRACKED WEB ON RUDDER IAW SRM 51-1-21. FABRICATED AND INSTALLED REPAIR WEB ON RUDDER STA ZR 59.54 IAW SRM 51-03-00-0, AND DWG 5701251.Aug 1, 2007 · N851UP · Doug DC873FSDR AWXA200701005Hinge Fitting · wornSAL - MAJOR REPAIR - C-06 CHECK - NR 5964976, THE NR 7 RUDDER HINGE FITTING HAS EXCESSIVE PLAY, RUDDER STATION 5605 / RIB 11. REPLACED THE NR 7 RUDDER HINGE FITTING, RUDDER STATION 5605 / RIB 11 IAW A320 AMM 27-21-41.Jul 25, 2007 · N633AW · Airbus A320231SDR AWXA200700980Hinge Fitting · wornSAL - MAJOR REPAIR - C-06 CHECK - NR 5964984, THE NR 5 RUDDER HINGE FITTING HAS EXCESSIVE PLAY, RUDDER STATION 2985/RIB 7. REPLACED THE NR 5 RUDDER HINGE FITTING, RUDDER STATION 2985/RIB 7 IAW A320 AMM 27-21-41.Jul 25, 2007 · N633AW · Airbus A320231SDR AWXA200700979Hinge Fitting · wornSAL - MAJOR REPAIR - C-06 CHECK - NR 5964981, THE NR 4 RUDDER HINGE FITTING HAS EXCESSIVE PLAY, RUDDER STATION 2632/RIB 6. REPLACED THE NR 4 RUDDER HINGE FITTING, RUDDER STATION 2632/RIB 4 IAW A320 AMM 27-21-41.Jul 25, 2007 · N633AW · Airbus A320231SDR AWXA200700978Hinge Fitting · wornSAL - MAJOR REPAIR - C-06 CHECK - NR 5964983, THE NR 3 RUDDER HINGE FITTING HAS EXCESSIVE PLAY, RUDDER STATION 2279/RIB 5. REPLACED THE NR 3 RUDDER HINGE FITTING, RUDDER STATION 2279/RIB 5 IAW A320 AMM 27-21-41.Jul 25, 2007 · N633AW · Airbus A320231SDR AWXA200700977Hinge Fitting · wornSAL - MAJOR REPAIR - C-06 CHECK - NR 5964982, THE NR 2 RUDDER HINGE FITTING HAS EXCESSIVE PLAY, RUDDER STATION 1926/RIB 4. REPLACED THE NR 2 RUDDER HINGE FITTING, RUDDER STATION 1926/RIB 4 IAW A320 AMM 27-21-41.Jul 25, 2007 · N633AW · Airbus A320231SDR HNAA0700198Web · corrodedWEB FOUND CORRODED ON FORE RUDDER MID HINGE. WEB ON FORE RUDDER MID HINGE LOCALLY FABRICATED AS PER DRAWING NUMBER 85540112, INSTALLATION CARRIED OUT ON WORK CARD SEQ 3041.Jun 9, 2007 · N907HA · Dhav DHC8102SDR 06FDEA04302Hinge Fitting · corrodedCORROSION EXIST AT VERT STAB REAR SPAR NR 3 RUDDER ATTACHMENT HINGE FITTING COMPLIED WITH EA NR 6-5540-106300. RUDDER RIB 12 AND 13 ATTACH FITTINGS CORROSION. MAJOR REPAIR IAW FED EX GMM 6-2-100.Dec 22, 2006 · N454FE · Airbus A310222SDR 06FDEA04301Hinge Fitting · corrodedVERT STAB REAR SPAR NR 2 RUDDER ATTACHMENT HINGE FITTING HAS CORROSION. COMPLIED WITH EA NR 6-5540-106300 RUDDER RIB 12 AND 13 ATTACH FITTINGS CORROSION. MAJOR REPAIR IAW FED EX GMM 6-2-100.Dec 22, 2006 · N454FE · Airbus A310322SDR DHL2006805518Angle · crackedLT RUDDER BASE ANGLE 2" CRACK STA ZR 61.156. REMOVED BASE ANGLE IAW SRM 51-3-0. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW BASE ANGLE IAW SRM 51-3-0, SRM 51-3-1 PG 3 (TORQUE). REFER TO JC EA27200005-001-D (W/O 600077018) FOR BASE ANGLESep 25, 2006 · N805DH · Doug DC873FSDR DHL2006809515Angle · crackedLT RUDDER BASE 2" CRACK AT STA ZR 59.000 CANT OF ANGLE. REMOVED CRACKED ANGLE IAW SRM 51-3-0. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE IAW SRM 51-3-0, SRM 51-3-1 (TORQUE). REFER TO JC EA27200004-001-D (WO 600016595) FOR FABRICATION OF AAug 14, 2006 · N809DH · Doug DC873FSDR 2006FA0000781Bracket · unsecureDURING THE INITIAL 200 HOUR PHASE 1 INSPECTION ON THIS AIRCRAFT, THE MOUNT BRACKETS THAT SECURE THE RUDDER SERVO BRIDLE CABLES AND PULLEYS WERE FOUND TO BE UNSECURED AT THE AFT ATTACH POINTS (FS 364.00) BOTH LT AND RDT BRACKETS WERE NOT ATTACHED. THE ASSOCIATEAug 3, 2006 · N36799 · Beech C90SDR QXEA200601784Mount · gougedPDX C4 - ON TRAILING RUDDER, THE UPPER FLANGE OF THE LOWER RADIUS ROD MOUNT HAS A GOUGE (INSIDE WHERE ROD END IS LOCATED). REPAIRED IAW DHC-8 RD 8-51-103.Jul 5, 2006 · N358PH · Dhav DHC8202SDR DU4R2006486Housing · corrodedCORROSION ON RUDDER CONTROL BEARING HOUSING. REMOVED AND REPLACED RUDDER BEARING HOUSING P/N 3913121 IAW DC-9/MD-80 SRM 51-30-05.May 19, 2006 · N923DL · Doug MD88SDR C1HA200695001Seal · damagedON TAXI INTO DEN, UPPER RUDDER INDICATOR DIDN'T MOVE FULLY TO THE LIMIT LINE WHEN RIGHT RUDDER WAS FULLY APPLIED. LEFT RUDDER OPERATED NORMALLY FOUND FIN FAIRING DAMAGED AT NR 6 SPOT ON RT SIDE. REMOVED AND REPLACED FAIRING AND REMOVED DAMAGED RUDDER BLADE SMay 13, 2006 · N295AS · Boeing 727290SDR QXEA200602217Panel · damagedPDX: TRAILING RUDDER LT SIDE HAS CUT IN REBATE FOR PANEL 323AL FROM BOX CUTTERS. MAINTENANCE REPAIRED IAW Q400 SRM 51-14-00-350-803, SRM 51-14-00-350-803 AND SRM 51-25-10-370-801.May 12, 2006 · N424QX · Bombdr DHC8402SDR QXEA200602222Access Panel · damagedPDX: FORE RUDDER, LT SIDE ACCESS PANEL REBATE FOR PANEL 323AL AHS CUTS FROM BOX CUTTERS. MAINTENANCE REPAIRED IAW Q400 SRM 51-14-00 TASK 51-14-00-350-803, AND Q400 SRM 51-25-10-370-801.May 11, 2006 · N424QX · Bombdr DHC8402SDR QXEA200602221Panel · damagedPDX: TRAILING RUDDER, RT SIDE ACCESS PANEL REBATE FOR PANEL 324DR HAS CUT MARKS FROM BOX CUTTERS. MAINTENANCE REPAIRED IAW Q400 SRM 51-14-00-850-803 AND SRM 51-14-00-850-803.May 10, 2006 · N424QX · Bombdr DHC8402SDR QXEA200602216Panel · damagedPDX: FORE RUDDER RT SIDE CUT MARKS ON REBATE FORE PANEL 323DR FROM BOX CUTTERS. MAINTENANCE REPAIRED IAW Q400 SRM TASK 51-14-00-350-803.May 10, 2006 · N424QX · Bombdr DHC8402SDR QXEA200601062Hinge · wornYYC - C4 VERTICAL STABILIZER REAR SPAR TOP FORE RUDDER ATTACH SAFETY HINGE HAS WEAR DAMAGE ON TOP FACE. REPARIED IAW DHC-8-200 SR, 51-40-11, PAGES 1-4 AND RD 8-51-102, ISSUE 1.Apr 4, 2006 · N353PH · Dhav DHC8202SDR QXEA200601063Hinge · wornYYC - C4 VERTICAL STABILIZER REAR SPAR FORE RUDDER ATTACH BOTTOM SAFETY HINGE HAS WEAR DAMAGE ON TOP FACE. REAPIRED IAW RD 8-51-102, ISSUE 1 AND DHC-8-200 SRM 51-40-11, PAGES 1-4.Apr 4, 2006 · N353PH · Dhav DHC8202SDR QXEA200601058Bracket · corrodedYYC - C4 FORE RUDDER FORWARD UPPER HINGE SAFETY BRACKET HAS FRETTING CORROSION FOUND ON UPPER PLATE. REPAIRED IAW RD 8-55-074, ISSUE 2.Mar 31, 2006 · N353PH · Dhav DHC8202SDR QXEA200600918Hinge · corrodedPDX - C4 LOWER FORE RUDDER SAFETY HINGE SHOWS SIGNS OF FRETTING ON UPPER SURFACE AROUND BOLT HOLE. REPAIRED IAW DHC-8-200 SRM 51-40-00 AND HORIZON AIR EA 2-55-133.Mar 31, 2006 · N354PH · Dhav DHC8202SDR QXEA200600695Lug · nickedYYC C4, FORE RUDDER, FRONT SPAR LEFT HAND SIDE, LUG FOR DAMPER ATTACHMENT HAS A NICK. REPAIRED IAW HORIZON AIR EA 2-55-114 AND RD 8-55-1667, ISSUE 1.Mar 4, 2006 · N350PH · Dhav DHC8202SDR CA060203005Stop · failedNO JAMMING OR EVIDENCE OF SEE ON EITHER RUDDER STOPS.Jan 31, 2006 · Cessna 150FSDR SIMA200602326Hinge · wornDURING COMPLIANCE WITH EO THE RUDDER II CENTER UPPER HINGE FLANGED BUSHING WAS FOUND LOOSE AND FITTING (LOWER HALF) WORN. MAINTENANCE REPLACED THE RUDDER II IAW AMM. PASSED FUNCTIONAL CHECK FLIGHT. AIRCRAFT RETURNED TO SERVICE. (K)Jan 18, 2006 · N618AE · Emb EMB145LRSDR SWAA053665Angle · crackedDURING SCHEDULED D CHECK, FOUND VERTICAL STAB LT ANGLE CRACKED AT NR 7 RUDDER HINGE. REPAIRED ANGLE PER SRM.Nov 17, 2005 · N620SW · Boeing 7373H4SDR MWEA050117Hinge Bracket · corrodedVERTICAL STABILIZER RUDDER HINGE BRACKET HAVE CORROSION AROUND BOLT HOLES TO ATTACH THE BEARING ASSEMBLY AND CORROSION IN THE FIN ATTACHMENT BOLT HOLES. REMOVED AND REPLACED RUDDER HINGE BRACKET.Oct 19, 2005 · N701ME · Doug MD88SDR 2005FA0001426Hinge · corrodedDURING SCHEDULED PHASE 2 INSPECTION OF AIRCRAFT, FOUND THE CENTER RUDDER HINGE ASSY HAVING INTERGRANULAR CORROSION AROUND THE HARDWARE ATTACHING TEE TO THE HINGE ASSY. THIS TYPE OF CORROSION IS PROBABLY DUE TO THE LOCATION OF THE PART AND THE AGE OF THE AIRCROct 12, 2005 · N585CE · Beech B200SDR 2005FA0001076Support · crackedRUDDER SUPPORT BRACKET ON RUDDER TOWER FACING PART AS INSTALLED ON AIRCRAFT, BOTTOM RIGHT LEG CRACKED, OUTSIDE AND INSIDE, AT BASE ABOVE THE WELD. CRACK WAS VISIBLE WITH SMALL MIRROR AND FLASHLIGHT WITH THE RUDDER OFF.Jul 29, 2005 · Diamon DA20C1SDR CA050524004Hinge Bracket · cracked(CAN) DURING AN INSPECTION A CRACK WAS FOUND IN THE CORNER OF A TOP RUDDER HINGE BRACKET. THE AMO HAS BEEN MONITORING THE WEAR ON THESE BRACKETS IN OUR HIGH TIME AIR FRAMES. SUBSEQUENTLY 5 HIGH TIME AIRFRAME SHAVE HAD THEIR RUDDER HINGE BRACKETS REPLACED. NOMay 24, 2005 · Cessna 172MSDR 2005FA0000803Support Bracket · crackedUPON REINSTALLATION OF RUDDER ASSY, FOUND RUDDER SUPPORT BRACKET AND STIFFENER ANGLE CRACKED UNDER RUDDER PRIMARY TRAVEL STOP AT FRAME STA 48. PROBABLE CAUSE: RUDDER OVER TRAVELING AGAINST PRIMARY STOP, WHEN GUST LOCK NOT INSTALLED AND WHEN PARKED OUTSIDE N WMay 21, 2005 · N198HB · Lear 60LEARSDR 05FDEA00998Arm · gougedNR 7 RUDDER HINGE ATTACHMENT BRACE ( A-FRAME) HAS GOUGE MARKS AND WEAR MARKS AT ATTACHMENT BOLT. REMOVED AND REPLACED NR 7 HINGE ARM IAW A310-200 AMM 55-36-47-4-01 AND 27-21-21-4-01.Apr 14, 2005 · N446FE · Airbus A310SDR ASAA0540049Balance Arm · damagedOKC - RUDDER BALANCE ARM HAS DAMAGE TO TOP SKIN UPON REMOVAL. REMOVED DAMAGE, FABRICATED AND INSTALLED A REPAIR SKIN SECTION AND DOUBLER IAW AS EA. CRACK-(Y SHAPE 3.7 X 3.75 X 2.75). (K)Jan 23, 2005 · N771AS · Boeing 7374Q8
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