JASC 5553

Service difficulty reports · 586

Reports filed under 5553 · Vertical Stabilizer, Attach Fittings, 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 = '5553'
  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 SIMA20150108008Drag Angle · crackedRIGHT VERTICAL STAB TO FUSELAGE FWD ANGLE HAS EVIDENCE OF A CRACK ON THE AFT END. APPROX 1/2 INCHES LONG. REPAIRED RT VERTICAL STAB TO FUSELAGE FWD ANGLE AFT END IAW EO CR-55MR-038 & ERS CR-5500-230.Jan 8, 2015 · N543EA · Cndair CL6002C10SDR SIMA20150108009Drag Angle · crackedRIGHT VERTICAL STAB TO FUSELAGE AFT ANGLE HAS EVIDENCE OF A CRACK ON THE FWD END APPROX 3/4 INCHES LONG. REPAIRED IAW ERS-CR-55MR-229.Jan 8, 2015 · N543EA · Cndair CL6002C10SDR ASOA20140830266Attach Bracket · wornDURING C-CHECK, THE TOP RUDDER ATTACH BRACKET ON THE VERTICAL STABILIZER WAS FOUND TO BE WORN AND WOULD NOT RETAIN THE HAT BUSHINGS. MAINTENANCE R & R THE BRACKET IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Aug 30, 2014 · N14977 · Emb EMB145LRSDR WVER220140722003Drag Angle · crackedVERTICAL STABILIZER LOWER AFT DRAG ANGLE IS CRACKED APPROXIMATELY 1 INCH AT FWD END, LT SIDE.Jul 22, 2014 · N509MJ · Cndair CL6002C10SDR DALA2014071104051Attach Fitting · crackedAFT ACCESSORY, VERTICAL STABILIZER DORSAL FIN ATTACH FITTING, RT SIDE HAS CRACK INDICATION. R & R DAMAGED FITTING IAW ERA 526008-14, REV 1.Jul 10, 2014 · N915DN · Doug MD9030SDR DALA14035979253Channel · crackedCRACK WAS FOUND ON CHANNEL ON THE VERTICAL STABILIZER ACTUATOR SUPPORT. REPAIRED IAW ERA 526678-14.Jun 14, 2014 · N953DN · Doug MD9030SDR CALA2014041700467Fitting · corrodedVERTICAL STAB REAR SPAR, RT PRIMARY TERMINAL FITTING, AFT DRAG BRACE FITTING IS CORRODED. R & R RT OTBD AFT VERTICAL DRAG BRACE FITTING IAW SRM 51-40-02.Apr 17, 2014 · N24729 · Boeing 737724SDR WVER201402219103Drag Angle · crackedRIGHT FORWARD VERTICAL STAB FUSELAGE ATTACHMENT DRAG ANGLE IS CRACKED. PERFORMED A MAJOR REPAIR IAW REO 690-55-31, REV A.Feb 21, 2014 · N910FJ · Cndair CL6002D24SDR WVER201402219102Drag Angle · crackedLEFT FWD VERTICAL STAB FUSELAGE ATTACHMENT DRAG ANGLE IS CRACKED. PERFORMED A MAJOR REPAIR IAW REO 690-55-31, REV A.Feb 21, 2014 · N910FJ · Cndair CL6002D24SDR ASOA2014022510018Drag Angle · crackedFUSELAGE TO VERTICAL ATTACH POINT LT DRAG ANGLE CRACKED AT FRAME 67. REPAIRED LT DRAG ANGLE IAW REO 690-55-31-004. MAJOR REPAIR.Jan 31, 2014 · N147PQ · Cndair CL6002D24SDR FDEA201401210152Attach Angle · damagedNOTED VERTICAL TIP PANEL ATTACH ANGLES, BOTH LT & RT SIDES HAS NUMEROUS ELONGATED HOLES AT VERTICAL STAB TIP STRUCTURE. FOUND TO BE OUT OF LIMITS IAW DWG 172N3014 SHT 1 REV D. REMOVED ANGLES IAW SRM 51-40-02. FABRICATED NEW ANGLES IAW DWG 172N3014 & SRM 51Jan 21, 2014 · N987FD · Boeing 757231SDR AALA20131217003Attach Angle · damagedRT HAND INTERNAL VERTICAL STAB ATTACH ANGLE CRACKED AT 1427. INSTALLED NEW ANGLE IAW SRM 55-02-00 & AARD 51-00-05-1.Dec 17, 2013 · N9619V · Doug DC983SDR ASOA20131017252Fitting · corrodedDURING C-CHECK, FRAME 75 TO VERTICAL STABILIZER FITTING WAS FOUND CORRODED. MAINTENANCE REMOVED THE CORROSION AND REPAIRED THE FITTING IAW EC 5310-01317. ACFT APPROVED FOR RETURN TO SERVICE.Oct 17, 2013 · N21129 · Emb EMB145XRSDR SIMA20131010003Drag Angle · crackedRT VERTICAL STABILIZER TO FUSELAGE AFT DRAG ANGLE HAS 1 INCH CRACK ALONG L/E OF ANGLE. REPAIRED THE RT VERTICAL STAB TO FUSELAGE AFT DRAG ANGLE IAW EO CR-53MR-164R1 PART B.Oct 10, 2013 · N514AE · Cndair CL6002C10SDR SIMA20131010002Drag Angle · crackedLEFT VERTICAL STABILIZER TO FUSELAGE FWD DRAG ANGLE HAS A 1.5 INCH CRACK ALONG T/E OF ANGLE. LT VERTICAL STAB TO FUSELAGE FWD DRAG ANGLE REPAIRED IAW EO CR-55MR-038.Oct 10, 2013 · N514AE · Cndair CL6002C10SDR SIMA20130911004Attach Angle · crackedLEFT SIDE VERTICAL STAB TO FUSELAGE AFT ATTACH ANGLE IS CRACKED. REPAIRED IAW EO CR-55MR-086Sep 11, 2013 · N500AE · Cndair CL6002C10SDR SIMA20130723013Drag Angle · crackedRT FUSELAGE TO VERT. STAB. DRAG ANGLE IS CRACKED APPROX 1.5" AT STATION 61.56 PERCENT STGR DATUM. R & R RT FUSELAGE TO VERT. STAB DRAG ANGLE AT STATION 61.56 PERCENT STGR DATUM IAW EO CR-55MR-053 AND ETA-CR-5500-064.Jul 23, 2013 · N517AE · Cndair CL6002C10SDR ABXA20130620475Attach Fitting · crackedVERTICAL STABILIZER TO FUSELAGE ATTACHMENT STRUCTURE BETWEEN STAB REAR SPAR AND T/E IS CRACKED ON FWD RT FLANGE ACCESS THROUGH PANEL 324CLX FS 1746. R & R ATTACHED STRUCTURE ANGLE IAW SRM-300 51-40-02. ACFT WAS GROUNDED.Jun 20, 2013 · N362CM · Boeing 767338SDR CA130606005Attach Angle · cracked(CAN) FOUND ONE AIRCRAFT WITH A CRACK IN THE H STAB ATTACH ANGLE, THE MAINTENANCE PROGRAM WAS AMENDED TO CARRY OUT A REPEAT OF HBC MSB 55-4114 EVEN THOUGH IT CALLED FOR A ONE TIME ONLY INSPECTION. WHEN CARRYING OUT THE BORESCOPE INSPECTION IT WAS OBSERVED Jun 4, 2013 · Beech 1900DSDR ASAA2013052895215Skate Angle · chafedVERTICAL STAB TO FUSELAGE RT SKATE ANGLE CHAFED BETWEEN FWD ATTACH LUGS AND RUDDER L/E. ACFT GROUNDED. REPAIRED VERTICAL STAB TO FUS. RT SKATE ANGLE IAW ASA EA 5530 01086. REPAIR 1.May 28, 2013 · N756AS · Boeing 7374Q8SDR ASAA2013052895163Skate Angle · chafedVERTICAL STABILIZER TO FUSELAGE LT SKATE ANGLE CHAFED FROM FWD ATTACH LUGS TO RUDDER L/E. ACFT GROUNDED. BLENDED CHAFE, CHECKED LIMITS, WAS OUT OF LIMITS IAW EA CM 5530-01086, ACCOMPLISHED REPAIR 2 IAW EA 5530 01086.May 28, 2013 · N756AS · Boeing 7374Q8SDR ASOA20130423154Drag Angle · crackedDURING A-CHECK, THE RT VERTICAL STABILIZER TO FUSELAGE DRAG ANGLE WAS FOUND TO BE CRACKED AT FRAME 76, STRINGER 1R. MX R & R THE ANGLE IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.May 10, 2013 · N11526 · Emb EMB135ERSDR AALA20130426023Skate Angle · chafedRIGHT VERTICAL STAB TO FUSELAGE PANEL SKATE ANGLE CHAFING IN SEVERAL AREAS. REPLACED SKATE ANGLE PER AARD 51-10-05-1.Apr 26, 2013 · N966AN · Boeing 737823SDR AALA20130426022Skate Angle · chafedLEFT VERTICAL STAB TO FUSELAGE PANEL SKATE ANGLE SUPPORT CHAFED IN SEVERAL AREAS. REPLACED SKATE ANGLE PER AARD 51-10-05-1.Apr 26, 2013 · N966AN · Boeing 737823SDR SWAA2013042615251Attach Angle · crackedRIGHT ATTACH ANGLE FOR VERTICAL STABILIZER TO FUSELAGE SKIN FWD FAIRING CRACKED. REMOVED AND REPLACED ANGLE IAW SRM.Apr 17, 2013 · N950AT · Boeing 717200SDR SIMA20130314014Angle · crackedLT FWD VERTICAL STAB-TO-FUSELAGE REENFORCEMENT ANGLE CRACKED ON AFT END. REMOVED CRACKED LT FWD VERTICAL STAB-TO-FUSELAGE REINFORCEMENT ANGLE, PREPPED AND INSTALLED SERVICEABLE ANGLE IAW AEA EO EM-53MR-1281.Mar 14, 2013 · N605KS · Emb EMB145LRSDR DALA13011125816Attach Fitting · damagedFRONT SPAR ATTACH FITTING, RT SIDE MISDRILLED HOLE, 4TH HOLE FROM BOTTOM. ERA 512205-14, REV ORG COMPLIED WITH.Mar 8, 2013 · N596NW · Boeing 757351SDR IPXA13M77514Fitting · shearedINSPECTION TYPE:4C, LT SIDE NR 4 BANJO FITTING TO PYLON CARRY THROUGH CAP HAS SHEARED. REPAIRED LT SIDE NR 4 BANJO FITTING TO PYLON CARRY THROUGH CAP REF STASA EA 011-5530-01-A4505, REV I/R, EO MD11-5530-50152-A AND FAA 8100-9.Feb 23, 2013 · N257UP · Doug MD11FSDR CA130220012Attach Fitting · corroded(CAN) EXCESSIVE DISSIMILAR CORROSION FOUND BETWEEN BULKHEAD ASSEMBLY AND STEEL FITTING THAT IS THE FWD ATTACH POINT FOR THE VERTICAL STABILIZER. RIVETS APPEARED TO BE IN PLACE BUT WERE FOUND TO BE NOT HOLDING ANYTHING. DAMAGE WAS FOUND TO BE SAME AS DAMAGE RFeb 20, 2013 · Piper PA34200SDR IPXA13M77085Fitting · shearedINSPECTION TYPE:1C, NR 4 BANJO FITTING HAS 3EA SHEARED CARRY THROUGH CAP FASTENERS, RT SIDE. REPAIRED NR 4 BANJO FIITTING IAW STA-SA EA 011-5530-01-A4433-IR AND EO MD11-5530-49779-A.Jan 24, 2013 · N275UP · Doug MD11FSDR ASOA20130123243TAttach Fitting · damagedVERTICAL STAB RT AND LT MOUNT LUGS WORN BEYOND LIMITS. OVERSIZED RT AND LT VERTICAL STAB BEARING HOUSINGS TO 1ST REWORK DIMENSIONS AND INSTALLED BUSHINGS.Jan 21, 2013 · N16541 · Emb EMB145LRSDR ASOA20130118032Attach Fitting · damagedDURING C-CHECK, FRAME 75 STR 2L-2R IS FRETTING AT BOLTS FOR VERTICAL STAB TO FUSELAGE BRACKET. MX PERFORMED REPAIR AT FRM 75 STR 2L-2R AT VERTICAL STAB TO FUSELAGE BRACKET IAW EC5310-01317. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Jan 18, 2013 · N16951 · Emb EMB145LRSDR EPUA20130124002Mount · damagedVERTICAL STABILIZER BOLT MOUNTING HOLES WORN. REPAIRED VERTICAL STABILIZER HOLES IAW FORM 8110-3 DATED 1-12-2013. REPLACED AN176 TAIL ATTACH HARDWARE WITH INCREASED DIAMETER AN177 HARDWARE.Jan 13, 2013 · N208SD · Cessna 208BSDR DALA13002420927Attach Fitting · damagedCOMPLETING BOLT HOLE EC OF VERTICAL STAB, FOUND 3 RT SIDE HOLES, THREAD CUT-DAMAGED INSIDE OF HOLES. REMOVED NUT PLATE CHANNEL & POLISHED HOLES. ACCOMPLISHED DVI OF REWORKED AREA, DAMAGE CONTAINED. ALL 3 HOLES ARE LARGER THAN THE .202" ALLOWABLE HOLE SIZE. Jan 11, 2013 · N927DA · Doug MD88SDR SIMA20130104014Angle · crackedFWD LT VERTICAL STAB TO FUSELAGE ANGLE HAS A CRACK APPROX 1" LONG. RAR FWD LT VERT STAB TO FUSELAGE ANGLE IAW EO EM-53MR-2062.Jan 4, 2013 · N809AE · Emb EMB135KLSDR IPXA13M76719Fitting · crackedINSPECTION TYPE: 3C, DURING NDT INSP FOR TASK CARD 8342. INSPECTION FOUND RT NR 4 BANJO FITTING CRACKED IN FWD FLANGE NEAR STA, Y=2164. REPAIRED RT SIDE NR 4 BANJO FITTING CRACK IAW EA 011-5530-01-A4392, REV IR AND EO MD11-5530-49571-A.Dec 27, 2012 · N250UP · Doug MD11FSDR DALA12016740936Attach Angle · crackedVERTICAL STAB TO FUSELAGE LT SKATE ANGLE AND FASTENERS ARE CRACKED STA 1474 CANT. CUT OUT CRACKED AREA AT VERTICAL STAB TO FUSELAGE LT SKATE ANGLE STA 1474 CANT. FABRICATED AND INSTALLED FILLER AND REPAIR ANGLE IAW SRM 53-05, FIG 23 THE CRACKED FASTENER WAS Dec 17, 2012 · N936DL · Doug MD88SDR ASOA2012121802665Attach Bracket · crackedVERTICAL STAB TO FUSELAGE LT CHANNEL BRACKET CRACKED ABOVE APU DOOR. REPAIRED IAW REO 670-55-31-062.Nov 19, 2012 · N712EV · Cndair CL6002C10SDR FXGA20121030001Attach Angle · crackedDURING INSPECTION, FOUND RT VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE CRACKED AT THE AFT PRESSURE BULKHEAD.Oct 26, 2012 · N1110J · Emb EMB120FCSDR CA121017009Nut · cracked(CAN) UPON INSPECTION, I NOTICED THE FWD VERTICAL FIN ATTACH HARDWARE, THAT THE NUT WAS CRACKED IN HALF ON ONE OF THE BOLTS. THE HARDWARE APPEARED TO BE THE ORIGINAL EQUIPMENT.Oct 15, 2012 · Cessna 172MSDR WVER2012101195601Drag Angle · crackedLEFT AND RIGHT VERTICAL STABILIZER LOWER DRAG ANGLES ARE CRACKED. CUT AWAY DAMAGED PORTIONS AND INSTALLED FILLERS AND DOUBLERS PER BOMBARDIER REO 690-55-31-004.Oct 11, 2012 · N956LR · Cndair CL6002D24SDR DALA1250289205Attach Angle · crackedDURING PSV, THE RT CROWN FUSELAGE SKIN PANEL AT STA 1493, BETWEEN LONGERONS 2R-3R JUST BELOW THE VERTICAL STABILIZER ATTACH ANGLE WAS FOUND TO BE CRACKED. THE CRACK ORIGINATED FROM THE 1ST FASTENER HOLE FROM STA 1493, ABOV STR 3R. (ERA 496882-14AD)Oct 5, 2012 · N905DA · Doug MD9030SDR GLBA2012083100042Attach Fitting · crackedVERTICAL STAB LT SPAR CAP ANGLE AT THE 20 PERCENT CHORD IS CRACKED AT THE UPPER END AT VSS 84.10. CRACK IS .7500 INCH IN LENGTH, BEGINNING AT THE SECOND FASTENER HOLE ON LT FORWARD HORIZ STABILIZER ATTACH FITTING. REPAIRED IAW FR-00-02506, REV 1, STEP 1.Aug 30, 2012 · N245GL · Beech 1900DSDR DU4R2012009Attach Angle · corrodedDURING SCHEDULED INSPECTION, FOUND RIGHT VERTICAL STABILIZER ATTACH ANGLE AT FS 967 AND 991 CORRODED.Jul 3, 2012 · N3796B · Lkheed 382G44K30SDR FDEA201207012433Fitting · crackedCRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT INSPECTION ON THE LOWER VERTICAL STABILIZER, NR4 BANJO FITTING, RT SIDE FWD FLANGE. CARRIED OUT REPAIR AS PER DRAWING SR10550013 SHEET 7, 8, AND 9 REVISION P.Jul 1, 2012 · N615FE · Doug MD11FSDR FDEA201207012432Fitting · crackedCRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT INSPECTION ON THE LOWER VERTICAL STABILIZER NR 4, BANJO FITTING, LT SIDE, FORWARD FLANGE. CARRIED OUT REPAIR AS PER SRM 55-30-02 FIGURE 201 REPAIR 3 REVISION 49.Jul 1, 2012 · N615FE · Doug MD11FSDR IPXA2M74492Fitting · damagedINSPECTION TYPE:4C, 2EA LOOSE FASTENERS ON FWD LT SIDE, LOWER FASTENERS OF NR 4 BANJO FITTING. REPAIRED FASTENER HOLES OF NR 4 LT BANJO FITTING REF EO MD11-5530- 46641-A APPX A, B. AND D.Jun 16, 2012 · N288UP · Doug MD11FSDR DALA1510059254Fitting · galledVERTICAL STABILIZER AFT LT OTBD ATTACH FITTING F, OR HORIZONTAL STABILIZER HAS GALLING. REPAIRED ON N/R CARD 24519 3300 0043, ENLARGED BORE TO 1.453 TO REMOVE DAMAGE IAW SRM 55-, 30-05. INSTALLED BUSHING.Jun 15, 2012 · N954DN · Doug MD9030SDR IPXA2M74490Fitting · crackedINSPECTION TYPE:4C, 2EA LOOSE FASTENERS ON FWD SIDE LOWER FASTENERS OF NR 4 RT BANJO FITTING. ACCOMPLISHED REPAIR OF VERTICAL STABILIZER AFT SPAR NR 4 BANJO FITTING FASTENERS AND CRACK COMMON TO NR 2 PYLON CARRY THROUGH CAP ATTACHMENT REF MD11-5530-46641-A.Jun 15, 2012 · N288UP · Doug MD11FSDR DALA1237969254Fitting · galledVERTICAL STABILIZER AFT LEFT OUTBOARD ATTACH FITTING FOR HORIZONTAL STABILIZER HAS GALLING. ENLARGED BORE TO 1.453 TO REMOVE DAMAGE PER SRM55-30-05. INSTALLED BUSHING ON NRC 24519-3300-0043.Jun 15, 2012 · N954DN · Doug MD9030
Back to JASC 5553