JASC 5534

Service difficulty reports · 820

Reports filed under 5534 · Vertical Stabilizer 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 = '5534'
  ORDER BY difficulty_date DESC"

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SDR IPXA09557205Fastener · damagedINSPECTION TYPE:C2 LIGHTNING STRIKE ON FASTENER ON LT SIDE VERTICAL STAB 6 INCHES AFT OF L/E WL 575. REPAIRED PER ATS ER 09-4262 DATED 26AUG09 AND UPS EO B757-5530-34728-A.Aug 15, 2009 · N464UP · Boeing 75724APFSDR USAA2009090392333Support · corrodedSAL - Q6 - MAJOR REPAIR - CORROSION ON SUPPORT STRUCTURE CHORD AT LEFT SIDE OF TRAILING EDGE OF VERTICAL STABILIZER FIN STA 182.30. REPLACED SUPPORT STRUCTURE AT LEFT SIDE OF TRAILING EDGE OF VERTICAL STABILIZER FIN STA 182.30 IAW B737 SRM 51-40-02 & 51-10-02Jul 29, 2009 · N454UW · Boeing 7374B7SDR SWAA094744Fitting · corrodedDURING SCHEDULED 12Y CHECK, FOUND VERTICAL STABILIZER AFT O/B DRAG ANGLE FITTING CORRODED. REMOVED AND REPLACED FITTING PER SRM.Jul 23, 2009 · N650SW · Boeing 7373H4SDR C2XA09TY169Fitting · chafedTYS - A/C CURRENTLY IN A C-CHECK STATUS WHEN INSPECTION FOUND CORROSION ON FRAME 75 VERTICAL STAB FITTING, 4 BOLT HOLES HAD SOME CORROSION. MAINTENANCE REMOVED THE FITTING AND REAMED THE FOUR HOLES AND BUSHINGS INSTALLED. THEN REINSTALL THE FITTING IAW EC 55Jul 22, 2009 · N14937 · Emb EMB145EPSDR FDEA200906262324Support · crackedLT NR2 ENGINE INTAKE DUCT (INTERNAL) SUPPORT FRAME AT STA ZFR 2033 FOUND WITH CRACK. REPAIR CARRIED OUT AS PER E.A. 1-5530-132119, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.Jun 26, 2009 · N617FE · Doug MD11FSDR SWAA093668Structure · delaminatedDURING SCHEDULED 8Y CHECK, FOUND VERTICAL STABILIZER L/E DELAMINATED. REPAIRED STABILIZER PER EA.Jun 6, 2009 · N404WN · Boeing 7377H4SDR FDEA200905261794Fitting · chafedFOUND CHAFING MARK ON VERTICAL STABILIZER FITTING NR 1 REPAIR PERFORMED BY NDT INSPECTION WITHOUT FINDINGS AND SURFACE REPAIR IAW RAS/DAHAM/4027020/2009 ISS A, APPROVED BY EA 6-5530-129170.May 26, 2009 · N746FD · Airbus A300B4622RSDR DXTA2009050603635Structure · damagedFOUND DAMAGE ON VENTRAL FIN. POSSIBLE LIGHTNING STRIKE. LOCATED, DRILLED, AND INSTALLED REPLACEMENT VENTRAL FIN USING SCREWS AND RIVETS PER SRM 51-40-01 AND SERVICE MANUAL DEVIATION FORM NUMBER 1-18X37K.May 5, 2009 · N102QS · Beech 400BEECHSDR C2XA09TY075Housing · corrodedBOTH SPHERICAL BEARING HOUSING'S ON VERTICAL STAB HAVE CORROSION. REAMED HOUSING AND INSTALLED NEW BUSHINGS IAW EMB AMM 55-30-02 AND COMPLIED WITH DIHEDRAL & INCIDENCE CHECKS IAW EMB 145 AMM 51-50-01. AIRCRAFT STILL IN C CHECK.Apr 24, 2009 · N12934 · Emb EMB145EPSDR C2XA09TY068Fitting · chafedFRAME 75 FRETTING AT VERTICAL STAB FITTING. REMOVED FITTING CLEANED AREA AND DYE PEN INSPECTED, NO DEFECTS NOTED AND RE-INSTALLED FITTING IAW EC5310-01317. AIRCRAFT STILL IN C-CHECK.Apr 23, 2009 · N12934 · Emb EMB145EPSDR WRLA2009109Channel · crackedDURING C-CHK IN TPE INSPECTION FOUND CRACK FROM VERT STAB ACCESS PNL 364FR. FOUND AFT FUSELAGE UPPER SKIN CHANNEL BOTH ENDS CRACKED AT STA 2065 BETWEEN X=13.65 AND X=-13.65 (REF EGAT NRC U05086). REPAIRED THE CHANNEL ON VERT STAB ACCESS PNL 364FR IAW MD-11F Apr 13, 2009 · N279WA · Doug MD11SDR COMA2009041350114Hinge Fitting · wornRUDDER ATTACH FITTING ON VERTICAL STAB CENTER BOTTOM HINGE BEARING HAS EXCESSIVE PLAY. REMOVED RUDDER CENTER LOWER HINGE FITTING, REMOVED AND REPLACED BEARING AND REINSTALLED FITTING PER EA 10-5531-02567.Apr 8, 2009 · N720SW · Cndair CL6002B19SDR IPXA09855434Structure · damagedINSPECTION TYPE:SV SURVEY SEQ 752-54-01 RT VERTICAL STAB REPAIR STA ZR 74.000 HAS FASTENER REPAIR. ACCOMPLISHED PER REO-G12648 AND EO DC8-5520-32835.Apr 8, 2009 · N752UP · Doug DC871FSDR ASOA200900464Drag Angle · crackedVERTICAL STAB DRAG ANGLE DIAPHRAGM CRACKED 1.1 INCH LONG ON RT AFT SIDE UNDER RUDDER.Apr 5, 2009 · N829AS · Cndair CL6002B19SDR AALA20090413TUL03Lug · damagedVERTICAL STAB RIGHT INBOARD LUG DIAMETER IS OUT OF LIMITS. INSTALLED AND HONED NEW BUSHINGS PER SRM 55-02-00.Apr 3, 2009 · N9616G · Doug DC983SDR AALA20090413TUL21Structure · damagedVERTICAL STAB LEFT OUTBOARD LUG DIAMETER IS OUT OF LIMITS. INSTALLED AND HONED NEW BUSHINGS PER SRM 55-02-00.Apr 3, 2009 · N9616G · Doug DC983SDR AALA20090413TUL05Lug · damagedVERTICAL STAB RIGHT OUTBOARD LUG BORE DIAMETER IS OUT OF LIMITS. INSTALLED AND HONED NEW BUSHINGS PER SRM 55-02-00.Mar 30, 2009 · N9616G · Doug DC983SDR AALA20090413TUL20Structure · damagedVERTICAL STAB LEFT INBOARD LUG BORE DIAMETER IS OUT OF LIMITS. INSTALLED AND HONED NEW BUSHINGS PER SRM 55-02-00.Mar 30, 2009 · N9616G · Doug DC983SDR ASOA200900260Drag Angle · crackedLT VERTICAL STAB LOWER DRAG ANGLE CRACKED (MARKED). CRACK LENGTH WAS VERIFIED IAW SRM NDTM 51-20-006. LEFT VERTICAL STAB TO FUSELAGE DRAG ANGLE REPAIRED BY COMPLIANCE WITH EC/TC REO 670-55-31-018 IAW REO 670-55-31-018 FOR LEFT SIDE ONLY. RESTORED PROTECTIVE Feb 26, 2009 · N390CA · Cndair CL6002C10SDR DL757090290Angle · corrodedVERTICAL FIN ANGLE CORRORED AT STATION 1786.699 STA 0. REPAIRED BY REPLACEMENT PER 55-30-13 ON NR 01228.Feb 22, 2009 · N651DL · Boeing 757232SDR ASOA200900213Drag Angle · crackedRT VERTICAL STABILIZER DRAG ANGLE VERIFIED CRACKED. REPAIRED PER REO 670-55-31-041.Feb 16, 2009 · N751EV · Cndair CL6002C10SDR SWAA090648Attach Fitting · corrodedDURING SCHEDULED 18Y CHECK, FOUND LT VERTICAL STABILIZER ATTACH FITTING LUGS CORRODED. REPAIRED FITTING PER SRM.Jan 29, 2009 · N515SW · Boeing 7375H4SDR SWAA090647Lug · corrodedDURING SCHEDULED 18Y CHECK, FOUND RT VERTICAL STABILIZER ATTACH FITTING LUGS CORRODED. REPAIRED FITTING PER SRM.Jan 29, 2009 · N515SW · Boeing 7375H4SDR CALA2009012000050Bushing · corrodedVERTICAL STAB LEFT INBOARD AFT LUG BOTH BUSHINGS HAVE CORROSION. REMOVED AND REPLACED BOTH BUSHINGS REF BAC DWG 65-52274 AND SOPM 20-50-03.Jan 19, 2009 · N24633 · Boeing 737524SDR CALA2009012000049Bushing · corrodedVERTICAL STAB RIGHT INBOARD AFT LUG BOTH BUSHINGS HAVE CORROSION. REMOVED AND REPLACED CORRODED BUSHINGS REF BAC DWR 65-52274 AND SOPM 20-50-03.Jan 19, 2009 · N24633 · Boeing 737524SDR IPXA09855255Repair · damagedINSPECTION TYPE:SV VERT STAB L/E REPAIR HAS SIGNS OF WRINKLING AND DOES NOT MATCH L/E CONTOUR SS 752-S4-04, STA ZFS 104.750. REPAIRED PER DC8 SRM 55-2-1 FIG 4.Jan 15, 2009 · N752UP · Doug DC871FSDR ASOA200801588Drag Angle · crackedRT VERTICAL FWD DRAG ANGLE APPEARS CRACKED. PERFORMED EDDY CURRENT INSPECTION OF RIGHT FORWARD VERTICAL STAB TO FUSELAGE DRAG ANGLE IAW CRJ 700 NDTM 51-20-006. DRAG ANGLE CONFIRMED CRACKED AND MARKED. RT DRAG ANGLE REPAIRED PER REO 670-55-31-018.Dec 1, 2008 · N716EV · Cndair CL6002C10SDR ASOA200801587Drag Angle · crackedLT VERTICAL FWD DRAG ANGLE APPEARS CRACKED. PERFORMED EDDY CURRENT INSPECTION OF LEFT FORWARD VERTICAL STAB TO FUSELAGE DRAG ANGLE IAW CRJ 700 NDTM 51-20-006. DRAG ANGLE CONFIRMED CRACKED AND MARKED. LT DRAG ANGLE REPAIRED PER REO 670-55-31-018. REMOVED PADec 1, 2008 · N716EV · Cndair CL6002C10SDR CALA0801078Drag Angle · corrodedVERTICAL STABILIZER AFT LEFT ATTACH LUG AREA, FWD DRAG ANGLE FITTING HAS CORROSION INSIDE O/B HOLE. REMOVED LT VERTICAL STABILIZER AFT I/B AND O/B ATTACH BOLTS, REMOVED AND REPLACED LT DRAG ANGLE PER B737 SRM 51-40-02. REINSTALLED LT VERTICAL STABILIZER AFT Nov 12, 2008 · N16648 · Boeing 737524SDR SWAA086162Fitting · corrodedDURING SCHEDULED 20Y CHECK, FOUND VERTICAL STABILIZER RT O/B FWD LUG FITTING CORRODED. REPAIRED FITTING PER SWA EA.Nov 12, 2008 · N348SW · Boeing 7373H4SDR SWAA086163Fitting · corrodedDURING SCHEDULED 20Y CHECK, FOUND VERTICAL STABILIZER LT O/B FWD LUG FITTING CORRODED. REPAIRED FITTING PER SWA EA.Nov 12, 2008 · N348SW · Boeing 7373H4SDR SWAA086066Fitting · corrodedDURING SCHEDULED 20Y CHECK, FOUND VERTICAL STABILIZER LT OUTBOARD REAR LUG FITTING CORRODED. REPAIRED FITTING PER EA.Nov 9, 2008 · N348SW · Boeing 7373H4SDR KCSA081562Angle · crackedVERTICAL STAB, FIN STA 586 HAS A 5 INCH CRACK IN AN ANGLE THAT ATTACHES INTO THE FRONT SPAR WEB AT BL 0 TO RBL 5.Nov 7, 2008 · N708CK · Boeing 747212BSDR SWAA086007Drag Angle · corrodedDURING SCHEDULED 20Y CHECK, FOUND VERTICAL STAB FITTING DRAG ANGLES CORRODED. REMOVED AND REPLACED DRAG ANGLES PER SRM.Nov 3, 2008 · N341SW · Boeing 7373H4SDR UPS08854002Structure · unknownINSPECTION TYPE:SV SSN 700-S4-02 RT SIDE VERTICAL STAB STATION 254 EXTERNAL REPAIR UNABLE TO VALIDATE. REPAIRED AS PER SRM 51-1-27.Oct 29, 2008 · N700UP · Doug DC871FSDR UPS08854001Structure · misrepairedINSPECTION TYPE:SV VERTICAL STAB ZR254 EXTERNAL DOUBLER DOES NOT MEET SRM GUIDELINES. INSTALLED NEW ROW OF RIVETS 51-3-0 51-1-21.Oct 29, 2008 · N700UP · Doug DC871FSDR ASOA200801361Drag Angle · crackedRT VERTICAL STAB DRAG ANGLE CRACKED. COMPLIED WITH REO 670-55-31-018. REMOVED FASTENERS AND CUT AWAY DAMAGED AREA IAW REO. RT SIDE FWD DRAG ANGLE, PER REO 670-55-31-018. PERFORMED EDDY CURRENT INSPECTION IAW NDTM 51-20-006. NO DEFECTS NOTED. FABRICATED DOct 18, 2008 · N712EV · Cndair CL6002C10SDR ASOA1289Drag Angle · crackedREMOVAL & REPLACEMENT OF RT AFT DRAG ANGLE. CUT AWAY DAMAGED AREA. FURTHER DAMAGE FOUND TO AREA UNDERNEATH REMOVED AREA. REMOVED DAMAGE. REMOVED TOOLING MARKS IN UPPER FLANGE TO A DEPTH OF .002 AND .015 DEPTH SUBMIT TO BOMBARDIER FOR FURTHER DISPOSITION. Oct 2, 2008 · Cndair CL6002C10SDR ASOA1296Drag Angle · crackedREMOVED & REPLACED AFT DRAG ANGLE ON VERTICAL STAB LEFT SIDE FAY SEALED AND APPLIED FINISH TO AREA. PERFORMED EDDY CURRENT INSPECTION OF FORWARD AND AFT V/STAB TO FUSELAGE DRAG ANGLES, RIGHT SIDE. FORWARD & AFT DRAG ANGLES VERIFIED CRACKED, FORWARD DRAG ANGLOct 2, 2008 · Cndair CL6002C10SDR ASOA1225Drag Angle · crackedPERFORMED EDDY CURRENT INSPECTION OF FORWARD AND AFT V/STAB TO FUSELAGE DRAG ANGLES, RIGHT SIDE. FORWARD AND AFT DRAG ANGLES VERIFIED CRACKED, FORWARD DRAG ANGLE IS MARKED AT THE END OF CRACK. REMOVED RT AFT DRAG ANGLE MADE TEMPLATE FOR AFT RT DRAG ANGLE (INSep 26, 2008 · Cndair CL6002C10SDR ASOA1224Drag Angle · crackedPERFORMED EDDY CURRENT INSPECTION OF FORWARD AND AFT V/STAB TO FUSELAGE DRAG ANGLES, LEFT SIDE. FORWARD AND AFT DRAG ANGLES VERIFIED CRACKED, FORWARD DRAG ANGLE IS MARKED AT END OF CRACK. REPAIR OF AFT DRAG ANGLE. REMOVED DAMAGED AREA FROM FWD DRAG ANGLE ANSep 26, 2008 · Cndair CL6002C10SDR 08FDEA03818Stiffener · crackedREAR STIFFENER BETWEEN THE TRAILING EDGE OF RIB 7 & THE RIB ON THE RIGHT SIDE OF THE VERTICAL STAB IS CRACKED. REMOVED & REPLACED STIFFENER IAW SRM 51-40-21 & 51-72-10.Sep 11, 2008 · N450FE · Airbus A310222SDR TRAX200801106Drag Angle · crackedRT AFT V/STAB TO FUSELAGE DRAG ANGLE CRACKED AT 67.5% REAR SPAR DATUM.Sep 4, 2008 · N709EV · Cndair CL6002C10SDR TRAX200801105Drag Angle · crackedLT AFT V/STAB TO FUSELAGE DRAG ANGLE CRACKED AT 67.5% REAR SPAR DATUM.Sep 4, 2008 · N709EV · Cndair CL6002C10SDR TRAX200801097Drag Angle · crackedCRACKED DRAG ANGLE RT LOWER VERT STAB. MARKED.Sep 3, 2008 · N709EV · Cndair CL6002C10SDR TRAX200801096Drag Angle · crackedCRACKED DRAG ANGLE LT LOWER VERT STAB. MARKED.Sep 3, 2008 · N709EV · Cndair CL6002C10SDR 08FDEA02156Web · crackedAIR STAIR COMPARTMENT ABOVE "S" DUCT AT STA 1303, LT SIDE OF YELLOW VERTICAL WEB WHERE STIFFENER PASSES THROUGH CUT OUT, CRACKED. DOT ON AFT SIDE OF WEB AND ACCESS THROUGH VERT STAB PANEL 9504 REMOVED DAMAGE, FABRICATED, TREATED, PRIMED AND INSTALLED REPAIR PJun 4, 2008 · N487FE · Boeing 727227SDR SWAA082499Stiffener · crackedDURING SCHEDULED 12Y CHECK, FOUND VERTICAL STABILIZER STIFFENER AFT OF STABILIZER MOUNT CRACKED AT STA 1088. REMOVED AND REPLACED STIFFENER PER SRM.May 6, 2008 · N625SW · Boeing 7373H4SDR 08FDEA01712Angle · crackedRIB NR 2 ATTACH ANGLE CRACKED AT STR 6R ATTACHMENT BOLT INSIDE VERTICAL STAB, STR 6R, RIB NR 2 FIN STA 22.5 CUT-OUT DAMAGED AREA IAW SRM 51-10-1 & 55-30-5 FIGURE 1, FABRICATED REPAIR ANGLE & REPAIR FILLER, TREATED & PRIMED PARTS IAW SRM 51-1-2, INSTALLED REPMay 1, 2008 · N203FE · Boeing 727200SDR TRAX200800457Structure · crackedSUSPECTED CRACK FWD OF FS 1181 ON LT VERTICAL BASE. COMPLIED WITH EC REO 670-55-31-032.Mar 19, 2008 · N355CA · Cndair CL6002C10
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