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"

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 CA080220018Skate Angle · chafed(CAN) V STAB TO FUSELAGE SKATE ANGLE LT CHAFED AND REPAIRED IAW CUSTOMER EA. (TC NR 20080220018)Feb 20, 2008 · Boeing 7374S3SDR TRAX200800195Drag Angle · crackedVERTICAL STAB TO FUSELAGE RT DRAG ANGLE CRACKED. REPAIRED RT VERT STAB DRAG ANGLE IAW REO 670-55-31-018 REFER TO ATTACHED M-234 ITEMS 2-5 FOR COMPLIANCE. CUT OUT DAMAGE, FABRICATED AND DRILLED FILLER AND DOUBLER ALL WORK IAW REO 670-55-31-31-018, FILLER ANDFeb 4, 2008 · N331CA · Cndair CL6002C10SDR TRAX200800194Drag Angle · crackedVERTICAL STAB TO FUSELAGE LT DRAG ANGLE CRACKED. REPAIRED LT DRAG ANGLE IAW REO 670-55-31-018 REFER TO ATTACHED M-234 ITEMS 2- 5 FOR COMPLIANCE. CUT OUT, DAMAGE FABRICATED AND DRILLED FILLER AND DOUBLER ALL WORK IAW REO 670-55-31-018 FILLER AND DOUBLER MADE Feb 4, 2008 · N331CA · Cndair CL6002C10SDR C2XA08TY017Bracket · corrodedTYS - DURING A CURRENT 3C INSPECTION THE VERTICAL STAB SPHERICAL BEARING BRACKET WAS FOUND WITH PITTING CORROSION. MAINTENANCE MEASURED THE AREA AND WAS FOUND TO BE OUT OF LIMITS. COMMENCE TO REAM TO FIRST OVERSIZE IAW EMB 14XR SRM 55-30-02 AND EC 5510-01157Jan 25, 2008 · N12122 · Emb EMB145XRSDR SWAA080344Bushing · corrodedDURING SCHEDULED 20Y CHECK, FOUND VERTICAL FIN LT REAR SPAR FITTING LUG BUSHING CORRODED. REMOVED AND REPLACED BUSHING PER BOEING DRAWING.Jan 16, 2008 · N697SW · Boeing 7373TOSDR SWAA080345Bushing · corrodedDURING SCHEDULED 20Y CHECK, FOUND VERTICAL FIN LEFT REAR SPAR FAIL SAFE FITTING LUG BUSHING CORRODED. REMOVED AND REPLACED BUSHING PER BOEING DRAWING.Jan 16, 2008 · N697SW · Boeing 7373TOSDR TRAX200800065Drag Angle · crackedLEFT VERTICAL STAB DRAG ANGLE CRACKED AT AFT END (MARKED). PERFORMED EDDY CURRENT INSPECTION OF LT VERTICAL STAB DRAG ANGLE IAW NDTM 51-20-006 TO LOCATE END OF CRACK. END OF CRACK IS MARKED. INSTALLED AND SEALED L/H DRAG ANGLE PER REO 670-55-31-018. Jan 9, 2008 · N317CA · Cndair CL6002C10SDR TRAX200800064Drag Angle · crackedRIGHT VERTICAL STAB DRAG ANGLE CRACKED AT AFT END (MARKED). PERFORMED EDDY CURRENT INSPECTION OF RIGHT HAND VERTICAL STAB DRAG ANGLE IAW NDTM 51-20-006 TO LOCATE END OF CRACK. END OF CRACK IS MARKED. INSTALLED AND SEALED RT DRAG ANGLE PER REO 670-55-31-018.Jan 9, 2008 · N317CA · Cndair CL6002C10SDR ABXA080021Angle · crackedANGLE CRACKED AT FASTENER - LEFT SIDE JUST FORWARD OF TIP FAIRING. REMOVED FORMER, FABRICATED NEW FORMER IAW DWG 9911981. REINSTALLED FORMER IAW DC9 SRM 51-30-2.Dec 18, 2007 · N959AX · Doug DC941SDR CALA0800001Bushing · corrodedVERTICAL FIN FED RIGHT FITTING HAVE CORROSION IN BUSHING. REPLACED PER ECRA 5530-01493.Dec 17, 2007 · N12318 · Boeing 7373T0SDR CALA0700781Fitting · corrodedVERTICAL STAB, LEFT AFT O/B FITTING FOUND CORROSION ON BOTH FACES. AFTER REMOVED BUSHINGS REPAIRED AS PER ECRA 5530-01494.Dec 17, 2007 · N12318 · Boeing 7373T0SDR SWAA074789Fitting · corrodedDURING SCHEDULED 10Y CHECK, FOUND VERTICAL STABILIZER RT AND LT FITTING CORRODED. REPAIRED FITTING PER EA.Sep 24, 2007 · N655WN · Boeing 7373H4SDR MWEA070214Support Angle · crackedVERTICAL STABILIZER TO FUSELAGE INTERSECTION LINE, AFT SPAR LEFT SUPPORT ANGLE IS CRACKED. FABRICATED AND INSTALLED ANGLE.Sep 12, 2007 · N803ME · Doug DC981SDR ABXA070309Bracket · crackedVERTICAL STABILIZER UPPER RUDDER ATTACH HINGED BRACKET - RIGHT - CRACKED. REMOVED AND REPLACED RUDDER BRACKET IAW DC9 SRM.Sep 2, 2007 · N930AX · Doug DC933FSDR UPS07550498Structure · delaminatedDELAMINATION VERTICAL STAB 2FT X 3FT. A/C FERRIED TO BFM D35760 ASSIGNED. REPAIR PER EO B757-5530-27491A. REMOVED VERTICAL STAB PANEL AND INSTALLED NEW PANEL IAW SRM 51-40-02.Aug 25, 2007 · N407UP · Boeing 75724APFSDR UPS07850709Stiffener · crackedINSPECTION TYPE:C2 FITTING CRACKED AT TOP OF VERTICAL STAB SPAR, BETWEEN LT AND RT SPAR CAPS. REPAIRED STIFFENER ON VERTICAL STAB SPAR IAW DWG 4651109 AND SRM 51-1-20 D.Aug 22, 2007 · N801UP · Doug DC873FSDR KCSA071297Web · crackedVERTICAL STAB HORZ WEB AT FIN STA 562 HAS 1 INCH CRACK AT 5TH FASTENER FROM REAR SPAR.Aug 14, 2007 · N710CK · Boeing 7472B4BSDR N93A09082007Fitting · corrodedDURING INSPECTION FOUND ON VERTICAL STAB ATTACH BULKHEAD AND FITTING CORRODED.Aug 9, 2007 · N495QS · Gulstm GIVSDR USAA070630Bushing · damagedAFT FACE OF BUSHING, FWD FACE OF R8 LUG ON VERT FIN PITTED. REMOVED PITTING & INSTALLED NEW BUSHING PER EA 98801; CORR TASK C55-706-11, DEFECT SIZE: .250 X .250 INCH.Aug 8, 2007 · N425US · Boeing 737401SDR USAA070629Lug · corrodedFWD FACE OF L8 LUG ON VERT FIN CORRODED & LITE GOUGE. FAB'D BUSHING PER EA 98801; CORR TASK C55-706-11, DEFECT SIZE: .25 X .25 INCH.Aug 8, 2007 · N425US · Boeing 737401SDR USAA070628Lug · corrodedRIGHT AFT I/B ATTACH FITTINGG FUW FACE OF BUSHING R8 LUG ON VERT FIN HAS CORROSION. FAB'D BUSHING & INSTALLED PER SOMP 20-50-03 BOEING DWG 65-52274; EA 98801; CORR TASK C55-706-01, DEFECT SIZE: .250 X .250 INCH.Aug 8, 2007 · N425US · Boeing 737401SDR USAA070626Bushing · corrodedR5 O/B AFT ATTACH FITTING FWD FACE OF BUSHING PITTED, R5 LUG HAS CORROSION. REMOVED BUSHING, CORROSION & INSTALLED NEW BUSHING PER EA 98801; CORR TSK C55-706-11, DEFECT SIZE: .250 X .250 INCH.Aug 8, 2007 · N425US · Boeing 737401SDR USAA070622Bushing · corrodedBUSHING, VERT STAB LEFT AFT O/B ATTACH FITTING FWD FACE LUG L-5 HAS CORROSION. REMOVED CORROSION, INSTALLED NEW BUSHINGS PER EA 98801; CORR LEVEL 2; TASK C55-706-11, DEFECT SIZE: .25 INCH.Aug 8, 2007 · N425US · Boeing 737401SDR USAA070618Lug · gougedAFT FACE OF L-8 LUG OF VERTICAL FIN GOUGED. REMOVED DAMAGED BUSHING, PITTING & REPLACED BUSHING PER EA 98801. CORROSION RESULT OF GOUGE. DEFECT SIZE: .250 INCH.Aug 8, 2007 · N425US · Boeing 737401SDR UPS07850443Attach Angle · crackedINSPECTION TYPE:C2 LEFT SIDE OF VERT STAB LWR ATTACH ANGLE CRACKED AT STA 1766. REPAIRED LEFT SIDE OF VERT STAB LWR ATTACH ANGLE AT STA 1766 IAW SRM 53-02-05-0 FIG 016A.Jul 22, 2007 · N851UP · Doug DC873FSDR DHL2007784516Support Angle · crackedCRACK AT BS 1342 WEB AND LT SUPPORT ANGLE INSIDE VERT STAB PANEL 9504. REMOVED CRACKED SUPPORT ANGLE INSIDE VERT STAB PANEL 9504 IAW B727 SRM 51-30-2. FABRICATED NEW SUPPORT ANGLE FROM .040, 7075T6, DIM. 3.75 BY 8.25 IAW B727 SRM 51-10-2. TREATED, PRIMED ANJul 11, 2007 · N784DH · Boeing 727227SDR DHL2007783515Angle · crackedCRACK AT UPPER SUPPORT ANGLE INSIDE VERT STAB LT PANEL 9701, FIN STA 239.1, WL 472.6. REMOVED STAB PANELS 9701 AND 9707 TO FOM IAW B727 SRM 51-30-2. REMOVED, FABRICATED NEW ANGLE INSIDE VERT STAB PANEL 9701 FROM 7075T6, .050, 3.25 BY 6 IAW B727 SRM 51-30-2, Jun 5, 2007 · N783DH · Boeing 727227SDR TRAX200700765Angle · crackedVERTICAL STABILIZER TO FUSELAGE ANGLE CRACKED ON LEFT T/E. [06-08-07] WORK ACCOMPLISHED ON EC/TC REO 670-55-31-018.May 31, 2007 · N713EV · Cndair CL6002C10SDR TRAX200700636Structure · crackedSUSPECT CRACK AT BASE OF VERTICAL STAB LT SIDE (MARKED). WORK COMPLETED IN ACCORDANCE WITH ALL CRJ 700 SRMS.May 4, 2007 · N706EV · Cndair CL6002C10SDR C2XA07SH024Bushing · wornSHV - DURING C-CHECK RIGHT SPHERICAL BEARING FITTING ON VERTICAL STAB HINGE POINT IS WORN BEYOND TOLERANCE. MX REPAIRED RIGHT SPHERICAL BEARING FITTING ON VERTICAL STAB HINGE POINT BY REAMING TO 2ND REWORK AND INSTALLING OVERSIZE BUSHING IAW EMB 145 SRM 55-30May 4, 2007 · N13936 · Emb EMB145EPSDR USAA070279Angle · wornRIGHT SKATE ANGLE WORN AT BS 1006, RT SIDE OF VERTICAL STAB SKATE ANGLE. FABRICATED REPLACEMENT ANGLE PER SRM 51-40-02, DEFECT SIZE: 2 X 1 INCH.Apr 12, 2007 · N421US · Boeing 737401SDR USAA070280Angle · wornBS 1006 LEFT VERTICAL STAB SKATE ANGLE WORN. FABRICATED & INSTALLED REPLACEMENT ANGLE PER SRM 51-40-02, DEFECT SIZE: 2 X 1 INCH.Apr 12, 2007 · N421US · Boeing 737401SDR DLM88070451Bushing · corrodedCORROSION ON BUSHINGS OF VERTICAL STAB PIVOT POINT OUTBOARD AND INBOARD SIDE. NEW BUSHINGS FABRICATED AND INSTALLED PER SRM 55-02D PARA 24A (A), (B) AND (C).Mar 29, 2007 · N943DL · Doug MD88SDR SWAA071557Fitting · corrodedDURING SCHEDULED 10Y CHECK, FOUND LT VERTICAL STAB FITTING LUG FACES CORRODED. REPAIRED FITTING PER EA.Mar 23, 2007 · N644SW · Boeing 7373H4SDR SWAA071558Fitting · corrodedDURING SCHEDULED 10Y CHECK, FOUND RT VERTICAL STAB FITTING LUG FACES CORRODED. REPAIRED FITTING PER EA.Mar 23, 2007 · N644SW · Boeing 7373H4SDR AWXA200700434Support Channel · crackedMCN - CRACKED VERTICAL STABILIZER SUPPORT STIFFENER CHANNEL, BS 1095, RBL 8.5. REPLACED VERTICAL STABILIZER SUPPORT STIFFENER CHANNEL, BS 1095, RBL 8.5 IAW B737-300 SRM 51-40-02.Mar 17, 2007 · N308AW · Boeing 7373G7SDR EIAA2007040Structure · corrodedSTAB COMPARTMENT VERTICAL FIN INSPECTION FOUND TOP BOX CORRODED (EXFOLIATION) LEFT SIDE CHORD AT STA 395. CORROSION BLENDED OUT HFEC INSPECTED, ALODINE AND PRIMED, FASTENERS INSTALLED.Feb 22, 2007 · N471EV · Boeing 747273CSDR DALA1154289258Fitting · corrodedVERTICAL STABILIZER FITTING CORROSION REPAIR OD2006-SR-044 NRC B55-061119-344 BOEING APPROVAL 1-259780511-3.Dec 20, 2006 · N958DN · Doug MD9030SDR CA061016007Attach Bracket · cracked(CAN) ONE OF THE TWO VERTICAL TAIL ATTACH BRACKETS WAS DISCOVERED CRACKED APPROXIMATELY 90% OF IT’S LENGTH DURING A SCHEDULED INSPECTION. THE CRACK LOCATION IS IN THE RADIUS WHERE THE VERTICAL LEG INTERSECTS THE HORIZONTAL LEG. THERE IS A SERVICE LETTER WHICOct 14, 2006 · Cessna 152SDR C2XA06TY063Hinge · wornTYS DURING A 2C INSPECTION THE RT VERTICAL STAB SPHERICAL BEARING WAS FOUND TO BE OUT OF LIMITS. MAINTENANCE REAMED THE HOLE TO THE FIRST OVERSIZE IAW EC 5510-01080. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL 2C WORK.Oct 12, 2006 · N12145 · Emb EMB145XRSDR 06FDEA2947Cap · damagedSNRM N00691: EXISTING REPAIR AT VERTICAL STABILIZER NR 4, BANJO FITTING CARRY THROUGH CAP.Aug 11, 2006 · N522FE · Doug MD11SDR SWAA062389Beam · crackedDURING SCHEDULED 20Y CHECK, FOUND VERTICAL STAB LT TRAILING EDGE BEAM CRACKED. REMOVED AND REPLACED VERTICAL STAB BEAM PER SRM.Jul 10, 2006 · N319SW · Boeing 7373H4SDR TRAX200600367Support Angle · crackedCRACK FOUND VERTICAL STABILIZER SUPPORT ANGLE AT 67.5 PERCENT REAR DATUM AND LT EXTERNAL REAR FUSELAGE.Jun 12, 2006 · N720EV · Cndair CL6002C10SDR 06FDEA2241Structure · corrodedVERT STAB BOX LOWER SURFACE AT FR 84 HAS CORR STR 2L REF N00680. COMPLIED WITH EA 6-5530-101044.Jun 7, 2006 · N427FE · Airbus A310203SDR AMTA200600370Structure · corrodedLT VERT STAB LOWER STRUCTURE AT BASE OF STAB WHERE PANEL 9501 ATTACHES STA APP 1052-1088-36 INCHES OF BARE METAL AND 2 AREAS OF FRETTING CORROSION IAW MM. REMOVED FRETTING CORROSION LT VERT STAB LOWER BASE STRUCTURE AT PANEL 9501, SRM. ORIG THICK .071 MTL LOJun 1, 2006 · N315TZ · Boeing 73783NSDR QXEA200602220Panel · damagedPDX: VERTICAL STAB, RT SIDE ACCESS PANEL REBATES FOR PANEL 322ER, 322FR, 322GR, 322AR AND 322DR ALL HAVE CUT MARKS FROM BOX CUTTERS. MAINTENANCE REPAIRED IAW Q400 SRM 51-14-00 TASK 51-14-00-350-803 AND SRM 51-23-00 TASK 51-23-00-390-802.May 10, 2006 · N424QX · Bombdr DHC8402SDR CA060421008Attach Angle · corroded(CAN) VERTICAL STAB LT TRAILING EDGE AT RUDDER STATION 174, PANEL ATTACH ANGLE CORRODED AND REPAIRED IAW CUSTOMER EA (TC NR 20060421008)Apr 20, 2006 · Boeing 737290CSDR WRNA200600033Fitting · corrodedDURING M72 CHECK, FOUND CORROSION ON EMPENNAGE FORWARD RIGHT FITTING ATTACHED TO VERTICAL STABILIZER. CLEANED, PRIMED AND APPLIED TOP COAT PER A300 SRM 51-40-12 AND REPLACED EMPENNAGE FORWARD RIGHT LONGITUDINAL BRACE FITTING PER A300 DRAWING 19R53870348 SHEETMar 31, 2006 · N501TR · Airbus A300B4203SDR WRNA200600032Support · corrodedDURING M72 CHECK, FOUND CORROSION AND LOOSE FASTENERS ON HORIZONTAL SUPPORT OF VERTICAL STABILIZER TRAILING EDGE STRUCTURE ABOVE RUDDER FITTING NR 1. FABRICATED FITTING FROM EXTRUSION BAC1505100797 PER A300 ACCORDING SRM 51-41-00, TREATED, PRIMED AND APPLIED Mar 30, 2006 · N501TR · Airbus A300B4203SDR IXXA06SMN100SAccess Door · crackedDURING ROUTINE C CHECK INSPECTION, LEFT HAND VERTICAL STABILIZER ACCESS DOOR EDGE CRACKED. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 06119 DATE 03-07-06, SEMAN DWG ED 4187 DATE 03-06-06, EO SEMAN 2006150 DATE 03-07-06. REMOVED FASTENERS IAW DC-8 SRM 51-1-21Mar 24, 2006 · N602AL · Doug DC873F
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