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 DHL2006750512Web · bentVERT STAB FWD TENSION TIE SUPPORT WEB BENT/STRESSED RT SIDE. REMOVED SUPPORT WEB ON VERT STAB FWD TENSION TIE RT SIDE IAW B727 SRM 51-30-2. FABBED WEB FROM 7075 T6 .032 SIZE 24 1/4 BY 6 PO 9002507 IAW B727 SRM 51-20-1 AND SRM 55-30-2. TREATED AND PRIMED PARMar 14, 2006 · N750DH · Boeing 7272M7SDR 06FDEA0959Web · crackedWHILE WORKING RUDDER TRIM ACTUATOR REPLACEMENT, FOUND VERTICAL FIN WEB CRACKED UNDER WASHER HOLDING THE PRESSURE SEAL FOR THE RTB CABLE AT FIN STA 87. *S/D* REPAIRED PER FEDEX EA 7-5330-96598.Mar 7, 2006 · N488FE · Boeing 727200SDR USAA060347Angle · wornRT SKATE ANGLE AT VERTICAL STAB INTERSPAR BOX HAS WEAR. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS IAW TR 53-20-05A, DEFECT SIZE: 1 X 3 INCH.Feb 22, 2006 · N778AU · Boeing 7374B7SDR USAA060346Angle · wornLT SKATE ANGLE AT VERTICAL STAB INTERSPAR BOX HAS WEAR. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS IAW TR 53-20-02A, DEFECT SIZE: 3 X 1 INCH.Feb 22, 2006 · N778AU · Boeing 7374B7SDR 06FDEA0736Web · crackedWHILE WORKING RUDDER TRIM ACTUATOR REPLACEMENT FOUND VERTICAL FIN WEB CRACKED UNDER WASHER HOLDING THE PRESSURE SEAL FOR THE RTB CABLE AT FIN STA 87. REPAIRED PER FED EX EA 7-5530-96598.Feb 19, 2006 · N488FE · Boeing 727200SDR DL76S100648Bolt · unknownJOINT BARREL NUT/BOLT ASSEMBLY OF VERTICAL FIN REPLACEMENT IAW EO 01-074297-12 ME05. C/W EO 01-074297-12 ME05.Jan 4, 2006 · N139DL · Boeing 767332SDR AU510002059Lug · broken(AUS) VERTICAL STABILIZER ACCESS LADDER UPPER ATTACHMENT LUGS BROKEN. SUSPECT CAUSED BY POOR SHIMMING OF THE UPPER ATTACHMENT FITTINGS. SEE ATTACHMENT FOR INVESTIGATION DETAILS. (CASA NR 510002059)Dec 12, 2005 · Airbus A330*SDR USAA051459Skate Angle · wornRT SIDE VERTICAL STAB AT FIN WL 0.0 HAS WEAR. MAJOR REPAIR, FABRICATED AND INSTALLED REPAIR PART IAW TR 53-20-05A, DEFECT SIZE: 1 INCH.Dec 5, 2005 · N783AU · Boeing 7374B7SDR USAA051335Beam · crackedVERTICAL FIN RIGHT AFT LOWER T/E AREA, THE I/B FLANGE OF THE TRAILING EDGE. REPLACED CRACKED BEAM, IAW SRM 51-40-02. DEFECT SIZE: 6 INCHES.Nov 4, 2005 · N779AU · Boeing 7374B7SDR ASAA0540379Skate Angle · chafedRT FWD SKATE ANGLE FOR VERTICAL FIN CHAFED 3 INCHES FROM FWD END ON IB SIDE. REMOVED AND REPLACED FWD SKATE ANGLE FOR VERTICAL FIN. (K)Aug 4, 2005 · N771AS · Boeing 7374Q8SDR ASAA0540378Skate Angle · chafedRT AFT SKATE ANGLE FOR VERTICAL FIN CHAFED 18 INCH FROM AFT END ON OB SIDE. REMOVED AND REPLACED AFT SKATE ANGLE FOR VERTICAL FIN. (K)Aug 4, 2005 · N771AS · Boeing 7374Q8SDR ASAA0540372Skate Angle · chafedRT FWD SKATE ANGLE FOR VERTICAL FIN CHAFED 3 INCHES FROM FWD END ON IB SIDE. REMOVED AND REPLACED FWD SKATE ANGLE FOR VERTICAL FIN. (K)Aug 3, 2005 · N771AS · Boeing 7374Q8SDR ASAA0540371Skate Angle · chafedRT AFT SKATE ANGLE FOR VERTICAL FIN CHAFED 18 INCHES FROM AFT END ON OB SIDE. REMOVED AND REPLACED AFT SKATE FOR VERTICAL FIN. (K)Aug 3, 2005 · N771AS · Boeing 7374Q8SDR VJ32005F00001Fitting · crackedWHILE PERFORMEING UNSCHEDULED MAINTENANCE. VERTICAL STABILIZER WAS REMOVED, WHILE THE MECHANIC WAS INSPECTING THE FITTINGS FOR REINSTALLATION OF THE VERTICAL STABILIZER NOTICED A CRACK COMING FROM BOTTOM RT LOWER MOUNTING HOLE ON FORWARD FITTING. AT THIS TIMJun 23, 2005 · N5530A · Beech F33ASDR 05FDEA01504Tie · corrodedVERTICAL FIN TENSION TIE RT FWD VERTICAL BOLT HOLE IN TENSION TIE & SHEAR FITTING HAS CORROSION. REPAIRED TENSION TIE PER FED EX EA 7-5530-86296.Jun 1, 2005 · N482FE · Boeing 727200SDR 05FDEA01503Tie · corrodedCORROSION, VERTICAL FIN TENSION TIE RIGHT FWD BOLT HOLE HAS CORROSION ON FACE OF TENSION TIE LUGS UNDER NUT & BOLT HEAD SIDE. REPAIRED TENSION TIE PER FED EX EA 7-5530-86296.Jun 1, 2005 · N482FE · Boeing 727200SDR DHL2005784548Web · crackedFOUND VERTICAL STAB SLANT WEB AT 1303 LOWER RIGHT CORNER CRACKED STA 1303, FRAME SECTION ABOVE CENTER INLET DUCT. COMPLIED WITH COTNEY AEROSPACE EA: EAZ04-1 REV : A, 8110-3 DATED 6/8/05. STOP DRILLED CRACK ON VERT STAB WEB BS 1303 RBL 22 IAW 727 SRM 51-10-1 May 18, 2005 · N784DH · Boeing 727227SDR C2XA05TY043Housing · wornTYS - DURING A SCHEDULED INSPECTION THE RIGHT VERTICAL STAB SPHERICAL BEARING HAS PLAY. MAINTENANCE REPAIRED THE SPHERICAL BEARING HOUSING IAW EMB-145 AMM 55-10-00 AND EC5510-01116.May 13, 2005 · N14902 · Emb EMB145LRSDR C2XA05TY042Housing · wornTYS - DURING A SCHEDULED INSPECTION THE LEFT VERTICAL STAB SPHERICAL BEARING HAS PLAY. MAINTENANCE REPAIRED THE SPHERICAL BEARING HOUSING IAW EMB-145 AMM 55-10-00 AND EC5510-01116.May 13, 2005 · N14902 · Emb EMB145LRSDR 05FDEA01245Fitting · corrodedVERTICAL LEADING EDGE PANEL 322CL HAS CORROSION ON LOWER SPLICE FITTING. REMOVED NUT PLATES IAW A310-200 SRM 51-40-21, REMOVED CORROSION IAW A310-200 SRM 51-74-10. CHECKED MATERIAL LOSS OUT OF LIMITS IAW A310-200 SRM 55-30-00. REMOVED AND REPLACED SPLICE FIMay 12, 2005 · N403FE · Airbus A310203SDR 05FDEA00964Bushing · looseBUSHINGS LOOSE ON UPPER CLEVIS FOR THE PCU ROD END. REPAIRED UPPER RUDDER CLEVIS BUSHINGS FOR THE PCU RODEND IAW FED EX EA 7-5530- 86276.Apr 11, 2005 · N272FE · Boeing 727200SDR QXEA200500506Fitting · chafedPDX - VERTICAL STAB REAR SPAR BACKUP FITTING HAS APPROXIMATELY 2 INCHES LONG HORIZONTAL CHAFE MARK ON WEB DIRECTLY ABOVE RUDDER TOP HINGE FITTING. REPAIRED IAW HORIZON AIR EA R-55-43 AND REO 670-55-31-003.Mar 23, 2005 · N613QX · Cndair CL6002C10SDR DHL2005782505Clip · crackedANGLED SHEAR TIE CRACKED JUST BELOW STRINGER 9L AT FIN STA 180.6 INSIDE VERTICAL FIN. REMOVED DAMAGED CLIP AT FIN STA 180.6 BELOW STR 9L IAW 727 SRM 51-30-2. FABBED NEW CLIP FROM 7075 T6 .050 PO NR 9001417 DIM 5 3/4 INCH BY 3 INCHES IAW 727 SRM 727 55-30-2 FMar 14, 2005 · N782DH · Boeing 727227SDR ASAA0540127Skate Angle · chafedPAE - VERTICAL STAB SKATE STA 1001-1016, STA 21-31 IS CHAFFED. VERTICAL SKATE CHAFED OUT OF LIMITS, FABRICATED AND INSTALLED NEW SKATE. (K)Feb 9, 2005 · N713AS · Boeing 737490SDR ASAA0540126Skate Angle · chafedPAE - VERTICAL STABILIZER SKATE STA 1001-1016, STA 2R-3R IS CHAFED. CHAFED OUT OF LIMITS, FABRICATED AND INSTALLED NEW SKATE. (K)Feb 9, 2005 · N713AS · Boeing 737490SDR USAA050234Angle · chafedPIT - FOUND SKATE ANGLE CHAFED, VERT STAB RT AND LT LOWER SKATE ANGLE. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-40-00 AND DWG 65-54842. (M)Feb 9, 2005 · N520AU · Boeing 7373B7SDR SWAA050009Fitting · corrodedDURING SCHEDULED D-CHECK, FOUND VERTICAL FIN REAR SPAR LT AND RT PRIMARY ATTACH CLEVIS FWD AND AFT LUGS CORRODED. REPAIRED VERTICAL FIN PER ER.Jan 2, 2005 · N398SW · Boeing 7373H4SDR AWXA200500126Channel · crackedMCN - MAJOR REPAIR - DURING C-17 CHECK A 1/2" CRACK WAS FOUND IN VERTICAL STABILIZER LOWER ANGLE (CHANNEL) ON AFT SIDE OF RT AFT LUGS BS 1016, STR 2 RT. MAINTENANCE REMOVED CRACKED VERTICAL STABILIZER LOWER CHANNEL AT BS 1016, STR 2 RT; FABRICATED A NEW REPLACDec 27, 2004 · N327AW · Boeing 7373Q8SDR SWIA200414609Angle · crackedVERTICAL STAB LOWER RIGHT CLOSING ANGLE CRACKED. ITEM FOUND AT C-CHECK INSPECTION. CLOSING ANGLE REPAIRED IAW EMB 120 SST-1280/99 REF SB 120-53-0074.Dec 1, 2004 · N16731 · Emb EMB120ERSDR SWIA200414228Angle · crackedRIGHT FUSELAGE VERTICAL STAB CLOSING ANGLE IS CRACKED, ITEM FOUND AT C-CHECK INSPECTION. RT FUSELAGE TO VERTICAL STAB CLOSING ANGLE REPAIRED IAW EMB EO SST128099Nov 1, 2004 · N57734 · Emb EMB120ERSDR SWIA200414227Angle · crackedLEFT FUSELAGE VERTICAL STAB CLOSING ANGLE IS CRACKED, ITEM FOUND AT C-CHECK INSPECTION. LEFT FUSELAGE TO VERTICAL STAB CLOSING ANGLE REPAIRED IAW EMB E.O.Nov 1, 2004 · N57734 · Emb EMB120ERSDR SWAA041848Fitting · corrodedDURING SCHEDULED D-CHECK, FOUND VERTICAL STAB FWD AND AFT BODY LUG FACE CORRODED. REPAIRED VERTICAL STAB PER ER.Jun 30, 2004 · N388SW · Boeing 7373H4SDR USAA04340Fitting · corrodedFOUND .25 INCH BY .25 INCH CORROSION ON THE FORWARD TEE FITTING OF THE OUTBOARD ATTACH FITTING ON THE LEFT AFT SIDE OF THE VERTICAL STAB. REMOVED CORROSION AND INSTALLED NEW BUSHINGS PER EA 78608. (M)Jun 20, 2004 · N424US · Boeing 737401SDR USAA04339Fitting · corrodedFOUND .25 INCH BY .25I NCH CORROSION ON THE FORWARD T-FITTING OF THE OUTBOARD ATTACH FITTING ON THE LEFT AFT SIDE OF THE VERTICAL STAB. REMOVED CORROSION AND INSTALLED NEW BUSHING PER EA 78608. (M)Jun 20, 2004 · N424US · Boeing 737401SDR USAA04338Fitting · corrodedFOUND .25 INCH BY .25 INCH CORROSION ON THE FORWARD TEE FITTING OF THE OUTBOARD ATTACH FITTING ON THE LEFT AFT SIDE OF THE VERTICAL STAB. CORROSOIN LEVEL 1, TASK JK-64-55200-C-001. REMOVED CORROSION AND INSTALLED NEW BUSHINGS PER EA 78608. (M)Jun 20, 2004 · N424US · Boeing 737401SDR SWAA041496Bracket · crackedDURING SCHEDULED HC1 CHECK, FOUND VERTICAL STAB SPRING BRACKET AT BS 1016, RBL 11, CRACKED. REPAIRED VERTICAL STAB SPRING BRACKET PER EA.May 25, 2004 · N726SW · Boeing 7377H4SDR 04FDEA01215Attach Bracket · corrodedRIGHT SIDE OF VERTICAL STAB FROM RIB 22 TO 26 OF REAR SPAR HAS SEVERAL AREAS OF CORROSION ON FLANGES (PANEL ATTACH BRACKET). REMOVED CORROSION AT RT SIDE OF VERTICAL STAB REAR SPAR AREA, 3 AREAS NEEDED REWORK. FABRICATED & INSTALLED REPAIRS IAW EA 6-5530-776May 11, 2004 · N428FE · Airbus A310203SDR 04FDEA01207Attach Angle · corrodedRT SIDE OF VERTICAL STAB T/E, AT RIB 26 TOP FLANGE (PANEL ATTACHMENT ANGLE BRACKET) HAS CORROSION ON INNER SIDE OF FLANGE. REPAIRED IAW EA 6-5530-77670A RT SIDE OF VERTICAL STAB T/E AT RIB 26 TOP FLANGE.May 10, 2004 · N428FE · Airbus A310203SDR ABXA040158Attach Angle · crackedLEFT VERTICAL STABILIZER ATTACH ANGLE CRACKED. REPAIRED ANGLE IAW DC-9 SRM.Apr 15, 2004 · N932AX · Doug DC933FSDR CALA0300678Fitting · corrodedINSPECTION FOUND VERTICAL STABILIZER RT REAR SPAR FORWARD DRAG ANGLE FITTING CORRODED AT OB MOUNTING BOLT AREA. THE FITTING WAS REMOVED AND REPLACED IAW SRM 51-40-02.Nov 29, 2003 · N16648 · Boeing 737524SDR C2XA03TY197Fitting · damagedTYS AFTER REAMING THE RT VERTICAL STAB SPHERICAL BEARING CASTING, THE HORIZ STAB FAIL THE DIHEDRAL CHECK. REMOVED AND REPLACED THE RT VERTICAL HINGE FITTING IAW EC 5510-01067 C/W BACKLASH CHECK IAW EMB 145 AMM27-40-00; C/W INCIDENCE AND DIHEDRAL CHECKS IAW EMNov 24, 2003 · N27962 · Emb EMB145SDR 2003UALA00829Fitting · corrodedVERT STAB LT FWD AND AFT DRAG FITTINGS HAVE CORROSION. MAJOR REPAIR ACCOMPLISHED. REPLACED BOTH FITTINGS.Nov 3, 2003 · N373UA · Boeing 737322SDR ABXA030424Structure · corrodedVERTICAL STABILIZER REAR SPAR RIGHT CHORD HAD CORROSION AT ZR 270. REMOVED CORROSION AT REAR SPAR RIGHT CHORD, FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR DOUBLER, ALODINED, PRIMED AND INSTALLED IAW DC-8 SRM 51-1-8, 55-2-0 AND REA D855-48068MR.Oct 25, 2003 · N847AX · Doug DC861SDR ABXA030423Structure · corrodedVERTICAL STABILIZER REAR SPAR LEFT CHORD HAD CORROSION ON AFT LEG BETWEEN ZR 262 AND ZR 268. REMOVED CORROSION ON REAR SPAR LEFT CHORD, FOUND OUT OF LIMITS. FABRICATED REPAIR DOUBLER, ALODINED, PRIMED AND INSTALLED IAW DC-8 SRM 51-1-8, 55-2-0 AND REA D855-48Oct 25, 2003 · N847AX · Doug DC861SDR 2003UALA00809Attach Fitting · corrodedVERTICAL STAB RIGHT O/B ATTACH LOG AND BOLT CORRODED. MAJOR REPAIR ACCOMPLISHED. REWORKED STAB ATTACHED LOG.Oct 24, 2003 · N374UA · Boeing 737322SDR AWXA200301325Channel · crackedMCN - MINOR REPAIR - DURING C-17 CHECK A 1.5 INCH CRACK WAS FOUND ON FUSELAGE ANGLE JUST AFT OF RT VERTICAL STABILIZER ATTACH FITTING BS 1093. MAINTENANCE REMOVED 2 EACH CRACKED ANGLES JUST AFT OF RT VERTICAL STABILIZER ATTACH FITTING BS 1093; FABRICATED 2 EAOct 6, 2003 · N156AW · Boeing 7373G7SDR XE42003F00000Bracket · brokenDURING ROUTINE INSPECTION OF THE TAIL COMPARTMENT, RUDDER LIMITER BRACKET ASSEMBLY, PN 5914138503 WAS FOUND BROKEN. THERE WAS NO INBOUND REPORT OF RUDDER LOAD FEEL OR HANDLING PROBLEMS ON THE FLIGHT. SUSPECT CONNECTING LINKAGE (ITEM NR 105) MOVED WITH RIGH Jul 3, 2003 · N937AT · Boeing 717200SDR MWEA030260Angle · crackedSTATION 1420 LEFT SIDE INNER VERTICAL STABILIZER TO FUSELAGE FITTING IS CRACKED. FABRICATED AND INSTALLED ANGLE.Jun 30, 2003 · N808ME · Doug DC982SDR MWEA030259Angle · crackedSTATION 1429 RIGHT SIDE INNER VERTICAL STABILIZER TO FUSELAGE FITTING IS CRACKED. FABRICATED AND INSTALLED NEW ANGLE.Jun 27, 2003 · N808ME · Doug DC982SDR CA030505008Spar · cracked(CAN) DURING CHANGE OVER CRACKS WERE OBSERVED UNDER THE FORWARD ATTACHMENT POINT. NEW SPAR MANUFACTURED. NO PARTS AVAILABLE FROM MANUFACTURE.May 5, 2003 · Dhav DHC6300
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