JASC 5530

Service difficulty reports · 2,534

Reports filed under 5530 · Vertical Stabilizer, 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 = '5530'
  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 DALA13055680978Skate Angle · crackedRIGHT INTERNAL SKATE ANGLE, BS 1418, INSIDE ACCESS PANEL, 6301B CRACKED. VERTICAL STAB REPAIRED IAW DWG 5912188 AND SRM 51-01.Oct 26, 2013 · N978DL · Doug MD88SDR DALA13055670978Angle · damagedRT LWR CORNER AND HOLE FOR ATTACH ANGLE ELONGATED. INSTALLED NEW ANGLE AND FRAME IAW DWG 5910242 AND SRM 51-30.Oct 26, 2013 · N978DL · Doug MD88SDR ASOA20130924172Drag Angle · crackedDURING 4A INSPECTION, THE LT AFT FUSELAGE TO VERTICLE STABILIZER DRAG ANGLE WAS FOUND TO BE CRACKED. DRAG ANGLE REPLACED.Sep 24, 2013 · N14905 · Emb EMB145LRSDR ASOA2013102509250Drag Angle · crackedVERTICAL STAB LOWER LT DRAG ANGLE CRACKED AT AFT END. REPAIRED IAW REO 670-55-31-018. MAJOR REPAIR -- SDR CLOSED.Sep 21, 2013 · N604QX · Cndair CL6002C10SDR ASOA2013102509249Drag Angle · crackedVERTICAL STAB LOWER LT DRAG ANGLE AFT OF 67.5 PERCENT, REAR SPAR DATUM CRACKED AT FWD END. REMOVED DRAG ANGLE IAW SRM 51-42-22-001-0013, DRILLED UP A TEMPLATE FOR NEW DRAG ANGLE. LOCATED AND DRILLED NEW DRAG ANGLE AND THEN COUNTER SUNK ANGLE IAW SRM 51-40-11Sep 21, 2013 · N604QX · Cndair CL6002C10SDR REXA2013092101886Panel · damagedPANEL 326CR HAS DAMAGED FASTENER HOLE. REPAIRED FASTENER HOLE ON PANEL 326CR IAW EA 955-01916,Sep 21, 2013 · N913XJ · Cndair CL6002D24SDR MJYA201309120014Structure · corrodedLEFT VERTICAL STAB HAS CORROSION.Sep 1, 2013 · N783TW · Doug DC915FSDR SWAA2013082319486Inlet · crackedVERTICAL STABILIZER RAM AIR INLET CRACKED. REPAIRED STABILIZER ASSEMBLY IAW SRM.Aug 22, 2013 · N992AT · Boeing 717200SDR ABXA20130819509Angle · crackedSTRUCTURE INSIDE OF VERTICAL STAB PANEL 324CLX, ON TOP OF FUSELAGE HAS CRACKS IN FWD ANGLE. REMOVED WEB TO FORM IAW SRM 51-40-02, DRILLED AND INSTALLED NEW STIFFENER IAW SRM 51-40-05 AND 51-40-02,Aug 19, 2013 · N769AX · Boeing 767281SDR DALA13039533756Support Channel · crackedDURING INSPECTION, FOUND VERTICAL STAB INTERNAL STRUCTURE, SUPPORT CHANNEL CRACKED AT LT AND RT ENDS ABOVE AND AFT OF STAB FORWARD TERMINAL FITTINGS. MX INSTALLED NEW SUPPORT CHANNEL A, TAG A22712 IAW SRM 51-40-02.Aug 13, 2013 · N3756 · Boeing 737832SDR DALA13039249020Fastener · looseDURING SCHEDULED INSPECTION, ONE FASTENER WAS FOUND TO BE LOOSE ON THE LT VERTICAL STABILIZER L/E JUST ABOVE ZFS 52-267 AND FWD OF THE VERTICAL STABILIZER FRONT SPAR. REPAIRED IAW SRM 53-03D AND AMDS 5530-01045-0801.Aug 13, 2013 · N920DE · Doug MD88SDR CALA2013081290355Fastener · looseRAMP REPORTED LOOSE FASTENER ON LT VERTICAL STABILIZER. SECURED FASTENER.Aug 11, 2013 · N467UA · Airbus A320232SDR CALA2013081290351Nut Plate · wrong partVERTICAL STAB BOX PANEL 322FL HAS 3 NUTPLATES MISSING AND 1 INSTALLED USING WRONG SIZE NUTPLATE CAUSING SCREW TO PROTRUDE FROM PANEL. LOCATIONS MARKED WITH TAPE. INST 4 NEW NUT PLATES ALL PROPERLY SIZED.Aug 11, 2013 · N221UA · Boeing 777222SDR DALA13038450905Structure · damagedTHE 4, 5 & 6 FASTENER ABOVE VFS 52.267 ELONGATED. DISTORTED VERTICAL STAB REAMED HOLES, HFEC INSPECTED, REPAIRED IAW ER/A 517473-14AD REVISION ORIGINAL.Aug 6, 2013 · N905DL · Doug MD88SDR DALA13038440905Structure · crackedFWD FLANGE VERTICAL STABILIZER CRACKED. FIRST FASTENER ABOVE VFS 52-267 SPLICE SHOWS CRACK INIDCATION RT SIDE. REMOVED L/E, ACCOMPLISHED INSPECTION, REPAIR ACCOMPLISHED IAW ER/A 517473-14AD, REV ORIGINAL.Aug 6, 2013 · N905DL · Doug MD88SDR ASOA2013080608833Fairing · gougedFOUND VERTICAL STAB LT LOWER MIDDLE FAIRING HAS A GOUGE. CLASSIFIED AS MAJOR REPAIR IAW GMM 5-3. REPAIRED IAW REO 601R-55-32-315.Aug 4, 2013 · N846AS · Cndair CL6002B19SDR IPXA13M79804Intercostal · crackedINSPECTION TYPE:2C, APPROX 1 INCH LONG CRACK, ALONG AFT EDGE OF INTERCOSTAL, AT VERTICAL STAB REAR SPAR RELIEF CUTOUT, AS SHOWN IN SRM 55-30-02, REPAIR 7, FIG 203. INSTALLED REPAIR AT VERTICAL STAB REAR SPAR INTERCOSTAL AFT EDGE AT RELIEF CUTOUT IAW SRM 55-3Aug 1, 2013 · N259UP · Doug MD11FSDR SWAA2013072518562Duct · crackedVERTICAL STABILIZER RAM AIR INLET DUCT CRACKED. REPAIRED DUCT IAW EA.Jul 25, 2013 · N983AT · Boeing 717200SDR ABXA20130723499Angle · crackedL/E VERTICAL STABILIZER FWD ANGLE HAS CRACKED INSIDE LT SIDE OF VERTICAL STABILIZER AT VERTICAL FUSE BOXED STRUCTURE INSIDE OF LOWEST PANEL OPENING. R & R FWD ANGLE INSIDE LEFT VERTICAL STABILIZER AT VERTICAL FUSE BOX IAW DWG 173T1215 AND SRM 51-40-02. ACFT Jul 23, 2013 · N767AX · Boeing 767281SDR DALA13034999205Angle · wornVERTICAL STABILIZER PANEL 350AB HAS AREA OF WEAR, A CRACK ON ANGLE AFT OF SEAL. REMOVED DAMAGE, FABRICATED REPAIR ANGLE, ALODINED, PRIMED AND INSTALLED IAW SRM 55-00-01, 51-70-01, 51-30-02 AND DWG 5912176, PG 4.Jul 15, 2013 · N905DA · Doug MD9030SDR IPXA3579556Strap · corrodedINSPECTION TYPE:C-8, VERTICAL STAB TOP CAP INTERNAL METAL STRAP HAS CORROSION. REPLACED METAL STRAP IAW BAC DWG 179N1011-4.Jul 14, 2013 · N468UP · Boeing 75724APFSDR DALA13034660976Structure · crackedDURING SCHEDULED INSPECTION, THREE FASTENER HOLES EXHIBITED CRACK INDICATIONS ON THE RT SIDE OF THE VERTICAL STABILIZER IAW AD 2011-15-01. REPAIRS ACCOMPLISHED IAW ER/A 516705-14AD.Jul 11, 2013 · N976DL · Doug MD88SDR DALA13034650976Structure · crackedDURING SCHEDULED INSPECTION, SEVEN FASTENER HOLES EXHIBITED CRACK INDICATIONS ON THE LT SIDE OF THE VERTICAL STABILIZER IAW AD 2011-15-01. REPAIRS ACCOMPLISHED IAW ER/A 516705-14AD.Jul 11, 2013 · N976DL · Doug MD88SDR REXA2013070801288Structure · gougedHORIZONTAL STAB VISOR IS GOUGED. REPAIRED IAW REO 690-55-32-051 AND EOR55027.Jul 8, 2013 · N906XJ · Cndair CL6002D24SDR ASAA2013070695468Skate Angle · chafedLEFT VERTICAL STAB TO FUSELAGE SKATE ANGLE CHAFED BETWEEN FWD AND AFT ATTACH LUG GROUNDED. REPAIRED DAMAGE TO SKATE ANGLE IAW EA 400 53EA 10673.Jul 6, 2013 · N705AS · Boeing 737490SDR ASAA2013062795417Skate Angle · chafedVERTICAL STAB TO FUSELAGE SKATE ANGLE CHAFED BETWEEN DORSAL T/E STAB FORWARD ATTACH LUG. ACFT GROUNDED. REMOVED DAMAGED SKATE ANGLE, FABBED NEW ANGLE AND INSTALLED IAW SRM 51-40-02-0G-0 AND 51-40-05-0G-0.Jun 27, 2013 · N705AS · Boeing 737490SDR DALA13033029258Skate Angle · damagedRIGHT INBD SKATE ANGLE WAS FOUND DAMAGED DURING DVI OF SURROUNDING STRUCTURE OF DORSAL FIN. REMOVED RIGHT INNER SKATE ANGLE. DRILLED NEW ANGLE. INSTALLED ANGLE IAW SRM 55-30-05, P27 AND DWG 5912188.Jun 26, 2013 · N958DN · Doug MD9030SDR WVER201306239023Drag Angle · crackedLEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT DRAG ANGLE IS CRACKED.Jun 23, 2013 · N902FJ · Cndair CL6002D24SDR SIMA20130620014Drag Angle · crackedVERTICAL STABILIZER FWD DRAG ANGLE CRACKED. REPAIRED IAW EO EM-53MR-1281.Jun 20, 2013 · N613AE · Emb EMB145SDR USAA2013070100026Hinge Fitting · excess play2S CHECK - EXCESSIVE PLAY ON VERTICAL STABABILIZER HINGE ARM FITTING NR 7 AT STAB STA 569, RIB 11. REPLACED VERTICAL STABABILIZER HINGE ARM FITTING NR 7 IAW AMM 55-36-41-0401.Jun 3, 2013 · N766US · Airbus A319112SDR USAA2013070100025Hinge Fitting · excess play2S CHECK - EXCESSIVE PLAY ON VERTICAL STABABILIZER HINGE ARM FITTING NR 5 AT STAB STA 249 BETWEEN RIB 5 TO RIB 6. REPLACED VERTICAL STABABILIZER HINGE ARM FITTING NR 5 IAW AMM 55-36-41-400-001-A.Jun 3, 2013 · N766US · Airbus A319112SDR USAA2013070100024Hinge Fitting · excess play2S CHECK - EXCESSIVE PLAY ON VERTICAL STABABILIZER HINGE ARM FITTING NR 2 AT STAB, STA 120 BETWEEN RIB 2 TO RIB 3. REPLACED VERTICAL STABABILIZER HINGE ARM FITTING NR 2 IAW AMM 55-36-41-400-001-A.Jun 3, 2013 · N766US · Airbus A319112SDR USAA2013062700013Hinge Fitting · excess play2S CHECK - EXCESSIVE PLAY ON VERTICAL STABILIZER NR 1 HINGE ARM FITTING AT VERTICAL STAB. STA. AMM 55-36-41-400-001-A.Jun 3, 2013 · N766US · Airbus A319112SDR USAA2013062700012Hinge Fitting · excess play2S CHECK - EXCESSIVE PLAY ON VERTICAL STABILIZER NR 4 HINGE ARM FITTING AT VERT STAB STA 206 & BETWEEN RIB 4 TO RIB 5. REPLACED VERTICAL STABILIZER NR 4 HINGE ARM FITTING IAW AMM 55-36-41-400-001-A.Jun 3, 2013 · N766US · Airbus A319112SDR 29GA201306210002Angle · corrodedDURING ROUTINE SCHEDULED MAINTENANCE, DISCOVERED RIGHT ANGLE ON VERTICAL AFT SPAR HAS CORROSION ABOVE AND BELOW UPPER RUDDER HINGE BRACKET. REMOVED CORROSION AND BLENDED AREA ON VERTICAL AFT SPAR RIGHT ANGLE AS REQUIRED AND INSTALLED WEB FLANGE STRAP.May 21, 2013 · N87551 · Beech 1900DSDR 29GA201306210003Angle · corrodedDURING ROUTINE SCHEDULE MAINTENANCE, DISCOVERED CORROSION ON THE VERTICAL STABILIZER AT STATION 70.0 AND 64.0. REMOVED CORROSION AND BLENDED AREA ON VERTICAL AFT SPAR RIGHT ANGLE AS REQUIRED.May 20, 2013 · N53545 · Beech 1900DSDR 29GA201305220002Structure · corrodedDURING ROUTINE SCHEDULED MAINTENANCE, DISCOVERED CORROSION ON VERTICAL STABILIZER STATION 70.0 AND 64.0.May 20, 2013 · N87551 · Beech 1900DSDR C77A20130505014Flange · damagedVERTICLE STAB LT SIDE L/E ATTACH FLANGE HAS DRILL/ SCREW DAMAGE, 2ND LT FASTENER HOLE UP FROM FUSELAGE SKIN. ENLARGED THE FASTENER HOLE, REMOVE THE HIGH METAL AND FILL IN VOID WITH SEALANT IAW SRM PART II 51-40-02 AND 51-10-03.May 5, 2013 · N603CZ · Emb ERJ170200LRSDR IPXA3M77842Intercostal · crackedINSPECTION TYPE:4C, APPROX .50" CRACK ALONG AFT EDGE OF INTERCOSTAL PN AJC7582-5 AT TYPICAL LOCATION IN RADIUS OF RELIEF CUT OUT FOR VERT STAB AFT SPAR. REPAIRED INTERCOSTAL (PN AJ7582-5) AT VERT STAB AFT SPAR RELIEF CUT OUT REF SRM 55-30-01, FIG 201 REPAIR 2Mar 27, 2013 · N296UP · Doug MD11FSDR DXTA2013032505337Structure · dentedVERTICAL STAB LEADING EDGE HAS SEVERAL DENTS. COLD WORKED DENTS IAW SRM 51-40-03. MINOR REPAIR.Mar 23, 2013 · N603QS · Cessna 560XLSDR HNAA2013032200152Hinge Fitting · corrodedAFT SPAR VERTICAL STABILIZER LOWER HINGE FITTING IS CORRODED. REPLACED AFT SPAR VERTICAL STAB LOWER HINGE FITTING IAW AMM 20-14-01.Mar 22, 2013 · N336EN · Dhav DHC8311SDR HNAA2013032200151Hinge Fitting · corrodedUPPER HINGE FITTING ON AFT VERTICAL STABILIZER IS CORRODED. REPLACED UPPER HINGE FITTING IAW AMM 20-14-01.Mar 22, 2013 · N336EN · Dhav DHC8311SDR DALA13010855816Panel · damagedDAMAGED VERTICAL STAB RT FWD TORQUE BOX PANEL. PANEL REMOVED AND INSTALLED. COMPLIED WITH IAW ERA 512204-14, REV ORG.Mar 7, 2013 · N596NW · Boeing 757351SDR DALA13009829207Skate Angle · crackedLT ANGLE CRACKED, LOWER VERTICAL. REMOVED ANGLE FROM ACFT, DRILLED, AND INSTALLED SKATE ANGLE IAW DWG5912188 AND SRM 51-01.Mar 2, 2013 · N907DA · Doug MD9030SDR DALA13002440927Structure · crackedON BOLT HOLE INSPECTION OF VERTICAL STAB, FOUND OVERSIZED HOLE WITH CRACK INDICATION. FOUND HOLE TO BE LARGER THAN .202" ALLOWABLE HOLE SIZE. OVERSIZED HOLE WAS REPAIRED IAW FINAL ER/A 510507-14AD REV ORIG ASSOCIATED ER/A 14-510507 ADDED FOR AC 0927.Jan 16, 2013 · N927DA · Doug MD88SDR DALA13002450927Structure · damagedON BOLT HOLE INSPECTION OF VERTICAL STAB, FOUND THREE HOLES DAMAGED. DAMAGE CLEAN-UP RESULTED IN OVERSIZING HOLES LARGER THAN ALLOWED SIZE. OVERSIZED HOLES WERE REPAIRED IAW ER/A 510499-14AD, REV ORIG ASSOCIATED ER/A 14-510499 ADDED FOR AC 0927.Jan 11, 2013 · N927DA · Doug MD88SDR DALA13002430927Structure · crackedON BOLT HOLE EC INSPECTION OF RT SIDE VERTICAL, 3 HOLE DOWN FROM COLLAR, FAULT FOUND OVERSIZED HOLE WITH CRACK INDICATION, CLEAN UP OF HOLE, NO HELP. FURTHER CLEANUP OF SUSPECTED HOLE WITH CRACK AND FOUND HOLE TO BE LARGER THAN .202" ALLOWABLE HOLE SIZE. OVEJan 11, 2013 · N927DA · Doug MD88SDR DALA12016080936Fairing · crackedON INSTALLATION OF VERTICAL STAB TIP FAIRING, FOUND A CRACK ON RT SIDE, EMINATING FROM A RADIUS OF UPPER SKIN. REMOVED FITTING ON RT STAB FAIRING BY ACCESS TO CRACK. NDT VERIFIED END OF CRACK, CHECK STOP DRILL, AND OPEN HOLES. FABRICATED, PRIMERED, TREATED, Dec 13, 2012 · N936DL · Doug MD88SDR DALA12015800955Skate Angle · crackedLEFT VERTICAL STABILIZER REPAIR DOUBLER-SKATE ANGLE-CRACKED AT STABILIZER T/E. REF NR 142, REMOVED PREVIOUS REPAIR ANGLE THAT WAS CRACKED AND REPAIRED BY FABRICATING NEW REPAIR ANGLE SAME AS PREVIOUSLY INSTALLED. REPAIRED IAW SRM 53-05, FIG 23.Dec 10, 2012 · N955DL · Doug MD88SDR GLBA2012112800120Structure · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND TWO CRACKS COMING OUT OF RIVET HOLE, ONE CRACK COMING OUT OF ANOTHER RIVET HOLE ON THE LONGERON UNDER FINGER DOUBLER AT FS 107, 0.375" IN LENGTH. MX REPAIRED THE AFFECTED AREA IAW EO 12-1900-53-073. MAJOR REPAIR.Nov 28, 2012 · N202UX · Beech 1900D
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