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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR AU960893Rib · corroded(AUS) VERTICAL STABILISER AFT SPAR UPPER RIB PNO 96-640000-11 AND LOWERRIB PNO 96-640000-105 SEVERELY CORRODED - RIBS SUPPORT RUDDER PIVOT FLANGES - INVESTIGATION FOUND MORE CORROSION IN FUSELAGE AND AFT CABIN FLOOR STRUCTURE, LUGGAGE DOOR FRAME - STEP SUPPORTSDR C2XA96IA157Rod Assy · corrodedIAH - DURING C-CHECK INSPECTION, THE VERTICAL STABILIZER LINK ROD ASSEMBLY WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE ROD ASSEMBLY PER ATR JIC 55-30-00 RAI 10000-002 AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR IXXA9694Angle · crackedDURING ROUTINE C-CHECK INSPECTION, THE RIGHT VERTICAL STABILIZER ATTACH ANGLE WAS FOUND CRACKED AND CORRODED AT THE FRONT SPAR. REPAIR OF THE ANGLE WAS ACCOMPLISHED IAW FAA DER APPROVED DRAWING A62-R112. (M)SDR DHL96721118Forging · crackedAT C-CHECK, FOUND VERTICAL FIN FRONT SPAR FORGING LT SIDE LOWER HORIZONTAL CHORD HAS CRACK FROM LBL .5 TO LBL 1.5. STOP DRILLED CRACK, INSTALLED CHORD REPAIR PER AVITAS ENGINEERING DRAWING 96PMSI124R-1.SDR DHL96721117Forging · crackedAT C-CHECK, FOUND VERTICAL FIN FRONT SPAR FORGING RT SIDE LOWER HORIZONTAL CHORD HAS CRACK FROM RBL 1.5 TO 4.5. LOWER VERTICAL WEB CRACKED FROM RBL 1.25 TO 5.75. STOP DRILLED HOLES AND INSTALLED FIN FRONT SPAR FORGING AND WEB REPAIR PER AVITAS ENGINEERING DRSDR HEEA967374Fin Assy · corrodedFIN ASSY IS CORRODED. (RIV-NUT IMPROPERLY INSTALLED AND CORRODED) SEPARATED AT AFT LOWER EDGE.SDR DHL96721116Forging · crackedVERTICAL FIN FRONT SPAR FORGING HAS INTERIM REPAIR PER AVITAS EO 96PMS I114RO-1. REMOVED INTERM REPAIR PER SRM 51-30-2, INSTALLED VERTICAL FIN FRONT SPAR FORGING PER AVITALS ENGINEERING DRAWING 96PMSI124D-1.SDR USAA960438Angle · crackedPIT - DURING Q-4 CHECK INSPECTION, FOUND 2 INCH CRACK IN DRAG ANGLE RADIUS RT VERTICAL STABILIZER. DRAG ANGLE STA 1089. INSTALLED REPAIR ANGLE PER SRM 53-05, FIGURE 23. (X)SDR CALA9600912Web · crackedINSPECTION FOUND A FOUR INCH CRACK IN STIFFENER WEB INSIDE VERTICAL FIN ABOVE S-DUCT AT STA 1348. THE CRACK WAS STOPPED DRILLED, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-2, 51-30-2 AND MM 51-20-11.SDR DL72W961256Stringer · crackedFOUND DURING A-2 LETTER CHECK, 1 INCH CRACK AT STRINGER TO BULKHEAD ATTACH BOLT AT FIN STA 180.6 STR 8 LT SIDE. REPAIRED PER M/M 55-30-0 FIG 803.SDR DL72S961245Stringer · crackedFOUND DURING B-2 LETTER CHECK, STRINGER CRACKED 1ST BAY FROM TOP OF VERT STAB LT SIDE. REPAIRED PER M/M 55-30-0 FIG 803.SDR DL72S961244Stringer · crackedFOUND DURING B-2 LETTER CHECK, STRINGER CRACKED 2ND BAY FROM TOP LT SIDE. REPAIRED PER M/M 55-30-0 FIG 803.SDR DL72S961242Web · crackedFOUND DURING B-2 LETTER CHECK, WEB ANGLE CRACKED LT SIDE 2ND BAY UP FROM ACCESS PANEL 9504. REPAIRED PER M/M 55-30-0 FIG 802.SDR DL72S961241Stringer · crackedFOUND DURING B-2 LETTER CHECK, TWO STRINGERS CRACKED 3RD BAY FROM TOP RT SIDE VERT STAB. REPAIRED PER M/M 55-30-0 PG 803.SDR DL72S961240Stringer · crackedFOUND DURING B-2 LETTER CHECK, STRINGER CRACKED RT SIDE 2ND BAY UP FROM ACCESS PNL 9504. REPAIRED PER M/M 55-30-0 FIG 803.SDR AU960764Hinge · corroded(AUS) FIN HINGE ASSEMBLIES CORRODEDSDR UPS96220195Fitting · crackedINSPECTION TYPE-C, CRACKED L-EXTRUSION AT RT FIN REAR SPAN CLOSURE RIB FITTING, ACCESS UNDER PANEL 9780. REMOVED AND REPLACED FITTING IAW SRM 51-30-2, 51-30-5.SDR AU960655Tailplane · cracked(AUS) LH AND RH SECTIONS OF TAILPLANE CRACKED IN EIGHT PLACES - MOST CRACKING WAS FOUND TO ORIGINATE FROM RIVETS IN RIBS AND INTERCOSTAL ANGLES - TWO CRACKS WERE ALSO FOUND IN THE SKIN - NUMEROUS RIVETS WORKING - FOUND DURING INSPECTION IAW NMD-55-34SDR DL72E961142Stringer · crackedSTRINGER CRACKED INSIDE TAIL CRAWLWAY 3RD BAY FROM TOP LT SIDE. REPAIRED PER MM 55-30-0 FIG 803.SDR C2XA96IA129Drag Angle · crackedIAH - DURING C-CHECK INSPECTION, THE LEFT VERTICAL STABILIZER DRAG ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE LEFT DRAG ANGLE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR DL72L961071Stringer · crackedTWO VERTICAL STABILIZER STRINGERS CRACKED RT SIDE FOURTH BAY FROM TOP, STR 8 AND STR 10. REPAIRED PER M/M 55-30-0, FIG 803.SDR DHL9670920CSpar Forging · corrodedAT C-CHECK FOUND CORROSION ON VERTICAL FIN FRONT SPAR FORGING BELOW S-DUCT AND LEFT SIDE OF SPLICE PLATE. INSTALLED NEW MODIFIED FRONT SPAR FORGING UPPER SPLICE PLATE BELOW S-DUCT PER AVITAS EO 96PMSI 123D-1, REPAIR 10 BY 3.SDR DL72S961056Stringer · crackedFOUND ON LETTER CHECK, RT STRINGER 10 CRACKED AT FIN STA 133 INSIDE VERTICLE STABILIZER CRAWL WAY. REPAIRED PER M/M 55-30-0, FIG 803 - ID PER PS900-5-1 NR 04.SDR CKSA96046Angle · corrodedKOSC - FLT 72016 - DURING 'C-1' CHECK INSPECTION FOUND, CARD NR 6000-0551 AREA, AFT FUSELAGE/VERTICAL STABILIZER. VERTICAL STABILIZER TO FUSELAGE ATTACH LEVEL 2 TASK NR 74798. REPAIRED VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE IAW DC-8 SRM 53-2-5, FIGURE SDR CKSA96045Angle · corrodedDURING 'C-1' CHECK INSPECTION FOUND, CARD NR 6000-0551 AREA, AFT FUSELAGE/VERTICAL STABILIZER. VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE RIGHT SIDE HAS STRESS CRACKS AND CORROSION. LEVEL 2 TASK NR 74799. CLEANED CORROSION AND FOUND TO BE OUT OF LIMITS. SDR CALA9600803Bracket · crackedINSPECTION FOUND A 1.5 INCH CRACK IN LT ANGLE BRACKET AT REAR SPAR OF VERTICAL STABILIZER. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-00-0, 51-40-3, 51-10-2 AND 51-30-2.SDR CALA9600802Bracket · crackedINSPECTION FOUND A 2 INCH CRACK IN RT ANGLE BRACKET AT REAR SPAR OF VERTICAL STABILIZER. THE CRACK WAS STOP DRILLED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-10-2 AND 51-30-2.SDR DL72S961033Stringer · crackedFOUND ON C-2 LETTER CHECK, STRINGER CRACKED SECOND BAY DOWN FROM TOP LEFT SIDE INSIDE VERTICAL FIN. REPAIRED PER M/M 55-30-0. FIG 803.SDR DL72S961032Stringer · crackedFOUND ON C-2 LETTER CHECK, STRINGER CRACKED TOP BAY RT SIDE AT ATTACH BOLT, INSIDE VERTICAL FIN. REPAIRED PER M/M 55-30-0, FIGURE 803.SDR C2XA96IA114Angle · crackedIAH - DURING C-CHECK INSPECTION, THE LEFT VERTICAL STABILIZER DRAG ANGLE WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE DRAG ANGLE AND THE AIRCRAFT WAS RETURNED TO SERVICE. ACFT TT: 14,059.3 HRS. CYCLES, 18,999. (X)SDR C2XA96IA107Angle · crackedIAH - DURING C-CHECK INSPECTION, THE VERTICAL STABILIZER RIGHT DRAG ANGLE WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE DRAG ANGLE AND THE AIRCRAFT WAS RETURNED TO SERVICE. ACFT TT: 14,059.3 HRS. CYCLES, 18,999. (X)SDR ARWR960700Skin · corrodedDURING C-CHECK, FOUND VERTICAL FIN LEADING EDGE LOWER PANEL LOWER ATTACH SCREW HOLE AREA HAS CORROSION. REMOVED DAMAGED AREA IAW SRM 55-2-1, FABRICATED FILLER AND DOUBLER IAW SRM 55-2-1, PAGES 17-18, ALODINED AND PRIMED IAW SRM 51-1-8. INSTALLED REPAIR IAW SSDR 96ZZZX2628Skin · corrodedDURING C-CHECK, FOUND FUSELAGE SKIN BELOW FREON EXHAUST DOOR HAS WORKING FASTENERS, LT SIDE. REMOVED INTERCOSTAL, FABRICATED NEW INTERCOSTAL, CLEANED CORROSION IN AREA, FOUND WITHIN LIMITS. TREATED AND PRIMED AREA AND INTERCOSTAL IAW SRM 51-1-8. INSTALLED RSDR IXXA9665Angle · crackedDURING ROUTINE C-CHECK INSPECTION, THE VERTICAL STABILIZER FUSELAGE ATTACH ANGLE AT STATIONS 1626, 1640, AND 1667, WAS FOUND CRACKED. REPAIR OF THE CRACKED ANGLE WAS ACCOMPLISHED IAW DOUGLAS ROD SKETCH 96-04-02-005, WHICH IS FAA DER APPROVED. (X)SDR SCNA96062Bolt · corrodedDURING HEAVY MAINTENANCE VISIT CORROSION WAS FOUND AT THE VERTICAL STABILIZER TRAILING EDGE SPLICE BOLTS NR 3 AND NR 4 OF RS 124. REMOVED BOLTS, CLEANED CORROSION FROM THE HOLES, TREATED WITH LP5.3 AND INSTALLED NEW BOLTS IN ACCORDANCE WITH B727 MM 51-20-11 ASDR USAA960385Angle · crackedPIT - DURING A SCHEDULED Q-1/C-1 CHECK INSPECTION, FOUND 3.5 INCH CRACK LEFT SIDE AFT DRAG ANGLE AT LOWER VERT STAB. INSTALLED DOUBLER REPAIR PER USAIR EA 32425. (M)SDR USAA960384Angle · crackedPIT - DURING A SCHEDULED Q-1/C-1 CHECK INSPECTION, FOUND 3.5 INCH CRACK RIGHT SIDE DRAG ANGLE LOWER VERT STABILIZER. INSTALLED DOUBLER REPAIR PER USAIR EA 32426. (M)SDR DL72S960849Stringer · crackedA .75 INCH CRACK IN VERT STAB STR 7 AT 3RD BULKHEAD ABOVE OPENING TO CRAWLWAY. REPAIRED PER M/M 55-30-0.SDR UPS96220047Forging · crackedINSPECTION TYPE C-HFEC INSP, DET CRACK ON RT SIDE OF VERT STAB FRONT SPAR FORGING AT FIRST HOLE AFT OF STA 1233 TOP ROW OF FASTENERS. CRACK IS .5 INCH LONG RUNS AFT OF HOLE. STOP DRILLED CRACK, REPAIRED VERT STAB CRACK PER DRAWING 65-62346 AND SRM 51-30-2.SDR 96ZZZX2239Channel · crackedDURING C/W AD 95-13-02 IAW SB 218 PART 2, VERTICAL STABILIZER CHANNEL WAS FOUND CRACKED AT THE BEND RADIUS. A NEW PART WAS MADE FROM THE SAME MATERIAL AND TO THE SAME DIMENSIONS IAW 43.131A. REASSEMBLY WAS C/W - NO PROBLEMS. THIS CHANNEL WAS NOT IN THE AREASDR DL72S960754Stringer · crackedFOUND ON C-2 LETTER CHECK, VERT STAB STRINGER CRACKED RT SIDE TAIL CRAWLWAY, FOURTH BAY UP. REPAIRED PER M/M 53-30-0.SDR UPS96205914Chord · crackedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED FIN STA 13.74 CHORD FOUND TO BE CRACKED. REMOVED, FABRICATED AND INSTALLED IAW SRM 51-30-2.SDR DL72S960657Stringer · crackedFOUND DURING B-2 LETTER CHECK, STRINGER CRACKED RT SIDE TAIL CRAWLWAY ONE AND ONE HALF BAYS DOWN. REPAIRED PER M/M 55-30-0.SDR DL72S960656Stringer · crackedFOUND DURING B-2 LETTER CHECK, STRINGER CRACKED IN TAIL CRAWLWAY BETWEEN 2ND AND 3RD BAY RT SIDE. REPAIRED PER M/M 55-30-0.SDR 96ZZZX1655Rivets · looseDURING SCHEDULED INSPECTIONS, LOOSE FASTENERS ON BOTH SIDES OF VERTICAL STABILIZER FORWARD SPAR WERE NOTED. ALTHOUGH A SIMILAR PROBLEM WAS ADDRESSED IN SB 2004 ON EARLIER MODEL 1900S, ADDITIONAL EVALUATION AND STUDIES ARE RECOMMENDED AS OTHER PREVIOUS IDENTIFSDR AU960396Vertical Fin · corroded(AUS) VERTICAL FIN AND LH AND RH STRINGERS CONTAINED EXFOLIATION CORROSIONSDR DL72S960546Former · crackedFOUND DURING C-2 LETTER CHECK, 1.25 INCH CRACK VERT STAB FORMER AT STRINGER ATTACH POINT, FIN STATION 110.4 AND STR 9 LEFT. REPAIRED PER M/M 55-30-3 PG 802.SDR 96FDEA00551Fitting · corrodedCORROSION (C53-137-01) BS 1342 LBL 17 STR 5L ON FITTING ANGLE. REMOVED AND REPLACED FITTING ON VERTICAL STABILIZER AT BS 1342 LBL 17 AT STR 5L PER SB 727-55-00.SDR 96ZZZX1731Rivets · looseDURING SCHEDULED INSPECTIONS, LOOSE FASTENERS ON BOTH SIDES OF VERTICAL STABLILIZER FORWARD SPAR WERE NOTED. ALTHOUGH A SIMILAR PROBLEM WAS ADDRESSED IN SB 2044 ON EARLIER MODEL 1900S, ADDITIONAL EVALUATION AND STUDIES ARE RECOMMENDED AS OTHER PREVIOUS IDENTISDR 96ZZZX1733Rivets · looseDURING SCHEDULED INSPECTIONS, LOOSE FASTENERS ON BOTH SIDES OF VERTICAL STABILIZER FORWARD SPAR WERE NOTED. ALTHOUGH A SIMILAR PROBLEM WAS ADDRESSED IN SB 2044 ON EARLIER MODEL 1900S, ADDITIONAL EVALUATION AND STUDIES ARE RECOMMENDED AS OTHER PREVIOUS IDENTIF
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