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 96ZZZX1821Suport · corrodedMAJOR INSPECTION FOUND VERTICAL STABILIZER SUPPORT, AFT LOWER, CORRODED. SUPPORT WAS REPLACED.SDR 96ZZZX1818Bulkhead · corrodedMAJOR INSPECTION FOUND FORWARD CANTED BULKHEAD WITH INTERGRANULAR CORROSION. BULKHEAD WAS REPLACED.SDR EISA96012Panel · damagedVERTICAL STABILIZER INTERIOR STRUCTURE PANEL UNDER ELEVATOR CONTROL RODS AREA HAS A PROTRUDING HOLE ON PANEL. REMOVED PROTRUSION FROM HOLE FABRICATED DOUBLER AND INSTALLED PER SRM 51-30-03. (M)SDR 96FDEA00314Lt Fitting · corrodedCORROSION (C53-137-01) BS 1342 LBL 17 STR 5L ON FITTING ANGLE. REMOVED AND REPLACED FITTING AT 1342, LBL 17 AT S5L PER.SDR 96FDEA00313Rt Fitting · corrodedCORROSION (C53-137-01) BS 1342 RBL 17 STR 5R ON FITTING ANGLE. REMOVED CORROSION TERMINAL FITTING AND INSTALLED NEW RT SPAR FITTING AT BS 1342 IAW BOEING SB 727-55-088.SDR 96ZZZX1652Rivets · looseDURING SCHEDULED INSPECTION, 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 IDENTIFISDR 9605452297Stringer · crackedDURING H-CHECK, FOUND CRACKS IN THE VERTICAL STABILIZER STR 8 AT STA 110 AND IN STR 11 AT STA 134. REPAIRED STRINGERS (P/N 65-16811-3, P/N 65-16810) PER EA 22-103467.SDR AU960192Housing · corroded(AUS) STABILIZER STRUT DAMPER SHAFT PULLED FROM FITTING DURING HEAVY VIBRATION FOLLOWING TAIL ROTOR DRIVE SHAFT FAILURE (MDR 96/0191) - FITTING EXHIBITED SIGNS OF SEVERE INTERGRANNULAR CORROSION - AIRCRAFT OPERATES IN A SALT LADEN ENVIRONMENTSDR USAA960260Angle · crackedPIT - DURING C-3 CHECK INSPECTION, FOUND 1.5 INCH CRACK IN LEFT DORSAL FIN DRAG ANGLE AT STATION 1126. STOP DRILLED CRACK AND INSTALLED DOUBLER REPAIR PER SRM 53-05 PG 506. (M)SDR UPS96805619Angle · corrosionWHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON VERTICAL STABILIZER TO FUSELAGE RT ATTACH ANGLE. REPAIRED ANGLE PER SRM 53-2-5, FIG. 16A.SDR 96ZZZX1653Rivets · 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 IDENTIFSDR UPS96205648Chord · crackedWHILE IN FOR MOD WORK, MAINTENANCE REPORTED LT INNER CHORD FIN STA 22.5 IS CRACKED. REMOVED DAMAGED AREA I.A.W. BOEING DWG 65C20296. INSTALLED REPAIR DOUBLER PER BOEING DWG 65C20296 AND SRM 51-30-2.SDR 96ZZZX3191Vertical Fin · plug looseBREAK OUT PLUG LOOSE. REMOVED AND REPLACED.SDR DL72L960257Stringer · crackedSTRINGERS CRACKED 3RD BAY UP IN VERT STAB ON LT AND RT SIDE UPPER END AND 3RD BAY UP RT LOWER. FOUND DURING A-2 LTR CK TPAMM AND REPAIRED PER SRM 55-30-0.SDR 96ZZZX1732Rivets · 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 IDENTIFSDR 96ZZZX1657Rivets · 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 AT OTHER PREVIOUS IDENTIFSDR 96ZZZX1656Rivets · 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 IDENTIFSDR 96FDEA00136Fitting · crackedLT VERTICAL FIN FRONT SPAR TERMINAL FITTING FWD O/B FLANGE IS CRACKED. REPAIRED LT VERTICAL FIN FRONT SPAR TERMINAL FITTING FWD O/B FLANGE IAW FEDEX EA 7-5510-26907.SDR UPS205333Mid Spar · chafedWHILE IN FOR C-CHECK MAINTENANCE REPORTED, LT VENT FIN MID SPAR CHORD IS CHAFED AT ACCESS PNL 9601. REPAIRED AS REQUIRED PER UPS EO 727-55-0309.SDR 96FDEA00130Stringer · crackedVERTICAL FIN STA 110, STR 8L IS CRACKED, BAY NR 6. REPAIRED CRACKED STRINGER PER SRM 55-30-4.SDR MWEA96019Angle · crackedDURING C-CHECK, FOUND VERTICAL STAB TO FUSELAGE EXTERIOR ATTACH ANGLE CRACKED ON LT SIDE APPROX 8 INCH FROM AFT END. INSTALLED DOUBLER REPAIR IAW SRM 53-05 FIG 23.SDR DL72S960278Stringer · crackedSTRINGER 8 ON LT SIDE OF VERT STAB AT FIN STA 180.6 IS CRACKED. FABRICATED REPAIR ANGLE IAW MM 55-30-0 PG 803.SDR CAL960162Angle · crackedMIA - INSPECTION FOUND A .5 INCH CRACK IN LEFT AND RIGHT VERTICAL STABILIZER TO FUSELAGE EXTERNAL ATTACH ANGLES LOCATED BETWEEN BS 1401 TO 1429. THE ANGLES WERE REMOVED AND REPLACED IAW SRM 51-30-2. (M)SDR 96ZZZX1654Rivets · 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 IDENTIFISDR 9600771154Fitting · crackedDURING T-CHECK, FOUND A CRACK IN THE NR 4 BANJO FITTING, FORWARD RIGHT FLANGE IN THE RADIUS. REPAIRED PER SRM 55-20-00, SHEETS 1-17.SDR AU960196Skin · corroded(AUS) VERTICAL STABILIZER LEADING EDGE SKIN PN 0531006-96 AND LEADING EDGE RIB PN 0531006-5 CORRODED IN AREA WHERE MASKED BY DORSAL FINSKIN - SUSPECT CAUSED BY INADEQUATE PROTECTION AND PROCEDURES DURING PAINT STRIPPING - PERSONNEL/MAINTENANCE ERROR - SEE MDSDR 96ZZZX1651Rivets · 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 IDENTIFSDR 96ZZZW19Cap · corrodedLEVEL 2 CORROSION - LOWER END OF NR 2 VERTICAL STABILIZER LEADING EDGE CAP IS CORRODED. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 55-2-1.SDR USAA951362Angle · crackedPIT - DURING Q-1/C-3 CHECK INSPECTION, FOUND .75 INCH VERTICAL CRACK AFT SIDE OF STA 1388, CANTED FRAME, IN ANGLE ON LEFT FRONT SPAR OF VERTICAL STABILIZER. INSTALLED ANGLE REPAIR PER SRM 55-02, FIGURE 26. (X)SDR C2XA95IA416Angle · crackedIAH - DURING C-CHECK INSPECTION, FOUND LEFT DRAG ANGLE CRACKED NEAR FORWARD END. MAINTENANCE REMOVED AND REPLACED THE DRAG ANGLE, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA95IA415Angle · crackedIAH - DURING C-CHECK INSPECTION, FOUND RIGHT DRAG ANGLE CRACKED NEAR FORWARD END. MAINTENANCE REMOVED AND REPLACED THE ANGLE, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M)SDR DL72S954728Stringer · crackedFOUND DURING E-2 LETTER CHECK, VERTICAL STAB STRINGERS CRACKED, STR 8 RIGHT STA 133.8 AND STR 9 RIGHT STA 133.8. REPAIRED PER M/M 53-30-0 PAR 3.SDR 96ZZZX248Dorsal Fin · damagedPILOT NOTICED TAIL FLUTTER, DIFFICULT TO CONTROL IN CROSSWIND. PILOT LANDED WITHOUT INCIDENT. UPON EXITING AIRPLANE, PILOT NOTICED HOLE IN DORSAL FIN. ABUSIVE HANDLING AND LOW TEMPERATURE SUSPECTED CAUSE OF PART MALFUNCTION.SDR 96ZZZX434End Plate · damagedREPAIR KNOCK-OUT PLUG IN VERTICAL FIN.SDR 95FDEA01879Stringer · wornVERTICAL FIN, BAY NR 9 FIN STA 180.6, STR 7R, WORN FASTENER HOLE AT THE RIB CHORD AND STR. REPAIRED WORN RIB CHORD AND STR PER FEDEX SRM 55-30-4, FIG 1 AND FEDEX EA 7-5510-26736. C/A ADDITION.SDR CAL951139Angle · crackedIAH - INSPECTION FOUND A .25 INCH CRACK AT FASTENER HOLE OF RT VERTICAL FIN ATTACH ANGLE. THE ATTACH ANGLE WAS REMOVED AND REPLACED IAW SRM 53-05, FIGURE 19. (X)SDR DL72S954582Tie Angle · crackedFOUND DURING E-2 LETTER CHECK, VERTICAL STAB STRINGER TIE ANGLES CRACKED AT STA 157.200 2ND BAY FROM TOP LT SIDE. TWO ANGLES CRACKED AT 4TH BAY FROM TOP STA 133.800. REPAIRED PER M/M 53-30-0 PAR 3.SDR HALA95164Attach Bolt · crackedLAX - DURING ACCOMPLISHMENT OF SPECIAL CARD ITEM NR 3950-1F, FOUND RIGHT FORWARD VERTICAL STABILIZER ATTACH BOLT CRACKED, LOCATED UNDER LEADING EDGE WRAP AROUND PANEL. REPLACED RIGHT FRONT SPAR VERTICAL STABILIZER ATTACH BOLT WITH P/N 3D0031-20-86. (M)SDR 96ZZZX229Angle · crackedSTL - DURING CHECK C, FOUND A .3750 INCH CRACK IN RIGHT SIDE OF VERTICAL STABILIZER ATTACH ANGLE, STA 1292. REPAIRED BY INSTALLLING DOUBLER PER SRM 53-05, FIGURE 23. AIRCRAFT TOTAL TIME: 40,618 HOURS, 36,293 CYCLES.SDR 96ZZZX228Angle · crackedSTL - DURING CHECK C, FOUND A 2.50 INCH CRACK AT LEFT SIDE OF VERTICAL STABILIZER ATTACH ANGLE, FS 1292. REPAIRED PER SRM 53-05, FIGURE 23. AIRCRAFT TOTAL TIME: 40,618 HOURS, 36,293 CYCLES.SDR CAL951060Angle · crackedIAH - INSPECTION FOUND A .75 INCH CRACK IN VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE, LT SIDE. A REPAIR WAS PERFORMED IAW SRM 53-05, FIGURE 23A. (X)SDR ABXA9600234Angle · corrodedDURING C-CHECK INSPECTION, FOUND VERTICAL STABILIZER REAR SPAR, RIGHT SUPPORT FOR PANEL 60407 CORRODED. REPAIRED IAW ABX REA D955-13589-MR.SDR DL72S954378Stringer · crackedFOUND DURING E-2 LETTER CHECK, VERT STAB STRINGER CRACKED AT FIN STA 110.4 AND STR 10 LEFT. REPAIRED PER M/M 55-30-0 PAR 3.SDR DL72S954377Angle · crackedFOUND DURING E-2 LETTER CHECK, VERTICAL STAB FORMER ATTACH ANGLE CRACKED AT FIN STA 157.2 AND STR8 LEFT. REPAIRED PER M/M 55-30-0 PAR 2.SDR CA951122013Fitting · cracked(CAN)MIDDLE FITTING FOR THE VERTICAL SABILIZER FOUND CRACKED ON REMOVAL.SDR UPS804944Angle · crackedWHILE IN FOR C-CHECK, MAINTENANCE FOUND RT VERTICAL STAB TO FUSELAGE ATTACH ANGLE HAS 1 INCH LONG CRACK. REPAIRED PER UPS EO DC8-5310-7585-A.SDR 95FDEA01590Stringer · crackedNR 7 STR IS CRACKED AT VERTICAL FIN STA 133.80 LT SIDE. REMOVED DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED PER FEDEX 55-30-4.SDR DL72S954228Stringer · crackedFOUND AT HMV, STRINGER 8R CRACKED IN VERTICAL STAB INTERIOR IN 2ND BAY DOWN. REPAIRED PER MM 55-30-0 PG 803.SDR DL72S954227Stringer · crackedFOUND AT HMV, STRINGER 11L CRACKED AT STA 1342 INSIDE VERT STAB. REPAIRED PER MM 53-30-0 PG 803.SDR DL72S954052Angle · crackedBULKHEAD ATTACH ANGLE CRACKED AT STR 10 LT SIDE FIN STA 180.600, INSIDE VERT STAB CRAWLWAY. FOUND AT D-2 LTR CK AND REPAIRED PER MM 55-30-0.
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