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 96ZZZM335Terminal Block · corrodedFOUND CORRODED TERMINAL BLOCK AFT OF HORIZONTAL STABILIZER REAR SPAR RIGHT SIDE INBOARD AT VERTICLE FIN TERMINAL BLOCK LABELED UB25. LOCATED ON ELEVATOR CONTROL BOX STRUCTURE. REMOVED AND REPLACED TERMINAL BLOCK UB25 AND REPLACED WIRE LUGS TO UB25. ELEVATORSDR 96ZZZX1892Fitting · crackedDURING C-CHECK, FOUND VERTICAL STABILIZER, FORWARD RT FUSELAGE TO STABILIZER ATTACH FITTING CRACKED. REPLACED FITTING, PN 5920103-2. ACFT TT: 22,675 HRS. ACFT TC: 41,431.SDR UPS204781Shear Tie · corrodedWHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION (C55-395-10-00-01) ON BOTH LT AND RT FWD SHEAR TIES INSIDE VERTICAL FIN TUNNEL AT FIN STA 87.0 UPPER END OF RIBS NR 5. MECHANICALLY REMOVED CORROSION. REWORK OUT-OF-LIMITS IAW SRM 55-50-00. REMOVED AND REPLSDR UPS204771Shear Tie · corrosionWHILE ON GROUND, MAINTENANCE FOUND CORROSION ON VERTICAL FIN SHEAR TIE FITTING, AT FIN STA 204 LT SIDE FORWARD END OF RIB NR 10 INSIDE TUNNEL, FOUND WHILE WORKING TAIL 227 CI 360676. REMOVED SHEAR TIE FITTING AT FIN STA 204 LT SIDE. REPLACED SHEAR TIE IAW WRSDR UPS204770Shear Tie · corrosionWHILE ON GROUND, MAINTENANCE FOUND CORROSION ON BOTH LT AND RT VERTICAL STABILIZER SHEAR TIES, AT FWD END OF RIB NR 9 AT FIN STA 180.6 INSIDE VERTICAL FIN TUNNEL. REMOVED AND REPLACED LT AND RT SHEAR TIES IAW 727 SRM 51-30-2.SDR UPS204769Shear Tie · corrosionWHILE ON GROUND, MAINTENANCE FOUND CORROSION ON RT VERTICAL STABILIZER SHEAR TIE FITTING, AT FIN STA 204 INSIDE VERTICAL FIN TUNNEL. REMOVED AND REPLACED FITTING ON RT VERTICAL STAB AT FIN STA 204 IAW SRM 51-30-2.SDR 95ZZZX6492Fin · crackedCRACKED VERTICAL FIN.SDR 95FDEA01525Stringer · crackedTHE NR 9 STRINGER CRACKED ON RT SIDE OF VERTICAL FIN AT FIN STA 157.2. CUT OUT CRACKED AREA OF NR 9 STR ON RT SIDE OF VERTICAL FIN AT FIN STA 157.2, FABRICATED AND INSTALLED REPAIR PARTS PER FEDEX SRM 55-30-4.SDR 95FDEA01524Stringer · crackedTHE NR 9 STRINGER CRACKED ON LT SIDE OF VERTICAL FIN AT STA 180.6. CUT OUT CRACKED AREA OF NR 9 STR ON LT SIDE VERTICAL FIN AT FIN STA 180.6, FABRICATED AND INSTALLED REPAIR FILLERS AND DOUBLERS IAW FEDEX SRM 55-30-4.SDR 95FDEA01523Stringer · crackedTHE NR 9 STR CRACKED ON RT SIDE OF VERTICAL FIN AT FIN STA 180.6. CUT OUT CRACKED AREA OF NR 9 STR ON RT SIDE OF VERTICAL FIN AT FIN STA 180.6, FABRICATED AND INSTALLED REPAIR FILLERS AND DOUBLERS IAW FEDEX SRM 55-30-4.SDR 95FDEA01522Stringer · crackedTHE NR 8 STR CRACKED ON RT SIDE OF VERTICAL FIN AT FIN STA 180.6. CUT OUT CRACKED AREA OF NR 8 STR ON RT SIDE OF VERTICAL FIN AT FIN STA 180.6, FABRICATED AND INSTALLED REPAIR PARTS PER FEDEX SRM 55-30-4.SDR DL72E954023Web · crackedAT HMV, FOUND WEB CRACKED VERT STAB INT STA 1303. FABRICATED AND INSTALLED NEW DOUBLER PER SRM 53-10-4 FIG 17.SDR DL72E954022Web · crackedAT HMV, FOUND WEB CRACKED VERT STAB INT STA 1303. FABRICATED AND INSTALLED NEW DOUBLER PER SRM 53-10-4 FIG 17.SDR DL72E954067Stringer · crackedAT HMV, FOUND STRINGER CRACKED VERTICAL STAB INTERIOR STR 8R LOC IN 5TH BAY UP FROM ACCESS HOLE. REPAIRED PER M/M 55-30-00 FIG 803.SDR DL72E953975Stringer · crackedSTRINGER CRACKED VERT STAB INTERIOR STR 8R CRACKED, LOCATED IN 3RD BAY UP FROM ACCESS HOLE. WORKED AT HMV, REPAIRED PER M/M 55-30-00.SDR HEEA955750Fin Assy · mis mfgMOUNTING INSERTS MIS-LOCATED. NUT PLATES NOT INSTALLED ON PAIRING RING. TOP TIP OF FIN NOT MODIFIED FOR ANT. NEEDS MOUNT BRKT INSTALLED.SDR MWEA95300Angle · crackedDURING C-CHECK, FOUND RIGHT SIDE VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE CRACKED BETWEEN AND EXTENDING BEYOND TWO FASTENERS NEAR AFT SPAR OF VERTICAL STABILIZER.SDR DL72S953832Web · crackedAT HMV, FOUND LOWER RT CORNER CRACKED VERT WEB INSIDE VERT STAB STA 1303. REPAIRED PER SRM 53-10-4 FIG 17.SDR DL72S953831Web · crackedAT HMV, FOUND LOWER LEFT CORNER CRACKED VERT WEB INSIDE VERT STAB AT STA 1303. REPAIRED PER SRM 53-10-4 FIG 17.SDR 95FDEA01288Web · cracked1303 WEB IN BAY NR 1 IN VERTICAL FIN IS CRACKED LT LWR CORNER. REPAIRED CRACK IN 1303 WEB IN BAY NR 1 OF VERTICAL FIN LT LOWER CORNER, PER FEDEX DRAWING SR 27-53-015.SDR 95FDEA01265Web · cracked1303 WEB IN BAY NR 1 AT VERTICAL FIN IS CRACKED LT LOWER CORNER. REPAIRED CRACK AT 1303 WEB IN BAY NR 1 OF VERTICAL FIN LT LOWER CORNER, PER FEDEX DRAWING SR 27-53-015.SDR DL72S953575Blkhd · crackedCRACK INSIDE VERTICAL STABILIZER AT STA 1303 BULKHEAD LOWER RT CORNER, VENTRAL WALL ABOVE S-DUCT HAS CRACK. CRACK WAS FOUND AT HMV, REPAIRED BY INSTALLING DOUBLER PER SRM 53-10-4 FIG 17.SDR ABXA9500870Fairing · crackedDURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 92-22-08, FOUND RIGHT UPPER HORIZONTAL TO VERTICAL STABILIZER FAIRING CRACKED AT FORWARD END. REPAIRED FAIRING IAW DC-9 SRM 55-03 FIG 17.SDR CAL950820Angle · crackedHOU - INSPECTION FOUND A 1 INCH CRACK IN VERTICAL STABILIZER LEFT ANGLE AT STATION 1388. THE AREA WAS REPAIRED BY INSTALLING A DOUBLER ANGLE CAP AND SPLICE PER SRM 55-02, FIGURE 2G. (M)SDR 95FDEA01164Stringer · crackedNR 8R STR IS CRACKED IN VERTICAL FIN BAY NR 8 FIN STA 180 WHERE STR ATTACHES TO WEB. REPAIRED NR 8R STR IN VERTICAL FIN, BAY NR 8, FIN STA 180. FEDEX SRM 55-30-4 FIG 1.SDR 95FDEA01162Stringer · crackedSTR NR 8R IS CRACKED IN VERTICAL FIN BAY NR 8 AT FIN STA 151.2. REPAIRED STR NR 8R IN VERTICAL FIN BAY NR 8 AT FIN STA 151.2 IAW FEDEX SRM 55-30-4.SDR 95ZZZX6501Fin · crackedVERTICAL FIN HAS CRACK IN LEADING EDGE AROUND KNOCKOUT PANEL.SDR UPS204127Fitting · corrodedWHILE IN FOR C-CHECK, MAINTENANCE FOUND THE TENSION TIE RIB AFT SHEAR FITTING VERTICAL BOLT HOLES HAVE CORROSION IN BORES. MAINTENANCE REMOVED THE CORROSION, REPLACED THE BUSHING DUE TO MISALIGNMENT. ALL WORK WAS PERFORMED BY BOEING PER CONTRACT 6-1171-TA-37SDR 95ZZZX5043Stabilizer · crackedCRACK FOUND DURING T-INSPECTION, 500 HOUR, AND 2 T-INSPECTIONS. AD NOT APPLICABLE. PART MODIFIED IAW AM 507-2367. REPLACED WITH FACTORY NEW ASSY.SDR USAA950935Angle · crackedPIT - DURING Q-4 CHECK INSPECTION, FOUND 1 INCH CRACK LEFT DRAG ANGLE STATION 1474 (CANTED FRAME). STOP DRILLED CRACK AND INSTALLED SKIN AND DOUBLER REPAIR PER SRM 53-05 FIG 23B CONF 7007. (M)SDR C2XA95IA148Drag Angle · crackedIAH - DURING A SCHEDULED MAINTENANCE CHECK, THE RIGHT DRAG ANGLE, ON THE VERTICAL STABILIZER, WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED DRAG ANGLE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR 95ZZZX6592Fin · damagedVERTICAL FIN DAMAGED (HOLE IN FIN).SDR USAA950851Angle · crackedPIT - DURING C-1 CHECK INSPECTION, FOUND .5 INCH CRACK IN VERTICAL STAB ATTACH ANGLE VERTICAL LEG AFT END LEFT SIDE. INSTALLED DOUBLER REPAIR 14 INCHES IN LENGTH PER SRM 53-05 FIG 23A. (M)SDR 95ZZZM319Hinge · crackedLIT - UPON REMOVAL OF RUDDER ASSY, DURING HEAVY MAIN BASE VISIT, UPPER VERTICAL STABILIZER TO RUDDER HINGE HAD FATIGUE CRACKING AROUND THE CENTER LUG OF THE HINGE. REMOVED AND REPLACED HINGE.SDR HEEA955445Fin Assy · mis mfgNUT PLATE MISALIGN WITH FAIRING 1/4" TOO FAR FORWARD. RING ASSY IS NOT LINED UP WITH L ANGLE, ABOUT 1/8" OUT TOO FAR. TIME SINCE REPAIR 0:00.SDR DL72W953264Web · crackedVERTICAL WEB INSIDE THE VERTICAL STAB CRACKED AT BASE OF RIB NR 1 AT LT AND RT LOWER CORNERS. REPAIRED PER SRM 53-10-4 FIG 17.SDR DL72W953127Stringer · crackedFOUND DURING E-2 LETTER CHECK, 1 INCH CRACK IN VERT STAB STRINGER 8 RT AT THIRD BULKHEAD ABOVE CRAWLWAY OPENING FIN STA 133.8. REPAIRED PER MM 55-30-0 PG 803.SDR 95ZZZM454Skin · crackedMCI - DURING OP-17, FOUND A ONE INCH CRACK IN SKIN ON VERTICAL STABILIZER LEFT SIDE AT BASE, FS 1330. STOP DRILLED CRACK PER SRM 51-10-1, AND REPAIRED PER ARA9370A. TOTAL CYCLES 24,723.SDR UPS203823T-Chord · crackedWHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACK ON T-CHORD FOR PANEL 9707 ON VERTICAL FIN AT FIN STA 225.6 RT SIDE. REPAIRED IAW SRM 51-30-2.SDR USAA950883Angle · crackedPIT - DURING Q-3/CX-2 INSPECTION, FOUND TWO 2 INCH CRACKS IN ATTACH ANGLES INNER VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLES LEFT AND RT AT STATION 1076. REPAIRED ATTACH ANGLES PER SRM 53-05 FIG 90 AND USAIR EO 5388X223. (M)SDR CAL950607Shear Tie · crackedGSO - INSPECTION FOUND A .75 INCH CRACK IN SHEAR TIE AT VERTICAL STABILIZER STATION 25, STRINGER 10R. THE SHEAR TIE WAS REMOVED. A NEW SHEAR TIE WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND BAC DRAWING 65-16881. (M)SDR CAL950606Shear Tie · crackedGSO - INSPECTION FOUND A .5 INCH CRACK IN SHEAR TIE AT VERTICAL STABILIZER STATION 25, STRINGER 7R. THE SHEAR TIE WAS REMOVED. A NEW SHEAR TIE WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND BAC DRAWING 65-16811. (M)SDR CAL950605Shear Tie · crackedGSO - INSPECTION FOUND A .5 INCH CRACK IN SHEAR TIE AT VERTICAL STABILIZER STATION 157, STRINGER 9R. THE SHEAR TIE WAS REMOVED. A NEW SHEAR TIE WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND BAC DRAWING 65-16812. (M)SDR 95ZZZM496Angle · crackedPIT - DURING Q-3/CX-2 INSPECTION, FOUND TWO 2 INCH CRACKS IN ATTACH ANGLES INNER VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLES LEFT AND RT AT STATION 1076. REPAIRED ATTACH ANGLES PER SRM 53-05 FIG 90 AND USAIR EO 5388X223. REF USAA950883.SDR 96ZZZM574Angle · crackedDURING D-CHECK, EMPANNAGE, LEADING PANEL NR 9707 FOR VERTICAL STABILIZER, HAS CRACKED ATTACHING ANGLE ON RIGHT SIDE OF VERTICAL STABILIZER FORWARD SPAR JUST OUTBOARD OF RIGHT VERTICAL FIN UPPER TERMINAL FITTING, AT UPPER END OF ANGLE. REMOVED T-ANGLE FOR REPASDR 96ZZZM573T-Angle · crackedDURING D-CHECK, EMPANNAGE, T-ANGLE CRACKED AT FORWARD SIDE OF VERTICAL STABILIZER FORWARD SPAR (L/E PANEL NR 9707 ATTACH ANGLE) AT LEFT SIDE UPPER END, JUST OUTBOARD OF LEFT VERTICAL FIN UPPER TERMINAL FITTING. REMOVED T-ANGLE FOR REPAIR. STOPPED DRILLED CRASDR P5CA9500654Angle · crackedCRACK ON VERTICAL STABILIZER AT STA 232.5 LEFT ANGLE ON NUTPLATE STRIP. REPAIRED PER BOEING SRM 51-40-04.SDR 96ZZZX1865Angle · corrodedDURING C-CHECK, LEFT VERTICAL STABILIZER STIFFENER ATTACH ANGLE CORRODED ABOVE UPPER RUDDER HINGE. REPAIRED IAW DC9 SRM CH 55. AIRCRAFT TT: 35,252. AIRCRAFT TC: 51,897.SDR DL72W952790Stringer · crackedAT HMV, STRINGER CRACKED INSIDE VERT STAB STR 9R CRACKED AT RIB ATTACH HOLE LOC IN FIFTH BAY UP FROM ACCESS HOLE. REPAIRED PER MM 55-30-0 PG 803.SDR DL72W952788Stringer · crackedAT HMV, STRINGER CRACKED INSIDE VERTICAL STAB STR 9R CRACKED AT RIB ATTACH HOLE LOC SECOND BAY UP FROM ACCESS HOLE. REPAIRED PER MM 55-30-0 PG 803.
Back to JASC 5530