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 UPS202813Chord · corrodedWHILE IN NAPLES FOR 'C' CHECK, MAINTENANCE FOUND CORROSION ON VERT STAB, INNER UPPER CHORD, LT SIDE, STA 1343. REPLACED PER UPS EO B727-5530-4601.Apr 4, 1995 · N921UP · Boeing 727180CSDR DL72W951393Web · crackedWEB CRACKED, TWO 1 INCH CRACKS IN STA 1303 UPPER WEB ABOVE AND TO RT SIDE OF 'S' DUCT (MARKED). FABRICATED REPAIR PLATE PER SRM 51-40-2 FIG 1.Apr 1, 1995 · N294WA · Boeing 727247SDR RMXA9520577Endplate · crackedVERT FIN ENDPLATE CRACKED AT KNOCKOUT PLUG.Mar 26, 1995 · N4493X · Bolkms BK117A3SDR 95ZZZX1964Skin · crackedSPW - DURING ROUTINE INSPECTION, MAINTENANCE FOUND DORSAL FIN CRACKED ON LT SIDE AT REAR PRESSURE BULKHEAD ATTACH POINT. THE CRACK WAS BETWEEN TWO RIVET HOLES. INSTALLED REPAIR IAW BEECH 1900 SRM 51-70-00, PAGE 17.Mar 21, 1995 · N122GL · Beech 1900CSDR DL72S951139Skin · crackFOUND DURING E-1 LETTER CHECK, SKIN CRACKED .5 INCH VERTICAL STAB LT SIDE BELOW ACCESS PNL 9501. REPAIRED PER SRM 55-30-3 FIG 1.Mar 16, 1995 · N402DA · Boeing 727232SDR UPS802653Angle · crackedWHILE IN 'C' CHECK MAINTENANCE FOUND CRACK ON RT VERT. STAB. TO FUSELAGE ATTACH ANGLE, FS 1766. INSTALLED REPAIR PER SRM 53-2-5.Mar 14, 1995 · N813UP · Doug DC873FSDR ABXA9500263Cap · corrodedDURING C-CHECK INSPECTION, A PREVIOUS REPAIR TO THE LEFT VERTICAL STABILIZER WAS FOUND WITH LEVEL I CORROSION. REMOVAL OF THE REPAIR REVEALED THE REAR SPAR CAP HAD BEEN SPLICED. REPAIRED IAW ABX REA D955-1116-MR.Mar 14, 1995 · N942AX · Doug DC931SDR 9504089945Bracket · crackedDURING LINE CHECK, FOUND CRACK IN VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE REPAIR, RIGHT SIDE ABOVE THE RUDDER LEADING EDGE. REPAIRED PER XEA X9-53-82.Mar 10, 1995 · N8925E · Doug DC931SDR 9503812705Longeron · crackedDURING PCK, MAINTENANCE FOUND VERTICAL STABILIZER, FIN STA 157.2, STR 7 LEFT CRACKED. REPAIRED PER NWA EA 27096482.Mar 10, 1995 · N802EA · Boeing 727225SDR DL72E951110Stringer · crackedDURING HMV INSPECTION PER EO 4-59253-3AD, FOUR DIFFERENT VERTICAL STABILIZER STRINGERS WERE FOUND CRACKED. THE CRACK LOCATIONS ARE STR8L AT STA 180.6, STR 9L AT STA 133.8, STR 7R AT STA 133.8, AND STR 1L AT STA 39.809. IN ACCORDANCE WITH M/M 55-30-0, PG. 803Mar 2, 1995 · N2823W · Boeing 727247SDR HEEA954465Fin Assy · mis mfgFIN TOO THICK AT MOUNTING INSERTS MAKING BOLTS TOO SHORT TO MOUNT TO TAILBOOM.Mar 1, 1995 · Bell 206L3SDR UPS202583Chord · corrodedWHILE IN NAPLES FOR 'C' CHECK, MAINTENANCE FOUND CORROSION ON CHANEL CHORD VERT FIN STA. 1342 RT. REPLACED CHANNEL CHORD PER UPS EO B727-5530-4601B.Feb 28, 1995 · N916UP · Boeing 72727CSDR UPS202582Chord · corrodedWHILE IN NAPLES FOR 'C' CHECK, MAINTENANCE FOUND CORROSION ON LWR. CHORD VERT FIN STA. 1342 LT. REPLACED CHORD PER UPS EO B727-5530-4601B.Feb 28, 1995 · N916UP · Boeing 72727CSDR UPS202581Chord · corrodedWHILE IN NAPLES FOR 'C' CHECK, MAINTENANCE FOUND CORROSION ON LWR. CHORD VERT FIN STA. 1342 RT. REPLACED CHORD PER UPS EO B727-5530-4601B.Feb 28, 1995 · N916UP · Boeing 72727CSDR UPS202248Chord · corrodedDURING C-CHECK, MAINTENANCE FOUND CORROSION ON VERTICAL FIN TORQUE BOX RT HORIZONTAL CHORD, RBL 19 FIN STA 0. INSTALLED REPAIR PER UPS ENGINEERING FILE NR 727-55-0273.Feb 25, 1995 · N937UP · Boeing 72725CSDR COM11798Angle · crackedDURING INSPECTION TASK 5530-324-03I AND 5530-324-02I, VERTICAL STABILIZER TO FUSELAGE ANGLE WAS FOUND TO BE CRACKED. REPLACED ANGLE IAW AERODESIGN REPORT 1446-1 AND EMB SRM.Feb 23, 1995 · N255CA · Emb EMB120RTSDR UPS202365Stiffener · corrosionWHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON VERTICAL FIN INTERSPAR SKIN STIFFENER RT SIDE AT VERTICAL FIN STA 233.746 INSIDE VERTICAL FIN. INSTALLED REPAIR IAW 51-30-5 AND 51-30-2.Feb 15, 1995 · N938UP · Boeing 727173CSDR HEEA954366Fin · separatedSEPARATED AT STINGER AND FIN OVERWEIGHT 17.1 LBS.Feb 14, 1995 · N2277A · Bell 206BSDR UPS202262Angle · crackedDURING 'C' CHECK, MAINTENANCE FOUND LEFT SKIN SUPPORT ANGLE CRACKED AT FS 1345, FIN STA 22.5. FABRICATED AND INSTALLED REPAIR PER SRM 51-40-3, 51-30-2.Feb 13, 1995 · N937UP · Boeing 72725CSDR UPS202261Angle · crackedDURING 'C' CHECK, MAINTENANCE FOUND RT SKIN SUPPORT ANGLE CRACKED AT FS 1345, FIN STA 22.5. FABRICATED AND INSTALLED REPAIR PER SRM 51-30-2, 51-40-3.Feb 13, 1995 · N937UP · Boeing 72725CSDR UPS202260Chord · corrodedDURING 'C' CHECK, MAINTENANCE FOUND RT INNER CHORD FIN CRACKED AND CORRODED AT FIN STA 22.5. FABRICATED AND INSTALLED REPAIR PER BOEING DRAWING 65C20296 AND 65C20381.Feb 13, 1995 · N937UP · Boeing 72725CSDR DL72S950571Skin · crackedDURING LETTER CHECK, FOUND 2 CRACKS IN PANEL FWD OF SADDLE PLATE LEFT SIDE VERTICAL STABILIZER. REPAIRED PER MM 54-30-0 PG 801-802.Feb 9, 1995 · N409DA · Boeing 727232SDR C2XA95IA023Angle · crackedIAH - DURING C-CHECK INSPECTION, FOUND RT FIN TO FUSELAGE ATTACH (DRAG) ANGLE CRACKED. MAINTENANCE REMOVED AND REPLACED RT ATTACH ANGLE, AIRCRAFT APPROVED FOR RETURN TO SERVICE. A/C TT - 8,443.7. CYCLES - 12,794. (X)Feb 7, 1995 · N57734 · Emb EMB120RTSDR DL72W950759Stringer · crackedDURING INSPECTION AT OVERHAUL, STRINGER 7R OF THE VERTICAL STABILIZER WAS FOUND CRACKED AT THE FIN STA 110.4 RIB ATTACHMENT TAB. IN ACCORDANCE WITH B727 S/B 55-0075, A REPAIR ANGLE WAS INSTALLED.Feb 2, 1995 · N293WA · Boeing 727247SDR DL72W950464Stringer · crackedDURING HMV, STR 9 LEFT INSIDE VERT STAB AT FIN STA 110 CRACKED. REPAIRED PER MM 55-30-0 PG 803 FIG 803.Feb 1, 1995 · N293WA · Boeing 727247SDR DL72S950599Stringer · crackedAT HMV, FOUND STRINGER 9 LT CRACKED AT 3RD BULHEAD UP FROM ACCESS PANEL INSIDE VERTICAL STABILIZER. REPAIRED PER SRM 55.Feb 1, 1995 · N492DA · Boeing 727232SDR DL72S950598Stringer · crackedAT HMV, FOUND STRINGER 4 LT. CRACKED AT 5TH BULKHEAD FROM ACCESS PANEL IN VERTICAL STABILIZER. REPAIRED PER SRM 55.Feb 1, 1995 · N492DA · Boeing 727232SDR DL72S950594Stringer · crackedSTRINGER CRACKED AT FS 133.800, STR 9L CRACKED AT RIB. FOUND DURING INSPECTION AT HMV2 IN ATL. REPAIRED PER MM 55-30-0 PG 803.Feb 1, 1995 · N492DA · Boeing 727232SDR DL72W950487Stringer · crackedFOUND DURING HMV, NR 5 STR CRACKED INSIDE VERT STAB AT STA 110.4. REPAIRED PER ERA 301113-14.Jan 30, 1995 · N293WA · Boeing 727247SDR DL72W950486Attach Angles · crackedFOUND DURING HMV, ATTACH ANGLE CRACKED AT NR 5 STR ABOVE NR 2 'S' DUCT INSIDE VERT STAB. REPAIRED PER SRM55-30-5 PG.1, FIG 1.Jan 30, 1995 · N293WA · Boeing 727247SDR DL72W950415Web · crackedSTA 1303 INSIDE VERT STAB WEB CRACKED AT BOTH O/B ENDS AT FLOORLINE. FABRICATED RT AND LT DOUBLERS 2024T3 .040 AS PER SRM 53-10-4 PG 45. DAMAGE FOUND AT HMV.Jan 23, 1995 · N293WA · Boeing 727247SDR 95ZZZX860Attach Angle · crackedSTL - DURING CHECK C, FOUND A .25 INCH CRACK IN VERTICAL STABILIZER RIGHT DORSAL FIN ATTACH ANGLE, FROM FASTENER HOLE TO EDGE. REPAIRED PER SRM 51-30 AND TWA STANDARD PRACTICES. AIRCRAFT TOTAL TIME: 38,864 HOURS; 35,359 CYCLES.Jan 20, 1995 · N409EA · Doug DC951SDR DL72W950155Web · crackedDURING HMV, FOUND IN THE VERTICAL STABILIZER INTERIOR AT STA 1303 WEB CRACKED ON RT SIDE ABOVE 'S' DUCT, REPAIRED PER SRM 53-10-4 FIGURE 12.Jan 6, 1995 · N291WA · Boeing 727247SDR DL72W950154Web · crackedDURING HMV, FOUND IN THE VERTICAL STABILIZER INTERIOR AT STA 1303 WEB CRACKED ON LEFT SIDE ABOVE 'S' DUCT, REPAIRED PER SRM 53-10-4 FIGURE 12.Jan 6, 1995 · N291WA · Boeing 727247
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