JASC 5342

Service difficulty reports · 578

Reports filed under 5342 · Fuselage, Stabilizer Attach Fittings, 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 = '5342'
  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 99ZZZX19Seat Track · corrodedDURING A C-CHECK, CORROSION WAS NOTED AT FS 344 - FS 380 LBL 45, SEAT TRACK.Nov 19, 1998 · N203AV · Boeing 727259SDR DLM90980869Angle · crackedFUSELAGE/ATTACH FITTING, VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE: REPAIR FOR CRACK. THE VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE ON THE LT SIDE OF THE AIRCRAFT WAS FOUND WITH A .90 CRACK AT FS 937. THE CRACKED FLANGE WAS TRIMMED OUT AND A .080 THICKApr 18, 1998 · N907DA · Doug MD9030SDR AU980146Fitting · corroded(AUS) STABILISER ATTACHMENT FITTING LOCATED IN REAR FUSELAGE CORRODED AND RIVETS MISSING.Jan 30, 1998 · Cessna 182HSDR 98ZZZX1076Fitting · crackedAIRFRAME WAS BEING STRIPPED OF FABRIC. HORIZONTAL STABILIZER AREA WOULD NORMALLY NOT BE VISIBLE AS THIS FABRIC IS GLUED AROUND THE TUBING IN THIS AREA. THIS ITEM IS COVERED UNDER SB 300-2-95.Jan 19, 1998 · N317N · Rhnflu EXTRA300SDR 9708039163Fitting · crackedDURING L-CHECK, FOUND CRACK ON VERTICAL STABILIZER ATTACH FITTING FS 908. REPAIRED PER EA 91-112873.Apr 17, 1997 · N8906E · Doug DC914SDR AU970407Fitting · corroded(AUS) FORWARD FIN ATTACHMENT PLATE BRACKETS CORRODED - TWO OF THE FIVE PLATE ATTACHMENT RIVETS WERE ALSO CORRODED AWAYApr 7, 1997 · Piper PA28140SDR AU970402Bracket · corroded(AUS) STABILISER FITTING BRACKET CORRODED BETWEEN BRACKET AND SKINApr 7, 1997 · Piper PA28140SDR 9704209958Fitting · crackedDURING H-CHECK, FOUND CRACK IN VERTICAL STABILIZER ATTACH FITTING AT FS 1095, RBL 6. REPLACED FITTING (P/N 4918093-2) PER EA 99-111864.Feb 21, 1997 · N917RW · Doug DC931SDR AU961085Bracket · broken(AUS) FORWARD FIN ATTACHMENT BRACKET BROKEN IN AREA DESCRIBED IN AIRTRACTOR SB 138 - AIRCRAFT IS FITTED WITH A 6.35MM (0.25IN)PLATEAug 7, 1996 · Airtrc AT502SDR CKSA96068Angle · corrodedDURING B-CHECK INSPECTION, FOUND CARD NR 6820-0551 AREA RUDDER AND TAB EXTERIOR, VERTICAL STAB TO FUSELAGE ATTACH ANGLE CORRODED AT FS 1766. REPAIRED IAW DOUGLAS SRM 53-2-5. TASK NR 79743.Jul 5, 1996 · N781AL · Doug DC863SDR 9608839751Angle · crackedDURING H-CHECK, FOUND A TWO INCH CRACK IN THE RIGHT SIDE DORSAL FIN ATTACH ANGLE FS 1171. REPAIRED ANGLE (P/N 5912141-60) PER EA 97-109496.Apr 17, 1996 · N751NW · Doug DC941SDR AU960267Adapter · corroded(AUS) VERTICAL FIN REAR ATTACHMENT ADAPTER CONTAINS SEVERE EXFOLIATION CORROSION IN AREA ADJACENT TO LH AND RH ATTACHMENT BOLTSMar 14, 1996 · Doug DC3CS1C3GSDR 96DHL7219A1Forging · crackedAFT AIRSTAIRS VERTICAL FIN FRONT SPAR FORGING APPROX FS 1195 HAS CRACK INDICATIONS IN RADIUS OF LOWER FLANGE EXTENDING APPROX 3 INCHES TO THE RIGHT OF SPLICE PLATE AT 6 O'CLOCK. STOP DRILLED CRACK. HFEC INSPECTION CONFIRMED CRACK ENDS AT STOP HOLE. FABRICATMar 12, 1996 · N721DH · Boeing 727228SDR UPS96805653Fitting · crackedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED VERTICAL ATTACH FITTING IS CRACKED AT FS 759 RBL 48. REPLACED FITTING PER SRM 51-1-21.Feb 17, 1996 · N811UP · Doug DC873FSDR UPS96805656Attach Angle · crackedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED VERTICAL STAB TO FUSELAGE ATTACH ANGLE HAS A 1 INCH CRACK ON AFT END. REPAIRED PER UPS EO.Feb 8, 1996 · N811UP · Doug DC873FSDR 96ZZZX884Attach Pan · crackedROUTINE INSPECTION FOUND HORIZONTAL AFT ATTACH BRACE (FORWARD OF BULKHEAD) WITH 2 CRACKS IN CORNERS.Jan 25, 1996 · N4515Q · Cessna 340CESSNASDR AU960042Fitting · corroded(AUS) UPPER STABILATOR ATTACHMENT FITTINGS CORRODED - AIRCRAFT HAD BEEN SITTING DORMANT FOR APPROXIMATELY 12 MONTHS - CORROSION FORMED BETWEEN ALUMINIUM SKIN AND STEEL FITTINGSJan 9, 1996 · Piper PA32300SDR UPS805086Angle · crackedWHILE IN FOR C-CHECK, MAINTENANCE FOUND LT VERTICAL STAB TO FUSELAGE ATTACH ANGLE CRACKED AT REAR SPAR, LOWER FWD SCREW HOLE. REPAIRED PER UPS EO DC8-5310-7584-A.Nov 16, 1995 · N779UP · Doug DC871FSDR 9511982287Chord · crackedDURING PERIODIC CHECK, FOUND CRACKS IN BOTH THE LEFT AND RIGHT VERTICAL STABILIZER TO BODY CHORD FOR THE NR 2 ENGINE BS 1343 AND 1360 RESPECTIVELY. REPAIRED CHORD (P/N 65-17555-1577), PER EA 22-98944.Jul 26, 1995 · N287US · Boeing 727251SDR 9507549990Angle · crackedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND 3 CRACKS IN THE RIGHT SIDE VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE AT THE AFT END. REPAIRED PER XEA X9-53-83.May 5, 1995 · N8950E · Doug DC931SDR 9507829924Angle · crackedDURING PERIODIC CHECK, FOUND CRACK IN THE LEFT SIDE VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE FS 1095. REPAIRED PER EA 99-097075. MFG PART NUMBER: 5912141-59.Apr 29, 1995 · N926RC · Doug DC932SDR UPS802820Angle · crackedWHILE IN 'C' CHECK, MAINTENANCE FOUND A CRACK ON RT VERT STAB TO FUSELAGE ATTACH ANGLE. INSTALLED REPAIR PER SRM 53-2-5.Apr 5, 1995 · N814UP · Doug DC873FSDR 9505389161Fitting · crackedDURING PERIODIC CHECK, FOUND CRACK IN VERTICAL STABILIZER SPAR ATTACH FITTING, LOWER RIGHT SIDE. REPLACED FITTING PER SRM 51-30-2 AND 55-30-0 FIG 2.Apr 4, 1995 · N8905E · Doug DC914SDR USAA950254Angle · crackedIND - DURING SCHEDULED CX-2 INSPECTION, FOUND A 1 INCH CRACK EXTENDING FROM VERTICAL LEG INTO HORIZONTAL LEG OF STABILIZER TO FUSELAGE ATTACH ANGLE. CUT OUT DAMAGED SECTION AND INSTALLED FILLER AND REPAIR DOUBLER PER SRM 53-05 FIG NR 23A. (W)Mar 17, 1995 · N802US · Doug DC981SDR 9504519996Angle · crackedDURING PERIODIC CHECK, FOUND CRACK IN VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE FS 1096 RIGHT SIDE. REPAIRED PER EA 99-097062, FIG.1.Mar 16, 1995 · N8932E · Doug DC931SDR 95ZZZM345Le Skin · crackedUPON A SCHEDULED INSPECTION AT AERO CORP INLAKE CITY, FLORIDA, THE VERTICAL STABILIZER L/E WAS FOUND WITH 5 CRACKED STIFFENERS. FABRICATED AND INSTALLED NEW STIFFENERS IAW DC9 SRM 55-02 AND MM 51-00. N/R NR027N1/0598.Jan 22, 1995 · N937VV · Doug DC932SDR ABXA9500089Angle · failedDURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 89-08-10 AND S.B.'S A53-154 AND A53-223, FOUND RIGHT DORSAL FIN ATTACH ANGLE BUCKLED AND FASTENERS PULLED. REPLACED RIGHT DORSAL FIN ATTACH ANGLE IAW DC-9 SRM 53-05, FIGURE 23 AND SB'S A53-154 AND A53-223.Jan 10, 1995 · N904AX · Doug DC931SDR ABXA9500088Angle · defectiveDURING C-CHECK INSPECTION WHILE COMPYING WITH AD 89-08-10 AND S.B.'S A53-154 AND A53-223, FOUND LEFT DORSAL FIN ATTACH ANGLE HAD ONE FASTENER HEAD MISSING AND SEVERAL FASTENERS NOT PORPERLY SEATED. REPLACED FASTENERS IAW DC-9 SRM 51-30-1 AND 51-30-5.Jan 6, 1995 · N904AX · Doug DC931
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