JASC 5533

Service difficulty reports · 77

Reports filed under 5533 · Ventral Structure, 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 = '5533'
  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 05FDEA02982Web · crackedVERTICAL STABILIZER 1303 WEB IS CRACKED AT LOWER LT CORNER. REPAIRED VERT STAB 1303 WEB IAW SRM 51-40-2.Sep 18, 2005 · N483FE · Boeing 727227SDR 05FDEA02203Structure · unknownVERTICAL STABILIZER RT SIDE OLD REPAIR AT XAR=417.800. REPAIR IAW SRM 55-00-01 FIG 3 VOL 1.Aug 2, 2005 · N381FE · Doug MD1010FSDR DHL2005740506Stringer · crackedVERT STAB FIN STA 180 STR IS CRACKED AT FRAME ATTACH BOLT. REMOVED FASTENERS FOR ACCESS AT VERT STAB FIN STA 180 S-8 RT AND TRIMMED OUT DAMAGED AREA SIZE 4 1/2 INCH BY 3 INCH IAW B727 SRM 55-30-4 FIG 1 AND 51-30-2. FABRICATED REPAIR FILLER P/N BAC 1517-1367 Mar 29, 2005 · N740DH · Boeing 7272Q9SDR C2XA05TY002Hinge · wornDURING A 4C INSPECTION THE RT AND LT VERTICAL STABLIZER SPHERICAL BEARING HOUSINGS WERE FOUND WORN. MAINTENANCE REAM AND INSTALL NEW BUSHINGS IAW EC5510-01107.Jan 4, 2005 · N14953 · Emb EMB145LRSDR 04FDEA02966Structure · corrodedEMPENNAGE, UPPER VERTICAL STAB AT AFT CTR SPAR APPROX ZFR 564 RT EXTRUSION. EXTERIOR SURFACE FOUND CORRODED. CORROSION REPAIRED AS PER FEDEX EA 1-5530-81578.Oct 22, 2004 · N602FE · Doug MD11FSDR 2003FA0001247Angle · damagedTWO ANGLES THAT ARE THE FORWARD MOUNTING STRUCTURE OF THE VERTICAL STABILIZER TO THE HORIZONTAL STABILIZER HAVE 2 HOLES EACH WITH BOLTS THAT ATTACH THE HORIZONTAL STAB., AND 5 HOLES EACH WITH 4 LOCKBOLTS INSTALLED THAT ATTACH TO THE VERTICAL STAB. THE TOP HOLEDec 16, 2003 · N6WU · Beech B200SDR 03FDEA02167Stringer · crackedVERTICAL FIN STR 8L AT FIN STA 157 IS CRACKED. REPAIRED CRACK IN STRINGE 8 LT AT FIN STA 157 PER SRM 55-30-4 FIG 1.Dec 11, 2003 · N287FE · Boeing 727200SDR SROM200300043Beam · dentedDURING D CHECK INSPECTION FOUND DENT IN RT TRAILING EDGE BEAM OF VERTICAL STABILIZER AT APPROX STA 17.25. REFORMED RT TRAILING EDGE BEAM IAW EA 5530-01100 AND EA 10007.Jul 22, 2003 · N736BP · Boeing 737205SDR 2003F00470Bearing · crackedAT C-CHECK, FOUND RIGHT FIN UPPER STABILIZER HINGE FITTING BEARING CRACKED AND BOTH RETAINERS CORRODED AT BS 1586. REMOVED AND REPLACED RIGHT STABILIZER HINGE BEARING ASSEMBLY. (M)May 20, 2003 · N7639U · Boeing 727222SDR MWEA020580Stabilizer · crackedVERTICAL STABILIZER DORSAL FIN LOWER LEFT INBOARD ATTACH ANGLE CRACKED AT FRAME STATION 1441 DOT 79. -- REMOVED ATTACH ANGLE, LOCATED AND DRILLED AND INSTALLED NEW ANGLE.Sep 24, 2002 · N813ME · Doug DC981SDR COOSDR010144Panel · delaminatedRIGHT VERTICAL STABILIZER ACCESS PANEL INNER AND OUTER SKIN DELAMINATED.Mar 1, 2002 · N79751 · Boeing 7272M7SDR P2EA2002V0022Fitting-During Q1+Q2 inspection.-VERTICAL STABILIZER SUPPORT FITTING WITH CRACK AT REAR SPAR CAVITY FIN STA 90.3.-Rudder support fitting repaired IAW E.O. No. B737HC55-007/02, DATED Feb 15, 2002 approved with FAA 8110-3 form, submited by Robert Manashi, (DERT-710167-Feb 20, 2002 · N239TA · Boeing 73725ASDR LR7A00183Longeron · crackedDURING SCHEDULED B-CHECK, THE DORSAL FIN ATTACH ANGLE WAS DISCOVERED CRACKED IN THE RADIUS AT FS 902 LBL 13 WL 285. REPAIRED PER MEA 382-53-00-115 AND LYNDEN DRAWING R00-0024-1.Sep 30, 2000 · N404LC · Lkheed 382GSDR AALA20001149Angle · crackedTUL - CANT. STA 1463, LEFT SIDE OF VERTICAL STABILIZER TO FUSELAGE ATTACH POINT ANGLE, ANGLE HAD CRACK, .3750 INCH IN LENGTH, EMITTING FROM RIVET HOLE. INSTALLED REPAIR DOUBLER PER AARD 53-10-00-2. (X)Jun 26, 2000 · N489AA · Doug DC982SDR TWAA0009611Attach Angle · crackedDURING CHECK-C MAINT, THE ATTACH ANGLE ON BOTTOM OF DORSAL FIN CRACKED THROUGH THE SCREW HOLE, LT SIDE APROX STA 1420. INSTALLED REPAIR ANGLE PER SRM 53-01 PAGE 0 WITH FASTENERS PER SRM 51-10-3.Jun 12, 2000 · N9305N · Doug DC983SDR DHL200071752DRib · crackedAT D-CK, PERFORMED HFEC INSPECTION ON FIN TENSION TIE RIB PER J/C 81303.5 CONFIRMED CRACK INDICATION ON LT AND RT AFT LUGS AD 84-21-05. REMOVED AND REPLACED TENSION TIE RIB PER B727 MM 55-30-51. REF: N/R 4662.Jan 17, 2000 · N717DH · Boeing 72723SDR 99ZZZX1826Delta Fin · crackedTOP SKIN OF RIGHT DELTA FIN CRACKED UNDER THE OUTBOARD STATIC WICK. CRACK EXTENDED ALONG SIDE OF STATIC WICK BASE. WAS NOTICED BY BLACK STREAKING ALONG ONE SIDE.Mar 1, 1999 · N119FX · Lear 31ASDR 99ZZZX1378Rib · crackedTHE RUDDER HINGE BRACKETS ON THE RUDDER BECAME LOOSE WHICH APPARENTLY CAUSED A CRACK TO DEVELOP IN THE AFT/LEFT CORNER OF THE END (TOP) RIB OF THE VERTICAL STABILIZER. ALSO, WAS LOSING SOME OF THE RIVETS IN THE VERTICAL STABILIZER SPAR AT THE TOP HINGE ATTACHFeb 19, 1999 · N99CA · Beech B99SDR P5CA9800434Bracket · corrodedLEVEL 1 CORROSION ON TWO L SHAPED BRACKETS ON THE HORIZONAL STABILIZER VENTRAL FIN TRAILING EDGE. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01 AND 51-10-02.Feb 15, 1998 · N3203Y · Boeing 747128SDR 97ZZZX4647Skin · corrodedPRE-UNIT, S/N 0274, AIRCRAFT UTILIZE - .020 INCH SKIN FILLED WITH FOAM FOR RIGIDITY IN THE CONSTRUCTION OF THE VENTRAL FIN. THE FOAM ALLOWS MOISTURE TO COLLECT AND CORROSION TO DEVELOP ON THE INSIDE SURFACES OF THE SKINS. POST-UNIT, S/N 0274, DELETES THE FOAOct 17, 1997 · N12AM · Cessna 500CESSNASDR QXEA9600334Web · crackedTWO INCH CRACK NOTED IN THE INNER WEB FLANGE, FORWARD SECTION OF THE RIGHT HAND SIDE OF THE BULLET FAIRING. CRACK NOTED DURING C-CHECK (NR400-99), CRACK REPAIRED IAW EA 4-55-13.Aug 19, 1996 · N491US · Fokker F28MK4000SDR S2YA960002Ventral Fin · damagedMAINTENANCE FOUND THE AFT BOTTOM SIDES OF BOTH VENTRAL FINS DAMAGED FROM OVERROTATION RUNWAY CONTACT DURING AN INSPECTION. DO NOT KNOW AT WHAT POINT THIS TOOK PLACE, TAKEOFF OR LANDING. RECEIVED BEECH ENGINEERING APPROVAL FOR THE REPAIR, COMPLETED IT, AND FIJan 18, 1996 · N901SK · Beech 1900DSDR AU960051Fitting · corroded(AUS) VERTICAL STABILISER LH AND RH FITTINGS CORRODED - THE STABILIZER BRACKETS HAD NEVER BEEN PAINTSTRIPPED - FOUND DURING INSPECTIONIAW AD/150/31 AMDT3 (REQUIREMENTS 2A AND 2B) - PERSONNEL/MAINTENANCE ERRORJan 18, 1996 · Cessna A152SDR UPS204609Fitting · corrosionWHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION LT LOWER SPLICE BEAM UPPER AND LOWER SHEAR FITTINGS. REPLACED PER SRM 51-30-2, MM 51-20-21, 51-20-00, 51-20-21.Sep 29, 1995 · N936UP · Boeing 727108CSDR 9514849104Angle · crackedDURING B-CHECK, FOUND A CRACK IN THE DORSAL FIN ATTACH ANGLE AT LONGERON 2L. REPAIRED ANGLE (P/N 5939711-1), PER EA 91-99249.Sep 12, 1995 · N94S · Doug DC915SDR DL72W953410Ventral Web · crackedFOUND DURING E-1 LETTER CHECK - LIGHTNING HOLE HAS CRACK LT VENTRAL WEB STA 1245 - LT VENTRAL WEB HAS CRACK AT TOP OF WEB AT STA 1225. REPAIRED PER MMM 53-11-0 PG 828 - 832.Aug 16, 1995 · N2816W · Boeing 727247SDR S2YA950001Angle · crackedDURING AN INSPECTION, MAINTENANCE FOUND A 1.50 INCH CRACK ON THE ATTACH ANGLES OF BOTH THE LT AND RT VENTRAL FINS. THE LOCATION IS BELOW THE AFT PRESSURE BULKHEAD, FS 557.50 AND IS CAUSED BY THE LACK OF SHIMMING AT THE SKIN OVERLAP. THE CRACKS WERE REPAIRED.Apr 28, 1995 · N891SK · Beech 1900D
Back to JASC 5533