JASC 5553

Service difficulty reports · 586

Reports filed under 5553 · Vertical 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 = '5553'
  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 C2XA05TY052Fitting · corrodedDURING A SCHEDULED 2C INSPECTION, THE VERTICAL STABILIZER RT FITTING WAS FOUND TO HAVE CORROSION INSIDE THE SPHERICAL BEARING HOUSING. THE CORROSION WAS REMOVED AND THE BEARING HOUSING WAS REAMED AND BUSHED AS PER EXPRESSJET EC5510-01124.Aug 26, 2005 · N13995 · Emb EMB145LRSDR 05FDEA02571Attach Angle · damagedVERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE RT SIDE FOUND 1EA EXTERNAL DOUBLER REPAIR. REPAIRD IAW SRM 55-20-00 FIGURE 3 VOL.1.Aug 19, 2005 · N556FE · Doug DC1010SDR SWAA052481Fitting · corrodedDURING SCHEDULED D-CHECK, FOUND LT & RT VERTICAL STAB FWD & AFT FAILSAFE CLEVIS LUG FACES CORRODED. REPAIRED LUG FACES PER BFG ER.Aug 18, 2005 · N612SW · Boeing 7373H4SDR SWAA052292Attach Fitting · corrodedDURING SCHEDULED D-CHECK, FOUND LEFT & RIGHT VERTICAL STAB PRIMARY & FAIL-SAFE ATTACH FITTINGS FWD & AFT CLEVIS LUG FACES CORRODED. REPAIRED LUG FACES PER BFG ER.Aug 2, 2005 · N610WN · Boeing 7373H4SDR 2005UALA00755Attach Fitting · corrodedVERTICAL STABILIZER LT AND RT AFT PRIMARY ATTACH LUG FITTINGS ON FUSELAGE HAD CORROSION REMOVAL BEYOND LIMITS. REPLACED LT AND RT AFT PRIMARY ATTACH LUGS AND INSTALLED NEW BUSHINGS PER BACO DRAWING 65-52274.Aug 1, 2005 · N912UA · Boeing 737522SDR SWAA052124Fitting · corrodedDURING SCHEDULED D CHECK FOUND, LT AND RT VERTICAL STAB ATTACH FITTING LUG FACES CORRODED. REPAIRED LUGS PER SRM.Jul 20, 2005 · N609SW · Boeing 7373H4SDR SWAA052073Fitting · corrodedDURING SCHEDULED D-CHECK, FOUND LT & RT VERTICAL STAB ATTACH FITTING FWD & AFT PRIMARY CLEVIS LUG FACES CORRODED. REPAIRED LUG FACES PER BFG ER.Jul 15, 2005 · N613SW · Boeing 7373H4SDR SWAA052015Fitting · corrodedDURING SCHEDULED D-CHECK, FOUND LT & RT VERTICAL STAB FWD & AFT FAILSAFE CLEVIS LUG FACES CORRODED. REPAIRED LUG FACES PER BFG ER.Jul 11, 2005 · N312SW · Boeing 7373H4SDR ABXA050166Angle · crackedLEFT DORSAL FIN ATTACH ANGLE CRACKED DURING ROUTINE LINE MAINTENANCE. REPAIRED IAW EA53420010-103 FOR ANGLE REPLACEMENT.Jul 8, 2005 · N943AX · Doug DC931SDR SWAA052004Fitting · corrodedDURING SCHEDULED D-CHECK, FOUND LT & RT VERTICAL STAB ATTACH FITTING FWD & AFT PRIMARY CLEVIS LUG FACES CORRODED. REPAIRED LUG FACES PER BFG ER.Jul 8, 2005 · N608SW · Boeing 7373H4SDR SWAA051967Fitting · corrodedDURING SCHEDULED D-CHECK, FOUND LT & RT VERTICAL STAB ATTACH FITTING FWD & AFT PRIMARY CLEVIS LUG FACES CORRODED. REPAIRED LUG FACES PER BFG ER.Jul 7, 2005 · N312SW · Boeing 7373H4SDR 2005FA0000998Fitting · crackedWHILE PERFORMING UNSCHEDULED MAINTENANCE, VERTICAL STABILIZER WAS REMOVED, WHILE THE MECHANIC WAS INSPECTING THE FITTINGS FOR REINSTALLATION OF THE VERTICAL STABILIZER NOTICED A CRACK COMING FROM BOTTOM RT LOWER MOUNTING HOLE ON FORWARD FITTING. AT THIS TIME Jun 23, 2005 · N5544A · Beech F33ASDR SWAA051827Fitting · corrodedDURING SCHEDULED D-CHECK, FOUND LT & RT VERTICAL STAB FWD & AFT FAILSAFE CLEVIS LUG FACES CORRODED. REPAIRED LUG FACES PER BFG ER.Jun 21, 2005 · N314SW · Boeing 7373H4SDR SWAA051785Fitting · corrodedDURING SCHEDULED D-CHECK, FOUND LT & RT VERTICAL STAB ATTACH FITTING FWD & AFT PRIMARY CLEVIS LUG FACES CORRODED. REPAIRED LUG FACES PER SRM & BFG ER.Jun 19, 2005 · N314SW · Boeing 7373H4SDR SWAA051592Lug · corrodedDURING SCHEDULED D-CHECK, FOUND LT & RT VERTICAL STAB FWD & AFT FAILSAFE CLEVIS LUG FACES CORRODED. REPAIRED LUG FACES PER BFG ER.May 30, 2005 · N660SW · Boeing 737301SDR SWAA051591Lug · corrodedDURING SCHEDULED D-CHECK, FOUND LT & RT VERTICAL STAB FITTING FWD & AFT PRIMARY CLEVIS LUG FACES CORRODED. REPAIRED LUG FACES PER BFG ER.May 30, 2005 · N660SW · Boeing 737301SDR SWAA051432Fitting · corrodedDURING SCHEDULED D-CHECK, FOUND LT & RT VERTICAL STAB FAILSAFE FITTING FWD & AFT PRIMARY CLEVIS LUG FACES CORRODED. REPAIRED LUG FACES PER BFG ER.May 17, 2005 · N311SW · Boeing 7373H4SDR SWAA051431Fitting · corrodedDURING SCHEDULED D-CHECK, FOUND LT & RT VERTICAL STAB ATTACH FITTING FWD & AFT PRIMARY CLEVIS LUG FACES CORRODED. REPAIRED LUG FACES PER BFG ER.May 17, 2005 · N311SW · Boeing 7373H4SDR SWAA051312Fitting · corrodedDURING SCHEDULED D-CHECK, FOUND LT & RT VERTICAL STAB FITTING FWD & AFT PRIMARY CLEVIS LUG FACES CORRODED. REPAIRED LUG FACES PER BFG ER.May 3, 2005 · N611SW · Boeing 7373H4SDR 05FDEA01178Attach Fitting · crackedEMPENNAGE - LT FAIRING PANEL ATTACHMENT IN BETWEEN VERTICAL STABILIZER LOWER UPPER SECTION AND LOWER CENTER SECTION AT APPROX PIN 122 ADJACENT TO ACCESS PANEL 363PL FOUND CRACKED AT AFT EDGE AREA. REPAIR AS PER EA 1-5530-80384 AND SRM 51-33-01 AND 51-35-01 VApr 29, 2005 · N576FE · Doug MD11SDR 05FDEA01023Fitting · corrodedVERTICAL STAB TENSION TIE LT AFT FITTING CORRODED. REPAIRED IAW EA 7-5530-86279.Apr 15, 2005 · N481FE · Boeing 727200SDR 05FDEA01022Fitting · corrodedVERTICAL STAB TENSION TIE RT AFT FITTING CORRODED. REPAIRED IAW EA 7-5530-86279.Apr 15, 2005 · N481FE · Boeing 727200SDR 05FDEA01020Attach Fitting · corrodedCORROSION VERTICAL STAB TENSION TIE LT FWD FITTING IS CORRODED. REPAIRED PER EA 7-5530-86277.Apr 15, 2005 · N481FE · Boeing 727227SDR 05FDEA01019Attach Fitting · corrodedCORROSION VERTICAL STAB TENSION TIE RT FWD FITTING IS CORRODED. REPAIRED PER EA 7-5530-86277.Apr 15, 2005 · N481FE · Boeing 727200SDR 2005FA0000642Pan · crackedDURING ANNUAL INSPECTION, TECH WAS INSPECTING TAIL SECTION. PAN IS ATTACHED TO A BULKHEAD WHICH ARE THE PRIMARY STRUCTURE (AFT) FOR THE HORIZONTAL AND VERTICAL STABILIZERS. TAIL FLEX IS TRANSFERRING TO THIS ASSY AND IS CAUSING CRACKS ON THE RADIUS. (K)Apr 12, 2005 · N234PS · Cessna 340ASDR 2005FA0000641Pan · crackedDURING ANNUAL INSPECTION TECHNICIAN WAS INSPECTING TAIL SECTION. THE PAN (AFT) IS ATTACHED TO BULKHEAD WHICH ARE PRIMARY STRUCTURE (AFT) FOR HORIZONTAL AND VERTICAL STABILIZER. TAIL FLEX IS TRANSFERRING TO THIS ASSY AND IS CAUSING CRACKS IN THE RADIUS. (K)Apr 12, 2005 · N98560 · Cessna 340ASDR SWAA050908Drag Angle · corrodedDURING SCHEDULED D-CHECK, FOUND VERTICAL STAB LT & RT DRAG ANGLES CORRODED. REMOVED AND REPLACED ANGLES PER SRM.Mar 24, 2005 · N605SW · Boeing 7373H4SDR SWAA050907Fitting · corrodedDURING SCHEDULED D-CHECK, FOUND VERTICAL STAB FITTING LT & RT PRIMARY CLEVIS LUG FACES CORRODED. REPAIRED LUG FACES PER SRM.Mar 24, 2005 · N605SW · Boeing 7373H4SDR C2XA05TY030Fitting · looseDURING A SCHEDULED C-CHECK INSPECTION, THE NR 1 RUDDER TO VERTICAL STABILIZER LOWER HINGE FITTING ATTACH POINT BUSHING WAS FOUND TO BE MIGRATED AND LOOSE. THE DEFECTIVE BUSHING WAS REMOVED; THE FITTING HOLE WAS DIMENSIONALLY CHECKED AND FOUND TO BE WORN. MAIMar 23, 2005 · N15941 · Emb EMB145ERSDR SWAA050808Clevis · corrodedDURING SCHEDULED D-CHECK, FOUND LT & RT VERTICAL STAB FITTING FWD & AFT PRIMARY CLEVIS LUG FACES CORRODED. REPAIRED LUG FACES PER SRM.Mar 15, 2005 · N663SW · Boeing 7373Q8SDR 05FDEA00441Attach Fitting · corrodedVERTICAL STAB UPPER EDGE LEFT AND RIGHT FORE TO AFT HAS CORROSION AROUND CAP ATTACH FASTENER HOLES REF N00734. REMOVED AND REPLACED RT CHORD IAW SRM 51-40-21 AND DRW A55371360 AND REPAIRED LT CHORD IAW SRM 51-74-40 FIG 201Mar 8, 2005 · N446FE · Airbus A310SDR LR7A05010Fitting · gougedDURING SCHEDULED C5 INSPECTION PER JOB CARD HC5511 FOUND VERTICAL STAB ATTACH TO HORIZONTAL STAB FITTING MAIN BOLT HOLE WITH THREAD TYPE GOUGES AT FS 1043, WL 287, LBL 15. REPLACED FITTING IAW SRM SMP583 CHP 51-60 & 51-70.Mar 6, 2005 · N404LC · Lkheed 382GSDR SWAA050265Attach Fitting · corrodedDURING SCHEDULED D-CHECK, FOUND VERTICAL STABILIZER PRIMARY CLEVIS FWD AND AFT LUGS CORRODED. REPAIRED VERTICAL STABILIZER PER ER.Feb 1, 2005 · N602SW · Boeing 7373H4SDR AWXA200500213Fitting · corrodedMCN - MAJOR REPAIR - DURING C-16 CHECK CORROSION WAS FOUND ON RT OUTBOARD DRAG ANGLE FITTING, FUSELAGE TO VERTICAL STABILIZER FORWARD FACE. MAINTENANCE REMOVED CORRODED RT OUTBOARD DRAG ANGLE FITTING; FABRICATED A NEW REPLACEMENT FITTING PER DWG 65-53834; INSJan 31, 2005 · N303AW · Boeing 7373G7SDR C2XA05TY004Fitting · corrodedTYS, DURING A SCHEDULED INSPECTION, THE VERTICAL STAB TO FUSELAGE FITTING ATTACH BRACKET WAS FOUND FRETTING ON SKIN AT FRAME 75. MAINTENANCE REMOVED THE STAB FITTING AT FRAME 75, CLEANED AND INSPECTED THE SKIN AND FITTING (NO CORROSION OR DAMAGE WAS FOUND), AJan 13, 2005 · N14953 · Emb EMB145LRSDR DL73S041058Fitting · corrodedVERTICAL STABILIZER ATTACH FITTINGS NR 3 AND NR 6 LUGS WORN ON THE AFT FACES DUE TO CORROSION. REPAIRED IAW ERA 095030-14.Nov 24, 2004 · N376DL · Boeing 737247SDR SWAA043314Drag Brace · corrodedDURING SCHEDULED D-CHECK, FOUND VERTICAL STAB REAR SPAR BODY RT AND LT DRAG BRACES CORRODED. REMOVED AND REPLACED DRAG BRACES PER SRM.Nov 11, 2004 · N399WN · Boeing 7373H4SDR SWAA042941Fitting · corrodedDURING SCHEDULED D CHECK, FOUND VERTICAL FIN RT AND LT REAR SPAR CLEVIS FWD AND AFT LUGS CORRODED. REPAIRED FIN PER ER.Oct 10, 2004 · N396SW · Boeing 7373H4SDR USAA040826Attach Fitting · chafedPIT - Q5, FITTINGS, .1250, .5, .5, .5 INCH AREAS, HEAVY CHAFING (4 AREAS), ALL 4 AFT LUGS OF VERT STAB ATTACH FITTINGS.Oct 2, 2004 · N383US · Boeing 7373B7SDR A6WA200460038Angle · crackedFOUND CRACK ON THE VERTICAL STAB TO FUSELAGE CLOSING ANGLE RIGHT SIDE AT APPROX FRAME 45. MAINTENANCE REQUESTED REPAIR FROM BAE SYSTEMS REF AVMAX FAX 656-2015004. (M)Sep 23, 2004 · N156TR · Bac 146200ASDR SWAA042739Fitting · corrodedDURING SCHEDULED D-CHECK, FOUND VERTICAL STABILIZER SPAR ATTACH FITTINGS AIRCRAFT SIDE, FWD LT FITTING AFT LUG AFT FACE CORRODED. REPAIRED VERTICAL STAB FITTINGS PER ER.Sep 21, 2004 · N675AA · Boeing 7373A4SDR SWAA042658Drag Brace · corrodedDURING SCHEDULED D-CHECK, FOUND LT VERTICAL STABILIZER AFT DRAG BRACE, CORRODED. REMOVED AND REPLACED LT VERTICAL STABILIZER DRAG BRACE PER SRM.Sep 14, 2004 · N675AA · Boeing 7373A4SDR DHL2004801545Angle · crackedLT VERTICAL STABILIZER LWR ATTACH ANGLE CRACKED 4.000, ZR 47.000 (FRONT SPAR PLANE) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW DC8 SRM 53-2-5 FIG 16A SHEET 1-2 PG 44A, B, C, D. REMOVED FASTENERS IAW DC8 SRM 51-1-21 PG 1. CUT OUT DAMAGED SECTION IAW DC8 SRM 53Sep 9, 2004 · N801DH · Doug DC873FSDR A6WA200460037Angle · crackedFOUND CRACK ON THE VERTICAL STAB TO FUSELAGE CLOSING ANGLE LEFT SIDE, AT APPROX FRAME 45. MAINTENANCE REQUESTED REPAIR FROM BAE SYSTEMS REF AVMAX FAX 656-2015003. (M)Sep 3, 2004 · N156TR · Bac 146200ASDR DL73S040783Attach Fitting · corrodedVERTICAL STABILIZER ATTACH LUGS FOUND CORRODED ON THE NR 3 AND NR 6 FORE AND AFT FACES. REPAIRED IAW ERA 092521-14.Aug 20, 2004 · N375DL · Boeing 737247SDR USAA040464Fitting · corrodedPIT - FOUND LUG CORRODED .150 INCH DIAMETER SPOTS (TWO EACH), RIGHT AFT OUTBOARD VERTICAL STAB ATTACH LUG ON FUSELAGE. REAMED AND REBUSHED PER EA 78920. (M)Aug 5, 2004 · N426US · Boeing 7374B7SDR USAA040436Fitting · wornPIT - FOUND LUG WITH WEAR ON BUSHING FACES,.005 INCH DEEP AND 1 INCH IN DIAMETER, VERT STAB AFT OUTBOARD ATTACH LUG BUSHINGS LT SIDES. REAMED AND REBUSHED PER EA 78920. (M)Aug 5, 2004 · N426US · Boeing 7374B7SDR USAA040418Attach Fitting · wornPIT - FOUND LUG WITH WEAR .005 INCH DEEP, 1 INCH DIAMETER, VERTICAL STAB AFT OUTBOARD ATTACH LUG RIGHT SIDE BUSHINGS. REBUSHED PER MM 55-30-00 AND DWG 65-52274. (M)Aug 5, 2004 · N426US · Boeing 7374B7SDR SWAA042218Fitting · corrodedDURING SCHEDULED D-CHECK, FOUND VERTICAL STAB FITTING LUGS, CORRODED. REPAIRED VERTICAL STAB FITTING LUGS PER SRM AND ER.Aug 3, 2004 · N391SW · Boeing 7373H4SDR SWAA042157Fitting · corrodedDURING SCHEDULED D-CHECK, FOUND VERTICAL STAB FITTING LUGS CORRODED. REPAIRED VERTICAL STAB FITTING PER ER.Jul 28, 2004 · N392SW · Boeing 7373H4
Back to JASC 5553