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 05FDEA00276Tie · corrodedCORROSION VERTICAL STAB TENSION TIE RT AFT VERTICAL BOLT HOLE AIRCRAFT AND TENSION TIE. *S/D* REPAIRED PER EA 7-5530-86241.Feb 10, 2005 · N235FE · Boeing 727200SDR 05FDEA00275Tie · corrodedCORROSION VERTICAL STAB TENSION TIE LT FWD VERTICAL BOLT HOLE AIRCRAFT AND TENSION TIE. *S/D* REPAIRED PER EA 7-5530-86241.Feb 10, 2005 · N235FE · Boeing 727200SDR 05FDEA00274Tie · corrodedCORROSION VERTICAL STAB TENSION TIE RT FWD VERTICAL BOLT HOLE AIRCRAFT AND TENSION TIE. *S/D* REPAIRED PER EA 7-5530-86241.Feb 10, 2005 · N235FE · Boeing 727200SDR 05FDEA00273Tie · corrodedCORROSION VERTICAL STAB TENSION TIE LT AFT VERTICAL BOLT HOLE AIRCRAFT AND TENSION TIE. *S/D* REPAIRED PER EA 7-5530-86241.Feb 10, 2005 · N235FE · Boeing 727200SDR USAA050312Hinge Bracket · wornPIT - FOUND HINGE PLATES WITH THREE WORN HOLES .25 INCH DIAMETER, RUDDER HINGE NR 7 PLATES ON VERTICAL STABILIZER. DEFECTIVE PART REPLACED WITH IDENT PART PER AMM 55-00-00. (M)Feb 9, 2005 · N520AU · Boeing 7373B7SDR SWAA050273Angle · crackedDURING SCHEDULED HC1 CHECK, FOUND RT VERTICAL STABILIZER FITTING ATTACH ANGLE AT STA 1007, CRACKED. REPAIRED STABILIZER PER EA.Feb 1, 2005 · N744SW · Boeing 7377H4SDR C2XA05TY007Bearing · wornTYS DURING A MODIFICATION OF AIRCRAFT, INSPECTION FOUND THE VERTICAL STAB, LEFT HAND SPHERICAL BEARING HAD AXIAL AND LATERAL PLAY. MAINTENANCE REAMED THE THE VERTICAL BEARING HOUSING AND INSTALL NEW BUSHINGS IAW EC5510-01108. ALL WORK WAS ACCOMPLISHED AND OJan 24, 2005 · N16944 · Emb EMB145ERSDR 05FDEA00130Spar · corrodedVERTICAL FIN REAR SPAR R & L PANEL SUPPORT STRUCTURE HAS MODERATE CORROSION AT PANEL ATTACH POINTS. REMOVED CORROSION IAW A310-200 SRM. APPLIED SURFACE PROTECTION IAW A310-200 SRM 51-23-10. AT RT SIDE RIB 26, TRIMMED OUT DAMAGED SECTION OF TOP FLANGE, INSTAJan 20, 2005 · N405FE · Airbus A310203SDR UPS05244037Forging · crackedINSPECTION TYPE: SV, RIGHT VERTICAL FIN FRONT SPAR LWR FORGING. A 2 INCH VISIBLE CRACK IN FORGING STA 1229-1231. CRACK IN RADIUS AREA OF STRAP 1.75 X .25 INCH. REPAIRED LEFT AND RIGHT VERTICAL STAB FRONT SPAR FORGING FOR FERRY FLIGHT STA 1229 - 1231 IAW UPSJan 5, 2005 · N948UP · Boeing 72725CSDR 04FDEA03386Hinge Bracket · gougedVERTICAL STABILIZER REAR SPAR, UPPER RUDDER HINGE FITTING BENT AND GOUGED. REMOVED AND REPLACED UPPER RUDDER HINGE SUPPORT BRACKET IAW MD10-10 MM 55-53-01-2 AND EA 8- 5530-83844, STABILIZER- VERTICAL STABILIZER RUDDER HINGE BRACKET, REPAIR. REFERENCE NON-RODec 7, 2004 · N377FE · Doug MD1010FSDR 04FDEA03374Structure · misrepairedVERTICAL STAB TOO LARGE COMPOSITE REPAIR ON LT SIDE L/E. EXISTING COMPOSITE REPAIRS PERFORMED IAW EA 6-5500-50375, DATED 06/23/2000. DAMAGED STEEL COVER WAS REPAIRED BY NEW ONE, IAW EA 6-5500-50375.Dec 6, 2004 · N452FE · Airbus A310SDR 04FDEA03240Angle · crackedCOMPLY WITH EA 8-5530-82462 INSPECTION AND REPLACEMENT OF UPPER VERTICAL STABILIZER RESPAR BASE ANGLE SB DC10-55-019R3. CLOSING ACTION ON 11/15/04, ON N/R S00005. COMPLIED WITH EA 8-5530-82462.Nov 28, 2004 · N68059 · Doug DC1010SDR SWAA043311Beam · crackedDURING SCHEDULED D-CHECK, FOUND VERTICAL STAB RT T/E BEAM AT STATION 79, CRACKED. REMOVED AND REPLACED BEAM SECTION PER SRM.Nov 11, 2004 · N399WN · Boeing 7373H4SDR SWAA043264Fitting · corrodedDURING SCHEDULED D-CHECK, FOUND VERTICAL FIN RT AND LT REAR SPAR CLEVIS FWD AND AFT LUGS CORRODED. REPAIRED VERTICAL FIN FITTING PER ER.Nov 8, 2004 · N600WN · Boeing 7373H4SDR GLBA20030756Bracket · crackedLT SIDE OF VERT STAB TO FUSELAGE L BRACKET CRACKED. REPAIRED CRACK IAW B1900 SRM 51-70 AND EO 04-UE122-01.Nov 6, 2004 · N122UX · Beech 1900DSDR SWAA043219Clevis · corrodedDURING SCHEDULED D-CHECK, FOUND VERTICAL STABILIZER AFT SPAR RT AND LT PRIMARY CLEVIS FWD AND AFT LUGS CORRODED. REPAIRED VERTICAL STABILIZER PER ER.Nov 5, 2004 · N600WN · Boeing 7373H4SDR 72300060Attach Fitting · corrodedCORROSION IN BORE OF RT STAB HINGE BEARING LUG.Oct 21, 2004 · N723CK · Boeing 7272H3SDR 72300059Attach Fitting · corrodedCORROSION IN BORE OF LT STAB HINGE BEARING LUG.Oct 21, 2004 · N723CK · Boeing 7272H3SDR ABXA040358Bracket · crackedRUDDER UPPER HINGE BRACKET CRACKED AT RIGHT MOUNT HOLE. REMOVED AND REPLACED UPPER HINGE BRACKET IAW DC-9 SRM 51-30-1.Oct 18, 2004 · N944AX · Doug DC931SDR ASAA0480527Skin · corrodedOKC - C-CHECK, AFT BELLY SKIN CORRODED STA 1098 TO STA 1110 BETWEEN LONG 29L AND 27L. REMOVED DAMAGE, HFEC, FABRICATED AND INSTALLED REPAIR DOUBLER IAW EA 5310-02398 AND EA 10582.Oct 2, 2004 · N973AS · Doug DC983SDR ASAA0480526Skin · gougedOKC - C-CHECK VERTICAL STAB UPPER SKIN GOUGED AROUND BANANA UPPER FAIRING PANEL 3705A ATTACHMENT AREA. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER/SKIN AND DOUBLER, IAW SRM 51-30-1 AND 51-30-2, EA 5530-01108 AND EA 10594.Sep 28, 2004 · N973AS · Doug DC983SDR DLM88040910Spar Cap · damagedVERTICAL STABILIZER HORIZONTAL STABILIZER HINGE PLATES HAD THREE HOLES WITH DAMAGE. REPAIRED IAW ERA 093177-14AD.Sep 23, 2004 · N902DE · Doug MD88SDR DHL2004801548Angle · crackedLEFT 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 5Sep 9, 2004 · N801DH · Doug DC873FSDR 04FDEA02592Fork · corrodedVERTICAL STAB STA 690/RIB 21 HINGE FORK NR 6 IS CORRODED. REMOVED AND REPLACED HINGE ARM ASSY IAW A310-200 AMM55-36-46-4-01, FUNCTIONAL TEST GOOD IAW A310-200 AMM 27-20-00-5.Sep 1, 2004 · N414FE · Airbus A310203SDR UPS04843100Attach Angle · crackedINSPECTION TYPE:C2 VERT STAB LOWER FRONT SPAR EXTERNAL DRAG ANGLE CRACKED AT STA 1756. REMOVED DOUBLER PER SRM 51-3-0, 51-1-21. STOP DRILLED CRACK PER SRM 53-2-0, NDT VERIFIED STOP DRILL PER SPM 06-10-01.001. FABBED REPAIR ANGLE FROM S25043-17-7PH .080. HEAug 23, 2004 · N708UP · Doug DC871FSDR SWAA041909Clevis · corrodedDURING SCHEDULED D-CHECK, FOUND VERTICAL STAB AFT SPAR CLEVIS, FWD AND AFT LUG, CORRODED. REPAIRED VERTICAL STAB PER ER.Jul 6, 2004 · N386SW · Boeing 7373H4SDR 04FDEA01913Bulkhead · crackedVERTICAL STAB BULKHEAD BELOW NR 2 ENGINE FUEL LINE DRAIN SCUFFER, BOTH ENDS GOUGED AND CRACKED. REMOVED AND REPLACED DRAIN SCUFFER SEAL FAB ON TRAVLER T4/440479 IAW SRM 51-31-01. BLENDED GOUGES IAW SRM 55-00-01. NDT CRACK CHECK, FOUND NO CRACKS, TREATED ANDJul 2, 2004 · N387FE · Doug DC1010SDR 04FDEA01912Bulkhead · gougedVERTICAL STAB BULKHEAD BELOW NR 2 ENGINE FUEL LINE DRAIN SCUFFER, BOTH ENDS GOUGED AND CRACKED. REMOVED AND REPLACED DRAIN SCUFFER SEAL FAB ON TRAVLER T4/440479 IAW SRM 51-31-01. BLENDED GOUGES IAW SRM 55-00-01. NDT CRACK CHECK, FOUND NO CRACKS, TREATED ANDJul 2, 2004 · N387FE · Doug DC1010SDR CA040625003Casting · cracked(CAN) DURING MAINTENANCE CHECK A CRACK WAS FOUND ON THE SPIDER CASTING AT RUDDER STATION 23.27 BELOW THE STANDBY RUDDER PCU IN THE VERTICAL STABILIZER. THE CRACK IS 3 INCHES IB OF OUTER EXTREMITIES, 7 INCHES FORWARD OF THE LOWER RUDDER HINGE POINT APPROX 1.5Jun 24, 2004 · Boeing 737201SDR IXXA060323SAngle · corrodedDURING ROUTINE C CHECK, FOUND LEFT SIDE VERTICAL STABILIZER TO FUSELAGE SKIN ATTACH ANGLE CORRODED AT STATION Y1606. REPAIRED PER ALL APPLICABLE DATA.Jun 17, 2004 · N41CX · Doug DC862FSDR USAA040288Beam · crackedPIT - FOUND BEAM CRACKED 2 INCHES, 3 INCHES FROM LOWER END OF VERT STAB LT T/E BEAM. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 53-30-13 FIG 1. (M)Jun 11, 2004 · N355US · Boeing 737301SDR 04FDEA01623Channel · elongatedCOMPLY WITH EA 8-5530-78221 STABILIZERS VERTICAL. RIGHT FWD ACCESS PANEL JAMB ELONGATED HOLES REPAIR, P/N AMC7265-2. COMPLIED WITH EA 8-5530-78221 STABILIZERS VERTICAL RIGHT FWD ACCESS PANEL JAMB ELONGATED HOLES REPAIR, P/N AMC 7265-2.Jun 5, 2004 · N68051 · Doug DC1010SDR SWAA041471Beam · crackedDURING SCHEDULED D CHECK, FOUND VERTICAL STAB T/E BEAM AT LT RUDDER STATION 13.3 TO RUDDER STATION 121.64, CRACKED. REMOVED AND REPLACED VERTICAL STAB BEAM PER SRM.May 24, 2004 · N380SW · Boeing 7373H4SDR SWAA041385Clevis · corrodedDURING SCHEDULED D CHECK, FOUND VERTICAL STAB REAR SPAR CLEVIS FWD AND AFT LUG FACES, CORRODED. REPAIRED VERTICAL STAB PER ER.May 14, 2004 · N389SW · Boeing 7373H4SDR UPS04242344Frame · crackedINSPECTION TYPE: C, VERT STAB JACKSCREW CUTOUT LT, FWD FRAME CRACKED AT FW STA 128 APPROX. CRACKED FRAME REMOVED IAW SRM 51-30-02. NEW FRAME INSTALLED IAW SRM 51-30-02Apr 26, 2004 · N930UP · Boeing 72722CSDR SWAA040961Fitting · corrodedDURING SCHEDULED D CHECK, FOUND VERTICAL FIN RT LUG AFT FACE AND BORE CORRODED. REPAIRED VERTICAL FIN LUG PER ER.Apr 1, 2004 · N304SW · Boeing 7373H4SDR C2XA04SH105Hinge Bracket · corrodedSHV- DURING C-CHECK THE UPPER CENTER HINGE BRACKET ON THE VERTICAL STABILIZER TO THE RUDDER WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 135 AMM 20-10-01 AND EMB 135 IPC 55-31-00. THE AIRCRAFT WAS APPROVED FOR RETURFeb 26, 2004 · N14508 · Emb EMB135ERSDR SWAA040373Fitting · corrodedDURING SCHEDULED D CHECK, FOUND VERTICAL STAB RT AND LT FITTING AFT SPAR LUGS CORRODED. REPAIRED VERTICAL STAB FITTING PER ER.Feb 5, 2004 · N665WN · Boeing 7373Y0SDR 2004FA0000017Bracket · crackedDURING RUDDER REMOVAL FOR REQUIRED MAINTENANCE, A CRACK WAS FOUND IN MIDDLE RUDDER HINGE BRACKET MOUNTED ON THE VERTICAL FIN. THE CRACK IS AT THE HINGE BEARING HOLE. DUE TO THE LOCATION, THIS CRACK WOULD NOT HAVE BEEN VISIBLE WITHOUT REMOVING THE RUDDER FIRSDec 19, 2003 · N801PC · Piper PA24260SDR 2003FA0001279Frame · crackedCRACKED FRAME AT TB/VERTICAL FIN SPAR JUNCTION. THIS IS THE SECOND SHIP WITH AN IDENTICAL CRACK THAT HAS BEEN SEEN IN THE LAST 90 DAYS. THE MFG SRM DETAILS THE REQUIRED REPAIRS. DETECTION IS POSSIBLE USING BRIGHT LIGHT AND MIRROR, OR BY DIRECT OBSERVATION. ADec 19, 2003 · N1YU · Cessna 150MSDR MWEA030465Angle · crackedVERTICAL STABILIZER RT FORWARD INSIDE ATTACH ANGLE IS CRACKED. FABRICATED AND INSTALLED NEW ANGLE.Dec 3, 2003 · N601ME · Doug MD88SDR C2XA03TY202Support Fitting · damagedDURING A SCHEDULED 2C INSPECTION THE LT AND RT VERT STAB SPHERICAL BEARINGS HAD AXIAL PLAY. MAINT REMOVED THE SPHERICAL BEARINGS, REAMED AND INSTALL THE 1ST OVERSIZE BUSHINGS, REINSTALL BEARINGS AND PERFORMED A DIEHEDRIAL CHECK IAW EC5510-01045; EC5510-01069 Dec 3, 2003 · N27506 · Emb EMB135ERSDR AWXA200301515Beam · crackedDURING C-12 CHECK 2 EACH CRACKS WERE FOUND ON VERTICAL STABILIZER TRAILING EDGE BEAM AT RT SIDE OF YAW DAMPER CAVITY INTERIOR, APPROXIMATELY RIB STA 100. MAINTENANCE REMOVED CRACKED SECTION OF VERTICAL STABILIZER BEAM AT RT SIDE OF YAW DAMPER CAVITY INTERIOR,Nov 11, 2003 · N908AW · Boeing 7572G7SDR CA031106012Channel · cracked(CAN) WHILE COMPLETING A X-RAY INSPECTION ON THE VERTICAL STABILIZER, A CRACK WAS NOTED ON THE RT VERTICAL FLANGE OF THE CHANNEL. THE CRACK IS APPROXIMATELY .6250 INCH IN LENGTH. IT IS LOCATED IN THE AREA COVERED BY AD95-13-02. THE AIRCRAFT HAD BEEN MODIFIED Nov 3, 2003 · Gulstm 690ASDR CA031106010Channel · cracked(CAN) DURING X-RAY INSPECTION OF THE VERTICAL STABILIZER A CRACK APPROXIMATELY .7500 INCH LONG WAS NOTED ON P/N 410008-85 CHANNEL LOCATED IN THE LOWER SECTION OF THE VERTICAL STABILIZER. THIS PART IS LOCATED IN THE AREA SUBJECT TO AD 95-13-02. THE CRACK IS RUNNov 3, 2003 · Gulstm 690ASDR A6WA200360062Angle · crackedFOUND VERTICAL STAB CLOSING ANGLE RT HAS CRACK. MAINTENANCE REQUESTED REPAIR FROM BAE SYSTEMS REF AVMAX FAX 1698-6910004. (M)Oct 28, 2003 · N291UE · Bac 146200ASDR SWAA032369Fitting · corrodedDURING SCHEDULED D CHECK, FOUND VERTICAL STAB ATTACH FITTING AFT SPAR CLEVIS LUGS CORRODED. REPAIRED CLEVIS LUGS PER SRM AND BFG ER.Oct 27, 2003 · N379SW · Boeing 7373H4SDR EIA2003143Beam · damagedVERTICAL STAB RT TRAILING EDGE BEAM FWD AND AFT WEBS DAMAGED, DO TO POWER PACK LOWER RUDDER INSTALLATION. INSTALLED FORWARD WEB DOUBLER AND 2 EA. FILLERS IAW MFG 747 SRM 51-30-02 AND ECRA 482-55-183-2Oct 20, 2003 · N482EV · Boeing 747212BSDR EIA2003139Frame · brokenVERTICAL STAB RT SIDE ACCESS PANEL 324 DR AFT SECTION OF PANEL ATTACH FRAME HAS SECTION BROKEN OFF. REMOVED DAMAGED, NDT AREA, FABBED AND INSTALLED REPAIR IAW ECRA 482-55-196-2Oct 20, 2003 · N482EV · Boeing 747212BSDR EIA2003140Web · damagedVERTICAL STAB RT HANDSIDE ACCESS PANEL 324DR AFT WEB AND GUSSET DAMAGED. REMOVED 2 EA. GUSSETS, FABRICATED 2 EA. GUSSETS, SPLICE PLATE, FILLERS (2EA) AND WEB AND INSTALLED IAW ECRA 482-55-183-2Oct 20, 2003 · N482EV · Boeing 747212B
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