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 VNAA202312130013Drag Angle · crackedCRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACENov 6, 2023 · N560NN · Cndair CL6002D24SDR VNAA202312130012Drag Angle · crackedDESCRIPTION: CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). CORRECTIVE ACTION: DRAG ANGLE WAS REPAIRED PER CRJ-900 SRM 55-31-00-201-001-A01Nov 6, 2023 · N560NN · Cndair CL6002D24SDR WX0A2023111531891Unknown · unknown(MAJOR REPAIR) DURING COMPLETION OF EO E5540-0010 (IMPROVED RUDDER HINGE LINE BEARING) HINGE ARMS NO.03 FOUND OUT OF LIMITS DUE TO HOLES DIMENSIONS / VERTICAL HINGE ARM #3 REPLACED PER AIRBUS DOSSIER #81304706 AND COMPLY WITH TD/81304706/008/2023#A SRM 55-36-4Nov 1, 2023 · N333NV · Airbus A319111SDR 2023FA0000698Spar Cap · corrodedFIELD REPAIR - CORROSION, VERTICAL STABILIZER, AFT SPAR CAP VFS 174.85 - VFS 238.39. REPORT NO. FR-680-0225-12507 DATED OCTOBER 12, 2023 WITH FAA FORM 8100-9.Oct 29, 2023 · N341QS · Cessna 680CESDR 2023FA0000675Spar Cap · corrodedCORROSION, VERTICAL STABILIZER, RH VERTICAL SPAR CAP, VFS 168.94: REMOVED CORROSION AND ACCOMPLISHED ULTRASONIC THICKNESS CHECK. VERIFIED NO CRACK INDICATIONS. REAPPLIED PROTECTIVE FINISH AND CIC. ALL WORK ACCOMPLISHED IAW TEXTRON AVIATION FIELD REPAIR: FR-68Oct 24, 2023 · N359QS · Cessna 680SOVSDR DALA2023102308670Unknown · unknownSHIP 3119 CORROSION FIXED BUSH ON VERTICAL STABILIZER LOWER RUDDER ACTUATOR. CORRECTIVE ACTION: REPLACED BUSHINGS (2 EA) ON VERTICAL STABILIZER LOWER RUDDER ACTUATOR AS PER A319 SRM 51-72-12-911-002. (0030108)Oct 22, 2023 · N319NB · Airbus A319114SDR HNAA2023112100450Unknown · unknownE003551 FOUND RH VERTICAL STABILIZER SPHERICAL BEARING HOUSING BORE OUT OF LIMITS. ENLARGED RIGHT HAND VERTICAL STABILIZER SPHERICAL BEARING HOUSING TO THE FIRST OVER SIZE IAW PIEDMONT EO1-55-23-0378.Oct 18, 2023 · N654AE · Emb EMB145LRSDR VNAA20231125004Fairing · erodedEXTENSIVE EROSION ON UPPER FAIRING 326BT. UPPER FAIRING 326BT WAS REPAIRED PER CRJ-900 S.R.M 51-73-00-201-001-A01 PAR. 4. B IN REFERENCE TO EA 21-C9-55-976 REV. A SECTION III PERMANENT REPAIROct 11, 2023 · N557NN · Cndair CL6002D24SDR VNAA202311230002Drag Angle · crackedCRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). CRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUOct 11, 2023 · N559NN · Cndair CL6002D24SDR VNAA202311230001Drag Angle · crackedCRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM Oct 11, 2023 · N559NN · Cndair CL6002D24SDR SWAA2023110808748Angle · crackedCRACK ANGLE LEADING EDGE SKIN LEADING EDGE LOC BS 1016 AND BTW STR 2L TO STR 2R VERTICAL STABILIZER 2023-635338<[01] REPLACED ANGLE AND FASTENERS ON LEADING EDGE SKIN LEADING EDGE LOC BS 1016 AND BTW STR 2L TO STR 2R VERTICAL STABILIZER IAW B737-700 SRM 51-40-Oct 7, 2023 · N909WN · Boeing 7377H4SDR VNAA202311290028Hinge Fitting · excess playDAMAGE T: ELONGATED HOLES DURING ADJUSTMENT OF THE NEW HINGE FITTING NO. 2 AND NO. 3 AT VERTICAL STABILIZER REAR SPAR MIDDLE SECTION, IN REF TO NRC: 00191. HINGE FITTING NO. 2 AND NO. 3 AT VERTICAL STABILIZER REAR SPAR MIDDLE SECTION WERE REPLACED PER RIL #21Oct 6, 2023 · N556NN · Cndair CL6002D24SDR VNAA202311280003Drag Angle · crackedCRACK ON VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE LH , BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00) CRACK ON VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE LH , BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (Oct 6, 2023 · N556NN · Cndair CL6002D24SDR GTIA2023100637517Arm · distortedRUDDER HINGE FITTING BR3 FOUND WITH DISTORTION. RAF01-3282903-2 CREATED.-VERIFIED NR #5001264862-0040 AND TC #1004087214-0010, REPAIR HAS BEEN ACCOMPLISHED IAW SPIRIT EA 5536-2310 REV. 00 WITH NO REINSPECTION REQUIRED.Oct 6, 2023 · N638NK · Airbus A320232SDR FDEA202310041698Fitting · crackedDURING ULTRASONIC INSPECTION FOR VERTICAL CRACKS BEHIND SERVICE REPAIR SR10550013 PER DRAWING NUMBER SN10550000 REV D ON RIGHT HAND SIDE LOWER VERTICAL STABILIZER FORWARD FLANGE OF UPPER REAR SPAR CAP, STATION 2164, EXISEING CRACK INDICATION FOUND FROM 2Oct 4, 2023 · N522FE · Doug MD11FSDR SWAA2023102305598Flap · crackedFOUND DENT WITH A CRACK OUT OF LIMITS ON UPPER SURFACE R/H WING I/B AFT FLAP AT 32' FROM I/B EDGE AND 10.5' T/E; LENGTH OF DENT CRACK =1.5'.<[01] APPLIED REPAIR AT UPPER SURFACE R/H WING I/B AFT FLAP PER B737 SRM<BR> 57-53-01-2R-4; SRM 51-70-10-2R-4 AND SRM 51Sep 28, 2023 · N915WN · Boeing 7377H4SDR AALA202311094580Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON BOLT OF FRONT SPAR FITTING RIGHT HAND SIDE AT VERTICAL STABILIZER. LOCATED AT STA 1016. REPLACED WITH IDENTICAL PART (PART NUMBER 170A1611-3). PER JOB CARD 08C32253004.Sep 26, 2023 · N807NN · Boeing 737823SDR AALA202309256355Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: RUDDER HINGE #4 ATTACHMENT FITTING HINGE BOLT HAS AXIAL AND RADIAL MOVEMENT. REPLACED RUDDER HINGE #4 PER EA 5520Y001.Sep 18, 2023 · N752US · Airbus A319112SDR AALA202309256834Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: RUDDER HINGE #2 ATTACHMENT FITTING HINGE BOLT HAS AXIAL AND RADIAL MOVEMENT. REPLACED RUDDER HINGE #2 PER EA 5520Y001.Sep 18, 2023 · N752US · Airbus A319112SDR AALA202309251709Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: RUDDER HINGE #7 ATTACHMENT FITTING HINGE BOLT HAS AXIAL AND RADIAL MOVEMENT. REPLACED RUDDER HINGE #7 PER EA 5520Y001.Sep 18, 2023 · N752US · Airbus A319112SDR SWAA2023102000378Angle · crackedCRACK ANGLE LEADING EDGE LOC BS 1016 AND BTW STR 3L TO STR 3R AT VERTICAL STABILIZER 2023-578002<[01] REPLACE ANGLE LEADING EDGE AND FASTENERS LOC BS 1016 AND BTW STR 3L TO STR 3R AT VERTICAL STABILIZER SI IAW B737-700 SRM 51-40-02 DWG 176A3101 REV. - SEE INDISep 14, 2023 · N7862A · Boeing 73779PSDR REXA2022100200778Angle · crackedVERTICAL STAB RIGHT AFT DRAG ANGLE IS CRACKED. REPAIRED RIGHT AFT DRAG ANGLE I.A.W. CRJ700 SRM 53-31-00-201-001-A01Sep 13, 2023 · N655CA · Cndair CL6002C10SDR IXXA2023092301Panel · delaminated10 INCH DIAMETER DELAMINATION FOUND ON R/H VERTICAL STABILIZER PANELSep 13, 2023 · N251AZ · Boeing 767323SDR JGVR20230913001Unknown · unknownREPAIRED CORRODED AREAS OF THE VERTICAL STABILIZER AFT SPAR CAPS BY MECHANICALLY BLENDING PERFORMING NDT AND REPORTING FOR REPAIR DISPOSITION. CLEANED TREATED AND PRIMED AREAS FOUND ACCEPTABLE AND TRIMMED THE LH SKIN BOND ASSEMBLY, FABRICATED AND INSTALLING RESep 13, 2023 · N397QS · Cessna 680CESDR SWAA2023101798951Plate · corrodedCORROSION BONDING JUMPER PLATE LOC. UPPER REAR SPAR BETWEEN HINGE 7AND 8 AT VERTICAL STABILIZER 2023-569575<[01] REPLACED BONDING JUMPER PLATE LOC. UPPER REAR SPAR BETWEEN HINGE 7AND 8 AT VERTICAL STABILIZER IAW B737-700 AND SRM 51-10-02 ITEM 9 AND DWG #175A16Sep 10, 2023 · N448WN · Boeing 7377H4SDR SWI2023F00472Unknown · crackedVERTICAL STABILIZER TO FUSELAGE ATTACHMENT RH FORWARD DRAG ANGLE POSSIBLE CRACK (C-CHECK RO 11/10/2023) REMOVED, FABRICATED AND REPLACED WITH NEW RH FWD DRAG ANGLE AT FUSELAGE TO VERT STAB ATTACHMENT REF REO 670-55-31-018 REV -A DATED 2016-11-10. COMPLIED Sep 5, 2023 · N713EV · Cndair CL6002C10SDR UIEA2023082900818Unknown · unknownRH VERTICAL STABILIZER EXTERIOR BTW FSS 220.521 TO FSS 270.784 WITH DELAMINATIONS.(<P>RH VERTICAL STABILIZER EXTERIOR BTW FSS 220.521 TO FSS 270.784 WAS REPAIRED IAW SRM 55-30-01-2R-1 REP 1 NOTE F FIG 201 PAGE 2 AND SRM 51-70-10-2R-4 REP 4 FIG 201 PAGE 1. REV Sep 1, 2023 · N1409A · Boeing 767306SDR UIEA2023082900819Unknown · unknownLH VERTICAL STABILIZER EXTERIOR BTW FSS 220.521 TO FSS 270.784 WITH DELAMINATION.(<P>LH VERTICAL STABILIZER EXTERIOR BTW FSS 220.521 TO FSS 270.784 WAS REPAIRED IAW SRM 55-30-01-2R-1 REP 1 NOTE F FIG 201 PAGE 2 AND SRM 51-70-10-2R-4 REP 4 FIG 201 PAGE 1. REV 4Sep 1, 2023 · N1409A · Boeing 767306SDR SWAA2023082893122Panel · crackedVERTICAL FIN LEADING EDGE COMPOSITE IS CRACKED AND HAS MATERIAL MISSING BELOW LEADING-EDGE PANEL 322C.<[01] REPAIRED VERTICAL FIN LEADING EDGE COMPOSITE BELOW L/E PANEL 322C REF SRM 55-30-01-2R-13Aug 24, 2023 · N452WN · Boeing 7377H4SDR VNA2023F00006Drag Angle · crackedCRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). REPAIRED PER CRJ900 SRM 55-31-00-201-001-A01Aug 22, 2023 · N555NN · Cndair CL6002D24SDR VNA2023F00007Drag Angle · crackedCRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). REPAIRED PER CRJ-900 SRM 55-31-00-201-001-A01Aug 20, 2023 · N555NN · Cndair CL6002D24SDR FDEA202308201464Intercostal · crackedEMPENNAGE: VERTICAL STABILIZER CENTER SPAR TO REAR SPAR LOWER PANEL LEFT HAND AFT END INTERCOSTAL AT STATION 2164 FOUND CRACKED. VERTICAL STABILIZER CENTER SPAR TO REAR SPAR LOWER PANEL LEFT HAND AFT END INTERCOSTAL AT STATION 2164 REPAIR CARRIED OUT AS PAug 20, 2023 · N631FE · Doug MD11FSDR JJBA20230821018Unknown · unknownVERT STAB, RH SKIN DENT AT AFT OF SPAR 41% AND 1 INCH UNDER RIB ZV 2799.0. SKIN REPAIRED WITH A DOUBLERAug 15, 2023 · N11192 · Emb EMB145XRSDR FDEA202308151408Fitting · crackedDURING HFEC SURFACE INSP ON RT SIDE, FWD FLANGE OF LOWER VERTICAL STAB REAR SPAR CAP, NR 4 BANJO FITTING UPPER SECTION AT STA Y=2164, FOUND CRACKED ALONG RADIUS BETWEEN LOWEST FASTENER & 2ND FASTENER WITH LENGTH APPROX 0.75 INCH. TRIMMED IAW SRM 55-30-02-2R FAug 15, 2023 · N631FE · Doug MD11FSDR FDEA202308151407Fitting · crackedDURING HFEC SURFACE INSP ON LT SIDE FORWARD FLANGE OF LOWER VERTICAL STAB REAR SPAR CAP, NR 4 BANJO FITTING UPPER SECTION AT STA Y=2164, FOUND CRACK ALONG RADIUS FROM LOWEST FASTENER TOWARDS THE 2ND FASTENER WITH LENGTH APPROXIMATELY 0.5 INCH. TRIMMED AS PERAug 15, 2023 · N631FE · Doug MD11FSDR SWAA2023091989140Panel · crackedLH VERTICAL FIN LEADING EDGE ACCESS PANEL 322AL LOWER AFT METAL CRACKED. LH VERTICAL FIN LEADING EDGE ACCESS PANEL 323AL LOWER AFT METAL CRACKED.<[01] VERIFIED AND INSPECTED REPLACED LH VERTICAL FIN LEADING EDGE ACCESS PANEL 322AL LOWER AFT METAL.Aug 14, 2023 · N447WN · Boeing 7377H4SDR SWAA2023083188582Access Panel · crackedCRACK ACCESS PANEL 324AL AT VERTICAL STABILIZER 2023-508338<[01] REPLACED RETAINER LOCATED ON ACCESS PANEL 324AL AT VERTICAL STABILIZER IAW. B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 172A6123 SHEET 1 REV: A;[02] CORRECTED STEP 1: REPLACED RETAINER LOCAug 11, 2023 · N410WN · Boeing 7377H4SDR SWAA2023083188583Access Panel · crackedCRACK ACCESS PANEL 323AL AT VERTICAL STABILIZER 2023-508333<[01] REPLACED RETAINER LOCATED ON ACCESS PANEL 323AL AT VERTICAL STABILIZER IAW. B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 172A6122 SHEET 1 REV: B;[02] CORRECTED STEP 1: REPLACED RETAINER LOCAug 11, 2023 · N410WN · Boeing 7377H4SDR SWAA2023090587191Panel · crackedCRACK ACCESS PANEL 321A DORSAL RIB 8 VERTICAL STABILIZER 2023-491823<[01] TOOL USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 25-JAN-24.;[02] REPLACED RIB 8 LOCATED AT DORSAL FIN VERTICAL STABILIZER I.A.W B737-700 SRM 51-40-02; DWAug 8, 2023 · N903WN · Boeing 7377H4SDR AALA202308079815Hinge Arm · wornAIRCRAFT IN BASE MAINTENANCE: VERTICAL STABILZER #4 RUDDER HINGE ARM LOWER MIDDLE FASTENER HOLE IS WORN / OBLONGED AT STATION 263 AND RIB 6. REPLACED HINGE ARM PER SRM 55-36-42.Aug 4, 2023 · N827AW · Airbus A319132SDR AALA202308040001Unknown · unknownON MAY 12TH FOUND AMERICAN AIRLINES 777-200 TAIL# 7AA WITH LARGE AREA OF DELAMINATION ON VERTICAL STABILIZER. TODAY AUG 4TH FOUND AMERICAN AIRLINES TAIL# 7AB WITH DELAMINATION ON VERTICAL STABILIZER.....WAS INFORMED OF ANOTHER AMERICAN AIRLINES 777 WITH THE SAAug 4, 2023 · N770AN · Boeing 777223SDR AALA202308023703Spring · crackedAIRCRAFT IN BASE MAINTENANCE: UPON REMOVAL OF VERTICAL STABILIZER FOUND ON STABILIZER AFT LOWER SPRING CRACKED AT BS 1016, BETWEEN S2L AND S2R. REPLACED SPRING PER SRM 51-40-02.Aug 1, 2023 · N909AN · Boeing 737823SDR REXA2022073100553Drag Angle · crackedRH VERTICAL STABILIZER AFT DRAG ANGLE CRACKED. INSTALLED SERVICEABLE DRAG ANGLE AFT ON RH SIDE VERTICAL STABILIZER WITH PN: AV670-21186-004 IAW CRJ900 SRM 51-42-21-001-001-A01, 51-42-13-001-001-A01 AND 51-42-27-001-001-A01Jul 29, 2023 · N186PQ · Cndair CL6002D24SDR SWAA2023090183513Angle · crackedCRACK ACCESS PANEL 324AL ON SUPPORT ANGLE AT VERTICAL STABILIZER 2023-469934<[01] REPLACED SUPPORT ANGLE ON ACCESS PANEL 324AL AT VERTICAL STABILIZER IAW B737-700 SRM 51-40-02; SRM 51-10-02.;[02] REPLACED SUPPORT ANGLE ON ACCESS PANEL 324AL AT VERTICAL STABILIJul 28, 2023 · N7832A · Boeing 73779PSDR FDEA202307281321Frame · crackedEMPENNAGE-VERTICAL STABILIZER LEFT HAND ACCESS PANEL 363ML CUTOUT FRAME STATION 2140 FOUND CRACKED. CRACKED FRAME AT EMPENNAGE VERTICAL STABILIZER LEFT HAND ACCESS PANEL #363ML CUTOUT STATION 2140 AREA REMOVED AND REPLACED AS PER MD-11 SRM 51-33-01-0G. FRAJul 28, 2023 · N609FE · Doug MD11FSDR SWIA20230928725Unknown · damagedDURING AUDIT OF 2C TASK CARD 55-320-322 ( INTERNAL ZONAL INSPECTION OF THE VERTICAL STABILIZER TIP ), FOUND THE VERTICAL STABILIZER LH FWD. TRUNNION I/B & O/B FACE HAS SEVERAL AREAS OF IMPACT DAMAGE. PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OJul 25, 2023 · N983SW · Cndair CL6002B19SDR 2023F00228Unknown · unknownMINOR CORROSION FOUND ON LH VERTICAL STAB REAR SPAR CAP. ACCOMPLISHED VERTICAL STAB AFT SPAR CORROSION REPAIR IAW TEXTRON AVIATION REPAIR LETTER DQ40368.Jul 16, 2023 · N361QS · Cessna 680CESDR JGVR20230714003Unknown · unknownBLENDED SEVERAL CORRODED AREAS ON THE RH SIDE OF THE VERTICAL STABILIZER JUST UNDER THE TIP CAP, PERFORMED NDT AND REPORTED RESULTS FOR REPAIR DISPOSITION. TREATED, PRIMED, AND TOP COATED REPAIR AREAS PER TEXTRON FIELD REPAIR.Jul 14, 2023 · N397QS · Cessna 680CESDR SWAA2023081477747Rib · crackedCRACK DORSAL FIN ANGLE AT RIB #8 AT VERTICAL STABILIZER 2023-443955<[01] REMOVED ANGLE LOC. DORSAL FIN AT RIB #8 IAW B737-700 SRM 51-40-02 AND PERFORMED CLEAN ON RIB IAW SOPM 20-30-03 AND PERFORMED DETAIL VISUAL INSPECTION AND NOT FOUND CRACK ON RIB. RE-INSTALJul 12, 2023 · N296WN · Boeing 7377H4SDR ASAA2023071145420Fitting · damagedVERTICAL STAB HINGE ARM #4 HAS DAMAGED HOLE FOR RUDDER HINGE FITTING GROUNDED - YES. REAMED HOLES TRUE AND ROUND ON #4 STAB HINGE ARM, HFEC AND DVI OF PART NO DEFECTS NOTED REF ASA EA A320-55EA-01883 REV 00 NEW FITTING AND FASTENERS INSTALLED ON CUSTOMER CARD Jul 11, 2023 · N844VA · Airbus A320214
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