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 DALA2015122407710Scoop · crackedVERTICAL STABILIZER L/E, INLET SCOOP CRACKED TOP CENTER, NEXT TO WELD. WELDED IAW SRM 55-05.Dec 23, 2015 · N902DE · Doug MD88SDR WVER1212201590705Drag Angle · crackedRIGHT AFT DRAG ANGLE AT FUSELAGE TO VERTICAL STABILIZER ATTACHMENT POINT IS CRACKED APPROXIMATELY 1".Dec 12, 2015 · N907FJ · Cndair CL6002D24SDR DALA2015121007488Splice · looseLOOSE FASTENERS ON SPLICE OF L/E AT VERTICAL STABILIZER BS ZFS=52.26. ALL HOLES COUNTERSINK WERE MEASURED IAW CARD 5530-01045-05, STEP 2, JOB 055-0001 AND WAS FOUND OUT OF LIMITS, 49 EA. REPAIRED IAW CARD 5530-01045-08, STEP 1, JOB 167-0001 AND SRM 55-03D, Dec 9, 2015 · N992DL · Doug MD88SDR WVER2015120700004Drag Angle · crackedLEFT FORWARD DRAG ANGLE AT FUSELAGE TO VERTICAL STABILIZER ATTACHMENT POINT APPEARS TO BE CRACKED.Dec 7, 2015 · N907FJ · Cndair CL6002D24SDR WVER2015120700003Drag Angle · crackedRIGHT FORWARD DRAG ANGLE AT FUSELAGE TO VERTICAL STABILIZER ATTACHMENT POINT IS CRACKED APPROXIMATELY 1".Dec 7, 2015 · N907FJ · Cndair CL6002D24SDR DALA2015120807456Structure · damagedVERTICAL STABILIZER HAS NUMEROUS WORKING/SMOKING FASTENERS IN THE L/E. REPAIRED VERTICAL STABILIZER BY REMOVING DAMAGED AREA IAW SRM 55-30-01, REPAIR 7. FABRICATED REPAIR PART AND INSTALLED REPAIR PARTS IAW SRM 55-30-01, REPAIR 7.Nov 27, 2015 · N891AT · Boeing 717200SDR WVER1122201590402Drag Angle · crackedVERTICAL STABILIZER LT DRAG ANGLE IS CRACKED APPROXIMATELY 2". REPAIRED IAW REO 690-55-31-004, REV-A, DATED 2009-03-04.Nov 22, 2015 · N904FJ · Cndair CL6002D24SDR ASAA2015111313804Skate Angle · chafedVERTICAL STABILIZER PANELS 323BL, 323CL,AND 324AL LOWER SUPPORT ANGLE HAS CHAFING MARKS BETWEEN BS 1017 AND BS 1138, STR 2L AND 3L . ACFT GROUNDED. BLENDED AREA IAW SRM 51-10-02 & EA NG-55EA-03820, REV NEW FOUND TO BE OUT OF LIMITS AT BS 1124, ORIG .063 REMNov 13, 2015 · N615AS · Boeing 737790SDR I5EA201911071005Structure · handler errorDURING TOWING RH VERTICAL STABILIZER HIT ANOTHER AIRCRAFT. DAMAGE LOCATED BETWEEN FIN STATION 283.50 AND 209.90. RUDDER STATION 196.46 APPROXIMATELYOct 30, 2015 · N441US · Boeing 7374B7SDR ASAA2015102913805Angle · chafedVERTICAL STABILIZER PANEL 323AL, LOWER SUPPORT ANGLE HAS CHAFING MARKS BETWEEN BS 1005 AND BS 1016 ,STR 2L AND 3L. ACFT GROUNDED. BLENDED AREA IAW SRM 51-10-02 & EA NG-55-EA-03820, REV NEW FOUND TO BE OUT LIMITS AT BS 1005 ORIGINAL .063 REMOVED .011 REMAININOct 29, 2015 · N615AS · Boeing 737790SDR K11A2015120172601Web · corrodedCORROSION UPPER SURFACE OF HORIZONTAL WEB IN VERTICAL STABILIZER MAIN BOX BS 1337-1342.Oct 15, 2015 · N726CK · Boeing 7272M7SDR WVER201510100002Drag Angle · crackedLT AFT VERTICAL STABILIZER DRAG ANGLE IS CRACKED APPROXIMATELY .500" LONG. CRACKED AT AFT RADIUS.Oct 10, 2015 · N242LR · Cndair CL6002D24SDR WVER201510100001Drag Angle · crackedRIGHT AFT VERTICAL STABILIZER DRAG ANGLE IS CRACKED. DAMAGE APPROXIMATELY .750" LONG AT AFT RADIUS.Oct 10, 2015 · N242LR · Cndair CL6002D24SDR K11A201511047261Frame · crackedBULKHEAD IN VERTICAL STAB MAIN BOX HAS TWO INCH CRACK IN AFT END OF RT LOWER TEE CHORD.Oct 8, 2015 · N726CK · Boeing 7272M7SDR DALA2015100305939Hinge · damagedACFT HAS SCRATCHED BORE ON OTBD LUG AT LT VERTICAL STABILIZER HINGE WHERE ATTACH HORIZONTAL STABILIZER. SCRATCHED BORE ON OTBD LUG AT LT VERTICAL STABILIZER HINGE WERE ATTACH HORIZONTAL STABILIZER WAS REPAIRED IAW SRM 51-02, PAR. 6.Oct 2, 2015 · N987DL · Doug MD88SDR IPXA2015092994104Tee Fitting · crackedTEE FITTING CRACKED AT FWD LWR CORNER JUST AFT OF L/E RT SIDE VERTICAL STABILIZER. REPAIRED IAW EO B767-5530-58861-B.Sep 29, 2015 · N316UP · Boeing 76734AFSDR WVER092820150001Drag Angle · crackedLEFT FORWARD VERTICAL STABILIZER DRAG ANGLE IS CRACKED APPROXIMATELY 2.5" LONG.Sep 28, 2015 · N905J · Cndair CL6002D24SDR SCNA20150927133Structure · dentedVERTICAL STAB L/E LT SIDE APROXIMATELY 4 FEET FROM BOTTOM IS DENTED. REPAIRED VERTICAL STAB L/E LT SIDE.Sep 27, 2015 · N715SY · Boeing 737752SDR DALA2015092605837Angle · crackedCRACKED RT INNER ANGLE ON VERTICAL STABILIZER L/E BETWEEN BS 1401 - 1438. THE ANGLE WAS REPLACED IAW SRM 51-30-2, 51-30-5, AND DWG 5912188-RE BD.Sep 25, 2015 · N918DE · Doug MD88SDR DALA2015100505981Doubler · crackedVERTICAL STABILIZER L/E CRACKED IN AFT INTERNAL DOUBLER. R & R DOUBLER IAW SRM 51-00-01.Sep 24, 2015 · N951DN · Doug MD9030SDR DALA2015091005533Fastener · missingLOOSE AND MISSING FASTENERS, TWO ROWS ABOVE AND TWO ROWS BELOW THE SPLICE AT ZFS=52.267, LT/RT SIDE. FASTENERS WERE REMOVED AND FASTENERS WERE INSTALLED IAW SRM 51-30-1, REPAIR WAS ACCOMPLISHED IAW ETI-88-15-319, REV 2, ERA 477118-14AD, REV B.Sep 9, 2015 · N910DL · Doug MD88SDR DALA2015090905599Fastener · looseVERTICAL STABILIZER L/E AT THE SPLICE, ZFS=52-237 HAS LOOSE FASTENERS. REPAIRED IAW PRI/ERA 538746-14AD AND DWGSG09550004, REV D.Sep 8, 2015 · N955DN · Doug MD9030SDR COEA2015090318919Stop Fitting · corrodedHEAVY CHECK COE & MINOR REPAIR. STOP FITTING AT FWD BASE OF VERTICAL STAB HAS LEVEL 2 CORROSION. REPLACED WITH OEM PART.Sep 3, 2015 · N919FX · Aerosp ATR42300SDR DALA2015090205399Scoop · crackedACFT HAS A CRACK ON VERTICAL STABILIZER INTAKE AIR SCOOP LT SIDE APPROXIMATELY BS Y=1478. CRACK ON VERTICAL STABILIZER INTAKE AIR SCOOP LT SIDE APPROXIMATELY BS=Y=1478 WAS REPAIRED AND FPI WAS ACCOMPLISHED AND WELDED AREA OF INTAKE AIR SCOOP LT SIDE NO CRACKSSep 1, 2015 · N989DL · Doug MD88SDR DALA2015090705469Angle · crackedCRACKED LT AND RT INTERNAL DORSAL ANGLES BETWEEN JOIN OF VERTICAL STABILIZER L/E AND FUSELAGE SKIN BS 1418. THE ANGLE WAS REPLACED IAW SRM 51-30-2 AND DWG 5912188, REV BD.Aug 30, 2015 · N910DL · Doug MD88SDR WVER0821201500001Drag Angle · crackedRT SIDE, VERTICAL STABILIZER, DRAG ANGLE, CRACKED 3" LONG. PERFORMED REPAIR IAW REO 690-55-31-004, REV-A, DATED 2009-03-04.Aug 21, 2015 · N932LR · Cndair CL6002D24SDR DALA2015082005095Angle · crackedSTABILIZER SUPPORT STRUCTURE LT ANGLE CRACKED. REMOVED ANGLE, REPLACEMENT ANGLE WAS FABRICATED FROM .090, 7075-0, HEAT TREATED TO T6 CONDITION. ON RO 702799 IAW DWG 9911808, DRILL AND TRIMMED ANGLE. TREATED AND PAINTED. INSTALLED NEW ANGLE ALL FASTENERS SECAug 18, 2015 · N936DL · Doug MD88SDR DALA2015082005094Angle · crackedDURING JACKSCREW INSPECTION FOUND VERTICAL STABILIZER SUPPORT STRUCTURE RT ANGLE CRACKED. ANGLE WAS FABRICATED FROM .090 7075-0 AND HEAT TREATED TO T6 ON RO 702799 IAW DWG 9911808. TREATED AND PAINTED. INSTALLED NEW ANGLE ALL FASTNERS SECURED REF SRM 51-30-Aug 18, 2015 · N936DL · Doug MD88SDR DALA2015073104780Splice · looseL/E SPLICE, ZFS= 52.267, LT SIDE HAS 37 LOOSE FASTENERS. REMOVED LOOSE FASTENERS. CLEANED AND CHECKED HOLES. OK IAW DWG SG09550004, REV D.Jul 30, 2015 · N954DN · Doug MD9030SDR DALA2015073104779Splice · looseL/E SPLICE, ZFS= 52-267, RT SIDE HAS 27 LOOSE FASTENERS. REMOVED LOOSE FASTENERS. CLEANED AND CHECKED HOLES IAW DWG SG09550004, REV D.Jul 30, 2015 · N954DN · Doug MD9030SDR DALA2015072404631Angle · crackedCRACKED LT AND RT INTERNAL DORSAL FIN ANGLES BETWEEN STA Y=1401-1418 AT VERTICAL STABILIZER ROOT. INTERNAL DORSAL FIN ANGLES BETWEEN BS Y=1401 TO Y=1418 AT VERTICAL STABILIZER ROOT WERE REPLACED IAW SRM 51-30-5. CRACK LENGTH: 1.125".Jul 22, 2015 · N988DL · Doug MD88SDR DALA2015071904472Angle · crackedCRACKED ANGLE BETWEEN VSS 2 - 26 TO -15 AT VERTICAL STABILIZER INNER STRUCTURE. THE ANGLE WAS REPLACED IAW SRM 51-30-05, 51-30-2, 51-10-3 PAR 21 AND 14 SRM 51-10-2 AND DWG 5912188, REV BD.Jul 18, 2015 · N984DL · Doug MD88SDR DALA2015071504389Support Angle · crackedDURING JACKSCREW INSPECTION FOUND RT VERTICAL STABILIZER STRUCTURE CRACKED. REMOVED RT VERTICAL STABILIZER SUPPORT ANGLE. THE SUPPORT ANGLE WAS FABRICATED, HEAT TREATED, DRILLED AND INSTALLED IAW DWG 9911808 AND SRM 51-30-04.Jul 14, 2015 · N932DL · Doug MD88SDR DALA2015071504388Support · crackedDURING JACKSCREW INSPECTION, FOUND LT VERTICAL SUPPORT STRUCTURE CRACKED. REMOVED LT VERTICAL STABILIZER SUPPORT STRUCTURE, CLIP, REPLACEMENT CLIP WAS FABRICATED. DRILLED, PAINTED AND INSTALLED IAW DWG 9911808 AND SRM 51-30-04 AS A REF.Jul 14, 2015 · N932DL · Doug MD88SDR ASOA20150714147Drag Angle · crackedDURING C-CHECK, THE LT DRAG ANGLE AT THE BASE OF THE VERTICAL STABILIZER WAS FOUND TO BE CRACKED. MAINTENANCE R & R THE ANGLE IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Jul 14, 2015 · N14198 · Emb EMB145XRSDR DALA2015071104292Angle · crackedCRACK ON LT VERTICAL STABILIZER DORSAL ANGLE. ANGLE DORSAL WAS REMOVED IAW SRM 51-30-2 AND 51-30-5, NEW ANGLE DORSAL WAS DRILLED AND ADJUSTED IAW SRM 51-10-4, NEW ANGLE WAS INSTALLED IAW SRM 51-30-2 AND 51-30-5.Jul 10, 2015 · N904DL · Doug MD88SDR DALA2015070604125Skate Angle · crackedVERTICAL STABILIZER LT SKATE ANGLE CRACKED. DOUBLER REPAIRED IAW SRM 55-30-05.Jul 5, 2015 · N949DN · Doug MD9030SDR DALA2015070704277Support Channel · crackedVENTRAL STABILIZER ACTUATOR SUPPORT CHANNEL CRACKED. REPAIRED IAW PRI ERA 537315-14.Jul 4, 2015 · N901DA · Doug MD9030SDR 2015FA0000308Nut · misinstalledDURING SB505-55-0003 COMPLIANCE, THE RT FORWARD VERTICLE STABILIZER TO FUSELAGE FRAME 43, ATTACH BOLT BARREL NUT WAS FOUND INSTALLED FROM THE FACTORY UPSIDE DOWN. THIS RESULTED IN WEAR DAMAGE TO THE UPPER SURFACE OF THE BARREL NUT HOLE IN FRAME 43 CAUSED BY CJul 1, 2015 · N14AH · Emb EMB505SDR VNAA2015062900028Drag Angle · crackedRIGHT VERTICAL STAB FORWARD DRAG ANGLE CRACKED. REPAIRED DRAG ANGLE IAW REO.Jun 29, 2015 · N725PS · Cndair CL6002C10SDR VNAA2015062900027Drag Angle · crackedLEFT VERTICAL STABILIZER FWD DRAG ANGLE CRACKED. REPAIRED IAW REO.Jun 29, 2015 · N725PS · Cndair CL6002C10SDR AALA201506239003Hinge Fitting · excess play3S CHECK, EXCESSIVE PLAY ON NR 2 RUDDER HINGE FITTING ON VERTICAL STABILIZER. REPLACED NR 2 RUDDER HINGE FITTING ON VERTICAL STABILIZER IAW SRMA 319 51-42-11 & AMM 55-36-41-0401.May 27, 2015 · N701UW · Airbus A319112SDR SWIA201541299Panel · crackedAFT DORSAL STRAKE FAIRING PANEL 321CT CRACK ON AFT SECTION. REPAIRED CRACK IN AFT SECTION OF THE AFT DORSAL STRAKE FAIRING PANEL 321CT IAW STS EA.May 20, 2015 · N708SK · Cndair CL6002C10SDR DALA2015052403511Structure · crackedCRACKED FLANGE ON VERTICAL FIN NEAR BS 1475. R & R FORMER AND DOUBLER IAW DWG 5910242.May 20, 2015 · N948DN · Doug MD9030SDR DALA2015051403265Structure · damagedFOUND FASTENER HOLE ON UPPER ROW COMMON TO SPLICE BAND FROM LT SIDE OF VERTICAL STABILIZER FIXED L/E TO BE OUT OF LIMITS. STA ZFS 52.267, C/W PRI 535916-14, REV 1 AND ER/A 535916-14AD, REV ORIGINAL, LP 1946704.May 14, 2015 · N916DE · Doug MD88SDR 5HAS2015FA0000199Bolt · shearedAIRCRAFT WAS RECEIVED FOR IT'S SCHEDULED 100 HR INSPECTION, UPON COMPLETION OF THE PRELIMINARY INSPECTION THE FIN ATTACH BOLT AN4-6A THAT IS INSTALLED VERTICALLY THROUGH FITTING, PN: 0431009-3 WAS FOUND SHEARED. THE NUT AND SHANK OF THE BOLT WAS STILL PRESENTMay 12, 2015 · N64895 · Cessna 152SDR DALA2015051103260Structure · damagedFOUND 20TH FASTENER HOLE ON UPPER ROW COMMON TO SPLICE BAND FROM LT SIDE OF VERTICAL STABILIZER FIXED L/E TO BE OUT OF LIMITS. FS ZFS 52.267. REPAIRED THE BUSHINGS IAW ERA 535916-14.May 10, 2015 · N916DE · Doug MD88SDR DALA2015051103253Angle · crackedCRACK ON RT ANGLE TO ATTACH INTERNAL VERTICAL STABILIZER BETWEEN FS 1458-1486, LONGERON 1R-2R. ANGLE WAS REMOVED, FABRICATED AND INSTALLED IAW SRM 51-30-02 AND 51-30-05. LP 1942008.May 10, 2015 · N935DN · Doug MD9030SDR DALA2015051103252Angle · crackedCRACK ON LT ANGLE TO ATTACH VERTICAL STABILIZER INTERNAL BETWEEN, STA 1458-1486, LONGERON 1L - 2L. ANGLE WAS REMOVED, FABRICATED AND INSTALLED IAW SRM 51-30-02 AND 51-30-05. LP 1942004.May 10, 2015 · N935DN · Doug MD9030SDR SWAA2015051139555Tail Cone · delaminatedRIGHT SIDE OF VERTICAL STABILIZER DELAMINATED TAIL CONE AREA. REPAIRED TAIL CONE IAW SRM.Apr 28, 2015 · N942AT · Boeing 717200
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