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 DL72S971820Web · crackedWEB CRACKED PAST STOP DRILL AT STA 1303 LT SIDE. INSIDE VERT STAB. REPAIRED PER SRM 53-10-4 FIG 17.Sep 12, 1997 · N528DA · Boeing 727232SDR CALA9701386Bracket · corrodedINSPECTION FOUND VERTICAL STABILIZER PANEL 374ER MOUNT BRACKET CORRODED. THE MOUNT BRACKET WAS REMOVED, A NEW MOUNT BRACKET WAS FABRICATED AND INSTALLED IAW SRM 51-31-01, 55-00-01, 55-32-01, AND 51-21-01.Sep 8, 1997 · N14090 · Doug DC1030SDR DL72S971692Stringer · cracked1.25 INCH CRACK IN VERT STAB S-9R AND SECOND BULKHEAD ABOVE CRAWL WAY OPENING. REPAIRED PER MM 55-30-0 PG 803.Aug 28, 1997 · N536DA · Boeing 727232SDR QXEA9700696Frame · crackedPDX - FRAME 58.5-2 CRACKED LEFT-HAND CORNER VERTICAL STAB BOX. REPAIRED IAW MM 53-10-5.Aug 12, 1997 · N490US · Fokker F28MK4000SDR QXEA9700623Angle · crackedPDX - LEFT CONNECTION ANGLE BETWEEN VERTICAL STABILIZER 1 CRACK AT 32 PERCENT. REPAIRED IAW F-28 MM 55-31-00 FIGURE 1.Aug 12, 1997 · N490US · Fokker F28MK4000SDR AALA971517Fitting · corrodedTUL - VERT STABILIZER CLOSURE RIB HORIZ FLANGE HAS .058 BLENDOUT AT LEFT TENSION TIE ATTACH BOLTHOLE, UNDER SIDE OF FLANGE IRREGULAR SURFACE WILL NOT ALLOW SEATING OF NUT AND WASHER. ACCOMPLISHED REPAIR PER ESO 11687 DATED 7/15/97. (M)Aug 8, 1997 · N867AA · Boeing 727223SDR HEEA0010569Fin Assy · corrodedFIN ASSY INSERTS CORRODED AND DRILLED CHIP ON FORWARD EDGE.Aug 6, 1997 · N5014Y · Bell 206L1SDR HEEA0010562Plate Assy · mis mfgMOUNTING BRACKET WILL NOT MOUNT TO BOTTOM OF VERTICAL FIN - (1) HOLE ALIGNMENT NOT SAME. (2) MOUNT BRACKET NOT WIDE ENOUGH TO ALLOW FOR RE-DRILLING.Aug 6, 1997 · Bell 206L1SDR HEEA0010540Spar Aft Fin · mis mfgMISMANUFACTURED PART. SPAR IS 1/16" NARROW AT LOWER END AND 1/8" NARROW AT TAIL ROTOR 90 DEGREE GEARBOX CASTING.Jul 31, 1997 · N7128R · Bell 412SDR DL72W971588Stringer · crackedSTRINGER CRACKED INSIDE VERT STAB ACCESS 9504 2ND BAY DOWN ON LEFT SIDE. REPAIRED PER M/M 55-30-0 FIG 803.Jul 29, 1997 · N295WA · Boeing 727247SDR CKSA97428Shear Tie · crackedDURING CPCP CHECK INSPECTION, FOUND INTERNAL VERTICAL STAB RIB NR 3 SHEAR TIE HAS SMALL CRACK AT STRINGER NR 8. REMOVED AND REPLACED SHEAR TIE IAW B727 SRM 51-10-1 AND 51-30-2. CORROSION TASK CARD NUMBER C55-395-10 PART 01 OF 01. NON-ROUTINE TASK CARD NUMBEJul 29, 1997 · N723CK · Boeing 727223SDR CALA9701179Bulkhead Web · crackedINSPECTION FOUND A 3 INCH CRACK IN BULKHEAD WEB PLATE AT STRINGER 7 AND RIB 8 OF LT SIDE OF VERTICAL STABILIZER INTERIOR. THE CRACKED PLATE WAS REMOVED, A REPLACEMENT PLATE WAS FABRICATED AND INSTALLED IAW SRM 51-40-2.Jul 26, 1997 · N45793 · Boeing 727232SDR DL72S971408Vert Stab · crackedAT MV2 FOUND STA 1303 CRACK, BULKHEAD, STA 1303 IN THE VERTICAL STAB, BOTH SIDES ARE CRACKED ON WEB. STOP DRILLED CRACKS AND FABRICATED DOUBLERS PER SRM 53-10-4 FIR 17. GOT OK TO INST DOUBLERS. REPAIRED BOTH SIDES PER SRM 53-10-4 FIG 17.Jul 15, 1997 · N477DA · Boeing 727232SDR CALA9701126Stringer · crackedVERTICAL STABILIZER INNER COMPARTMENT NR 6 RIB AND STRINGER 10 (LEFT) CRACKED 1. CUT OUT DAMAGED SECTION. FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH SRM 55-30-4.Jul 10, 1997 · N79748 · Boeing 727224SDR CALA9701049Angle · crackedINSPECTION FOUND A .25 INCH CRACK IN FORWARD RT INNER ATTACH ANGLE OF VERTICAL STABILIZER. THE ANGLE WAS REPLACED IAW SRM 51-30-2.Jul 2, 1997 · N937MC · Doug DC982SDR ABXA9701190Angle · crackedDURING C-CHECK, FOUND THE VERTICAL STABILIZER TO FUSELAGE RIGHT ATTACH ANGLE CRACKED. REMOVED AND REPLACED THE ANGLE IAW DC-9 SRM 53-05.Jul 1, 1997 · N931AX · Doug DC933FSDR ABXA9701189Angle · crackedDURING C-CHECK, FOUND THE VERTICAL STABILIZER TO FUSELAGE LEFT ATTACH ANGLE CRACKED. REMOVED AND REPLACED THE ANGLE IAW DC-9 SRM 53-05.Jul 1, 1997 · N931AX · Doug DC933FSDR W8PA970645Bushing · corrodedVERTICAL STABILIZER LEFT FORWARD MOUNTING LUG CLEVIS AFT BUSING HAS MIGRATED OUT OF CLEVIS LUG. HONED BORES TO REMOVE CORROSION, FABRICATED AND INSTALLED NEW BUSHINGS. (M)Jun 24, 1997 · N952WP · Boeing 7373B7SDR W8PA970779Bushing · corrodedVERTICAL STABILIZER AFT ATTACH LUGS AND CLEVISES HAVE CORROSION ON BUSHING FACES. REMOVED AND REPLACED BUSHINGS. (M)Jun 16, 1997 · N952WP · Boeing 7373B7SDR HEEA0010132Bracket · mis mfgMISMANUFACTURED. OPENING ON BRACKETS TOO SMALL TO RECEIVE HORN.Jun 16, 1997 · Bell 212SDR HEEA0010131Bracket · mis mfgMISMANUFACTURED. OPENING ON BRACKETS TOO SMALL TO RECEIVE HORN.Jun 16, 1997 · Bell 212SDR ABXA9701374Bracket · corrodedWHILE COMPLYING WITH 'D' INSPECTION, FOUND THE LOWER RUDDER HINGE BRACKET CORRODED. REPLACED HINGE BRACKET IAW DC-9 MM 20-16-0.Jun 12, 1997 · N962AX · Doug DC941SDR UPS97823715Fitting · crackedINSPECTION TYPE:D, VERT STABILIZER, 3RD FROM TOP RUDDER HINGE SUPPORT FITTING CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW SRM 51-3-0 AND DWG 5619438.Jun 11, 1997 · N819UP · Doug DC873FSDR 9712242290Angle · corrodedDURING M-CHECK, FOUND CORROSION ON ATTACH ANGLE FOR ACCESS PANEL 9601, FIN FS 225. REPAIRED PER EA 22-150346.Jun 11, 1997 · N290US · Boeing 727251SDR CALA9700925Angle · crackedINSPECTION FOUND A 1.5 CRACK IN VERTICAL STABILIZER LEADING EDGE INTERNAL ATTACH ANGLE, RT SIDE. THE CRACK WAS LOCATED JUST BELOW AFT SIDE OF PANEL CUTOUT NR 6301A. THE ATTACH ANGLE WAS REPLACED IAW EA 5340-01012 AND SRM 51-60-0.Jun 9, 1997 · N83872 · Doug DC982SDR CALA9700926Angle · crackedINSPECTION FOUND VERTICAL STABILIZER LEADING EDGE LEFT INTERNAL ATTACH ANGLE CRACKED IN HALF JUST BELOW AFT SIDE OF PANEL CUTOUT NR 6301A. A NEW ATTACH ANGLE WAS INSTALLED IAW SRM 51-30.Jun 6, 1997 · N83872 · Doug DC982SDR HEEA0010032Vertical Fin · defectiveVERT FIN STINGER IS NOT BONDED.Jun 4, 1997 · N2277A · Bell 206B3SDR HEEA0010031Fin Assy · corrodedFIN ASSY CORRODED BEYOND REPAIR.Jun 4, 1997 · Bell 206L1SDR HEEA0010027Fin Assy · crackedSEVERAL CRACKS NOTED IN FIN ASSY.Jun 4, 1997 · N3116P · Bell 206L3SDR CA970612011Bracket · seperated(CAN) WHILE INSPECTING THE VERTICAL FIN, A CRACKLING NOISE WAS NOTED. INSPECTION REVEALED A FINE CRACK BETWEEN THE BRACKETS.May 22, 1997 · Cessna 152SDR UPS97223038Tension Tie · corrodedINSPECTION TYPE:SI, VERTICLE FIN TENSION TIE RIB ALL SIX BUSHINGS ARE LOOSE AND MIGRATING. WHILE PREPARING RIB FOR REBUSHING HOLES FOUND HOLES TO BE CORRODED OUT OF LIMITS IAW EO 727-55-0071. REPLACED TENSION TIE IAW SRM 51-10-1, 51-30-2.May 21, 1997 · N914UP · Boeing 72727CSDR P2EA97048Bracket · misdrilledPAE - FOUND CHECK MAINTENANCE VISIT, PREEXISTING MIS-DRILLED HOLES TWO ON LEFT UPPER TANG BRACKET TO VERTICLE STAB. REPLACED LEFT UPPER AND LOWER TANG BRACKETS IAW MM 51-30-2. (M)May 20, 1997 · N204AU · Boeing 737247SDR P5CA9700917Fairing · crackedVERTICAL FIN L/E FAIRING 321A T/E DEFORMED. REFORMED FAIRING AND CRACK CHECK PER BOEING SRM 51-40-01 AND NOT MM 51-00-00.May 18, 1997 · N855FT · Boeing 747124SDR P5CA9700736Fairing · deformedVERTICAL L/E FAIRING 321A T/E DEFORMED. REPAIRED PER BOEING SRM 51-40-01.May 18, 1997 · N855FT · Boeing 747124SDR EISA97135Web · crackedDURING ROUTINE C-CHECK, FOUND TORN WEB AT UPPER END OF VERTICAL STABILIZER LEADING EDGE. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR PER SRM 51-30-02. (M)May 15, 1997 · N366PA · Boeing 727221SDR DL72S970947Stringers · crackedFOUR STRINGERS CRACKED IN THE VERT STABILIZER AT INBD RIB ATTACHMENT TABS. DAMAGED STRINGERS ARE AS FOLLOWS: STR 9R AT VERT STAB STA 180.6, STR 10L AT VERT STAB STA 133.8, STR 9R AT VERT STAB STA 157.2 AND STR 10L AT VERT STAB STA 180.6. STOP DRILLED CRACKSMay 14, 1997 · N8873Z · Boeing 727225SDR DL72W970919Stringer · crackedSTRINGER 8 CRACKED INSIDE VERT STAB RT SIDE FIN STA 133.800. REPAIRED PER M/M 55-30-0.May 13, 1997 · N2816W · Boeing 727247SDR DL72S970911Web · crackedINSIDE VERTICAL STAB AT FUSELAGE STA 1303 VERTICAL WEB CRACKED AT BOTH LOWER CORNERS. REMOVED T-ANGLE SUPORT AND ANTI-ICE DUCT TO GAIN ACCESS TO AREA. DRILLED OUT FASTENERS IN WEB REPAIR AREA. FABRICATED ROUGH DEMINSION DOUBLERS. INSTALLED DOUBLERS PER SRMMay 13, 1997 · N8873Z · Boeing 727225SDR DL72S970910Stringer · crackedSTRINGER 10, LT SIDE AT FIN STA 180.6 INSIDE VERTICAL STAB, 5TH BAY IS CRACKED. BEGAN M/M REPAIR PER M/M 55-30-0 FIG 803. INSTALLED REPAIR PER M/M 55-30-0 FIG 803.May 13, 1997 · N8873Z · Boeing 727225SDR DL72S970953Stringer · crackedSTRINGER FLANGE CRACKED INSIDE VERTICAL STRINGER 6L AT 2ND FROM TOP FRAME. FABRICATED REPAIR ANGLE PER M/M 55-30-0 PG 803. INSTALLED DOUBLER (REPAIR ANGLE) PER M/M 55-30-0, PG 803.May 8, 1997 · N526DA · Boeing 727232SDR UPS97223300Beam · corrodedINSPECTION TYPE:SI, WHILE PERFORMING TC NR 2231 (VERTICAL TAIL TIE BEAM SPLICE INSPECTION UPPER SPLICE) DISCOVERED SPLICE TO BE CORRODED AROUND BUSHING AREAS. REMOVED VERTICAL TAIL BEAM SPLICE FABRICATED AND INSTALLED NEW BUSHINGS PER MM 27-20-141.May 7, 1997 · N914UP · Boeing 72727CSDR HAIHEEA9817Stabilizer Assy · mis mfgSTAB ASSY INSERTS ON TOP AND BOTTOM INSTALLED IN WRONG SPOT.May 7, 1997 · Bell 206L1SDR DL72S970915Stringer · crackedFOUND AT MV2 IN ATL, CRACKED STR 10 LT SIDE AT FIN STA 133.8 INSIDE VERTICAL STAB, 3RD BAY UP. ACCOMPLISHED REPAIR PER M/M 53-30-0 FIG 803.May 6, 1997 · N8873Z · Boeing 727225SDR DL72S970899Stringer · crackedDURING MID VISIT, FOUND STRINGER CRACKED STR 9 RT SIDE AT FIN STA 157.2, INSIDE VERTICAL STAB 4TH BAY UP. REPAIRED PER M/M 55-30-0 FIG 803.May 6, 1997 · N8873Z · Boeing 727225SDR HAIHEEA9684Fin Assy · separatedFIN ASSY SEPARATED AT LOWER END AND OVER WEIGHT.Apr 30, 1997 · N81671 · Bell 206L3SDR HAIHEEA9649Fin Assy · corrodedFIN ASSY DENTED ON TRAILING EDGE. CORRODED AND SEPARATED.Apr 29, 1997 · N5017G · Bell 206L1SDR HAIHEEA9648Fin Assy · separationFIN ASSY SEPARATED ON TRAILING EDGE AND CORRODED.Apr 29, 1997 · N8590X · Bell 206L3SDR HAIHEEA9449Vertical Fin · separationSEPARATION ON TRAILING EDGE OF VERT FIN. NOT REPAIRABLE BY SI#206-2037 AT THIS STATION. SEPARATION IN AREA ALLOWING NO FIELD REPAIRS (FIG. 3-1 VIEW B PAGE 3-2 OF ABOVE SI#206-2037.Apr 19, 1997 · N5006F · Bell 206L1SDR 97ZZZX2358Drain Tube · cloggedA MODERATE AMOUNT OF REPAIR DEBRIS WAS FOUND AT THE BASE OF THE FIN AND A WATER LINE WAS SEEN ON THE FIN SKIN. THIS PROMPTED DISASSSEMBLY OF THE FIN DRAIN SYSTEM WHICH WAS CLOGGED COMPLETELY BY REPAIR DEBRIS. RUDDER TRIM AND ELEVATOR CABLES RUN THROUGH THIS Apr 15, 1997 · N193CS · Swrngn SA226TBSDR CALA9700696Channel · crackedINSPECTION FOUND A 1 INCH CRACK IN SUPPORT CHANNEL AT BASE OF VERTICAL FIN. A REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW SRM 53-10-2 AND 51-30-2.Apr 5, 1997 · N12235 · Boeing 737222
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